TECHNICAL REPORT
ANALYSIS OF AIRCRAFT EXHAUST
EMISSION MEASUREMENTS
By: Leonard Bogdan and H.T. McAdams
CAL No. NA-5007-K-1
Prepared For:
ENVIRONMENTAL PROTECTION AGENCY
DIVISION OF EMISSION CONTROL TECHNOLOGY
CHARACTERIZATION & CONTROL DEVELOPMENT BRANCH
ANN ARBOR, MICHIGAN 48103
Contract No. 68-04-0040
October 15, 1971
CORNELL AERONAUTICAL LABORATORY, INC.
OF CORNELL UNIVERSITY, BUFFALO, N. Y. 14221
-------
The work upon which this publication is based was
performed pursuant to Contract No. 68-04-0040 with the
Environmental Protection Agency.
-------
CORNELL AERONAUTICAL LABORATORY, INC.
BUFFALO, NEW YORK 14221
ANALYSIS OF AIRCRAFT EXHAUST
EMISSION MEASUREMENTS
By: Leonard Bogdan
H.T. McAdams
CAL Report No. NA-5007-K-1
Contract No. 68-04-0040
October 15. 1971
Prepared For:
ENVIRONMENTAL PROTECTION AGENCY
DIVISION OF EMISSION CONTROL TECHNOLOGY
CHARACTERIZATION & CONTROL DEVELOPMENT BRANCH
ANN ARBOR, MICHIGAN 48103
PREPARED BY:
/"i
Leonard Bogdan '
Principal Research Engineer
Vehicle Research Department
APPROVED BY:
K.D. Bird, Head
Vehicle Research Department
A/. "T
H.T. McAdams
Principal Research Engineer
Systems Research Department
/?. 2>.O'^.^_
A.D. O'Connor, Head
Systems Research Department
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TABLE OF CONTENTS
ANALYSIS OF AIRCRAFT EXHAUST EMISSION MEASUREMENTS
Page
FOREWORD iii
ACKNOWLEDGEMENT iv
ABSTRACT v
LIST OF SYMBOLS vi
Part 1 TECHNICAL REPORT 1-1
1.1 Introduction 1-2
1.2 Methodology of Data Analysis 1-3
1.2.1 General Comments 1-3
1.2.2 Detailed Procedure 1-4
1.3 Statistical Analysis 1-21
1.4 Presentation of Results 1-22
1.5 Discussion 1-25
1.6 Summary 1-32
1.7 References 1-33
Appendix A - Span-Gas Checks of Test Organizations'
Instrumentation A-l
Part 2 SUMMARY OF DATA 2-1
2.1 Data Treatment and Commentary 2-2
2.1.1 Piston Engines 2-2
2.1.1.1 Scott Research Laboratories 2-2
2.1.1.2 Teledyne Continental Motors 2-4
2.1.2 Auxiliary Power Units - AiResearch 2-6
2.1.3 Turbine/Turboprop Engines 2-8
2.2 Tabulated Results 2-12
Table I Piston Engines (Scott) 1-1
Table II Piston Engines (Continental) II-l
Table III Auxiliary Power Units (AiResearch) III-l
Table IV Turbine/Turboprop Engines IV-1
Table V Reprocessed Data V-l
ii
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FOREWORD
This report was prepared by Cornell Aeronautical Laboratory, Inc.
(CAL), Buffalo, New York under Environmental Protection Agency (EPA) Contract
No. 68-04-0040. The work was administered under the direction of the Office
of Air Programs, Characterization £ Control Development Branch, Division of
Emission Control Technology, Mr. Barry D. McNutt, Project Officer.
This is the Phase I Technical Report that describes and summarizes
the results of studies conducted during the period from June 1971 through
September 1971 to translate field-measurement data on aircraft engine emissions
into a format useful for the promulgation of realistic standards. The basic
input data were supplied by the EPA.
The effort was performed jointly by the Vehicle Research Department
and the Systems Research Department of CAL. Acknowledgement is made of the
significant technical contributions to the program by P. A. Reese and G. D.
Higgins who were responsible for computer programming. A special note of
acknowledgement is in order for Mrs. A. Guendel, Mrs, S. J. Sweet and
Mr. J. E. Blickenstaff who so ably performed the operational functions of
data logging and transciption, curve fairing and related tasks. R. A Grom
and his staff merit recognition for prompt and efficient response to
digitization requirements in the context of meeting crucial program deadlines.
111
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ACKNOWLEDGEMENT
The Office of Air Programs, Environmental Protection Agency, would
like to acknowledge valuable assistance (in terms of time, manpower and
material) received from the following organizations in gathering the data
in this report.
American Airlines, Overhaul Facilities, Tulsa, Oklahoma.
TWA, Overhaul Facilities, Kansas City, Missouri.
United Airlines, Overhaul Facilities, San Francisco, California.
United States Air Force, Kelly Air Force Base, San Antonio, Texas.
United States Navy, Naval Air Rework Facility, Norfolk, Virginia.
United Aircraft, Pratt and Whitney Aircraft Division, East Hartford,
Conn.
General Motors, Detroit Diesel Allison Division, Indianapolis,
Indiana.
Garrett Corporation, Air Research Manufacturing Company of
Arizona, Phoenix, Arizona.
Continental Teledyne, Muskegon, Michigan.
Department of Transportation, Federal Aviation Administration.
Air Transport Association.
Aerospace Industries Association.
U.S. Bureau of Mines, Bartlesville Energy Research Center,
Bartlesville, Oklahoma.
Southwest Research Institute, Vehicle Emission Laboratory,
San Antonio, Texas.
Scott Research Laboratories, Plumsteadville, Pennsylvania.
Office of Air Programs, DECT, Test and Evaluation Branch,
Ypsilanti, Michigan.
Cornell Aeronautical Laboratory, Buffalo, New York.
IV
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ABSTRACT
An account is presented of the analytical procedures and data
processing techniques employed in translating field-measurement data of
aircraft exhaust emissions into a form consistent with the needs for the
promulgation of realistic standards. Pollutant mass emissions for carbon
monoxide (CO) hydrocarbons (HC) and the oxides of nitrogen (NO ) are computed
A
for an aircraft operational cycle comprised of the following modes: taxi/idle,
take-off, climb out and approach. The calculations are for specific engine
power (or thrust) settings for each mode as well as for specified times in
mode. Numerical results are tabulated for each individual engine tested
together with summaries obtained by aggregating engine data on a model basis.
Data are presented for turboprop/turbine engines, light-utility piston engines
and auxiliary power units'.
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LIST OF SYMBOLS*
CO = concentration of CO in exhaust, ppm
COz = concentration of CO- in exhaust, o/o
F = mass rate of fuel flow, Ib/hr
MC = concentration of hydrocarbons in exhaust, ppmC
Mx = molecular weight of "x" (NL, = 1.008
NO = concentration of NO in exhaust, ppm
NOZ = concentration of N0? in exhaust, ppm
NOX = concentration of NO + N02 in exhaust, ppm
MT = mass emission rate of component "x", Ib/hr
& = atomic hydrogen-carbon ratio of fuel
*
As used in equations in test of Part 1 of this report unless otherwise noted
in the context.
VI
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Part 1
TECHNICAL REPORT
1-1
-------
1.1 INTRODUCTION
The constituent components of the exhaust emissions resulting from
aircraft operations include the same pollutants produced by highway vehicular
traffic as well as certain other sources of pollutants, and thus play a
similar role in the general air pollution problems. While aircraft exhaust
emissions presently are considered to constitute a small portion of the total
atmospheric pollution burden of a community (Ref. 1), the relative proportion
of this burden is expected to increase in the future because of (a) the
continuing development of technology for successfully decreasing emissions
from highway vehicles and (b) the anticipated growth in the number of aircraft
and aircraft operations in the next decade. It is the more tangible evidence
of the aircraft emissions in the form of smoke and odors that has generated a
reaction from the public. That aircraft exhaust emissions constitute a
segment of the general air pollution problem that warrants a technically-
based assessment is manifest.
Recognition of the dimensions of these problems at the federal level
of government is reflected by the passage of an Act cited as the "Clear Air
Amendments of 1970". This act specifically directed the initiation of a
study to determine the effects of aircraft emissions on air quality, the
technological feasibility of controlling such emissions and, finally, the
issuance of proposed emission standards. In compliance with the last of these
directives, the EPA instituted a broadlyAbased experimental program to measure
the exhaust emissions from aircraft engines currently used in the commercial,
military and general aviation sectors that comprise the aviation scene within
the country. Auxiliary power units (APU) were also included within the scope
of this effort. These basic or "raw" measurements consisted of data on
emission concentrations together with pertinent information on engine
maintenance history, engine settings and ambient conditions during test.
These data were forwarded to CAL for processing and analysis directed to the
ultimate objective of producing a statistical format conducive to the promulga-
tion of realistic standards. Numerical specifications for typical operational
1-2
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landing-take-off (LTO) cycles for the various model engines were provided
by the EPA.
Part 1 of this report discusses the methodology adopted at CAL for
processing the input data and presents the rationale underlying the selection
of the specific analytical procedures. The objective was to generate an
output in the form of a set of best estimates, comprising a mean value
supplemented by a measure of statistical dispersion, for emissions for specific
engines, specific categories of operational modes and other applicable
constraints. The end purpose of this analysis was the establishment of a
rational basis for specifying engine exhaust emission standards. An additional
objective involved the identification and possible isolation of the sources of
variability in engine emissions and, to the maximum extent possible with the
available data, the appraisal of the relative importance of the sources.
Results of these latter studies will be incorporated in a separate report to
be published during November 1971.
Summaries of the numerical data and the results obtained for light-
utility piston engines, auxiliary power units and turboprop/turbine engines
are included in Part 2. Because each of these engine categories required a
unique analytical procedure in data treatment, a brief description of these
procedures, together with pertinent observations, precedes the set of data
sheets.
The test data presented represent a complete inventory of all of the
pertinent information received by CAL.
1.2 METHODOLOGY OF DATA ANALYSIS
1.2.1 General Comments
The specific methods and details pertinent to the data processing and
the analytical procedures that are described constitute an attempt to best
adjust the methodology to the ultimate objectives and the nature of the input
1-3
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data supplied for processing. In this respect a learning cycle was involved
with the methodology subject to adjustment as the results from the processing
of the initial quantities of test data were assessed (the field data were
received at CAL in a piecemeal fashion). The unique flexibility and advantages
realized by virtue of those methods ultimately selected is made apparent in
the succeeding discussion.
For reasons that will be clarified later, different methodologies
for data analysis were required for each of the following categories of
engines: (a) thrust turbines and turboprops, (b) piston engines and (c)
auxiliary power units. Even within these general categories there were
further variations in the manner of processing as dictated by the type of
data which were provided. All of these factors are discussed in detail in
their appropriate places in this report. Because of the high level of
interest of the EPA in the commercial thrust turbines and turboprops, this
engine category was the object of the most extensive data processing. Also,
the major portion of all tests submitted for analysis were in this category.
For example, this report contains data on a total of 392 engine tests comprised
of 199 turbine/turboprop tests, 140 piston engine tests and 53 tests on APU's,
A concise overview of the entire set of operations comprising data
processing and analysis is obtained by reference to the flow chart of Figure 1.
In its entirety, this flow chart is applicable only to the analysis performed
upon data for turboprop and turbine (commercial) engines. Certain portions
of the flow chart operations were common to other engine categories as well
(for example, data for all categories of engines was at least coded and
keypunched). The following descriptive summary faithfully follows the sequence
of the flow chart.
1.2.2 Detailed Procedures
Editing
Upon arrival at CAL, the primary data sheets were logged and examined
for completeness of information, consistency of parameter dimensions and
1-4
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RAW DATA
STANDARD
FORMAT?
CONVERT TO MASS
EMISSION RATES
PLOT DATA VIA LDX FOR:*
(1) LB. CO/LB. FUEL VS % RATED THRUST
(2) LB. HC/LB. FUEL VS % RATED THRUST
(3) LB. NOX/LB. FUEL VS % RATED THRUST
(4) FUEL FLOW VS % RATED THRUST
i
in
DIGITIZE
FAIRED
CURVES
ENGINE MODE
T OR HP. SETTINGS
INTERPOLATE
FOR
SELECTED MODES
TIME 1
IN MODES
COMPUTE EMISSIONS
FOR LTO CYCLE
FOR TURBOPROPS THE %
RATED TAKEOFF HORSE-
POWER IS USED.
PERFORM
STATISTICAL
ANALYSIS
.> EXPECTED (MEAN) VALUES
AND STANDARD DEVIATIONS
Figure 1 FLOW CHART - DATA PROCESSING AND ANALYSIS - TURBINE AND TURBOPROP ENGINES
-------
reasonableness of the data. Where feasible, the necessary dimensional
conversions and calculations were made; otherwise, missing information was
obtained, if possible, by contacting the testing organization. A complete
listing of testing organizations, the geographical location of the respective
test sites and the types of engines tested at each is shown in Table 1.
At this stage of the process the rated take-off power or thrust
setting for each engine was entered since, as will be demonstrated, this
parameter represents the common base against which the exhaust emissions and
engine fuel flow were plotted.
Format
As shown in the flow chart, the primary data supplied by the various
test organizations were to have been presented in a standard format devised by
the EPA. Standard format sheets for the turbine engines and piston engines
are shown in Figures 2 and 3 respectively. In the majority of the cases,
however, the data received departed in varying degrees from the standard
sheet, both in format and in the actual data content supplied. For example,
relevant information such as engine history data, data on ambient conditions
and pollutant emissions often were lacking. Most troublesome of all were
those numerous cases in which certain elements of information essential to
data reduction and analysis were missing. As an example, thrust data was not
always given for all test modes, and in some cases, CO^ concentrations were
not recorded. In addition, there were inconsistencies in the basis of reporting
pollutant concentrations, whether wet or dry basis, whether hydrocarbons were
recorded as methane or as carbon, and whether all units of measurement were
consistent throughout. A significant amount of time and effort was consumed,
therefore, in editing the received data, in attempting to retrieve missing
information, and in modifying the format to a sufficient extent to make it
* '
compatible with established processing procedures. In many cases, such
*
Keypunch operators had been pre-trained to work directly from data entered
on the standard format sheets.
1-6
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Table 1
SUMMARY OF SOURCES OF EMISSIONS MEASUREMENTS
TEST ORGANIZATION
PRATT AND WHITNEY AIRCRAFT
DETROIT DIESEL ALLISON DIV.
TELEDYNE-CONTINENTAL
AIRESEARCH
BUREAU OF MINES
EPA TEAM
SOUTHWEST RESEARCH INSTITUTE
SCOTT RESEARCH LABORATORIES
TEST SITE
E. HARTFORD, CONN.
INDIANAPOLIS. IND.
MUSKEGON, MICH.
PHOENIX. ARIZ.
AMERICAN AIRLINES MAINTENANCE
AND ENG'RG. CENTER TULSA, OKLA.
UNITED AIRLINES
SAN FRANCISCO. CALIF.
KELLY AFB. TEXAS
TWA. KANSAS CITY, MO.
NORFOLK, NAS. VA.
GENERAL AVIATION AIRPORTS
TYPE ENGINES TESTED
JT3D, JT8D, JT9D - TURBINES
(EXPERIMENTAL AND
PRODUCTION TYPES)
T56 (PRODUCTION TYPES) -
TURBOPROPS
LIGHT UTILITY, GENERAL
AVIATION - PISTON
AUXILIARY AND SMALL
PROPULSION UNITS
JT3D, JT8D. R-R SPEY -
TURBINES
JT3C, JT3D, JT4A, JT8D -
TURBINES
T56 - TURBOPROPS, J79 -
TURBINES
JT4A. JT3D, JT8D, CJ805 -
TURBINES
J52, J57, TF30 - TURBINES
LIGHT UTILITY - PISTON
TYPE EMISSION MEASUREMENT
ALL EMISSIONS WET
CO. CO2, NOX - DRY
HC - WET
CO, NO - DRY
HC WET
ALL EMISSIONS WET
ALL EMISSIONS WET
ALL EMISSIONS WET
ALL EMISSIONS - WET
ALL EMISSIONS WET
ALL EMISSIONS - DRY
ALL EMISSIONS - DRY
-------
Figure 2 a
AIRCRAFT EMISSIONS BASELINE DATA SHEET
Date:
Sheet No.
of
Sheets
Test Organization,
Engine Supplier
Individual in Charge
Engine Data:
Engine Serial No.*
Engine Type and Model_
Engine Total Time, hrs.
"Time Since Hot Section Overhaul," hrs.**_
Time Since:
N-| Compressor Overhaul, hrs.
Compressor Overhaul, hrs._
Combustor Can Replacement, hrs., (indicate part number)
Overhaul, hrs. , N^ Turbine Overhaul, hrs.
Overhaul, hrs
Fuel Fuel H/C Ratio
, First Stage Nozzle Guide Vane
, N Turbine
Operational Data:
Inlet Air Temperature, °F: Start
Atmospheric Pressure: Start
, Finish
, Finish
Inlet Air Humidity, Ibs, H20/lb. dry air
Relative Humidity
Sample Line: Temperature, °C , Flow rate, liters/min.
Sample Line Transport Time, sec.
'Attach engine history sheet as appropriate.
**A.A. - Time Since Hot Section Inspection, TWA - Time Since Hot Section Maintenance,
U.A. - Time Since Engine Heavy Maintenance, also may refer to time since hot section was
brought to "zero" time; give your interpretation of your entry as necessary.
Comments:
1-8
-------
Figure 2 b
i
to
Test
Time
Mode
Power
Thrust,
Ibs. or
Shp.
%Max.
Engine
Speed
(RPM)
N1
N2
Measured
Fuel
Flow
(Ib/hr)
Gas
Generator
Air Flow
(Ib/sec)
Calcu-
lated
F/A
Compressor
Discharge
Temp.
(°F)
Engine
Pressure
Ratio,
EPR
Turbine
Inlet
Temp.
(°F)
Exhaust
Gas
Temp.
TT? (OF)
Exhaust
Gas
Pressure,
Pj psia
-------
Figure 2 c
CO (Wet)
ppmV
CO2 (Wet)
%V
THC (Wet)
ppmV C
NO (Wet)
ppmV
NO2 (Wet)
ppmV
NOX (Wet)
ppmV
Aldehydes (Wet)
ppmV
Smoke
Particulates
-------
Figure 3 a
AIRCRAFT EMISSIONS BASELINE DATA - PISTON ENGINES
Date:
Sheet No.
of
Sheets
Test Organization_
Engine Supplier
Individual in Charge.
Engine Serial No.*_
Engine Type and Model.
Engine Total Time, hrs..
Time Since Last Engine Overhaul, hrs..
Fuel
Inlet Air Temperature, °F: Start.
Atmospheric Pressure: Start
, Finish.
_, Finish
Inlet Air Humidity, Ibs. h^O/lb. dry air.
Relative Humidity
Sample Line: Temperature, °C
Flow Rate, liters/min
Sample Line: Transport Time, sec.
'Attach engine history sheet as appropriate.
Comments:
1-11
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Figure 3 b
i
ti
Is)
Test
Time
Mode
Carbu-
retor
Heat
Power
%Max.
Engine
Speed
(RPM)
Intake
Manifold
Pressure
(in. Hg)
Measured
Fuel
Flow
(Ib/hr)
Air
Flow
(Ib/hr)
Calcu-
lated
F/A
Exhaust
Gas
Temp.,
(°F)
CO
(Wet)
ppmV
C02
(Wet)
%V
THC
(Wet)
ppmV C
NO
(Wet)
ppmV
NO2
(Wet)
ppmV
NOX
(Wet)
ppmV
Aldehydes
(Wet)
ppmV
-------
modification was not possible; a complete transcription of the data into
standard sheets was necessitated.
Coding and Key Punching
Once the data were edited to a sufficient extent to be useable in
the analysis process, these data had to be coded and key punched for entry
into subsequent computer processing. Coding consisted of such matters as
assigning serial numbers to engine models, fuel types, testing organizations
and engine suppliers by which they could subsequently be identified, identifying
the various pollutants by an appropriate code, and assigning a sequence of
numbers to the various power settings in a test in such a way that the several
test points could retain their time sequence identity in subsequent processing.
In addition pertinent comments related to the particular test (such as presence
of retrofits on the engine, use of fuel additive, unusual test problems, etc.)
were encoded. The data was then key punched in a format which allowed re-
trieval of substantially all the information received from any one test
organization.
Conversion of the Data
As seen by reference to the data sheets shown in Figures 2 and 3,
all of the pollutant emissions were given in terms of concentrations, either
as parts per million by volume or as a percentage volume. A more useful and
meaningful quantity for data analysis is the mass emission rate of the
pollutant.
Equations for converting concentration data into mass emissions data
were derived from the basic chemical equation for the combustion of a hydro-
carbon fuel in air. The details of this derivation will not be included in
this report. Instead, only the final conversion formulae will be documented
with the observation that they are in general accord with those given in
Ref. 2. The pertinent equations are listed below:
1-13
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M C0 F
M
(M
c H > to*
(3)
The above equations were programmed for the IBM 370/165 computer
to perform the data conversion. To utilize these particular equations, the
emission concentrations must be expressed on a wet (or actual) concentration
basis. Since some of the input data received were measured on a dry basis
(see Table 1 for details), appropriate corrections to these data were necessary,
Correction simply involves the multiplication of the dry concentration data
by a correction factor to obtain the required wet concentration data. The
appropriate equations that define the correction factors are listed below:
a. CO and CO,, are measured on a wet basis, N() on a dry
basis and NO to be converted to a wet basis
(K = correction factor)
*
In this report the hydrocarbon mass emissions are always given in terms of
methane, NL = 16.04.
1-14
-------
b. All measurements are on a dry basis
1OO
In both cases, the correction is for the water of combustion.
One observation common to all of the preceding equations is that the
carbon dioxide component is overwhelmingly dominant in terms of the concentra-
tions and mass rate emissions among all the effluents.
Data Plotting
Following the conversion of CO, HC and NO concentration data to
mass emission rates, a set of four plots was made for each turbine and turbo-
prop engine tested by means of Long Distance Xerography (LDX) .
The Xerox LDX plotter is basically a combination of the Xerox
process (light-sensitive electrostatic drum) and a flying-spot scanner. The
beam of the cathode-ray tube in the LDX plotter has discrete beam locations
addressable in two coordinates. The output of the plotter is recorded on
paper strip 8-1/2 inches wide. The usable width for recording purposes is
7.82 inches. This width accommodates 1024 discrete addressable locations
separated by 1/131 inch. Along the length of the paper strip, the same
distance between addressable locations applies, but recording can be carried
out continuously up to a total length of 2000 feet, the length of the roll of
paper. In practice, the paper is usually cut into 11-inch lengths to provide
standard-sized 8-1/2 inch by 11-inch sheets. For present purposes it was
found convenient to use a standard 5-inch by 5-inch plot and to scale the
data in such a way as to conform to this standard format. For thrust-rated
engines, each measured thrust value in the test was expressed as a percentage
of the take-off thrust rating for the engine, and these normalized thrust
1-15
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values were used as the abscissae for the LDX plots. Three of the plots in
the series employed pounds of pollutant per thousand pounds fuel as ordinates.
The other one showed the relation between thrust and fuel flow. By means of
the LDX process, the points were plotted and displayed very rapidly. Continuous
curves were faired (manually) to these points for subsequent interpolative use.
One major advantage of this approach was that the plots made evident any
discrepancies in the data and thus introduced an additional control on the
quality of the data included in the final analysis of emissions. This approach
also provided a means whereby engineering judgment could be brought to bear on
the problem, especially where data were sparse in some regions of the curve.
Purely analytical methods such as least-squares curve fitting would not have
permitted this interpretive process.
Curve Fairing
Fairing of the LDX plots was purely a manual procedure. The normal
process involved a visual scanning of a large quantity of plots for a given
type engine to help define the general shape of the various curves. This
knowledge proved useful in the fairing process in those test situations where
data points were sparse, missing or poorly spaced. The plots for HC and CO
generally approximate an equilateral hyperbola with a sharp "knee" just above
the idle/taxi thrust settings. Unfortunately much of the initial test data
obtained had very few points in this critical region in the 10% to 30% range
*
of rated power or thrust. By relying on data from those test runs where
adequate data were available to reliably define the shape of the entire curve,
it was possible to fair (and use) the data from tests where a poor spacing of
the data points existed. In addition, random data points widely divergent
from the normal trend of the bulk of the data were excluded by the fairing
process: These points were first checked to ascertain they were not influenced
by an processing errors.
This information was relayed later to the EPA who in turn requested the test
organizations to take measurements in this region of power settings.
Accordingly some of the later data received provided LDX plots that were very
well defined in all regions of the curve.
1-16
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Digitizing of the Faired Curves
With the fairing of curves to the points plotted by LDX, a means was
available for interpolating emission rates for any desired thrust ratio. Also
by virtue of the fuel flow versus thrust curve, pounds of emission per pound
of fuel could be converted to pounds of pollutant per hour for each of the
interpolated points. In order to extract these quantities from the curves,
however, it was necessary to read the curves for each desired input datum.
At this point in the analysis, several options were available. The
curves could have been read, for example, with or without mechanical aids;
moreover, the curves could have been read only at those values of thrust or
power associated with a particular operational mode, or they could have been
read at a number of points in consideration of any future changes in the
definition of the operating modes. In the interest of flexibility, it was
decided that the curves should be read at a sufficient number of points to
permit them to be approximated by connecting straight-line segments. Accord-
ingly, for the CO, HC and NO curves, twelve points were read from each of
A
the faired curves. These points were closely spaced in regions of the curve
exhibiting high curvature and spaced relatively far apart in regions of the
curve which were approximately linear. Because the fuel flow vs thrust curves
were monotonic and exhibited relatively little curvature, it was concluded
that they could be well approximated by fewer straight-line segments. Hence
these curves were only read at five points. Samples of the faired LDX plots
showing the points at which the curves were read are shown in Figure 4.
These figures represent a complete set of plots for a test run identified as
CAL ID No. 393. The alphabetical sequence of the letters [and progression of
other symbols) preserves the original chronological order in which the test
points were taken. Precise location of the original data point input
represented by each letter (or symbol) is at the lower left-hand corner of
the symbol in each instance.
1-17
-------
(0
o> -
J
UJ
m
0) '>
J '"
I
20
7. RRTED
10
I
60
I
80
393
CO
NGX
V. »
CD
~1
100
7. RflTED
T
JO
JO
393
HC
V. RflTED
100
'/. RRTED
Figure 4 TYPICAL SET OF FAIRED LDX PLOTS FOR A TEST
1-18
-------
The sample plots represent one of the better sets of data in that
there are an adequate number of well-spaced test points. Each curve was
read at that point marked with an 'x1 as shown.
*
To facilitate curve reading, a Calma Model 303 Digitizer was used.
The Calma digitizer reduces graphical analog data to digital magnetic tape
for subsequent computer processing and analysis. The equipment consists of
the console, a backlighted tracking bed, balanced torque-motor chart drive,
stylus-carriage assembly, direct digital pick-off mechanism, data and control
electronics frame and an output incremental tape drive.
To digitize graphical analog data directly on magnetic tape, the
operator traces the analog plot with a movable stylus/carriage assembly. As
the plot is traced, movement of the stylus in either the X or Y direction
causes pulses to be generated by the direct digital pick-off mechanism. For
purposes of this program, the device was operated in its single-point mode.
**
By locating the stylus on each of the points to be read, the operator could
rapidly and efficiently record the X, Y coordinates of the curve points for
subsequent use in the interpolation process.
To evaluate the repeatability of the digitizing process, one of the
plots was read in duplicate. A comparison of the results of the two sets of
coordinates is shown in Table 2. As can be seen, the maximum difference
between duplicate readings is considerably less than 1% of full scale.
*
The Calma Company, 346 Mathew Street, Santa Clara, California.
k*These points were pre-marked as a part of the fairing process.
1-19
-------
Table 2
REPEATABILITY OF DIGITIZING PROCESS
Run
X
6.40
7.20
9.20
11.00
14.80
20.80
29.20
43.40
52.80
58.20
76.00
99.40
#1
L
4.69
3.71
3.05
2.53
1.93
1.93
0.97
0.53
0.37
0.32
0.14
0.08
Run
X
6.40
7.00
9.40
11.00
15.00
20.40
29.00
43.40
52.80
58.20
76.00
99.20
#2
y
4.68
3.71
3.05
2.54
1.93
1.44
0.99
0.53
0.37
0.31
0.13
0.08
Interpolation for Selected Modes
After the curves were faired and digitized, the data were loaded on
a computer tape and the tape processed by a program which interpolated for
selected operating modes for each engine. Mode selection, time-in-mode
information and the corresponding engine settings were supplied by the EPA.
The following modes were specified: taxi/idle, take-off, climb-out, approach
and taxi/idle. Climb-out and approach times correspond to those associated
with operations below an altitude of 900 meters above ground level. Engine
settings for turboprops were given in terms of a percentage rated take-off
horsepower while those for thrust-type turbines were in terms of percentage
rated take-off thrust.
1-20
-------
By virtue of the available plots, now stored in the computer and
accessible by interpolation, specified percentage rated thrust values were
then used as the basis for interpolating mass emission rates for CO, HC and
NO as well as the fuel mass rate. These rate values, when combined with the
given times in mode, made possible the computation of the total mass of
emissions for a typical landing-take-off (LTO) cycle.
The engine power settings initially were subject to changes by the
EPA to permit an evaluation of the effects of such variations within the
operational modes on individual and aggregated mass emissions of pollutants.
One of the salient features of the data processing procedures adopted is the
ease of accommodating such changes of input. Engine settings used in the
processing of the turbine/turboprop data to establish the so-called "base line"
from which proposed standards were promulgated are given in Figure 6 of this
report.
A significantly different procedure was employed for processing the
piston engine data, which came from two independent sources (as shown in
Table 1). This cahnge in method was necessitated since these sets of data
were incompatible with each other and with the turbines from the data processing
standpoint. Specifically, the one set (Continental Teledyne) lacked CO
measurements while the other (Scott Research Laboratories) lacked horsepower
data for the various engine power settings. The auxiliary power units comprised
a distinct category apart from the other engines and were accorded separate
treatment.
1.3 STATISTICAL ANALYSIS
Outputs from the overall assessment were subjected to only a routine
statistical treatment during this first phase of the program. Identifiably
different engine types and models were separated into individual groupings.
For the set of engines pooled within each group, mean values and standard
deviations from the mean were computed for various engine operational parameters
and pollutant quantities for each mode. Specific details concerning these
1-21
-------
quantities are included in the next section of the report. Standard deviations
were computed on a "best estimate" basis by applying the theory of small
number statistics. In essence, this involves using the quantity N-l as the
divisor of the sums of squares (N = number of samples summed).
A more thorough statistical treatment of these data will be conducted
during the second phase of this program. A report of this study will be
published during November 1971. The objective of this analysis will be to
attempt to identify and isolate those factors which contribute significantly
to the variance in the data and to define the relative magnitude of the
contribution of each.
1.4 PRESENTATION OF RESULTS
All of the numerical data presented in the report are in the form of
computer print-out data sheets. Each engine test for which data were received
has been included in the listing. In all cases the data for each engine test
have been processed to the maximum extent possible (i.e., each mode in the
LTO cycle appropriate to that engine as well as the aggregation of the emissions
over the entire cycle). In those cases where insufficient data are provided
to permit complete processing, the emission data are converted from a con-
centration basis to a mass emission basis. On the other hand, when engine
fuel flow data are unavailable, the conversion to mass emissions is not
possible and the test organization's raw measurement results are simply
*
reproduced.
The general format employed on the computer print-out sheets is
specified by the EPA. The data given for each engine test include the test
information received as well as the results of the data analysis procedures.
Input data is reproduced following the general guidelines of the standard
EPA data sheets (Figures 2 and 3), and, in substance, includes almost all of
Only about 2% of the data are included in this category.
1-22
-------
*
the data initially supplied by the testing organization.
Following this "replay" of the input data, the calculated mass
emissions data are tabulated for each engine power setting of the test sequence,
These data are expressed as mass pollutant per 1000 Ibs fuel, mass pollutant
per hour and mass pollutant per 1000 horsepower-(or thrust) hours (when CO-
measurements are available, similar data are given for C0_ although it is not
classified as a pollutant).
The final tabulation of data is that for the emissions for the LTD
cycle for that engine. Data format provided by the EPA for these data is
shown in Figure 5. For the turbine/turboprop engine category the EPA also
provided the following data for each model (note that the initial idle/taxi
and final idle/taxi modes are treated as distinct and separate parts of the
LTD cycle): engine power setting, useage weighting factor and time in mode.
Numerical specifications for these quantities are given in the commentaries
**
pertinent to each data set.
Piston engines were tested at power settings corresponding to various
nominal modes (the number of modes generally being a larger number than that
given in Figure 5). As a consequence, with EPA concurrence, the modes
corresponding to the EPA LTO cycle were directly selected from the testing
organizations test sequence (no interpolation on power settings was done as
for the turbine/turboprop category). In this case, the EPA provided only
specifications for weighting factors and times in mode (no power settings).
Some testing organizations, which did not use the standard data forms,
provided additional engine parameter data not required for present data
processing purposes. In such cases not all of these inputs are reproduced.
**
In the context of this report the following data sets are recognized:
turbine/turboprop, piston engine (Scott), piston engine (Continental), APU,
1-23
-------
MODE
TAXI/
IDLE
TAKE-
OFF
CLIMB-
OUT
APPROACH
TAXI/
IDLE
POWER
SETTING
POWER
OUTPUT
EMISSION
RATE
FUEL
RATE
USE AGE
WEIGHTING
FACTOR
TIME IN
MODE
TOTAL FOR CYCLE
# POLLUTANT/1000 # FUEL/CYCLE
# POLLUTANT/1000 #T-HR/CYCLE
# POLLUTANT/1 OOOK #T AT T.O.
POLLUTANT
MASS
FUEL
MASS
#POL/
1000 #
FUEL
ENERGY
OUTPUT
#POL/
ENERGY
OUTPUT
I
N>
-fc.
Figure 5 LTD CYCLE EMISSIONS - EPA FORMAT SHEET
-------
The arrangement of the data within the data sets groups the engines
by model. Following each group is an aggregated summary of the LTO-cycle
emissions for this model engine. The number of engines included in each
summary is shown at the top of the summary sheet. Since the summary accounts
show means and standard deviations in each of the tabular columns, engines
that did not have complete data (e.g., HC or CO was missing or possibly a
mode was missing) are not included in the summary because of the distortions
that would be thereby produced in the results.
As per instructions, all emissions data for the military turbine
engines are converted into a mass basis. Data for the auxiliary power units
are also on a mass basis. An additional calculation is made for the APU's
(where applicable) to determine the so-called "air power" for those units
operated with air bleed loading. This quantity is added to the shaft horse-
power (if any) of the unit to provide a measure of the total energy output.
It is important to note that the mass emissions of the hydrocarbons
rms of methane while those for nitric oxides (I
NCL. This useage is consistent throughout this report.
are in terms of methane while those for nitric oxides (NO ) are in terms of
A.
1.5 DISCUSSION
To date the principal function of CAL in this program has been in
coordinating and consolidating the mass of field test data, in developing
suitable data processing procedures and, finally, in processing the raw data
in accordance with guidelines supplied by the Office of Air Programs of the
EPA. There has been no requirement or intent to draw conclusions or inferences
from the final results that have been obtained. Rather the objective of this
report is to present the raw data input, describe the details of the data
processing procedures and to present the results. Thus the substance of this
section of the report is devoted to generally clarifying sundry background
details concerned with data handling and to explanatory comments related to
the tabulated data.
1-25
-------
Despite the somewhat circumscribed role of CAL in this program
(as described above), CAL's view of its overall function has been broader than
mere calculations of the results of engine emission tests. CAL has believed
an analysis of data must proceed within a framework that includes an engineer-
ing awareness and understanding of the real world within which the test results
have been obtained. Accordingly, very early in the program (29 June 1971),
project personnel visited Pratt $ Whitney Aircraft to observe testing operations
in progress and to discuss operational and instrumentation details with
cognizant personnel. This trip was extremely valuable in providing the "real
world" background within which the data transmitted for analysis had been
obtained.
The ultimate purpose of the data processing was to obtain results
for the emission of each engine for the complete LTO cycle in accordance with
Figure 5. A listing of the specific information provided by the EPA to
accomplish this purpose is given in Figure 6. Engine operating cycles, as
supplied by EPA, have been constructed based on time-in-mode considerations
of high activity periods at major air carrier airports. The first taxi-idle
mode is defined to include the total time between propulsion engine start-up
and the initiation of the turn into the runway. The take-off, climb-out and
approach modes approximate the times spent in these modes. The last taxi-/idle
mode includes the taxi/idle time between termination of the landing run and
final shutdown of the propulsion engine. Both the time-in-mode and power
setting information was obtained by the EPA from engine manufacturers, air
frame manufacturers, the airlines and the FAA. The weighting factors are the
fraction of the propulsion engines operating on a given aircraft in any given
mode. Results obtained from processing the data in accordance with the
requirements of Figure 6 are presented in Tables I, II and IV. This set of
results constitutes the aircraft emissions baseline data. Summaries obtained
by aggregating all engines of a given model are included also.
The basic emissions data was reprocessed a number of times using
power settings and weighting factors different from those given in Figure 6.
These inputs, provided by the EPA, were designed to evaluate the effects of
1-26
-------
Figure 6
SUMMARY OF EPA INPUTS EMPLOYED FOR LTO-CYCLE EMISSION CALCULATIONS
MODES
FIRST
TAXI/IDLE
TAKE OFF
CLIMB
APPROACH
LAST
TAXI/IDLE
CLASS T1
TURBOPROPS/TURBINES
POWER
SETTING
% RATED
T56 = 3%
Al RESEARCH = 6%
100%
90%
30%
T56 = 3%
Al RESEARCH = 6%
W.F.
1
1
1
1
1
T.I.M.
19
0.5
2.5
4.0
7.0
CLASS T2
TURBINES
POWER
SETTING
% RATED
CJ805 = 4%, JT3C = 5%
JT3D = 5%, JT4A = 5%
JT8D = 6%. SPEY = 4%
100%
85%
40%
CJ805 = 4%, JT3C = 5%
JT3D = 5%, JT4A = 5%
JT8D = 6%, SPEY = 4%
W.F.
1
1
1
1
1
T.I.M
19
0.7
2.2
4.0
7.0
CLASS T3
TURBINES
POWER
SETTING
% RATED
JT9D = 7%
100%
85%
30%
JT9D = 7%
W.F.
1
1
1
1
1
T.I.M.
19
0.7
2.2
4.0
7.0
CLASS P1
LIGHT UTILITY PISTON
POWER
SETTING
% RATED
«
*
*
«
*
W.F.
1
1
1
1
1
T.I.M.
12
0.3
5.0
6.0
4.0
tsj
-J
W.F. = USEAGE WEIGHTING FACTOR
T.I.M. = TIME IN MODE, MINUTES
*NOT SPECIFIED, MODE DATA WAS SELECTED DIRECTLY FROM
TEST ORGANIZATION'S SCHEDULE OF TEST MODES AS GIVEN
ON DATA SHEETS
-------
operational changes on emissions. Table V presents model summary data for
the turboprop/turbine category generated by using altered weighting factors
and power settings. This data represents a recomputation of the baseline data,
taking into account possible ground operational changes. The tables reflect
what the emissions would be for those engines normally used on 3 engine aircraft
if one engine was shut off during both taxi/idle modes (2/3 weighting factor)
and the power output of the remaining engines was increased 50% to maintain
total aircraft power at the same level. For engines normally used on 2 or 4
engine aircraft the tables reflect what the emissions would be if 1/2 of the
engines were shut off during both taxi/idle modes (1/2 weighting factor) and
the power output of the remaining engines was increased 100% to keep the total
aircraft power at the same level.
A few comments on grouping within models are appropriate. Special
treatment was accorded the JT8D models as per directions. The JT8D engine is
somewhat unique in that the by-pass airflow and the combusted exhaust gases
exit through a common duct. Mixing of the exhaust gases with the bypass airflow
was found to occur at engine idle settings resulting in dilution of the sampled
gases when the nominal multi-probe gas sampling configuration was ued. To
combat this problem Southwest Research Institute (SWRI) measured emissions of
the JT8D engines in the idle mode using a single axial probe (Ref. 3). Thus
all SWRI JT8D data has been treated as "undiluted" and all other JT8D data as
"diluted".
Another factor unique to JT8D engines is the presence of smokeless
combustor cans (retrofits) on some of the older models. These are identified
by remarks of the test organization under the "comments" section of each engine
data sheet. Thus Table IV has four separate summaries for the JT8D model:
diluted-ordinary, diluted-smokeless, undiluted-ordinary, undiluted-smokeless.
A separate grouping was also accorded the T56-A7 and the T56-A15
turboprop engines. The former represent overhauled engines tested at Kelly
AFB by SWRI while the latter are new engines tested by the manufacturer,
Allison.
1-28
-------
In all cases, model groupings exclude engines which lack complete
data (either missing data on one of the pollutants, or, in the case of piston
engines, a missing mode). Their inclusion would bias and distort the means
and standard deviations computed for each model.
Reference to the data sheets will show that in some cases data were
measured on aldehyde concentration, smoke index and particulates. These data
were not processed and are simply reproduced for completeness. Analysis of
these quantities was performed by the individual testing organizations and the
results are included in their respective final reports. These final reports
should be consulted for specific details concerning the background of the
emissions concentration data which have been processed on this program.
In general, that portion of the tabulated data for each engine
that corresponds to input information from the test organization, has been
reproduced without change. In some cases the units of certain quantities were
changed to preserve consistency among the data sets and in others approximate
values were estimated. For example, H/C information was not often provided
*
on the data sheets since the fuel had not been analyzed in situ. CAL-estimated
values would therefore be inserted to permit data processing. An H/C value of
approximately 2 was used for turbine fuel.
Relative humidity and temperature at the test sites were usually
given but not the corresponding specific humidity (Ibs water per Ib dry air).
In these circumstances the specific humidity data, as read from a graphical
presentation (Ref. 4), were entered.
SWRI provided an initial measured H/C value for tests at TWA. Since this
value (1.722) seemed too low, CAL chose to ignore this figure and used a
value of 2.02. Later SWRI notified CAL that a reappraisal indicated a
value of 1.968 for H/C. Since these two values were so close and time so
critical, the H/C ratio was not changed.
1-29
-------
Averaged data were used if a range of values for ambient parameters
was given. For example, the Bureau of Mines reported sizeable variations in
the sample line temperature during test operations (of the order of 70°C). The
figure given is the arithmetic mean of the extremes.
In the tabulated data, all missing, unavailable or non-measured
information is denoted by -0.00 to differentiate it from a true measurement
which is actually zero. Concentration measurements shown as a true zero
represent a value of less than one part per million.
No mode-type operational data for military engines was provided;
consequently only the conversion to mass emissions was made. The T56 turboprop,
although a military engine, is considered to be equivalent to the 501 civil
version and hence was used in the baseline calculations.
The Office of Air Programs conducted a program of span gas checks at
each of the test sites to gain assurance that there were no large discrepancies
among these test organizations attributable to poor quality calibration gases
or poor sampling techniques. Results of these tests are given in Appendix A.
In the preparation of this report, every possible effort has been
made to eliminate errors in data transcription, conversion of pollutant
concentration data to mass emission form, and calculation of pollutant burden
over the LTD cycle. In view of the stringent time constraints of the program,
however, it will be appreciated that it is virtually impossible to guarantee
that the report will be error free. If a particular entry appears out of
context, therefore, it may need to be validated by checking with the original
data source.
The methods employed to reduce the concentration data to mass
emission form and to calculate the pollutant burden over the LTO cycle were
selected as the most reasonable and timely within the constraints of the
program. We recognize, however, that there will undoubtedly be instances
1-30
-------
in which the reader may wish to depart from the methods employed in the report
or to undertake an alternative analysis for specific purposes. It is for these
reasons that we have provided, wherever possible, the raw input concentration
data as well as the data in mass-emission form.
In the case of the turbine engines we have employed a computer-aided
graphical technique to interpolate emissions at specified power or thrust
values. Such interpolation suffers from the limitations of all interpolative
procedures in that a certain arbitrariness is involved in extending the results
obtained from a limited number of test points to situations in which actual
observations were not available. Unfortunately, the engine operating condition
most subject to this type of error is the taxi/idle mode with its attendant heavy
influence on the total emissions calculated for the LTD cycle. In many
instances, the taxi/idle mode as actually run in the test is at a higher
percentage of rated power or thrust than is called for by the EPA-designated
LTD cycle (see Fig. 6). In these cases, it was necessary to extrapolate to
the desired power or thrust setting. Such extrapolation is difficult at best
and, in the present analysis, was often further aggravated by lack of test
points in the critical "knee" of the CO and HC curves at engine settings
slightly above taxi/idle values. The only recourse under these circumstances
is to rely on engineering judgment or to invoke mathematical conventions, such
as regression analysis, which may be equally arbitrary. For final arbitration
of this question, the reader may wish to make his own interpolations from either
the raw concentration data or the data as converted to mass emission form, both
of which have been provided in the report. The method of analysis employed in
this report is not claimed to be absolute any more than any other interpolative
procedure can make such claim.
As has been previously pointed out, a major advantage which can be
claimed for the computer-aided graphical analysis is the speed with which data
may be manipulated in compliance with changes in the questions to be answered
by the data base. For example, if it is desired to know the effect on emissions
of a change in ground-operation tactics, the relevant information can be
quickly and efficiently retrieved from the data. The same facility is available
1-31
-------
as a means for checking the accuracy of the plotted data. By virtue of the
accessibility of the digitized curves in the computer, the original curves
could be "reconstituted" and visually scanned for possible errors. In
addition to performing this error check, we also performed an extrapolation
check in that region of the pollutant curve where it was necessary to extra-
polate in order to obtain mass emissions for the taxi/idle mode. It is for
these reasons that the results for the LTO cycle can be reported with considerable
confidence.
1.6 SUMMARY
Experimental data consisting of concentration measurements of
pollutants in the exhaust gases generated by turboprop and thrust turbine air-
craft engines, light-utility piston aircraft engines and auxiliary power units
have been processed, wherever applicable and possible, to establish mass
emissions over specified landing-take-off (LTO) cycles. These experimental
data and the LTO cycle specifications were furnished by the Office of Air
Programs, EPA and the intent of the processing was to provide baseline data
with the view of promulgating emission standards.
Processing of the data for commercial engines in the turboprop/turbine
category was designed to permit calculation of pollutant mass emissions over
an entire LTO cycle where the engine power settings could be arbitrarily speci-
fied. This purpose was achieved by graphically establishing a functional rela-
tionship between mass pollutants/unit fuel consumed and percent rated power
for each individual engine. Thus by interpolation techniques, emissions
corresponding to any desired engine power setting could be determined. This
capability permitted evaluation of the effects of changes in engine operating
cycles on mass emissions over the LTO cycle (compare engine model summary
data between Table IV and Table V).
In contrast to the situation for the turboprop/turbine engine category,
the piston engine emission data were measured under conditions of very uniform
consistency between engine power setting and engine operational mode. LTO
1-32
-------
cycle emissions for this class of engines were computed by using the measured
in-mode concentration measurements. No interpolative routines were necessary.
Military turbine engine emissions data were only converted from a
concentration basis to a mass emission basis. No LTD cycle criteria were
defined for these engines.
Auxiliary power units represent a distinctly unique source of exhaust
pollutants within the context of the types of aircraft engines tested. Only the
mass emissions for each power setting employed in the test sequence are given.
Total horsepower loading for each unit is given by calculating the power associ-
ated with air bleed loading (as contrasted with shaft power loading) wherever
appropriate.
All of the pertinent data on each engine tested and supplied to CAL
has been reproduced in this report.
All of the emissions data has been processed to the maximum extent
possible within the constraints imposed by the available supporting information
and the requirements of the Office of Air Programs. A total of 392 engine test
runs are reported. This total includes 199 turboprop/turbine engines, 140 piston
engines and 53 auxiliary power units.
1.7 REFERENCES
1. Nature and Control of Aircraft Engine Exhaust Emissions, Report of
the Sec. of HEW to the U.S. Congress, U.S. Gov't Printing Office,
Document No. 91-9, 1969.
2. Hum, R.W. Elwood, J.H. and Vaught, J., "Procedure for the Continuous
Sampling and Measurement of Gaseous Emissions from Aircraft Turbine
Engines", Final Draft SAE E-31 Committee Paper, 25 May 1971.
3. Personal communication, Charles Hare, Southwest Research Institute,
9 August 1971.
4. Taylor, C.F. and Taylor, E.S., The Internal Combustion Engine, Second
Edition, International Textbook Company, Scranton, Pa. (1969) p. 31.
1-33
-------
Appendix A
SPAN-GAS CHECKS OF TEST ORGANIZATIONS INSTRUMENTATION
Seven span gas cylinders were analyzed by three of the laboratories
involved in the aircraft baseline emission. These initial checks were made at
those aircraft study laboratories located in the Western half of the country;
EPA (T&EB Mobile) at Phoenix (AiResearch), Southwest Research Institute (SWRI)
at San Antonio (Kelly AFB) and Bureau of Mines (BOM) at Tulsa (American Airlines).
The exercise was not intended to be a correlation of laboratories but an attempt
to uncover major differences in analysis among laboratories which might be
caused by the use of poor quality calibration gases or poor sampling techniques.
The results that have been obtained raise questions concerning carbon monoxide
analyses but the overall effort has been worthwhile in building confidence in
comparability among the above-named laboratories engaged in the emissions measure-
ment program.
Table A-l is a summary of the data collected. Detailed information
was accumulated also concerning the physical specifications of each instrument
used so that an estimate could be made of instrumental sensitivity and expected
accuracy. The sample cell length and calibration range were found to vary
considerably from one instrument to another. Based on this type of information,
an optimistic accuracy band was estimated for each instrument and is given as
a parenthetical value adjacent to each data point in Table A-l. The largest
variation in expected accuracy is seen to occur among the CO instruments.
Variation in concentration measurements was also the largest for CO but this
fact is not considered entirely attributable to instrument variation.
Sampling systems were checked for leaks by plugging the sample line
and observing the flow drop-off. All systems appeared to be tight.
A cylinder of hydrocarbon-free air was used to check the hydrocarbon
level in the zero gas being used by these laboratories. The zero gas at SWRI
A-l
-------
was found to contain less than 0.6 ppm propane and the BOM span gas contained 1.6
ppm propane. The EPA span gas at Phoenix contained zero hydrocarbon relative to
the reference cylinder.
At those laboratories using chemiluminescence instrumentation for
oxides of nitrogen measurement, a determination of the NO^-NO converter efficiency
was made. EPA and SWRI converters approached 100% efficiency. This particular
test is made by introducing oxygen into a bag of NO in N~ span gas and observing
the oxidation of NO to N0~. If the NO line remains constant during the oxidation
Lt A,
process, the indication is that the thermal converter is working properly.
A similar series of cross checks was then conducted at those emissions
measuring laboratories in the Eastern half of the country. These test sites
included the following: Detroit Diesel Allison Division (Indianopolis, Indiana),
Teledyne Continental Motors (Muskegan, Michigan), Pratt £ Whitney Aircraft
(East Hartford, Connecticut), Scott Research Laboratories (temporary lab at
Allentown Pennsylvania Airport) and Scott Research Laboratories (temporary
lab at Naval Air Station, Norfolk, Virginia). Addition cylinders of high-
concentration gases were employed at those labs involved in light-utility piston
engine studies (Teledyne Continental and Scott Allentown). These additional
results are given in Table A-2 which is similar in format to Table A-l.
[NOTE: The material in Appendix A has been abstracted by CAL from
two internal memoranda of the Office of Air Programs, Tests £ Evaluation
Branch, Ypsilanti (to R.C. Stahman from M.W. Korth). This inclusion is at
the behest of the EPA.]
A-2
-------
Table A-1
SPAN GAS CROSS CHECK
(WESTERN LABORATORIES)
CYLINDER NO.
A247
HYDROCARBON
(ppm, PROPANE)
13359-B
HYDROCARBON
(ppm, PROPANE)
A6775
CO, ppm
A672
co_ %
A6741
co_ %
UV/2> '»
A2334
NO, ppm
SSB-162
NO, ppm
(MAIN
TERM.)
70.0 (± 1)
10.8 (± 1)
84 (i 25)
cnn (+ 25)
87 (± 1)
20.0 (± 1)
EPA
(BLDG. 2042)
72.2 (+ 1)
10.5 (± 1)
82 (+ 25)
404 /+ oc\
1 R7 l+ nRl
4y 1+ nci
82.2 (+ 1)
21.0 (± 1)
(T&EB
PHOENIX)
70 (+ 1)
10.6 (± 1)
120 (± 10)
ccn (+ ORt
1 el /j. nc)
41? (+ 05t
92.5 (+ 1)
21.0 (+ 1)
SWRI
(KELLY
AFB)
67.5 (+ 1.5)
8.4 (+ 1)
94 (± 2)
1 ^1 f-L f\fi\
4 OR /+ OR)
82 (± 1)
19 (± 1)
BOM
(AMERICAN)
69 (± 1)
9.2 (± 0.5)
95 (± 1)
con /-*- int
1 t\A /4- OR\
477 (+ n^l
87 (± 1)
18 (± 1)
A-3
-------
Table A-2
SPAN GAS CROSS CHECK (EASTERN LABORATORIES)
CYLINDER NO.
A-247
uvnonr*A Dnmvi
(ppm, PROPANE)
13359-B
uvnDftp A Dnmvi
(ppm, PROPANE)
A6775
A672
PO fnnml
C02 (%)
A-6741
m iv \
A-2334
SSB-162
NO (ppm)
1-15738
IVin fnnml
IMU ippmj
A-1905
ro (%i
1-4523
MVnDDPADROM
(ppm, PROPANE)
FF-17054
CO (%1
CCtn
HC
(ppm, PROPANE)
EPA
71 l+ 11
/I \± II
in 7 (4- K\
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en (4. 1)
ovi \2_ 'I
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101 (+ 9)
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1.68 (± ?)
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NENTAL
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19.5 (+ 3)«
SCOTT
NORFOLK
CO 1 (4. 1 1
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con (4. on)
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ALLENTOWN
1 ocn /4- Rn\**
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NDIR
CHEMI LUMINESCENT
-------
Part 2
SUMMARY OF DATA
2-1
-------
2. 1 DATA TREATMENT AND COMMENTARY
Data for light-utility piston engines and auxiliary power units are
presented in the first three tables following this discussion. Table I
contains data on piston engines tested by Scott Research Laboratories and
Table II contains similar data obtained from Teledyne Continental Motors.
Table III is a compilation of data on auxiliary power units (APU); these data
were provided by AiResearch.
2.1.1 Piston Engines
Tests on piston engines were conducted by Scott Research Laboratories
on engines installed in aircraft. Accordingly, these engines span a broader
spectrum of engine age and condition than do the "brand new" engines tested by
Teledyne Continental. Differences in the methods of testing and data reduction
employed by Scott and by Teledyne Continental, however, necessitated different
approaches to mass emissions analysis and precluded incorporating the two sets
of data into a single compilation. In view of this fact, care should be taken
in comparing results from the two sources, particularly if the intent is to
establish emission response to factors such as engine age. Observed differences
in emissions may be artifacts of the differences in testing procedures rather
than being attributable to independent causes.
2.1.1.1 Scott Research Laboratories
Piston engines tested by Scott Research Laboratories are included
in Table I. For the most part, these engines were subjected to a 10-mode
test cycle, but in a few instances certain of the modes are missing. From
among the ten modes used by Scott, five were selected as being equivalent
to those designated by EPA in their LTD cycle. These five modes were
then employed in the LTO cycle calculations. Since no horsepower measurements
were provided by Scott, it was not possible to reduce the emissions to the
basis of pounds pollutant per thousand horsepower hours.
2-2
-------
All concentration data provided by Scott Research Laboratories were
expressed on a dry basis. To convert these data to emission mass form, therefore,
it was necessary to introduce a correction to convert concentrations from dry
to wet basis. Correction was made only for the water of combustion, it being
assumed that water vapor in the intake air was negligible. The correction
factor used was the one proposed by the SAE E-31 Committee :
too
100 + K/z (CO 1- COZ)
where CO and C0_ concentrations are expressed as percent by volume, and a.
is the atomic hydrogen/carbon ratio of the fuel. Then,
Concentration (Wet basis) = K Concentration (dry basis)
and the corrected concentrations were converted to pounds pollutant per pound
of fuel by the formulas proposed by the E-31 Committee and presented in Part 1
of this report.
It should be noted that, for many of the engines tested by Scott,
triplicate runs were made. In the statistical summary for an engine model,
these replicate runs were not distinguished from runs on separate engines;
consequently, the standard deviations computed for the emission quantities are
expected to be somewhat underestimated relative to what might have been
observed if there had been no replication of engines. In the triplicate runs
on 0-200 engines, the first two runs were done on one exhaust and the third
**
run was done on the other.
In the statistical summaries it will be noted that the number of engines
included in each model summary is sometimes less than the number of engines
actually processed as individuals. The difference resides in the fact that for
R.W. Hum et^ &1_., "Procedure for the Continuous Sampling and Measurement
of Gaseous Emissions From Aircraft Turbine Engines," Final Draft SAE E-31
Committee Paper (May 25, 1971).
t
Letter dated July 22, 1971 from Mr. A.F. Souza, Scott Research Laboratories
to Mr. Charles Gray, Jr., Environmental Protection Agency.
2-3
-------
several of the engines the data was incomplete in some sense. For example, if
data for one of the pollutants or for one of the modes was missing for a
particular engine, that engine was excluded from the statistical summary so as
not to bias the mean value or standard deviation.
2.1.1.2 Teledyne Continental Motors
Table II summarizes twenty-one engines belonging to model categories
0-200-A, 0-470-R or IO-520-P. For the most part, these engines were subjected
to a 13-mode test cycle, including Idle-Taxi, Take-Off, Climb, and Pattern.
Two forms of the Idle-Taxi mode were employed, Idle-Taxi-Low and Idle-Taxi-High.
Similarly, two versions of the Climb mode, Rich and Lean, were used, but in some
of the tests only one of these modes was run. Some convention was necessary,
therefore, in order to comply with the 5-mode LTO cycle designated by EPA. In
all cases, Idle-Taxi-High was used as the EPA-designated Idle-Taxi mode, and
the mode designated Pattern by Teledyne Continental was renamed Approach, to
comply with the EPA designation. In the case of the Climb mode, the LTO
cycle computations were made with both Climb-Rich and Climb-Lean data. In
all cases where both modes were run, two LTO cycle computations are included;
otherwise, the LTO cycle computation is made with whichever of the two Climb
modes is available.
A distinguishing feature of the Teledyne Continental tests is that CO-
was not measured. Consequently, the normally used formulas for converting
concentrations to mass emissions are not applicable, and an alternative
conversion had to be invoked. The method employed in Table II is the one used
by Teledyne Continental and was kindly provided by them.
First, it should be noted that all effluents except Total Hydrocarbons
are expressed in the raw data on a dry basis. Except for hydrocarbons, therefore,
the following dry-to-wet correction factor was employed:
p
Correction Factor, K = 1 - M. ( / )
l\
2-4
-------
where oc = Hydrogen/carbon atom ratio
F = Fuel flow, Ib/hr
and A = Air flow, Ib/hr
This expression for the correction factor is an approximation that is accurate
when the specific humidity of the inlet air is low. The complete equation is
given in SAE procedure J177. Conversion of CO and NO concentrations to the
corresponding mass flow rates was then accomplished by means of the following
formula:
Pollutant Mass Flow Rate (Ib/hr) =
M cone (PPM) .
-z- (F+A)' *
"EX '0* J
where M = molecular weight of pollutant
and Max = molecular weight of exhaust
For conversion of total hydrocarbon concentrations to mass flow rate, the
formula is:
Pollutant Mass Flow Rate (Ib/hr) =
(F +A)
The exhaust molecular weight, AJ£X , varies as a function of air/fuel ratio.
This relationship can be approximated as a straight line, and was represented
in the computer calculation by the equation
A?£A = 21. 236,+ 0.515 A/F
According to Teledyne Continental, this expression is valid for air/fuel ratios
less than stoichiometric, but MEK assumes the constant value 28.96 for air/fuel
*
ratios greater than stoichiometric.
Justification for these relationships can be found in C.F. Taylor and E.S.
Taylor, The Internal Combustion Engine, Second Edition, International Textbook
Company, Scranton, Pa. (1969) pp. 37-39.
2-5
-------
Certain conventions must also be followed with regard to molecular
weights. To maintain consistency with other data in this report, some modification
of the Teledyne Continental input parameters was made. For example, elsewhere
in this report it has been customary to express Total Hydrocarbons as methane,
molecular weight 16.04. This value departs somewhat from the value of 14.67
used by Teledyne Continental on the basis of formulas employed by the State of
California for heavy duty gasoline engine tests. Also, in the interest of
consistency, the hydrogen-carbon ratio was taken as 1.84 rather than the 2.12
used by Teledyne Continental on the assumption of a representative gasoline
with formula C0H,-. NO was computed as NO- equivalent, using the molecular
o 1 / ^
weight 46.01.
Separate statistical summaries were made for the Climb-Rich and
Climb-Lean categories. It will be noted that the number of engines included
in each model summary is often less than the number of engines actually
processed as individuals. As previously noted, the difference resides in the
fact that for several of the engines the data was incomplete in some sense.
For example, if data for one of the pollutants or for one of the modes was
missing for a particular engine, that engine was excluded from the statistical
summary so as not to bias the mean value or standard deviation.
2.1.2 Auxiliary Power Units -- AiResearch
Table III is a compendium of emissions tests made by AiResearch on
auxiliary power units. Concentrations in this table are on a wet basis --
that is, the emission concentrations are corrected to concentration in wet
exhaust from combustion with dry air.
Mass of pollutant per 1000 pounds of fuel was computed by AiResearch
and submitted as part of their report; consequently, it was not necessary
to convert pollutant concentrations to mass emission form. Though AiResearch
also provided figures for mass of pollutant per hour, it was found more
expeditious to compute the mass flow by multiplying pounds pollutant per 1000
pounds of fuel by the corrected fuel flow rate. Note that NO and N02 concentrations
2-6
-------
were reported separately by AiResearch. These separately measured quantities,
as well as the combined concentration of total oxides of nitrogen (NO ), are
reproduced in Table III, but mass emission rates are included only for NO .
The total nitrogen oxides are computed as NO , molecular weight 46.01.
In addition to the computations performed by AiResearch and
incorporated in Table III, additional computations were performed to express
emissions on the basis of pounds pollutant per horsepower hour. For this
purpose, it was considered advisable to take into account, wherever possible,
both shaft horsepower and the horsepower induced by bleed air loading. In
this way, emissions can be charged against the combined equivalent horsepower
rather than against the less realistic value of shaft horsepower, which is
often small or negligible.
The basis for computing total horsepower as the sum of shaft
horsepower and air horsepower was provided by Mr. Charles Dawson of the
Environmental Protection Agency, Ann Arbor.
The ideal compression power was taken as isentropic, and the
applicable formula for air horsepower is based on the assumption of perfect
gas laws and the belief that constant specific heats can be assumed with
sufficient accuracy. Typical pressure ratios are about 3 (temperature ratio
& 1.36) and inlet compressor temperatures are near normal ambients. For
steady flow,
K-r
Air Ht>» I.+I5 WcpT, [(*/?,)"-']
where w = corrected bleed flow, Ibs/sec
7 = compressor inlet temperature, °F
Pa = compressor discharge pressure, psia
P, = compressor inlet pressure, psia
Mean compression temperatures are taken as 190°F (650° Rankine) and K = 1.398.
The formula thus reduces to
2-7
-------
Air HP =
= 0.3-V-/
r / P \ <->.£. a? ,
* fJ ->
L ( /y-. 7/ -I
[(£
'.285 ,
r)'-
"-J
In reducing the AiResearch data to horsepower basis, the air horse-
power as computed from the above formula was added to. the corrected shaft
horsepower. This combined quantity was used as divisor in reducing pounds of
pollutant per hour to pounds of pollutant per horsepower hour.
2.1.3 Turbine/Turboprop Engines
Data for turbine and turboprop engines are presented in Tables IV
and V. Table IV contains baseline data, in which a normal LTD cycle and
conventional ground-operation tactics are employed. The basis of the LTD
cycle, as prescribed by EPA, is discussed in Part 1 of this report. Basically,
the cycle consists of taxi/idle prior to takeoff, takeoff, climbout, approach
and taxi/idle subsequent to landing. To each of these modes a time in mode is
assigned in accordance with airport experience.
Table IV presents, for the most part, two pages of information for
each engine. On the first page is tabulated the identification of the engine,
the engine supplier, the test organization, such essential engine data as thrust
or power rating and engine-overhaul history, and prevailing ambient test
conditions. This information is followed by a tabulation of test data,
including pollutant concentrations and a description of the test modes in
terms of engine operating conditions.
At this juncture it should be pointed out that verbal names assigned
to the various test modes varied considerably from one test organization to
another. In view of this fact and the fact that subsequent designation of
modes is mandated by the EPA-prescribed LTD cycle, test modes are tabulated
2-8
-------
only in numerical terms. Each test mode is tabulated as a pair of integers
separated by a slash. The number preceding the slash denotes the mode under
test, whereas the number following the slash denotes the mode previously tested.
Thus the entry "3/5" denotes that the data in that line of the table is for the
third mode and that the mode which preceded it is in the test sequence was
mode 5. Similarly, "3/2" denotes that the third mode was preceded in the test
sequence by mode 2. The modes are numbered in ascending order of power or
thrust settings; accordingly, the slash notation makes evident whether a particular
mode was tested as part of an ascending or descending sequence of power or thrust
settings. The sequence of testing is further elucidated by the column
labeled either "Clock-Time" or "Elapsed Time." Clock time, such as 2037,
denotes "2037 hours", or 8:37 p.m. Elapsed time is in minutes and is measured
from a zero time reference at the beginning of the test sequence. If the time
entry is -0.00, no time-of-test information was available.
For each test mode, the actual thrust or shaft horsepower is tabulated;
this number is followed by "Percent Rated T.O." obtained by dividing the test-
mode setting by the rated thrust or horsepower. The resulting values are
expressed as integer percentages and are truncated, rather than rounded,
quantities. Thus, for example, 5% brackets a range from 5.00% to 5.99%.
This fact should be borne in mind in comparing the mass emissions computed from
raw data with mass emissions values interpolated for the LTO-cycle calculations.
Mass emissions for each test mode were computed according to the
conversion formulas of Section 1.2, Methodology of Data Analysis, and are
expressed as pounds of pollutant per thousand pounds of fuel and as pounds of
pollutant per hour. Pounds of pollutant per hour is the product of fuel
consumption rate, in pounds per hour, and pounds of pollutant per pound of
fuel. Finally, the pollutant mass is expressed on the basis of mass of
pollutant per unit of energy. For turboprops, this unit is taken as 1000
horsepower hours; for turbines, the corresponding unit is 1000 pounds thrust
hours, since horsepower rating is not applicable in this instance.
2-9
-------
The converted quantities expressed as pounds of pollutant per pound
of fuel were plotted against percent power or thrust and processed as described
in Section 1.2 to obtain interpolated values at specified settings for idle/
taxi, takeoff, climbout and approach, as specified by EPA. These interpolated
values then formed the basis for the calculations tabulated as the second page
of information for each engine. If for some reason, such as incomplete data,
it is impossible to complete the LTO-cycle calculation, then the second page
of information is omitted.
Pollutant mass for a particular mode is computed by multiplying pounds
of pollutant per hour by time in mode. Similarly, energy for that mode is
found by multiplying thrust or power by time in mode. Division of pollutant
mass by energy for each mode gives the corresponding pounds of pollutant
per horsepower hour or per pound thrust hour. In a similar manner, pounds
of pollutant per pound of fuel for the entire cycle is obtained by dividing
the total pollutant mass for the cycle by the total fuel mass for the cycle.
The result is a quantity which can be interpreted as the average rate at which
pollutant is generated per pound of fuel, the average reflecting appropriately
the times spent in the various modes. The pounds of pollutant per 1000 horsepower
hours or per 1000 pounds thrust hours is similarly computed by dividing the
total pollutant mass for the cycle by the total energy for the cycle.
It will be noted that in some instances the emission rate or mass is
recorded as 0.0. This type of entry may occur, for example, when it is
necessary to obtain CO or HC values at 100 percent thrust by extrapolation
of the corresponding plots of pollutant mass emission versus power or thrust.
If the extrapolation yields a negative value, the extrapolated value is
defined to be zero. Such a result is completely consistent with facts, because
it will not occur unless the pollutant mass is indeed negligible at high
power or thrust settings.
Statistical summaries following the results for individual engines
are computed in two ways, the two summaries being differentiated by changes
in "useage weighting factors." The summary appearing in Table IV applies to
2-10
-------
the data for individual engines as displayed in that table and is based on
useage weighting factors of unity for all modes. In Table V, the useage
weighting factors are 1.00 for takeoff, approach and climb modes but are
reduced to either 0.50 or 0.67 for the two taxi/idle modes. The reduced values
are based on a modification of ground-operation tactics in which, for two-
engine or four-engine aircraft, only half of the engines are in operation and
for three-engine aircraft only two-thirds of the engines are in operation.
The thrust or power settings for the engines remaining in operation are increased
proportionately to compensate for the engines not in operation. Comparison
of the two statistical summaries will reveal that substantial reductions in CO
and HC emissions may occur as a result of this change, primarily because of
the steep negative slope of the CO and HC curves at low power or thrust
settings.
2-11
-------
2.2 TABULATED RESULTS
2-12
-------
TABLE I
LIGHT-UTILITY PISTON ENGINES
SCOTT RESEARCH LABORATORIES
CONTENTS:
1-2 TO 1-107 INDIVIDUAL ENGINE RUNS - COMPLETELY PROCESSED
1-108 TO 1-110 MODEL SUMMARIES
1-111 TO 1-116 INDIVIDUAL ENGINE RUNS - MASS EMISSION
CONVERSIONS ONLY
1-117 TO 1-123 INDIVIDUAL ENGINE RUNS - INPUT DATA
REPRODUCED ONLY
1-1
-------
OATEl T/16/T1
TEST ORGANIIATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEDYNE-CONTINENTAL
ENGINE DAT*
CAL ID NUMBER: \t>t ENGINE TYPE AND MODELi O-ZOO-A
RATED HORSEPOWER: 100.
ENGINE TOTAL TINE: 284. MRS
FUEL: AV GAS 80/87 FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA *»«»»..»
INLET AIR TEMPERATURE, DEGREES f: START 77.50 FINISH 79.00
ATMOSPHERIC PRESSURE: START 30.01 FINISH 30.01
INLET AIR HUMIDITY, CRN H20/L8 AIR: 0.01
RELATIVE HUMIDITY: 64.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER! 20*S98-»-AA
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOU 1 -0.0 5. 60
IOLF/TAXI 2 -0.0 11. SO
RUN UP 1 -0.0 17.60
RUN UP-LEAN 4 -0.0 18.40
RUN UP-RICH 5 -0.0 16.70
TAKE-OFF 6 -0.0 49.60
CLIMB 7 -0.0 49.60
DESCENT fl -0.0 32.80
DESCENT ON 6 -0.0 19.20
APPROACH 9 -0.0 22.00
TAXI
TEST
MODF
1
2
3
4
5
6
7
a
a
9
10
TEST
MODE
1
2
3
4
5
f>
7
S
a
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
336.00
460.00
607.00
796.00
807.00
1110.00
1110.00
1076.00
975.00
874.00
491.00
MASS EMI
CO
LB/1K
LB FUEL
911.54
11)2.61
986.27
1077.62
943.42
1153. 39
1 153.39
869.16
1331.37
1055.73
1081.90
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURt
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
70.59
62.38
27.32
33.77
23. 6H
18.82
18.82
15.77
29.38
23.13
33.06
MEASURED
FUEL FLOH
LB/HR
11.50
49.60
49.60
22.00
a. 90
FUEL
-0,
CO
IORY)
PERCENT V
1.70
4.80
4.40
5.00
4.10
6.50
6.50
4.10
7.10
4.80
4.30
MASS EMI
N02
LB/1K
Lfl FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
L"S.
2.30
0.25
4.12
2.70
0.60
9.461
.0
CO
2
IORYI
PERCENT V
4.00
3.30
4.40
4.10
4.50
4.70
4.70
5.30
3.40
4.20
3.50
MASS CNI
C02
LB/1K
LB FUEL
1548.36
1223.49
1549.65
1388.41
1626.95
1310.38
1310.38
1765.34
1001.75
1451.45
1183.65
CO
LB/IK
LB FUEL
1132.63
1153.39
1153.39
1055.73
1081.90
8.90
THC
(DRYI
PPNV
5003.00
4616.00
2128.00
2736.00
1797.00
1852.00
1852.00
1299.00
2736.00
1852.00
2294.00
MASS EMI
NO
LB/1K
LB FUEL
0.65
0.78
5.15
3.29
J.59
5.77
5.77
11.21
1.76
5.60
1.53
LTD CYCLE
CO
LH/1K
HOURS
13025.24
57207.91
57207.91
23226.13
9628.91
MEASURED CALCULATED
AIR Fitly F/A
LB/HR
62.00 0.03861
119.00 0.04045
202.00 0.04237
204.00 0.04413
195.00 0.04125
540.00 0.05349
540.00 0.05349
398.00 0.04461
387.00 0.05093
247.00 0.04322
08.00 0.
NO
(DRYI
PPNV
16.00
20.00
140.00
93.00
95.00
198.03
198.00
322.00
57.00
155.00
17.00
MASS Ell
. NOX
LB/1K
Lfl FUEL
0.65 '
0.78
5.15
3.29
3.59
5.77
5.77
11.21
1.76
5.60
1.53
EMISSIONS
CO
EMISSION
LBS.
2.605
0.286
4.7*8
2.323
0.645
10.607
1.121
NO
2
1CRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS E^l
CO
LO/MK
5104.60
13025.24
17)58.29
19828.18
15755.14
57207.91
57207.91
28508.27
52169.76
23226.11
9628.91
HC
LB/IK
LB FUF.L
62. sn
13.82
18.82
23.1)
33.06
03790
NO
X
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
395.31
717.39
4B0.81
621.40
395.49
933.53
933.53
517.30
1151.83
513.24
294.20
HC
LB/IK
HOURS
717.39
933.53
933.53
513.24
294.20
ALDEHYDES
(DRYI
18.00
13.00
-0.00
-0.00
-0.00
6.00
5.00
5.00
6.00
6.00
6.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.143
0.005
0.077
0.051
0.020
0.297
0.031
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-o.oo
-0.00
-0.00
MASS EMI
C02
LB/HR
8670.79
14070.09
27273. 19
25546.71
27169.98
64994.84
64994.84
57903.03
39268.48
31931. 80
12314.45
ND
LB/IK.
LB FUFL
0.78
5.77
5.77
5.60
1.55
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-O.OU
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
3.63 3.63
8.91 8.91
90.7? 90.72
60.68 60.58
59.96 59.96
286.24 286.24
286.24 286.24
367.76 167.76
66.82 68.82
123.19 123.19
13.61 13.61
NO NO
LB/IK EMISSION
HUURS LRS.
8.91 0.0016
2X6.24 0.0014
2U6.24 0.0238
123.19 0.0121
13.61 0.0009
C.0402
0.0042
1-2
-------
0«IE: 7/16/71
TEST ORGANISATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEOYNE-CONTINENTAL
ENGINE DATA
CAL in NUMBER: IAT
ENGINE TYPE AND MODEL! 0-200-A
RATED HORSEPOWER: 100.
284. HRS
FUEL H/C RATIO: 1.840
SERIAL NUMBER! 204598-9-AB
FINISH
FINISH
62.00
30.00
ENGINE TOTAL TIME!
FUEL: AV GAS 30/87
OPERATIONAL DATA «..4...
INLET AIR TEMPERATUREi DEGREES Ft START 80.90
ATMOSPHERIC PRESSURE: START 30.00
INLET AIR HUMIDITY, CRN H20/L8 AIR: 0.01
RELATIVE HUMIDITY: 96.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00. (-LOW RATE. LITERS/MIN:
SAMPLE LINE TRANSPORT TIME. SEC! 1.60
NUMBER OF TESTS: 11
COMMENTS:
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 6.40
IDLE/TAX 2 -0.0 9.80
RUN UP 1 -0.0 11.30
RUN UP-LEAN 4 -0.0 16.70
RUN UP-RICH 5 -0.0 16.70
TAKE-OFF 6 -0.0 SI. 90
CLIMB 7 -0.0 51.50
DESCENT 6 -0.0 IS. 90
DESCENT ON a -0.0 18.10
APPROACH 9 -0.0 22.00
TAXI
TEST
»noE
1
2
1
4
5
6
7
a
B
9
10
TFST
MODE
I
2
a
n
9
10
TtSI
«ICOF
2
6
7
1
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
UEGREES F
247.00
370.00
639.00
560.00
699.00
1099.00
1099.00
1087.00
979.00
8K.OO
471.00
MASS EMI
CO
LB/IK
LB FUEL
719.99
1137.42
923.94
916.91
9)9.03
1182.90
1182.90
872.16
1 363. 17
1978.93
U58. 2J
TIME IN
MDDE
HIN.
12.00
0.30
9.00
,.00
4.00
FOR CYCLF
FOR CYCLE/Lfl
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-0.00
MASS EMI
HC
I B/IK
IB FUFL
19.94
14.18
8.69
11.29
7.91
9.72
9.72
9.99
9.88
7.90
12.23
MEASURER
FUEL FLOW
LB/HR
9.90
91.90
91.90
22.00
8.10
FUEI
-0
CO
IDRY)
PERCENT V
3.30
S.70
4.70
4.40
4.80
7.00
7. no
4.60
.4.10
9.70
6.20
MASS EMI
N02
LI/IK
LB FUEL
0.0
0.0
0.0
3.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
L1S.
1.96
0.26
4.27
2.20
0.94
9.239
0
CO
2
(DRYI
PERCENT V
9.80
4.30
9.90
9.20
9.90
4.90
.90
.00
.80
.90
.90
MASS EMI
C02
IB/ IK
LB FUEL
1988.27
I34U.19
1698.81
1702.60
1683.40
1300.98
1300.98
1787.43
1004.97
1497.32
1320.89
CU
LB/1K
LB FUEL
1137.42
1182.90
1182.90
107S.93
1198.23
8.10
THC
(DRY)
PPMV
1596.00
1241.00
768.00
946.00
709.00
991.00
991.00
532.00
1025.00
729.10
II43.00
MASS EMI
NO
LB/IK
LB FUEL
2.26
I. 31
7.33
4.93
5.09
4. 83
4.83
10. S3
1.38
5.97
1.63
LTD CYCLF
CO
LB/U
HOURS
11146.7C
60898.79
60898.79
21736.91
9381.67
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
81.00 0.04323
108.00 0.04764
232.00 0.04807
201.00 0.04941
199.00 0.04892
964.00 0.09619
964.00 0.09615
435.00 0.04973
382.00 0.05666
249.00 0.05008
89.00 0.
NO
IORYI
PPMV
63.00
40.00
727.00
144.00
159.00
174.00
174.00
338.09
50.00
179.00
53.00
MASS EMI
NOX
LB/IK
LB FUEL
2.26
1.31
7.13
4.93
5.09
4.83
4.83
10.53
1.38
5.57
1.6)
EMISSIONS
CO
EMISSION
LBS.
2.229
0.304
5.055
2.374
0.629
10.591
1.147
NO
2
tCRYl
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-o.oo
MASS EMI
CO
LB/HR
4607.90
11146.70
17831.94
15312.31
15615.03
6CB98.79
60898.79
30961.79
52217.22
23716.51
9381.67
HC
LB/U
LB FUEL
14.18
5.72
5.72
7.90
12.23
05085
NO
X
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
127.63
138.99
166.88
148.55
132.10
294.47
294.47
212.79
578.44
173.87
99.06
HC
LB/IK
HOURS
138.99
294.47
294.47
173.87
99.06
ALDEHYDES
IDRYI
14.00
12.00
-0.00
-0.00
-0.00
-0.00
8.00
9.00
3.00
6.00
9.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
Hf.
EMISSION
LBS.
0.028
0.001
0.024
0.017
0.007
0.078
0.008
SMOKE
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-'1.00
MASS EMI
C02
LR/MR
12724.94
13212.29
32737.02
28433.48
28112.71
66979.94
66979.14
63453.1)9
38490.22
32060.96
10698.90
Nil
Lll/lK
LB FUEL
1.31
4.33
4.D3
9.57
1.43
PtRIICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HB LB/HR
14.45 14.45
12.85 12.65
141.46 141.46
82.31 82.31
84.96 84.96
248.65 248.69
248.65 248.65
373.66 373.68
52.94 52.94
122.44 122.44
11.17 13.17
N.I NO
LB/IK EMISSION
HCURS LBS.
12.85 C.0026
241.65 0.0012
24H.65 0.0206
122.44 C.0122
13.17 0.0009
0.0376
0.0041
1-3
-------
DATEl 7/16/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEDVNE-CONTINENTAL
ENGINE DATA
CAL 10 NUMBER: 168 ENGINE TYPE AND MODEL) 0-200-4
RATED HORSEPOWER! 100.
ENGINE TOTAL TINE! 28*. MRS
FUEL: AV GAS 80/87 FUEL H/C RATIO: 1.840
OPERATIONAL DATA »««««««««««»»««««««««»
INLET AIR TEMPERATURE, DEGREES F: START 82.00 FINISH 81.00
ATMOSPHERIC PRESSURE: START 30.02 FINISH 30.02
INLET AIR KUHIDITY, CRN H20/LS AIR: 0.01
RELATIVE HUMIDITY: 51.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -O.CC, FLOU RATE. LITERS/NIK: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER: 20*598-9-AC
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOU
LB/HR
IDLE-LOU 1 -0.0 3.90
IDLE/TAXI 2 -0.0 8.90
RUN UP i -0.0 16. 7C
PUN UP-LEAN * -0.0 16.70
RUN UP-RICH 5 -0.0 16. 7C
TAKE-OFF 6 -0.0 50.60
CLIH9 7 -0.0 50.60
DESCENT 6 -0.0 35.50
DESCENT 8 -0.0 44.80
APPROACH 9 -0.0 22.00
TAXI
TESI
HUDE
[
2
3
4
5
6
1
a
a
9
10
TEST
NODE
,
2
1
4
5
6
7
8
a
9
10
TESI
NODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGRFES F
291.00
437.00
762.00
695.00
796.00
1256.00
1256.00
1233.00
1099.00
99B.OO
583.00
NASS FMI
CO
LB/1K
LB FUEL
807.49
1144.38
959.58
936.86
906.69
1107.04
1107.04
872. 82
1333.50
1102.97
1173.73
TIME IN
MOO?
NIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLF./LB
10
EXHAUST
GAS
PRESSURE
PS1A
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
N*SS EMI
HC
LB/1K
LB FUEL
29.77
16.62
10.10
10.74
9.78
7. 19
7.19
6.14
1 1.45
8.50
13.08
MEASURED
FUEL FLOW
LB/HR
8.90
50.60
50.60
22.00
fl.10
FUEL
-0.
CU
IORY)
PERCENT V
3.20
5.00
4.60
4.40
4.30
5.90
1.90
4.30
7.^0
5.50
5.70
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FURL
USED
UBS.
1.7B
0.25
4.20
2.20
0.54
8.975
.0
CO
2
lopri
PERCENT V
4.60
3.70
5.00
5.00
5.20
4.80
4.80
5.60
J.70
4.50
4.00
NASS EMI
C02
LB/1K
LB FUEL
1823. «2
1330.57
1638. B3
1672.75
1722.79
1415.11
1415.11
1786.01
1047.61
1417.92
1294.17
CO
LB/IK
LB FUEL
1144.38
1107.04
1107.04
1102.97
1173.73
B.10
THC
(DRYI
PPMV
2060.00
1268.00
845.00
881.00
810.00
669.00
669.00
528.00
1109.00
740.00
1109.00
NASS EMI
NO
LB/IK
LB FufL
1.24
1.39
6.85
4.62
6.03
5. 58
5.58
10.37
2.25
4.68
1.49
LTD CYCLE
CO
LB/IK
HOURS
10184.94
56016.20
56016.20
24265.27
9507.20
MEASURED CALCULATED
AIR FLOU F/A
LB/HR
47.00 0.03758
98.00 0.04163
198.00 0.04540
199.00 0.04448
201.00 0.04487
570.00 0.05055
570.00 0.05055
434.00 0.04653
453.00 0.05293
247.00 0.04735
83.00 0.
NO
IORYI
PPMV
30.00
37.00
200.00
132.00
174.00
181.00
IB 1.00
311.00
76.00
142.00
44.00
MASS FMI
NOX
LFI/1K
LB FUEL
1.24
1.39
6.85
4.62
6.03
5.58
5.5t
10.37
2.25
4.6B
1.49
EMISSIONS
CO
EMISSION
LBS.
2.037
0.280
4.649
2.427
0.637
10.030
1.117
NO
2
(DRYI
PPMV
-0.00
-0.00
-o.oo
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LR/HR
3149.20
10184.94
16025.02
15645.57
15141.74
56016.20
56016.20
30985.12
59740.81
24265.27
9507.20
HC
LB/IK
LB FUEL
16.62
7.19
7.19
e.5o
13.08
04622
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS EMI
HC
LB/HR
116.11
147.93
168.59
179.42
163.36
J63.7B
363.78
717.90
512.76
186.98
105.94
HC
LB/IK
HOURS
147.93
363.76
363.78
186.96
105.94
ALDEHYDES
IDRY)
13.00
12.00
-0.00
-0.00
-0.00
-0.00
7.00
5.00
7.00
7.00
10.00
NASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.030
0.002
0.030
0.019
0.007
0.087
0.010
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
71 12.90
11842.09
2736d.39
27934.92
28770.60
71604.61
71604.63
63403.21
46933.1 1
31194.17
10482.77
NO
ia/i<
LE FUEL
1.19
5.59
5.5B
4.61
1.49
PARTICULATES
-0.00
-0.00
-0.00
-o.oo
-o.oo
-0.00
-0.01
-0.00
-0.00
-0.00
-0.00
NASS EMI MASS EMI
NO N0>
LB/HH LB/HR
4.15 4.85
12.18 12.38
114. 44 114.44
77.10 77.10
100.64 100.64
282.27 282.27
282.27 282.27
360.10 368.10
100.78 100.78
102.90 102.90
12.15 12.05
NO NO
LB/IK EMISSION
HOURS LBS.
12. 3B 0.0025
282.27 O.OOM
282.27 0.0234
102.90 0.0103
12.05 0.0008
0.0384
0.0043
1-4
-------
0»IE: 7/16/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEOYNE-CONTINENTAL
ENGINE DATA
CAL 10 NUMBER! 169 ENGINE TVPE AND MODEL: 0-200-A
RATED HORSEPOWER: 100.
ENGINE TOTAL TIME! 43. HRS
FUEH AV GAS 80/87 FUEL M/C RATIO: 1.6*0
OPERATIONAL DATA «»«««»««»»«
INLET AIR TEMPERATURE. DEGREES F: START 70.00 FINISH 72.00
ATMOSPHERIC PRESSURE: START 30.24 FINISH 30.23
INLET AIR HUMIDITY, CRN H20/L8 AIR: 0.01
RELATIVE HUMIDITY: 76.oc PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLO* Kilt, LITERS/HIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
KUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER: 213378-7144
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 5.60
1 OLE/TAX 1 2 -0.0 8.10
RUN UP 3 -0.0 12.40
RUN UP-lt«N * -0.0 13.20
RUN UP-RICH 5 -0.0 14.10
TAKE-OFF 6 -0.0 49.60
CLIMB 7 -0.0 49.60
DESCENT fl -0.0 35.50
DESCENT ON 8 -0.0 44.80
APPROACH 9 -0.0 22.00
IAXI
TESI
MODE
1
2
3
4
5
6
7
8
a
9
10
TEST
MODE
1
2
3
4
5
6
7
B
a
9
10
TESI
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TFMP
DEGREES F
258.00
114.00
560.00
493.00
605.00
1121.00
1121.00
1054.00
1043.00
BIO. 00
392.00
MASS FMI
cn
LB/1K
LB FUEL
927.19
94B.43
1117.43
1107.26
991.49
1172.87
1172.87
901.64
1196.27
1163. Bl
902.23
T 1 ME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
MASS EMI
HC
Lfl/lK
LB FUEL
60.16
32.54
73.36
27.45
71.34
12.35
12.35
13.03
17.48
17.72
22. OB
MEASURED
FUEL FLOW
LB/HR
B.10
49.60
49.60
22.00
5.60
FUFL
-0.
CO
IDRYI
PERCENT V
6.10
5.70
7.00
6.40
6. ao
9.80
9.80
6.50
9.80
3.60
5.60
MASS F.MI
NO 2
LB/1K
Lfl FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LHS.
1.6?
0.25
4.12
2.20
0.38
8.560
,0
CO
2
(ORYI
PERCENT V
6.50
6.10
5.40
5.00
6.80
6.90
6.90
7.90
6.50
6.10
6.70
MASS EMI
C02
LB/IK
LB FUEL
1552.36
1594.77
1354.42
1359.19
1557. 85
1297.51
1297.51
1721.82
1246.67
1297.03
1696.06
CU
LB/IK
LU FUEL
948.43
1172.87
1172. 87
1163. Bl
902.23
5.60
THC
IDRYI
PPMV
6911.00
3415.00
7555.00
2770.00
2555.00
1802.00
1802.00
1640.00
2501.00
22B6.00
2393.00
MASS EMI
NO
LB/IK
LB FUEL
0.27
0.90
2.41
I.B2
1.68
2.9]
2.91
5.31
11.41
1.64
1.24
LIU CYCLE
cn
IB/IK
HOURS
7682.27
58174.41
58174.41
25603.76
5052.48
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
63.00 0.06193
94.00 0. C5667
135.00 0.05928
145. OC 0.05478
163.00 0.06449
540.00 0.07B63
540.00 0.07R63
428.00 0.06745
481.00 0.07723
239.00 0.06975
66.00 0.
NO
IDRYI
PPMV
11.00
33.00
92.00
64.00
70.00
148.00
148.00
233.00
569.00
74.00
47.00
MASS FMI
NOX
LB/IK
LR FUEL
0.27
0.90
2.41
1.82
1.68
2.91
2.91
5.31
11.41
1.64
1.24
EMISSIONS
CO
EMISSION
IBS.
1.536
0.291
4.878
2.560
0.339
9.555
1.116
NO
2
(ORYI
PPNV
-0.00
-0.00
-c.on
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-K.oo
MASS EMI
co
LC/HR
5192.29
7682.27
13851,. 14
14615.86
1398C.02
58174.41
58174.41
32008.31
S3592.65
25603.76
5052.48
HC
LH/IK
LB FUEL
32.54
17.35
12. .35
17.72
22.08
05836
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS tMI
HC
LB/HR
336.91
263.60
2B9.65
362.30
300.84
612.64
612.64
462. S3
783.32
389.79
123.65
HC
LB/IK
HOUPS
263.60
612.64
612.64
3B9.79
123.65
ALDEHYDES
IDRYI
10.00
20.00
-0.00
-0.00
-0.00
-0.00
6.00
13.00
6.00
4.00
6.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.053
0.003
0.051
0.039
O.OOB
0.154
0.018
SMOKE
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-O.JO
-0.00
-0.00
-0.00
MASS EM
C02
LB/HR
8693.21
12917.63
16794.84
17941.24
21965.73
64356.58
64356.58
61124.42
5585C.9H
2*534.71
9497.94
NO
LB/IK
LB FUEL
0.90
2.91
2.91
1.64
1 .24
PiRTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LP/HB LB/HR
1.54 1.54
7.31 7.31
29.91 29.91
24.01 24.01
23.64 23.64
144.31 144.31
144. Jl 144.31
ien.46 I88.»6
511.11 511.11
36.19 36.19
6.97 6.97
NC NO
LC/1K EH1SSION
HLU*S LBS.
7.31 0.0015
144. Jl 0.0007
144.31 0.0120
36.19 C.0036
6.97 0.0005
0.0182
0.0021
1-5
-------
OATEI 7/16/Tt
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEDYNE-CONTINENTAL
ENGINF DATA
CAL ID NUH8ER: 170 ENGINE TYPE AND MODEL: 0-200-4
RATED HORSEPOkER: 100.
ENGINE -TOTAL TIME: 43. MRS
FUEL: «v GAS ao/87 FUEL H/C RATIO: 1.840
DPERATIONAL DATA «»«««.
INLET AIR TEMPERATURE, DEGREES F: START 72.00 FINISH 72.00
ATMDSPHFRIC PRESSURE: START 30.23 FINISH 10.25
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 75.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOU RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: II
COMMENTS:
SERIAL NUNBERl 213178-7148
CARB. TEST FNGINE MEASURED
HEATEP. MODE RPM FUEL FLOW
LB/HR
IOLE-LOM 1 -0.0 3.90
IOLE/T4XI 2 -C.O 6.10
RUN UP 3 -0.0 15.00
RUN UP-LE4N 4 -0.0 13.20
RUN UP-RICH 5 -0.0 13.20
T4KE-OFF -0.0 49.60
CLIMB -0.0 49.60
DESCENT -0.0 35.50
DESCENT ON -0.0 42.00
APPROACH -0.0 20.20
TA«I
TEST
MODE
1
2
3
4
5
6
7
a
B
9
10
TFST
MODE
1
2
3
4
5
6
7
fl
n
0
10
TEST
MOOC
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
179.00
280.00
527.00
471.00
583.00
1076.00
1076.00
1054.00
1031.00
-0.00
-0.00
MASS EMI
CO
LB/1K
LR FUEL
B20.67
941.81
958.47
914.99
993.99
1175.87
1 175.97
915.05
1196.29
1145.96
U98.79
TIME IN
MODE
"IN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LR FUEL
46.99
35.55
21.74
29.03
20.13
13.57
13.57
13.61
17.60
1 8.36
22.66
MEASURED
FUcL FLOW
LB/HR
8.10
49.60
49.60
20.20
6.40
FUEL
-0
CO
(DRY)
PERCENT V
4.70
.90
.50
.80
.70
.60
.60
.60
.60
.30
.40
MASS EMI
.N02
LI/IK
LB FUEL
0.0
1.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
I. 62
0.25
4. 12
2.0?
0.43
8.434
0
CO
2
(DRY)
PERCENT V
6.40
6.50
7.20
6.80
7.10
6.70
6. 70
7.80
A. 50
6.10
6.50
MASS EMI
C02
LB/1K
L8 FUEL
1755.86
1754.58
1765.76
1814.08
1710.09
1299.44
1289.44
1699.16
1262.03
1323.31
1649.88
CO
LB/1K
LB FUEL
841.91
1175.87
1175.87
1145.96
898.79
6.40
THC
(DRY)
PPMV
4699.00
3593.00
2432.00
2995.00
2266.00
1935.00
1935.00
1714.00
2487.00
2322.00
2377.00
MASS FMI
NO
LB/1K
LR FUEL
0.43
1.41
4.36
2.82
3.06
3.64
3.64
5.81
12.73
2.13
1.49
LTD CYCLE
CO
LR/1K
HOURS
6618.70
58323.27
59323.27
23148.42
5752.27
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
46.00 0.05391
97.00 0.05477
181.00 0.06011
161.00 0.05514
159.00 0.06053
539.00 0.07689
539.00 O.C7689
425.00 0.06752
451.00 0.07628
220.00 0.06836
76.00 0.
NO
IDRYI
PPMV
15.00
50.00
170.00
101.00
120.00
I8l.no
181.00
255.00
627.00
94.00
54.00
N4SS EMI
NOX
LB/1K
LB FUEL
0.43
1.41
4.36
2.82
3.06
.1.64
3.64
5.81
12.73
2.13
1.49
EMISSIONS
CO
FMISSION
LBS.
1.364
0.292
4.841
2.315
0.385
9. 196
1.090
NC
2
ORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.oo
-0.00
-0.00
-0.00
-0,00
-0.00
MASS EMI
CO
LB/HR
1200.62
6818.70
12876.99
10757.83
11668.62
5H121.27
58325.27
32494.23
49824.06
23I44.42
5752.27
HC
LV1K
LO FUEL
35.35
13.57
13.57
18.36
22.6f>
05654
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
193.27
286.36
326.11
383.15
265.67
673.28
673.28
483.15
739.25
170.90
145.02
HL
LB/1K
HOURS
286.36
673.28
673.29
370.90
145.02
ALDEHYDES
(DRY)
19.00
9.00
-0.00
-0.00
-0.00
-0.00
6.00
8.00
7.00
6.00
10.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.057
0.003
0.056
0.037
0.010
0.163
0.019
SMOKE
-0.00
-0.00
-0.00
-n.oo
-o.oo
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO?
L8/HR
6847.96
14212.06
26496.13
25945.96
22937.11
63956.11
63956.31
60320.04
53005.14
26730.77
10879.20
NO
LB/1K
LB FUEL
1.41
3.64
3.64
2.13
1.48
P4RTICUIATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI M4SS EMI
Nil NOX
LP/I-R L8/MR
1.68 1.68
11.43 11.43
65.38 65.38
37.18 37.18
40.35 40.35
180.62 180.62
180.62 180.62
201.15 206.15
534.51 534.51
41.06 43.06
9.45 9.45
NO NO
LQ/1K EMISSION
HOURS LBS.
11.41 0.0023
110.62 0.0009
U0.62 0.0150
41.06 0.0043
9.45 0.0006
0.0231
0.0027
1-6
-------
DATE: 7/16/71
TEST ORGANIJATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER! leLEOYNE-CONTINENTAL
ENGINE DATA
CAL in NUMBER: 171 ENGINE TYPE AND MODEL: 0-200-*
RATED HORSEPOWER: 100.
ENGINE TOTAL TIMEI 44. MRS
FUEL: AV GAS 80/87 FUEL H/C RATIO: 1.840
OPERATIONAL DATA ».«»»»»»
INLET AIR TEMPERATURE. DEGREES F: START 72.00 FINISH 75.50
ATMOSPHERIC PRESSURE: START 30.23 FINISH 30.23
INLET AIR HUH I nilY, CRN M20/L8 AIR: 0.01
RELATIVE HUMIDITY: 73.00 PERCENT
SAMPLF LINE: TEMPERATURE, DEGREES C: -0.00. FLOU RATE. LITERS/KIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC> 1.60
NUMBER OF TESTS: II
COMMENTS:
SERIAL NUMBER: 213378-TUC
CARB. TEST ENGINE MEASURED
HEATED MODE RPM FUEL FLOM
LB/HR
IDLE-LOU 1 -0.0 3.90
IDLE/TIKI 2 -0.0 6.40
RUN UP 3 -0.0 13.20
RUN UP-LEAN 4 -0.0 13.00
RUN UP-RICH 5 -0.0 12.40
TAKE-OFF 6 -0.0 49.60
CLIMB 7 -0.0 49.60
DESCENT 8 -0.0 35. 50
DESCENT ON 6 -0.0 42.00
APPROACH 9 -0.0 21.10
TAXI
TFST
MODE
I
2
3
4
5
6
7
H
fl
9
10
TFST
MODE
7
a
a
9
in
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
r,AS
TFMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-0.00
-0.00
MASS EMI
CO
IB/ IK
LA FUEL
833.95
908.75
931.62
K90.7B
904. 94
1095.79
1095.79
902.15
1329.63
1170.23
1007. fll
TIME IN
400E
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLF./LB
10
EXHAUST
GAS
PRFSSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
39.39
29.36
24.25
26.16
23.43
19.10
19.10
17.30
18.03
16.24
IB. 24
MEASURED
FUEL FLOW
LB/HS
6.40
49.60
49.60
21.10
5.60
FUEL
-0
CO
(DRY)
PERCENT V
5.00
6.00
6.50
6.00
6.40
9.10
9.10
6.80
II .70
9.40
7.40
MASS EMI
N02
LB/ IK
LB FUEL
0.0
3. 0
0.0
0.0
0.0
0.0
o.o
0.0
0.0
0.0
0.0
FUEL
USED
LOS.
1.28
0.2S
4.12
2.11
0.38
8.130
0
CO
2
ICRVI
PERCENT V
6.70
7.00
7.30
7.30
7.60
7.40
7.40
8.20
5.80
6.60
7.20
MASS EMI
C02
LB/1K
L3 FUEL
1755.84
1665.83
1643.94
1702.86
1688.27
1400.09
1400.09
1709.31
1035.64
1291.00
1540.70
CC
LB/1K
LB FUEL
908.75
1095.79
1095.79
1170.23
1007. HI
5.60
THC
IORYI
PPMV
4124.00
3385.00
2954.00
3077.00
2893.00
2770.00
2770.00
2277.00
2770.00
2277.00
2339.00
MASS EMI
NO
Lfl/lK
LB FUlrL
fl.41
1.22
3.34
2.07
2.30
4.02
'.02
6.25
3.12
1.82
1. 16
LTU CYCLE
CO
LB/IK
HUURS
5816.02
54351.38
54351.38
24691.92
5641. 73
MEASURED CALCULATED
AIR FLOU F/A
LB/HR
46.00 0.05636
75.00 0.06201
156.00 0.06545
178.00 0.06318
147.00 0.06626
553.00 0.07795
553.00 O.C7795
425.00 0.07044
422.00 O.CB328
228.00 0.07568
64.00 0.
NO
IDRYI
'PPMV
15.00
49.00
142.00
85.00
99.00
203.00
203.00
287.00
178.00
89.00
52.00
MASS EMI
Nat
LB/IK
LB FUEL
0.41
1.22
3.34
2.07
2.30
4.02
4.0?
6.25
3.32
1.82
1.16
EMISSIONS
CO
EMISSION
IBS.
1.163
0.272
4.511
2.469
0.37%
8.793
1.082
NO
2
ICRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
-0.00
MASS EMI
CO
LB/Hrt
3252.42
5D16.C2
12297.36
13361.63
11219.99
S4351.18
543S1.3B
32026.15
55844.25
24691.92
5643.73
Hf.
LB/IK
LB FUEL
29.36
19.10
19.10
16.24
18.24
C6694
NO
X
IDRYI
PPHV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
HC
LR/HR
153.64
187.92
320. OB
392.45
290.47
947.53
947.53
614.19
757.21
342.56
102.17
HC
LB/IK
HUURS
167.92
947.53
947.53
342.56
102.17
ALDEHYDES
IDRYI
23.00
16.00
-0.00
-0.00
-0.00
-0.00
e.oo
9.00
11.00
a. oo
10.00
MASS tMI
NO 2
LR/HR
0.0
0. 0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LDS.
0.03B
0.005
0.079
0.034
0.007
0.162
0.020
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-n.oo
-0.00
-0.00
MASS til
en?
L8/MR
6B47.77
10661.12
21699.96
25542. H4
20934.58
69444. t3
69444.6)
60680.34
43496.96
27240.13
8627.90
NO
Lrt/IK
LB FUEL
1.22
4.02
4.02
1.12
1. 16
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
tin NOX
LM/HP LB/HR
1.60 1.60
7.00 7.80
44.13 44.13
31.09 31.09
28.51 28.51
199.15 199.15
U9.15 199.15
222.02 222.02
139.55 139.55
18.40 38.40
6.51 6.51
NO NO
LO/1K EMISSION
HCURS LBS.
7.40 0.0016
199.15 0.0010
199.15 0.0165
38.40 0.0038
6.51 0.0004
0.0234
0.0029
1-7
-------
DATE: 7/16/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEDYNE-CONTINENTAL
ENGINE DATA
CAL ID NUMBER: 172 ENGINE TYPE AND MODEL I 0-200-4
RATED HORSEPOWER: 100.
ENGINE TOTAL TIME: 289. MRS
FUEL: AV GAS BO/67 FUEL H/C RATIO: 1.840
OPERATIONAL DATA *««*«*»»«««*
INLET AIR TENPERATUREi DECREES F: START 78.50 FINISH 78.00
ATMOSPHERIC PRESSURE: START 30.30 FINISH 30.30
INLET AIR HUMIDITY. CRN H20/L8 AIR: 0.01
RELATIVE HUMIDITY: 67.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOW RATE. LITERS/MIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER 1 205317-9-AA
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 4.70
IDLE/TAXI 2 -0.0 8.10
RUN UP 3 -0.0 16.70
BUN UP-LEAN 4 -0.0 16.70
RUN UP-RICH 5 -0.0 15.80
TAKE-OFF 6 -0.0 50.60
CLIMB 7 -0.0 50.60
DESCENT a -0.0 35.50
DESCENT ON 9 -0.0 44.60
APPROACH 9 -0.0 22.90
TAXI
TEST
MODE
1
2
3
4
5
6
7
a
a
9
10
FFST
MOriE
1
2
1
4
5
6
7
8
3
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOT«L
EXHAUST
GAS
TEMP
DEGREES F
247.00
336.00
572.00
538.00
594.00
1065.00
1065.00
1009.00
986.00
607.00
181 .00
MASS EMI
CO
LB/1K
L« FUEL
978.93
10B5.56
1014. Bl
964.23
1049.36
1 194.32
1194.32
967.85
1234.23
1144.41
1008.21
TIME IN
MODE
1IN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LR/IK
LB FUEL
60.10
24.30
17.90
19.59
16.69
14.92
14.92
11.95
24.78
15.56
18.22
MFASUREfl
FUCL FLOW
Lb/HR
a. 10
SO. 60
50.60
22.90
7.20
FUEL
-0,
CO
(DRY)
PERCENT V
6.90
7.30
7.70
6. 70
7.80
10.90
10.90
7.60
11.30
a. 90
7.20
MISS EM!
N02
L8/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
1.62
n.25
4.20
2.29
0.4R
9.845
.0
CO
2
(DRY)
PERCENT V
6.60
6.00
7.10
7.10
7.00
7.30
7.30
a. 10
6.80
6.60
7.00
MASS EMI
C02
Lfl/lK
LB HJEL
1471.25
1401.92
1499.23
1605.47
1479.68
1256.77
1256.77
1620.76
1166.99
1333.44
1540.13
CO
LB/1K
LB FUEL
1085.56
1194.32
1194.32
1144.41
1008.31
7.20
THC
IDRYI
PPMV
7396.00
2853.00
2325.00
2377.00
2166.00
2377.00
2377.00
1638.00
3962.00
2113.00
2272.00
MASS EMI
NO
L«/1K
LO FUEL
0.21
0.66
1.85
1.84
1.41
7.36
7.36
3.89
U.49
1.56
0.99
LTQ CYCLE
CO
LP/1K
HUURS
8793.07
60432.72
60432.72
26206.86
7259.13
MEASURED CALCUIATED
AIR FLOW F/A
LB/HR
52.00 0.06634
90.00 0.06347
191.00 0.06990
195.00 0.06525
180.00 0.06986
544.00 O.C8577
544.00 0.06577
419.00 0.07344
468.00 0.08624
250.00 0.07326
84.00 0.
NO
(DRY)
PPMV
9.00
27.00
84.00
78.00
64.00
409.00
409.00
186.00
473.00
74.00
43.00
MASS EMI
NOX
LB/1K
L3 FUEL
0.21
0.66
1.U5
1.84
1.41
7.36
7.36
3.69
8.49
1.56
0.99
EMISSIONS
CD
EMISSION
LRS.
1.759
0.302
5.016
2.621
0.486
10.184
1.151
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CD
LP/HR
4t.OC.98
8793.07
17281.34
16102.63
16579.89
60437.72
60432.72
34358.69
55293.67
26206.86
7259.13
HC
LP/IK
LB FUEL
24.30
14.92
14.92
15.56
18.22
06710
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
?82.45
196. 82
29a.B5
327.19
263.69
754.78
754.78
424.11
1110.34
356.34
131.19
HC
LR/ IK
HUURS
196.82
754.78
754.78
356.34
131.19
ALDEHYDES
(DRY)
21.00
13.00
-0.00
-0.00
-0.00
-0.00
8.00
8.00
13.00
9.00
11.00
MASS FMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
O.OJ9
0.004
0.063
0.036
0.009
0.150
0.017
\
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO?
LB/HK
6914.86
11355.52
25037.06
26811.36
23373.88
63592.62
63592.62
57536.85
52281.05
30535.66
11088.90
NO
LB/1K
LB FUEL
0.66
7.36
7.36
1.56
0.99
PART1CULATES
-0.00
-O.CO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
0.99 0.99
5.34 5.34
30.97 30.97
30.79 30.79
22.15 22.35
372.47 372.47
372.47 372.47
138.12 138.12
38C.17 380.17
35.79 35.79
7.12 7.12
NO NO
IB/IK EMISSION
HOURS LBS.
5.34 0.0011
372.47 0.0019
372.47 C.0309
35.79 0.0036
7.12 0.0005
0.0379
0.0043
1-8
-------
DATE: JM6/T1
TEST ORGANUATIONI SCOTT/GEN AVIATION
ENCINE SUPPLIER: TELEOYNE-CONTINENTAL
ENGINE OAT*
C»L ID NUN8ERI IT]
ENGINE TYPE «NO NODELl 0-200-A
RATED HQRSEPOUERI 100.
2*9. MRS
FUEL H/C RMIOI 1.6*0
SERIAL NUNBERl
205)17-9-AB
FINISH
FINISH
78.30
30.26
ENGINE TOTAL TIME)
FUEL! AV GAS SO/87
OPERATIONAL DATA ««»««..«..
INLET AIR TENPERATUREi DEGREES Ft START 79.00
ATMOSPHERIC PRESSURE! START 30.26
INLET AIR HUMIDITY, GRN H20/LB AIRl 0.01
RELATIVE HUNIOITVI 69.00 PERCENT
SAMPLE LINEl TEKPERATUREi DEGREES C> -O.OOt FLOM RATEi LITERS/BIN:
SAMPLE LINE TRANSPORT TIME. SEC< 1.60
NUMBER OF TESTSl 11
COMMENTS!
CARB. TEST ENGINE MEASURED
HEATER MODE RPN FUEL FLOM
LB/HR
IDLE-LOW 1 -0.0 3.90
IDLE/TAXI 2 -0.0 T.20
RUN UP 3 -0.0 16.70
RUN UP-LEAN 4 -0.0 15.60
RUN UP-RICH 5 -0.0 14.10
TAKE-OFF 6 -0.0 49.60
CLIMB 7 -0.0 49.60
DESCENT B -0.0 35.50
DESCENT ON 8 -0.0 44.60
APPROACH 9 -0.0 22.00
TAXI
TEST
MODE
I
2
)
4
5
6
7
a
a
9
10
TEST
MODE
1
2
1
4
5
6
7
8
9
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
FXHAUST
GAS
TEMP
DEGREES F
202.00
336.00
560.00
521.00
577.00
1054.00
10)4.00
1020.00
IC09.00
818.00
415.00
MASS EMI
CO
LB/1K
IB FUEL
857.62
960.59
979.16
1)3.71
879.00
1183.57
1183.57
960.61
1270.15
1162.66
992.82
TIME IN
MODE
MIN.
12.00
0.10
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRFSSURF
PSIA
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
IB/IK
1.8 FUEL
51.89
21.81
18.97
28.10
15.94
14.36
14.36
12.10
16.72
16.62
19.81
MEASURED
FUEL FLOM
LB/HR
7.20
49.60
49.60
22.00
6.40
FUEL
-0
CO
IORY1
PERCENT V
5.60
6.30
6.90
6.30
6.00
10.50
10.50
7.40
11.10
9.70
6.70
MASS EMI
K02
LB/U
Lfl FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
1.44
0.25
4.1?
2.20
0.43
8.434
0
CO
2
IDRVI
PERCENT V
7.00
6.70
7.10
.00
.60
.20
.20
.00
.30
.20
.70
MASS EMI
C02
LB/U
i a FUEL
1684.38
1605.12
1593.40
1610.07
1749.40
1275.19
1275.19
I6II.7I
1132.69
1301.86
1559.95
CO
LB/U
LB FUEL
960.59
1181.57
1161.57
1162.66
992.82
6.40
THC
IORVI
PPMV
5916.00
2497.00
2334.00
3311.00
1900.00
2225.00
2225.00
1628.00
2551.00
2171.00
2334.00
MASS EMI
NO
LB/1K
LB FUEL
0.43
1.03
2.42
2.02
2.00
5.41
5.41
4.12
2.97
1.69
1.05
LTCI CYCLE
cn
LB/1K
HOURS
6916.22
58704.88
58704.88
25578.50
6354.07
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
45.00 0.06132
64.00 0.06169
194.00 0.06616
185.00 0.06336
170.00 0.06394
537.00 0.06319
537.00 0.08139
420.00 0.07207
465.00 0.08250
239.00 0.07061
74.00 0.
NO
(DRY)
PPMV
17.00
41.00
104.00
83.00
83.00
292.00
292.00
193.00
156.00
77.00
43.00
MASS FNI
NDX
LB/U
LB FUEL
0.43
1.03
2.42
2.02
2.00
5.41
5.41
4.12
2.97
1.69
1.05
EMISSIONS
CO
EMISSION
LBS.
1.383
0.294
4.87)
2.558
0.426
9.533
1.1)0
NO
2
IORYI
PPNV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
MASS EMI
CO
LB/HR
3344.70
6916.22
16355.30
14752.60
12391.90
58704.88
58704.88
14101.55
56902.63
25578.50
6334.07
HC
LB/U
LO FUEL
21.61
14.36
14.36
16.62
19.61
06348
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
202.37
157.00
116.85
444.05
224.78
712.46
712.46
429.66
748.97
363.56
126.77
HC
LB/U
HOURS
157.00
712.46
712.46
365.56
126.77
ALDEHYDES
(DRY)
21.00
13.00
-0.00
-0.00
-0.00
-0.00
9.00
6.00
7.00
14.00
9.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
MC
EMISSION
LBS.
0.031
0.004
0.059
0.037
0.006
0.139
0.016
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FNI
C02
IB/KB
6569.09
11556.69
26442.71
25755.14
24666.53
63249.28
63249.29
57925. «
50744.4)
26640.95
9963.67
Nil
LB/1K
LB FUEL
1.0)
5.41
5.41
1.69
1.05
PARTICIPATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NCI NOX
LP/HK LB/HR
1.67 1.6T
7.19 7.19
40.49 40.49
11.92 31.92
26.16 26.16
268.16 269.16
269.16 268.16
146.09 146.09
133.04 133.04
37.16 >7.18
6.70 6.70
SO NO
LO/1K EMISSION
HOURS LBS.
7.19 0.0015
268.16 0.001)
266.16 0.0223
37.18 0.0017
6.70 0.0004
0.0292
0.0035
1-9
-------
DATE! T/16/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEDYNE-CONTINENTAL
ENGINE DATA
CAL ID NUMBERI 174 ENGINE TYPE AND MODEL! 0-200-A
RATED HORSEPOXER: 100.
ENGINE TOTAL TINE: 290. MRS
FUEL: AV GAS 80/87 FUEL H/C RATIO: 1.840
OPERATIONAL DATA »«*»«««»«*«*»»»*»'
INLFT AIR TEMPERATURE. DEGREES F: START 80.50 FINISH 80.00
ATMOSPHERIC PRESSURE: START 30.28 FINISH 30.20
INLET AIR HUMIDITY, CRN H20/L8 AIRl 0.01
RELATIVE HUMIDITY: 64.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, L1TERS/MIN: 7.00
SAMPLE LINE TRANSPORT TINE, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBERI 20SJIT-9-AC
CARB. TEST ENGINE MEASURED
HEATFR MODE RPM FUEL FLOW
LB/HR
IDLE-LOU 1 -0.0 3.90
IDLE/TAXI 2 -0.0 7.20
RUN UP 3 -0.0 15.80
RUN UP-LEAN 4 -0.0 15.80
RUN UP-RICH 5 -0.0 16.70
TAKE-OFF 6 -0.0 49.60
CLIMB 7 -0.0 49.60
DESCENT a -0.0 35.50
DESCENT ON 8 -0.0 43.90
APPROACH 9 -0.0 22.00
TAXI
TFST
MODE
I
2
3
4
5
6
7
8
8
9
10
TEST
MODE
!
2
3
'i
*
h
7
8
a
9
10
TEST
MOOF
2
6
7
9
10
EXHAUST
GAS
TEMP
DEGREES f
224.00
392.00
67). 00
617.00
717.00
1121.00
1121.00
1065.00
1020.00
852.00
482.00
MASS EMI
CO
LB/IK
LB FUEL
866.63
1023.85
1075.25
inru.}}
IOT3.74
1091.82
1091.82
924.61
1345.20
1196.39
10R2.84
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
HC
LB/1K
LB FUEL
74.85
29.97
23.03
21.85
20.75
17.14
17.14
13.22
46.19
19.74
27.45
MEASURED
F'JEL FLOW
LB/HR
7.20
49.60
49.60
22.00
6.40
-0.
CO
IORV)
PERCENT V
6.10
7.70
8.20
7.50
8.60
9.60
9.60
7.50
12.90
9.70
8.40
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
D.O
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LOS.
1.44
0.25
4.12
2.20
0.43
.0
CO
2
(DRY)
PERCENT V
7.20
7.10
6.90
7.30
7.00
7.90
7.90
8.70
5.70
6.40
6.90
MASS EMI
C02
L8/1K
LB FUEL
1607.22
1483.34
1421.62
1536.10
1398.79
1411.71
1411.71
1685.21
933.92
1740.28
1397.56
CO
LR/1K
LB FUFL
1023.85
1091.82
1091.82
1196.39
1082.84
6.40
THC
(DRY)
PPMV
9199.00
3935.00
3066.00
2849.00
2849.00
2632.00
2632.00
1872.00
7734.00
2795.00
3718.00
MASS EMI
NO
LB/1K
LB FUEL
0.35
0.83
1.55
1.43
1.42
8.13
8.13
4.21
1.44
1.38
1.25
LTD CYCLE
CO
IB/ IK
HOURS
7371.69
54154.37
54154.37
26320.59
6930.14
MEASURED CALCULATED
AIR FLOU F/A
LB/HR
44.00 0.06(05
82.00 0.07065
177.00 0.07172
182.00 0.07008
1B6.00 0.07392
554.00 0.08237
554.00 0.08237
424.00 0.07565
419.00 0.09084
234.00 0.07646
71.00 0.
NO
(ORYI
PPMV
15.00
38.00
72.00
65.00
6B.OO
435.00
435.(10
208.00
84.00
68.00
59.00
MASS EMI
NOX
LB/IK
LB FUEL
0.35
0.83
1.55
1.43
1.42
8.13
8.13
4.21
1.44
1.38
1.25
EMISSIONS
CO
EMISSI'JN
LBS.
1.474
0.271
4.495
2.632
0.464
MO
2
ICRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
-c.oo
-0.00
-0.00
-c.oo
-0.00
MASS EMI
CO
LB/HK
3379.87
7371.69
16988.92
15870.03
18245.52
54154.37
54154.37
32823.64
59054.12
26320.59
6130.14
HC
LB/IK
IB FUEL
29.97
17.14
17.14
19.74
27.45
07296
NO
X
IORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
291.91
215.76
363.81
345.27
346.55
850.34
350.34
469.22
2027.73
434.36
175.68
HC
LB/IK
HOURS
215.76
850.34
850.34
434.36
175.68
ALDEHYDES SMOKE
(DRY)
32.00
16.00
-0.00
-0.00
-0.00
-0.00
9.00
11.00
18.00
10.00
9.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.043
0.104
0.071
0.043
0.012
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
6268.17
106B0.04
22461.52
24270.43
23359.83
70020.38
70020.88
59825.01
40999.05
27286.13
8944.38
NO
LB/IK
L8 FUEL
O.B3
8.11
8.13
1.38
1.25
PART1CULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EHI
ND NOX
LB/HR LB/HR
1.37 1.37
5.98 5.98
24.50 24.50
22.59 22.59
23.72 23.72
403.06 403.06
403.06 403.06
149.52 149.52
63.16 63.16
30.31 30.31
8.00 8.00
NO NO
LB/IK EMISSION
HOURS LBS.
5.98 0.0012
403.06 0.0020
4C3.06 0.0335
30.31 0.0030
B.OC 0.0005
TOTAL FOR CYCLE
TOTAL FOR CYCLE/LB FUEL
9.336
1.107
0.173
C.OZ1
0.0402
0.0048
1-10
-------
DATE! 7/16/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEDYNE-CONTINENTAL
ENGINE DATA ««««»«« «...
CAL ID NUMBER! 181 ENGINE TYPE AND MODEL! 0-200-A
RATED HORSEPOWER: 100.
ENGINE TOTAL TIME! 311. HRS
FUEL: AV GAS 80/87 FUEL H/C RATIO! 1.840
OPERATIONAL DATA «««««»»«»««««
INLET AIR TEMPERATURE, DEGREES H START 74.00 FINISH 75.80
ATMOSPHERIC PRESSURE! START 29.92 FINISH 29.92
INLET AIR HUMIDITY. GRN H20/L8 AIR! 0.01
RELATIVE HUMIDITY! 73.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00. FLOU RATE. LITERS/HIM! 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS!
SERIAL NUMBER: Z13
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOU 1 -0.0 4.70
IDLE/TAXI 2 -0.0 7.20
RUN UP 1 -0.0 15.80
RUN UP-RICH 5 -0.0 15.00
TAKE-OFF 6 -0.0 48.60
CLIMB 7 -0.0 48.60
DESCENT ON 8 -0.0 40.10
APPROACH 9 -0.0 22.00
TAXI 10 -0.0 6.40
RUN UP-LEAN
TEST
MODE
1
2
3
5
6
7
fl
9
10
4
TEST
MORE
1
2
3
5
6
7
B
9
10
4
TEST
100F
2
6
7
9
10
TOTAL
TOIAL
EXHAUST
GAS
TEMP
DEGREES F
314.00
404.00
628.00
673.00
1099.00
1099.00
1031.00
1087.00
448. 00
670.00
MASS EMI
CO
LB/U
LB FUEL
674. T>.
850. H
697.36
713.11
1216.81
1216.81
1204.90
1099.66
774.17
711.91
TIME IN
NODE
NIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/Lfl
4
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
IB/IK
LB FUEL
4?. 69
31.30
26.83
23.47
22.09
22.09
25.32
23.39
27.37
29.90
MEASURED
FUEL FLOW
LB/HR
7.20
48.60
48.60
22.00
6.40
FUEL
-0
CO
IORY)
PERCENT V
4.30
5.80
4.70
4.90
10.50
10.50
10.00
8.50
5.30
4.;o
MASS EMI
NO?
Lfl/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
1.44
0.24
4.03
2.20
0.43
8.346
0
CO
2
IDRYI
PERCENT V
.10
.60
.60
.70
.60
.60
.40
.80
.20
7.60
MASS EMI
C02
LB/1K
LB FUEL
1997.00
1751.61
2004.93
1989.39
1201.76
1201.76
1211.62
1382.25
1882.45
1942.21
CO
LB/IK
Lfl FUEL
850.77
1216.81
1216.81
1099.66
774.37
15.40
THC
IORYI
PPMV
4750.00
3726.00
3157.00
2816.00
3328.00
3328.00
3669.00
3157.00
3271.00
3210.00
MASS FMI
NO
IB/IK
LB FUEL
0.39
-0.00
5.00
3.18
1.75
1.75
4.02
1.51
1.39
5.08
LTD CYCLE
CO
LB/IK
HOURS
6125.56
59137.13
59137.13
24192.56
4955.94
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
59.00 0.05952
87.00 0.06385
200.00 0.06282
-0.00 0.06402
513.00 0.08133
513.00 0.08133
4?4.00 0.07878
243.00 0.07273
79.00 0.06392
-0.00 0.
NO
(DRY)
PPMV
15.00
-0.00
205.00
133.00
92.00
92.00
203.00
71.00
58.00
190.00
MASS INI
NOX
LB/IK
LB FUEL
0.39
-0.00
i.OO
.18
.75
.75
.02
.51
.39
.08
EMISSIONS
CO
EMISSION
LBS.
1.225
0.296
4.908
2.419
0.332
9.1BO
1.100
NO
2
ICRVI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
MASS EMI
CO
LP/HR
3171.18
6125.56
11018.36
10696.69
59117.13
591)7.13
48316.27
24192.56
4955.94
11271.41
HC
LB/IK
Lfl FUEL
31.30
22.09
22.09
23.39
27.37
05756
NO
X
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
200.63
225.38
423.88
352.07
1073.49
1073.49
1015.28
514.61
175.18
460.49
HC
LB/IK
HOURS
225.38
1073.49
1073.49
514.61
175.18
ALDEHYDES
IORY)
20.00
10.00
-0.00
-0.00
-0.00
6.00
3.00
6.00
6.00
-0.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.045
0.005
0.089
0.051
0.012
0.203
0.02*
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/HR
91BS.89
12611.60
31677.84
29840.83
58405.43
58405. 43
48586.06
30409.57
12047.66
29910.08
NO
LB/IK
LB FUEL
-0.00
1.75
1.75
1.51
1.39
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
1.82 1.82
-O.OC -0.00
78.94 78.94
*7.69 47.69
85.11 85.11
fl5.ll 85.11
161.11 161.11
33.19 33.19
e.91 8.91
78.17 78.17
NO NO
LB/IK EMISSION
HCIJRS LBS.
-0.00 -0.0000
8S.1I 0.0004
85.11 0.0071
33.19 0.0033
8.91 0.0006
-0.0000
-0.0000
1-11
-------
DATE! 7/16/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEOYNE-CONTINENTAL
ENGINE DATA
CAI 10 NUMBER: 132 ENGINE TYPE AND MODEL: 0-200-A
RATED HORSEPOWER: 100.
ENGINE TOTAL TINE: 311. MRS
FUEL: AV GAS 80/87 FUEL H/C RATIO! 1.8*0
OPERATIONAL DATA »««»«»»*»»»»»«««»«
INLET AIR TEMPERATURE. DEGREES F: START 75.80 FINISH 77.80
ATMOSPHERIC PRESSURE: START 29.93 FINISH 29.93
INLET AIR HUMIDITY, GRN M20/LB AIR: 0.01
RELATIVE HUMIDITY: 65.oo PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -O.CC, FlOU RATE. LITERS/MIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER: 213 US-TO-AB
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
L8/HR
IDLE-LOU 1 -0.0 4.70
IDLE/TAXI 2 -0.0 7.20
RUN UP 3 -0.0 15.00
SUN UP-LEAN * -0.0 15.00
RUN UP-RICH 5 -0.0 15.00
TAKE-OFF 6 -0.0 49.60
CLIMB 7 -0.0 49.60
OESCEMT 8 -0.0 33.70
OESCF.NT ON 8 -0.0 40.10
APPROACH 9 -0.0 22.00
TAXI
TEST
MODE
1
2
3
4
5
6
7
8
a
9
10
TEST
MODE
1
2
3
4
5
6
7
8
a
9
10
TEST
MOOE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
247.00
381.00
684.00
650.00
706.00
1087.00
1087.00
1054.00
1043.00
863.00
448.00
MASS EMI
CO
IB/IK
L8 FUEL
4Bfl. S3
667.20
692.56
683.30
573.34
1189.50
11B9.50
H79.82
1168.26
1074.99
790.53
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
47.86
28.04
22.63
24.65
20.39
42.84
42.84
36.4)
71.35
46.00
-0.00
MEASURED
FUEL FLOW
LB/HR
7.20
49.60
49.60
22.00
5.60
FUEL
-0,
CO
IDRYI
PERCENT V
2.80
4.40
5.00
4.70
3.90
10.70
10.70
6.70
10.60
8.70
5.40
MASS EMI
N02
LO/1K
lfl FUFL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUFL
USED
L8S.
1.44
0.25
4.12
2.20
0.38
8. JBO
.0
CO
2
(ORYI
PERCENT V
8.30
8.60
9.30
B. 90
9.60
6.80
6.80
8.20
6.60
7.00
8.40
MASS EMI
C02
LB/1K
I 8 FUEL
2275.35
2048.99
2023.99
2033.01
2217.46
1187. 76
1187.76
1691.90
1142.92
1359.00
1932.15
CO
IB/IK
LB FUEL
667.20
1189.50
1189.50
1074.99
790.53
5.60
THC
IDRYI
PPMV
4790.00
3229.00
2853.00
2960.00
2422.00
6728.00
672H.OO
4844.00
11303.00
6500.00
-0.00
MASS EMI
NO
LH/1K
L8 FUEL
0.75
1.49
6.23
1.30
5.22
1.94
1.94
4.59
5.39
1.64
1.49
LTD CYCLE
CO
LB/1K
HOURS
48C3.B3
58999.11
58999.11
23649.72
4426.95
MEASURED CALCULATED
AIR FLOH F/A
LB/HR
62.00 0.05345
92.00 0.06146
190.00 0.06709
191.00 0.06403
198.00 0.06310
515.00 0.08472
515.00 0.08472
398.00 0.07116
405.00 0.08552
244.00 O.C7609
70.00 0.
NO
IORYI
PPMV
26.00
60.00
274.00
13B.OO
216.00
106.00
106.00
213.00
298.00
81.00
62.00
MASS EMI
NOX
LB/1K
L8 FUEL
0.75
1.49
6.2)
3.30
5.22
1.94
1.94
4.59
5.39
1.64
1.49
EMISSIONS
CO
EMISSION
LBS.
0.961
0.295
4.897
2.365
0.297
8.814
1.052
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
MASS FMI
CD
LB/HR
2296.07
4803.83
10388.38
10249.46
8600.05
58999. 11
58999.11
29650.08
46847.07
23649.72
4426.95
HC
LB/IK
LB FUEL
28.04
42.84
42. 84
46.00
-0.00
06374
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
MASS EMI
HC
LB/HR
224.96
201.91
339.49
369.69
305.88
2124.67
2124.67
1227.72
2860.98
1011.96
-0.00
HC
LB/1K
HOURS
201.91
2124.67
2124.67
1011.96
-a. oo
ALUEHYOES
IORYI
17.00
9.00
-0.00
-0.00
-0.00
-0.00
6.00
5.00
9.00
4.00
5.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.040
0.011
0.176
0.101
-0.000
-0.000
-0.000
SMOKE
-0.00
-o.oo
-0.00
-0.00
-o.oo
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
en 2
LB/HR
10694.11
14752.72
30359.79
30495. 18
33261.84
58912.67
58912.67
57016.86
45810.95
29898.05
10620.02
NO
LB/IK
LB FUEL
1.49
1.94
I .94
1.64
1.49
PART1CULATES
-O.CO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS E"I MASS EMI
NO NDX
L6/HK LB/HR
3.50 3.50
10.76 10.76
93.51 93.51
49.43 49.43
7P.24 78.24
96.00 96.00
96.00 96.00
154.83 154.83
216.13 216.33
36.17 36.17
n.15 8.35
NT NO
Li/ IK EMISSION
HOURS LBS.
10.76 0.0022
96.00 0.0005
96.00 0.0080
36.17 0.0036
8.35 0.0006
C.0148
0.001B
1-12
-------
DUE: T/I6/7I
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEOYNE-CONTINENTAL
ENGINE DATA
CAL 10 NUMBER: 181 ENGINE TYPE AND MODEL" O-200-A
RATED HORSEPOWER: 100.
ENGINE TOTAL TINE: 311. HRS
FUEL: AV GAS 10/87 FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA ««.«««««.«...««.«»«.».....»».«...».«»......».««
INLET AIR TENPERATUREt DEGREES F: START 77.80 FINISH 77.80
ATMOSPHERIC PRESSURE: START 24.9* FINISH 29.94
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 62.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -O.OC, FLOW RATE, LITERS/MIN: T.OO
SAMPLE LINE TRANSPORT TIME. SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER: 211 I7S-70-AC
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IOLE-LOH I -0.0 4.70
IOLE/TAXI 2 -0.0 7.20
RUN UP 1 -0.0 IS. 00
RUN UP-LEAN * -0.0 14.10
RUN UP-RICH 5 -0.0 14.10
TAKE-OFF 6 -0.0 47.70
CLINK 7 -0.0 47.70
DESCENT 8 -0.0 34.60
DESCENT ON 8 -0.0 40.10
APPROACH 9 -0.0 22.00
TAXI
TEST
MODE
1
Z
3
4
5
6
7
8
a
9
in
TEST
MODE
1
2
1
4
5
6
7
8
B
9
in
TEST
MODE
2
ft
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TFMP
DEGREES F
258.00
392.00
699.00
661.00
717.00
IC99.00
1099.00
1054.00
1043.00
861.00
426.00
MASS EMI
CO
LB/IK
LB FUEL
505.02
61)8.67
666.82
710.32
622.80
1210.69
1210.69
879.00
1226.43
1092.27
755.65
TIME IN
MDOF
MIN.
12.00
0.30
5.00
b.OO
4.00
FOR CYCLE
FOR CVCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
IB/IK
L8 FUEL
34.79
14.23
11.32
12.27
9.84
11.43
11.43
18.09
27.94
22.29
25.15
MEASURED
FUEL FLOM
LB/HR
7.20
47.70
47.70
22.00
4.60
FUEL
-0
CO
(DRY!
PERCENT V
2.50
3.90
4.00
4.30
3.70
9.20
9.20
6.60
10.70
1.60
5.20
MASS EMI
NO 2
LH/IK
LB FUEL
0.0
0.0
0.0
n.o
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
L4S.
1.44
0.24
3.96
2.20
0.38
8.213
0
CO
2
(DRY)
PEKCENT V
7.20
7.40
8.00
7.80
8.20
6.00
6.00
8.40
6.30
7.00
8.40
MASS EMI
C02
LB/IK
LB FUEL
2285.29
2053.14
2095.45
2024.50
2168.69
1240.61
1240.61
1749.78
1170.60
1396.90
1917.94
CO
LB/IK
LB FUEL
688.67
1210.69
1210.69
1092.27
755.65
5.60
THC
IDRVI
PPMV
3007.00
1407.00
1186.00
1297.00
1021.00
1517.00
1517.00
2383.00
4256.00
3064.00
3022.00
MASS EMI
NO
LB/IK
LB FUEL
0.61
1.51
8.16
3.91
5.14
3.29
3.29
5.51
4.41
1.50
1.98
LTD CYCLE
CO
LB/IK
HOUHS
4958.45
57749.94
57749.94
24029.84
4231.64
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
62.00 0.04639
93.00 0.05305
194.00 0.05605
180.00 0.05662
185.00 0.05545
512.00 0.07178
512.00 0.07178
417.00 0.07042
418.00 0.08228
244.00 0.07402
69.00 0.
NO
(DRY)
PPNV
19.00
52.00
298.00
144.00
186.00
152.00
152.00
253.00
234.00
72.00
83.00
MASS EMI
NOX
LB/IK
LB FUEL
0.63
1.51
8.16
1.91
5.14
3.29
3.20
5.51
4.41
1.50
1.99
EMISSIONS
CO
EMISSION
LUS.
0.992
0.289
4.791
2.403
0.284
8.760
1.067
NO
2
ICRVI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HK
2373.61
4958.45
10002.31
10015.52
8781.43
57749.94
57749.94
3C275.07
49174.69
24029.84
4231.64
HC
LB/IK
LB FUEL
14.23
11.43
11.43
22.29
25.15
06421
NO
X
IORVI
PPMV
-0.00
-0.00
-o.oo
' -0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
HC
LB/HR
163.51
102.45
169.85
173.02
138.78
545.37
545.37
626.05
1120.34
490.33
140.85
HC
LB/IK
HOURS
102.45
545.37
545.37
490.33
140.85
ALDEHYDES
(DRY)
15.00
9.00
-0.00
-0.00
-0.00
-0.00
10.00
7.00
0.00
5.00
4.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.020
0.003
0.045
0.049
0.009
0.127
0.015
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/HK
10740.81
14782.63
31431.76
28545. "50
30578.47
59177.05
59177.05
60542.30
46941.16
30731.84
10740.48
NO
L8/IK
IB FUEL
.51
.29
.29
.50
.98
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LO/MH LB/KR
2.1)6 2.96
10. d6 10.86
122.40 122.40
55.09 55.09
72.51 72.51
156.72 156.72
156.72 156.72
110.03 1*0.63
176.66 176.66
33.04 33.04
11.09 11.09
NU NO
LB/IK EMISSION
HOURS LBS.
10.86 0.0022
106.72 0.0008
156.72 0.0130
31.04 0.0033
11.09 0.0007
0.0200
0.0024
1-13
-------
DATEl T/16/T1
TEST DRGANUATION: SCOTT/GEN »VI«TtON
ENGINE SUPPLIER: TELEOYNE-CONTINENTAL
ENGINE DATA
CAL 10 NUMBER: 184 ENGINE TYPE AND MODEL: 0-200-A
RATED HURSEPUNER: 100.
ENGINE TOTAL TIME: 809. MRS
FUEL: AV GAS 80/87 FUEL H/C RATIO: 1.840
OPERATIONAL DATA ««
INLET AIR TEMPERATURE, DEGREES F: START 79.80 FINISH 79.80
ATMOSPHERIC PRESSURE: START 30.03 FINISH 30.03
INLET AIR HUMIDITY, GRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 58.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -O.OC, FLOU RATE, L1TERS/MIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER: 199599-9-AA
CARB. TEST ENGINE MEASURED
HEATER MODE RPH FUEL FLOW
LB/HR
IDLE-LOU 1 -0.0 4.70
IDLE/TAXI 2 -0.0 7.20
BUN UP 3 -0.0 14.10
RUN UP-LEAN 4 -0.0 14.10
RUN UP-RICH 5 -0.0 14. 1C
TAKE-OFF 6 -0.0 44.80
CLIMR 7 -0.0 44.80
DESCENT 8 -0.0 38.30
DESCENT ON 8 -0.0 36.40
APPROACH 1 -0.0 21.10
TAXI
TEST
MODE
I
2
3
4
5
6
7
8
a
9
in
TEST
MODF
1
2
3
4
5
6
7
A
a
i
10
TEST
MODF
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
291.00
392.00
661.00
673.00
684.00
1143.00
1141.00
998.00
964.00
830.00
448.00
MASS Ell
CO
LB/1K
LB FUEL
975.21
085.22
996. ID
887.29
372.10
1076.76
1076.76
951.25
1285.34
1 114.44
857.60
T1MF IN
MODE
MIN.
12.00
0. 30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLF/LB
10
FXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUFL
47.75
20.40
18.24
15.60
15.39
14.77
14. 11
12.95
18.10
17.28
16.26
H6«SUREU
FUEL FLOK
LB/HR
7.20
44.80
44.80
21 .10
5.60
FUEL
-0,
CO
(DRY)
PERCENT V
7.20
6.20
6.40
6.50
6.30
8.80
9. 80
7.00
10.60
D.40
6.20
MASS EMI
N02
LB/IK
LB FUFL
0.0
0.0
0.0
0.0
0.0
0.0
o.o
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
1.44
0.22
3.72
2.11
0.18
7.86R
.0
CO
2
IDRYI
PERCENT V
7.10
7.70
7.80
a. 10
a. 10
7.50
7.50
7.70
5.80
6.60
8.20
MASS EMI
C02
LB/1K
LB FUEL
1510.99
1727.39
1716.12
1737.30
1761.76
1441.90
1441.90
1644.09
1105.04
1375.81
1782.16
CO
LB/1K
LB FUEL
885.22
1076.76
1076.76
1114.44
B57.60
5.60
THC
IDRYI
PPMV
6155.00
2495.00
2274.00
1996.00
1941.00
2107.00
2107.00
1664.00
2606.00
2274.00
2052.00
MASS EMI
NO
LB/1K
LB FUF.L
0.36
0.75
3.31
2.94
3.09
4.76
4.76
3.97
1.18
1.63
2.20
LTtl CYCLE
CO
LB/1K
HDURS
6373.60
48238.84
48238.84
23514.60
4802.57
MEASURED CALCULATED
AIR FLOU F/A
LB/HR
53. OC 0.06934
87.00 0.06558
169.00 0.06684
170.00 0.06848
171.00 0.06752
506.00 0.07667
506.00 0.07667
453.00 0.06893
375.00 0.07801
234.00 0.07099
68.00 0.
NO
IORYI
PPHV
16.00
32.00
144.00
131.00
136.00
237.00
237.00
178.00
59.03
75.00
97.00
MASS EMI
NOX
LB/IK
LB FUEL
C.36
0.75
3.31
?.94
3.09
4.76
4.76
3.97
1.18
1.63
2.20
EMISSIONS
CO
EMISSION
LBS.
1.275
0.241
4.004
2.351
0.322
A. 193
1.041
Nil
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
4583.47
6373.60
12636.09
12510.77
12296.57
48238.84
48238.84
36432.81
46786.24
23514.60
4802.57
HC
LB/IK
LR FUEL
2C.40
14.77
14.77
17. 2B
16.26
06754
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
224.41
146.90
257.14
220.03
216.98
661.49
661.49
496.01
658.77
364.58
91.03
HC
LB/IK
HOURS
146.90
661.49
661.49
364.58
91.03
ALDEHYDES
IORYI
11.00
7.00
-0.00
-0.00
-0.00
-0.00
0.0
4.00
4.00
6.00
9.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.029
0.003
0.055
0.036
0.006
0.130
0.017
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO?
LB/HR
7101.63
12437.13
24197.23
24495.94
24840. 85
64597. 17
64597.17
6296B.55
40223.40
29029.55
9980.08
NO
LB/IK
LB FUEL
0.75
4.76
4.76
1.63
2.20
PAKTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
1.67 1.67
5.40 5.40
46.70 46.70
41.42 41.42
43.60 43.60
213.39 213.39
213.39 213.39
152.17 152.17
42.77 42.77
34.49 34.49
12.34 12.34
NO NO
IB/ IK EMISSION
HOURS LBS.
5.40 0.0011
213.39 0.0011
213.39 0.0177
34.49 0.0034
12.34 0.0008
0.0241
0.0031
1-14
-------
CUTE: 7/16/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIED! TELEOYNE-CONTINENTAL
ENGINE OATi
C«L ID NUMBER: 185 ENGINE 7VPE AND NODELI 0-200-A
RATED HORSEPOWER: 100.
ENGINE TOTAL TIMEl 809. MRS
FUEL! AV GAS 80/87 FUEL H/C RATIOI 1.6*0
OPERATIONAL DATA ».
INLET AIR TEMPERATURE, DECREES F: START 78.00 FINISH 79.90
ATMOSPHERIC PRESSUREl START 30.03 FINISH 30.03
INLET AIR HUMIDITY, CRN H20/LB AIRl 0.01
RELATIVE HUMIDITY: 56.00 PERCENT
SAMPLE LINE: TEMPERATURE, OEGREES Ci -0.00, FLU* RATE, LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: II
COMMENTS:
SERIAL NUMBER: 199599-9-AB
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 4.70
IDLE/TAXI 2 -0.0 7.20
RUN UP J -0.0 13.20
RUN UP-LEAN 4 -0.0 13.20
RUN UP-RICH 5 -0.0 13.20
TAKE-OFF 6 -0.0 31.80
CL1M6 7 -0.0 31.80
DESCENT 8 -0.0 26.40
DESCENT ON 8 -0.0 37.40
APPROACH 9 -0.0 17.60
TAXI
TEST
MODF
,
2
3
4
5
&
7
a
a
4
10
TEST
MODF
I
2
1
4
5
b
7
a
d
g
10
TEST
none
2
6
7
1
10
TOTAL
TOTAL
EXHAUST
CAS
TEMP
OEGREES F
247.00
181.00
673.00
639.00
684.00
1300.00
1300.00
1110.00
986.00
863.00
460.00
USS EMI
CO
LB/1K
LB FUEL
717.00
730.99
732.87
157.34
665.54
178.66
178.66
196.64
1271. 16
916.69
618.52
USE IN
MODE
NIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
HC
LB/IK
16 FUEL
40.23
20.69
15.36
17.39
13.52
3.55
1.55
6.3*
19.06
16.78
17.40
MEASURED
FUEL FLOW
LB/HR
7.20
31.80
31.80
17.60
6.40
FUEL
-0.
CO
OKY)
PERCENT V
4.80
4.90
5.00
5.10
4.40
1.10
1.10
2.50
10.30
4.40
5.110
MASS EMI
NC12
LJMK
LB FUEL
0.0
0.0
0.0
O.P
O.C
0.0
0.0
9.0
0.0
0.0
0.0
FUEL
USED
LBS.
1.44
0.16
2.64
1.76
0.43
6.427
,0
CO
2
IORY)
PERCENT V
7.90
8.40
8.60
a. 30
8.80
11.30
11.30
10.10
5.80
7.50
8.30
MASS EMI
C02
LB/IK
LB FUEL
1905. U7
1968.93
1980.59
1936.58
2091.43
2B63.77
2883.77
2530.50
1124.68
1687.89
1840.42
CO
LB/U
LB FUEL
730.99
178.66
178.66
916.69
818.52
6.40
THC
IORVI
PPMV
4575.00
2022.00
1830.00
2045.00
1561.00
382.00
382.00
694.00
2697.00
2045.00
2153.00
MASS EMI
ND
LU/1K
LB FUEL
0.55
1.74
A.9D
2.93
7.58
40.55
40.55
21.91
1.66
2.61
2.85
LTD CYCLE
CO
LR/1K
HOURS
5263.09
5681.51
5661. 51
16133.79
5298.52
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
SB. 00 0.06090
91.00 0.06254
168.00 0.06360
166.00 0.06286
171.00 0.06156
470.00 0.05663
470.00 0.05663
370.00 0.05802
385.00 0.07664
210.00 0.06044
79.00 0.
NO
IDRYI
PPHV
22.00
71.00
290.00
120.00
305.00
1520.00
1520.00
913.00
82.00
111.00
123.00
MASS Fit
NOX
L8/1K
LH FUEL
0.55
1.74
6. 98
2.91
7.58
40.55
40. ?5
23.91
1.66
2.61
2.85
EMISSIONS
CO
EMISSION
LBS.
l.OM
0.023
0.472
1.613
0.351
3.517
0.547
NO
2
IORYI
PPMV
-0.01
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-o.oa
-o.oo
-0.00
-0.00
MASS EMI
CO
LB/HR
3463.92
5263.09
9673.90
9996. 85
8785.14
5681.51
5681.51
10524.21
47341.18
16111.79
5238.52
HC
LB/IK
LB FUEL
20.69
3.55
3.55
16.78
17.40
06616
NO
X
IORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
L8/HR
189.09
148.99
202.78
229.58
178.50
113.00
113.00
167.32
712.95
295.25
111.37
HC
LB/IK
HOURS
146.99
113.00
113.00
295.25
111.37
ALDEHYDES
IORY)
13.00
10.00
-o.oo
-o.oo
-o.oo
-o.oo
3.00
-0.00
2.00
6.00
6.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
hC
EMISSION
LBS.
C.030
0.001
0.009
0.030
0.007
0.077
0.012
S10KE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 7
Lfl/HR
8957.60
14176.29
26141.60
25562.85
21606.86
91703.88
91703.83
66805.06
42062.66
29706.60
11778.70
NO
LB/IK
LB FUEL
1.74
40.55
40.55
2.61
2.H5
PARTICULARS
-O.CO
-0.00
-O.CO
-0.00
-0.00
-0.00
-0.00
-O.CO
-0.00
-0.00
-0.00
MASi FMI MASS EMI
NO NUX
LO/HR LB/HR
2.61 2.61
12.53 12.53
92.16 92.16
38.64 38.64
100.03 100.03
1289.54 1289.54
1289.54 1289.54
631.31 631.31
62.17 62.17
45.96 45.96
19.25 18.25
NCI NO
LR/IK EMISSION
HOURS LBS.
12.53 0.0025
1219.54 0.0064
1289.54 0.1070
45.96 0.0046
18.25 0.0012
0.1218
0.0190
1-15
-------
DATE! 7/16/T1
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEOYNE-CONTINENTAL
ENGINE DATA
CAL ID NUMBER" 186
ENGINE TYPE AND MOOELI 0-200-A
RATEO HORSEPOKER: 100.
809. MRS
FUEL H/C RATIO: 1.840
SERIAL NUMBER! 199599-4-AC
FINISH
FINISH
60.00
90.03
ENGINE TOTAL TIME:
FUEL! AV GAS 80/87
OPERATIONAL DATA ««»«««««
INLET AID TEMPERATUREi DEGREES F: START 80.00
ATMOSPHERIC PRESSURE: START 30.03
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 53.00 PERCENT
SAMPLE LINE: TEMPERATUREt DEGREES C: -0.00, FLOM RATE, LITERS/HIN:
SAMPLE LINE TRANSPORT TINE, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
CARD. TEST ENGINE MEASURED
HEATER MODE KPN FUEL FLOW
L8/HR
IDLE-LOW 1 -0.0 4.70
IDLE/TAXI 2 -0.0 7.20
RUN UP 3 -0.0 13.20
RUN UP-LEAN 4 -0.0 13.20
RUN UP-RICH 5 -0.0 13.20
TAKE-OFF 6 -0.0 49.60
CLIMB 7 -0.0 49.60
DESCENT 8 -0.0 32.80
DESCENT ON 8 -0.0 37.40
APPROACH 9 -0.0 22.00
TAXI
TEST
MODE
1
2
3
4
5
&
7
8
8
9
10
rest
MOUE
1
2
3
4
5
6
7
9
a
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
280.00
426.00
751.00
684.00
785.00
1188.00
1189.00
1099.00
1031.00
108.00
504.00
MASS EMI
CO
LB/IK
LO FUEL
846.05
916.95
SOT. 31
809.79
603.10
1126.25
1126.25
998.87
1300.10
1158.96
927.57
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
FXHAUST
GAS
PRESSURE
PSIA
-n.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
50.64
27.65
16.54
17.9?
13.52
14.80
14.80
12.88
17.08
17.09
20.77
MEASURED
FUEL FLOW
LB/HR
7.20
49.60
49.60
22.00
6.40
FUEL
-0,
CO
IIMY)
PERCENT V
6.00
5.80
6.00
5.70
4.20
9.60
9.60
7.80
11.30
9.20
7.20
MASS EMI
NC12
LB/IK
LB FUF.L
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
(1.0
0.0
o.o
FUEL
USED
LBS.
1.44
0.25
4.12
2.20
0.43
8.434
.0
CO
2
IORY)
PERCENT V
7.70
8.20
B. 80
8.10
9.70
7.40
7.40
7.80
6.00
6.60
U.20
MASS EMI
CO 2
LB/IK
LB FUEL
1705.99
1814.76
1860.41
1852.73
2189.23
1364.06
1364.06
1569.45
1084.64
1306.36
1659.84
CO
LB/IK
IB FUEL
816.95
1126.25
1126.25
1158.96
927.57
6.40
THC
IORYI
PPMV
6270.00
3428.00
2146.00
2202.00
1644.00
2202.00
2202.00
1756.00
2592.00
2369.00
2815.00
MASS EMI
NO
LB/IK
L8 FUFL
0.39
1.76
2.54
2.15
4.01
2.39
2.39
2.57
0.81
1.20
1.33
LTD CYCLE
r.o
LR/IK
HOURS
5682.04
55862.00
55802.00
25497.16
5936.45
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
55.00 O.C6640
88.00 0.06632
164.00 0.06925
163.00 0.06572
174.00 0.06456
548.00 0.08003
548.00 0.08003
382.00 0.07313
381.00 0.08217
239.00 0.07478
76.00 0.
NO
(DRY)
PPMV
17.00
76.00
115.00
92.00
170.00
124.00
124. 00
122.00
43.00
58.00
63.00
MASS EMI
NOX
LB/IK
Lfl FUEL
0.39
1.76
2.54
2.15
4.U1
2.39
2.39
2.57
0.81
1.20
1.33
EMISSIONS
CO
FHISSION
LBS.
1.176
0.279
4.637
2.550
0.398
9.040
1.072
NO
2
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
cu
L6/HR
3976.45
5882.04
10656.46
10689.19
7963.50
55862.00
55862.00
32763.03
48623.59
25497. 16
5936.45
HC
LB/IK
L6 FUEL
27.65
14.80
14.80
17.09
20.77
07255
NO
X
IDRYI
PPHV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
?37.99
199.11
2 1 B . 29
236.50
178.53
733.85
733.85
422.43
638.78
376.02
132.93
HC
LB/IK
HOURS
199.11
733.85
733.85
376.02
132.93
ALDEHYDES
IORYI
21.00
13.00
-0.00
-0.00
-0.00
-0.00
7.00
6.00
19.00
11.00
9.00
MASS EMI
N02
IB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.040
0.004
O.Ool
0.038
0.009
0.151
0.018
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
L3/HR
8018.13
13066.29
24557.42
24456.04
28697.77
67657.38
67657.38
51478.07
40565.63
28739.97
10622.97
NO.
LB/IK
LB fUFL
1.76
2.39
2.19
1.20
1.13
PARTICUIATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HH LB/HR
1.85 1.85
12.66 12.66
33.55 33.55
28.34 28.34
5?. 94 52.94
118.52 118.52
118.52 118.52
84.17 84.17
30.39 3C.39
26.40 26.40
8.53 8.53
NO NO
LB/IK EMISSION
HflURS LBS.
12.66 0.0025
118.52 0.0006
118.52 0.0098
26.40 0.0026
8.53 0.0006
0.0162
0.0019
1-16
-------
DATE: 7/16/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEOYNE-CONT INENTAL
ENGINE 0»H
CAl 10 NUMBER! 167
ENGINE TYPE AND MODEL: 0-200-A
RATED HORSEPOUER: 100.
952. MRS
FUEL H/C RATIO: 1.840
SERIAL NUMBER: 199196-8-AA
FINISH
FINISH
86.50
21.11
ENGINE TOTAL TINE:
FUEL: 4V CIS 80/87
OPERATIONS DAT* ««««««««»««««««»«
INLET AIR TEMPERATURE, DEGREES F: START 8».00
ATMOSPHERIC PRESSURE: START 24.97
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVF HUMIDITY: 50.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOK RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS!
CARB. TESf ENGINE MEASUKFO
HEATER HODt RPN FUEL FLOH
LB/HR
IDLE-LOW 1 -0.0 4.70
IDLF/Ti«l 2 -0.0 a. 10
RUN UP 3 -0.0 11.20
RUN UP-LEAN 4 -0.0 14.10
RUN UP-RICH 5 -0.0 14.10
TAKE-OFF 6 -0.0 44.60
CLIMB 7 -0.0 49.60
DESCENT 8 -0.0 13.70
DESCENT (IN 8 -0.0 40.10
APPROACH 9 -0.0 21.10
TAXI
TFSI
MODE
1
2
)
4
5
6
7
a
a
9
10
Tt-ST
HOOfc
1
2
1
4
5
&
7
S
q
9
10
TFST
HOOF
2
6
7
)
10
TIITAL
im«L
EXHAUST
GAS
TEMP
DEGREES F
125.00
426.00
695.00
661.00
706.no
1087.00
1087.00
1031.00
1009.00
852.00
460.00
MASS EMI
cn
LB/1K
13 FUEL
1049.79
1147.20
H20.70
780.41
804.6%
1207.04
1207.04
RSI. 97
1265.71
1104.02
1104.61
TIME IN
MODE:
M1N.
12.00
0.10
s.no
6.00
4.00
FOR CYCLE
FOR CYCIF/LB
10
EXHAUST
GAS
PXESSURC
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-o.ro
MASS EMI
HC
LA/IK
LB FUEL
111.22
15.71
19.55
20.21
19.04
20.23
20.21
15.82
27.71
20.61
26.32
MEASURED
FUEL FLUB
LB/HR
8.10
49. 60
44.60
?i. in
6.40
FUE1
-0
CO
IrtRYl
PERCENT V
7.20
7.50
5.00
4.60
4.90
1.00
4.00
5.40
9.50
1.40
i.7n
MASS EMI
N02
LB/1K
LR FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
n.o
0.0
FUEL
USED
LBS.
1.62
0.25
4.12
t. 11
n.lt
d. 524
0
CO
2
(ORVI
PERCENT V
5.10
5.30
7.10
7.10
7.20
5.80
5.80
7.20
5.30
5.*0
6.00
MASS EMI
C02
LB/IK
LB FUEL
1214. IB
1271.77
1831.10
1D92.60
IB57.71
1222.21
1222.21
1784.05
1109.49
1381.04
1358.56
CO
LB/IK
LB FUEL
1 147.20
1207.04
1207.04
1 104.02
1109. 6>
6.40
THC
irmri
PPMV
11559.00
4076.00
2080.00
2080.00
2024.00
2634.00
2634.00
1747.00
3632.00
2412.00
3169.00
MASS EMI
Nil
IB/IK
L1) FUEL
0.10
0.43
4.13
2.42
3.51
2.64
2.69
7.92
3.00
2.18
0.44
LTD CYCLE
Cll
LO/1K
HOURS
4242.12
548(.9.13
54864. 13
23294.71
7101.64
MEASURED CALCULATED
AIR FLOH F/A
LR/HK
47.00 0.06494
86.00 0.06191
162.00 0.05717
175.00 0.05531
174.00 0.05712
526.00 0.07049
526.00 0.07049
410.00 0.05432
412.00 0.0711)
234.00 O.C6330
70.00 0.
NO
IORYI
PPHV
4.00
17.00
I53.no
87.00
130.00
122.00
122.00
305.00
1)7.00
89.00
42.00
HASS EMI
NDX
LB/IK
LB FUEL
0.10
0.41
4.1)
2.42
3.51
2.64
2.64
7.92
3.00
2.18
0.99
EMISSIONS
CO
EMISSION
LBS.
1.H5U
0.299
4.969
7.124
0.476
9.41?
1.165
NO
2
IOHYI
PPMV
-o.oo
-0.00
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
-c.oo
-o.oo
-c.oo
-c.oo
fASS EMI
CO
Lfl/HK
4933.98
9292.32
10833.23
11001.73
11345.54
59864.13
5486S.13
28778.41
50755.00
23294.77
7101.64
hC
Lb/lK
Ld FUEL
35.71
20.21
20.23
2P.6I
26. 12
06551
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
MASS tMI
HC
LB/HR
532.15
289.23
258.11
J84.46
268.40
1001.51
ino3.5l
513.24
1111.14
4)4.86
168.45
HC
LB/IK
HOURS
284.2)
1003.51
1001.51
434. R6
168.45
ALOEHVDES
(OR VI
5.00
11.00
-0.00
-0.00
-0.00
-0.00
a. oo
7. on
7.00
6.00
9.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
o.o
0.0
n.o
c.o
0.0
HC
EMISSION
ins.
0.05ft
G.005
o.oe)
0.043
0.011
0.201
0.024
SMOKE
-0.00
-0.00
-0.10
-0.00
-0.00
-0.00
-o.no
-o.oo
-o.oo
-o.no
-0.00
MASS FMI
CC12
Lfl/HR
5706.62
10317.56
24170.45
26685. 6d
26194.00
60621. *0
60621.50
60290.84
44490.71
29102.14
8694.75
NO
LB/U
LB FUEL
0.4)
2.69
2.69
2.11
0.99
P«RTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-P. 00
-0.00
-0.00
-0.00
MASS EMI MASS EHI
NO NUX
LR/HR L8/HR
0.4 0.45
1.4 3.46
54.4 54.45
34.1 34.10
49.4 49.44
133.30 133.30
1)3.30 133.30
266.49 266.94
120.23 120.23
46.02 46.02
6.36 6.36
NO NO
LS/1K EMISSION
MCURS LOS.
1.46 0.0007
133.30 0.0007
133.30 C.01II
46.02 0.0046
(. .36 O.OO04
0.0175
0.0020
1-17
-------
OATEl 7/16/71
TEST ORGANIZATION: SCOTT/CEN AVIATION
ENGINE SUPPLIER! TELEOYNE-CONTINENTAl
ENGINE DATA
CAL ID NUMBER: IBB ENGINE TYPE AND MODEL i O-ZOO-A
RATED HORSEPOWER: 100.
ENGINE TOTAL TINE: 952. MRS
FUEL: AV GAS 80/87 FUEL H/C RATIC: 1.840
OPERATIONAL DATA »»«««»««««»«««««««««««««««««««
INLET AIR TEMPERATURE! DEGREES F: START 86.50 FINISH 88.00
ATMOSPHERIC PRESSURE: START 29.97 FINISH 29.97
INLET AIR HUMIDITY. CRN H20/L8 AIR: 0.01
RELATIVE HUMIDITY: 48.00 PERCENT
SAHPLE LINE: TEMPERATUREf DEGREES C! -O.CC. FLCN RATE, LITERS/MIN: 7.00
SAMPLE LINE TRANSPORT TINEf SEC: 1.60
NUMBER OF TESTS: II
COMMENTS:
SERIAL NUMBER: 199196-B-AB
CARS. TFST FNGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 2.20
IDLE/TAXI 2 -0.0 6.40
RUN UP 3 -0.0 13.20
RUN UP-LEAN 4 -0.0 13.20
RUN UP-RICH 5 -0.0 12.40
TAKE-OFF 6 -0.0 49.60
CLIMB 7 -0.0 49.60
OF.SCENT 8 -0.0 31.80
DESCENT ON 8 -0.0 41.10
APPROACH 9 -0.0 21. 1"
TAXI
TEST
MODE
1
2
3
4
5
6
7
8
a
9
10
TEST
xnoE
,
^
3
4
5
6
7
3
fl
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
291.00
404.00
684.00
650.00
695.00
1C87.00
1087.00
1043.00
1043.00
R63.00
437.00
MASS EMI
cn
LB/1K
LB FUEL
937.86
1009. 32
656.71
702.42
520.07
1226.61
1226.61
842.17
1240.82
1046.78
1065.37
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PKFSSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
IB/ IK
LB FUEL
82.76
27.92
19.06
18.85
15.26
19.28
19.28
13.73
54.05
19.57
22.64
MEASURFP
FUEL FLOW
LB/HR
6.40
49.60
49.60
21 .10
4.70
FUEL
-0,
CO
(DRY)
PERCENT V
4.20
6.70
3.90
4.10
).00
9.20
9.20
5.40
9.60
7.40
7.10
MASS EMI
NII2
Lfl/U
LB FUEl
0.0
0.0
0.0
0.0
0.0
0.0
n.o
0.0
0.0
0.0
0.0
FUEL
USER
LBS.
1.28
0.25
4.12
2.11
0.31
B. 070
.0
CO
2
(DRY)
PERCENT V
6.20
6.40
7.90
7.50
8.50
5.70
5.70
7.40
5.30
6.00
6.10
M»SS EMI
C02
L8/1K
LB FUEL
1473.60
1513.36
2090.13
2018.88
2315.24
1194.07
1194.07
1813.33
1076.34
1397.26
1438.18
CO
LB/1K
LB FUEL
1008.32
1226.61
1226.61
1096.78
1065.37
4.7U
THC
IDRY)
PPMV
9553.00
3239.00
1976.00
1921.00
1537.00
2525.00
2525.00
1537.00
7302.00
2306.00
2635.00
MASS EMI
NO
LB/1K
LB FUEL
0.60
1.16
11.89
4.22
10.82
2.67
2.67
8.38
4.86
2.00
1.06
LTO CYCLE
CO
LB/1K
HOURS
6453.24
60839.69
60039.69
23142.10
5007.25
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
24.00 0.06232
73.00 0.06259
171.00 0.05551
169.00 0.05466
166.00 0.05376
523.00 0.07094
523.00 0.07094
390.00 O.C6010
411.00 0.07332
734.00 0.0b369
53.00 0.
NO
(OR VI
PPMV
24.00
47.00
430.00
150.00
380.00
122.00
122.00
327.00
229.00
B2.00
43.00
MASS FMI
NOX
LB/IK
LB FUEL
0.60
1.16
11.89
4.22
10.82
2.67
2.67
8.38
4. 86
2.00
1.06
EMISSIONS
CO
EMISSION
L6S.
1.291
0.304
5.050-
2.314
0.335
9.294
1.152
NO
2
IDRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HH
2063.30
6453.24
866B.54
9271.89
6448.82
60839.69
60839.69
26781.11
50997.65
23142.00
5007.25
HC
L3/1K
LB FUEL
27. 9Z
19.28
19.29
19.57
22.64
062B7
NO
X
I DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
182.08
178.67
251.54
248.80
1B9.23
956.33
956.33
436.57
2221.60
413.02
106.43
HC
LB/IK
HOURS
179.67
956.33
956.33
413.02
106.43
ALDEHYDES
IORYI
20.00
1 1.03
-0.00
-0.00
-0.00
-0.00
22.00
23.00
26.00
8.01
-0.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
FMISSIUN
LBS.
0.036
0.005
0.079
0.041
0.007
0.168
0.021
SXIIKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
L8/HH
3241.91
9685.48
27589.68
26649.18
28708.92
59225.08
59225.98
57663.98
44237.76
29482.11
6759.42
NO
LB/1K
L8 FUEL
1.16
2.67
2.67
2.00
1.06
PARTICULATES
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.01
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
1. 31 1.31
7.44 7.44
156.99 156.99
55.72 55.72
134.17 134.17
132.52 132.52
132.52 132.52
266. 18 266.38
199.82 199.82
42.12 42.12
4.98 4.98
NO NO
LB/1K EMISSION
HOURS LBS.
7.44 0.0015
U2.52 0.0007
132.52 0.0110
42.12 0.0042
4.98 0.0003
0.0177
0.0022
1-18
-------
DATE: 7/16/71
itst ORGANIZATION: scorr/GEN AVIATION
ENGINE SUPPLIER: TELEOYNE-CONTINENTAL
FNG1N
CAL 10 NU'BERl 189 ENGINE TYPE AND NOOELl 0-200-4
BATED KORSEPOUERI 100.
ENGINE TOTAL TINEl 953. MRS
FUEL: AV GAS 80/67 FUEL H/C RATIOl 1.640
OPERATIONAL RAT A »
INLET AIR TEMPERATURE. DEGREES F: START 88.SO FINISH 88.50
AIHOSPHERIC PRESSURE: START 29.96 FINISH 29.46
INLET AIR HUMIDITY, CRN H20/LB AIRl 0.01
RELATIVF HUMIDITY! 46.00 PERCENT
SAPPLE LINE: TEMPERATURE, CEGREES C" -0.00. FLOW RATE, LITERS/NIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER! 199196-8-AC
CARB. TEST ENGINE PEASURFD
MEATE1 NODE RPM FUEL FLOX
L8/HR
IQir-LOU 1 -0.0 3.00
IOLE/TAXI 2 -0.0 5.60
BUS UP 3 -0.0 13.20
RUN UI'-LF AN 4 -0.0 12.40
RUN UP-RICH 5 -0.0 12.40
TAKF-OFF 6 -0.0 48.60
CLI1H 7 -0.0 48.60
(1FSCEN1 8 -0.0 31.80
DESCENT ON a -o.o 39.20
APPROACH 9 -O.n 19.30
TAXI
irsr
mini
i
2
\
i
5
6
1
a
.1
9
10
rfsT
MODF
1
2
a
q
10
Itbl
HOOE
?
6
V
0
10
FOUL
1UIAL
CXHAUS 1
CAS
T"=HP
QKGHf.ES F
2d0.on
392.00
7<*o. on
71 7.00
740.00
1199.00
1 199.00
1121.00
1041.00
903.00
492.00
1ASS E:tl
CM
IB/IK
LB FUEL
793.49
904.74
6M.75
699. IB
501.21
1100.37
1100.37
894.87
1336.66
1100.72
1020.74
lIMe |N
MODE
MIN.
12.00
0.10
5.00
6.01
4.0T
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
HC
LB/1K
LB FUEL
61.48
23.08
18.46
18.54
16.64
17.30
IT. 30
14.87
27.56
20.91
23.48
MEASURED
FUEL FLOb
L8/HR
5.60
48.60
48.60
19.30
5.60
FUEL
-0
CD
IORY)
PERCENT V
5.60
.90
.00
.10
.60
.40
.40
.00
1 .ifl
.10
.20
MASS EMI
Nil?
IB/ IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
IBS.
1.12
0.24
4.03
1.91
0.3B
7.702
I)
Cll
2
IORVI
PERCENT V
7.90
8.20
10.30
9.40
10.70
7.60
7.60
B.60
5.80
7.30
7.70
MASS EMI
CU2
LB/IK
LB FUFL
1758.82
1689.37
2159.26
2024.82
2340.98
1397.86
1397.86
1727.41
998. 4S
1187.39
1506.01
CO
LB/1K
LB FUEL
904.74
1100.37
1100.37
1100.72
1020.74
5.60
THC
IORYI
PPMV
7576.00
3074.00
2416.00
2361.00
2086.00
2580.00
2580.00
2031.00
4392.00
3019.00
3294.00
MASS EMI
NO
LB/IK
LB FUEL
0.72
1.36
8.59
3.02
17.81
4.04
4.04
5.1?
1.28
1.81
1.23
LTD CYCLE
CO
LB/IK
HOURS
5066.52
53478.04
53478.04
21243.91
5716.12
MEASURED CALCULATED
AIR FLOW F/A
L6/HR
36.00 0.06601
66.00 0.07127
173.00 0.06913
158.00 0.06776
167.00 0.06629
542.00 0.08012
542.00 0.08012
383.00 0.07798
367.00 O.C8640
214.00 0.07764
63.00 0.
NO
IORYI
PPMV
31. 00
63.00
392.00
134.00
560.00
210.00
210.00
244.00
71.00
91.00
ftO.O'l
MASS ftl
NOX
LB/U
LB FUEL
0.72
1.36
8.59
3.02
12.81
4.04
4.04
5.12
1.28
l.BI
1.23
EMISSIONS
CO
EMISSION
IBS.
1.013
0.267
4.439
2.124
0.383
8.227
1.068
NO
i
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS FNI
CO
LB/HR
23HC.48
5066.52
6101.43
9669.84
6215.84
53478.04
53478.04
28456.70
52396.86
21243.91
5716.12
HC
LB/U
LB FUEL
23.08
17.30
17.30
2C.9I
23.48
07S2B
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
184.44
129.27
243.69
229.87
206.28
840.64
040.6*
472.87
1080.32
403.65
1 J1.51
HC
LB/IK
HOURS
129.27
840.64
840.64
403.65
131.51
ALOEHYOFS
IDRVI
29.00
9.00
-0.00
-0.00
-0.00
-0.00
11.00
10.00
13.00
10.00
B.OO
MASS EMI
NC2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.026
0.004
0.070
0.040
0.009
0.149
0.019
SMOKE
-0.00
-0.00
-0.30
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS E*I
CO 2
LB/HK
5276.45
9460.46
28502.26
25107.70
29028.20
67935.88
67935.89
54931.71
39139.22
25776.50
H43I.66
NO
LB/IK
LA FUEL
.36
.04
.04
.81
.23
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
IE/MR LB/HR
2.16 2.16
7.60 7.60
113.40 113.40
37.42 37.42
158.82 158.82
196.24 196.24
196.24 196.24
162.93 162.93
50.09 50.09
34.89 34.89
6.87 6.87
NO NO
LB/IK EMISSION
HOURS LBS.
7.60 0.0015
196.24 0.0010
196.24 0.0163
34.89 0.0035
6.87 0.0005
0.0227
0.0030
1-19
-------
DATE: 7/16/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEDYNE-CONTINENTAL
ENGINE DATA
C»L ID NUMBER! 190 ENGINE TYPE AND MODEL1 0-200-A
RATED HORSEPOWER: too.
ENGINE TOTAL TINE: 714. MRS
FUEL: AV GAS 80/87 FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA *»»»»»»»«»
INLET AIR TEMPERATURE, DEGREES F: START 90.50 FINISH 67.50
ATMOSPHERIC PRESSURE: START 29.as FINISH 29.as
INLET AIR HUMIDITY, CRN H20/LH AIR: 0.01
RELATIVE HUMIDITY: 50.OC PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER: 204579A
CARB. TFST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
1 OLE-LOW 1 -0.0 2.20
IDLE/TAXI 2 -0.0 7.20
RUN UP 3 -0.0 19.30
RUN UP-LEAN 4 -0.0 15.80
HUN UP-RICH 5 -0.0 16.70
TAKE-OFF 6 -0.0 49.60
CLIHR 7 -0.0 49.60
DESCENT 8 -0.0 34.60
OFSC6NT UN 8 -0.0 39.20
APPROACH 9 -0.0 21.10
TAXI
TEST
MODE
1
2
3
4
5
6
1
a
a
9
10
TEST
MODE
1
2
3
4
5
6
7
8
e
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
325.00
426.00
673.00
65C.OO
695.00
1076.00
1076.00
1054.00
1031.00
841.00
437.00
MASS EMI
CO
LB/IK
LB FUEL
1006.62
1045.68
887.77
878.23
897.09
1242.10
1242. 10
387.43
1207.14
1 123.11
997.82
T IMF IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLF/LB
10
EXHAUST
CAS
PKESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
53.22
24.21
18.73
19.52
16.13
18.83
18.83
13.47
20.09
19.01
21.00
MFASURED
FUEL FLHK
LB/HR
7.20
49.60
49.60
21.10
7.20
FUEL
-0.
co
(01YI
PERCENI V
a. 20
It. 30
6.70
6.50
6.80
11.00
11.00
6.80
10.40
9.10
8.20
MASS EMI
NU2
IB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
1.44
0.25
4.12
2.11
0.48
8.397
,0
CO
2
(DRY)
PERCENT V
7.50
7.40
8.30
8.20
8.30
6.60
6.60
a. 50
6.70
7.00
8.10
MASS EMI
C02
LB/IK
LB FUEL
1446.61
1464.84
1727.98
1740.79
1720.46
1170.97
1170.97
1742.94
1222.11
1357.43
1548.67
CO
LB/IK
Lfl FUEL
1045.68
1242.10
1242.10
1123.11
997.82
7.20
THC
IORYI
PPMV
7570.00
3355.00
2468.00
2523.00
2135.00
2911.00
2911.00
1802.00
3022.00
2690.00
3022.00
MASS EMI
ND
LB/IK
LB FUEL
0.44
1.01
4.14
2.55
2.71
1.74
1.74
6.67
3.30
2.53
1.50
LTD CYCLF
CO
LB/IK
HOURS
7528.87
61608.27
61608.27
23697.54
7184.27
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
24.00 0.07640
82.00 0.07448
232.00 0. 07C49
190.00 0.06916
201.00 0.07080
519.00 0.08349
519.00 0.08349
418.00 0.07151
416.00 0.08115
233.00 0.07619
84.00 0.
NO
(DRY)
PPMV
22.00
49.00
190.00
115.00
125.00
94.00
94. GO
311.00
173.00
125.00
75.00
MASS [Ml
NOX
LB/IK
LB FUEL
0.44
1.01
4.14
2.55
2.71
1. 74
1.74
6.67
3.30
2.53
1.50
EMISSIONS
CO
EMISSION
LBS.
1.506
n.3oa
5.113
2.370
0.481
9.778
1.164
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.oo
-0.00
-o.oo
MASS EMI
CO
LB/HR
2214.56
7528.87
17133.85
13876.00
14981.41
616C8.27
61608.27
307C5.C8
47327.68
23691.54
7184.27
HC
L8/1K
LB FUFL
24.21
18.83
18.83
19.01
21.06
07687
NO
X
(DRY)
PPMV
-0.00
-0.00
-O.OC
-O.OP
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
117.09
174.30
361.47
308.47
269.39
933.76
933.76
466.02
787.63
401.20
151.64
HC
L8/IK
HOURS
174.30
933.76
933.76
401.20
1 5 1 . 64
ALDEHYDES
IORY)
25.00
20.00
-0.00
-0.00
-0.00
-0.00
11.00
10.00
13.00
15.00
13.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.035
0.005
0.078
0.040
0.010
0.167
0.020
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
en 2
LB/HR
3182.54
10546.82
33350.04
27504.45
28731.60
58080.29
58080.29
60305.72
47906.77
28641.64
11150.43
NO
L8/1K
LB FUEL
1.01
1.74
1.74
2.53
1.50
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LP./HR LB/HR
0.98 0.98
7.30 7.30
79.81 79.81
40.32 40.32
45.23 45.23
86.48 86.48
86.48 86.48
230.67 230.67
129.12 129.12
51.47 53.47
10.79 10.79
NO NO
LB/IK EMISSION
HOURS LBS.
7.30 n.0015
H6.4R 0.0004
86. 46 0.0072
S3. 47 0.0053
10.79 0.0007
0.0151
0.0018
1-20
-------
DATE: 7/16/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEOYNE-CONTINENTAL
ENGINE DATA
CAL 10 NUMBER: 191 ENGINE TYPE AND MODEL: 0-200-A
RATED HORSEPOMER: 100.
714. HRS
FUEL H/C RATIO: 1.640
SERIAL NUMBER! 2045T9B
FINISH
FINISH
69.50
29.66
ENGINE TOTAL TIME:
FUEL: AV GAS 80/87
OPERATIONAL DATA «««»!
INLET AIR TEMPERATURE, DEGREES F: START 69.00
ATMOSPHERIC PRESSURE: START 29.86
INLE1 AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 30.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FlOU RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
T.OO
CAHB. TtST ENGINE MEASURED
HEATED MOOC RPM FUEL FLOW
LB/HR
IDLE-LOw I -0.0 5.60
IDLE/TAVI 2 -0.0 H. 10
RUN IIV 1 -0.0 15.00
RUN UP-LtAN 4 -0.0 15.00
RUN UP-RICH 5 -0.0 14.10
TAKE-I.'FF 6 -0.0 49.60
CLIMB 7 -0.0 49.60
DESCENT 8 -0.0 34.60
lit SCENT ON 8 -0.0 41.10
APPROACH 9 -0.0 21.10
1AX. 1
IFSr
MODE
1
2
\
tt
5
h
7
8
0
q
10
TKST
MODE
1
2
1
4
S
6
7
d
8
9
10
TEST
MODE
2
6
1
<*
in
TOTAL
101 AL
E XHAUST
r,»s
TEMP
DEGREES F
101.00
437.00
684.00
650.00
69%. 00
1076.00
1076.00
I054.00
1041.00
B?0.nO
4
-------
DATE: 7/16/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEDYNE-CONTINENTAL
ENGINE DATA
CAI 10 NUMBER: 192 ENGINE TYPE AND MODEL: 0-200-*
RATED HORSEPOWER: 100.
ENGINE TOTAL TIKE: 715. MRS
FUEL: AV GAS 80/87 FUEL N/C RATIO: 1.840
OPERATIONAL DATA »«»«««««««««««««««««««««««««
INLET AIR TENPERATUREi DECREES F: START 89.30 FINISH 89.00
ATMOSPHERIC PRESSURE: START 29.86 FINISH 29.66
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 50.00 PERCENT
SAMPLE LINE: TEMPERATURE, DECREES C: -0.00, FLOW RATE, LITERS/MIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER: 20*5790
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
L8/HR
IDLE-LOU 1 -0.0 3. CO
IDLE/TAXI 2 -0.0 6.40
RUN UP 3 -0.0 13.20
RUN UP-LEAN 4 -0.0 13.20
RUN UP-RICH 5 -0.0 13.20
TAKE-OFF 6 -0.0 48.60
CLIMB 7 -0.0 4B.60
DESCENT 8 -0.0 34.60
DESCENT ON 6 -0.0 41.10
APPROACH 9 -0.0 22.00
TAXI
TEST
MODE
1
2
3
4
5
6
7
8
0
q
10
TEST
MODE
I
2
3
4
5
6
7
8
9
9
in
TEST
MOIIE
2
6
7
9
10
TOTAL
TOTAL
FXHAUST
GAS
TEMP
DEGREES F
314.00
426.00
740.00
673.00
751.00
1188.00
1188.00
1143.00
1065.00
942.00
518. on
MASS EMI
C(J
LB/1K
LI FUF.L
663. 70
1019.54
774.41
817.20
632.18
1100.03
lino. 03
964.93
1309.98
1171.43
1114.50
TIME IN
"ODE
MIN.
12.00
0.10
5. JO
6.00
4.00
FOR CYCLE
FOR CYCL6/LB
10
EXHAUST
GAS
PRFSSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.oo
-0.00
MASS EMI
HC
LB/1K
L8 FUFL
71. 74
30.91
18.66
20.39
16.92
16.38
16. 31)
16.34
25.40
21.15
11.79
MEASURED
f'IF.L FLOW
LB/HR
6.40
48.60
48.60
22.00
5.60
FUEL
-0,
CO
(DRY)
PERCENT V
6.70
8.40
6.00
6.30
4.70
9.50
9.50
7.80
12.00
10.10
9.70
MASS EMI
NQ2
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
3.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
1.28
0.24
4.03
2.20
0.38
8. 112
,0
no
2
I DRY!
PERCENT V
a. oo
7.80
9.40
9.00
10.10
7.70
7.70
8.30
6.10
7.00
7.40
MASS EMI
C02
LB/IK
L9 FUEL
1620.37
1487.51
1906.27
1834.29
2134.53
1400.91
1400.91
1613.30
1046. 21
1275.64
1335.91
CO
LB/IK
Lfl FUFL
1019.54
1100.03
1100.03
1171.43
1114.50
5.60
THC
IOKV)
PPMV
9717.00
4447.00
2525.00
274*. 00
2196.00
2470.00
2470.00
2306.00
4063.00
3184.00
4831.00
MASS EMI
NO
LB/IK
LB FUEL
0.68
1.26
7.84
3.66
7.51
2.61
2.61
5.16
1.78
1.96
1.02
LTD CYCLE
CO
LB/IK
HOURS
6525.07
53461.47
53461.47
25771.38
6241.17
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
35.00 0.07255
72.00 0.07718
165.00 0.07200
162.00 0.07177
172.00 0.06884
543.00 0.08097
543.00 0.08097
406.00 0.07554
411.00 0.08659
236.00 0.08111
60.00 0.
NO
IORYI
PPMV
32.00
63.00
370.00
172.00
340.00
137.00
117.00
254.00
99.00
103.00
54.00
MASS EMI
NOX
LB/IK
LB FUEL
0.68
1.26
7.84
3.66
7.51
2.61
2.61
5. 16
1.78
1.96
1.02
EMISSIONS
cn
EMISSION
LBS.
1.305
0.267
4.437
2.577
0.418
9.005
1.107
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
2591.08
6525.07
10222.17
10787.04
8344.78
53461.47
53461.47
33386.44
53840.00
25771.38
6241.17
HC
LB/IK
LB FUEL
30.91
16.38
16.38
21.15
31.79
08172
NO
X
(ORY)
t>PMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
MC
LB/HR
715.22
197.84
246.38
269.18
223.30
796. 08
796.08
565.30
1044.04
465.30
178.02
HC
LB/IK
HOURS
197.84
796.08
796.08
465.30
178.02
ALDEHYDES
IORYI
30.00
17.00
-0.00
-0.00
-0.00
-0.00
9. GO
6.00
9.00
11.00
9.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.040
0.004
0.066
0.047
0.012
0.168
0.021
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
Lfl/HK
4861.11
9520.04
25162.73
24212.64
28175.82
68084. 13
68084.13
55820.25
43002.33
28064.lt)
7481.07
NO
LB/IK
LB FUEL
1.26
?.61
2.61
1.96
1.02
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
MASS EMI MASS EMI
NO NOX
L6/HR LB/HR
2.03 2.03
8.04 8.04
103.54 103.54
48.37 48.37
99.16 99.16
126.64 126.64
126.64 126.64
178.58 170.58
72.96 72.96
43.1 7 4}. 17
5.71 5.71
NO NO
LB/IK EMISSION
HOURS LBS.
8.04 C.0016
126.64 0.0006
126.64 0.0105
43.17 0.0043
5.71 0.0004
0.0175
0.0021
1-22
-------
DATE: 7/38/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: LYCOMING
ENGINE DATA
CAL ID NUMBER: 229
ENGINE TYPE AND NODELI D-120-A2B
RATED HORSEPOHERl ISO.
297. MRS
FUEL M/C RATIOI 1.8*0
SERIAL NUNBERl
ENGINE TOTAL TINEl
FUEL I AV GAS 80/8T
OPERtTIONtL nATA «»»«»
INLET AIR TEMPERATURE! DEGREES Fl START 84.50 FINISH 86.90
ATMOSPHERIC PRESSURE: START 30.12 FINISH 30.32
INLET AIR HUMIDITY. CRN H20/LB AIRI 0.01
RELATIVE HUMIDITY: 40.00 PERCENT
SAFPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOW RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: V
COMMENTS:
CARD. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLON
LB/HR
ll)Lt-LOU 1 -0.0 6.40
IOLE/IAXI 2 -0.0 8.10
RUN UP 3 -0.0 -0.00
rAKE-QFF 6 -0.0 70.30
CLIMB 7 -0.0 70.10
DESCENT 8 -0.0 34.20
DESCENT ON 8 -0.0 41.10
APPROACH 1 -0.0 14.30
IAII
icsv
MODE
1
2
3
6
7
n
H
1
10
TrsT
NUDE
,
2
3
6
7
A
8
;
4
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
673.00
706.00
198.00
1412.00
1412.00
1323.00
1233.00
1031.00
807.00
Hits EMI
CO
LB/1K
L8 FUEL
914.91
736.44
1106.62
1233. SI
1233.91
967.06
1359.22
1040.20
658. 85
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
39.93
20.19
21.90
30.39
30.35
19.96
36.93
20.32
17.77
MEASURED
FUEL FLOK
LB/HN
8.10
70.30
TO. 30
19.30
16.70
FUEL
-0
CO
(DRY)
PERCENT V
6.70
9.90
9.60
11.60
11.60
8.30
11.20
8.70
5.20
MASS EMI
N02
LB/U
LB FUEL
0.0
9.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LOS.
1.62
0.35
5.B3
1.93
1.12
10.855
0
CO
2
(DRY)
PERCENT V
9.40
10.00
7.60
6.90
6.90
8. 80
5.80
1.10
10.90
MASS EMI
C02
LB/1K
LB FUFL
1796.36
1961.20
1376.91
1192. 89
1192.89
1611.00
918.38
1484.10
2090.30
CO
LB/IK
LB FUEL
716.44
1211.91
1233.51
1040.20
658.85
16.70
THC
IORYI
PPMV
5100.00
2892.00
3296.00
4984.00
4984.00
2391.00
6199.00
2968.00
2449.00
MASS EMI
NO
LB/1K
LB FUEL
0.48
0.86
0.68
1.28
1.28
1.93
0.34
1.30
1.14
LTD CYCLE
CO
LB/1K
HOURS
5969.14
86715.71
86719.75
20079.84
11002.71
MEASURED CALCULATED
AIR FLOU F/A
LB/HR
78.00 0.07642
102.00 0.07429
-0.00 0.08137
734.00 0.08BS6
734.00 0.08896
499.00 0.08004
401.00 0.09196
220.00 0.07832
215.00 0.
NO
IDRY)
PPMV
24.00
42.00
36.00
73.00
73.00
101.00
20.00
66.00
95.00
MASS EMI
NO I
LB/1K
LB FUEL
0.48
0.86
0.60
.28
.28
.93
.34
.30
.14
EMISSIONS
CO
EMISSION
LBS.
1.19)
0.434
7.197
2.008
0.737
11.569
1.066
NO
2
IDRV)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
5215.39
5965.14
-0.00
86715.75
86715.79
37908.73
99863.74
20075.84
11002.71
HC
LB/1K
LB FUEL
20.39
30.35
30.39
20.12
17.77
07296
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EHI
HC
LB/HR
227.37
165.14
-0.00
2113.89
2113.89
625.44
1501.56
392.25
296.78
HC
LB/1K
HOURS
165. 14
2133.85
2133.85
392.29
296.78
ALDEHYDES
(DRYI
18.00
14.00
-0.00
-0.00
21.00
10.00
13.00
11.00
12.00
MASS EMI
N02
LB/HR
0.0
0.0
P.O
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.033
0.011
0.177
0.039
0.020
0.2BO
0.026
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
MASS EMI
CU2
LB/HR
11496. 43
15885.71
-o.oo
B1045.19
81045.19
63151.27
38567.58
28643.07
34907.41
NO
LB/IK
LB FUEL
0.86
I.2B
1.28
1.30
1.14
PABTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
IB/HR LB/HR
3.07 3.07
6.97 6.97
-0.00 -0.00
89.64 89.64
89.64 89.64
75.77 75.77
11.90 11.90
25.02 25.02
19.12 19.12
Nil NO
LB/IK EMISSION
HOURS LBS.
6.47 0.0014
84.64 0.0004
89.64 0.0074
25.02 0.0025
19.12 0.0013
0.0131
0.0012
1-23
-------
0«TE: 7/30/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER: LYCONING
ENGINE DATA
CAL ID NUMBER: 230 ENGINE TYPE AND MODEL: 0-120-428
RATED HORSEPOHER: no.
ENGINE TOTAL TINE: 257. MRS
FUEL: AV GAS BO/8T FUEL H/C RATIO: 1.840
OPERATIONAL DATA *««««.»..««»«...»««
INLET AIR TEMPERATURE, DEGREES F: START 84.50 FINISH 84.00
ATMOSPHERIC PRESSURE: START 30.32 FINISH 30.32
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 42.OC PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 9
COMMENTS:
SERIAL NUMBER: 2666* e
2853
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOU 1 -0.0 10.60
IDLE/TAXI 2 -0.0 8. 10
RUN UP 3 -0.0 30.90
TAKE-OFF 6 -0.0 61.30
CLIMB 7 -0.0 69.30
DESCENT e -0.0 40.10
DESCENT ON 8 -0.0 41.10
APPROACH 9 -0.0 21.10
TAXI
TFST
MODE
!
2
3
6
7
a
a
9
10
TEST
MODE
1
2
3
6
7
B
X
9
10
TES1
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
617.00
751.00
953.00
1412.00
1412.00
I36B.OO
1222.00
1054.00
705.00
MASS EMI
CO
LB/IK
LB FUEL
544.46
598.61
1140.03
1191.89
1 191.39
929.97
1355.33
1055.68
558.43
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRFSSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
HC
LB/1K
LB FUEL
28.52
19.10
23.66
80.14
80.14
16.69
37.82
22.53
19.05
MEASURED
FUEL FLOU
LB/HR
9. 10
69.30
69.30
21.10
5. 60
FUEL
-0.
CO
IDRYI
PERCENT V
4.20
4.70
10.60
11.60
11.60
7.80
12.90
8.90
4.30
MASS EMI
NC12
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
usto
LBS.
1.62
0.35
5.75
2.11
0.36
10.204
,0
CO
2
IORYI
PERCENT
11.00
10.90
7.80
6.70
6.70
a. 90
5.70
7.80
11.00
MASS EMI
CQ2
LB/IK
LB FUEL
2240.53
2191. 2B
1318.09
1081.66
1081.66
1667.26
940.95
1453.71
2244.56
CO
LB/IK
LB FUEL
59d,61
1191. 89
1191.89
1055.68
558.43
5:60
THC
IORYI
PPMV
V
3841.00
2619.00
3841.00
13619.00
13619.00
2444.00
6286.00
3317.00
2561.00
MASS EMI
NO
LB/IK
LB FUEL
0.72
1.19
0.76
0.71
0.71
2.04
0.38
1.27
1.22
LTO CYCLE
CO
LB/IK
HOURS
4843.75
82597.56
B2597.56
22274.91
3127.21
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
141.00 0.07113
106.00 0.07244
338.00 0.08717
676.00 0.09173
676.00 0.09173
476.00 0.07817
403.00 0.09016
238.00 0. C7899
73.00 0.
NO
IORYI
PPMV
34.00
57.00
43.00
42.00
42.00
104.00
22.00
65.00
57.00
MASS Ft!
NOX
LB/IK
LB FUEL
0.72
1.1?
0.76
0.71
0.71
2.04
0.38
1.27
1.22
EMISSIONS
CO
EMISSION
LBS.
C.970
0.413
6.856
2.221
0.210
10.675
1.046
NO
2
IDRY)
PPMV
-C.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-C.OO
MASS CMI
en
LB/HR
5771.32
4848.75
35227.02
82597.56
82597.56
37291.90
55703.92
22274.91
3127.21
HC
LB/IK
LB FUEL
19.10
do. 14
80.14
22.53
19.05
07100
NO
X
IDRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
302.28
154.74
731.07
5553.92
5553.92
669.22
1554.59
475.46
106.67
HC
L8/1K
HOURS
154.74
5553.92
5553.92
475.46
106.67
ALDEHYDES
IORYI
16.00
12.00
-0.00
34.00
34.00
10.00
6.00
8.00
10.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.031
0.028
0.461
0.04B
0.007
0.574
0.056
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/HR
23749.62
17668.36
4072B.91
74958.75
74958.75
66857.19
38673.11
30673.17
12569.55
NO
LB/IK
LB FUEL
1.19
0.71
0.71
i.2r
1.22
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS Ed MASS EMI
NO NOX
LB/HR LB/hR
7.67 7.67
9.66 9.66
25.47 23.47
49.12 49.12
49.12 49.12
81.67 81.67
15.60 15.60
26.72 26.72
6.81 6.81
NO NO
LB/1K EMISSION
HOURS LBS.
9.66 0.0019
49.1? 0.0002
49.12 0.0041
26.72 0.0027
6.81 0.0005
0.0094
0.0009
1-24
-------
DATE: 7/30/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER: LYCOHING
ENGINE DATA
CAL ID NUMBER: 231 ENGINE TYPE AND NOOELI O-SZO-AZB
RATED HORSEPOMER: HO.
ENGINE TOTAL TIME: lit. KRS
FUEL: AV GAS 80/87 FUEL H/C RATIOI 1.8*0
OPERAIIONAL DATA ««««««««««««««««««.«
INLET Aid TEMPERATURE, DEGREES F: START 85.50 FINISH 64.00
ATHDSPHtRIC PRESSURE! START 3C.32 FINISH 30.28
INLET AIR HUN 101IT. CRN M20/LB AIR: 0.01
RELATIVE HUMIDITY: 4i.oc PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 9
COMMENTS:
SERIAL NUMBER: 26664C
CARS. TEST ENGINE MEASURED
HEATER NODE RPH FUEL FLOM
LB/HR
IOLE-LOM 1 -0.0 5.60
IDLE/TAXI 2 -0.0 7.20
RUN UP 1 -0.0 30.90
TAKE-OFF 6 -0.0 69.30
CLIMB 7 -0.0 69.30
DESCENT 8 -O.n 41.10
DESCENT ON n -0.0 40.10
APPROACH 9 -0.0 19.30
TAXI 10 -0.0 B. 10
TEST EXHAUST EXHAUST CO CO THC
MODE GAS GAS IORYI 2 (DRY)
TEMP PRESSURF PERCENT V IORYI PPMV
1
2
3
6
7
n
e
9
10
TCST
MODE
1
2
1
6
1
H
n
9
10
fEsr
toot
2
b
7
9
10
TOTAL
TIITAL
DEGREES r
565.00
706.00
1076.00
1390.00
1390.00
1345.00
1211.00
1009.00
78S.OO
MASS EMI
CD
IB/ IK
LS FUEL
423.23
490.0)
1187.51
1215.85
1215.85
959.58
1354.48
1026.46
593.69
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FC1H CYCLt/LB
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
38.91
19.21
25.69
45.32
45.32
17.18
41.16
21.83
16.72
MEASURED
FUEL FLOW
LB/HR
7.20
69.30
69.30
19.30
8.10
FUFL
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
75.00 0.06745
91.00 0.06951
331.00 0.08243
724.00 0.09833
724.00 0.08833
481.00 0.07675
392.00 0.09092
221.00 0.07930
106.00 0.07152
NO NO NO
IORYI 2 X
PPMV IDRVI IORYI
PERCENT V
3.10
3.70
10.40
11.40
11.40
8.10
13.00
5.70
4.60
MASS CHI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LAS.
1 .44
0.15
5. J5
1.93
0.54
10.011
11.20
11.30
6.90
6.80
6.80
8.70
5.70
8.10
10.80
MASS EMI
C02
LB/1K
LB FUEL
2402.52
2351.57
1237.92
1139.52
1139.52
1619.40
931.13
1501.57
2190.08
CO
IB/IK
LB FUEL
490.05
1215.85
1215. B5
1026.46
594.69
4976.00
2532.00
3928.00
7420.00
7420.00
2532.00
6897.00
3230.00
2532.00
MASS EMI
NO
LB/1K
LB FUEL
0.83
1.24
0.96
0.51
0.51
1.71
. 0.34
1.36
1.12
LTD CYCLE
CO
LB/1K
HOURS
352H.38
R4258.44
B425B.44
19810.62
4808.85
37.00
57.00
51.00
29.00
29.00
88.00
20.00
70.00
53.00
MASS FHI
NOX
LB/1K
LB FUEL
0.83
1.24
0.96
0.51
0.51
1.71
0.34
1.36
1.12
EMISSIONS
CO
EMISSION
LBS.
C.706
0.471
6.993
1.981
0.322
10.424
1.041
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
237C.06
3528.38
36694.17
84256.44
84258.44
19438.70
54314.82
19810.62
4808.85
HC
LB/IK
LB FUEL
19.21
45.32
45.32
21.83
18.72
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
217.88
138.29
793.74
3140.93
3140.93
706.07
1650.36
421.24
151.60
HC
LB/IK
HOURS
138.29
3140.9}
3140.93
421.24
151.60
ALDEHYDES SMOKE
(DRY)
15.00
9.00
-0.00
21.00
21.00
6.00
-0.00
6.00
7.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.02B
0.016
0.261
0.042
0.010
0.356
0.036
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/HH
13454.10
16931.27
38251.71
78468.81
78968.81
66557.19
37418.64
2B9BO. 25
17739.67
NO
LB/IK
L6 FUEL
1.24
0.51
0.51
1.36
1.12
PARTICULATES
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
MASS FHI
NO
LB/HR
4.65
8.93
29.56
35.21
35.21
70.38
13.73
26.18
9.10
NO
LB/IK
HOURS
8.93
35.21
35.21
26.18
9.10
00
00
00
00
00
00
00
00
00
MASS EMI
NO I
LB/HR
4.65
6.93
29.56
35.21
35.21
70.38
13.73
26.18
9.10
NO
EMISSION
LBS.
o.ooie
0.0002
0.0029
0.0026
0.0006
0.0081
0.0008
1-25
-------
am: 8/17/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCONING
ENGINE DATA
CAL ID NUMBERI )84 ENGINE TYPE AND MODEL: 0-320-B3B
RATED HORSEPOWER: 160.
ENGINE IOr»L TINE: 563. MRS
FUEL: AV GAS 100/130 FUEL H/C RATIO! 1.840
OPERATIONAL DATA ««»«««»»««.
INLET AIR TEMPERATURE, DEGREES F: START 84.00 FINISH 77.00
ATMOSPHERIC PRESSURE: START 2<).eo FINISH 29.80
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.02
RELATIVE HUMIDITY: 78.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/NIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER! L-439VJ9
CARS. TEST ENGINE MEASURED
HEATER NODE RPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 IS. 20
IDLE/TAXI 2 -0.0 19. SO
RUN UP 3 -0.0 32.80
RUN UP-LEAN 4 -0.0 16.40
RUN UP-RICH 5 -0.0 30.50
TAKE-OFF 6 -0.0 50.40
CLIMB 7 -0.0 45.70
DESCENT 8 -0.0 42.20
DESCENT ON 8 -0.0 42.20
APPROACH 9 -0.0 36.30
TAXI
TEST
MODE
1
2
3
4
5
6
7
8
8
9
10
TFST
MODE
1
2
1
4
5
6
7
n
e
9
10
TEST
MODE
I
6
7
)
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
I Mi. 00
191.00
426.00
426.00
415.00
830.00
740.00
695.00
594.00
516.00
269.00
MASS EMI
CO
LB/1K
L9 FUEL
72B. 12
687.93
140.63
39.36
209.65
1161.35
882.12
B95.07
1265.66
1180.83
401. 39
TINE IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CVCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
HC
LB/1K
LB FUEL
102.24
44.59
16.38
7.24
36.36
28.06
24.38
24.30
33.08
33.36
58.70
MEASURED
FUEL FLOW
LB/HR
19.90
50.40
45.70
36.30
17.60
FUEL
-0.
CO
(DRY)
PERCENT V
1.70
1.70
0.50
0.10
0.60
7.60
6.20
6.20
8.90
6.50
0.90
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
o.o
0.0
FUFL
USED
L9S.
3.98
0.25
3.79
3.63
1.18
12.834
.0
CO
2
IDRYI
PERCENT V
2.60
3.10
6.20
5.00
5.00
5.30
7.70
7.50
4.90
4.30
3.40
MASS EMI
C02
LB/1K
LB FUEL
1749.71
1971.03
2895.78
3092.54
2745.08
1272.52
1721.34
1701.23
1094.87
12^7.38
2382.54
CO
LB/1K
LB FUEL
687.93
1161.35
882.12
1180.83
401.39
17.60
THC
(DRY)
PPMV
4168.00
1924.00
962.00
321.00
1817.00
3206.00
2992.00
2939.00
4061.00
3206.00
2298.00
MASS EMI
NO
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
C.O
0.0
0.0
0.0
0.0
LTD CYCLE
cu
LB/U
HOURS
13689.71
59532.20
40313.06
42864.07
7064.44
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
176.00 0.02233
247.00 0.02358
479.00 0.03164
246.00 0.02402
431.00 0.02706
541.00 0.06197
548. OC 0.06581
502.00 0.06492
432.00 0.06675
385.00 0.05234
233.00 0.
NO
(DRY)
PPNV
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
MASS EMI
NOI
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
EMISSIONS
CO
EMISSION
LBS.
2.738
0.293
3.346
4.2B6
0.473
11.136
0.868
NO
2
IDRVI
PPMV
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
CO
LB/MR
11067.43
13689.71
4875.05
645.58
6394.36
58532.20
40313.06
37771.74
53410.84
42864.07
7064.44
HC
LB/IK
LB FUEL
44.59
28.06
24.38
33.36
58.70
02136
NO
X
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
1554.07
887.35
537.19
118.69
1109.04
1414.13
1114.19
1025.46
1395.78
1210.84
1033.07
HC
LB/IK
HOURS
887.35
1414.13
1114.19
1210.84
1033.07
ALDEHYDES
IDRVI
5.00
4.00
-0.00
-0.00
-0.00
-0.00
6.00
8.00
10.00
6.00
4.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.177
0.007
0.092
0.121
0.069
0.467
0.036
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/HR
26595.58
39223.42
94981.56
50717.61
83724.88
64135.02
78665.25
71791.81
46203.38
44554.00
41932.66
NO
LB/U
LB FUEL
U.O
0.0
0.0
0.0
0.0
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO N0»
LB/HR LB/MR
0.0 0.0
0.0 0.0
C.O 0.0
0.0 0.0
0.0 0.0
0.0 0.0
0.0 0.0
0.0 0.0
0.0 0.0
0.0 0.0
C.O 0.0
NO NO
L"/|K EMISSION
HOURS LBS.
0.0 0.0
0.0 0.0
0.0 0.0
0.0 0.0
0.0 0.0
0.0
0.0
1-26
-------
DATE! 9/u/Ti
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIED! LYCONING
ENGINE DATA
CAl ID NUMBER! 315 ENGINE TYPE AND MODEL! O-320-B1S
RATED HORSEPOUERl 160.
ENGINE TOTAL TINEI 56). MRS
FUEL I 4V GAS 100/110 FUEL H/C RATIO! 1.840
OPERATIONAL DATA »«»««««««»»«««»
INLET AIR TEMPERATURE, DEGREES Fl START 76.SO FINISH 72.00
ATMOSPHERIC PRESSUREi START 29.10 FINISH 29.80
INLET AIR HUMIDITY, GRN H20/LB AIRl 0.02
RELATIVE HUMIDITY! 94.00 PERCENT
SANPLE LINE! TEMPERATURE, DEGREES Cl -a.00. FLOM RATE, LITERS/MINI T.OO
SAMPLE LINE TRANSPORT TINE, SECl 1.60
NUMBER OF TESTSl 11
COMNENTSl
SERIAL NUMBER! l-»l«l-l«A
CARD. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOM
LB/HR
IDLE-LOW 1 -0.0 16.40
IDLE/TAM 2 -0.0 19.90
RUN UP ! -0.0 12.80
DUN UP-LEAN 4 -0.0 IS. 20
RUN UP-RICH 5 -0.0 M.60
TAKE-OFF 6 -0.0 50.40
CLIMB T -0.0 45.70
DESCENT 8 -0.0 44.90
DESCENT ON 8 -0.0 4). 40
APPROACH 9 -0.0 36.30
TAXI 10 -0.0 10.80
TEST EXHAUST EXHAUST CO CO THC
MODE GAS GAS IORVI 2 (DRY)
TEMP PRESSURE PERCENT V (DRY) PPMV
1
2
3
4
5
6
7
8
9
9
10
TEST
MODE
8
9
10
TESI
MODE
2
6
7
9
10
TOTAL
TOTAL
DEGREES F
381.00
549.00
863.00
942.00
863.00
1177.00
1289.00
1300.00
1121.00
tag). ao
549.00
MASS ENI
CO
LB/1K
LB FUEL
523.34
549.77
1057.14
1047.22
1051.39
1170.22
1014. OB
880.90
1285.36
1032.3)
1045.90
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLF.
FOR CYCLE/LB
PSIt
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS ENI
HC
LB/IK
LB FUEL
119.52
32.52
23.58
23.13
26.16
23.31
21.27
21.88
26.30
20.04
65.98
MEASURED
FUEL FLOU
LB/HR
19.90
50.40
45.70
36.10
IB. 80
FUEL
MEASURED CALCULATED
AIR FLOW F/A
IB/HR
197.00 0.04672
261.00 0.05921
37(1.00 0.07611
172.00 0.07351
356.00 0.07325
544.00 0.08588
524.00 0.08286
535.00 0.0801B
444.00 0.09169
414.00 0.08238
250.00 0.02565
NO NO NO
IORYI 2 X
PPMV (ORYI IORYI
PERCENT V
2.60
3.50
8.60
3.20
8.20
10.70
9.00
7.60
12.50
9.10
2.80
MASS FNI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
IBS.
1.98
0.25
1.79
1.63
1.26
12.915
6.40
9.00
.50
.10
.20
.40
.60
.50
.70
8.40
2.10
MASS EMI
C02
LB/IK
LB FUEL
2024.07
2221.22
1448.54
1464.82
1450.51
1271.61
1522.54
1730.12
1082.50
1497.25
1349.89
ca
LB/IK
LB FUEL
549,77
1170.22
1014.08
1032.33
1045.90
10368.00
3615.00
1350.00
3190.00
1562.00
3722.00
3296.00
3296.00
4466.00
3084.00
3084.00
MASS EMI
NO
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
LTD CYCLE
CO
LB/U
HOURS
10940.34
58978.99
46343.61
37473.54
19662.95
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
MASS EMI
NOX
LO/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
EMISSIONS
CO
EMISSION
LBS.
2.188
0.295
3.841
3.747
1.317
11.194
0.882
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
8582.69
10940.34
14674.02
15917.69
11221.94
58978.99
46341.61
19200.18
55784.61
37471.54
19662.95
HC
LB/IK
LB FUEL
12.52
21.11
21.27
20.04
65.98
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
1960.16
647.17
771.56
154.65
826.56
1174.99
972.03
971.66
1141.48
727.35
1240.17
HC
LB/IK
HOUPS
647.17
1174.99
972.0]
727.35
1240.37
ALDEHYDES SMOKE
(DRY)
5.00
4.00
-0.00
-0.00
-0.00
-0.00
6.00
5.00
17.00
8.00
5.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.129
0.006
0.081
0.071
0.083
0.372
0.029
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS ENI
C02
LB/HR
11194.67
44202.19
47512.19
22265.24
45816.15
64089.00
69579.94
76990.31
46980.50
54)50.17
25377.96
NO
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
PARTICULATES
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
MASS EMI.
NO
LB/HR
C.O
0.0
0.0
0.0
0.0
C.O
0.0
0.0
0.0
0.0
0.0
NO
LB/IK
HOURS
0.0
0.0
0.0
0.0
0.0
00
00
00
00
00
00
00
00
00
oo
00
MASS EMI
NOX
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
NO
EMISSION
LBS.
0.0
0.0
0.0
0.0
0.0
0.0
0.0
1-27
-------
0*TEl 8/1T/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: LTCOMING
ENGINE DATA
CAL 10 NUMBER! 386 ENGINE TYPE AND NODELl 0-320-B3B
RATED HORSEPOUERl 160.
ENGINE TOTAL TINEI 563. MRS
FUEL: AV GAS 100/130 FUEL H/C RATIO: 1.840
OPERATIONAL DATA »«»»»»««»««««
INLET AIR TEMPERATURE, DEGREES Fl START 66.00 FINISH 68.00
ATKOSPHERIC PRESSURE: START 29.97 FINISH 29.97
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY! 51.00 PERCENT
SAMPLE LINEl TEMPERATURE, CEGREES C: '0.00, FLOH RATE, LITERS/MIX:
SAMPLE LINE TRANSPORT TINE. SECi 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER! L-4393-39B
9893
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOH
LB/HR
IDLE-LOW 1 -0.0 14.10
IOLE/TAX! 2 -0.0 19.90
RUN UP 3 -0.0 38.70
RUN UP-LEAN 4 -0.0 21.10
RUN UP-RICH 5 -0.0 38.70
TAKE-OFF 6 -0.0 73.80
CLIMB 7 -0.0 S9.80
DESCENT 8 -0.0 55.10
DESCENT ON 8 -0.0 56.30
APPROACH 9 -0.0 43.40
TAXI
TEST
MODE
[
2
3
4
5
6
7
8
8
9
10
TEST
MODE
1
2
3
4
5
6
7
a
8
q
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
3J6.00
527.00
807.00
852.00
807.00
1278.00
1 300.00
1278.00
1076.00
1076.00
482.00
MASS EMI
CO
Ufl/lK
LB FUEL
969. 75
1074.22
986.44
961.83
961.54
815.59
654.21
716.08
1265.48
1012.24
776.83
T I ME IN
MUDF
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
FXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
90.67
34.40
19.97
19.07
18.93
21.61
18.58
18.60
24.20
17.33
25.92
MEASURED
FUEL FLOH
LB/HR
19.90
73.80
59.80
43.40
19.90
FUEL
-0,
CO
IDRY)
PERCENT V
7.50
9.70
7.90
7.60
7.50
6.50
5.20
5.80
11.90
8.80
5.90
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
3.98
0.37
4.96
4.34
1.33
14.986
.0
CO
2
IORYI
PERCENT
6.90
B. 00
a. oo
8.10
8.00
9.30
10.60
10.30
6.70
a. 50
9.10
HASS EMI
C02
LB/IK
LI) FUEL
1401.80
1392.03
1569.54
1610.67
1611.52
1833.49
2095.37
1998.08
1119.49
1536.24
1882.57
CO
LB/IK
LB FUEL
1074.22
815.59
654.21
1012.24
776.83
19.90
THC
(ORYI
PPMV
V
12244.00
5424.00
2792.00
2631.00
2578.00
3007.00
2578.00
2631.00
3974.00
2631.00
3437.00
MASS EMI
NO
LB/IK
LB FUEL
0.38
0.87
2.81
2.10
2.23
8.47
19.51
14.95
3.06
5.59
2.16
LIO CYCLE
CO
LB/U
HOURS
21376.88
60190.32
39121.91
43931.20
15458.83
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
149.00 0.07271
222.00 0.08455
449.00 0.07494
247.00 0.07390
453.00 0.07297
905.00 0.07411
770.00 0.07345
697.00 0.07496
580.00 0.08864
500.00 0.08120
246.00 0.
NO
IDRY)
PPMV
18.00
48.00
137.00
101.00
106.00
411.00
944.00
737.00
175.00
296.00
100.00
MASS EMI
NOX
LB/IK
LR FUEL
0.38
0.87
2.B1
2.10
2.23
8.47
19.51
14.95
3.06
5.59
2.16
EMISSIONS
CO
EMISSION
LBS.
4.275
0.301
3.247
4.393
1.036
11.252
0.884
NO
2
IDRV)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
MASS EMI
CO
LB/HR
13673.47
21376.88
38175.32
20294.60
37211.61
60190.32
39121.91
39456.23
71246.38
43931.20
15458.83
HC
L8/1K
LB FUEL
34.40
21.61
18.58
17.33
25.92
07067
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
1278.46
684.60
772.71
402.38
732.56
1594.75
1110.82
1025.07
1362.67
752.24
515.76
HC
LB/IK
HOURS
684.60
1594.75
1110.82
752.24
515.76
ALDEHYDES SMOKE
(ORYI
7.00
3.00
-0.00
-0.00
-0.00
-0.00
-0.00
3.00
3.00
2.00
3.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.137
0.008
0.092
0.075
0.035
0.347
0.023
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
19765.35
27701.35
60741.27
33985.21
62365.63
135311.44
125302.81
110093. BB
63027.39
66672.56
37463.13
NO
LB/IK
Lfl FUFL
0.87
8.47
19.51
5.59
2.16
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
5.39 5.39
17.38 17.38
108.74 108.74
44.30 44.30
86.19 86.39
625.14 625.14
1166.57 1166.57
823.52 823.52
172.10 172.10
242.72 242.72
43.04 43.04
NO NO
LB/IK EMISSION
HOURS LBS.
17.38 0.0035
625.14 0.0031
1166.57 0.0968
242.72 0.0243
43.04 0.0029
0. 1306
O.OOB7
1-28
-------
DATE! 8/1T/T1
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LTCQMING
ENGINE DAT!
»»*
C»L ID NUMBER! 387 ENGINE TYPE AND MODEL I 0-3JO-83B
R»TED KORSEPOHERI 160.
ENGINE TOTAL TINEl 435. MRS
FUEL! »V GAS 100/130 FUEL H/C RATIOI 1.840
OPERATIONAL DATA »«»«««»««<
INLET AIR TENPERATUREi DEGREES Fl START 70.00 FINISH
ATMOSPHERIC PRESSUREl START 29.97 FINISH
INLET AIR HUMIDITY. CRN H20/LS AIR! 0.01
RELATIVE HUMIDITY! 44.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES Cl -0.00. FLOH RATE. LITERS/MINI
SAMPLE LINE TRANSPORT TINE. SEC! 1.60
NUMBER OF TESTS: 11
COMMENTS!
SERIAL NUMBER! L-4J3&-39
72.00
21.97
7.00
:J895
CARB. TtSI ENGINE MEASURED
HEATER MODE RPN FUEL FLOW
LB/HR
IDLE-LOU 1 -0.0 10.30
IDLE/TAXI 2 -0.0 15.20
RUN UP 3 -0.0 21.10
RUN UP-LEAN 4 -0.0 U.BO
RUN UP-RICH 5 -0.0 19.90
TAKE-OFF 6 -0.0 79.70
CLIMB T -0.0 6B.OO
DESCENT a -0.0 31.60
DESCENT ON B -0.0 33.90
APPROACH 9 -0.0 33.20
TAXI
TEST
NODE
,
2
3
4
5
6
7
8
a
9
10
TEST
MODE
1
2
3
4
3
6
T
a
a
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
404.00
493.00
863.00
908.00
886.00
1267.00
1379.00
1267.00
im.oo
1087.00
482.00
MISS EMI
CO
LB/IK
LR FUEL
1131.36
1134.42
1093.76
1077.36
1074.59
839.55
227.96
695.13
1230.92
993.51
1086.97
TIMF IN
MOOF
NIN.
12.00
0.30
5.00
6.00
4.00
FOD CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSU
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
108.59
36.21
19.94
18.96
21. aa
45.93
20.41
18.56
' 22.93
19.02
13.77
MEASURED
FUEL FLOW
LB/HR
13.20
79.70
68.00
35.20
16.40
FUEL
-0.
CO
(DRVI
PERCENT V
10.00
10.50
9.20
9.00
9.00
7.40
1.70
5.70
11.50
3.60
9.20
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
3.04
0.40
5.64
3.52
1.10
13.701
.0
CO
2
IORYI
PERCENT V
S.90
7.30
7.50
7.60
7.60
9.70
13.10
10.60
7.00
6.60
7.40
MASS EMI
C02
LB/IK
LB FUEL
1067.52
1261.06
1400.99
1429.45
1425.78
1729.12
2760.06
2031.11
1177.23
1561.03
1373.73
CO
LB/U
LB FUEL
1134.42
839.55
227.96
993.51
1086.97
16.40
THC
(DRY)
PPMV
16435.00
5750.00
2929.00
2766.00
3200.00
7068.00
2658.00
2658.00
3743.00
2875.00
4990.00
MASS EMI
NO
LB/IK
LB FUEL
1.49
0.52
. 1.74
1.38
1.35
9.86
62.69
14.50
2.48
3.95
1.03
LTD CYCLE
CO
LB/IK
HOURS
17547.18
66912.25
15501.26
34971.57
17826.35
MEASURED CALCULATED
AIR FLOK F/A
LB/HR
101.00 0.08209
164.00 0.08546
23.50 0.07892
210.00 0.07834
223.00 0.07834
958.00 0.08184
974.00 0.06107
658.00 0.07579
566.00 0.08793
408.00 0.08080
182.00 0.
NO
IDRVI
PPMV
74.00
29.00
89.00
70.00
69.00
529.00
2846.00
724.00
141.00
208.00
53.00
MASS EMI
NOX
LB/IK
LB FUEL
1.49
0.52
1.74
1.38
1.35
4.86
62.69
14.50
2.48
3.95
1.03
EMISSIONS
CO
EMISSION
LBS.
3.309
0.335
1.287
3.497
1.194
9.822
0.717
NO
2
IORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CD
LB/HR
12091.35
17347.18
23078.32
20254.29
21384.38
66912.25
15501.26
35868.54
66346.38
34971.57
17826.35
HC
LB/IK
LB FUEL
36.21
45.93
20.41
19.02
33.77
07943
NO
X
IDRVI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
IB/MR
1138.12
550.34
420.81
356.51
435.46
3660.29
1388.09
457.94
1236.76
669.58
553.76
HC
LR/1K
HOURS
350.34
3660.29
1388.09
669.58
553.76
ALDEHYDES SMOKE
IORYI
10.00
7.00
-0.00
-0.00
-0.00
-0.00
11.00
7.00
4.00
4.00
2.00
MASS EMI
N02
L8/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.110
0.018
0.115
0.067
0.037
0.348
0.025
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/HR
11208.96
19168.09
29560.77
26873.63
28373.06
137811.13
187684.23
104805.25
63453.54
34948.18
22529.13
NO
LB/IK
LB FUEL
0.52
9.86
62.69
3.95
1.03
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI. MASS EMI
NO NOI
LB/HR LB/HR
15.69 15.69
7.96 7.96
36.67 36.67
25.88 25.88
26.93 26.93
785.69 785.69
4262.59 4262.59
748.34 748.34
133.62 133.62
138.93 138.93
16.87 16.87
NO NO
L8/IK EMISSION
HOURS L6S.
7.96 0.0016
785.69 0.0039
4262.59 0.3538
138.93 0.0139
16.87 0.0011
0.3743
0.0273
1-29
-------
DATE: 8/17/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCONING
ENGINE DATA ***********
C»L ID NUHBERl )8B ENGINE TYPE AND NODELt 0-320-B3B SERIAL NUMBER! L-4336-39A
RATED HORSEPONER: 160.
ENGINE TOTAL TINEI 413. MRS
FUEL! AV GAS 100/130 FUEL H/C RATIOI 1.840
OPERATIONAL DATA «»»*»*««»»««»««»»»«»»««»»*«*»»
INLET AIR TEMPERATURE. DECREES Fl START 75.00 FINISH 77.50
ATMOSPHERIC PRESSURE: START 21.70 FINISH 29.70
INLET AIR HUMIDITY, CRN H20/L8 AIRt 0.01
RELATIVE HUMIDITY! 3d.00 PERCENT
SAMPLE LINE: TEMPERATUREi CEGREES C: -O.OOi FLOW RATEi LITERS/BIN! 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
9897
CARB. TEST FNGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 12.90
10LE/TAXI 2 -0.0 18.80
RUN UP 3 -0.0 24.60
RUN UP-LEAN 4 -0.0 21.10
RUN UP-RICH 5 -0.0 21.10
TAKE-OFF 6 -0.0 68.00
CLIMB 7 -0.0 56.30
DESCENT 8 -0.0 50.40
DESCENT ON 3 -0.0 51.60
APPROACH 9 -0.0 34.00
TAXI
TEST
MODE
1
2
3
4
5
&
7
a
8
9
10
TEST
MODE
I
?
3
4
5
6
7
8
fl
9
10
TEST
XODE
2
6
;
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
426.00
304.00
a 74. 00
919.00
874.00
1345.00
1356.00
1323.00
1155.00
1121.00
5.18
MASS EMI
CO
LB/1K
LB FUEL
1141.35
1079.38
1077.92
1090.53
1054.66
835.45
525.21
703.54
1260.02
1025.45
1053.03
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
115.24
32.46
20.55
20. la
20.05
24.85
18.26
17.71
23.03
21.59
31.26
MEASURED
FUEL FLOU
LB/HR
18.80
68.00
56.30
34.00
17.60
FUEL
-0.
CO
(DRY)
PERCENT V
9.60
9.40
B. 80
a. 90
a. 50
7.10
4.20
5.80
11.90
9.00
9.00
MASS EMI
NO 2
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
n.o
0.0
n.o
n.o
0.0
0.0
0.0
FUEL
USED
L1S.
3.76
0.34
4.67
3.40
1.18
13.352
.0
CO
2
(DRY)
PERCENT
5.70
7.70
7.40
7.30
7.50
9.70
11.70
10.60
6.80
8.40
7.80
MASS EMI
C02
LB/IK
LB FUEL
1064.78
1389.24
1424.21
1405.43
1462.15
1793.38
2298.91
2020.24
1111.30
1503.79
1433.94
CO
LB/IK
LB FUEL
1079.38
835.45
525.23
1025.45
1053.03
17.60
TMC
(DRY!
PPMV
V
16924.00
4936.00
2929.00
2875.00
2821.00
3688.00
2549.00
2549.00
3797.00
3309.00
4665.00
MASS EMI
NO
LB/IK
LB FUEL
0.14
0.79
1.93
1.45
1.49
9.84
22.90
13.03
1.90
3.82
1.19
LTD CYCLE
CD
LB/IK
HOURS
20292.36
56810.52
29570.25
34865.23
18533.28
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
123.00 0.07957
209.00 0.08165
276.00 0.07662
235.00 0.07663
238.00 0.07560
828.00 0.07890
752.00 0.07351
641.00 0.07620
535.00 0.08698
3BB.OO 0.08201
198.00 0.
NO
(DRY)
PPMV
7.00
42.00
96.00
72.00
73.00
509.00
1115.00
6S4.00
109.00
204.00
62.00
MASS EMI
NOX
LB/IK
LB FUEL
0.14
0.79
1.93
1.45
1.49
9.84
22.90
13.03
1.90
3.82
1.19
EMISSIONS
CO
EMISSION
L8S.
4.058
0.284
2.454
3.487
1.242
11.525
0.863
NO
2
(DRV)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI
CO
IB/MR
14723.39
20292.36
26516. 88
23010.13
22253.20
56810.52
2957C.25
35456.31
65017.04
34865.23
18533.28
HC
LB/IK
IB FUEL
32.46
24.85
18.26
21.59
31.26
08008
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.ob
-0.00
MASS EMI
HC
LB/HR
1486.57
610.27
505.48
425.71
422.98
1690.08
1027.83
892.49
1188.14
734.16
550.18
HC
LB/IK
HOURS
610.27
1690.08
1027.83
734.16
550.18
ALDEHYDES SMOKE
IDRY1
13.00
9.00
-0.00
-0.00
-0.00
-0.00
8.00
8.00
6.00
5.00
6.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.122
o.ooa
0.085
0.073
0.037
0.326
0.024
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
13735.08
26117.63
35035.58
29654.48
30851.27
121949.63
129428.50
101820.25
58375.07
51129.01
25237.27
NCI
LB/IK
LB FUEL
0.79
9.84
22.90
3.82
1.19
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
1.76 1.76
14.89 14.89
47.52 47.52
30.58 30.58
31.39 31.39
668.97 668.97
1289.44 1289.44
656.73 656.73
97.82 97.82
129.81 129.81
20.97 20.97
NO NO
LB/IK EMISSION
HOURS LBS.
14.89 0.0030
668.97 0.0033
1289.44 0.1070
129.81 0.0130
20.97 0.0014
0.1277
0.0096
1-30
-------
OATEI a/ir/Ti
TEST ORGAN 11AT ION I SCOTT/SEN AVIATION
ENGINE SUPPLIER! LYCQNING
ENGINE DATA »»»*»«««»««»»
CAL 10 NUNBERl 1*9 ENGINE TYPE AND NOOELl 0-320-638
RATED HORSEPOMERI 140.
ENGINE TOTAL TINEl 433. MRS
FUEL! AV CAS 100/130 FUEL M/C RATIOl 1.640
OPERATIONAL DATA »*««*«*«««»««
INLET AIR TEMPERATURE. DECREES Fl START 77.50 FINISH
ATNOSPHERIC PRESSUREl START 29.70 FINISH
INLET AIR HUNIOITY, GRN H20/LB AIRl 0.01
RELATIVE HUNIOITVl 54.OC PERCENT
SAMPLE LINEl TENPERATURE. DEGREES Ct -0.00, FLOH RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TINE. SECI 1.60
NUMBER OF TESTS I 11
COMMENTSl
SERIAL NUMBERS L-4JJ4-30
79.00
2*. TO
CARS. TEST ENGINE MEASURED
HEATER MODE PPM FUEL FLOW
LB/HR
IOLE-LOH 1 -0.0 15.20
IDLE/TAXI 2 -0.0 14. »0
RUN UP -0.0 24. «0
RUN UP-LEAN -0.0 21.10
RUN UP-RICH -0.0 22. JO
TAKE-OFF -0.0 72.70
CLIMB -0.0 35.10
DESCENT -0.0 49.20
DESCENT -0.0 92.70
APPROACH -0.0 38.70
TAXI
TEST
NODE
10
TEST
MODE
1
2
3
4
5
6
7
8
9
9
10
7EST
MODE
2
6
7
«
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
471.00
983.00
942.00
979.00
964.00
1199.00
1211.00
1222.00
1143.00
1099.00
605.00
NASS ENI
CO
LB/IK
LB FUEL
869.39
644. 19
1137.06
1133.68
1074.08
1198. tl
1271.97
1205.89
1419.79
1231.39
994.60
TIME IN
MODE
NIN.
12.00
0.30
9.00
6.00
4.00
FOR CYCLE
FOR CVCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
106.60
28.90
24.16
22.90
23.50
39.34
31.19
28.62
16.82
22,91
38.62
MEASURED
FUEL FLOW
LB/HR
16.40
72.70
99.10
38.70
17.60
FUEL
-0
CO
10k VI
PERCENT V
6. TO
5.10
9.60
9.90
8.90
11.30
12.10
11.20
14.30
11.50
B.20
NASS EMI
H02
LB/IK
LB FUEL
n.o
n.o
0.0
0.0
0.0
0.0
0.0
0.0
n.o
0.0
n.o
FUEL
USED
IBS.
1.28
0.36
4.57
3.87
1.18
13.266
0
CO
2
(ORYI
PERCENT V
7.50
10.50
.10
.10
.50
.10
.60
7.10
5.40
7.00
7.90
MASS EMI
C02
LB/U
Lfl FUEL
1522.08
2083.88
1121.34
1331.26
1422.15
1183.20
1090.12
1201.08
842.41
1177.70
liOS.56
CO
LB/U
LB FUEL
644.19
1198.51
1271.97
1231.39
994.60
17.60
THC
IORV)
PPNV
14410.00
3940.00
3362.00
3292.00
3400.00
6476.00
9181.00
4641.00
6476.00
3670.00
5559.00
NASS ENI
NO
LB/IK
LB FUEL
0.81
.34
.96
.43
.70
.93
.31
.95
.73
.51
.14
LTO CYCLE
CO
LB/IK
HOURS
10964.73
87131.29
70085.50
47654.91
17504.91
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
165.00 0.07257
211.00 0.07319
249.00 0.07937
230.00 0.07878
250.00 0.07774
767.00 0.08870
566.00 0.08972
522.00 0.08737
500.00 0.09539
406.00 0.08790
201.00 0.
NO
IDRVI
PPMV
38.00
113.00
101.00
73.00
86.00
112.00
76.00
110.00
45.00
86.00
57.00
NASS ENI
NOX
LB/IK
LB FUEL
0.81
2.34
.96
.43
.70
.93
.31
.95
.73
.51
.14
EMISSIONS
CO
EMISSION
LBS.
2.113
0.436
5.817
4.765
1.173
14.304
1.078
NO
2
IDRVI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS ENI
CO
LB/HR
13153.93
10564.73
27972.14
23920.55
23951.95
87131.25
70083.50
59327.66
74821.00
47634.91
17904.91
HC
LB/IK
LB FUEL
26.50
39.34
31.19
22.51
36.62
07719
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS ENI
HC
LB/HR
1620.28
467.44
594.42
474.74
524.05
2659.88
1718.71
1407.98
1940.67
671.01
679.69
HC
LB/IK
HOURS
467.44
2899.88
1718.71
871.01
679.69
ALDEHYDES
IDRVI
9.00
6.00
-0.00
-0.00
-0.00
-0.00
7.00
6.00
6.00
5.00
6.00
NASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.093
0.014
0.143
0.087
0.046
0.363
O.C29
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS EMI
C02
LB/HR
23139.57
34173.57
32305.06
28089.49
31713.94
66016.56
60065.95
59093.00
44394.73
49977.04
26497. 89
NO
LB/IK
LB FUEL
2.34
1.95
1.31
1.91
1.14
PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
NASS EMI MASS ENI
NO NOX
LB/NR LB/HR
12.25 12.25
38.43 36.43
48.34 48.34
30.19 30.19
38.02 36.02
141.85 141.85
72.31 72.31
93.71 93.71
38.68 38.68
36.94 56.34
19.99 19.99
NO NO
LB/IK EMISSION
HOURS LBS.
38.49 0.0077
141.89 0.0007
72.31 0.0060
58.54 0.0059
19.99 0.0013
0.0216
0.0016
1-31
-------
DATE: 7/28/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOM1NG
ENGINE DATA
CAL ID NUMBER! 232 ENGINE TYPE AND MODEL: O-320-E2A
RATED HURSEPOKER: no.
ENGINE TOTAL TIMEl 139*. MRS
FUEL: AV GAS 80/87 FUEL H/C RATIO: 1.840
OPERATIONAL DATA »««»»
INLET AIR TEMPERATURE, DEGREES F: START 81.00 FINISH 81.00
ATMOSPHERIC PRESSURE: START 30.05 FINISH 30.05
INLET AIR HUMIDITY. CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 48.00 PERCENT
SAMPLE LINE: TEMPERATURE. CEGREES C: -0.00, FLOM RATE. LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: II
COMMENTS:
SERIAL NUMBER: L-26201-2TAA
3883
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLON
LB/HR
IDLE-LOW 1 -0.0 5.90
IDLE/TAXI 2 -0.0 5.10
RUN UP 3 -0.0 25.80
RUN UP-LEAN 4 -0.0 23.40
RUN UP-RICH 5 -0.0 25.80
TAKE-OFF 6 -0.0 64.50
CLIMB 7 -0.0 66.80
DESCENT 8 -0.0 29.30
DESCENT ON 8 -0.0 41.00
APPROACH 9 -0.0 11.70
TAXI
TEST
HODF
1
2
3
4
5
6
r
8
e
9
10
TEST
HOOF
1
2
3
4
5
6
7
8
8
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
303.00
426.00
874.00
785.00
942.00
1211.00
121 1.00
1143.00
1043.00
852.00
415.00
MASS EMI
CO
LB/IK
LB FUEL
771.15
1101.40
1002.38
959.36
986.27
1042.01
1042.01
840.50
1312.42
399.44
613.40
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUFL
28.36
29.87
15.62
15. «a
13.54
15.37
15.37
12.90
29.55
13.87
12.04
MEASURED
FUEL FLOK
LB/HR
5.90
64.50
66.80
11.70
34.00
FUEL
-0.0
CO
(DRY)
PERCENT V
2.70
6.10
8.50
7.80
8.20
9.20
9.20
6.90
12.20
7.30
2.70
MASS EMI
Nfl2
LB/IK
LB FUF.L
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
1.18
0.32
5.54
1.17
2.28
10.495
CO
2
(DRY)
PERCENT V
4.20
4.80
B.40
8.40
8.40
8.40
8.40
9.50
6.10
8.90
6.10
MASS EMI
C02
LB/IK
LB FUEL
1834.78
1361.74
1556.44
1623.32
1587.45
1494.86
1494.86
1818.24
1031.05
1722.97
2177.44
CO
LB/IK
LB FUEL
1101.40
IC42.01
1042.01
899.44
611.40
34.00
THC
IORYI
PPMV
1734.00
2889.00
2312.00
2254.00
1965.00
2369.00
2369.00
1849.00
4797.00
1965.00
925.00
MASS EMI
NO
LB/IK
LB FUEL
1.17
0.80
. 2.19
1.94
1.74
4.60
4.60
7.68
2.33
3.78
3.47
LTD CYCLE
CO
LB/IK
HOURS
6498.25
67209.38
69605.94
10523.48
20855.48
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
72.00 0.03326
64.00 0.05254
298.00 0.07922
275.00 0.07594
300.00 0.07767
734.00 0.08251
761.00 0.08251
358.00 0.07628
413.00 0.08787
141.00 0.07562
443.00 0.
NO
IHRYI
PPMV
25.00
27.00
113.00
96.00
88.00
247.00
247.00
384.00
132.00
187.00
93.00
MASS EMI
NOX
LB/IK
LB FUEL
1.17
0.80
2.19
1.94
1.74
4.60
4.60
7.68
2.33
3.78
3.47
EMISSIONS
CO
EMISSION
LBS.
1.300
0.336
5.777
1.052
1.397
9.863
0.940
NO
2
IORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
4549.77
6498.25
25861.43
22448.94
25445.80
67209.38
69605.94
24626.66
53809.28
10523.48
20855.48
HC
L8/1K
LB FUEL
29.87
15.37
15.37
13.87
12.04
04145
NO
X
(DRY)
PPNV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
167.35
176.26
402.87
371.54
349.23
991.18
1026.52
377.95
1211.75
162.23
409.21
HC
LB/IK
HOURS
176.26
991.18
1026.52
162.23
409.21
ALDEHYDES
IORYI
11.00
15.00
-0.00
-0.00
-0.00
-0.00
7.00
4.00
-0.00
10.00
10.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.035
0.005
0.085
O.C16
0.027
0.169
0.016
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CD?
LB/HR
11120.22
8034.26
40156.05
37985.63
40956.25
96418.25
99856.38
53274.17
42273.24
20158.80
74032.94
NO
LB/IK
LB FUEL
C.10
4.60
4.60
3.78
3.47
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
6.92 6.92
4.72 4.72
56.47 56.47
45.38 45.38
44.85 44.85
296.39 296.39
306.96 306.96
225.12 225.12
95.63 95.63
44.28 44.28
117.99 117.99
NO NO
LB/IK EMISSION
HOURS LBS.
4.72 0.0009
296.39 0.0015
3C6.96 0.0255
44.28 0.0044
117.99 0.0079
0.0402
0.0038
1-32
-------
DATE! 7/28/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPIIERI LrCONING
ENGINE OAT*
SERIAL NUMBER I 1-26201-2IAB
CAL ID NUMBER! 213 ENGINE TYPE AND NOOELI 0-120-E2A
RATED HORSEPOUERI HO.
ENGINE TOTAL TINEI U»4. MRS
fUELI AV GAS 60/8T FUEL H/C BATIOI 1.8*0
OPERATIONAL DATA «»*»««»»*«»»«**««
INLET AIR TEMPERATURE. DEGREES Fl START 81.00 FINISH 81.00
ATMOSPHERIC PRESSURE! START JO.05 FINISH 30.01
INLET AIR HUMIDITY, CRN M20/LB AIRI 0.01
RELATIVE HUMIOITYl 46.00 PERCENT
SAMPLE LINEl TEMPERAIURE. DEGREES Cl -0.00. FLOM RATE. LITERS/NINI T.OO
SAMPLE LINE TRANSPORT TIME. SECl 1.60
NUMBER OF TESTSl 11
COMMENTS:
JG55
CARS. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOH
LB/HR
IDLE-LOU I -0.0 4.40
IDLE/TAXI 2 -0.0 11.70
RUN UP 3 -0.0 29.30
RUN UP-LEAN 4 -0.0 29.30
RUN UP-RICH -0.0 29.30
TAKE-OFF -0.0 44.50
CLIMB -0.0 64. JO
DESCENT -0.0 41.00
DESCENT ON -0.0 56.30
APPROACH -0.0 IT. 60
TAXI
TEST
MODE
10
TFST
MODE
1
2
1
4
5
10
TEST
NODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
291.00
446.00
697.00
841.00
919.00
121}. 00
12)1.00
1141.00
1054.00
874.00
448.00
MASS EMI
CO
IB/ IK
18 FUEL
487.81
833.26
1012.01
1059.97
1032. 18
1078.22
1078.22
877.00
1166.18
910.71
614.81
TIME IN
MODE
MIN.
12.00
0.10
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
MC
L8/1K
LB FUEL
26.22
18.19
15.69
17.09
14.59
14.95
14.95
12.96
11.52
14.81
12.67
MEASURED
FUEL FLOW
LB/HR
11.70
64.50
64.50
17.60
11.70
FUEL
-0
CO
(DRY)
PERCENT V
2.10
5.70
a. 70
9.00
8.90
9.10
9.30
7.20
11.00
7.70
1.60
MASS EMI
N02
LB/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
2.14
0.32
5.35
1.76
0.78
10.560
0
CO
2
IDRV)
PERCENT V
6.40
7.90
8.10
7.90
8.30
7.90
7.90
9.20
5.70
8.80
8.10
MASS EMI
C02
LB/1K
LB FUEL
2135.85
1814.56
1509.69
1461.90
1512.45
1434.09
1439.09
1760.72
941.19
1671.25
2173.50
CU
LB/IK
LB FUEL
833.26
lore. 22
1078.22
910.71
614.81
11.70
THC
IORY)
PPMV
1971.00
2196.00
2309.00
2534.00
2196.00
2252.00
2252.00
1858.00
5217.00
2140.00
1295.00
MASS EMI
NO
LB/U
LB FUEL
2.14
2.23
1.15
1.95
2.19
7.90
7.90
13.18
1.42
6.04
3.51
LTD CYCLE
CO
LB/IK
HOURS
9749.15
69545.06
69545.06
16180.40
7191.22
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
125.00 0.04048
143.00 0.06348
335.00 0.07887
331.00 0.07452
336.00 0.08061
725.00 0.08079
725.00 0.08079
495.00 0.07634
550.00 0.09014
208.00 0.07713
151.00 0.
NO
(DRY)
PPHV
56.00
91.00
172.00
101.00
115.00
415.00
415.00
659.00
111.00
304.00
126.00
MASS EMI
NOX
LB/IK
LB FUEL
2.14
2.21
1.15
1.95
2.19
7.90
7.90
13.18
1.92
6.04
3.53
EMISSIONS
CO
EMISSION
LBS.
1.950
0.348
5.772
1.638
0.482
10.190
0.965
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
4585.37
9749.15
30217.85
31057.14
10242.71
64545.06
64545.06
15956.86
76916.00
16180.40
7191.22
HC
LB/IK
LB FUEL
18.19
14.95
14.95
14.81
12.67
05468
NO
X
IORYI
PPNV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
246.48
215.11
459.62
500.81
427.17
964.49
964.49
511.42
1774.60
260.71
148.20
HC
LB/IK
HOURS
215.11
964.49
964.49
260.73
148.20
ALDEHYDES
IDRYI
9.00
10.00
-0.00
-0.00
-0.00
-0.00
10.00
7.00
12.00
10.00
9.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.043
0.005
0.080
0.026
0.010
0.164
0.016
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/MR
21957.00
21230.36
44233.87
42831.55
44314.65
42821. 16
92821.56
72189.69
52989.10
29414.05
25429.88
NO
LB/IK
LB FUEL
2.21
7.90
7.90
0.04
1.53
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR L8/HR
20.08 20.08
26.11 26.11
98.19 98.19
57.25 57.25
64.19 64.19
509.74 509.74
509.74 509.74
54C.57 540.57
107.87 107.87
106.21 106.21
41.15 41.35
ISO NO
LB/IK EMISSION
HOURS LBS.
26.13 0.0052
509.74 0.0025
509.74 0.0421
106.21 0.0106
41.35 0.0028
0.0635
0.0060
1-33
-------
DATE: 7/zem
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: LYCOMING
ENGINE OAT*
CAL ID NUMBER: 234 ENGINE TYPE AND MODELt O-320-E2A
RATED HORSEPOKER: no.
ENGINE TOTAL TINE! 1394. HRS
FUEL: AV GAS 80/8T FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA »»».»«.».««««««.......»«.«.«»...«.«.««.««...«....»».
INLET AIR TEMPERATURE, DEGREES Fi START 84.50 FINISH 84.60
ATMOSPHERIC PRESSURE: START 30.05 FINISH 30.05
INLET AIR HUMIDITY. CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 44.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00. FLOW RATE. LITERS/MIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER! L-26201-27AC
9867
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 9.40
IDLE/TAXI 2 -0.0 10.50
RUN UP 3 -0.0 27.00
RUN UP-LEAN 4 -0.0 27.00
RUN UP-RICH 5 -0.0 28.10
TAKE-UFF 6 -0.0 66.80
CLIMB 7 -0.0 66.80
DESCENT 8 -0.0 37.50
DESCENT ON 8 -0.0 50.40
APPROACH 9 -0.0 17.60
TAXI
TEST
NODE
1
2
3
4
5
6
7
B
a
9
10
TEST
MODE
1
2
1
4
5
6
7
a
a
9
10
TEST
NODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
314.00
415.00
942.00
B74.00
9S6.00
1222.00
1222.00
1143.01
1043.00
852.00
448.00
MASS EMI
CO
LB/1K
LB FUEL
410.61
676.71
1066.28
1046.64
1035.49
1093.31
1093.31
878.06
1157.95
930.49
584.89
TIME IN
NUOE
NIN.
12.00
0.10
5. no
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
HC
LB/1K
LB FUEL
22.70
13.71
15.64
15.94
14.33
14.80
14.80
12.79
32.92
15. OB
1 1.62
MEASURED
FUEL FLOU
LB/HR
10.50
66.80
66.80
17.60
10.50
FUEL
-0,
CO
IORYI
PERCENT V
1.70
4.00
8.40
8.30
1.20
9.10
9.10
6.90
11.90
7.00
3.10
MASS EMI
ND2
LB/IK
18 FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
2.10
0.33
5.54
1.76
0.70
10.442
.0
CO
2
IORYI
PERCENT V
6.50
7. BO
7.30
7.50
7.60
7.50
7.50
a. so
5.30
8.00
7.50
MASS EMI
C02
LB/1K
LB FUEL
2466.80
2073.36
1455.97
1486.00
1501.94
1415.80
1415.80
1759.53
950.28
1670.86
7223.38
CO
LB/IK
LB FUEL
676.71
1093.31
1093.31
930.49
584.89
10.50
THC
IORYI
PPNV
1641.00
1415.00
2151.00
2207.00
1981.00
2151.00
2151.00
1755.00
5037.00
1981.00
1075.00
MASS EMI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
LTD CYCLE
CO
LB/IK
HOURS
7105.46
73033.06
73031.06
16376.57
6141.36
MEASURED CALCULATED
AIR FLOU F/A
LB/HR
128.00 0.03891
135.00 0.05528
304.00 0.07396
306.00 0.07438
321.00 0.07424
746.00 O.C7R09
746.00 O.C7809
453.00 0.07324
493.00 0.08113
208.00 0.07037
139.00 0.
NO
IORYI
PPNV
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/IK
LB FUEL
-0.00
-0.01
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
EMISSIONS
CO
EMISSION
LBS.
1.421
0.365
6.062
1.638
0.411
9.897
0.948
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
3859.75
7105.46
28789.59
28259.15
29097.35
73033.06
73033.06
32927.20
68440.81
16376.57
6141.36
HC
LB/IK
LB FUEL
13.71
14.80
14.80
15.08
11.62
04961
NU
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
Lfl/HR
213.39
143.96
422.22
430.36
402.60
988.70
988.70
479.65
1659.15
265.43
121.97
HC
LB/IK
HOURS
143.96
988.70
988.70
265.43
121 .97
ALDEHYDES
(DRY)
7.00
6.00
-0.00
-0.00
-0.00
-0.00
9.00
7.00
10.00
8. no
9.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
L8S.
0.029
0.005
0.082
0.027
0.008
0.151
0.014
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
23187.94
21770.32
39311.28
40122.08
42371.21
94575.38
94575.38
659U2.I1
47894.15
29407.16
23345.46
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS ENI MASS EMI
NO NOX
LB/HR LB/HR
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-o.oo -o.oo
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
Ml NO
LB/IK EMISSION
HCUaS LBS.
-0.00 -0.0000
-0.00 -0.0000
-0.00 -0.0000
-0.00 -0.0000
-0.00 -0.0000
-o.oooo
-0.0000
1-34
-------
DATE! T/28/71
TEST ORGANIIATIONI SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCONING
ENGINE 0»r«
SEOUL NUMBER! L-27474-27AA
CAL 10 NUMBER! 239 ENGINE TYPE «NO MODEL! 0-920-E2A
RATED HORSEPOMERI 110.
ENGINE TOTAL TINE! 1029. HIS
FUEL I *V GAS 80/8T FUEL H/C RATIOl 1.840
OPERATIONAL DATA *****»*
INLET AIR TEMPERATURE, DEGREES FI START 77.00 FINISH 77.00
ATMOSPHERIC PRESSURE! START 29.T6 FINISH 29.76
INLET AIR HUMIDITY, GRN H20/LB AIRI 0.01
RELATIVE HUNIOITYI 49.00 PERCENT
SAMPLE LINEl TEMPERATURE, DEGREES Cl -0.00. FLOW RATE, LITERS/NIN: 7.00
SAMPLE LINE TRANSPORT TIME, SECl 1.60
NUMBER OF TESTS! 11
COMMENTS!
386S
CARB. TEST ENGINE MEASURED
HEATER NODE RPN FUEL FLOW
LB/HR
IDLE-LOU 1 -0.0 17.60
IDLE/TAXI 2 -0.0 23.40
RUN UP 1 -0.0 41.00
RUN UP-LEAN 4 -0.0 32. BO
RUN UP-RICH 5 -0.0 41.00
TAKE-OFF 6 -0.0 7). BO
CLIMB 7 -0.0 73.80
DESCENT B -0.0 91.60
DESCENT ON B -0.0 91.60
APPROACH V -0.0 28.10
lAKI
TEST
MODE
a
9
10
TEST
NODE
1
2
3
4
5
6
7
a
B
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TFMP
DEGREES F
329.00
404.00
964.00
B97.00
99B.OO
1199.00
1199.00
1199.00
1121.00
A97.00
4*8.00
MASS EMI
CO
LB/I«
LB FUEL
961.71
1109.32
1123.14
1109.33
1124.92
1211.43
1211.43
1118.57
11II.9B
1190. OB
B19.69
TIME IN
NODE
HIN.
12.00
0.30
9.00
6.00
4.00
FOR CYCLE
FOR CVCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/U
LB FUEL
30.62
24.03
21.91
IB. 72
19.70
19.43
19.43
19.99
20.20
26.99
19.13
MEASURED
FUEL FLOW
LB/HR
23.40
73. BO
73. BO
2B.IO
19.90
FUEL
-0
CO
IORYI
PERCENT V
3.30
.00
.80
.60
.80
1 .10
1 .10
.80
.80
10.20
1.90
MASS EMI
102
LB/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
4.68
0.37
6.13
2.B1
1.33
19.318
0
CO
2
IDRYI
PERCENT V
.40
.70
.90
.60
.90
.10
.10
.60
7.70
7.30
5.60
MASS EMI
C02
IB/ IK
LB FUEL
1968.19
1369.34
1390.93
1379.88
1352.66
1217.91
1217.31
1362.97
1372.29
1293.27
1840.20
CO
LB/IK
LB FUEL
1109.32
1211.43
1211.43
1190.08
819.69
19.90
THC
IORYI
PPMV
1821.00
2269.00
3277.00
2829.00
2997.00
3109.00
3109.00
2997.00
3109.00
4174.00
1997.00
MASS EMI
NO
LB/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
LtO CYCLE
CO
LB/IK
HOURS
29998.02
89403.19
89403.19
32317.19
16231.38
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
202.00 0.0324B
297.00 0.09133
490.00 O.OBI89
363.00 0.08117
491.00 0.08176
789.00 0.08619
789.00 0.08619
969.00 0.08219
970.00 0.08267
309.00 O.OB332
243.00 0.
NO
IDRYI
PPHV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NDX
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
EMISSIONS
CO
EMISSION
LBS.
9.192
0.447
7.420
3.232
1.088
17.378
1.139
NO
2
IORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
cr>
LB/HR
17049.32
2595C.02
46048.97
36385.91
46121. 82
89403.19
89403.19
97718.06
97397.70
32317.15
16231.38
HC
LB/1K
LB FUEL
24.03
19.43
H.43
26.99
19.13
04915
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
938.83
562.21
881.88
614. 10
807.82
1434.16
1434.16
1010.92
1042.19
797.41
390.66
HC
LB/IK
HOURS
562.21
1434.16
1434.16
797.41
380.66
ALDEHYDES
IDRY)
7.00
-0.00
-0.00
-0.00
-0.00
-0.00
8.00
8.00
7.00
a:oo
6.00
MASS EMI
NU2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.112
0.007
0.119
0.076
0.026
0.340
0.022
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.30
-0.00
-0.00
MASS EMI
C02
LB/HR
27600.08
31948.97
39371.89
49299.92
99499.99
89891.81
89891. HI
70329.44
70809.94
36340.76
36619.93
NO
LB/U
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-fl.CO
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO ND>
LB/HH LB/HR
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
NO NO
LB/IK EMISSION
HOURS LBS.
-0.00 -0.0000
-0.00 -0.0000
-0.00 -0.0000
-0.00 -0.0000
-0.00 -0.0000
-0.0000
-0.0000
1-35
-------
O/tTEl 7/28/71
TEST ORGANISATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOMING
ENGINE OAT*
t»L ID NUMBER! 236 ENGINE TYPE AND MODEL! 0-120-E2A
RATED HORSIPOKERl 130.
ENGINE TOTAL TINE: 1026. MRS
FUEL: »V GAS 80/87 FUEL H/C RATIO! 1.8*0
OPERATIONAL DATA »»«««»«»«««»
INLET AIR TENPERATUREt DEGREES Ft START 77.50 FINISH 77.30
ATMOSPHERIC PRESSURE! START 21.76 FINISH 29.76
INLET AIR HUMIDITY, CRN H20/LB AIRl 0.01
RELATIVE HUMIDITY: 51.oo PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOH RATE, LITERS/BIN: 7.00
SAMPLE LINE TRANSPORT TIME, SECl 1.60
NUMBER OF TESTS: II
COMMENTS:
SERIAL NUMBER! L-27474-27AB
S371
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOW I -0.0 17.60
IDLE/TAXI 2 -0.0 22.30
RUM UP 3 -0.0 37.30
RUN UP-LEAN 4 -0.0 34.00
RUN UP-RICH 5 -0.0 34. 00
TAKE-OFF 6 -0.0 70.30
CLIMB 7 -0.0 70.30
DESCENT 8 -0.0 51.60
DESCENT ON 8 -0.0 52.70
APPROACH 9 -0.0 28.10
TAXI
TEST
MODE
1
2
3
4
5
6
7
a
a
9
10
TEST
MODE
1
2
a
8
9
10
IEST
none
l
6
7
9
10
TOTAL
TOTAL
FXHAUST
GAS
TEMP
DEGREES F
269.00
404.00
986.00
919.00
1166.00
1199.00
1199.00
1155.00
1121.00
419.00
504.00
MASS tMI
CO
Lfl/lK
LI FUEL
795.22
991.64
1124.99
1 1 30 . 0 1
1081.06
1223.55
1223.55
1146.54
1136.02
1161.47
823.96
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
30.42
21.17
22.28
21.97
20.39
21.33
21.13
18.84
20.73
25.20
17.96
MEASURED
FUEL FLOW
LB/HR
22.30
70.30
70.30
28.10
22.30
FUEL
-0
cn
IORY)
PERCENT V
1.90
3.70
6.70
6.50
6.70
8.70
3.70
7.50
7.10
6.70
2.90
MASS EMI
N02
LB/1K
LB FUEL
o.c
0.0
o.o
0.0
0.0
0.0
0.0
o.o
0.0
0.0
0.0
FUEL
USED
IBS.
4.46
0.35
5.83
2.81
1.49
14.950
0
CO
2
(ORYI
PERCENT
2.80
3.70
5.10
4.90
5.60
5.40
5.40
5.50
5.30
4.70
4.10
MASS EMI
C02
LU/IK
LB FUF.L
1841.32
1558.09
1345.50
1338.46
1419.71
1193.26
1193.26
1321.08
1332.43
1280.18
1830.33
CO
LB/1K
LB FUEL
991.64
1223.55
1223.55
1161.47
823.96
22.30
THC
(DRY)
PPMV
V
1269.00
1379.00
2317.00
2207.00
2207.00
2648.00
2648.00
2152.00
2262.00
2538.00
1104.00
MASS EMI
NO
LB/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
LTD CYCLE
CO
LB/1K
HOURS
22113.51
86015.50
86015.50
32637.37
18374.28
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
214.00 0.02283
256.00 0.03554
410.00 0.05643
371.00 0.05455
379.00 0.05859
740.00 0.06733
740.00 0.06733
561.00 0.06184
575.00 0.05417
301.00 0.05476
271.00 0.
NO
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/1K
LB FUF.L
-0.00
-o.oo
-o.ou
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
EMISSIONS
CO
EMISSION
LBS.
4.423
0.430
7.139
3.264
1.231
16.487
1.103
NO
2
IDRVI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
13995.86
22113.51
42187.24
38420.38
36755.89
86015.50
86015.50
59161.46
59868.45
32637.37
18374.28
HC
LB/1K
LB FUEL
21.17
21.33
21.33
25.20
17.96
03345
NO
X
(ORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
535.37
472.03
835.56
747.13
693.43
1499.41
1499.41
972.22
1092.39
708.07
400.61
HC
LB/1K
HOURS
472.03
1499.41
1499.41
708.07
400.61
ALDEHYDES
IORY)
6.00
6.00
-0.00
-0.00
-0.00
-0.00
6.00
6.00
6.00
6.00
5.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.094
0.007
0.124
0.071
0.027
0.324
0.022
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS F.HI
C02
LB/HR
32407.25
34745.30
50456.21
45507.49
48270.14
83886.00
83886.00
68167.69
70218.88
35972.99
40816.39
NO
Lfl/lK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
NO ND
LB/IK EMISSION
HCURS LBS.
-0.00 -0.0000
-0.00 -0.0000
-0.00 -0.0000
-0.00 -0.0000
-0.00 -0.0000
-o.oooo
-0.0000
1-36
-------
DATE! T/28/71
TfST ORGANUATIONI SCOTT/GEN AVIATION
ENCINE SUPPLIER! LYCOMING
ENGINE DATA
CAL ID NUMBER: 237 ENGINE TYPE »NO MODELI O-SZO-EZA
RATED HORSEPOHFR: 150.
ENGINE TOTAL TINEI 1025. MRS
FUEL: AV GAS 80/87 FUEL H/C RATIO! 1.840
OPERATIONAL DATA ««<.»»««»»».«»»«««««..»««»«»«.«.»«
INLET AIR TEMPERATURE, DEGREES F: START 76.50 FINISH 76.90
ATMOSPHERIC PRESSURE! START 24.76 FINISH 29.76
INLET AIR HUMIDITY. CRN H20/LB AIRa 0.01
RELATIVE HUMIDITY! SO.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES Cl -O.OC, FLOM RATE, LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TIME, SECt 1.60
NUMBER OF TESTS! 11
COMMENTS:
SERIAL NUMBER! L-2T4T4-27AC
J373
CAHB. TFST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOW | -0.0 11.90
IDLE/TAXI 2 -0.0 19.90
RUN UP 3 -0.0 34.00
RUN UP-LEAN 4 -0.0 32.80
RUN UP-RICH 5 -0.0 32.80
TAKE-OFF 6 -0.0 72.70
CLINK 7 -0.0 72.70
DESCENT 8 -0.0 50.40
DESCENT ON 8 -0.0 50.40
APPROACH 9 -0.0 25.80
TAXI
TEST
KOBE
1
2
3
4
5
6
7
a
e
i
10
TEST
NODE
I
2
)
4
5
6
7
H
a
t
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
56.00
415.00
919.00
830.00
986.00
1188.00
nna.oo
1143.00
1121.00
919.00
504.00
MASS EMI
CO
LB/1K
LS FU6L
703.49
905.51
1152.97
1117.41
11)3.16
1217. 80
1237.80
1133.88
1090.77
1153.15
738.11
TINE IN
NODE
NIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE /IB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EHI
HC
LB/IK
LB FUEL
20.90
20.09
24.11
21. ar
21.31
19.04
19.04
18.98
19.41
25.80
1 7.50
NEASURFO
FUEL FLti*
LB/HR
19.90
72.70
72.70
25.80
21.10
FUEL
-0.
CO
IORYI
PERCENT V
2.50
5.20
10.20
10.10
10.00
11.40
11.40
10.10
9.50
10.10
4.60
MASS FMI
N02
LR/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
L9S.
1.98
0.36
6.03
2.58
1.41
14.371
.0
CO
2
(ORYI
PERCENT V
4.50
6.20
7.30
7.50
7.50
6.90
6.90
7.60
7.80
7.20
7.80
MASS EMI
C02
LB/IK
LB FUEL
1989.62
1696.37
1296.52
1327.08
1335.34
1177.15
1177.15
1340.59
1407.15
1291.62
1966.51
CO
LS/IK
L8 FUEL
905.51
1237.80
1237.80
1153.15
738.11
21.10
THC
(DRY)
PPMV
17Q3.00
2014.00
3724.00
3393.00
3283.00
3062.00
3062.00
2952.00
2952.00
3945.00
1904.00
MASS EMI
Nil
LB/iK
LB FUEL
0.51
0.57
1.24
o.ao
0.95
1.05
1.05
1.44
2.64
l.ll
0.95
LTD CYCLE
CO
LB/IK
HOURS
18019.70
89987.61
89987.63
29751.19
15574.08
MEASURED CALCULATED
AIR FLOM F/A
LB/KR
249.00 0.03371
237.00 . 0.05411
369.00 0.08311
359.00 0.08335
359.00 0.08283
764.00 0.08672
764.00 0.08672
552.00 0.08357
562.00 0.08162
280.00 0.08232
261.00 0.
NO
IDRV)
PPMV
11.00
20.00
67.00
43.00
51.00
59.00
59.00
78.00
140.00
59.00
36.00
MASS EMI
HOI
LB/IK
LI FUEL
0.51
0.57
1.24
o.no
0.95
l.OS
1.05
1.44
2.64
1.11
0.95
EMISSIONS
CO
EMISSION
LBS.
3.604
0.450
7.469
2.975
1.043
15.541
1.081
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
13999.50
18019.70.
39201.08
37307.10
37167.69
89997.61
B99d7.63
57147.47
54974.58
29751.19
15574.08
HC
LB/IK
LB FUEL
20.09
19.04
19.04
25.80
17.50
05829
NO
X
IORYI
PPHV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
575.04
399.71
819.70
717.79
698.85
1384.29
1384.29
956.62
978.36
665.54
369.20
HC
LB/IK
HOURS
399.71
1)84.29
1384.29
665.54
369.20
ALDEHYDES
IDRYI
7.00
7.00
-0.00
-0.00
-0.00
-0.00
8.00
8.00
7.00
e.oo
6.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
o.o
0.0
HC
EMISSION
LBS.
0.080
0.007
0.115
0.067
0.025
0.293
0.020
SMOKE
-O.QO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS CHI
C02
LB/HR
39593.46
33757.81
44081.74
43528.09
43799.09
85578.69
85578.69
67565. Kl
70920.31
33323.73
41493.24
NO
LB/IK
LB FUEL
0.57
1.05
1.05
1.11
0.95
PARTICULATES
-0.00
-O.nO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
10.12 10.12
11.38 11.38
42.30 42.30
26.09 26.09
31.14 31.14
76.50 76.50
76.50 76.50
72.49 72.49
133.07 133.07
28.55 28.55
20.02 20.02
NO NO
LB/IK EMISSION
HOURS LBS.
11.38 0.0023
76.50 0.0004
76.50 0.006)
28.55 0.0029
20.02 0.0013
0.0132
0.0009
1-37
-------
DATE: 7/29/71
TEST ORGANIZATION! SCOTT/CEN AVIATION
ENGINE SUPPLIES! LVCWING
ENGINE DATA
CAL ID NUMBER: 241 ENGINE TYPE AND MODEL I O-320-E2A
RATED HORSEPOWER: iso.
ENGINE TOTAL TINEI 767. MRS
FUEL! AV GAS 80/87 FUEL H/C RATIO! 1.840
OPERATIONAL DATA »«««««»«*»«««»»»«»««»«««»«««»«»»!
INLET AIR TEMPERATURE, DEGREES F: START 81.00 FINISH 81.00
ATMOSPHERIC PRESSURE: START 29.80 FINISH 29.80
INLET AIR HUMIDITY. CRN H20/L8 AIR! 0.01
RELATIVE HUMIDITY: 42.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00. FLOM RATE, LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER I L-2784»-27»A
9875
CARB. TCST ENGINE MEASURED
HEATER MODE RPM FUEL FLOM
Lfl/HH
IDLE-LOU 1 -0.0 12.90
IDLE/TAXI 2 -0.0 14.10
RUN UP 3 -0.0 35.20
RUN UP-LEAN 4 -0.0 35.20
RUN UP-RICH 5 -0.0 34.00
TAKE-OFF 6 -0.0 73.80
CLIMB 7 -0.0 73.80
DESCENT 8 -0.0 SI. 60
DESCENT ON 8 -0.0 44.50
APPROACH 9 -0.0 22.30
TAXI
TEST
MODE
1
2
3
4
5
6
7
a
8
9
10
TfST
MODE
1
2
3
4
5
6
7
a
a
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
FXHAUST
GAS
TEMP
DEGREES F
381.00
471.00
998.00
942.00
1076.00
1379.00
1379.00
1312.00
1312.00
1031.00
594.00
MASS EMI
CO
LB/1K
LB FUEL
916.70
85-..B8
1036.28
1019.98
100ft. 48
1149.23
1149.23
1085.81
944.06
1123.03
630.07
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LS/IK
LB FUFL
22.94
16.62
16.71
15.60
15.31
14.51
14.51
14.83
14.06
21.62
12.26
MEASURED
FUEL FLOl.
LB/HR
14.10
73.80
73.80
22.30
11.70
FUEL
-0.
CO
IORYI
PERCENT V
3.00
4.90
a. 90
8.70
8.60
10.60
10.60
9.80
7.90
1.80
2.90
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
2.82
0.37
6.13
2.23
0.78
12.128
.0
CO
2
(DRY)
PERCENT V
4.10
6.50
8.20
8.40
a. 40
7.80
7.80
8.20
a.ao
7.50
6.30
MASS EMI
C02
LB/IK
LB FUEL
1796.68
1783.88
1500.17
1538.25
1547.69
1328.73
1328.73
1427.51
1652.32
1350.40
2150.64
CO
LB/IK
LB FUEL
855.88
1149.23
1149.23
1123.03
630.07
11.70
THC
(DRY)
PPMV
1436.00
1661.00
2506.00
2337.00
2280.00
2337.00
2337.00
2337.00
2055.00
3294. OC
985.00
MASS EMI
NO
LB/IK
LB FUEL
0.7D
1.3?
3.61
2.60
2.81
2.83
2.83
1.80
6.311
I. 81
1.64
LIO CYCLE
CO
LB/IK
HOURS
12067. B5
84813.44
84813.44
25043.50
7371.76
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
156.00 0.03408
170.00 0.05387
401.00 0.08032
404.00 0.08017
392.00 0.07968
808.00 0.08647
808.00 0.08647
579.00 0.08444
525.00 0.07802
245.00 O.C8190
152.00 0.
NO
IORYI
PPMV
17.00
46.00
189.00
136.00
146.00
159.00
159.00
99.00
321.00
96.00
46.00
MASS FMI
NOX
LB/IK
LB FUEL
0.7B
1.32
3.61
2.60
2.81
2.83
.2.83
1.80
6.30
i.ai
1.64
EMISSIONS
CO
EMISSION
LBS.
2.414
0.424
7.040
2.504
0.494
12.875
1.044
NO
2
(DRV)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
CO
Ld/HR
10791.39
1200'. 85
36477.06
35692.12
34288.16
84813.44
84813.44
56027.69
42010.79
25043.50
7371. 7B
HC
LB/IK
LB FUEL
16.62
14.51
14.51
21.62
12.26
04331
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
795.89
234.29
588.24
549.11
520.63
1070.93
1070.93
765.21
625.88
482.10
143.40
HC
LB/IK
HOURS
234.29
1070.93
1070.93
482.10
143.40
ALDEHYDES
IORVI
13.00
4.00
-0.00
-0.00
-0.00
-0.00
6.00
5.00
5.00
6.00
5.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.047
0.005
0.089
0.048
0.010
0.199
0.016
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C03
LB/HR
23177.09
25152.75
52805.94
54146.53
52621.50
98059.94
9B059.94
73659.44
73528.31
301 13.98
25162.49
NO
LA/IK
LB FUEL
1.32
2.H3
2.13
l.ftl
1.64
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
10.05 10.05
18.61 18.61
127.24 127.24
91.65 91.65
95.61 95.61
208.97 208.97
20H.97 208.97
92.97 92.97
280.39 280.39
40.30 40.30
19.21 19.21
NO NO
LB/IK EMISSION
HOURS LBS.
18.61 0.0037
208.97 0.0010
20B.9T 0.0173
40.30 0.0040
19.21 0.0013
0.0274
0.0022
1-38
-------
MTEl 7/21/71
TEST 0*5AN HAT I ON I SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOMING
CNCINE 0»T« «
SERIAL NUMBER I L-JT«4»-»»Ai
CAL 10 NUMBER I 242 ENGINE TYPE »ND NODEll 0-12O-E2*
RATED NORSIPOHeRl HO.
ENGINE TOTAL TINII 741. MRS
FUEL I »V 0»l 60/67 FUEL N/C «»TIOI I. MO
OPERATIONAL DATA »»»«»«»«»
INLET AIR TEMPERATURE, DEGREES Fl START 62.30 FINISH 12.30
ATMOSPHERIC PRESSUREl START 21.«0 FINISH 24.60
INLET AIR HUBIDITT, GkN H20/LB AIRI 0.01
RELATIVE HUNIOITTl «0.00 PERCENT
SAMPLE LINEl TEMPERATURE. OECREES Cl -0.00, FLOU RATE. LITERS/MINI T.OO
SAMPLE LINE TRANSPORT TINE, SECl 1.40
NUNSER OF TESTSI II
CONNENTSl
J877
CAR). TFST ENCINE NEtSUREO
HEATER NODE RPN FUEL FLOW
LB/HR
IDLE-LOU -0.0 12.40
IDLE/TAXI -0.0 12.40
RUN UP -0.0 32.80
RUN UP-LEAN -0.0 31.60
RUN UP-RICH -0.0 32.60
TAKE-OFF -0.0 70.30
CLIMB -0.0 TO. 10
DESCENT -0.0 50.40
DESCENT ON -0.0 41.00
APPROACH -0.0 17.60
TA«I
TEST
MODE
7
9
a
i
10
TEST
NODE
1
2
I
4
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EIHAUST
GAS
TEMP
DECREES F
241.00
404.00
964.00
652.00
1244.00
1278.00
1278.00
1211.00
1211.00
964.00
471.00
MASS EMI
CO
LB/1K
in FUEL
372.21
6S8.28
1041.16
1042. IS
1010.24
1160.53
1160.53
1076.60
418.07
1123.43
577.04
TINE IN
NOUE
NIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/IB
10
EIHAUST
CAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-O.OD
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS ENI
HC
LR/1K
LB FUEL
18.65
15.23
17.45
16.37
16.73
15.62
15.82
15.46
14.52
22.26
13.04
MEASURED
FUEL FLOW
LB/HR
12.40
70.10
70.10
17.60
11.70
FUEL
-0
CO
(ORYI
PERCENT V
1.40
3.50
4.00
4.00
8.40
10.60
10.60
4.40
7.40
4.70
2.60
NASS ENI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
18$.
2. SB
0.15
5.81
1.76
0.76
11.110
0
CO
2
(DRY)
PERCENT V
4.70
7.10
B.20
8.20
8.10
7.60
7.60
8.00
8.40
7.40
6.40
NASS (Ml
C02
LB/IK
LB FUEL
2224.02
209B.I6
1440.46
1441.84
1504.61
1307.18
1307.18
1414.42
1660.44
1347.22
2231.80
CO
LB/IK
LS FUEL
658.28
1160.53
1160.53
1123.43
577.04
II. TO
THC
1 ORYI
PPNV
1081.00
1414.00
2634.00
2468.00
2523.00
2523.00
2525.00
2357.00
2115.00
1355.00
1026.00
NASS ENI
NO
LB/IK
LB FUEL
1.24
1.62
4.14
2.68
2.64
2.8»
2.88
2.46
T.78
2.17
2.22
LTD CYCLE
CO
LB/IK
HOURS
8441.78
61585.16
61565.38
14781.14
6751.42
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
168.00 0.03146
166.00 0.04467
373.00 0.08085
360.00 0.08077
375.00 0.08076
765. OD 0.08571
765.00 0.08571
567.00 0.0617]
465.00 0.07844
143.00 0.08103
154.00 0.
NO
IORYI
PPMV
26.00
59.00
218.00
141.00
134.00
160.00
160.00
131.00
344.00
114.00
61.00
NASS EMI
NOK
LB/IK
LB FUEL
.24
.62
.14
.68
.64
.88
.en
.46
.78
.17
.22
EMISSIONS
CO
EMISSION
LBS.
1.648
0.408
6.772
1.478
0.452
11.108
I. 000
NO
2
IORVI
PPMV
'0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS ENI
CO
L6/HR
7381.51
8441.76
34149.87
32411.79
11741.41
81565.18
81585.18
5427C.45
18460.88
14781.14
6751.42
HC
LB/IK
LB FUEL
li.23
15.82
15.62
22.26
11.04
04216
NO
X
(DRY)
PPNV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS ENI
HC
LB/HR
240.53
146.48
572.41
517.21
548.64
1112.16
1112.16
774.17
545.30
341.85
152.54
HC
LB/IK
HOURS
146.46
1112.16
1112.16
341.65
152.54
ALDEHYDES
IORYI
4.00
7.00
-0.00
-0.00
-0.00
-0.00
7.00
4.00
6.00
7.00
5.00
NASS ENI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.014
0.006
0.042
0.034
0.010
0.187
0.016
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS ENI
C02
LB/HR
26684.85
27066.14
48687.54
47143.83
44515.27
41904.06
41404.06
72371.75
66060.06
21710.46
26112.01
NO
IB/IK
LB FUEL
1.82
2.88
2.08
2.17
2.22
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
-o.oo
MASS ENI NASS EMI
NO N0>
LB/MR LB/HR
16.54 16.54
23.51 23.51
135.87 135.67
84.74 84.74
86.64 86.64
202.28 202.28
202.26 202.28
124.23 124.21
119.07 114.07
18.14 18.14
26.02 26.02
NO NO
LB/IK EMISSION
HOURS LBS.
21.51 0.0047
202.28 0.0010
202.28 0.0168
18.14 0.0036
26.02 0.0017
0.0261
0.0023
1-39
-------
OATEl 7/28/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCONING
ENGINE OUT* *»»******»«**»»»***»*»»**»»»
C»L 10 NUMBER! 243 ENGINE TYPE AND MODEL! O-320-62*
RATED HORSEPOHERl 150.
ENGINE TOTAL TINEl 768. HRS
FUEL: AV GAS 80/87 FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA «««.««..«.»«««.«««««».....«..«.........«...........».«
INLET AIR TEMPERATURE, DEGREES fl START 86.00 FINISH 86.00
ATMOSPHERIC PRESSURE! START 29.80 FINISH 29.80
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 34.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLO* RATE, LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TIME, SEC! 1.60
NUMBER OF TESTS: II
COMMENTS:
SERIAL NUMBER! L-27B46-27AC
9879
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 11.70
IDLE/TAXI 2 -0.0 11.70
RUN UP 3 -0.0 31.60
RUN UP-LEAN 4 -0.0 30.50
RUN UP-RICH 5 -0.0 30.50
TAKE-OFF 6 -0.0 71.50
CLIMB 7 -0.0 71.50
DESCENT S -0.0 46.90
DESCENT ON a -0.0 44.50
APPROACH 9 -0.0 17.60
TAXI
TEST
MODE
1
2
3
4
5
6
7
a
a
9
10
TEST
MODE
1
2
1
4
5
6
7
a
a
9
10
TEST
MODE
2
6
7
q
10
TOTAL
TOTAL
EXHAUST
GAS
TFMP
DEGREES F
269.00
392.00
R97.00
785.00
975.00
1256.00
1256.00
1166.00
1166.00
919.00
437.00
1ASS EMI
CO
LB/1K
LB FUEL
435.76
595.43
10)5.67
1042.34
1025.01
1154.77
1154.77
1100.21
991.73
1119.33
561.76
TIME IN
MODE
Ml N.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LH
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
16.15
12.98
17.38
16.76
16.30
15.24
15.24
14.95
14.29
22.35
11.66
MEASURED
FUEL FLOH
L3/HR
11.70
71.50
71.50
17.60
11.70
FUEL
-0
CO
(DRY)
PERCENT V
1.40
3.10
a. 90
a. 90
a. eo
10.60
10.60
9.60
8.40
10.00
2.50
MASS EMI
N02
LB/1K
LB FUEL
n.o
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LUS.
2.14
0. 16
5.93
1.76
0.78
11.176
0
CO
2
(DRY)
PERCENT
5.00
7.30
a. 20
B.10
a. 30
7.70
7.70
7.80
8.50
7.70
6.40
MASS EMI
C02
IB/IK
LB FUEL
2445.26
2203.08
1499.29
1490.53
1519.01
1318.02
1318.02
1404.55
1576.79
1354.21
2259.60
CO
LB/1K
LB FUEL
595.43
1154.77
1154.77
1119.33
561.76
11.70
THC
(DRY)
PPMV
V
906.00
1180.00
2608.00
2498.00
2443.00
2443.00
2443.00
2278.00
2114.00
3486.00
906.00
MASS EMI
NO
LB/1K
LB FUEL
0.82
1.26
2.62
1.69
1.84
1.75
1.75
1.28
3.84
1.42
1.48
LTD CYCLE
CO
LB/1K
HOURS
6966.52
82566.31
82566.31
19700.20
6572.63
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
159.00 0.03039
154.00 0.04878
360.00 O.OB037
346.00 0.07989
349.00 0.08025
779.00 0.08610
779.00 0.08610
523.00 0.08177
517.00 0.07909
194.00 0.08378
155.00 0.
NO
10RYI
PPMV
16.00
40.00
137.00
88.00
96.00
98.00
98.00
68.00
198. 00
77.00
40.00
MASS EMI
NOX
LB/1K
LB FUEL
0.82
1.26
2.62
.69
.84
.75
.75
.28
.84
.42
1.48
EMISSIONS
CO
EMISSION
LBS.
1.393
0.413
6.853
1.970
0.440
11.070
C.990
NO
2
(ORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
-o.oo
MASS EMI
CO
LB/HR
5098.36
6966.52
32727.20
31791.24
31262.77
82566.31
82566.31
51599.77
44132.11
19700.20
6572.63
HC
LB/IK
LB FUEL
12.9B
15.24
15.24
22.35
11.66
04185
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
188.96
151.87
549.25
5 1 1 . 04
497.07
1089.85
1089.85
701.25
636.10
393.32
136.42
HC
LB/IK
HOURS
151.87
1089.85
1089.85
393.32
136.42
ALDEHYDES
(ORV)
7.00
9.00
-0.00
-0.00
-0.00
-0.00
7.00
7.00
7.00
3.00
6.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.030
0.005
0.090
0.039
0.009
0.175
0.016
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/Hrt
28609.55
25776.00
47377.38
45461.20
46329.86
94238.00
94238.00
65873.25
70167.06
23834. 14
26437.30
NO
LB/IK
LB fUEL
1.26
1.75
1.75
1.42
1.48
PARTICULATES
-0.00
-O.CO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LE/HR LB/HR
9.57 9.57
14.77 14.77
82.75 82.75
51.63 51.63
56.02 56.02
125.38 125.38
125.38 125.38
6C.04 60.04
170.87 170.87
24.92 24.92
17.27 17.27
NO NO
LB/1K EMISSION
HOURS LBS.
14.77 0.0030
125.38 0.0006
125.38 C.0104
24.92 0.0025
17.27 0.0012
0.0176
0.0016
1-40
-------
DATE: 7/30/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: ITCOX INC
ENGINE 0»t»
C»L ID NUNBER: 2si ENGINE TYPE AND MOOED 0-320-62*
RATED HORSEPOWER! 190.
ENGINE TOTAL TINEl 720. MRS
FUEL: AV 0»S 80/87 FUEL H/C RATIOI 1.840
OPERATIONAL DATA ««««««»««««
INLET AIR TEMPERATURE. DEGREES f> START 74.00 FINISH 72.00
ATMOSPHERIC PRESSUREl START 29.89 FINISH 29.89
INLET AIR HUMIDITY, CRN H2O/LH AIRl 0.01
RELATIVE HUMIOITYl 52.00 PERCENT
SAMPLE LINEl TEMPERATURE. CEGREES Cl -0.00, FLOM RATE, LITERS/MINI T.OO
SAMPLE LINE TRANSPORT TINE. SEC: 1.60
NUNBER OF TESTS: II
COMMENTS:
SERIAL NUMBER I L-16344-2TAB
S881
CARD. TST ENGINE MEASURED
HEATER NODE RPH FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 I*. 10
IDLE/TAXI 2 -0.0 16.40
RUN UP 3 -0.0 35.20
RUN UP-LF.AN 4 -0.0 14.00
RUN UP-RICH 9 -0.0 34.00
TAKE-OFF 6 -0.0 71.90
CLIMB 7 -0.0 71.90
DESCENT a -0.0 49.70
DESCENT ON 8 -0.0 $0.40
APPROACH 9 -0.0 21.40
TAXI
TEST
MODE
,
2
1
4
5
6
7
a
a
-------
OATEl 7/30/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOHING
ENGINE DATA
CAL ID NUHBEK: 212 ENGINE TYPE AND NODEL> 0-320-62*
RATED HORSEPOKER: 1>0.
ENGINE TOTAL TIME! T20. MRS
FUEL: «V GAS 80/87 FUEL H/C RATIO! 1.8*0
OPERATIONAL DATA »»»»«««««««»«»»»
INLET AIR TENPERATURE. DEGREES F: START 71.00 FINISH 72.00
ATMOSPHERIC PRESSURE! START 29.85 FINISH 29.85
INLET AIR HUMIDITY, CRN H20/LB AIRl 0.01
RELATIVE HUMIDITY: 57.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOti RATE, LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TIME, SECl 1.60
NUMBER OF TESTSl II
COMMENTS:
SERIAL NUMBER 1 L-16344-27AC
9883
CAR9. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOU
LB/HR
IDLF-LOH 1 -0.0 14.10
IDLE/TAXI 2 -0.0 14.10
RUN UP 3 -0.0 34.00
RUN UP-LEAN 4 -0.0 32.80
RUN UP-RICH 5 -0.0 34.00
TAKE-OFF 6 -0.0 69.10
CLIMB 7 -0.0 64.10
DESCENT 8 -0.0 41.00
DESCENT ON 8 -0.0 44.50
APPROACH 1 -0.0 22.30
TAXI
TEST
MODE
1
2
3
4
5
6
7
3
a
9
10
TEST
MODE
1
2
3
4
S
6
7
8
a
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TFMP
DEGREES F
280.00
426.00
998.00
942.00
1054.00
1323.00
1323.00
1233.00
1199.00
919.00
448.00
MASS FMT
CO
LB/1K
L1) FUEL
479.92
562.43
1063.31
1036.82
1070.49
1030.04
1030.04
842.94
990.47
1028.10
449.01
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/Lfl
10
EXHAUST
GAS
PRESSUHE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
18.32
16.21
17.15
16.30
15.14
13.60
13.60
12.40
14.95
17.63
14.12
MEASURED
FUEL FLOM
LB/HR
14.10
69.10
69.10
22.30
14.10
FUEL
-0
CO
(DRY)
PERCENT V
1.40
2.40
7.80
7.60
8.00
a. 10
8.10
6.20
7.50
7.70
1.80
MASS EMI
N02
Lfl/lK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
2.B2
0.15
5.74
2.23
0.94
12.075
0
CO
2
IDRYI
PERCENT
4.40
6. 10
6.80
7.00
6.90
7.60
7.60
8. 50
7.60
7.20
6.20
MASS EMI
C02
LB/1K
LB FUEL
2369.92
2246.07
1456.51
1500.46
1450.71
1518.52
1518.52
1815.78
1576.99
1510.48
2430.03
CO
LB/1K
LB FUEL
562.4}
1030.04
1030.04
1028.10
449.01
14.10
THC
(ORV)
PPMV
V
933.00
1208.00
2196.00
2086.00
1976.00
1867.00
1867.00
1592.00
1976.00
2306.00
988.00
MASS EMI
NO
LB/1K
LB FUEL
1.30
1.77
2.66
2.06
1.78
2.30
2.30
4.38
6.62
2.43
4.18
LTO CYCLE
cn
LB/1K
HOURS
7930.21
71175.56
71175.56
22926.66
6331.00
MEASURED CALCULATED
AIR FLOU F/A
LB/HR
189.00 0.02767
186.00 0.04018
383.00 0.06901
373.00 0.06889
383.00 0.07027
790.00 0.07372
790.00 0.07372
500.00 0.06863
517.00 O.U7097
254.00 0.07033
191.00 0.
NO
(DRY)
PPNV
23.00
46.00
119.00
92.00
81.00
110.00
110.00
196.00
305.00
lll.no
102.00
MASS EMI
NOX
LB/1K
L6 FUEL
1.30
1.77
2.66
2.06
1.78
2.30
2.30
4.38
6.62
2.43
4.18
EMISSIONS
CO
EMISSION
LBS.
1.586
0.356
5.908
2.293
0.424
10.566
0.875
NO
2
IDHV)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
CO
LB/HR
6766.91
7930.21
36152.54
34007.54
36396.76
71175.56
71175.56
34560.65
44075.76
22926.66
6331.00
HC
LB/1K
LB FUEL
16.21
13.60
13.60
17.63
14.12
03772
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
HC
LB/HR
258.28
228.60
582.94
534.59
514.88
939.58
939.58
508.25
665.08
393.24
199.02
HC
LB/1K
40URS
228.60
"39.58
939.58
393.24
199.02
ALDEHYDES SMOKE
(DRY)
3.00
3.00
-0.00
-0.00
-0.00
-0.00
.00
.00
.00
.00
.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.046
0.005
0.078
0.039
0.013
0.181
0.015
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
33415.92
31669.52
49521.21
49215.02
49324.72
104929.50
104929.50
74447.00
70176.25
33683.77
34263.38
NO
L8/1K
LB FUEL
1.77
2.30
2.30
2.43
4.18
PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MASS EMI MASS EMI
ND NOX
LB/HR LB/HR
18.26 18.26
24.97 24.97
90.60 90.60
67.62 67.62
60.53 60.53
15P..77 158.77
158.77 158.77
179.46 179.46
294.41 294.41
54.29 54.29
58.93 58.93
NO NO
IB/ lH EMISSION
HOURS LBS.
24.97 C.0050
158.77 O.OOOB
158.77 0.0132
54.29 0.0054
51.93 0.0039
(1.0283
0.0023
1-42
-------
DATE! T/28/71
tKT OBGANItATIONl SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCONINC
ENGINE DATA
CAL 10 NUMBER! 260 ENGINE TYPE AND MODELI 0-320-E2A
RATED HORSEPOMERI 130.
ENGINE TOTAL TIME! 130. KRS
FUEL! AV GAS 80/87 FUEL H/C RATIO! 1.840
OPERATIONAL DATA *»**»**»».»*
INLET AIR TEMPERATURE, DEGREES Fl START 86.00 FINISH 66.00
ATMOSPHERIC PRESSUREl START 30.15 FINISH 30.19
INLET AIR HUMIDITY, GUN H20/LB AIRI 0.01
RELATIVE HUMIDITY! 45.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES Ct -0.00, FLOH RATE, LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TINE, SECl 1.60
NUMBER OF TESTS! 11
COMMENTS!
SERIAL NUMBER! L-29302-2TAB
3385
CARB. TEST ENGINE MEASURED
HEATER HOilE RPN FUEL FLOW
LB/HR
1 OLE-ton 1 -0.0 7.00
IDLE/TAXI 2 -0.0 5.30
RUN UP 1 -0.0 15.80
RUN UP-LEAN 4 -0.0 15.80
RUN UP-RICH 5 -0.0 15.80
TAKE-OFF 6 -0.0 38.70
CLIMB 7 -0.0 38. TO
DESCENT 8 -0.0 22.90
DESCENT ON B -0.0 22.90
APPROACH 9 -0.0 15.80
TAXI
TEST
MOOE
1
2
3
4
5
6
7
a
a
9
10
TEST
MODE
1
2
3
4
5
6
T
8
B
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DECREES f
791.00
404.00
1020.00
986.00
1076.00
1300.00
1300.00
1222.00
1188.00
919.00
448.00
MASS FMI
CO
LB/1K
LR FUEL
757.00
869.81
1013.06
994.66
996.06
1068.62
1068.62
895.16
842.48
1041.49
7A8.06
TIME IN
NODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIli
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
IB/IK
LB FUEL
23.09
20.60
18.19
17.71
16.10
14.59
14.59
14.49
13.86
20.77
18.51
NEASUHED
FUEL FLOW
IB/Ml
5.30
38.70
38.70
15.80
5.30
FUEL
-0
CO
(DRY)
PERCENT V
4.40
.40
.00
.80
.80
.00
.00
.00
.50
.40
5.10
MASS EMI
NU2
IB/IK
LB FUEL
0.0
0.0
0.0
3.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
1.06
0.19
3.21
1.58
0.36
6.401
0
CO
2
(OR VI
PERCENT V
7.10
8.20
7.70
7.80
7.80
7.80
7.80
8.60
B. 90
7.30
8.10
MASS EMI
C02
LB/1K
LB FUEL
1919.28
1751.05
1532.05
1562.83
1565.03
1415.17
1455.17
IT2T.98
1812.49
1449.43
1916.67
CO
IB/ IK
LB FUEL
869. 81
1068.62
1068.62
1061.49
768.06
5.30
THC
IORVI
PPMV
2425.00
264T.OO
2536.00
2425.00
2202.00
2146.00
2146.00
19T9.00
1867.00
7870.00
2146.00
MASS EMI
NO
IB/ IK
LB FUEL
0.85
1.14
2.27
2.01
1.53
0.16
0.16
0.71
2.32
1.39
1.53
LTD CYCLE
CO
LB/IK
HOURS
4610.00
41355.53
41355.53
16771.47
4070.71
MEASURED CALCULATED
AIR FLOH F/A
LB/HR
87.00 0.05453
63.00 0.06875
182.00 0.07399
183.00 0.07344
183.00 0.07334
436.00 0.07891
436.00 0.07891
274.00 0.07295
279.00 0.07187
178.00 0.07429
66.00 0.
NO
IORYI
PPNV
30.00
51.00
109.00
96.00
73.00
B.OO
8.00
34.00
109.00
65.00
62.00
MASS EMI
NOX
L8/IK
LB FUEL
0.85
1.14
2.27
2.01
1.53
0.16
0.16
0.71
2.32
1.39
1.53
EMISSIONS
CO
EMISSION
LBS.
0.922
0.207
3.433
1.677
0.273
6.511
1.017
NU
2
IORYI
PP»V
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
5298.97
461C.OO
16006.27
15715.56
15737.71
41355.53
41355.53
20499.14
19292.84
16771.47
4070.71
HC
IB/ IK
LB FUEL
20.60
14.59
14.59
20.77
18.51
06204
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
KC
L8/KR
167.26
109.20
290.60
279.83
254.45
564.76
564.76
131.92-
117.38
328.19
98.10
HC
LB/IK
HOURS
109.20
564.76
564.76
328.19
98.10
ALDEHYDES
IORYI
9.00
7.00
-0.00
-0.00
-0.00
-0.00
6.00
5.00
4.00
4.00
6.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.022
0.003
0.047
0.033
0.007
0.111
0.017
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/Hit
13434.95
9280.34
24206.34
24692.66
24727.46
56314.95
56314.95
39970.77
41506.02
22900.91
10158.34
NO
LB/IK
LB FUEL
1.14
0.16
O.la
1.35
1.53
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS f.Hl MASS EMI
NO NO I
LB/HR LB/HR
5.93 3.93
6.03 6.03
35.82 35.82
31.77 31.77
24.19 24.19
6.04 6.04
6.04 6.04
16.35 16.35
53.14 33.14
21.32 21.32
8.13 8.13
MO NO
LB/IK EMISSION
HOURS LBS.
6.03 0.0012
6.04 0.0000
6.04 0.0003
21.32 0.0021
8.13 0.0003
0.0044
0.0007
1-43
-------
omi T/zem
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPIIERI LYCOMING
ENGINE DATA ********.**********
CAL 10 NUMBER I 261 ENGINE TYPE AND NODELI O-320-E2A SERIAL NUKSEA: L-291M-27AC
RATED HORSEPOKER: no.
ENGINE TOTAL TINE» 110. MRS
FUEL: AV GAS 80/87 FUEL H/C RATIOl l.»40
OPERATIONAL DATA »»»»«»»»«»»»«»
INLET AIR TEMPERATURE, DEGREES Fl START 8B.OO FINISH 88.00
ATMOSPHERIC PRESSURE! START 30.15 FINISH 30.19
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 49.00 PERCENT
SAMPLE L1NEI TEMPERATURE, DEGREES C: -0.00, FLOH RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIKE, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
7.00
(j837
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
L9/HR
IOLE-LO* 1 -0.0 1.00
IDLE/TAXI 2 -0.0 T.OO
RUN UP 3 -0.0 15.80
RUN UP-LEAN 4 -0.0 15.80
RUN UP-RICH 5 -0.0 15.80
TAKE-OFF 6 -0.0 38.70
CLIMB 7 -0.0 38. TO
DESCENT 8 -0.0 21.10
DESCENT ON 8 -0.0 24.60
APPROACH 9 -0.0 14.10
TAXI
TEST
MODE
1
2
3
4
5
6
7
8
a
9
10
TEST
MODE
1
2
3
4
5
6
7
8
a
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES f
-0.00
448.00
1043.00
1009.00
1065.00
1289.00
1289.00
1211.00
1188.00
94?. 00
448.00
HISS EMI
CO
LB/IK
LB FUEL
784.44
911.56
1007.12
999.35
1002.37
1070.03
1070.03
889.11
995.42
1073.78
736.98
TIME IN
NODE
M1N.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
'0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
23.66
20.76
19.45
16.62
16.96
15.64
15.64
15.41
16.84
22.91
19.24
MEASURED
FUEL FLOW
LB/HR
7.00
38.70
38.70
14.10
5.30
FUEL
-0.
CO
IDRYI
PEOCENT V
4.40
6.80
7.20
7.90
7.10
8.00
8.00
6.20
7.10
7.70
4.60
MASS EMI
N02
L9/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
1.40
0.19
3.21
1.41
0.36
6.571
,0
CO
2
(ORYI
PERCENT V
6.70
8.00
7.00
8.00
7.00
6.90
6.90
7.70
7.10
6.50
7.80
MASS EMI
C02
LB/IK
LB FUEL
1876.81
1685.02
1538.46
1574.16
1552.77
1450.08
1450.08
1734.98
1564.03
1424.22
1963.50
CO
LB/IK
LB FUEL
911.56
1070.03
1070.03
1073.78
736.98
5.30
THC
IDRY)
PPMV
2317.00
2704.00
2428.00
2317.00
2097.00
2042.00
2042.00
1876.00
2097.00
2869.00
2097.00
MASS EMI
NO
LB/IK
LB FUEL
0.79
1.03
2.25
1.65
1.55
0.18
0.18
0.80
1.54
I. 10
1.74
LTD CYCLE
CO
LB/IK
HOURS
6380.93
41409.97
41409.97
15140.36
3905.98
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
87.00 0.05272
83.00 0.06977
182.00 0.06718
183.00 0.07472
182.00 0.06655
435.00 0.07031
435.00 0.07031
253.00 0.06529
284.00 0.06699
157.00 0.06755
66.00 0.
NO
IDRYI
PPMV
27.00
47.00
98.00
80.00
67.00
8.00
8.00
34.00
67.00
48.00
66.00
MASS EMI
NOX
LB/IK
LB FUEL
0.79
1.03
2.25
1.65
1.55
0.18
o.ia
0.80
1.54
1.10
1.74
EMISSIONS
CO
EMISSION
LBS.
1.276
0.207
3.437
1.514
0.262
6.696
1.019
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/KR
5491.07
6380.93
15912.56
15631.69
15837.50
41409.97
41409.97
18760.25
24487.26
15140.36
3905.98
HC
L8/1K
LB FUEL
20.76
15.64
15.64
22.91
19.24
05838
NO
X
IORVI
PPNV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
165.61
145.32
307.33
262.57
267.90
605.36
605.36
325.11
414.21
323.09
101.98
HC
LB/IK
HOURS
145.32
605.36
605.36
323.09
101.98
ALDEHYDES
IORYI
8.00
7.00
-0.00
-0.00
-0.00
-0.00
8.00
5.00
4.00
4.00
5.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LAS.
0.029
0.003
0.050
0.032
0.007
0.121
0.018
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
13137.65
11795.14
24307.69
24871.78
24533.78
56118.02
56118.02
36607.98
38474.99
20081.54
10406.52
NO
LB/IK
LI FUEL
1.03
0.18
0.18
1.10
1.74
PARIICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
5.53 5.53
7.24 7.24
35.58 35.58
26.00 26.00
24.55 24.55
6.80 6.80
6.80 6.80
16.90 16.90
37.96 37.96
15.50 15.50
9.21 9.21
NO NO
L8/1K EMISSION
HOURS LBS.
7.24 0.0014
6.80 0.0000
6.80 0.0006
15.50 0.0016
9.21 0.0006
0.0042
0.0006
1-44
-------
OilEl 7/16/71
TEST ORGANIZATION! SCOTT/REN AVIATION
ENGINE SUPPLIERI LTCONING
ENGINE 0»r»
CAL ID NUNBERl 160 ENGINE TYPE AND NODEll O-120-E2D
RATED MOkSEPOVEII 150.
ENGINE TOTAL TIMEI 527. MRS
FUEL! AV GAS 10/87 Full M/C RATIO! 1.840
OPERATIONAL DATA «»«««»«»«»»«<
INLET All TEMPERATURE, DICREES Fl START BO.00 FINISH
ATMOSPHERIC PRESSURE! START 10.04 FINISH
INLET All HUMIDITY, CRN H20/LB Alll 0.01
RELATIVE HUMIDITY! 6B.OO PERCENT
SAMPLE LINE! TEMPEIATUIE, DEGREES Cl -0.00, FLOW RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS! 11
COMMENTS!
SERIAL NUMBER! 1-2JMV1TAA
10.00
30.04
9839
CARB. TEST ENGINE MEASURED
HEATER NODE RPN FUEL FLOH
IB/Hit
IDLE-LOU l .Q.o 5.60
IDLE/TAXI 2 -0.0 8.10
RUN UP 3 -0.0 26.40
RUN UP-LEAN * -0.0 29.70
RUN UP-RICH 5 -0.0 24.60
TAKE-OFF 6 -0.0 51.50
CL1NB 7 -0.0 51.50
DESCENT 8 -0.0 15.50
DESCENT ON B -0.0 15.50
APPROACH 9 -0.0 14.10
TA»I
TEST
NODE
1
2
)
4
5
6
7
a
a
<)
10
TEST
NODE
,
2
3
4
5
6
7
a
8
i
10
TEST
NODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TF.NP
DEGREES F
560.00
560.00
1009.00
953.00
1043.00
1114.00
1314.00
1256.00
1222.00
964.00
650.00
NASS EMI
CO
LB/U
LB FUEL
744.28
738.96
B24.25
798.74
794.68
962.92
927.55
707.11
924.20
802.80
401. B5
TIME IN
MODE
BIN.
12.00
O.l'O
5.00
6.00
4.00
FOP. CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PS1A
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS ("I
HC
LB/IK
LB FUEL
31.05
23.24
18.07
17.56
15.15
17.19
16.66
16.74
19.79
19.27
16. 29
MEASURED
FUEL FLOM
IB/HO
8.10
51.50
51.50
14.10
6.40
FUEL
-0
CD
(DRY)
PERCENT V
5.30
5.50
6.30
5.50
5.90
7.50
7.50
5.40
7.30
5.90
2.10
MASS EMI
N02
LB/U
LB FUEL
0.0
0.0
1.0
0.0
0.0
0.0
0.0
0.0
0.0
1.0
0.0
FUEL
USED
LBS.
1.62
0.26
4.27
1.41
0.43
7.991
0
CO
2
(DRY)
PERCENT V
8.70
8.30
8.90
8.20
8.90
8.00
8.60
9.80
8.10
8.70
9.10
NASS ENI
C02
LB/U
LB FUEL
1919.64
1870. Tl
1829.57
1871.08
1883.51
1613.83
1671.14
2016.93
1659. 98
1860.00
2498.15
CO
LR/IK
LB FUEL
788.96
962.92
927.55
802.80
401.85
6.40
THC
IDRVI
PPNV
I860. 00
2835.00
2412.00
2111.00
1990.00
2352.00
2352.00
2232.00
2714.00
2473.00
1628.00
NASS EMI
Nn
LB/IK
LB FUEL
0.67
I.U6
5.76
3.86
3.61
1.65
3.51
10.00
5.60
3.64
2.44
LTO CYCLE
CO
LB/IK
HOURS
6390.56
49590.45
47768.96
11119.45
2571.85
MEASURED CALCULATED
All FLOM F/A
LB/HR
69.00 0.06616
100.00 0.06508
120.00 0.07119
294.00 0.06432
106.00 0.06914
611.00 0.072B7
-0.00 0.07545
451.00 0.07080
420.00 0.07140
174.00 0.06B50
88.00 0.
NO
IORYI
PPNV
29.00
45.00
268.00
162.00
161.00
173.00
173.00
465.00
268.00
163.00
85.00
MASS EMI
NOX
LB/U
LB FUEL
0.67
1.06
5.76
.86
.61
.65
.51
1 .00
.60
.64
.44
EMISSIONS
CO
EMISSION
LBS.
1.278
0.248
3.965
1.132
0.172
6.745
O.(50
NO
2
IDKYI
PPMV
-0,00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
MASS ENI
CO
IB/MR
4167.98
6190.56
21760.11
18930.02
14544.07
49590.45
47768.96
25110.15
12986.62
11114.45
2571. B5
HC
IB/IK
LB FUEL
23.29
17.29
16.66
19.27
16.29
05118
NO
X
IDRVI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS EMI
HC
LB/HR
171.85
188.66
477.14
416.12
377.64
390.67
857.96
594.42
702. IB
271.73
104.26
HC
LB/U
HOURS
188.66
890.67
857.96
271.73
104.26
ALDEHYDES
IORYI
14.00
9.00
-0.00
-0.00
-0.00
-0.00
9.00
2.00
4.00
7.00
9.00
MASS EMI
N02
LB/HR
0.0
O.U
0.0
0.0
0.0
0.0
0.0
0.0
0.0
o.o
0.0
HC
EMISSION
LOS.
0.03B
0.004
0.071
0.027
0.007
0.148
0.018
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS ENI
C02
LB/HR
10749.96
15152.79
48300.66
44344.59
46334.32
81112.19
86061.94
71601.13
58929.30
26225.92
15988.15
NO
LB/IK
LB FUEL
1.06
3.65
3.51
3.64
2.44
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI NASS EMI
NO NOX
LB/HR LB/HR
3.75 3.75
8.59 8.59
152.05 152.05
91.58 91.58
88.71 at. 71
187.89 167.69
180.99 180.94
355.16 355.16
198.92 198.42
51.37 51.37
15.61 15.61
NO NO
LB/IK EMISSION
HOURS LBS.
a. 54 0.0017
187.89 0.0009
180.94 0.0150
51.17 0.0051
15.61 0.0010
0.0219
0.0030
1-45
-------
OATtl T/16/T1
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LTCONING
ENGINE DATA
C»L ID NUMBER! 161 ENGINE TYPE AND MODEL! 0-320-E2D
RATED HORSEPOWER! 190.
ENGINE TOTAL TINE! 327. MRS
FUEL! AV GAS 90/17 FUEL H/C RATIO! 1.8*0
OPERATIONAL DATA «»«««»«»«««««»«««
INLET AIR TEMPERATURE. DECREES Fl START 85.50 FINISH 69.10
ATMOSPHERIC PRESSURE! START 30.10 FINISH 10.10
INLET AIR HUMIDITY, CRN H2D/LB AIR! 0.02
RELATIVE HUMIDITY! 58.OC PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES Cl -0.00, FLOW RATE, LITERS/NIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER! L-2J499-2TA9
9841
CARB. TEST ENGINE MEASURED
HEATER NODE RPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 ».70
IDLE/TAXI 2 -0.0 6.40
RUN UP 3 -0.0 24.60
RUN UP-LEAN * -0.0 22.00
RUN UP-RICH 5 -0.0 22.00
TAKE-OFF 6 -0.0 93.90
CLIMB 7 -0.0 53.50
DESCENT e -0.0 39.20
DESCENT ON 8 -0.0 34.60
APPROACH 9 -0.0 15. BO
TAXI
TEST
MODE
1
2
3
4
5
6
7
K
8
1
10
TEST
MODE
I
2
1
4
5
6
7
8
8
1
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES f
916.00
560. 00
998.00
942.00
1054.00
-0.00
-0.00
1199.00
1143.00
930.00
605.00
MASS EMI
CO
LB/IK
L8 FUFL
315.68
515.76
797.62
759.79
d07.05
535.40
515.40
710.90
963.14
779.80
393.91
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
50. 99
20.25
18.74
14.76
16.41
10.79
10.79
15.57
19. 13
18.18
19.23
MEASURED
FUEL FLO*
LB/HR
6.40
53.50
53.50
15.80
4.70
FUEL
-0
CO
(DRY)
PERCENT V
1.70
.30
.10
.60
.20
.20
.20
3.60
8.00
6.00
2.30
MASS EMI
NCI2
LH/IK
L8 FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
1.2B
0.27
4.44
1.56
0.31
7.883
0
CO
2
IORYI
PERCENT V
8.70
9.40
9.10
9.10
9.10
11.50
11.50
10.10
8.50
9.30
9.30
MASS EMI
C02
LB/IK
LB FUEL
2538.34
2308.33
1869.5H
1939.93
1861.17
2303.40
2303.40
2014.56
1607. 89
1899.12
2502.58
CO
LB/IK
LB FUEL
515.76
535.40
535.40
779.80
393.91
4.70
THC
IDRYI
PPMV
4795.00
2262.00
2503.00
1900.00
2201.00
1478.00
1478.00
2141.00
2804.00
2443.00
1960.00
MASS EHI
NO
LB/IK
LB FUEL
1.40
1.80
6.01
3.19
3.42
20.33
20.33
9.97
i.OO
3.59
2.19
LTD CYCLE
CO
LB/IK
HOURS
3300.84
28644.13
28644.13
12320.80
1851.37
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
65.00 0.05011
86.00 0.05939
305.00 0.07116
276.00 0.06857
272.00 0.07149
720.00 0.07218
720.00 0.07218
500.00 0.07296
404.00 0.07755
197.00 0.07153
65.00 0.
NO
IORV)
PPMV
46.00
70.00
280.00
143.00
160.00
971.00
971.00
478.00
253.00
168.00
78.00
MASS EHI
NOX
LB/IK
Lfl FUEL
1.40
1.80
6.01
3.19
3.42
20.33
20.33
9.97
5.00
3.59
2.19
EMISSIONS
CO
EMISSION
LRS.
0.660
0.143
2.377
1.232
0.124
4.537
0.576
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
1483.68
3300.84
19621.38
16715.44
17755. C4
28644.13
28644.13
27867.23
33324.64
12320.80
1851.37
MC
L9/1K
LB FUEL
20.25
10.79
10.79
18.18
19.23
09420
NO
X
IORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
HC
LB/HR
239.68
129.58
461.11
324.81
360.99
577.31
577.31
610.19
668.96
787.31
"0.36
HC
LB/IK
HOURS
129.58
577.31
577.31
287.31
90.36
ALDEHYDES SMOKE
IDRYI
21.00
13.00
-0.00
-0.00
-0.00
-0.00
7.00
7.00
5.00
7.00
9.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
o.n
o.n
HC
EMISSION
LBS.
0.026
0.003
0.048
0.029
0.006
0.112
0.014
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HH
11930.21
14773.27
45991.67
42678.54
40945.83
123231.75
123231.75
78970.63
55633. 01
30006.05
11762.13
NO
LB/IK
Lfl FUEL
l.BO
20.33
20.33
3.59
2.19
P1RTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.oo
-o.oo
-o.oo
-0.00
-0.00
MASS EMI MASS EMI
Nn NOX
LB/HR LB/HR
6.59 6.59
11.50 11.50
147.94 147.94
70.11 70.11
75.20 75.26
1087.74 1087.74
1087.74 1087.74
39C.71 390.71
171.11 173.11
56.67 56.67
10.31 10.31
NO NO
LB/IK EMISSION
HOURS LBS.
11.50 0.0023
1087.74 0.0054
1087.74 0.0903
56.67 0.0057
10.31 0.0007
0.1044
0.0132
1-46
-------
OAfEl 7/16/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! IVCONING
ENGINE DATA o«»»«««««««»«.»»»«««»«««.»»»«««»«»
CAL 10 NUMBER! 162 ENGINE TYPE AND NODELI O-120-E2D SERIAL NUMBER! l-M«»»-2TAC
RATED HORSEPOWER! 190.
ENGINE TOTAL TINEl »2TJ. MRS
FUEL! AV GAS *0/IT FUEL H/C RATIOl 1.140
OPERATIONAL DATA «»»««««»»«»*«««
INLET AIR TEMPERATURE, DEGREES Fl START 61.00 FINISH 14.00
ATMOSPHERIC PRESSUREl START JC.IO FINISH 10.10
INIEI AIR HUMIDITY. CAN H20/LB AIR) 0.01
RELATIVE HUKIOITYl 41.00 PERCENT
SAMPLE LINES TEMPERATURE. DEGREES Cl -0.00. FLO* RATE. LITERS/MINI T.OO
SAMPLE LINE TRANSPORT TINE. SECt 1.60
NUMBER OF TESTS! II
COMMENTS!
,'843
CARB. TEST ENGINE MEASURED
HEATER NODE RPN FUEL FLOW
LB/HR
IOLE-LO* | -0.0 6.40
IDLE/TAXI 2 -0.0 B.90
RUN UP 3 -0.0 26.40
RUN UP-LFAN 4 -0.0 26.40
RUN UP-RICH 5 -0.0 26.40
TAKE-OFF 6 -0.0 66.30
CLIMB 7 -0.0 68.10
DESCENT B -0.0 32. BO
DESCENT ON B -0.0 35.50
APPROtCH 9 -0.0 IS. 00
TAXI
TEST
MODE
1
2
a
9
10
TEST
MODE
1
2
10
TES1
MODE
2
6
7
-------
D«TEl 7/16/Tl
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOMING
ENGINE DATA
CAL ID NUMBER! ITS ENGINE TYPE AND MODEL! O-320-E2D
RATED HORSEPOKERl ISO.
ENGINE TOTAL TINE! 426. MRS
FUEL! AV GAS 80/87 FUEL H/C RATIOl 1.8*0
OPERATIONAL DATA »«««««»»««»»««»««
INLET AIR TEMPERATUREf DEGREES Fl START 82.00 FINISH 62.50
ATMOSPHERIC PRESSURE: START 30.17 FINISH 30.17
INLET AIR HUMIDITY, CRN H20/LS AIR! 0.02
RELATIVE HUMIDITY: 73.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/HIM: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS! 11
COMMENTS:
SERIAL NUHBERl L-26214-27AA
9845
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOU 1 -0.0 6.40
IDLE/TAXI 2 -0.0 12.40
RUN UP 3 -0.0 26.40
RUN UP-LEAN 4 -0.0 26.40
RUN UP-RICH 5 -0.0 26.40
TAKE-OFF 6 -0.0 6"). 30
CLIMB 7 -0.0 61.30
DESCENT B -0.0 37.40
DESCENT ON 8 -0.0 40.10
APPROACH 9 -0.0 17.60
TAXI
TFST
MOOE
1
2
3
4
5
6
7
8
a
9
10
IESI
MODE
I
2
3
4
5
6
1
fl
0
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
FXHAUST
GAS
TFMP
DEGREES F
460.00
437.00
no 7. oo
740.00
863.00
1368.00
1368.00
1166.00
1166.00
B07.00
516.00
MASS EMI
CO
LB/1K
LB FUFL
943.75
1184.59
805.77
808.15
830.62
1073.41
1073.41
675.60
756.35
863.36
974.85
TIMF IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
47.19
73.08
15.06
16.45
13.79
11.63
1 1.63
10.58
11.21
15.40
?4.89
MEASURED
FUEL FLOW
LB/HR
12.40
69.30
69.30
17.60
8.10
FUEL
-0.
CO
(DRY)
PERCENT V
7.50
8.70
5.90
5.60
6.20
9.50
9.50
5.40
6.20
6.80
7.20
MASS EMI
HO 2
LB/1K
LB FUEL
3.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
L3S.
2.48
0.15
5.75
1.76
0.54
10.881
,0
co
2
IORVI
PERCENT
7.90
5.20
8.70
B.20
8.70
8.20
8.20
10.60
10.20
8.90
7.40
MASS EMI
CC12
LB/1K
LB FUEL
1561.93
1112.48
1666.87
1859.33
1831.33
1455.77
1455.77
2083.71
1955.09
1775.46
1574.25
cn
LB/IK
LB FUEL
1184.59
1073.41
1073.41
863.36
974.85
8.10
THC
(ORYI
PPMV
V
6548.00
1372.00
1126.00
1990.00
1797.00
1797.00
1797.00
1476.00
1605.00
2118.00
3210.00
MASS EMI
NO
LB/IK
LB FUEL
0.?5
0.13
5.20
2.84
2.86
1.09
1.09
12.08
12.68
3.48
0.82
LTD CYCLE
CO
LB/IK
HOURS
14688.95
74387.13
74367.13
15195.11
7896.26
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
73.00 0.07436
124.00 0.06961
328.00 0.06925
327.00 0.06472
325.00 0.06958
785.00 0.08279
785.00 0.08279
484.00 0.07387
507.00 0.07591
214.00 0.07337
94.00 0.
NO
(DRY I
PPMV
12.00
6.00
232.00
120.00
130.00
59.00
59.00
5B8.no
633.00
167.00
37.00
MASS EM]
NOX
LB/IK
LB FUEL
0.25
0.13
5.20
2.84
2.86
1.09
1.09
12.08
12.60
3.48
O.B2
EMISSIONS
CO
E-MSSION
LBS.
2.938
0.372
6.174
1.520
0.529
11.532
1.060
NO
2
IORYI
PPCV
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
6040.01
14688.95
21272.23
21335.19
21928.27
74387.13
74387.13
25267.30
30329.43
15195.11
7896.26
HC
La/ IK
L3 FUEL
73.08
11.* 3
11.63
15.40
24.89
06928
NO
X
IDRYI
PPHV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
HC
Lfl/HR
302.02
906.25
397.71
434.22
364.00
805.88
805.88
395.55
449.67
271.06
201.62
HC
LB/IK
HOURS
906.25
805.88
805.88
271.06
201.62
ALDEHYDES SMOKE
IORYI
34.00
28.00
-0.00
-0.00
-0.00
-0.00
9.00
10.00
12.00
18.00
15.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
o.iai
0.004
0.067
0.027
0.014
0.293
0.027
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
9996.36
13794.73
49285.43
49086.36
48347.09
100884.94
100884.94
77930.81
78399.06
31248.06
12751.43
N(l
LB/IK
LB FUEL
C.13
1.09
1.09
3.48
0.82
PARTICULATES
-0.00
-0.00
-0.00
-n.oo
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EKI MASS EMI
NO NOX
LR/hR LB/HR
1.59 1.59
1.66 1.66
137.39 137.39
75.09 75.09
75.52 75.52
75.88 75.88
75.88 75.88
451.92 441.92
508.62 508.62
61.30 61.30
6.67 6.67
NO NO
Lfl/lK EMISSION
HOURS LBS.
1.66 0.0003
75. BR 0.0004
75.88 C.0063
61.30 0.0061
6.67 0.0004
0.0136
0.0012
1-48
-------
OATEl 7/16/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER: LYCOMING
ENGINE DATA »«««»«»»»»««»»««
C»L 10 NUMBER! 176 ENGINE TYPE »ND MOOELl 0-320-E20 SERIAL NUMBER) L-262I4-27AB
RATED HORSEPOKER: 190.
ENGINE TOTAL TINE) 426. MRS
FUEL I AV GAS 60/«7 FUEL H/C RATIO! 1.6*0
OPERATIONAL DATA «»««««»*»*»*
INLET AIR TEMPERATURE. DEGREES Ft START 81.50 FINISH 61.00
ATMOSPHERIC PRESSURE! START 30.16 FINISH 30.16
INLET AIR HUMIDITY, CRN H20/LB AIRl 0.02
RELATIVE HUMIDITY! 72.00 PERCENT
SAMPLE LINE! TEMPERATURE. DEGREES C" -0.00, FLON RATE, LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTSl 11
COMMENTS:
9847
CARS. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOK
LB/HR
IDLE-LOW 1 -0.0 $.60
IDLE/TAXI 2 -0.0 8.90
HUH UP 3 -0.0 26.40
RUN UP-LEAN 4 -0.0 26.40
RUN UP-RICH 5 -0.0 26.40
TAKE-OFF 6 -0.0 67.30
CLIMB 7 -0.0 67.30
DESCENT 8 -0.0 38.30
DESCENT ON 8 -0.0 39.20
APPROACH 9 -0.0 17.60
Tail
TEST
MODE
1
2
1
4
5
&
7
a
a
9
10
TEST
MODE
t
2
3
4
5
6
7
a
8
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
348.00
415.00
818.00
717.00
863.00
1368.00
1168.00
1166.00
1155.0(1
785.00
516.00
MASS EMI
CO
L6/1K
L? FUEL
518.66
98?. 19
6*0.85
nil. 47
834.27
1084.92
1084.92
671.61
766.43
871.90
827.74
TIME IN
MODE
KIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYC.LE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-o.no
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
25.86
23.73
20.20
20.83
19.41
16.81
16.81
17.61
17.18
18.79
20.92
MEASURED
FUEL FLOW
LB/HR
8.90
67.110
67. 10
17.60
7. 20
FUEL
-0,
cn
(DRY)
PERCENT V
3.60
7.00
6.10
5.70
6.30
9.70
9.70
5.30
6.20
6.80
5. BO
MASS EMI
NO 2
IB/ IK
LH FUEL
0.0
n.o
o.n
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
1.76
0.34
5.59
1.76
0.48
9.945
.0
CO
2
(DRY)
PERCENT V
9.60
7.10
8.30
7.90
8.70
a. 10
8.10
10.40
9.90
8.70
8.10
MASS EMI
CO 2
LB/1K
LB FUEL
2256.94
1565.60
1797.65
1810.67
1810.18
1423.47
1423.47
20T0.6T
1922.86
1752.73
1816.30
CO
LB/1K
LB FUEL
982.39
1064.92
1084.92
871.90
627.74
7.20
THC
(DRY)
PPMV
3018. On
2952.00
2559.00
2493.00
2559.00
2624.00
2624.00
2427.00
2427.00
2559.00
2559.00
MASS ENI
NO
LB/1K
LB FUEL
0.71
0.58
4.91
2.47
2.50
1.10
1.10
9.39
10.05
2.49
0.87
LTO CYCLE
CO
LB/1K
HOURS
8743.23
73015.13
73015.13
15345.46
59S9.7C
MEASURED CALCULATED
AIR FLOK F/A .
LB/HR
74.00 0.06199
103.00 0.06692
322.00 0.06774
322.00 0.06412
323.00 0.07040
754. OC 0. 08368
754.00 0.08368
491.00 0.07299
491.00 0.07501
212.00 0.07272
89.00 0.
NO
-------
OJTEl T/I6/T1
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: LYCOMING
ENGINE DATA
CAL ID NUMBERi ITT ENGINE TYPE AND NODELI 0-320-E2D
RATED HORSEPOHER: ISO.
ENGINE TOTAL TINEl 427. MRS
FUEL: AV GAS 80/87 FUEL H/C RATIO: 1.8*0
OPERATinNAL DATA ««««»«».».«»«»«»«»«»»«.«.»«»
INLET AIR TEMPERATURE, DEGREES Fl START 85.00 FINISH 85.SO
ATMOSPHERIC PRESSURE: START 30.16 FINISH 30.15
INLET AIR HUMIDITY, CRN HZO/LB AIR: 0.02
RELATIVE HUMIDITY: 66.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOH RATE, LITERS/KIN: T.OO
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER! L-2628A-2TAC
9849
CARB. TEST ENGINE MEASURED
HEATER MUDE RPM FUEL FLOH
LB/HR
IOLE-LOU 1 -0.0 5.60
IDLF/TAXI 2 -0.0 8.90
RUN UP 3 -0.0 27.30
RUN UP-LEAN 4 -0.0 25.50
RUN UP-RICH 5 -0.0 26.40
TAKE-OFF 6 -0.0 69.30
CLIMB 7 -0.0 69.30
DESCENT 8 -0.0 36.40
DESCENT ON 8 -0.0 39.20
APPROACH 9 -0.0 17.60
TAXI
TEST
MODE
1
2
3
4
5
6
7
a
a
9
10
TFSI
MODI:
1
2
3
4
b
6
7
d
t)
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
260.00
359.00
740.00
673.00
785.00
1323.00
1323.00
1110.00
1121.00
751.00
493.00
MASS FMI
CO
LB/iK
LB FUEL
6 1 4 . 09
1035.75
844.56
863.82
845.83
1117.75
1117.75
710. 39
802.09
892.08
864.00
TIME IN
10DE
HIM.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FH!
HC
LB/IK
LB FUEL
27.88
26. 76
18.00
20.02
18.63
17.55
17.55
IS. 59
15. 78
18.42
21.35
MEASURED
FUEL FLOW
LB/HR
8.90
69.30
69.30
17.60
8.10
FUEL
-0,
CD
(DRY)
PERCENT V
3.80
7.40
6.20
5.70
6.00
10.00
10.00
5.60
6.40
7.00
6.10
MASS FMI
HOi
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
1.76
0.35
5.75
1.76
0.54
10.181
.0
CO
2
IDRY)
PERCENT V
8. 40
6.70
B. 40
7.40
a. 10
7.80
7.60
10.10
9.50
a. 60
7.90
MASS EMI
C02
LB/IK
LB FUEL
21)2.89
1473.45
1797.87
1762.05
1794.15
1369.87
1369.87
2014.52
ia?o.70
1722.04
1758.13
CO
LB/IK
LB FUEL
1035.75
1117.75
1117.75
892.08
664.00
a. 10
THC
(DRY)
PPJtV
3012.00
3338.00
2307.00
2307.00
2307.00
2741.00
2741.00
2144.00
2198.00
2524.00
2632.00
MASS EMI
NO
LB/IK
LB FUEL
0.64
0.39
4.45
2.49
2.55
1.08
i.oa
9.26
9.63
2.76
o. ei
LTD CYCLE
CO
LB/IK
HOURS
9218.13
77460.06
77460.06
15700.64
6998.41
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
72.00 0.05771
100.00 0.06723
332.00 0.06852
310.00 0.06186
323.00 0.06630
768.00 0.08386
768.00 0.08386
468.00 0.07296
486.00 0.07412
211.00 0.07320
9B.OO 0.
NO
IORYI
PPMV
24.00
17.00
199.00
100.00
110.00
59.00
59.00
444.00
468.00
132.00
35.00
MASS EMI
NOX
LB/IK
LB FUEL
0.64
0.39
4.45
2.49
?.55
l.OB
i.oe
9.26
9.63
2.76
0.81
EMISSIONS
CO
EMISSION
LBS.
1.844
0.387
6.429
1.570
0.469
10.699
1.051
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
MASS EMI
CD
LB/HR
3438.91
9218.13
23056.55
22027.43
22330.03
77460.06
77460.06
25876.22
31441.85
1570C.64
6998.41
MC
LB/IK
LB FUEL
26.76
17.55
17.55
IB. 42
21.35
06605
NO
X
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
156.11
238.15
491.35
510.60
491.73
1216.00
1216.00
567.39
616.45
324.23
172.94
HC
L3/1K
HOURS
238.15
1216.00
1216.00
324.23
172.94
ALDEHYDES
IORY)
19.00
15.00
-0.00
-0.00
-0.00
-0.00
11.00
9.00
11.00
12.00
18.00
MASS EMI
N02
LB/HK
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
MC
EMISSION
LBS.
0.048
0.006
0.101
0.032
0.012
0.199
0.020
SMOKE
-o.no
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI
en 2
LB/HR
11944.16
13113.66
49081.77
44932.34
47365.41
94931.56
94931.56
73328.44
73331.38
30307.91
14240.82
NO
LB/IK
LB FUEL
0.39
1.01
1.03
2.76
0.81
PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EKI MASS EMI
NO NOX
LB/HR LD/HR
3.57 3.57
3.48 3.48
121.56 121.56
63.48 63.48
67.24 67.24
75.07 75.07
75.07 75.07
336.99 336.99
377.65 377.65
48.63 48.63
6.60 6.60
NU NO
LB/IK EMISSION
HOURS LBS.
3.48 0.0007
75.07 0.0004
75.07 C.0062
48.63 0.0049
6.6C 0.0004
0.0126
0.0012
1-50
-------
OATE1 7/28/71
TEST ORGANIZATIONI SCOTT/CEN AVIATION
ENC1NE SUPPLIERI LYCOMINC
ENGINE DATA
C»L 10 NUNRERl 2)1 ENGINE TYPE »NO MODEL: 0-320-E3D
RATED HORSEPOMER: 130.
ENGINE TOTAL TINEl »4. MRS
FUELl »V GAS 10/87 FUEL H/C RATIO: 1.840
OPERATIONAL OAT* ««»»«»«««««»«»«««««
INLET AIR TENPERATURE, DEGREES F: START 79.00 FINISH 79.00
ATMOSPHERIC PRESSURE! START 29.70 FINISH 29.70
INLET AIR HUMIDITY, GRN H20/L8 AIRl 0.01
RELATIVE HUNIOITVi 42.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES Cl -0.00, FLOM RATE, LITERS/MINI T.OO
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBERl L-29465-27AA
J857
CARB. TEST ENGINE MEASURED
HEATER MODE RPN FUEL FLOW
LB/HR
IOLF-LOM 1 -0.0 IS. 20
IDLE/TAXI 2 -0.0 18.80
RUN UP ) -0.0 34.00
RUN UP-LEAN 4 -0.0 11.60
RUN UP-RICH 5 -0.0 31.60
TAKE-OFF 6 -0.0 75.00
CLIMB T -0.0 75.00
DESCENT 8 -0.0 41.00
DESCENT ON 8 -0.0 38.70
APPROACH 9 -0.0 27.80
TAXI
TESI
MODE
1
2
3
4
5
6
7
a
0
i
10
TEST
MODE
1
2
T
4
5
6
7
8
n
9
10
TESI
NODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
314.00
426.00
953.00
874.00
IC09.00
1256.00
1256.00
1143.00
1177.00
89(1.00
437.00
MASS FNI
CO
LB/1K
LB FUEL
1116.58
1229.96
1138.21
lion. 9i
1115.22
1202.97
1202.97
1034.02
692.54
1170.57
984.35
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CVCLF
FOR CYCLE/IB
10
EXHAUST
GAS
PRESSURE
PSI1
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LR FUEL
75.99
43.28
17. £9
17.19
17.69
12.97
12.97
12.54
10.40
26.91
18. en
MEASURED
FUEL FIOH
IB/KB
18.80
75.00
75.00
27.80
18.80
FUEL
-0.
CO
IDRYI
PERCENT V
4.20
7.40
9.90
9.70
9.70
10.90
10.90
8.90
5.50
10.50
5.30
MASS EMI
NU2
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
3.76
0.37
6.22
2.78
1.26
14.400
,0
CO
2
(DRV)
PERCENT V
2.90
4.30
7.40
7.70
7.60
7.20
7.20
8.30
10.40
7.20
5.40
MASS EMI
CO 2
LB/IK
L8 FUEL
1211. 37
1122.96
1336.77
1383.10
1372.90
1248.53
1248.53
1515.15
2057.57
1261.18
1575.81
CO
LB/IK
LB FUEL
1229.96
1Z02.97
1202.97
1170. 57
984.35
18.80
THC
IDRYI
PPHV
4991.00
4547.00
2717.00
2717.00
2717.00
2052.00
2052.00
1885.00
1442.00
4215.00
1775.00
MASS EMI
NO
LB/IK
LB FUEL
0.13
0.16
1.25
0.86
0.87
0.74
0.74
1.15
9.97
0.81
0.64
LTD CYCLE
CO
LB/IK
HOURS
23123.14
90222.44
90222.44
32541.79
18505.72
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
158.00 0.03596
192.00 0.05723
372.00 0.08167
351.00 0.08202
349. OC 0.08159
802.00 0.08519
802.00 0.08519
470.00 0.08046
494.00 0.07346
290.00 0.08432
216.00 0.
NO
IORYI
PPMV
3.00
6.00
66.00
46.00
46.00
41.00
41.00
60.00
482.00
44.00
21.00
MASS FMI
N0«
LB/IK
LB FUEL
0.13
0.16
1.25
0.86
0.87
0.74
0.74
1.15
9.97
0.81
0.64
EMISSIONS
CO
EMISSION
LBS.
4.625
0.451
7.488
3.254
1.240
17.058
1.185
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/KR
16971.97
23123.14.
38699.22
35041.46
35240.89
90222.44
90222.44
42394.89
26801.39
32541.79
18505.72
HC
LB/IK
LB FUEL
43.28
12.97
12.97
26.91
18.88
05092
NO
X
IORVI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
1155.09
813.74
6C8.28
562.14
565.34
972.77
972.77
514.26
402.44
748.16
354.96
HC
LB/IK
HOURS
813.74
972.77
972.77
748.16
354.96
ALDEHYDES
IORY)
9.00
10.00
-0.00
-0.00
-0.00
-0.00
7.00
7.00
3.00
8.00
6.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.163
0.005
0.081
0.075
0.074
0.347
0.024
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
C02
LB/HR
18412.78
21111.62
45450.32
43705.81
43383.68
93639.56
93639.56
62121.20
79628.06
35060.89
29625.27
NO
LB/IK
LB FUEL
0.16
0.74
0.74
0.81
0.64
PARFICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI MASS EMI
NO NOX
IP/KB LB/HR
1.99 1.99
3.08 3.08
42.38 42.38
27.30 27.30
27.45 27.45
55.74 55.74
55.74 55.74
46.95 46.95
385.80 385.80
22.40 22.40
12.04 12.04
NO NO
LB/IK EMISSION
HOURS LBS.
3.08 0.0006
55.74 0.000]
55.74 0.0046
22.40 0.0022
12.04 0.0008
0.0086
0.0006
1-51
-------
0«TEl 7/28/71
TEST ORGANIZATION: SCOTT/GFN AVIATION
ENGINE SUPPLIER I LYCOMING
ENGINE 0»TA
CAL 10 NUMBER: 239
ENGINE TYPE AND MODEL: O-320-E3D
RATED HORSEPONERI 150.
55. MRS
FUEl H/C RATIO: 1.840
SERIAL NUNBERl L-29465-27AB
FINISH
FINISH
82.00
29.70
ENGINE TOTAL TIME:
FUEL: AV GAS 80/87
OPERATIONAL DATA ««»»»«»»«
INLET AIR TEMPERATURE, DEGREES F: START 82.00
ATMOSPHERIC PRESSURE: START 29.70
INLET AIR HUMIDITY, GRN H20/LB AIR: 0.01
RELATIVE HUMIDITY! 41.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOK RATE, LITERS/M1N:
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
9859
CARB. TEST ENGINE MEASURED
HEATER MODE RPN FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 15.20
IDLE/TAXI 2 -o.o la.eo
RUN UP 3 -0.0 32.80
RUN UP-LEAN « -0.0 32.80
RUN UP-RICH 5 -0.0 31.60
TAKE-OFF 6 -0.0 72. 7P
CLMS 7 -0.0 72.70
DESCENT a -0.0 43.40
DESCENT ON 8 -0.0 39.80
APPROACH 9 -0.0 23.40
T»XI
TEST
MODE
1
2
)
4
5
6
7
fl
a
9
10
TEST
MODE
1
2
J
4
5
6
7
a
a
t
10
TEST
MOOF
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
269.00
381.00
953.00
886.00
1009.00
1278.00
1278.00
1155.00
1177.00
897.00
415.00
MASS EMI
CO
LB/1K
LB FUEl
88*. 70
1034.47
1135.70
1 110.97
1112.98
1179.45
1179.45
1010.51
708.70
1177.31
964.69
TIMF IN
MODE
HIN.
12.00
0.30
5.00
A. 00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
27.96
23. in
18.77
22.21
18.77
12.44
12.44
12.80
10. 5/
26.80
18. 80
MEASURED
FUEL FLOM
LB/HR
18.80
72.70
72.70
23.40
17.60
FUEL
-0
CO
I DRY!
PERCENT V
3.10
5.80
10.00
9.70
9.80
10.60
10.80
8.70
5.70
10.50
5.00
MASS EMI
N02
IB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
IBS.
3.76
0.36
6.03
2.34
1.18
13.677
0
CO
2
IDRV)
PERCENT V
3.80
5.30
7.50
7.60
7.70
7.50
7.50
a. 50
10.40
7.10
5.30
MASS EMI
CD2
LB/IK
LB FUEL
1705.88
1485.27
1318.33
1367.67
1374.01
1286.93
1286.93
1551.23
2031.70
1250.85
1606.69
CO
LB/IK
LB FUEL
1034.47
1179.45
1179.45
1177.33
964.69
17.60
THC
IDRV)
PPMV
1709.00
2269.00
2885.00
3389.00
2885.00
1989.00
1989.00
1933.00
1485.00
4174.00
1709.00
MASS EMI
NO
LR/1K
LB FUEL
0.42
0.47
.32
.05
.03
.22
.22
.49
10.37
0.88
0.70
LTD CYCLE
CO
LB/IK
HOURS
19448.06
85745.94
85745.94
27549.56
16978.53
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
181.00 0.03331
212.00 0.05306
360.00 0.08264
362.00 0.08190
350.00 0.03256
785.00 0.08597
785.00 O.C8597
500.00 0.08041
508.00 0.07440
252.00 0.08387
204.00 0.
NO
(DRY)
PPMV
9.00
16.00
71.00
56.00
55.00
68.00
68.00
78.00
508.00
48.00
22.00
MASS EMI
NOX
LB/IK
LB FUEL
0.42
0.47
.32
.05
.03
.22
.22
.49
10.37
0.88
0.70
EMISSIONS
CO
EMISSION
LBS.
1.890
0.429
7.117
2.755
I.13S
15.328
1.121
NO
2
IORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
13462.71
19448.06
37250.84
36439.79
3517C.25
65745.94
85745.94
43855.97
28206.31
27549.56
16978.53
HC
LB/IK
LB FUFl
23. IB
12.44
12.44
26.80
18.88
04003
K3
X
(DRY!
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
425.07
435.74
615.50
729.16
592.98
904.42
904.42
55B.07
420.87
627.22
332.37
HC
LB/IK
HOURS
435.74
904.42
904.42
627.22
332.37
ALDEHYDES
IORY)
7.00
8.00
-0.00
-0.00
-0.00
-0.00
11.00
7.00
6.00
9.00
8.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.087
0.005
0.075
0.063
0.022
0.252
0.018
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EXI
CO 2
L9/HR
25929.39
27923.02
43897.08
44859.62
43418.84
93559.81
93559. HI
67321.44
80861.69
29269.94
28277.71
NO
Lfl/lK
LB FUEL
0.47
I.P2
l.?2
0.88
0.70
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
N3 NOX
L8/HR LB/HR
6.42 6.42
8.81 8.81
43.44 43.44
34.56 34.56
32.42 32.42
86.68 88.68
88.68 88.68
64.58 64.58
412.91 412.91
20.69 20.69
12.27 12.27
NO NO
LB/IK EMISSION
HOURS LBS.
8.81 0.0018
03.68 C.0004
83. 68 0.0074
20.69 0.0021
12.27 0.0008
0.0125
0.0009
1-52
-------
OATEl 7/28/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOKING
ENGINE 0»T»
C»L 10 NUMBER! 240 ENGINE TYPE AND MODEL! O-120-6JD
RATED MORSEPOMERl 150.
ENGINE TOTAL TINEl SS. HRS
FUEL! »V CIS 80/87 FUEL H/C RATIO! 1.840
OPERATIONAL DATA »*»**>»********.
INLET AIR TEMPERATURE, DEGREES Ft START 78.00 FINISH 78.00
ATMOSPHERIC PRESSURE! START 29.70 FINISH 29.70
INLET AIR HUMIDITY. CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY! 40.00 PERCENT
SAMPLE LINE: TENPEflATURE< DEGREES C: -0.00. FLO* RATEt LITERS/MINI
SAMPLE LINE TRANSPORT TINE. SECl 1.60
NUMBER OF TESTS: 11
COMMENTS!
SERIAL NUMBER! L-29465-27AC
b661
CARB. TEST ENGINE MEASURED
HEATER NODE RPM FUEL FLO*
LB/NR
IDLE-LOU 1 -0.0 16.40
IDLE/TAXI 2 -0.0 19.40
RUN UP i -0.0 12. 80
RUN UP-LEAN 4 -0.0 32.60
RUN UP-RICH 5 -0.0 11.60
IAKE-OFF 6 -0.0 75.00
CLIMB 7 -0.0 75.00
DESCENT 8 -0.0 44. SO
DESCENT ON a -0.0 19.80
APPROACH 9 -0.0 27.00
TAXI
TEST
MODE
1
2
J
4
5
&
7
a
a
q
10
TEST
NOOC
1
2
}
4
5
6
7
a
a
9
10
TEST
MDOF
2
6
7
4
10
TOTAL
TOTAL
EXHftUST
GAS
TF.MP
DEGREES F
2S8.00
415.00
H74.nO
830.00
942.00
1278.00
I27B.OO
1168.00
1166.00
919.00
448.00
KASS EMI
CO
LB/1K
LB FUEL
842.51
1047.64
1111.56
1105.40
1109.55
1168.45
1168.45
492.11
721.80
1191.10
916.09
TIME IN
MODE
MIN.
12.00
0.10
5.00
6.00
4.00
FOR CrCLE
FOR CTCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
25.17
22.65
19.1,1
24.14
20.11
IJ.'iS
11.55
13. 'S3
11.15
24.18
17.78
MEASURED
FUEL FLOW
LB/HR
19.90
75.00
71.00
27.00
16. 00
FUEL
-0,
CO
(DRY I
PERCENT V
2.90
6.40
9.60
9.50
9.50
10.10
10.10
8.30
5.70
10.60
4.80
MASS EMI
N(12
LB/IK
LA FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
l.VB
0.17
6.22
2.70
1.26
14.540
.0
CO
2
(DRY)
PERCENT V
1.90
5.70
7.40
7.50
7. SO
7.10
7.10
8.40
10.10
7.00
5.4C
MASS tMI
C02
LB/IK
LB FUEL
I7S0.26
1466.01
1142.5?
1371.18
1175.09
1301.17
1301.17
1577.95
2009.56
1215.88
1654.66
CO
LB/IK
LB FUEL
1047.64
1168.45
1168.49
1191.10
936.09
18.80
THC
IURYI
PPMV
[537.00
2416.00
2965.00
1621.00
1124.00
2086.00
2086.00
1476.00
1537.00
3788.00
1542.00
MASS EMI
NO
LB/IK
LB FUEL
0.43
0.48
1.25
-0.00
0.90
0.50
0.50
1.43
9.21
0.79
0.70
LTD CYCLE
CO
LB/IK
HOURS
20847.91
87633.56
87631. 56
32159.61
1759a.43
MEASURED CALCULATED
AIR FLO* F/A
LB/HR
198.00 0.03274
225.00 0.05772
360.00 0.08132
363.00 0.09065
ISO. 00 0.08042
813.00 0.08282
813.00 0.08282
SI7.00 0.07814
506.00 0.07115
287.00 0.08373
220.00 0.
NO
IDRYI
PPMV
4.00
18.00
66.00
-0.00
47.00
27.00
27.00
73.00
443.00
43.00
22.00
MASS EMI
NOX
LB/U
LB FUFL
0.43
0.48
1.25
-o.oo
0.40
0.50
0.50
1.41
9.21
0.74
0.70
EMISSIONS
CO
EMISSION
LBS.
4.170
0.438
7.274
1.216
1.174
16.276
1.114
NO
2
I08YI
PPMV
-C.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
13817.43
2C847.93
37115. 08
36257.00
15010.20
87613.56
87613. S6
44158.55
28727.52
12159.61
17548.43
HC
LB/U
LB FUEL
22.65
13.55
13.55
24.38
17.78
04848
NO
X
IDRY(
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
419.42
450.74
643.12
791.92
660.80
1016.47
1016.47
602.10
443.65
658.20
314.29
HC
LB/IK
HOURS
450.74
1016.47
1016.47
658.20
334.29
ALDEHYDES
IORYI
7.00
6.00
-0.00
-0.00
-0.00
-0.00
7.00
7.00
6.00
10.00
5.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.090
0.005
0.084
0.066
0.022
0.268
o.oie
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS E«l
C02
LB/HR
29196.61
29174.02
44014.62
44974.64
41452.86
97587.50
97587.50
70218.94
79980.25
33168.81
11107.51
NO
LB/IK
LB FUEL
0.4a
0.50
0.50
0.79
0.70
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
7.04 7.04
9.63 9.6}
41.06 41.06
-o.no -o.oo
28.47 28.47
17.71 37.73
37.73 37.71
63.79 63.79
366. '3 366.73
21.4} 21.4]
13.25 11.25
NO NO
LB/IK EMISSION
HOURS LBS.
9.61 0.0019
17.73 0.0002
37.71 0.0011
21.41 0.0021
13.25 0.0009
0.0081
C.0006
1-53
-------
DATE: 7/JO/71
TEST ORGANIZATION) SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCONING
ENGINE DATA
CAL ID NUMBER: 226
ENGINE TYPE AND MODEL: 10-360-A/8
RATED HORSEPOWER! 200.
62. MRS
FUEL H/C RATIOl 1.6*0
SERIAL NUMBER) 1-6967-51»«
BO.00
30.10
ENGINE TOTAL TINEt
FUEL: AV GAS loo/iio
OPERATIONAL DATA «««««
INLET AIR TEMPERATURE, DECREES Fl START 77.90 FINISH
ATMOSPHERIC PRESSURE! START 30.10 FINISH
INLET AIR HUMIDITY, GRN H20/LB AIR) 0.01
RELATIVE HUMIDITY: 51.00 PERCENT
SAMPLE LINE) TEMPERATURE. DEGREES Cl -0.00, FLOM RATE. LITERS/MIN:
SAMPLE LINE TRANSPORT TIME. SEC) 1.60
NUMBER Of TESTS) 8
COMMENTS)
7.00
CARB. TEST ENGINE MEASURED
HEATER NODE RPM FUEL FLOM
LB/HR
IDLE-LOW 1 -0.0 16.40
IDLE/TAXI 2 -0.0 17.60
RUN UP 3 -0.0 46.90
TAKE-OFF 6 -0.0 91.40
CLIMB 7 -0.0 70.30
DESCENT 8 -0.0 62.10
APPROACH 9 -0.0 48.10
TAXI
TEST
MODE
1
2
3
6
7
a
9
10
TEST
MODE
1
2
3
6
7
fl
9
10
TEST
none
7
6
7
9
10
TOTAL
TOTAL
' EXHAUST
GAS
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
HASS EMI
CO
LB/1K
LB FUEL
1016.79
690.50
883.54
1083.65
1085.17
1117.91
1116.36
1190.25
TIME IN
MODE
MlN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CVCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EM!
HC
LB/1K
LB FUEL
93.63
29.97
22.31
14.81
15.16
16.58
18.17
46.43
MEASURED
FUEL FLOH
LB/HR
17.60
91.40
70.30
48.10
18.80
FUEL
-0,
CO
(DRY)
PERCENT V
6.90
4.00
6.60
9.40
9.20
9.60
9.60
8.90
MASS EMI
N02
LB/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
3.52
0.46
5.83
4.81
1.26
15.881
.0
CO
2
(DRY)
PERCENT V
5.70
7.40
8.20
7.90
7.70
7.50
7.50
5.60
MASS EMI
CO 2
LB/1K
LB FUEL
1319.77
2007.11
1724.79
1430.96
1427.31
1372.26
1370.35
1176.72
CO
LB/IK
LB FUEL
690.50
1083.65
1085.37
1116.36
I19C.25
18. BO
THC
IDRV)
PPNV
11094.00
3031.00
2910.00
2243.00
2243.00
2486.00
2728.00
6062.00
MASS EMI
NO
LB/IK
LB FUEL
-0.00
-0.00
4.60
2.37
2.91
2.79
2.85
-0.00
LTD CYCLE
CO
LB/IK
HOURS
12152.71
99045.56
76301.31
53696.78
22376.60
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
170.00 0.06413
222.00 0.05427
562.00 O.C69BO
1026.00 0.08125
788.00 0.07946
686.00 0.08059
531.00 O.C8070
197.00 0.
NO
(DRY)
PPHV
-o.on
-0.00
209.00
125.00
150.00
146.00
149.00
-0.00
MASS EMI
NOX
LB/IK
LB FUEL
-0.00
-0.00
4.60
2.37
2.91
2.79
2.85
-0.00
EMISSIONS
CO
EMISSION
LBS.
2.431
0.495
6.333
5.370
1.499
16.128
1.016
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
16675.38
12152.71
41438.17
99045.56
76301.31
69422.44
53696.78
22376.60
HC
LB/IK
LB FUEL
29.97
14.81
15.16
18.17
46.43
07075
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
1535.54
527.41
1046.39
1353.57
1065.41
1029.62
873.91
872.90
HC
LB/IK
HOURS
527.41
1353.57
1065.41
873.91
872.90
ALDEHYDES SMOKE
(DRV)
7.00
7.00
-0.00
-0.00
5.00
5.00
5.00
9.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.105
0.007
0.088
O.OB7
0.058
0.347
0.022
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
21644.13
35325.10
80892.56
130789.38
100339. 81
85217.44
65913.81
22122.31
NO
L8/1K
LB FUEL
-0.00
2.3V
2.91
2.85
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LR/HR LB/HR
-0.00 -0.00
-0.00 -0.00
215.54 215.54
216.34 216.34
204.34 204.34
173.42 173.42
136.89 136.89
-n.OO -0.00
NO NO
L8/1K EMISSION
HOURS LBS.
-0.00 -0.0000
216.34 0.0011
204.34 0.0170
136.89 0.0137
-0.00 -0.0000
-0.0000
-0.0000
1-54
-------
DATE! T/10/T1
TEST ORGANISATION! SCOTT/CEN AVIATION
ENGINE SUPPLIES I ITCOHING
ENGINE 0«T»
C«l 10 NUMBER! 227 ENGINE TYPE AND MODEL! IO-360-A/B
RATED HORSEPOWER! 200.
ENGINE TOTAL TINEl 62. MRS
FUEL" AV G«S 100/130 FUEL H/C RATIO! 1.8*0
OPERATIONAL DATA «*»»»»»'
INLET AIR TEMPERATURE, DEGREES Fl START 60.50 FINISH 80.50
ATMOSPHERIC PRESSUREl START 10.12 FINISH 30.12
INLET AIR HUH101TY, CRN H20/LB AIRi 0.01
RELATIVE HUNIOITri 49.00 PERCENT
SAMPLE LINEl TEMPERATURE, DECREES C: -0.00. FLOy RATE. LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TIME. SEC! 1.60
NUMBER OF TESTS: a
COMMENTS!
SERIAL NUMBER! L-496T-MAR
CARS. TEST ENGINE MEASURED
HEATER NODE RPN FUEL FLOW
LB/HR
IDLE-LOU -0.0 12.90
IDLE/TAXI -0.0 18.80
RUN UP -0.0 44. 50
TAKE-OFF -0.0 93.80
CLINS -0.0 71.90
DESCENT -0.0 64.50
APPROACH -0.0 4*. 50
TAXI
TEST
MODE
1
2
3
6
7
8
9
10
TEST
MODE
1
2
3
6
7
a
9
10
TEST
MODE
2
fi
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.60
-0.00
-0.00
MASS EMI
CO
LB/IK
LB FUEL
855.12
747.26
1058.47
1146.82
1159.99
1147.97
1159.00
1210.44
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-O.OD
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS tH!
HC
LB/U
LB FUEL
W
161. ,15
50. 76
22.15
15.58
I5.il9
16.13
18.18
102.09
MEASURED
FUEL FLO*
LB/HR
18.80
93.80
71.50
44.50
17.60
FUEL
-0
CO
IORVI
PERCENT V
6.10
5.30
8.60
10.30
10.30
10.20
13.20
11.50
MASS EMI
NQ2
LB/IK
LB FUEL
n.o
0.0
0.0
0.0
0.0
3.0
0.0
0.0
FUEL
USED
LBS.
3.76
0.47
5.93
4.45
1.18
15.793
0
CO
2
IORTI
PERCENT V
6.30
B. 40
7.50
7.60
7.40
7.50
7.30
6.00
MASS EMI
C02
LB/IK
LB FUEL
1387.97
1860.87
1450.37
1329.57
1309.43
1326.26
1303.30
992.28
CO
LB/IK
LB FUEL
747.26
1146.82
1159.96
1159.00
1210.44
17.60
THC
(DRV)
PPMV
20079.00
6286.00
3143.00
2444.00
2386.00
2503.00
2794.00
16936.00
PASS EMI
NO
LB/U
LB FUEL
1.08
3.47
3.23
1.26
1.85
2.24
2.30
0.76
LTD CYCLE
CO
LB/U
HOURS
14048.54
107571.94
82938.50
51575.68
21303.72
MEASURED CALCULATED
AIR FLO* F/A
LB/HR
131.00 0.06720
230.00 0.06618
502.00 0.07622
1024.00 0.08427
777.00 0.08339
704.00 O.C8340
484.00 0.08268
165.00 0.
NO
IORYI
PPMV
47.00
150.00
160.00
69.00
100.00
121.00
123.00
44.00
MASS EMI
NDX
LB/IK
LB FUEL
1.08
3.47
3.23
1.26
1.85
2.24
2.30
0.76
EMISSIONS
CO
EMISSION
LBS.
2.810
0.538
6.884
5.158
1.427
16.816
1.065
NO
2
IORVI
PPMV
-C.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
HASS EMI
CO
LB/HR
11013.69
14048.54
47101.85
107571.94
82938.50
74C44.00
51575.68
21303.72
HC
LB/IK
LB FUEL
50.76
15.58
15.39
18.18
102.09
08982
NO
K
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS ENI
HC
LB/HR
2080.07
954.28
981.89
1461.87
1100.36
1040.63
809.13
1796.86
HC
LB/IK
HOURS
954. JB
1461.87
1100.36
809.13
1 796.86
ALDEHYDES SMtlKE
IDRYI
23.00
14.00
-0.00
-0.00
10.00
7.00
4.00
12.00
MASS ENI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.191
0.007
0.091
0.081
0.120
0.491
0.031
-0.00
'0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/HR
17904.80
349B4.31
64541.46
124713.50
93624.38
8554). 88
57997.01
17464.14
NO
LB/IK
LB FUEL
3.47
1.26
1.85
2.10
0.76
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS ENI
NO NOX
LB/HR IB/MR
13.96 13.96
65.31 65.31
143.94 143.94
lie. 37 118.37
132.26 132.26
144.28 144.28
102.16 102.16
13.19 13.39
SO NO
LB/IK EMISSION
HOURS LBS.
65.31 0.0131
I1B.37 0.0006
132.26 0.0110
102.16 0.0102
13.39 0.0009
0.0357
0.0023
1-55
-------
OtTEl 7/30/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOMING
ENGINE DATA
C»L ID NUMBER: 225 ENGINE TYPE AND NODELI io-360-A/s
RATED HORSEPOWER I 200.
ENGINE TOTAL T1XEI 63. MRS
FUEL: »V GAS 100/130 FUEL M/C RATIO! 1.640
OPERATIONAL DATA ««»«»«««««««»«««»«
INLET AIR TEMPERATURE, DEGREES Fl START 85.50 FINISH 67.00
ATMOSPHERIC PRESSURE! START 30.10 FINISH 30.10
INLET AIR HUMIDITY, CRN H20/LB AIRl 0.01
RELATIVE HUMIDITY: 40.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES C: -0.00, FLO* RATE, LITERS/NIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS! 6
COMMENTS!
SERIAL NUMBER! L-696T-51AC
CARB.
HEATER
IDLE-LOW
IDLE/TAXI
RUN UP
TAKE-OFF
CLIMB
DESCENT
APPROACH
TAXI
TEST
MODE
1
2
3
6
7
6
9
10
ENGINE
RPM
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
MEASURED
FUEL FLO*
LB/HR
16.40
17.60
46.90
105.50
73.80
64.50
46.90
16.80
MEASURED
AIR FLOW
LB/HR
182.00
200.00
549.00
1146.00
610.00
706.00
513.00
162.00
CALCULATED
F/A
0.07104
0.07382
0.07522
0.06801
0.08507
0.08510
0.06484
0.08262
TEST
MODE
1
2
3
6
7
8
9
10
EXHAUST
GAS
TEMP
DEGREES F
426.00
471.00
930.00
1211.00
1267.00
1233.00
1076.00
538.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO CO THC
(DRY) 2 IORYI
PERCENT V (DRY) PPMV
PERCENT V
6.90
7.80
7.70
10.90
10.30
10.30
10.30
9.60
7.40
7.50
8.30
7.80
7.80
7.80
7.70
6.30
10028.00
6029.00
2626.00
2626.00
2328.00
2388.00
2746.00
17908.00
NO
(DRY)
PPMV
46.00
58.00
-0.00
149.00
142.00
149.00
152.00
132.00
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
(DRY)
PPHV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
(DRV)
15.00
6.00
-0.00
-0.00
5.00
9.00
8.00
27.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
NODE
1
2
3
&
7
n
9
10
MASS EMI
CO
LB/1K
LB FUEL
910.92
990.88
956.54
1161.26
1135.04
1134.67
1138.65
1096.29
MASS EMI
HC
LB/1K
LB FUFL
75.82
43.86
18.68
16.02
14.69
15.07
17.39
117.12
MASS EMI HASS EMI MASS EMI
N02 CO2 NO
LO/1K LB/1K L8/1K
LB FUEL L8 FUEL LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
1534.97
1497.01
1620.05
1305.68
1350.54
1350.09
1337.47
1130.40
1.00
1.21
-0.00
2.61
2.57
2.70
2.76
2.48
MASS EMI
NOX
LB/1K
LB FUEL
1.00
1.21
-0.00
2.61
2.57
2.70
2.76
2.48
MASS EMI
CO
LB/HR
14939.07
17439.44
44661.66
122513.13
83765.75
73145.94
53402.79
20610.24
MASS EMI
HC
LB/HR
1243.47
772.02
876.24
1690.43
1084.32
971.78
815.40
2201.93
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
MASS EMI
C02
LB/HR
25173.54
26347.36
75980.25
137749.19
99669.44
87080.94
62727.17
21251.55
MASS EMI
NO
LH/HR
16.36
21.30
-0.00
275.08
189.69
173.90
129.45
46.55
MASS EMI
NQX
LB/HR
16.36
21.30
-0.00
275.08
189.69
173.90
129.45
46.55
LTD CYCLE EMISSIONS
TEST
MODE
2
6
7
9
1(1
TOTAL FOR
TOTAL FOR
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
CYCLE
CYCLE/LB
MEASURED
FUEL FLOM
LB/HR
17.60
105.50
73.80
46.90
18.80
FUEL
FUEL
USED
LBS.
3.52
0.53
6.13
4.69
1.26
16.122
CO
L8/1K
LB FUEL
990.88
1161.26
1135.04
1136.65
1096.29
CO
IB/ IK
HOURS
17439.44
122513.13
83765.75
53402.79
20610.24
CO
EMISSION
LBS.
3.468
0.613
6.95)
5.340
1.361
17.774
1.102
MC
LB/1K
LB FUEL
43.86
16.02
14.69
17.39
U7.12
HC
LB/1K
HOURS
772.02
1690.43
1064.32
AI5.40
2201.93
HC
EMISSION
LBS.
0.154
0.008
0.090
0.082
0.14A
0.482
0.030
NO
Ltt/lK
LB FUEL
1.21
2.61
2.57
2.76
2.49
NO
LB/1K
HOURS
21.30
275.08
169.69
129.45
46.55
NO
EMISSION
LBS.
0.0043
0.0014
0.0157
0.0129
0.0031
0.0374
0.0023
1-56
-------
3313
DATE: a/ 6/71
TEST ORGANISATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOMING
FNGINE 0»T»
C»L 10 NUMBERl 2T1 ENGINE TYPE AND MODEL! IO-360-AIA
RATED HORSEPOHER: 200.
ENGINE TOTAL TIXEl 1023. MRS
FUELI AV GAS 100/110 FUEL H/C RATIO) 1.640
OPERATIONAL DATA «»»««««««««
INLET AIR TEMPERATURE* DEGREES Ft START 84.00 FINISH
ATMOSPHERIC PRESSUREi START 30.20 FINISH
INLET AIR HUMIDITY, CRN H20/LB AIRI 0.01
RELATIVE HUMIOITYl 36.00 PERCENT
SAMPLE LINE: TEMPERATURE, CEGREES Cl -O.OC, FLOW RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SECl 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUNBERI L-2928-5UA
89.00
30.20
T.OO
CARB. TEST ENGINE MEASURED
HEATER NUDE RPM FUEL FLOW
LB/HR
IDLE-LOU 1 -0.0 5.90
IDLF./TAXI 2 -0.0 9.40
RUN UP 3 -0.0 2T.OO
RUN UP-LEAN 4 -0.0 27.00
RUN UP-RICH 5 -0.0 27.00
TAKE-OFF 6 -0.0 98.40
CLIMB 7 -0.0 70.30
DESCENT 8 -0.0 58.60
APPROACH 9 -0.0 31.60
TAX!
TEST
MODE
1
2
3
4
5
6
7
8
9
10
TEST
MODE
I
2
3
4
5
6
7
a
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
FXHAUST
GAS
TEMP
DEGREES f
448.00
560. OU
1031.00
998.00
1031.00
1233.00
12)3.00
1188.00
1076.00
673.00
MASS ENI
CO
(.B/U
IB FUEL
1399. 85
1323.11
923.15
9)6.53
936.53
1212.14
1147.29
1156.24
990.31
1366.20
TIME IN
MODE
HIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MEASURED
FUF.L FLO*
LB/HR
9.40
98.40
70.30
31.60
9.40
FUEL
-0.
CO
IORV)
PERCENT V
8.80
9.30
6.90
7.00
7.00
9.90
9.20
9.10
7.50
9.40
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
o.o
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LOS.
1.88
0.49
5.83
3.16
0.63
11.997
,0
CO
2
IORYI
PERCENT V
3.90
4.90
8.20
8.10
8.10
6.60
7.00
6.80
7.80
4.50
MASS EMI
CO 2
LB/IK
LB FUEL
974.77
1095.34
1723.76
1702.74
1702.74
1269.70
1371.59
1357.54
1616.24
1027.63
CO
LB/IK
LB rUFL
1323.11
1212.14
1147.29
990.31
1366.20
9.40
THC
IORVI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NO
LB/IK
LB FUEL
0.16
-0.00
9.85
6.66
5.32
2.80
3.95
4.55
fl.7?
2.70
LTD CYCLE
CO
LB/IK
HOURS
12437.25
119274.56
80654.69
31293.82
12842.30
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
58. OC O.C5994
96.00 0.06673
324.00 0.06985
323.00 0.06988
323.00 0.06988
1060.00 0.07696
778.00 0.07541
646.00 0.07407
371.00 0.07092
94.00 0.
NO
IORY)
PPMV
6.00
-0.00
448.00
303.00
242.00
139.00
193.00
218.00
402.00
113.00
MASS EMI
NOX
LB/IK
LD FUEL
0.16
-0.00
9.85
6.66
5.32
2.80
3.95
4.55
8.72
2.70
EMISSIONS
CO
EMISSION
LBS.
2.487
0.596
6.694
3.129
0.860
13.768
1.148
NO
2
IDRVI
PPMV
-C.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
cn
IB/ MR
8259.10
12437.25
24925.14 .
25286.38
25286.38
119274.56
80654.69
67755.31
31?9». 82
12642.30
HC
LB/IK
LQ FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
06544
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
HC
LB/IK
HOURS
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES SMOKE
IORYI
66.00
45.00
-0.00
-0.00
-0.00
-0.00
18.00
12.00
15.00
26.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
-0.000
-0.000
-0.000
-0.000
-o.ooo
-0.000
-0.000
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-O.JO
-0.00
MASS FMI
C02
LR/HR
5751.13
10296. 11
46541.55
45973.95
45973.95
124938.13
96422.44
79551.63
91136.38
9659.74
NO
LB/IK
LB FUEL
-0.00
2.80
3.95
8.72
2.70
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
0.92 0.92
-0.00 -0.00
265.82 265.82
179.78 179.78
143.59 143.59
275.07 275.07
277.92 277.92
266.61 266.61
275.51 275.51
25.36 25.36
NO NO
LB/IK EMISSION
HOURS LBS.
-0.00 -0.0000
275.07 0.0014
277.92 0.0231
275.51 0.0276
25.36 0.0017
-0.0000
-0.0000
1-57
-------
DATE: 8/ 6/71
TEST ORG»NIZ»TIONI SCOTT/CEN AVIATION
ENGINE SUPPLIER: Lreox INC
ENGINE DATA
C»L 10 NUMBER: 272 ENGINE TYPE AND NODELI io-36O-»u
RATED HORSEPOMERl 200.
ENGINE TOTAL TINEl 1023. MRS
FUEL: AV GAS loo/no FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA «»««»««««««»«««»
INLET AIR TENPERATURE, DEGREES F: START 78.00 FINISH 7S.OO
ATMOSPHERIC PRESSURE: START 30.18 FINISH 30.18
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.02
RELATIVE HUMIDITY: 77.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOM RATE, LITERS/NIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER: L-2«z«-5iAB
CARB. TEST ENGINE MEASURED
HEATER NODE RPM FUEL FLOM
LB/HR
IDLE-LOU I -0.0 4.70
IDLE/TAXI 2 -0.0 8.20
RUN UP 3 -0.0 30. JO
RUN UP-LEAN 4 -0.0 30.50
RUN UP-RICH 5 -0.0 30.50
TAKE-OFF 6 -0.0 93.80
CLIMB 7 -0.0 70.30
DESCENT 8 -0.0 58.60
APPROACH «> -0.0 29.30
TAXI
TESI
MODE
1
2
3
4
5
6
7
e
9
10
TESI
MODE
(
2
3
4
5
ft
7
a
9
10
TEST
MflOE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
549.00
583.00
1087.00
1065.00
1110.00
1233.00
1244.00
1199.00
1054.00
673.00
MASS EMI
CO
LR/1K
Lfl FUEL
1036.84
1137.71
824.19
815.86
820.10
1118.28
1130.95
1066.39
978.72
1030.79
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS ENI
HC
LB/1K
IB FUEL
273.05
I03.ee
20.96
21.11
18.64
16.87
16.48
18.49
20.40
264.92
MEASURED
FUEL FLO*
LB/HR
8.20
93.80
70.30
29.30
8.20
FUEL
-0
CO
IDRYI
PERCENT V
8.80
8.60
.90
.80
.90
.10
.20
3.10
7.20
8.80
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
1.64
0.47
5.83
2.93
0.55
11.473
0
CO
2
IORY)
PERCENT
4.30
5.30
8.30
8.30
8.40
7.10
7.00
7.00
7.40
4.20
MASS EMI
C02
LB/IK
LB FUEL
796.04
1101.66
1821.75
1834.44
1834.56
1370.90
1352.05
1447.99
1580.50
772.99
CO
LB/IK
LB FUEL
1137.71
1118.26
1UC. 95
978.72
1030.79
8.20
THC
IDRY)
PPMV
V
40464.00
13711.00
2620.00
2620.00
2341.00
2397.00
2341.00
2452.00
2620.00
42471.00
MASS EMI
NO
LB/IK
LB FUEL
0.12
0.37
8.67
5.61
4.79
3.33
3.29
3.74
5.34
0.90
LTD CYCLE
CO
LB/IK
HOURS
9329.18
104894.31
79505.81
28676.38
6452.44
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
36.00 0.08078
79.00 0.07161
373.00 0.06684
374.00 0.06638
373.00 0.06715
1036.00 0.07649
774.00 0.07650
660.00 0.07140
340.00 O.C6900
62.00 0.
NO
IDRYI
PPMV
6.00
17.00
378.00
243.00
210.00
165.00
163.00
173.00
239.00
47.00
MASS EMI
NOX
LB/IK
LB FUEL
0.12
0.37
8.67
5.61
4.79
3.33
3.29
3.74
i.34
0.90
EMISSIONS
cn
EMISSION
LBS.
1.866
0.524
6.599
2.868
0.566
12.423
1.088
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
4873.14
9329.18
25137.68
24883.68
25012.97
104894.31
79505.81
62490.20
26676.38
8452.44
HC
LB/IK
LB FUEL
103.88
16. SI
16.46
20.40
284.92
OB129
NO
X
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-'0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
1263.34
851.84
639.32
643.77
568.41
1582.43
1158.66
1063.41
597.64
2336.35
HC
LB/IK
HOURS
851.84
1582.43
1158.66
597.64
2336.35
ALDEHYDES SMOKE
IORYI
38.00
30.00
-0.00
-0.00
-0.00
-0.00
12.00
10.00
10.00
34.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.170
0.008
0.096
0.060
0.157
0.491
0.043
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
3741.39
9033.57
55563.50
55950.36
55954.01
128589.88
95048.88
84652.13
46308.64
6338.50
NO
LB/IK
LB FUEL
0.37
3.33
3.29
5.34
0.90
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
C.55 0.55
3.03 3.03
264.54 264.54
171.24 171.24
146.24 146.24
312.40 312.40
231.38 231.38
219.23 219.23
156.35 156.35
(.42 7.42
NO NO
LB/IK EMISSION
HOURS LBS.
3.03 0.0006
312.40 0.0016
231.38 0.0192
156.35 0.0156
7.42 0.0005
0.0375
0.0033
1-58
-------
3 3 CO
D»TE: B/ 6/71
TEST ORGAN HAT I ON: SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOMING
ENGINE DATA
C»l 10 NUMBERl 273 ENGINE TYPE AND MODEL! IO-360-A1A
RATED NORSEPOMERI 200.
ENGINE TOTAL TIME! 1024. MRS
FUEL! AV GAS 100/130 FUEL H/C RATIOI l.8»0
OPERATIONAL DATA «»««««««««
INLET AIR TEMPERATURE! OCGREES Fl START TT.OO FINISH
ATMOSPHERIC PRESSURE! START 30.IB FINISH
INLET AIR HUMIDITY, GUN H20/L8 AIR1 0.02
RELATIVE HUMIDITY! 79.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES Ct -0.00, FLON RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS! 10
COMMENTS:
SERIAL NUMBER I L-242I-JIAC
BO.00
30.11
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOM
LB/HR
IDLE-LOU 1 -0.0 4. TO
IDLF/TAXI 2 -0.0 8.20
RUN UP 3 -0.0 28.10
RUN UP-LEAN * -0.0 2B.10
RUN UP-RICH 5 -0.0 2T.OO
TAKE-OFF 6 -0.0 92.60
CLIMB T -0.0 70.30
DESCENT a -0.0 SO. 40
APPROACH 9 -0.0 27.00
TAKt
IEST
MODE
1
2
3
*
5
6
7
H
9
10
TCSI
nriDE
i
z
3
4
5
6
7
s
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
504.00
560.00
1065.00
1020.00
1087.00
1256.00
1256.00
liaa.oo
1054.00
69*. 00
MASS EMI
CO
LB/1K
LB FUEL
841.23
963.51
816.02
827.59
799.38
1128.55
1064.56
974.35
967.60
1061. 39
TIHE IN
MOdE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS (Ml
HC
LBMK
LB FUFL
386.17
191.34
23.13
25.60
20.11
18.90
16.54
18.94
18.34
204.69
HEAiUREU
FUEL FLOW
LB/HR
B. 20
92.60
70.30
27.00
9.40
FUEL
-0.
CO
(DRY)
PERCENT V
7.50
7.60
6.10
6.20
6.00
9.20
a. so
7.60
7.30
9.00
MASS EMI
urn
LB/IK
LB FUEL
0.0
0.0
o.n
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
1.64
0.46
5.83
2.70
0.63
11.268
,0
CO
2
IORYI
PERCENT V
4.50
9.70
B. 70
a. 60
a. 90
7.00
7.40
7.90
7.70
5.10
MASS EH]
C02
LB/IK
LB FUEL
793.05
1135.42
1828.6*
1803.66
1863.08
1349.18
1456.20
1591.35
1603.62
945.02
CO
LB/IK
LB FUEL
963.51
1128.55
1064.56
967.60
1061.39
9.40
THC
IORYI
PPMV
60115.00
26352.00
3019.00
3349.00
2635.00
2690.00
2306.00
2580.00
2416.00
30305.00
MASS EMI
NO
LB/IK
LB FUEL
0.88
1.79
9.12
5.55
5.32
2.76
3.52
5.92
5.62
2.01
LTD CYCLE
CO
LB/IK
HOURS
7900.81
104504.06
74B3B.56
26125.09
9977.05
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
33.00 0.08473
76.00 0.07456
344.00 0. 06968
342.00 0.06987
333.00 0.06990
1017.00 0.07666
793.00 0.07493
586.00 0.07301
315.00 0.07067
81.
NO
IDRYI
PPMV
48.00
86.00
415.00
253.00
243.00
137.00
171.00
281.00
258.00
104.00
MASS EMI
NOX
LB/IK.
LB FUEL
o.aa
1.79
9.12
5.55
5.32
2.76
3.52
5.92
5.62
2.01
EMISSIONS
CO
EMISSION
LBS.
1.580
0.523
6.212
2.613
0.668
11.595
1.029
00 0.
NO
2
IDRV)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/KR
3953.77
7900.81
22930.11
23255.19
21583.27
104504.06
74838.56
49107.16
26125.09
9977.05
HC
Lfl/IK
LB FUEL
191.34
18.90
16.54
18.34
204.69
08042
NO
X
IORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
1815.01
1568.98
649.96
714.43
542.87
1750.02
1162.81
954.76
495.20
1924.06
HC
L8/1K
HOURS
1568.98
1750.02
1162. ai
495.20
1924.06
ALDEHYDES SMOKE
IDRYI
44.00
42.00
-0.00
-0.00
-0.00
-0.00
15.00
10.00
9.00
23.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.314
0.009
0.097
0.050
0.129
0.597
0.053
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
en 2
LB/HR
3727.35
9310.46
51384.69
50683.33
50303.05
124934.25
102370.81
80204.00
43297.61
8883.17
NCI
LB/IK
L8 FUEL
1.79
2.76
3.52
5.62
2.01
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO N0>
LB/HR LA/HR
4.16 4.16
14.69 14.69
256.24 256.24
1S5.87 155.87
143.58 143.58
255.61 255.61
247.30 247.30
298.23 298.23
151.66 151.66
18.14 IB. 94
NO NO
LB/IK EMISSION
HOURS LBS.
14.69 0.0029
255.61 0.0013
247.30 0.0205
151.66 0.0152
18.94 0.0013
0.0412
0.0037
1-59
-------
DATE: 8/ 6/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOMING
ENGINE DATA
CAL ID NUMBER: 274 ENGINE TYPE AND MODEL: io-360-»i«
RATED HORSEPOHER: 200.
ENGINE TOTAL TIME: 1024. MRS
FUEL: AV GAS 100/130 FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA «««»»««»»»««
INLET AIR TEMPERATUREt DEGREES F: START 79.00 FINISH
ATMOSPHERIC PRESSURE: START 30.18 FINISH
INLET AIR HUMIDITY, CRN H20/L8 AIR: 0.02
RELATIVE HUMIDITY: 79.00 PERCENT
SAMPLE LINE: TEMPERATURE, CEGREES C: -0.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TINE, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER: L-2829-5UD
79.00
30.18
CARD. TEST ENGINE MEASURER
HEATER MODE RPM FUEL FLOM
LB/HR
IDLE-LOW 1 -0.0 8.20
IDLE/TAXI 2 -0.0 8.20
RUN UP 3 -0.0 28.10
RUN UP-LEAN 4 -0.0 28.10
RUN UP-RICH 5 -0.0 29.30
TAKE-OFF 6 -0.0 94.90
CLIMn 7 -0.0 85.60
DESCENT S -0.0 -0.00
APPROACH 9 -0.0 27.00
TAXI
TEST
MODE
1
2
3
4
5
6
7
a
9
10
TESI
MHDE
1
?
3
4
>
6
7
8
9
10
TEST
MODE
2
6
7
9
10
TOTAL
inTAL
EXHAUST
GAS
TEMP
DEGREES F
538.00
617.00
1031.00
986.00
1C09.00
1711.00
1222.00
uan.oo
1031.00
673.00
MASS EMI
CO
LB/IK
LB FUEL
71)3.01
1006. 14
1038.33
1053.21
1048.54
1245.70
1233. 11
1310.46
1005.18
1010.67
T 1 NF IN
HOOF
KIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/L8
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-1.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
531.87
342.15
30.65
33.83
26.64
18.15
17.74
18.30
21.43
349.21
MEASURED
FUEL FLOW
L8/HR
8.20
94.40
85.60
27.00
8.20
FUEL
-0.
CO
(DRY1
PERCENT V
«. 50
9.90
8.50
8.70
8.50
10.90
10.00
11.60
7.30
9.10
MASS EMI
NH?
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
o.n
0.0
FUEL
USED
L8S.
1.64
0.47
7.10
2.70
0.55
12.469
.0
CO
2
(DRY)
PERCENT V
3.20
4.10
7.60
7.50
7.50
6.50
6.50
6.00
7.10
3.60
MASS EMI
C02
LB/IK
LB FUtL
469.08
654.71
1458.71
1426.58
1453.67
1167.18
1188.09
1065.02
1536.09
628.22
CO
LB/IK
L8 FUFL
1006.14
1245.70
1233.11
1005.18
1010.67
8.20
THC
IDRYI
PPMV
99541.00
58782.00
4381.00
4880.00
3771.00
2773.00
2662.00
2828.00
2717.00
54900.00
MASS EMI
NO
L8/1K
LB FUEL
0.14
0.23
3.09
2.15
1.92
1.39
1.39
0.95
4.70
0.36
LTD CYCLE
CO
LB/IK
HOURS
8250.38
118216.56
105554.31
27139.89
8287.5?
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
43.00 0.10251
57.00 0.09377
31U.OO 0.07675
316.00 0.07749
331.00 0.07604
991.00 0.08252
900.00 0.08106
-0.00 0.08369
310.00 0.06821
56.
NO
(DRY)
PPMV
9.00
14.00
154.00
108.00
95.00
14.00
75.00
51.00
208.00
20.00
MASS EMI
NOX
LB/IK
LB FUEL
0.1',
0.23
3.09
2.15
1.92
1.39
1.39
C.95
4.70
0.36
EMISSIONS
CO
EMISSION
LflS.
1.651
J.591
4.761
2.714
0.555
14.271
1.145
00 0.
NO
2
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
6502.71
8250.38
29177.05
29595.32
30722.12
118216.56
105554.31
-0.00
27139.89
8287.52
HC
LB/IK
LB FUEL
342.15
18.15
17.74
21.43
349.21
08597
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
4361.37
2805.62
861.27
950.75
780.61
1722.45
1518.18
-0.00
578.52
2863.52
HC
LB/IK
HOURS
2805.62
1722.45
1518.18
578.52
2863.52
ALDEHYDES SMOKE
(DRV)
43.00
60.00
-0.00
-0.00
-0.00
-0.00
20.00
13.00
15.00
34.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
O.C
0.0
0.0
HC
EMISSION
L8S.
0.561
0.009
0.126
0.058
0.192
0.945
0.076
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-O.JO
-0.00
MASS Ell
CO 2
LB/HH
3846.43
5368.59
40989.62
40086.96
42592.36
110765.25
101700.25
-0.00
41474.53
5151.38
NO
LB/IK
L8 FUEL
0.21
1.39
1.39
4.70
0.36
PARUCULAIES
-0.00
-0.00
-0.00
-0.00
-0.00
-O.CO
-0.00
-0.00
-o.oo
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
1.13 1.13
1.92 1.92
86.13 86.83
60.35 60.35
56.40 56.40
131.83 131.83
119.40 119.40
-0.00 -0.00
127.02 127.02
2.99 2.99
NO NO
LB/IK EMISSION
HCUKS LBS.
1.92 0.0004
131.83 0.0007
119. 4C 0.0099
127.02 C.0127
2.99 0.0002
0.0239
0.0019
1-60
-------
D»IE: 7/16/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER I LYCOMING
ENGINE DATA
SERIAL NUMBER: L-7682-51AA
C«L 10 NUMBER I ITS ENGINE TYPE AND MODEL: 10-360-4186
RATED HORSEPONER: 200.
ENGINE TOTAL TIME: 660. HRS
FUEL: AV GAS 80/87 FUEL H/C RATIO: 1.840
OPERATIONAL DATA -»»»***»»***
INLET AIR TEMPERATURE, DEGREES Fl START 89.00 FINISH 90.50
ATMOSPHERIC PRESSURE! START 30.1} FINISH 30.1)
INLET AIR HUMIDITY, CRN H20/LB AIRl 0.02
RELATIVE HUMIDITY: 59.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C> -0.00, FLOW RATE, LITERS/MIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOk
LB/HR
IDLE-LOU I -0.0 22.30
IDLE/TAXI 2 -0.0 23.40
RUN UP 3 -0.0 36.30
RUN UP-LEAN 4 -0.0 37.50
RUN UP-RICH 5 -0.0 36.30
TAKE-OFF 6 -0.0 85.60
CLINH 7 -0.0 B2.00
DESCENT 9 -0.0 64.50
APPROACH 9 -0.0 44.50
TAXI
TFSI
MODE
1
7
e
9
10
TEST
HOOC
1
2
1
4
5
6
7
fl
<»
10
TEST
MODE
2
6
7
9
10
TOT At
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
415.00
471.00
762.00
717.00
TBS. 00
1099.00
1166.00
1112.00
953.00
527.00
HASS EMI
CO
LB/IK
LB FUEL
1369.01
1305.65
1385.42
1)55. 12
1366.89
1100. Bl
1143.66
1156.40
1402.71
1374.35
TIME IN
*OOE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
FXHAUST
GAS
PRESSURE
PS1A
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
74.28
57.63
32.49
35.99
36.86
24.66
22.91
22.55
26.59
55.06
MEASURFD
FUEL FLOk
LB/HR
23.40
85.60
82.00
44.50
21.10
FUEL
-0
CO
IDRYI
PERCENT V
a. 40
10.00
11.90
12.60
12.30
10.30
10.80
10.80
14.00
9.00
MASS EMI
NO 2
LO/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
4.68
0.43
6.61
4.45
1.41
17.778
0
CO
2
(DRY)
PERCENT V
3.20
4.70
5.80
5.60
5.30
B.20
7.90
7.70
5.70
3.60
MASS EMI
CO 2
LB/1K
LB FUEL
819.44
964.34
908.31
946.31
925.43
1376.97
1314.43
1295.42
897.33
863.77
CO
LB/IK
LB FUEL
1305.85
1100. ai
1143.66
1402.71
1374.35
21.10
THC
IDRVI
PPNV
7956.00
TT06.00
5691.00
5843.00
5792.00
4029.00
3778.00
3677.00
4634.00
6296.00
MASS EMI
NO
LB/1K
LB FUEL
0.32
0.06
0.20
0.21
0.13
2.46
1.69
1.67
0.38
0.15
LTD CYCLE
CO
LB/1K
HOURS
10556.97
94228. B8
93780.19
62420.42
28998.79
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
201.00 0.05868
225.00 0.07278
347.00 0.09503
361.00 0.08810
348.00 0.08537
945.00 0.08756
891.00 0.08850
697.00 0.08761
424.00 O.C9458
195.00 0.
NO
IORYI
PPMV
12.00
3.00
12.00
12.00
7.00
140.00
97.00
95.00
23.00
6.30
MASS EMI
NOX
LB/IK
LB FUEL
0.32
0.06
0.20
0.21
0.13
2.46
1.69
1.67
0.38
0.15
EMISSIONS
CO
EMISSION
LBS.
6.111
0.471
7.784
6.242
1.941
22.551
1.269
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
30528.90
30556.97
5029C.82
50816.97
49617.92
94228.88
93780.19
74587.50
62420.42
28998.79
MC
LB/1K
LB FUEL
57.63
24.66
22.91
26.59
55.06
06253
NO
X
(DKYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
1656.46
1348.60
1179.25
1349.64
1338.16
2111.00
1878.86
1454.39
1183.31
1161.84
HC
LB/1K
HOURS
1148.60
2111.00
1878.86
1183.31
1161.84
ALDEHYDES SMOKE
IORYI
86.00
73.00
-0.00
-0.00
-0.00
-0.00
11.00
9.00
11.00
79.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.270
0.011
0.156
0.118
0.078
0.632
0.036
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS EMI
C02
LB/H*
18273.42
22565.58
32971.62
35486.63
33592.91
117868. ai
107783.56
83954.81
39931.14
18225.4)
NO
LB/IH
Lfl FUFL
0.06
2.46
1.64
0.38
0.15
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/MR LB/HR
7.16 7.16
1.51 1.51
7.13 7.1)
7.95 7.95
4.64 4.64
210.38 210.38
138.35 138.35
107.77 107.77
16.84 16.84
3.18 3.18
NO NO
IB/ IK EMISSION
HOURS LBS.
1.51 0.0003
210.38 0.0011
I3K.35 0.0115
16.84 0.0017
J.1B 0.0002
0.0147
0.0008
1-61
-------
DATE: 7/16/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: LYCOMING
ENGINE DATA **«»»»»«»«»»«**«»«»»<
CAL ID NUMBER: 179 ENGINE TYPE AND MODEL: IO-360-MB6
RATED HORSEPOWER: 200.
ENGINE TOTAL TIME: 663. MRS
FUEL: AV GAS 80/87 FUEL H/C RATIO: 1.840
OPERATIONAL DATA »«»««««'
INLET AIR TEMPFRATURE, DEGREES F: START 89.00 FINISH 89.00
ATMOSPHERIC PRESSURE: START 3C.12 FINISH 30.12
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.02
RELATIVE HUMIDITY: 59.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER:
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLON
LB/HR
IDLE-LOW 1 -0.0 14.10
IDLE/TAXI 2 -0.0 l-i.lO
RUN UP 3 -0.0 34.00
RUN UP-LEAN 4 -0.0 34.00
RUN UP-RICH 5 -0.0 34.00
CLIMB 7 -0.0 79.00
DESCENT 8 -0.0 66.80
APPROACH 9 -0.0 44.50
TAXI 10 -0.0 14.10
TAKE-OFF
TEST
MODE
1
2
3
4
5
7
8
9
10
6
TFST
MODE
i
2
3
4
5
7
B
9
10
6
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
303.00
404.00
717.00
650.00
740.00
1177.00
1155.00
964.00
538.00
1110.00
MASS EMI
CO
LB/1K
LB FUEL
1 182.94
1105.38
1362.15
1335.31
1315.66
1123.16
1114.34
1336.37
I32B.70
1036.20
TIME IN
HOOF.
HIM.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
6
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
96.05
78.83
46.33
51.53
49.38
24.89
23.89
27.20
56.83
29.47
MEASURED
FUEL FLOW
LB/HR
14. 10
96.10
79.00
44.50
14.10
FUEL
-0
CO
I DRY!
PERCENT V
5.30
6.40
11.80
10.10
10.00
10.00
9.80
12.60
8.30
9.00
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
2.82
0.48
6.56
4.45
0.94
15.252
0
CG
2
IDRY)
PERCENT V
3.00
4.50
5.00
4.50
4.70
.60
.60
.00
.70
.10
MASS EMI
C02
LB/IK
LB FUEL
1052.07
1221.19
906.89
914.79
971.58
1341.20
1357.83
999.88
930.66
1465.29
CO
LB/IK
LB FUEL
1105.38
1016.20
1123.16
1336.37
1328.70
96.10
THC
(DRY)
PPMV
7514.00
7969.00
7008.00
6806.00
6553.00
3870.00
3668.00
447R.OO
6198.00
4470.00
MASS EMI
NO
LB/IK
LB FUEL
0.99
1.11
0.28
0.22
0.26
2.12
2.15
0.61
0.37
2.93
LTO CYCLE
CO
LB/IK
HOURS
155K5. B4
99578.21
88729.94
59468.54
18734. 6R
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
136.00 0.04283
144.00 0.05500
321.00 0.08228
324.00 0.07196
329.00 0.07224
1050.00 0.08353
735.00 O.C8250
440.00 O.CB9I8
133.00 0.05960
-0.00 0.08127
NO
IDRY)
PPMV
27.00
39.00
15.00
10.00
12.00
115.00
115.00
35.00
14.00
155.00
MASS EMI
NOX
LB/IK
LB FUEL
0.99
I. 11
0.28
0.22
0.26
2.1?
2.15
0.61
0.37
2.91
EMISSIONS
CO
EMISSION
LBS.
3.117
0.498
7.365
5.947
1.255
18.182
1.192
NO
2
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
en
LD/HR
16679.41
15585.84
46313.20
4540C.62
44732.42
£8729.94
74438.00
59468.54
18734.68
99578.25
HC
LB/IK
LB FUEL
78.83
29.47
24.89
27.20
56.83
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
HC
LB/HK
1354.32
1111.47
1575.30
1752. 18
1678.83
1966.65
1595.67
1210.45
001.24
2832.53
HC
LB/IK
HOURS
1111.47
2832.53
W66.65
1210.45
801.24
ALDEHYDES SMOKE
IDRY)
90.00
53.00
-0.00
-0.00
-0.00
13.00
10.00
5.00
79.00
-0.00
MASS EMI
NQ2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.222
0.014
0.163
0.121
0.054
0.574
0.038
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
14834.22
17218.72
30834.07
31732.71
33033.80
105955.06
90702.69
44494.52
13122.26
140813.88
NO
LB/IK
LB FUEL
1.11
2.93
2.12
0.61
0.37
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
13.96 13.96
15.60 15.60
9.67 9.67
7.38 7.38
3.82 8.82
167.61 167.61
143.48 143.48
27.13 27.13
5.19 5.19
281.69 281.69
NO NO
LP/1K EMISSION
HOURS LBS.
15.60 0.0031
261.69 0.0014
167.61 0.0139
27.13 0.0027
5.19 0.0003
0.0215
0.0014
1-62
-------
D»TE: 7/16/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOHING
ENGINE DMA
C»L 10 NUMBER! ItO
ENGINE TYPE AND MODEL! IO-160-A1B6
RtTED HORSEPOUERt 2CO.
666. MRS
FUEL N/C RATIOI 1.8*0
SERIAL NUNBERI L-T682-5UC
ENGINE TOTAL TIME!
FUEL! AV GAS 80/87
OPERATIONAL DATA »««»««.«««««««.
INLET AIR TEMPERATURE, DEGREES Fl START 89.00 FINISH 89.00
ATMOSPHERIC PRESSURE! START 30.11 FINISH 30.11
INLET AIR HUMIDITY, CRN H20/LB AIR! 0.02
RELATIVE HUMIDITY! 58.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES Cl -0.00, FLOW RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SECl 1.60
NUMBER OF TESTS! 10
COMMENTS:
CARB. TEST ENGINE MEASURED
HEATER MODE RPN FUEL FLOK
LB/HR
IDLE-LOW 1 -0.0 14.10
IDLE/TAXI 2 -0.0 14.10
RUN UP 3 -0.0 34.00
RUN UP-LEAN 4 -0.0 4.00
RUN UP-RICH 5 -0.0 3Z.80
TAKE-OFF 6 -0.0 85.60
CLIMB 7 -0.0 84.40
DESCENT 8 -0.0 66.80
APPROACH 9 -0.0 45.70
TAXI
TEST
MODE
,
Z
)
4
5
6
T
8
9
10
IF.S1
MODE
I
2
3
4
5
6
1
8
9
10
TEST
none
2
6
7
9
10
TOTAL
TOTAL
FXHAUST
GAS
TEMP
DEGREFS f
325.00
US. 00
751.00
695.00
807.00
1121.00
1155.00
1141.00
975.00
516. 00
XASS EMI
CO
LB/1K
L» FUEL
1303.18
1017.27
1300.07
1275.32
1277.77
1020.24
1147.66
1110.96
1103.00
1040.01
TIME IN
MODE
UK.
12.00
0.30
5.00
6.00
4. no
FOR CYCLE
FOR CTCLF/LB
10
EXHAUST
GAS
PRESSURl:
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
-0.00
181.82
40.17
42.98
37.17
16.91
15.43
18.81
27.56
173.31
MEASURED
FUEL FLOW
LB/HR
14.10
85.60
84.40
43.70
12.90
FUEL
-0.
CO
(DRYI
PERCENT V
6.00
6.50
10.80
9.90
10.00
8.20
9.50
9.00
11.10
6.60
MASS EMI
NO 2
LB/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
IBS.
2.82
0.43
7.01
4.57
0.66
15.687
,0
CO
2
IdSYI
PERCENT
3.30
4.20
5.40
5.20
5.30
7.80
7.00
7.10
5.70
4.10
MASS EMI
C02
L6/1K
LB FUEL
1126.34
1048.02
1021.15
1052.51
1064.06
1524.83
1328.69
1377.06
1051.32
1064.66
CO
LB/IK
LB FUtl
1032.27
1020.24
1147.66
1303.00
1040.03
12.90
THC
IORVI
PPMV
V
-0.00
20210.00
5826.00
5826.00
5106.00
2373.00
2230.00
2661.00
4100.00
19203.00
MASS EMI
NO
LB/IK
LB FUEL
0.54
0.42
0.43
0.38
0.42
-0.00
1.94
1.16
-0.00
0.93
ITO CYCLE
CO
LB/1K
HOURS
14555.02
87332.38
96861.94
59547.03
13416.44
MEASURED CALCULATED
AIR FLOW F/A
LR/HR
147.00 0.04396
129.00 0.05990
336.00 0.07873
339.00 0.07361
329.00 0.07418
983.00 0.07528
924.00 0.07785
739.00 0.07614
459.00 0.08064
119.00 0.
NO
IORYI
PPMV
11.00
16.00
22.00
18.00
20.00
-0.00
98.00
57.00
-0.00
36.00
MASS EMI
NOX
LB/IK
LB FUEL
0.54
0.42
0.41
0.38
0.42
-0.00
1.94
1.16
-0.00
0.93
EMISSIONS
CO
EMISSION
LBS.
2.911
0.437
8.040
5.955
0.899
18.241
1.163
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
18377.61
14555.02
44202.31
5101.27
41910.92
87312.38
96861.94
74212.19
59547.0!
11416.44
HC
LB/IK
LB FUEL
183.82
16.91
15.41
27.56
173.31
06034
NO
X
IORVI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
HC
LB/HR
-0.00
2591.86
1365.64
171.93
1225.61
1447.45
1302.21
1256.67
1259.70
2235.67
HC
LB/IK
HOURS
2591.86
1447.45
1102.21
1259.70
2215.67
ALDEHYDES SMOKE
IORYI
53.00
74.00
-0.00
-0.00
-0.00
-0.00
40.00
21.00
10.00
21.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
O.ll
0.0
0.0
0.0
0.0
0.0
0.0
MC
EMISSION
LBS.
0.518
0.007
C.I08
0.126
0.150
0.909
0.058
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
15881.45
I477f.03
34725.91
4210.01
14901.27
130525.19
112141.44
91987.56
48045.24
13734.10
NO
LB/IK
LB FUEL
0.42
-0.00
1.94
-0.00
0.9]
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LO/HR LB/HR
7.55 7.55
5.88 5.88
14.79 14.79
1.52 1.52
11.77 11.77
-0.00 -0.00
164.1} 164.11
77.20 77.20
-0.00 -0.00
12.02 12.02
NO NO
LB/IK EMISSION
HOURS LBS.
5.88 0.0012
-0.00 -0.0000
164.13 0.0136
-0.00 -0.0000
12.02 0.0008
-0.0000
-0.0000
-------
D»TE: 7/30/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: LYCOMING
ENGINE DATA
CAL ID NUMBER: 256 ENGINE TYPE AND MODEL: lo-360-eie
RATED HCRSEPOHER: leo.
ENGINE TOTAL TIME: 1179. HRS
FUEL: av GAS 100/130 FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA »«««««»«««««««««««««««»««
INLET AIR TEMPERATURE, DEGREES F: START 80.00 FINISH 85.00
ATMOSPHERIC PRESSURE: START 30.is FINISH 30.15
INLET AIR HUMIDITY, GRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 40.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN:' 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
ANALYSIS DONE ON FRONT EXHAUST.
SERIAL NUMBER: L-»e35-siAA
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOM
LB/HR
IDLE-LOU 1 -0.0 12.30
IDLE/TAXI 2 -0.0 15.80
RUN UP 3 -0.0 28.10
RUN UP-LEAN 4 -0.0 21.10
RUN UP-RICH 5 -0.0 28.10
TAKE-OFF 6 -0.0 54.50
CLIMB 7 -0.0 43.90
DESCENT 8 -0.0 38.70
APPROACH 9 -0.0 28.10
TAXI
TEST
MODE
,
2
3
4
5
6
7
D
9
10
TEST
MODE
I
2
3
4
b
6
7
a
9
10
TFST
MUDF
2
6
7
q
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
628.00
695.00
1312.00
1300.00
1323.00
1401.00
1435.00
1401.00
1256.00
740.00
MUSS EHI
CO
Lfl/lK
LB FUEL
1028.71
963. 17
555.31
563.32
568.62
951.37
629.3?
528.38
730.56
1055.80
TINF IN
MODE
HIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
124.08
36.80
15.80
14.01
12.57
16.99
12.69
12.78
17.55
49.87
MEASURED
FUEL FLOW
LB/HR
15.80
54.50
43.90
28.10
14.10
FUEL
-0.
CO
(DRY)
PERCENT V
7.70
6.50
3.40
3.50
3.50
6.50
4.00
3.20
4.70
7.10
MASS EHI
NCI 2
LB/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
L3S.
3.16
0.27
3.64
2.81
0.94
IO.B31
.0
CO
2
(DRY)
PERCENT V
5.80
A. 70
8.80
8.90
8.80
7.10
8.70
8.90
8.10
5.90
MASS EMI
C02
LB/1K
LB FUEL
1217.50
1559.93
2258.35
2250.70
2246.33
1632.80
2150.64
2308.99
1978.24
1378.52
CO
LB/1K
LB FUEL
963.17
951.37
629.32
730.56
1055.80
14.10
THC
(DRY)
PPMV
16217.00
4336.00
1689.00
1520.00
1351.00
2027.00
1408.00
1351.00
1971.00
5856.00
MASS EMI
NO
L8/1K
LB FUEL
0.22
0.88
16.82
7.98
8.06
5.27
19.87
24.60
9.88
0.73
LTD CYCLE
CO
LB/IK
HOURS
15218.15
51849.87
27627.01
20528.59
14886.77
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
122.00 0.07073
182.00 0.0634B
373.00 0.05699
279.00 0.05781
372.00 0.05729
639.00 0.06415
572.00 0.05920
516.00 0.05634
354.00 0.06010
155.00 0.
NO
(DRY)
PPMV
10.00
36.00
627.00
302.00
302.00
219.00
769.00
907.00
387.00
30.00
MASS EMI
NOX
LB/IK
LB FUEL
0.22
0.88
16.82
7.93
8.06
5.27
19.87
24.60
9.88
0.73
EMISSIONS
CO
EMISSION
LBS.
3.044
0.259
2.293
2.053
0.997
S.646
0.798
NO
2
(DRY!
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
12653.10
15218.15
15604.71
11886.09
15978.15
51849.87
27627.01
20448.18
20528.59
14886.77
HC
LB/1K
LB FUEL
36.80
16.99
12.69
17.55
49.87
06350
NO
X
IORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
1526.24
581.41
443.97
295.64
353.23
926.05
556.96
494.43
493.05
703.22
HC
LB/1K
HOURS
581.41
926.05
556.96
493.05
703.22
ALDEHYDES
(DRY!
35.00
23.00
-0.00
-0.00
-0.00
-0.00
7.00
11.00
7.00
11.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.1 16
0.005
0.046
0.049
0.047
0.264
0.024
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/H«
14975.20
24646.83
63459.68
47489.70
63121.84
889B7.81
94413.00
89358.00
55588.48
19437.13
NO
LB/IK
LB FUEL
0.88
5.27
19.87
9.88
0.73
PARTICULATFS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LE/HR LB/HR
2.70 2.70
13.84 13.84
472.68 472.68
168.46 168.46
226.46 226.46
286.94 286.94
872.41 872.41
951.99 951.99
277.65 277.65
1C. 33 10.33
NO NO
LB/IK FMISSION
HCURS LBS.
13.84 0.0028
286.94 0.0014
872.41 0.0724
277.65 0.0278
10.33 0.0007
0.1051
0.0097
1-64
-------
0»IEl 7/30/71
TEST ORGANISATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER: LYCOMING
ENGINE DATA
CAl 10 NUMBER! 257 ENGINE TrPE AND MODEL! IO-360-B1E
RATED MORSEPOHER! 180.
ENGINE TOTAL TINEl 1180. HRS
FUEL! AV GAS 100/130 fUEL H/C RATIO! 1.140
OPERATIONAL DATA *»**»*»****»«*
INLET AIR TEMPERATURE, DEGREES ft START 85.00 FINISH 83.00
ATMOSPHERIC PRESSURE! START JO.15 FINISH 30.15
INLET AIR HUMIDITY, GKN H20/L6 AIR! 0.01
RELATIVE HUMIDITY! 38.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES Cl -0.00, FLO* RATE, LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TIME, SEC! , 1.60
NUMBER OF TESTS! 10
COMMENTS:
ANALYSIS DONE ON FRONT EXHAUST.
SERIAL NUMBER! L-4«15-51A8
CARS. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
L8/HR
IDLE-LOU 1 -0.0 12.30
IDLE/TAXI I -0.0 15.80
RUN UP 1 -0.0 29.90
RUN UP-LEAN * -0.0 21.10
RUN UP-RICH 5 -0.0 24.90
TAKE-OFF 6 -0.0 54.50
CLIMB 7 -0.0 43.90
DESCENT 8 -0.0 38. TO
APPROACH 9 -0.0 28.10
TIKI
TEST
MODE
1
2
1
4
5
6
;
8
9
ID
IFST
MODE
1
2
3
4
S
6
7
8
9
10
TEST
none
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
504.00
650.00
1267.00
1300.00
1)12.00
1368.00
1156.00
1323.00
1244.00
785.00
MASS EMI
CO
LB/IK
LB FUEL
7J9.73
842.82
662.44
643.03
670.05
910.02
919.45
857.21
742.58
1182.91
TIMF IN
MODE
MIN.
12.00
0.10
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUIIL
370.24
121.42
18.84
16.28
14.70
18.00
17.5)
17.3?
16.89
106.56
MEASURED
FUEL FLOW
L6/HR
15.80
54.50
43.90
28.10
14.10
FUEL
-0.
CO
(DRV)
PERCENT V
4.90
5.50
4.20
4.10
4.30
6.50
6.10
5.60
4.70
8.90
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
3.16
0.27
3.64
2.BI
0.94
10.831
,0
CO
2
IORYI
PERCENT V
4.20
6.30
8.40
8.60
8.50
7.40
7.10
7.40
7.90
4.90
MASS EMI
C02
L6/1K
LB FUEL
996.24
1516.88
2081.70
2119.25
2081.12
1663.60
1681.49
1779.82
1961.14
1023.28
CO
LB/1K
LB FUEL
842.82
930.02
919.45
742.58
1182.91
14.10
THC
IORYI
PPMV
42822.00
13835.03
2086.00
1812.00
1647.00
2196.00
2031.00
1976.00
1867.00
13999.00
MASS EMI
NO
LB/IK
LB FUEL
0.42
1.11
11.81
6.11
5.76
5.76
6.56
7.90
9.65
0.2?
LTD CYCLE
CO
LB/IK
HOURS
13316.52
50686.14
40363.69
20866.39
16679.00
MEASURED CALCULATED
AIR FLOU F/»
LB/HR
96.00 0.06297
170.00 0.06147
383. OC 0.05914
273.00 0.05942
384.00 0.05983
643.00 0.06554
521.00 0.06229
469.00 0.06124
353.00 0.05918
132.00 0.
NO
IDRYI
PPMV
17.00
44.00
456.00
237.00
225. 00
245.00
265.00
314.00
372.00
10.00
MASS EMI
N0>
LB/IK
LB FUEL
0.42
1.11
11. 81
6.11
5.76
5.76
6.56
7.90
9.65
0.22
EMISSIONS
CO
EMISSION
LBS.
2.661
0.253
3.350
2.087
1.117
9.471
0.874
NO
2
IORVI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
-0.00
MASS EMI
CO
LB/HR
9098.62
13316.52
19807.08
13567.86
20034.50
50686.14
40363.69
33174.61
20866.39
16679.00
HC
LB/IK
Lfl FUEL
121.42
18.00
17.53
16.89
106.56
07141
NO
X
(ORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
4553.98
1918.46
563.42
343.42
439.49
9UO.T4
769.69
670.42
474.72
1502.53
HC
LB/IK
HOURS
1918.46
980.74
769.69
474.72
1502.53
ALDEHYDES
(DRY)
28.00
24.00
-0.00
-0.00
-0.00
-0.00
7.00
5.00
6.00
in. oo
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.384
0.005
0.064
0.047
0.101
0.601
0.055
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
12253.69
23966.63
62242.77
44716.15
62225.37
90666.25
73817.19
68879.13
55108.03
14428.23
NO
LB/IK
LB FUEL
1.11
5.76
6.56
9.65
0.22
P ARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MASS EMI MASS EMI
NO NO I
LB/HR LB/HR
5. IB 5.18
17.50 17.50
353.23 353.23
128.82 128. B2
172.19 172.19
313.81 313.81
2B8.02 288.02
305.54 305.54
271.28 271.28
3.08 3.08
NO NO
LB/IK EMISSION
HCURS LBS.
17.50 0.0035
313.81 0.0016
288.02 0.0239
271.28 0.0271
3.08 0.0002
0.0563
0.0052
1-65
-------
DATE: 7/30/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: LYCONING
ENGINE DATA
CAL ID NUMBER 1 258 ENGINE TYPE AND MODEL: IO-360-B1E
RATED HORSEPOMER: 180.
ENGINE TOTAL TINE: 1100. MRS
FUEL: AV GAS 100/130 FUEL H/C RATIO: 1.8*0
OPF.RATIONAL DATA «»»««»«»«»»
INLET AIR TEMPERATURE. DEGREES F: START 84.00 FINISH 85.00
ATMOSPHERIC PRESSURE: START 30.15 FINISH 30.15
INLET AIR HUMIDITY, GRN H20/L8 AIR: 0.01
RELATIVE HUMIDITY: 36.00 PERCENT
SAMPLE LINE: TEMPERATUREf DEGREES C: -0.00, FLOW RATE, LITERS/MIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
ANALYSIS DONE ON REAR EXHAUST.
SERIAL NUMBER: L-4835-ilAC
CARB. TEST ENGINE MEASURED
HEATER MODE RPN FUEL FLOU
LB/HR
IDLE-LOW 1 -0.0 12.30
IDLE/TAXI 2 -0.0 14.10
RUN UP 3 -0.0 29.90
RUN UP-LEAN 4 -0.0 19.30
RUN UP-RICH 5 -0.0 28.10
TAKF-OFF 6 -0.0 56.30
CLIMB 7 -0.0 41.90
DESCENT 3 -0.0 38. TO
APPROACH 9 -0.0 28.10
TAXI
TEST
MdDE
,
2
1
4
5
6
7
a
9
10
TES1
NODE
1
2
1
4
5
6
7
a
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
FXHAUST
GAS
TEMP
DEGREES F
594.00
650.00
1166.00
1143.00
1188.00
1345.00
1267.00
1222.00
1121.00
762.00
MAIS EMI
CO
LB/IK
LB FUEL
1031.89
1048.35
914.65
918.32
918.32
1001 .04
1035.90
1037.10
1057.95
1187.41
TIME IN
MODE
XIN.
12.110
0.30
5. no
6.00
4.00
FOR CYCLF.
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
277.76
92.30
22.05
18.93
18.93
18.70
19.91
19.29
22.02
175.51
MEASURED
FUEL FLOM
LB/HR
14.10
56.30
43.90
28.10
14.10
FUEL
-0
CO
(DRY)
PERCENT V
8.20
7.50
6.00
6.10
6.10
6.90
7.20
7.10
7.10
9.70
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
o.o
0.0
FUEL
USED
LHS.
2.82
0.28
3.64
2.81
0.94
10.500
0
CO
2
IORYI
PERCENT
4.00
5.80
7.00
7.10
7.10
6.80
6.60
6.50
6.20
4.30
MASS EMI
C02
LB/IK
LB FUEL
790.89
1273.84
1676.64
1679.42
1674.42
1550.07
1492.00
1491.81
1451.56
£27.06
CO
LB/IK
LB FUEL
1049.35
1001.04
1035.90
1057.95
1187.41
14.10
THC
(DRY)
PPMV
V
38540.00
11529.00
2525.00
2196.00
2196.00
2251.00
2416.00
2306.00
2580.00
25034.00
MASS EMI
NO
LA/IK
LB FUEL
0.10
0.62
4.26
2.40
2.40
3.79
3.40
3.60
2. 84
0.12
LTD CYCLE
CO
LB/IK
HOURS
14781.80
56358.69
45475.98
29728.33
16742.45
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
95.00 0.07571
144.00 0.06759
354.00 0.06161
229.00 0.06236
333.00 0.06236
648.00 0.06482
499.00 0.06543
440.00 0.06447
316.00 0.0632B
119.00 0.
NO
IDRYI
PPMV
5.00
27.00
170.00
97.00
97.00
159.00
144.00
150.00
116.00
6.00
MASS EMI
NDI
LB/IK
LB FUEL
0.10
0.62
4.26
2.40
2.40
3.79
3.40
3.60
2.84
0.12
EMISSIONS
CO
EMISSION
LBS.
2.956
0.282
3.775
2.971
1.122
11.107
1.051
NO
2
IORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
MASS EMI
CO
L8/HR
12692.21
14781.80
27346.05
17723.48
25804.67
56358.69
45475.98
40135.62
29728.33
16742.45
HC
LB/IK
LB FUEL
92.30
18.70
19.91
22.02
175.51
07777
NO
X
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
3416.49
1301.38
659.15
365.42
532.04
1053.01
873.96
746.58
618.70
2474.70
HC
L8/1K
HOURS
1301 .38
1053.01
873.96
618.70
2474.70
ALDEHYDES SMOKE
(DRY)
26.00
31.00
-0.00
-0.00
-0.00
-0.00
11.00
7.00
11.00
30.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.260
0.005
0.073
0.062
0.166
0.566
0.054
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.10
-0.00
-0.00
-0.00
MASS EMI
CO?
LB/HR
9727.96
17961.06
50131.57
32412.75
47191.62
87268.75
65498.59
57732.91
40788.94
11661.49
NO
L8/1K
LB FUEL
0.62
3.79
3.40
2.84
0.12
PART1CULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
1.27 1.27
8.74 8.74
127.28 127.23
46.29 46.29
67.40 67.40
213.32 213.32
149.39 149.39
139.28 139.28
79.78 79.78
1.70 1.70
NO KG
LO/1K EMISSION
HOURS LBS.
.74 0.0017
21 .32 O.Onil
14 .39 0.0124
7 .78 0.0080
.70 0.0001
0.0233
0.0022
1-66
-------
DATE: 7/16/71
TEST ORGANISATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER I TELEOYNE-CCNTINENTAL
ENGINE OAIA
CAL 10 NUMBER I 196 ENGINE TYPE AND MODEL I 10-360-C
RATED HORSEPOMERl 210.
ENGINE TOTAL TINE: 169. MRS
FUEL: AV GAS 100/130 FUEL H/C RATIOl 1.8*0
OPERATIONAL DATA »»*»»««.««««<
INLET AIR TEMPERATURE, DEGREES fs START 90.00 FINISH 88.00
ATMOSPHERIC PRESSURE: START 30.14 FINISH 30.1*
INLET AIR HUNIOITY, CRN H2Q/LB AIR: 0.01
RELATIVE HUMIDITY: 51.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -O.OC, FLO* RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIKE, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER: F/5163*-70CA
CARB. TEST ENGINE MEASURED
HEATER roof RPM FUEL FLOM
LB/HR
IDLE-LOU 1 -0.0 16.40
IDLE/TAXI 2 -0.0 22.30
RUN UP 3 -0.0 23.40
RUN UP-LFAN * -0.0 19.90
RUN UP-RICH 5 -0.0 22.30
TAKE-OFF 6 -0.0 109.00
CLIMB 7 -0.0 73.80
DESCENT 8 -0.0 56.30
APPROACH 9 -0.0 41.00
TAXI
TEST
MODE
1
2
1
4
5
6
7
a
9
10
TESI
MODE
1
2
3
10
fESl
1UDE
}
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
44H.OO
471.00
852.00
740. On
874.00
1222.00
1323.00
1256.00
1143.00
460.00
(ASS EMI
CO
LB/1K
LH FUEL
604.84
542.5*
938.12
088.00
883.27
1001.35
1039.68
1085.87
1094.7*
485.83
THE IN
MOOE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FCR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
339.87
307.11
54.56
62.82
57.12
43.77
19.66
19. OH
27.16
456.93
MEASURED
FUEL FLI1U
LB/HR
22.30
109.00
73.80
41.00
23.40
FUEL
-0
CO
(DRY)
PERCENT V
3.90
3.4n
7.70
6.60
6.90
8.50
8.90
9.40
9.60
3.10
MASS EHI
N02
LB/1K
L8 FUF.L
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
4.46
0.54
6.13
4.10
1.57
16.798
0
CO
2
IOHYI
PERCENT V
5.30
5.90
8.10
7.60
8.10
8.00
8.10
7.80
7.70
*.70
MASS EMI
C02
LB/1K
LB FUEL
1291. 49
1*79.25
1550.57
1606.66
1629.17
1*80.80
1*86.73
1415.74
1379.65
1157.34
CO
LB/1K
LB FUEL
5*2.5*
1001.35
1039.68
109*. 7*
485.83
23.40
THC
(DRY)
PPMV
38264.00
33605.00
7BI9.00
8152.00
7819.00
6*88.00
2939.00
288*. 00
4159.00
50907.00
MASS EMI
NO
LB/1K
LB FUEL
0.28
0.52
2.68
1.72
2.06
-0.00
4.37
3.97
3.91
0.36
LTD CYCLE
CO
LB/IK
HOURS
12098.58
1091*7.38
76728.19
4*88*. 21
11368. *8
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
1*5.00 0.06097
212.00 0.05909
266.00 0.07676
228.00 0.0696*
257.00 0.0730*
1221.00 0.079*5
839.00 0.08010
630.00 0.08112
453.00 0.08222
182.
NO
IORVI
PPMV
11.00
20.00
134.00
7B.OO
98.00
-0.00
228.00
209.00
209.00
14.00
MASS EHI
NOX
LB/1K
LB FUEL
0.28
0.52
2.68
1.72
2.06
-D.OO
4.37
3.97
3.91
0.36
EMISSIONS
CO
EMISSION
LBS.
2.420
0.5*6
6.368
4.488
0.762
14.584
0.868
00 0
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
9919.40
12098.58
21951.99
17671.25
19696.82
109147.38
76728.19
61134.72
4*38*. 21
11368.48
HC
LB/IK
LB FUEL
307.11
43.77
19.66
27.16
456.93
060*8
NO
X
IDRVI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
5573.87
68*8.65
1276.67
1250.07
1278.33
*77l.*5
1451.1*
1074.24
1113.67
1C692.12
HC
LB/1K
HOURS
68*8.65
*77l.*5
1451.14
1113.67
10692.12
ALDEHYDES SMOKE
IORY)
51.00
-0.00
-0.00
-0.00
-0.00
-0.00
18.00
16.00
13.00
24.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
1.370
0.024
0.120
0.111
0.716
2.342
0.139
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/KR
21180.45
32987.23
36283.26
31972.41
36330. *0
161*07.13
109720.63
79706.31
56565. *6
27081.77
NO
LB/1K
LB FUEL
0.52
-0.00
4.37
3.91
0.36
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
4.60 4.60
11.69 11.69
62.75 62.75
34.30 3*. 30
45.95 45.95
-0.00 -0.00
322.86 322.86
223.27 223.27
160.51 160.51
8.43 8.43
Nn NO
LB/IK EMISSION
HOURS LAS.
11.69 0.0023
-0.00 -0.0000
322.86 0.0268
160.51 0.0161
B.43 0.0006
-0.0000
-0.0000
1-67
-------
01TE: T/16/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEDYNE-CONTINENTAL
ENGINE DATA
CAL 10 NUMBER: 197 ENGINE TYPE AND MODEL: IO-36O-C
RATED HURSEPOHER: 210.
ENGINE TOTAL TIME: 169. MRS
FUEL: AV GAS 100/130 FUEL H/C RATIO: i.a»o
OPERATIONAL DATA ««»«»»««»..«.......».«».«..»...«.......«.».»«»...
INLET AIR TEMPERATURE, DECREES f: START 88.00 FINISH 86.00
ATMOSPHERIC PRESSURE: START 30.13 FINISH 30.13
INLET AIR HUMIDITY, CRN H20/L8 AIR: 0.01
RELATIVE HUMIDITY: 52.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOW RATE, LITERS/HIM 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER: F/5163*-70CS
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL Ft DM
LB/HR
IDLE-LOW 1 -0.0 18.60
IDLE/TAXI 2 -0.0 22.30
RUN UP 3 -0.0 24.60
RUN UP-LFAN 4 -0.0 19.90
RUN UP-RICH 5 -0.0 22.30
TAKE-OFF 6 -0.0 106.70
CLIMB 7 -0.0 7B.SO
DESCENT 8 -0.0 59.80
APPROACH 9 -0.0 38.70
TAXI
TEST
MODE
1
2
3
4
5
6
7
8
9
10
IFSf
MODE
I
2
3
4
5
6
7
B
9
10
TEST
HOOF
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGRFES F
269.00
34B.OO
740.00
690.00
785.00
1244.00
1334.00
1233.00
1C99.00
349.00
14SS EMI
CO
LR/1K
LA FUEL
541.41
512.98
755.96
aio.ei
805.68
978.09
1004.63
1083.60
1110.51
487.65
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOB CYCLE
FOP CYCLE/LB
10
EXHAUST
GAS
PRFSSUDE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
600.44
521.80
51.45
50.75
49.60
29.94
19.66
20.29
39.19
467.54
MEASUHEO
FUEL FLOH
LR/HH
22.30
106.70
78.50
38.70
24.60
FUEL
-0.
CO
(DRY)
PERCENT V
3.90
3.70
5.60
6.80
6.50
8.30
8. 60
9.50
9.90
3.20
MASS EMI
NC12
L8/1K
LB FUFL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
L9S.
4.46
0.53
6.52
3.87
1.65
17.027
,0
CO
2
(DRY)
PERCENT V
3.00
4.30
8.70
9.40
9.10
8.40
8.40
7.90
7.50
4.70
MASS EMI
C02
LB/1K
LB FUEL
654.36
936.71
1845.31
1761.06
1772.26
1555.31
1541.79
1415.91
1321.87
1125.37
CO
LB/IK
LB FUEL
512.98
978.09
1004.63
II 10.51
487.65
24.60
THC
IDKY)
PPMV
76527.00
65714.00
6655.00
7431.00
6987.00
4436.00
2939.00
3105.00
MOO. 00
53569.00
MASS EMI
NO
Lfl/lK
LB FUEL
0.11
0.32
1.97
3.27
2.79
4.61
4.47
3.45
3.02
0.35
LTD CYCLE
cn
LB/IK
HOURS
11439.49
104361.94
78863.63
42976.82
11996.22
MEASURED CALCULATED
AIR FLOH F/A
LB/HR
103.00 0.06883
151.00 0.06851
298.00 0.06904
217.00 0.07796
265.00 0.07508
1227.00 0.07928
904.00 0.07998
668.00 0.08212
41S.OO 0.08367
I8S.OO 0.
NO
(DRY)
PPMV
5.00
14.00
89.00
167.00
137.00
238.00
233.00
184.00
164.00
14.00
MASS EMI
NOX
LB/IK
LB FUEL
0.11
0.32
1.97
3.27
2.79
4.61
4.47
3.45
3.02
0.35
EMISSIONS
CO
EMISSION
LBS.
2.288
0.522
6.546
4.293
0.804
14.457
0.849
NO
2
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
10178.42
11439.49
18596.60
16135.05
17966.63
104361.94
78863.63
64803.08
42976.82
11996.22
HC
LB/IK
LB FUEL
521.80
29.94
19.66
39.19
467.54
,06220
NU
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
11418. 6T
11636.12
1265.72
1009.84
1106.09
3194.49
1543.56
1213.05
1516.61
11501.46
HC
LB/IK
HOURS
11636.12
3194.49
1543.56
1516.61
11501.48
ALDEHYDES SMOKE
IDHY)
10.00
31.00
-0.00
-0.00
-0.00
-o.on
14.00
7.00
12.00
21.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
o.n
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
2.327
0.016
0.128
0. 152
0.771
3.394
O.l«9
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/HR
12302.00
20688.71
45394. 48
35045.15
39521.47
165951.63
121030.75
84671.50
51155.22
27684.13
NO
LB/IK
LB FUEL
0.32
4.61
4.47
3.02
0.35
PAKTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/t-R
2.14 2.14
7.11 7.11
48.55 48.55
65.09 65.09
62.20 62.20
491.54 491.54
350.96 350.96
206.16 206.16
116.94 116.94
8.62 8.62
NO NO
LB/IK EMISSION
HOUKS LBS.
7.11 0.0014
491.54 0.0025
350.96 0.0291
116.94 0.0117
6.62 0.0006
0.0453
0.0027
1-68
-------
DITEl 7/16/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEDVNE-CONTINENTAL
ENGINE DATA
CAL ID NUMBER" 14B ENGINE TYPE AND MODEL 1 IO-36O-C
RATED HORSEPOWER! 210.
ENGINE TOTAL TIME! 170. HRS
FUEL: AV G»S 100/130 FUEL N/C RATIOI 1.840
OPERATIONAL D»T» »»«**»*
INLET AIR TEMPERATURE, DEGREES F! START 14.00 FINISH 94.00
ATMOSPHERIC PRESSUREi START 10.12 FINISH 30.12
INLET AIR HUNIOITT. GRN H20/LB AIR! 0.02
RELATIVE HUMIDITY! 46.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES C: -0.00, FLOW RATE! LITERS/MINI
SAMPLE LIKE TRANSPORT TIME, SECl 1.60
NUMBER OF TESTS! 10
COMMENTS!
SERIAL NUMBER! F/31614-70CC
CARB. TFST ENGINE MEASURED
HEATER NODE RPM FUEL FLOH
LB/HR
IOLE-LOH -0.0 12.90
IDLE/TAXI -0.0 16.40
RUN UP -0.0 24.60
RUN UP-LEAN -0.0 21.10
RUN UP-RICH -0.0 21.40
TAKE-OFF -0.0 109.00
CLIMB 7 -0.0 77.40
DESCENT 6 -0.0 59. BO
APPROACH 9 -0.0 39.60
TAXI
TEST
MODE
1
2
3
4
5
6
7
a
9
10
TES!
MODE
,
2
3
4
5
A
7
8
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TFMP
DEGREES f
381.00
448.00
773.00
729.00
B07.00
1155.00
1312.00
1222.00
1099.00
482.00
MJSS EMI
CO
LB/1K
Lfl FUEL
931.96
497.97
771.01
851.87
944.90
1097.89
488.96
1092.11
1049.07
482. 17
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOB CYCLE/LB
10
EXHAUfiT
GAS
PRESSURE
PSIA
-0.00
-0.0(1
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS [HI
HC
LB/IK
LB FUEL
278. 52
267.09
26.91
30.59
29.58
23.
-------
DATE: 91/77/10
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEOYNE-CONTINENTAL
ENGINE DATA
CAL ID NUMBER: 161 ENGINE TYPE AND MODEL I 10-360-C
BATED HORSEPOKER: 210.
ENGINE TOTAL TIME: 700. MRS
FUEL: AV GAS 100/130 FUEL M/C RATIO: 1.8*0
OPERATIONAL DATA ».»«««»»»«««»««»«
INLET AIR TEMPERATUREi DEGREES f. START 76.00 FINISH 79.00
ATMOSPHERIC PRESSURE: START 30.23 FINISH 30.23
INLET AIR HUMIDITY, CRN H20/LB AIR: 162.00
RELATIVE HUMIDITY: ai.oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -O.CO. FLDN RATE, LITERS/HIM: 7.On
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER Of TESTS: 10
COMMENTS:
SERIAL NUMBERI SOS9-6-C
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOU 1 -0.0 17.60
IDLE/TAXI 2 -0.0 18. BO
RUN UP 3 -0.0 22.30
RUN UP-LEAN 4 -0.0 19.90
RUN UP-RICH 5 -0.0 16.40
TAKF-QFF 6 -0.0 99.60
CLIMB 7 -0.0 70.30
DESCENT 8 -0.0 44.50
APPROACH 9 -0.0 23.40
TAXI
TEST
NODE
1
2
3
4
5
6
7
a
9
10
TEST
MODE
,
2
J
4
5
6
7
8
9
10
TEST
MUflE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
751.00
762.00
874.00
B74.00
BB6.00
1155.00
1177.00
1043.00
B63.00
62B.OO
MASS EMI
CD
LB/IK
LB FUEL
399.56
457.79
604.53
419.29
500.21
95B.95
736.86
B26.93
685.77
451. 14
TINF IN
MODE
HIM.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
70.05
38.88
17.38
16.40
11.11
31.15
14.68
16.08
22.41
180.93
MEASURED
FUEL FLOW
LB/HR
18. BO
99.60
70.30
23.40
17.60
FUEL
-0.
CO
(DRY)
PERCENT V
2.80
3.40
4.80
3.20
3.90
8.00
5. DO
6.60
5.40
1.60
MASS FM1
N02
LB/IK
LB FUEL
0.0
o.n
0.0
0.0
0.0
o.o
0.0
0.0
o.o
0.0
FUEL
USED
LflS.
3.76
0.50
5.83
2.34
1.18
13.612
.0
CO
2
IDRYI
PERCENT V
10.50
11.10
11.00
12.00
11.70
8.40
9.90
9.30
10.20
10.00
MASS EM
CD2
LB/IK
LB FUEL
2154.26
214B.2K
2176.73
2470.47
2157.81
1582.05
1976.20
1830.83
2035.27
1969.02
CO
LB/IK
LB FUEL
457.79
958.95
736.86
685.77
451.14
17.60
THC
IORYI
PPMV
8571.00
5042.00
2409.00
2185.00
1513.00
4538.00
2017.00
2241.00
1081.00
25209.00
MASS EH1
NO
LB/IK
LB FUEL
1.13
1.90
5.52
4.52
3.52
15.26
12.94
8.25
5.97
1.38
LTO CYCLE
CO
L6/1K
HOURS
8606.47
95510.94
51801.38
16046.96
7940.13
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
236.00 0.06472
252.00 0.06843
291.00 0.07323
273.00 0.07004
221.00 0. 071*6
1159.00 0.07793
885.00 0.07298
546.00 0.07472
299.00 0.07290
201.00 0.
NO
(DRY!
PPMV
48.00
86.00
267.00
210.00
167.00
775.00
620.00
401.00
286.00
67.00
MASS EMI
nox
LB/IK
LB FUtL
1.11
1.90
5.52
4.52
3.52
15.26
12.94
B.25
5.97
1.38
EMISSIONS
CO
EMISSION
LBS.
1.721
0.47B
4.300
1.605
0.532
8.635
0.634
NO
2
IDRYI
PPMV
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
7032.30
8606.47
134B0.90
8343.77
8203.39
955IC.94
51801.38
36798.50
16046.96
7940.13
HC
L8/1K
LB FUEL
18.88
31. 15
14.68
22.41
1BC.93
07389
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LD/HR
1232.87
730.96
1B7.49
126.29
182.27
3102.94
1031.73
715.61
524.37
3184.39
HC
IB/IK
HOURS
730.96
3102.94
1031.73
524.37
3184.39
ALDEHYDES SMOKE
IDRY)
26.00
20.00
^0.00
-0.00
-0.00
-0.00
7.00
10.00
B.OO
27.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.146
0.016
0.086
0.052
0.211
0.511
0.038
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS E;U
CO 2
LB/HR
41435.01
44147.67
48540. 9B
49162.27
38668.13
157572.50
138927.06
81471.81
47625.21
34654.83
NO
LB/IK
LB FUEL
1.90
15.26
12.94
5.97
1.33
PARFICULATES
-0.00
-0.00
-n.oo
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
MASS em MASS EMI
NO NO I
LB/MR LB/HR
19. tO 19.80
35.76 35.76
123.17 123.17
89.94 89.94
57.70 57.70
1519.80 1519.80
909.55 909.55
367.24 167.24
139.60 139.60
24.27 24.27
NO NO
LB/IK EMISSION
HOURS LBS.
35.76 0.0072
1519.80 0.0076
909.55 0.0755
119.60 0.0140
24.27 0.0016
0.1058
0.0078
1-70
-------
DATE: 8/17/61
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEDYNE-CONTINENTAL
ENGINE 0»I»
CAL 10 NUMBER! )62 ENGINE TTPE AND MODELI IO-360-C
RATED HORSEPOUERl 210.
ENGINE TOTAL TIMEl TOO. MRS
FUEL! »V GAS 100/130 FUEL H/C RATIOl 1.840
OPERATIONAL OAT A »««»»»»»«»«»
INLET AIR TEMPERATURE, DEGREES Ft START T9.00 FINISH 80.00
ATMOSPHERIC PRESSUREi START 30.2* FINISH 30.2*
INLET AIR HUMIDITY, CRN H20/LB AIRl 0.02
RELATIVE HUNIOITVi 75.00 PERCENT
SAMPLE LINEl TEMPERATURE, DEGREES C: -0.00, FLOW RATEi LITERS/MIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER Of TESTSl 10
COMMENTS:
SERIAL NUMBERI 50591-6CA
CARB. TEST ENGINE MEASURED
HEATER NDOE RPM FUEL FLOW
LB/HR
IDLE-LOU 1 -0.0 21.10
IDLE/TAXI I -0.0 19.40
RUN UP 3 -0.0 22.30
RUN UP-LEAN * -0.0 19.90
RUN UP-RICH 5 -0.0 18. 80
TAKE-OFF 6 -0.0 93. BO
CLIMB 7 -0.0 63.30
DESCENT 8 -0.0 41.00
APPROACH 9 -0.0 27.00
TAX
TEST
MODE
1
9
10
TEST
MODE
I
2
'
*
s
6
7
a
9
10
FES!
MORE
2
h
1
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
560.00
605.00
810.00
785.00
052.00
1155.00
1211.00
1076.00
919.00
673.00
MASS EMI
CO
LB/IK
LB FUEL
352.98
*70.00
581.42
485.05
502.99
912. 15
643.86
787.74
744.06
496.55
TIME IN
MODE
MIN.
12.00
0.30
1.00
6.00
4.00
FOR CYCLE
FOR CYCLF./L8
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
1 6/1*
LB FUEL
146.22
88.24
21.83
14.98
12.52
29.71
13.90
18.05
30.80
145.88
MEASURED
FUEL FLO*
LB/HR
19.90
93.80
63.30
27.00
19.90
FUEL
-0
CO
IDRVI
PERCENT V
2.30
3.40
4.40
3.60
3.70
7.60
5.00
6.10
5.60
3.60
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
3.98
0.47
5.25
2.70
1.33
13.736
0
CO
2
(DRY)
PERCENT V
9.20
10.10
10.60
11.20
11.00
8.80
10.50
9.30
9.20
9.20
MASS EMI
C02
LB/IK
L3 FUEL
2218.47
2193.69
2200.82
2371.03
2349.58
1659.49
2124.46
1887.01
1920.65
1993.84
CO
LB/IK
LB FUFL
470.00
91Z.15
643.86
744.06
496.55
19.90
THC
IORYI
PPNV
16636.00
11146.00
2884.00
1941.00
1608.00
4325.00
1885.00
2440.00
4048.00
18466.00
MASS EMI
NO
LB/IK
LB FUEL
2.12
1.79
5.84
3.61
3.42
6.62
16.73
9.67
5.87
1.27
LTO CYCLE
CO
LO/1K
HOURS
9352.91
SS559.69
40756.21
20089.66
9881.44
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
257.00 0.06052
250.00 0.06695
292.00 0.06991
269.00 0.06836
252.00 0.06782
1110.00 0.07768
82.00 0.07179
509.00 0.07199
335.00 0.06999
234.00 0.
NO
IORY)
PPMV
84.00
79.00
269.00
163.00
153.00
336.01)
791.00
456.00
269.00
56.00
MASS EMI
NOX
LB/IK
LB FUEL
2.12
1.79
5.84
3.61
3.42
6.62
16.73
4.67
5.87
1.27
EMISSIONS
CO
EMISSION
LBS.
1.871
0.429
3.383
2.009
0.662
8.352
0.608
NO
2
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-C.OO
-0.00
-C.OO
-0.00
-0.00
MASS EMI
CO
LB/HR
7447.95
9352.91
12965.73
9652.43
9456.25
85559.69
40756.21
32297.39
20089.66
9881.44
HC
LB/IK
L6 FUEL
88.24
29.73
13.90
30.80
145.88
06737
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
3085.34
1756.03
486.73
248.06
235.37
2788.61
880.00
739.40
831.71
2902.93
HC
LB/IK
HOURS
1756.03
2788.61
880.00
831.71
2902.93
ALDEHYDES SMOKE
IDRYI
46.00
30.00
-0.00
-0.00
-0.00
-0.00
13.00
11.00
10.00
29.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.351
0.014
0.073
0.083
0.194
0.716
0.052
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO?
LB/HR
46809.66
4J654.36
49078.20
47183.55
44172.10
155659.81
134477.94
77367.56
51857.42
39677.47
NO
LB/IK
L8 FUEL
1.79
6.F.2
16.73
5.B7
1.27
PARTICUI ATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LR/HR
44.68 44.68
35.70 35.70
130.20 130.20
71. 79 71.79
64.23 64.23
621.32 621.32
1059.06 1C59.06
346.57 396.57
158.51 158.51
25.25 25.25
NO NO
LB/IK EMISSION
HOURS LBS.
35.70 0.0071
621.32 0.0031
1059.06 0.0879
15U.51 0.0159
25.25 0.0017
0.1157
0.0084
1-71
-------
DATE: 8/17/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEOTNE-CONTINENTAL
ENGINE DATA
CAL 10 NUMBER! 36* ENGINE TYPE AND NOOELl IO-36O-C
RATED HORSEPOWER: 210.
ENGINE TOTAL TINEl 700. MRS
FUEL: AV GAS 100/130 FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA *»*<
INLET AIR TEMPERATURE, DEGREES F: START 78.00 FINISH 78.00
ATMOSPHERIC PRESSURE: START 30.21 FINISH 30.21
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.02
RELATIVE HUMIDITY: 79.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/HIM:
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER! 50S91-6-CC
CARB. TEST ENGINE MEASURED
HEATER MDDE RPM FUEL FLOW
LB/HR
IDLE-LOU 1 -0.0 15.20
IDLE/TAXI 2 -0.0 16.40
RUN UP 3 -0.0 25.80
RUN UP-LEAN 4 -0.0 24.60
RUN UP-RICH 5 -0.0 22.30
TAKE-OFF 6 -0.0 93.80
CLIMB 7 -0.0 64.50
DESCENT 8 -0.0 45.70
APPROACH 9 -0.0 25.80
TAXI
TEST
MODE
,
2
3
4
5
6
7
8
9
10
TFST
MODE
1
2
3
4
5
6
7
1
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
FXHAUST
GAS
TEMP
DEGREES F
617.00
673.00
975.00
953.00
998.00
1312.00
1390.00
127S.OO
942.00
B07.00
«»SS EMI
cn
LB/IK
LB FUEL
554. 97
67?. 88
862.43
835.06
781.92
rot. 71
630.46
738.99
601.19
512.60
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
HOH CYCLE
FOR CYCLF/lfl
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
244.67
131.66
25.11
33.09
19.71
28.94
16.02
0.19
21.53
85.47
MEASURED
FUEL FLOW
LB/HR
16.40
93.80
64.50
25.80
18.80
FUEL
-0.
CO
(ORYI
PERCENT V
4.50
5.60
7.20
6.90
6.30
5.70
5.00
6.00
4.70
4.00
MASS FMI
NI12
LB/IK
LB FUFL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
3.28
0.47
5.35
2.58
1.26
12.942
.0
CO
2
(DRY)
PERCENT V
8.90
9.30
9.30
9.30
9.70
10.30
10.80
10.40
10.80
10.60
HASS EMI
C02
LB/IK
LB FUEL
1662.44
1755.79
1750.29
1770.14
1891.60
1992.32
>I39.70
2012.61
2170.57
2134.35
CO
LB/IK
LB FUEL
672.88
701.71
630.46
601.19
512.60
18.80
THC
(DRY)
PPMV
35935.00
19132.00
3660.00
4769.00
2773.00
4104.00
2218.00
26.60
2939.00
11645.00
MASS EMI
NO
LB/1K
LB FUEL
0.43
0.75
2.70
1.50
2.20
18.52
13.98
8.78
8.30
1.31
LTD CYCLE
CO
LB/IK
HOURS
11035.27
65820.31
40664.91
15510.64
9636.94
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
157.00 O.CT829
185. 00 0.07736
311.00 0.07765
299.00 0.07677
276.00 0.07478
1185.00 0.07518
838.00 0.07321
577.00 0.07512
337.00 0.07216
233.00 0.
NO
IORY)
PPMV
22.00
38.00
137.00
80.00
108.00
916.00
675.00
434.00
395.00
62.00
MASS EMI
NOX
LB/IK
LB FUEL
0.43
0.75
2.70
1.59
2.20
18.52
13.98
8.78
8.30
1.31
EMISSIONS
CO
EMISSION
LBS.
2.207
0.329
3.375
1.551
0.646
8. 108
0.626
NO
2
ICRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
Lb/HR
8131.58
11035.27
22250.59
20562.24
17436.70
65820.31
40664.91
33771.85
15510.64
9636.94
HC
LB/IK
LB FUEL
131.66
2H.94
16.02
21.53
85.47
07207
NO
X
IORVI
PPNV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EH1
HC
LB/HR
3718.99
2159.24
647.79
813.94
439.56
2714.18
1033.13
B. 57
555.49
1606.81
HC
LB/IK
HOURS
2159.24
2714.18
1033.13
555.49
1606.81
ALDEHYDES SMOKE
(DRY)
40.00
28.00
-0.00
-0.00
-0.00
-0.00
20.00
10.00
22.00
27.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.432
0.014
0.086
0.056
0.108
0.694
0.054
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/HR
25269.15
28794.93
45157.55
43545.42
42182.66
186879.06
138010.50
91976.13
56000.78
40125.76
NO
LB/IK
LB FUEL
C.75
18.52
13.98
8.30
1.31
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS PHI MASS FMI
NO NOX
LP/HR L8/HR
6.53 6.53
12.30 12.30
69.54 69.54
39.16 39.16
49.10 49.10
1737.40 1737.40
901.73 901.73
401.25 401.25
214.12 214.12
24.54 24.54
NO NO
LB/IK FHISS1CN
HOURS LBS.
12.30 0.0025
1737.40 0.0087
901.73 0.0748
214.12 0.0214
24.54 0.0016
0.1090
0.0084
1-72
-------
OATEl B/IT/Tt
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEOVNE-CONTINENTAL
ENGINE DATA
SERIAL NUMBERI M4S1-4-D
CAL ID NUNBERI >H ENGINE TYPE AND MODEL I 10-160-C
RATED HORSEPOMERI 110.
ENGINE TOTAL TIMEl TOO. MRS
fUELl »V GAS 100/110 FUfL M/C RATIOI 1.140
OPERATIONAL DATA *»«»»»«»»»»«*»«
INLET AIR TEMPERATURE, DEGREES Fl START 74.00 FINISH 81.00
ATMOSPHERIC PRESSURE! START 10.21 FINISH 30.21
INLET AIR HUMIDITY, CRN H20/LB AIRI 0.02
RELATIVE HUMIOITYl 74.00 PERCENT
SAMPLE LINE! TEMPERATURE. DEGREES Ct -0.00, FLO* RATE. LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TINE. SECI 1.60
NUMBER OF TESTS! 10
COMMENT Si
CARS. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IOLE-LOH -0.0 14.40
IDLE/TAII -0.0 21.10
RUN UP -0.0 11. to
DUN UP-LEAN -0.0 35.20
RUN UP-RICH -0.0 22.30
TAKE-OFF -0.0 46.10
CLIMB 7 -0.0 66.80
DESCENT S -0.0 44.20
APPROACH 4 -0.0 21.60
TAX
TEST
MODE
1
2
)
4
1
6
7
a
4
10
TEST
MODE
1
2
>
4
5
4
;
a
»
10
TEST
MOnE
2
6
7
9
10
TOTAL
TOTtL
EXHAUST
GAS
TEMP
DEGREES F
675.00
717.00
1011.00
1020.00
1065.00
1)00.00
1112.00
1211.00
1110.00
762.00
MASS EMI
CO
LB/IK
LB FUEL
178.74
Ml. 67
815.44
761.51
402.41
944.45
477.71
1083.12
1011.14
511.16
TIME IN
MODE
KIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIt
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
IB/I».
LB FUEL
171.30
260.04
12. 26
28.60
11.96
)2.7'J
23.10
10.74
100.27
414.40
MEASURED
FUEL FLOW
LB/HR
21.10
46.10
66.80
21.80
21.10
FUEL
-0
CD
(ORYI
PERCENT V
5.10
5.10
7.10
6.30
6.60
7.40
9.10
9.20
9.40
4.80
MASS EMI
ND2
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
4.22
0.48
5.54
2.18
1.41
14.014
0
CO
2
IORVI
PERCENT V
7.20
8.40
4.20
10.00
9. SO
7.40
U.JO
7.50
7.10
6.20
MASS EMI
C02
LB/1K
LB FUEL
1235.31
1131.14
1741.64
1844.26
1814.74
1542.60
1174.1)
1)87.62
1247.52
1077.48
CO
LB/IK
LB FUEL
541.67
449.4!
977.71
1051.19
1)1.16
21.10
THC
IDRYI
PPNV
60010.00
19137.00
4671.00
4111.00
5164.00
441 T. 00
3170.00
4566.00
11611.00
72566.00
MASS FNI
NO
LB/U
LB FUEL
0.12
0.47
1.16
3.18
1.87
-0.00
4.22
3.17
1.62
1.05
LTD CYCLE
CO
LB/1K
HOURS
12484.27
41242.00
61110.84
25018.22
11207.41
MEASURED CALCULATED
AIR FLON F/A
LB/HR
168.00 0.06591
208.00 0.0804)
181.00 0.07721
437.00 0.07668
273.00 0.07641
1118.00 0.07245
771.00 0. 07742
147.00 O.C7468
112.00 0.08406
158.00 0.
NO
IORVI
PPHV
24.00
51.00
271.00
160.00
144.00
-0.00
213.00
164.00
88.00
58.00
MASS EMI
NOX
LB/IK
LB FUEL
0.52
0.47
1.16
1.18
1.87
-0.00
4.22
1.17
1.62
1.01
EMISSIONS
CO
EMISSION
LBS.
2.447
0.416
5.421
2.102
0.711
11.627
0.828
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
11516.64
12484.27
27032.01
26801.75
17894.24
91242.00
65110.84
53299.54
25018.22
11207.41
HC
LB/IK
LB FUEL
260.04
32.71
21.30
100.27
419.90
08114
NO
I
IORVI
PPNV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
7468.42
1486.86
1019.41
1006.67
801.86
3147.19
1156.24
1515.01
2186.11
9701.82
HC
LB/IK
HOURS
5486.88
11 47. 39
1556.24
2386.31
9703.82
ALDEHYDES SMOKE
IORY)
37.00
46.00
-0.00
-0.00
-0.00
-0.00
19.00
28.00
57.00
61.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
1.097
0.016
0.124
0.2)4
0.610
2.1)1
0.152
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS ENI
C02
LB/HR
24582.73
32308.03
11011.41
66811.75
40464. 81
111048.11
105151.69
68270.81
29691.01
22741.44
NO
L8/U
IB FUEL
0.97
-0.00
4.22
1.62
1.01
PART1CULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR 18/HR
10.11 10.11
20.11 20.11
169.48 169.48
III. B2 111.82
86.40 86.40
-0.00 -0.00
282.10 282.10
116.06 116.06
38.47 36.47
22.24 22.24
NO NO
LB/IK EMISSION
HOURS LBS.
20.51 0.0041
-0.00 -0.0000
282.10 0.0234
18.47 0.0038
22.24 0.0015
-0.0000
-0.0000
1-73
-------
DATE: T/28/TI
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEOYNE-CONTINENTAL
ENGINE DATA *««»«»««*««»«*.*
CAL ID NUMBER! 253 ENGINE TTPE AND MODEL: 10-470-C
RATED HORSEPOWER: 290.
ENGINE TOTAL TINE: 761. MRS
FUEL! AV GAS 100/130 FUEL H/C RATIO! 1.840
OPERATIONAL DATA «*««»»»
INLET AIR TENPERATUREi DEGREES F! START M.OO FINISH 76.00
ATMOSPHERIC PRESSURE: START 10.15 FINISH 30.15
INLET AIR HUMIDITY, CRN H20/LB AIR! O.Ot
RELATIVE HUMIDITY: 60.00 PERCENT
SAMPLE LINE: TEMPERATURE, REGREES C: -0.00, FLOU RATE. LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TIME, SF.C: 1.60
NUMBER OF TESTS: 10
COMMENTS:
i» »»**»»»»
SERIAL NUMBER! 7101»-7-CA
9949
CAKB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOU 1 -0.0 19.30
IDLE/TAXI 2 -0.0 26.40
RUN UP 3 -0.0 38.70
RUN UP-LEAN 4 -0.0 38.70
RUN UP-RICH 5 -0.0 31.60
TAKE-OFF 6 -0.0 107.20
CLIMB 7 -0.0 86.10
DESCENT 8 -0.0 73. BO
APPROACH 9 -0.0 52.70
TAXI
TEST
NODE
1
2
3
4
5
6
7
a
t
10
TEST
"006
1
2
1
4
5
6
7
8
9
10
TEST
NOOE
2
6
;
9
10
TOTAL
TOT«L
EXHAUST
GAS
TEMP
DEGREES F
359.00
560.00
986.00
964.00
975.00
1412.00
1401.00
1312.00
1222.00
706.00
MASS EMI
CO
LB/1K
LR FUEL
613.60
B84 . 86
1057.22
987.41
1 0 1 1 . 66
868. 10
S73.00
970.99
933.49
883.81
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
IB/ IK
LB FUEL
573.19
249.37
25.72
26.01
23.06
15. 11
15.40
19.37
18.79
336.42
MEASURED
FUEL FLOW
LB/HR
26.40
107.20
86.10
52.70
33.40
FUEL
-0.
CO
(DRY)
PERCENT V
4.40
6.70
7.60
6.90
7.00
6.10
6.00
6.30
6.20
6.60
MASS EMI
NO?
L3/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
o.n
0.0
0.0
FUEL
USED
LBS.
5.2R
0.54
7. 15
5.27
2.24
20.470
.0
CO
2
IDRYI
PERCENT V
2.90
5.30
6.60
6.90
6.70
7.90
7.70
7.20
7.00
4.10
MASS EMI
C02
LB/IK
L9 FUEL
635.43
1099.80
1442.56
1551.45
1521.43
1766.46
1760.32
1664.58
1655.97
862.65
CO
LB/1K
LB FUEL
BS4.86
868.10
873.00
933.49
883.81
33.40
THC
(ORYI
PPMV
71867.00
32966.00
3228.00
3173.00
2786.00
1959.00
1848.00
2299.00
2179.00
43865.00
MASS EMI
NO
LB/1K
LB FUEL
0.05
0.15
1.19
0.99
0.97
4.46
7.91
5.66
4.97
0.35
LTD CYCLE
CO
LB/1K
HOURS
23360.36
93060.00
75165.13
49194.84
29519.12
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
108.00 0.06B56
233.00 0.07168
435.00 0.06768
445.00 0.06568
362.00 0.06510
1296.00 0.06573
1038.00 0.06435
872.00 0.06378
622.00 0.06238
255.00 0.
NO
IDRYI
PPHV
2.00
7.00
52.00
42.00
41.00
191.00
331.00
234.00
201.00
16.00
MASS EMI
NDX
LB/1K
LB FUEL
0.05
0.15
1.19
0.99
0.97
4.46
7.91
5.66
4.97
0.35
EMISSIONS
en
EMISSION
LBS.
4.672
0.465
6.239
4.919
1.978
18.273
0.893
SO
2
IOPY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MASS EMI
CO
LB/HR
11342.46
23360.36
40914.38
38212.92
31968.57
93060.00
75165.13
68411. Bl
49194.84
29519.12
HC
LB/IK
LB FUEL
249.37
15.97
15.40
18.79
336.42
.07107
NO
X
IORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MISS EMI
HC
LB/HR
11078.06
6583.29
995.27
1006.41
728.70
1711.64
1325.91
1429.80
990.22
11236.30
HC
LB/IK
HOURS
6583.29
1711.64
1325.91
990.22
11236.30
ALDEHYDES SMOKE
(DRY)
69.00
41.00
-0.00
-0.00
-0.00
-0.00
7.00
6.00
6.00
30.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
1.317
0.009
0.110
0.099
0.753
2. 207
0.112
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
12263. 62
29034.82
55827.01
60041.07
4B077.09
189364.56
151563.31
122846. C6
07269.81
28812.54
NO
LB/IK
LB FUEL
0.15
4.46
7.91
4.97
0.35
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI MASS EMI
NO NOX
LB/HH LB/HR
C.86 0.88
4.01 4.01
45.98 45.98
38.21 38.21
30.76 30.76
478.62 478.62
681.10 681.10
417.38 417.38
261.97 261.97
11.75 11.75
NO NO
LB/IK EMISSION
HOURS LBS.
4.01 0.0008
478.62 0.0024
681.10 0.0565
261.97 0.0262
11.75 0.0008
0.0867
0.0042
1-74
-------
DATE: 7/26/71
TEST ORGANIZATION! SCOTT/CEN AVIATION
ENGINE SUPPLIER! TELEOYNE-CONTINENTU
ENGINE DATA
CAL 10 NUMBER! 354 ENGINE TYPE AND MODEL! 10-470-C
RATED NORSEPOMEIIl 290.
ENGINE TOTAL TINEI T6I. HRS
FUEL! AV GAS 100/110 FUEL H/C RATIO! 1.8*0
OPERATIONAL DATA ««.»«»»««««»««»«
INLET AIR TEMPERATURE. DEGREES F: START 79.00 FINISH 80.00
ATMOSPHERIC PRESSURE: START 30.15 FINISH 10.IS
INLET AIR HUMIDITY, CRN H20/L8 AIR: 0.01
RELATIVE HUMIDITY! 44.00 PERCENT
SAMPLE LINEi TEMPERATURE, DEGREES Cl -0.00, FlOX RATE, LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER! 71018-7-CB
J351
CARS. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IOLE-LO* -0.0 5.30
IDLE/TAXI -0.0 10. SC
RUN UP -0.0 26.40
RUN UP-LEAN -0.0 22.90
RUN UP-RICH -0.0 22.90
TAKE-OFF -0.0 66. BO
CLIMB -0.0 61.90
DESCENT -0.0 59. BO
APPROACH 9 -0.0 36. 9C
IAII
TEST
MODE
1
2
a
q
10
TEST
MORE
,
2
)
4
5
6
7
a
9
10
TFSI
iont
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
370.00
639.00
964.00
997.00
964.00
I36B.OO
1390.00
1345.00
1211.00
695.00
MASS EMI
en
LB/1K
Lfl FUEL
657.05
755.25
1095.21
1045.56
1043.23
907.62
863.30
907.60
949.07
964.92
TIMF IN
NUDE
MIN.
12.00
0.30
s.no
6.00
4.00
FOR CYCLF
FOR CYCLE /IB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
MASS EMI
HC
IB/ IK
LR FUEL
421.92
120.54
26.99
-0.00
22.69
IB. 39
14.73
16.82
20.95
269.92
MEASURED
FUEL FION
LB/HF.
10.50
66.80
61.50
36.90
14.10
FUEL
-0
CO
(DRY)
PEBCFNT V
4.30
5.30
7.70
5.90
6.90
6.30
5.80
6.20
6.50
7.60
MASS EM!
N02
LB/1K
LR FUEL
0.0
0.0
0.0
0.0
0.0
o.o
0.0
n.o
0.0
0.0
FUEL
USEO
LUS.
2.10
0.33
5.10
3.69
0.94
12.173
0
CO
2
IORV)
PERCENT V
4.10
7.40
6.30
.5.50
6.20
7.50
7.60
7.40
7.10
4.60
MASS EMI
C02
LB/U
L« FUFL
994.36
1656.87
1395.09
1511.43
1472. B6
1697.71
1777.40
1702.06
1627.13
917.64
CO
LB/1K
LB FUEL
755.25
907.62
863.30
948.07
964.92
14.10
THC
(DRY)
PPMV
48212.00
14770.00
3344.00
-0.00
2620.00
2229.00
1728.00
2006.00
2508.00
37120.00
MASS EMI
Nfl
LB/1K
LB FUEL
0.09
0.66
1.60
1.43
1.39
6.65
7.80
6.76
4.91
0.33
LTO CYCLE
CO
LB/IK
HOURS
7930.17
60629.03
53092.76
14983.78
13605.35
MEASURED CALCULATED
AIR FLOH F/A
LB/HR
39.00 0.06223
117.00 0.06577
292.00 0.06689
263.00 0.05315
258.00 0.06236
795.00 O.C6505
744.00 0.06293
713.00 0.06405
433.00 0.0643B
115.00 0.
NO
IURY)
PPMV
3.00
28.00
69.00
49.00
56.00
291.00
319.00
291.00
205.00
16.00
MASS EMI
NOX
LB/IK
LB FUEL
0.08
0.66
1.60
1.43
1.39
6.65
7.80
6.76
4.91
0.33
EMISSIONS
CO
EMISSION
LBS.
1.596
0.303
4.407
3.499
0.912
10.706
0.879
NO
2
IDRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
-0.00
MASS EMI
CO
LB/HR
3482.37
793C.17
28649.49
23943.31
23889.92
60629.03
53092.76
54274.61
34983.78
13605.35
HC
LB/IK
LB FUEL
120.54
18.39
14.73
20.95
269.92
074B2
NO
X
(DRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
2736.18
1265.71
712.59
-0.00
519.53
1228.56
905.93
1005.73
773.08
3805.83
HC
L9/IK
HOURS
1265.71
1228.56
905.93
773.08
3905.83
ALDEHYDES SMOKE
IORV)
53.00
35.00
-0.00
-0.00
-0.00
-0.00
8.00
9.00
22.00
33.00
MASS EMI
NU2
Ld/KR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.253
0.006
0.075
0.077
0.255
0.667
0.055
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
-0.00
MASS EMI
CO I
Lfl/HR
5217.09
17397.09
36830.27
35069.81
33728.39
113406.94
109309.81
101782.94
60041.24
12938.75
NO
LB/IK
LB FUEL
0.66
6.65
7.60
4.91
0.31
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI MASS EMI
NO NOX
LB/HR LK/HR
0.40 0.40
6.99 6.88
42.17 42.17
12.66 32.66
11.85 31.85
444.19 444.19
479.64 479.64
404.05 404.05
181.23 181.23
4.70 4.70
NO NO
IK/IK EMISSION
HOURS LBS.
6.88 0.0014
444.19 0.0022
479.64 0.0398
181.23 0.0181
4.70 0.0003
0.0618
0.0051
1-75
-------
0»IE: 7/30/71
TEST ORGANISATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEDYNE-CONTINENTAL
ENGINE DATA
CAL ID NUMBER: 255 ENGINE TYPE AND MODELi io-4TO-c
RATED HORSEPOWER: 290.
ENGINE TOTAL TINEi 761. MRS
FUEL: AV GAS 100/130 FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA »»»«««««.
INLET AIR TENPERATUREi DEGREES Fl START 80.00 FINISH 80.00
ATMOSPHERIC PRESSURE: START 30.IS FINISH 30.19
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 43.CO PERCENT
SAMPLE LINE: TEMPERATURE, GEGREES C: -0.00, FLOW RATE. LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER: Tiois-7-cc
CARS. TEST ENGINE MEASURED
HEATER MODE RPN FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 5.30
IDLE/TAXI 2 -0.0 7.00
RUN UP 3 -0.0 19.30
RUN UP-LEAN 4 -0.0 22.90
RUN UP-RICH 5 -0.0 22.90
TAKF-OFF 6 -0.0 103.70
CLIMB 7 -0.0 79.10
DESCENT 8 -0.0 63.30
APPROACH 9 -0.0 38.70
TAKI
TEST
MODE
1
2
3
4
5
6
7
d
t
10
IFSI
MODE
1
2
3
4
5
6
7
8
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
460.00
751.00
1099.00
1099.00
1143.00
1401.00
1469.00
1368.00
1334.00
830.00
MASS EMI
CO
Lfl/lK
LB FUEL
556.08
888.73
1121.54
958.81
982.25
996.92
838.70
925.59
931.47
813.48
TIME IN
MODE
M1N.
12.00
0.30
5.00
h.OO
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
IB/ IK
L8 FUEL
580.74
237.75
37.07
33.81
23.40
18.25
12.94
18.61
21.25
336.17
MEASURED
FUEL FLOW
LB/HR
7.00
103.70
79.10
38.70
5.30
FUEL
-0.
CO
(DRY)
PERCENT V
4.20
6.70
7.80
6.60
6.60
6.80
5.50
6.10
6.20
6.30
MASS FMI
Ntl2
LH/IK
LB FUEL
(1.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
ins.
1.40
0.52
6.57
J.87
0.36
12.709
.0
CO
2
IORY)
PERCENT
3.40
5.40
5.80
6.90
6.70
6.90
7.60
7.00
7.00
4.80
MASS EMI
cr>2
LB/1K
LB FUEL
707.31
1125.52
1310.34
1574.99
1566.72
1573.48
1820.94
1668.99
1652.39
973.84
CO
LB/1K
LB FUEL
888.78
986.9?
838.70
931.47
813.48
5.30
THC
IDRY)
PPMV
V
76585.00
31293.00
4502.00
4063.00
2745.00
2196.00
1482.00
2141.00
2470.00
45457.00
MASS EMI
NU
LB/1K
LB FUEL
0.07
0.31
1.15
1.00
0.98
5.15
7.46
5.98
4.71
0.30
LTD CYCLE
cn
LB/IK
HOURS
6221.49
102344.06
66341.25
36047.82
4311.45
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
30.00 0.07704
69.00 0.07133
210.00 0.06572
264.00 0.06469
264.00 0.06321
1200.00 0.06476
966.00 0.06141
748.00 O.C6190
456.00 0.06252
42.
NO
IDRY)
PPMV
3.00
14.00
57.00
42.00
40.00
216.00
298.00
240.00
191.00
14.00
MASS EMI
NOX
LB/IK
LB FUEL
0.07
0.31
1.35
1.00
0.98
5.15
7.46
5.98
4.71
0.30
EMISSIONS
CO
EMISSION
LBS.
1.244
0.*1Z
5.506
3.605
0.2B9
11.156
0.878
00 0.
NO
2
ICRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
IB/MR
2947.24
6221.49
21645.66
21956.82
22493.50
102344.06
66341.25
58589.96
36047.82
4311.45
HC
IB/ IK
LB FUEL
237.75
18.25
12.94
21.25
136.17
07347
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MASS EMI
MC
LB/HR
3077.90
1664.23
715.53
774.14
535.80
1892.91
1023.80
1177.76
822.49
1781.67
HC
LB/IK
HOURS
1664.23
1892.91
1023.80
822.49
1781.67
ALDEHYDES SMOKE
(DRY)
94.00
45.00
-0.00
-0.00
-0.00
-0.00
19.00
8.00
13.00
64.00
MASS 6"1
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LSS.
0.333
0.009
0.085
O.OB?
0.119
0.629
0.049
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C(12
LB/HR
3748.7?
7878.65
25289.63
36067.23
35877.82
163170.25
144036.56
105640.31
6)947.51
5161.33
NO
LB/IK
LB FUEL
0.31
5.15
7.46
4.71
0.33
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
0.35 0.35
2.14 2.14
25.98 25.98
22.95 22.95
22.39 22.39
533.98 533.98
590.42 590.42
378.64 378.64
182.41 182.41
1.57 1.57
NO NO
LH/1K EMISSION
HOURS LBS.
2.14 0.0004
533.98 0.0027
590.42 0.0490
1C?. 41 0.0182
1.57 0.0001
0.0704
0.0055
1-76
-------
DATE: 7/16/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEOYNE-CONTINENTAL
ENGINE DATA
CAL 10 NUMBER! 191 ENGINE TYPE AND MODEL! IO-4TO-V
RATED HORSEPOMER! 260.
ENGINE TOTAL TIMEI 111. HRS
FUEL! AV GAS 100/110 FUEL H/C DATIOl 1.140
OPERATIONAL DATA «»»«»«««««««»«.
INLET AIR TEMPERATURE. DEGREES Ft START 85.00 FINISH 65.00
ATMOSPHERIC PRESSUREl START 30.23 FINISH 30.23
INLET AIR HUMIDITY, GRN H20/LB AIR! 0.01
RELATIVE HUMIDITY! 47.00 PERCENT
SAMPLE LINE! TEMPERATURE. DEGREES Cl -0.00, FLO* RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SEC! 1.60
NUMBER OF TESTS: 10
COMMENTS!
SERIAL NUMBER! 17001J-7-V-RA
j'943
CARB. 1EST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
L8/MR
IOLE-LOM I -0.0 25.20
IDLE/TAXI 2 -0.0 29.30
RUN UP 3 -0.0 41.00
RUN UP-LEAN 4 -0.0 41.00
RUN UP-RICH 3 -0.0 41.00
TAKE-OFF 6 -0.0 111.30
CLIMB 7 -0.0 80.90
DESCENT a -0.0 76.20
APPRDACH 9 -0.0 63.30
TAXI
TEST
MODE
I
2
1
4
5
6
7
a
9
10
TF.ST
MODE
,
2
3
4
5
6
7
a
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TUTAL
EXHAUST
GAS
TEMP
DEGREES F
390.00
852.00
1199.00
1256.00
1256.00
1469.00
1446.00
1)68. 00
1323. 00
671.00
MASS EHI
cn
LB/IK
LI FUFL
655.76
621.72
1037.42
944.14
968.53
865.57
861.28
955.02
975.96
802.91
TIME IN
MODE
Ml N.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
HC
IB/I*.
LB FUEL
1T4.78
121.66
34.02
34.51
34.11
39.99
22.50
24.23
25.65
145.30
MEASURED
FUEL FLO*
LB/HR
29.30
111.30
80.90
63.30
29.30
FUEL
-0.
CO
(ORYI
PERCENT V
2.60
6.50
9.10
7.90
8.20
7.50
7.00
7.80
9.30
5.00
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
5. 86
0.56
6.71
6.13
1.96
21.424
,0
CO
2
(ORYI
PERCENT V
4.20
7.80
e.io
fl.SO
a. 40
9.40
9.10
8.70
8.50
6.00
MASS EMI
C02
LB/IK
LB FUEL
1664.40
1549.32
1450.90
1596.12
1558.89
1704.53
1759.25
1638.64
1570.41
1513.97
CO
LB/IK
LB FUEL
821.72
865.57
861.28
975.96
802.97
29.30
THC
IDRYI
PPMV
12100.00
16806.00
5210.00
5042.00
5042.00
6050.00
3193.00
3529.00
3809.00
15798.00
MASS EMI
NO
LR/1K
LB FUEL
0.21
0.44
1.54
1.24
1.22
3.09
3.35
2.40
2.57
1. OB
LTD CYCLE
CO
LB/IK
HOURS
24076. 2B
96337.56
69677.63
61778.50
23526.95
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
272.00 0.03766
319.00 0.07404
459.00 0.08208
475.00 0. 071112
471.00 0.07909
1317.00 0.08056
977.00 0.07565
896.00 0.077HI
731.00 0.07941
312.00 0.
NO
(ORYI
PPMV
5.00
21.00
82.00
63.00
63.00
163.00
166.00
122.00
133.00
41.00
MASS EMI
NOX
LB/IK
LB FUEL
0.21
0.44
1.54
1.24
1.2?
3.09
3.35
2.40
2.57
1.08
EMISSIONS
CO
EMISSION
LBS.
4.815
0.482
5.783
6.178
1.576
18.834
0.879
NO
2
I ORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
16525.05
24076.28
42534.27
38709.55
39709.71
96337.56
69677.63
71248.56
61778.50
23526.95
HC
LB/IK
LB FUEL
121.68
39.99
22.50
25.65
145.30
05X72
NO
X
(ORYI
PPMV
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MASS EMI
HC
LB/HR
4404.54
3565.22
1394.70
1414.94
1398.40
4450.77
1820.29
1846.20
1623.74
4257.38
HC
LB/IK
HOURS
3565.22
4450.77
1820.29
1623.74
4257.38
ALDEHYDES SMOKE
(DRY)
54.00
50.00
-0.00
-0.00
-0.00
-0.00
29.00
13.00
10.00
36.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.713
0.022
0.151
0.162
0.285
1.334
0.062
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
MASS CHI
CO 2
LB/HR
41942.79
45395.13
59486.81
65440.75
63914.66
189714.50
142323.00
124864.56
99406.81
44359.34
NO
LB/IK
LB FUEL
C.44
3.09
3.35
2.57
1.08
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
5.22 3.22
12.78 12.78
62.96 62.96
50.71 50.71
50.11 50.11
343.91 343.91
271.41 271.41
183.05 183.05
162.60 162.60
31.69 31.69
Nfl NO
LB/IK EMISSION
HOU'S IBS.
12.78 0.0026
343.91 0.0017
271.41 0.0225
162.60 0.0163
31.69 0.0021
0.0452
0.0021
1-77
-------
DATE: 7/16/71
TEST ORGANIZATION! SCOTT/GEN »VI»TION
ENGINE SUPPLIER! TELEDYNE-CONTINENTAL
ENGINE DATA
CAL 10 NUMBER: 19* ENGINE TYPE AND MODEL' IO-4TO-V
RATED HORSEPOWER: 260.
ENGINE TOTAL TINE: 971. MRS
FUEL: AV GAS 100/110 FUEL H/C RATIO: 1.8*0
OPERAT10NAL DATA »««
INLET AIR TEMPERATURE, DEGREES fs START 9*.00 FINISH 9*.00
ATMOSPHERIC PRESSURE: START 30.23 FINISH 30.23
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 34.00 PERCENT
SAMPLE LINE: TEMPERATURE, CEGRECS C: -0.00, FLOW RATE, LITERS/MIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER! 170012-7-V-RB
9945
CARB. TEST ENGINE MEASURED
HEATER MCJDE RPM FUEL FLOM
L8/HR
IDLF-LOW 1 -0.0 2*. 00
IDLF/TAXI 2 -0.0 29.30
RUN UP 3 -0.0 42.80
RUN UP-LEAN * -0.0 41.00
RUN UP-RICH 5 -0.0 41.60
TAKE-OFF 6 -0.0 116.00
CLIMB 7 -0.0 B7.90
DESCENT B -0.0 75.00
APPROACH 9 -0.0 63.30
TAXI
TEST
MODE
1
2
1
4
5
6
7
R
9
10
TEST
MOOE
1
2
1
*
5
b
;
a
9
10
TEST
MODE
2
6
7
q
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES e
40*. 00
841.00
1188.00
1199.00
1199.00
1435.00
1457.00
1390.00
1300.00
729.00
MASS EMI
CO
LB/1K
LI FUEL
518.99
770.17
1000.58
953.68
943.39
907.11
823.18
937.32
1062. 19
879.42
TIME IN
MODE
HIM.
12.00
0.10
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
300.13
96.97
30.68
21.52
24.62
31.40
20.00
22.23
?5.39
203.13
MEASURED
FUEL FLO*
LB/HR
29.30
116.00
87.90
63.30
29.30
FUEL
-0.
CO
(ORYI
PERCENT V
2.40
5.40
9.70
7.60
7.30
7.80
6. BO
7.90
9.30
6.60
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
L8S.
5.86
0.58
7.30
6.33
1.96
22.029
,0
CO
2
(DRY)
PERCENT V
4.20
7.70
8.40
8.20
8.00
9.10
9.60
8.80
8.00
5.90
MASS EMI
C02
L8/1K
LB FUEL
1482.04
1725.53
1517.93
1616.74
1624.41
1662.83
1825.98
1640.51
14)5.64
1235.21
CO
LB/1K
LB FUEL
770.17
907.11
823.18
1062.19
B79.42
29.30
THC
(DRY)
PPMV
23956.00
10647.00
4658.00
2995.00
3327.00
4714.00
2884.00
3272.00
3BB2.00
2661B.OO
MASS EMI
NO
LB/IK
L6 FUEL
0.0
0.09
1.17
0.87
0.96
2.20
1.73
1.40
0.92
0.37
LTO CYCLE
CO
LB/IK
HOURS
22566. 05
105225.19
T2357.69
67234.18
25766.91
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
229.00 0.04229
339.00 0.06563
487.00 0.08124
4B1.00 0.07449
488.00 O.C7219
1364.00 0.08006
1078.00 0.07672
883.00 O.C7859
710.00 O.OB197
280.00 0.
NO
(DRY)
PPMV
0.0
4. on
62.00
42.00
45.00
115.00
87.00
72.00
49.00
17.00
MASS EMI
NOX
LB/IK
LB FUEL
0.0
0.09
1.1'
0.87
0.96
2.20
1.71
1.40
0.92
0.37
EMISSIONS
CO
EMISSION
LB3.
4.513
0.526
6.006
6.724
1.726
19.495
0.885
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
12935.82
22566.05
42824.93
39100.89
39244.96
105225.19
72357.69
70298.63
67216.38
25766.91
HC
LB/IK
LB FUEL
(16.97
11.40
20.00
25.39
203.13
07085
NO
X
IORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MSSS EMI
HC
LB/HR
7395.07
2548.21
1313. 17
882.50
1024.37
3642.17
1757.58
1667.55
1607.39
5951.68
HC
LB/IK
HOURS
2548.21
3642.17
1757.56
1607.39
5951.68
ALDEHYDES SMOKE
(DRY)
37.00
33.00
-0.00
-0.00
-0.00
-0.00
11.00
21.00
6.00
38.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.510
o.oie
0.146
0.161
0.399
1.233
0.056
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
35568.91
50558.11
64967.31
66286.50
67575.50
192887.75
160503.81
123038.38
90876.06
36191.68
NO
LB/IK
LB FUEL
0.09
2.20
1.73
0.92
0.17
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LE/HR LB/HR
C.O 0.0
2.75 2.75
5C.I3 50.13
35.49 35.49
39.74 39.74
254.63 254.63
152.06 152.06
105.24 105.24
58.19 58.19
10.90 10.90
NO NO
LB/IK EMISSION
HOURS LBS.
2.75 0.0005
254.83 0.0013
152.06 0.0126
5D.I9 0.0058
10.90 0.0007
0.0210
0.0010
1-78
-------
MTEI 7/14/71
TEST OKCANllATtO»l SCOT1/CEN AVIATION
ENGINE SUFFLIERl TElEOTW-COHTININTil
ENGINE 0»T» **»*«*«*»***»*
CM. 10 NUNBEII 1*9 ENCINE TYFE MO NODELI IO-4TO-V 1(1 111 NUWEII |TOOl»-7-»-«C
IATEO HOItfFOHEIl 2*0.
ENCINE TOTM. TIHEI *T1. Nil
Will »V GAS 180/1 JO FUEL H/C IATIOI 1.140
OPERATION*!. OAT* **«***«*«»
INLET All TIIPEI4TUM, OK*EES Fl ST4IT 44.00 FINISH 44.00
ATKOSPKEIIC FISSSMEl STAIt 10.I* FINISH 10.14
INLET All KUNIDITV. GIN HIO/L8 Alll 0.01
IELATIVE HUNIOmi 11.00 PEICENT
SANPLE LINEl TEWEIATUIE. OE&IEES Cl -0.00. FLOM IATE. LITEIS/NINl T.OO
SANPLE LINE TRANSPUT TINE. SECl I.AO
NUNIE* OF TESTSI 10
CONNENTSl
S947
CAII. TEST ENCINE NEAIUIED
MCATII "001 «FN FUEL FLOM
LI/HI
IDLE- LOU -0.0 24.00
IOLE/TAII -0.0 24.JO
UN UF -0.0 42.20
UN UF-LEAN -0.0 41.40
UN UP-IICH -0.0 41.60
TAKE-OFF -0.0 111.10
CLINB -0.0 11.10
DESCENT -0.0 T4.40
AFFIOACH -0.0 98.60
Till
TEST
NODE
1
2
1
4
5
6
7
1
9
10
TEST
NODE
1
2
1
4
5
6
7
8
9
10
TEST
NODE
2
6
T
4
10
TOTAL
TOTAL
E«HAUST
CAS
TENF
OECIEES F
140.00
414.00
1112.00
123A.OO
1222.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LI /IK
LB FUEL
143.44
133.49
1114.44
IOTA. 23
1044.42
444.04
864.37
440.36
1027.01
Ml. 31
TIKE IN
NODE
KIN.
12.00
0.10
3.00
6.00
4.00
FOR CYCLE
FOB CYCLE/LB
10
EIHAUST
CAS
PRESSUDF
FSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS Cl
NC
Lt/U
LB FUEL
110.71
124.41
41.16
41.33
40.11
31.76
41.14
31.76
21.67
124.36
NEASUREO
FUEL FLOD
IB/MR
24.10
111.10
1.10
31.60
24.10
fUEL
-0
CO
(ORVI
FEICENT V
7.10
4.10
10.00
4.10
1.40
a. 10
7.10
7.40
a. 20
6.10
HASS EMI
N02
LB/IH
IB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
3.B6
0.37
4.46
3.16
1.46
21.204
0
CO
2
IDITI
FEICENT V
7.10
7.30
7.10
7.30
.70
.60
.40
.30
.60
.30
MASS ENI
CO 2
IB/In
L» FUEL
1407.71
1412.12
1241.00
1361.71
1420.41
1340.24
1702.12
1340.08
1449.61
1434.13
CO
LB/IK
LB FUEL
833.63
444.04
164.37
1027.0]
161.31
24.10
THC
<0«YI
FFMV
14810.00
17351.00
6711.00
6971.00
6072.00
B233.00
3406.00
9614.00
3100.00
14881.00
NASS ENI
NO
Lfl/H
LB FUEL
0.37
0.41
0.71
0.72
0.64
1.42
1.06
0.16
1. 21
1.01
LTD CYCLE
cn
LB/IK
HOURS
29070.62
107002.14
72430.36
40111.70
29447.41
NEASUIID CALCULATED
All FLON F/A
il/NI
249.00 0.01191
111.00 0.07410
441.00 0.01272
491.00 0.01101
440.00 0.07414
1210.00 0.0(111
440.00 0.07491
191.00 0.07142
66B.OO 0.07419
311.00 0.
NO
IOITI
FPNV
10.00
44.00
11.00
11.00
33.00
76.00
91.00
44.00
62.00
44.00
NASS ENI
NOI
LI/ IK
LB FUEL
0.97
0.41
0.71
0.72
0.64
1.42
1.06
O.B4
i.2a
1.01
ENISSIONS
CO
EMISSION
LBS.
3.014
0.119
4.011
4.011
1.709
14.214
0.410
NO
2
IDIYI
FFNV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS ENI
CO
LB/KI
21902.94
29070.62
47444.09
44771.44
41461.92
107002.14
72430.96
64477.11
60111.70
29447.48
MC
LB/IK
LB FUEL
126.48
91.76
41.14
21.47
124.96
06611
NO
I
IORYI
PFNV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
.-0.00
NASS ENI
MC
Ll/HR
3111.74
1709.41
1191.01
1811.79
1641.48
60B0.28
3491.61
2BII.38
1387.13
1746.10
HC
LB/IK
HOU«S
1703.48
6010.28
1491.41
1117.19
1744.10
ALDEHYDES SMOKE
IOIVI
34.00
41.00
-0.00
-0.00
-0.00
-0.00
10.00
4.00
-0.00
33.00
NASS ENI
N02
I*/ HI
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
ENISSION
LBS.
0.741
0.010
0.214
0.114
0.294
1.491
0.061
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS ENI
C02
LB/HI
11713.40
41444.94
91904.41
96711.24
94014.41
174201.14
142649.44
111101.61
17642.18
42404.41
NO
LB/IK
LB FUEL
0.41
1.42
1.04
1.28
1.03
FAITICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS ENI NASS ENI
NO N0«
LB/KK LB/MI
13.38 13.31
26.69 26.69
24.44 24.44
30.09 30.09
26.47 24.47
160.41 160.43
86.83 88.83
64.02 64.02
74.74 74.74
30.19 10.19
NO NO
LB/IK ENISSION
HOURS LBS.
26.63 0.0031
160.43 0.0008
11.13 0.0074
74.74 0.0079
10.19 0.0020
0.0210
0.0011
1-79
-------
DATE: 8/17/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEDYNE-CONTINENTAL
ENGINE 0>T«
CAL ID NUMBER: 378 ENGINE TYPE AND MODELI io-47o-vo
RATED HORSEPOWER: 260.
ENGINE TOTAL TIME: 165. MRS
FUEL I 4V GAS 100/130 FUEL M/C RATIOl 1.840
OPERATIONAL DATA «»«««««»««««»*»«««««««»«
INLET AIR TEMPERATURE, DEGREES F: START 89.50 FINISH 90.00
ATMOSPHERIC PRESSURE: START 30.06 FINISH 30.06
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 46.00 PERCENT
SAMPLE LINE: TEMPERATURE, CEGREES C: -0.00, FLOU RATE, LITERS/NIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER) M9063VO
3955
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOU
LB/HR
IDLE-LOW 1 -0.0 19.30
IDLE/TAXI 2 -0.0 26.40
RUN UP 3 -0.0 47.50
RUN UP-LEAN 4 -0.0 24.60
RUN UP-RICH 5 -0.0 51.00
TAKE-OFF 6 -0.0 96.70
CLUB 7 -0.0 77.40
DESCENT 8 -0.0 70.30
APPROACH 9 -0.0 59. DO
T4XI
TEST
MODE
1
2
3
4
5
6
7
a
9
10
TEST
MODE
1
2
3
4
5
6
7
a
q
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
673.00
874.00
1199.00
1256.00
1233.00
-0.00
-0.00
1356.00
1278.00
886.00
MOSS EMI
CO
LB/1K
LB FUEL
556.84
442.05
715.01
514.95
494. 12
647. 14
090. OB
761.40
907.71
605.05
TIME IN
MOTE
MIN.
12.00
0.10
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LR FUEL
109.17
17.76
14. 13
8.37
9.33
24.15
13.71
14.94
16.03
19.52
MEASURED
FUEL FLOM
LB/HR
26.40
96.70
77.40
59.80
24.60
FUEL
-0.
CO
IORY)
PERCENT V
3.50
3.00
5.70
1.80
1.60
5.30
5.60
6.30
7.70
4.60
MASS EMI
N02
LI/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
L«.
5.28
0.48
6.42
5.98
1.65
19.BI6
,0
CO
2
IORY)
PERCENT V
a. oo
10.50
10.20
11.00
11.00
10.90
10.60
10.20
9.20
10.50
MASS EMI
C02
LB/IK
LB FUEL
1999.82
2440.95
2010.37
2342.16
2J72.27
2091.17
2052.36
1916.92
1704.04
2170.02
CO
LK/1K
LB FUEL
442. OS
647. 14
690. OB
907.71
605.05
24.60
THC
IORY)
PPMV
11981.00
2105.00
2051.00
1079.00
1187.00
3454.00
1943.00
2159.00
2375.00
2591.00
NASS EMI
NO
LB/1K
LB FUEL
0.39
0.90
3.44
2.67
2.41
11.80
1 1.92
9.01
4.18
1.19
LTD CYCLE
CO
LB/1K
HOURS
11670.07
62578.69
53411.85
54280.79
14884.31
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
232.00 0.05871
359.00 0.06269
601.00 0.07381
331.00 0.06003
689.00 0.06716
1248.00 0.07558
988.00 0.07500
880.00 0.07663
711.00 0.07095
321.00 0.
NO
IDRYI
PPMV
15.00
37.00
167.00
120.00
108.00
688.00
589.00
454.00
216.00
55.00
MASS FNI
NOX
LB/1K
LB FUEL
0.39
0.90
3.44
2.67
2.43
13. ao
11.92
9.01
4.18
1.19
EMISSIONS
CO
EMISSION
LBS.
2.334
0.113
4.433
5.428
0.997
13.505
0.682
NO
2
IORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/MR
10747.02
11670.07
33963.04
12667.88
25200.25
62578.69
53411.B5
5352D.33
5428C.79
14884.31
K
LD/1K
LB FUFL
1 (.76
24. 15
13.71
16.03
19.52
07027
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
HC
LB/HR
2106.97
468.97
699.91
206.01
475.88
2335.71
1061.37
1050.57
958. 8B
480.16
HC
LB/1K
HOURS
468.97
2335.71
1061.37
958.88
480. 16
ALDEHYDES SMOKE
(DRY)
21.00
12.00
-0.00
-0.00
-0.00
-0.00
8.00
e.oo
8.00
6.00
MASS FMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.094
0.012
0.088
0.096
0.012
0.322
0.016
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/HR
38596.54
64177.09
95492.75
57617. OB
120985.56
202216.00
158852.38
136165.06
101901.69
533B2.45
NO
LB/1K
LB FUEL
0.90
13.80
11.92
4.18
1.19
PAKTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/hR LB/HR
7.57 7.57
23.64 23.64
161.44 163.44
65.71 65.71
124.18 124.18
1334.32 1334.32
922.75 922.75
613.58 633.58
250.11 250.11
29.23 29.23
NO NQ
L6/IK EMISSION
HOURS LBS.
23.64 0.0047
1334.32 0.0067
922.75 0.0766
250.11 0.0250
29.23 0.0020
0.1150
0.0058
1-80
-------
DAfEl B/IT/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEDVNE-CONTINENTAL
ENGINE DATA *»«»»«*«««»»*<
CAL 10 NUMBER! 1T9 ENGINE TYPE AND MODEL! IO-4TO-VO
RATED HORSEPOWER I 260.
ENGINE TOTAL TINE! 183. MRS
FUEL! AV GAS 100/190 FUEL H/C RATIO! 1.840
OPERATIONAL DATA ««««»»»«««»««»«««»»«».«.
INLET AIR TEMPERATURE, DEGREES Fl START 69.00 FINISH 90.50
ATMOSPHERIC PRESSURE! START 90.06 FINISH JO.06
INLET AIR HUMIDITY, GUN H20/LB AIRl 0.01
RELATIVE HUMIDITY! 49.00 PERCENT
SAMPLE LINE! TEMPERATURE. DEGREES C: -0.00, FLOU RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TINE, SECl 1.60
NUMBER OF TESTS! 10
COMMENTS!
SERIAL NUMBER! 149063VOA
7.00
9957
CARB. TEST ENGINE MEASURED
HEATER NODE 8PM FUEL FLOM
LB/HR
IDLE-LOU 1 -0.0 21.10
IDLE/TAXI 2 -0.0 26.40
RUN UP 3 -0.0 49.20
RUN UP-LEAN 4 -0.0 26.40
RUN UP-RICH 5 -0.0 49.20
TAKE-OFF 6 -0.0 123.10
CLIMB 7 -0.0 94.90
DESCENT a -0.0 77.40
APPROACH 9 -0.0 63.30
TAXI
TEST
MODE
1
2
3
4
5
6
7
a
9
10
TEST
NODE
1
2
3
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
605.00
863.00
9T5.00
1043.00
975.00
1256.00
1233.00
1177.00
1076.00
314.00
MASS EMI
CO
LB/1K
LB FUEL
659.36
563. 79
751.73
645.49
621.73
666.56
725.19
886.74
961.34
817.13
TIME IN
MODE
HIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUS1
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
193.69
35.11
15.70
13.11
12.00
32.2?
14.87
14. 35
16.54
ieo.94
MEASURFH
FUEL FLOU
LB/HR
26.40
123.10
94.90
63.30
24.60
FUEL
-0
CO
(ORYI
PERCENT V
4.90
4.50
6.30
5.30
5.10
5.60
6.00
7.60
a. 40
7.00
MASS EHI
N02
LB/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
5.28
0.62
T.ea
6.33
1.65
21.750
0
CO
2
(DRY)
PERCENT V
7.60
10.60
10.40
11.10
11.30
10.90
10.50
9.50
9.00
7.60
MASS EMI
C02
LB/1K
LB FUEL
1606.87
2160.65
1949.62
2124.08
2164.46
2018.54
1994.01
1741.59
1618.37
1393.94
CO '
LD/1K
LB FUEL
583.79
666.56
725.19
961.34
817.13
24.60
THC
(DRY)
PPNV
25132.00
4726.00
2309.00
1879.00
1718.00
4726.00
2148.00
2148.00
2524.00
27065.00
MASS EMI
NO
LB/IK
LB FUEL
0.33
1.11
5.08
3.14
3.24
13.28
6.23
4.33
4.34
0.81
LTD CYCLE
CO
LB/IK
HOURS
15411.92
62053.94
68820.50
60852.84
20101.36
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
222.00 0.06956
343.00 0.07121
617.00 0.07754
341.00 0.07571
643.00 0.07556
1571.00 0.07754
1200.00 0.07651
931.00 0.07966
742.00 0.08141
247.00 0.
NO
(DRY)
PPMV
15.00
52.00
259.00
157.00
162.00
679.00
314.00
226.00
231.00
42.00
MASS EMI
NOX
LB/IK
LB FUEL
0.33
1. 11
5.08
3.14
3.24
13.28
6.23
4.33
4.34
o.ai
EMISSIONS
CO
EMISSION
LBS.
3.082
0.410
5.712
6.085
1.347
16.637
0.765
NO
2
IDRY)
PPNV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
13912.55
15411.92
36985.15
17040.80
30569.14
82053.94
68820.50
68633. 88
60852.84
20101.36
HC
LB/IK
LB FUEL
35.11
32.22
14.67
16.54
160.94
08027
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
4086.80
927.01
776.35
346.01
590.15
3965.97
1411.06
1110.98
1047.22
44*1.24
HC
LB/IK
HOURS
927.01
3965.97
1411.06
1047.22
4451.24
ALDEHYDES SMOKE
IDRV)
25.00
18.00
-0.00
-0.00
-0.00
-0.00
8.00
13.00
6.00
27.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.185
0.020
0.117
0.105
0.296
0.725
0.033
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
33904.91
57041.21
95930.88
56075.80
106491.25
250943.75
189231.88
134799.06
102442.94
34290.91
NO
LB/IK
LB FUEL
1.11
13.28
6.23
4.34
0.61
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
7.00 7.00
29.25 29.25
249.75 249.75
82.92 82.92
159.60 159.60
1634.19 1634.19
591. 5a 591.58
335.24 335.24
274.87 274.87
19.81 19.81
NO NO
LB/IK EMISSION
HOURS LBS.
29.25 0.0059
1634.19 0.0082
591.58 0.0491
274.87 0.0275
19.61 0.0013
0.0919
0.0042
1-81
-------
0«TE: 6/17/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER) TELEDYNE-CONTINENTAL
ENGINE DAT*
C»L ID NUMBER: 180 ENGINE TTPE AND HODELI ID-4TO-VO
RATED HORSEPOWER! 260.
ENGINE TOTAL TINE: 185. MRS
FUEL: AV GAS 100/130 FUEL H/C RATIOI i.a»o
OPERATIONAL DATA »
INLET AIR TEHPERATUREt DEGREES Fl START 81.50 FINISH 83.00
ATMOSPHERIC PRESSURE: START 30.0* FINISH 30.04
INLET AIR HUHIDITY, CRN H20/LB AIRt 0.01
RELATIVE HUMIDITY: 61.00 PERCENT
SAMPLE LINE: TEMPERATURE, CEGHEES C: -O.OC, FLOW RATE, IITERS/NIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER! 149063VOB
9359
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOU 1 -0.0 21.10
IOI.fi/T4XI 2 -0.0 24.60
RUN UP 3 -0.0 49.20
RUN UP-LEAN 4 -0.0 29.90
RUN UP-RICH 5 -0.0 49.20
TAKE-OFF 6 -0.0 107.20
CLIM1 7 -0.0 80.90
DESCENT . 8 -0.0 68.60
APPROACH 9 -0.0 59. 60
TAXI 10 -0.0 24.60
TEST
NODE
1
2
3
4
5
6
7
a
9
10
TCSI
HODE
1
2
1
4
5
6
7
a
9
10
TEST
MCDF
2
6
7
9
10
TOTAL
TOTAL
FXHAUST
GAS
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
IB/ IK
LB FUEL
769.01
488.16
753.84
641.03
616.47
713.30
677.65
131. a4
946.88
981.41
TIME IN
MODE
MIH.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
172.91
38.72
20.09
18.93
0.17
24.63
14.23
15. OS
13. 20
166.82
MEASURED
FUEL FLUX
L3/HR
24.60
107.20
80.90
S9.80
24.60
FUEL
CO
IORY)
PERCENT V
6.40
3.80
6.00
5.00
4.70
5.70
5.40
6.80
8.00
7.80
MASS fMI
ND2
LB/1K
LB FUEL
o.n
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
o.o
FUEL
USED
LBS.
4.92
0.54
6.71
5.98
1.65
19.799
CO
2
IORY)
PERCENT V
7.90
11.40
9.80
10.50
10.70
10.10
10.50
9.50
8.80
7.50
MASS EMI
C.02
LB/1K
LH FUCL
1491.48
2301.01
1934.65
2115.11
2205.16
1985.91
2070.33
1B2S.96
1636.54
1131.66
CO
LB/U
LB FUEL
488.16
713.30
677.65
946.88
881.43
THC
IDSYI
PPMV
25132.00
5263.00
2792.00
2578.00
22.50
3437.00
1987.00
2148.00
2685.00
25776.00
MASS EMI
ND
LB/1K
LB FUEL
0.49
3.73
4.66
3.54
3.40
3.04
6.J7
4.06
3.93
0.50
LTD CYCLE
CO
IB/ IK
HOURS
12008.63
76465.94
54821.76
56623.63
21683.12
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
218.00 0.07786
328.00 0.07164
615.00 0.07383
366.00 0.07210
643.00 0.07041
1354.00 0.07402
1038.00 0.07367
639.00 0.07595
704.00 0.07878
245.00 0.08299
NO
IORYI
PPMV
25.00
177.00
226.00
168.00
158.00
148.00
309.00
202.00
202.00
27.00
MASS EMI
NO*
LB/1K
LB FUEL
0.49
3.73
4.66
3.54
3.40
3.04
6.37
4.06
3.93
0.50
EMISSIONS
CO
EMISSI
LBS.
2.40?
0.382
4.550
5.662
1.45.1
14.449
0.730
NO
2
IDRYI
PPMV
-C.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
16226.07
12008.63
37089.73
19166.70
30330.55
76465.94
54821.76
57063.87
56623.63
21683.12
HC
LB/IK
LB FUEL
38.72
24.63
14.28
10.20
166.82
NO
X
IORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
3649.27
952.55
988.47
56S.99
8.32
2640.69
1155.32
1032.36
1088.42
4103.82
HC
1.8/ IK
HOURS
952.55
2640.69
1155.32
1088.42
4103.82
ALDEHYDES SMOKE
IDRYI
31.00
15.00
-0.00
-0.00
-0.00
-0.00
3.00
6.00
2.00
24.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.191
0.013
0.096
0.109
0.275
0.683
0.035
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HK
31470.14
56604.81
95184.61
63241.88
108491.75
212888.94
167489.19
125260.50
97865. 19
32758.71
NO
LB/1K
LB FUEL
3. 73
3.04
6.37
3.93
0.50
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NDX
LB/HR LB/HR
1C. 41 10.41
91.88 91.88
229.47 229.47
105.78 105.78
167.48 167.48
326.12 326.12
515.27 515.27
278.41 278.43
234.84 234.84
12.33 12.33
NO NU
LB/1K EMISSION
HOURS LBS.
91.88 0.0184
326.12 0.0016
515.27 0.0428
234.84 0.0235
12.33 0.0008
0.0871
0.0044
1-82
-------
OATtl 8/17/71
TEST ORGANIIATIONI SCOTT/OEN AVIATION
ENGINE SUPPLIERl TELfOVNC-CONTHMNIU
ENCINE 0414
C4L 10 NUMBER! III ENCINE WE 4NO NOOELI IO-4TO-VO
I4TEO HORSEPOKERt 240.
ENCINE TOT41 TINII It). MRS
FUILI »V G4S 100/1)0 FUEl H/C RATIOl I.MO
OPERATIONAL 0414 »«w«.«.«.».»»««««.»««»««»««»««»»»»
INLET tIR TEMPERATURE. DECREES F: STtRT 16.00 FINISH 86.00
ATMOSPHERIC PRESSURE! ST4RT 30.0* FINISH 30.0*
INLET 4IR HUMIDITY. CRN H20/LB 4IR! 0.02
E14TIVE HUNIOITTI ST.00 PERCENT
SAMPLE LINE: TENPFRtTURE. CEGREES C: -0.00. FLOM R4TEi IITERS/NIN1
S4NPLE LINE TRANSPORT TINE. SFC: 1.60
NUMBER OF TESTSl 10
COMMENTSi
SERIAL NUMIERI 490IIVO
9961
C4R1. TEST ENGINE NE4SUIEO
HE4TER NODE RP» FUEL PLOM
LI/M
IOLE-LOM -0.0 10.90
IDLE/T4II -0.0 IT.40
RUN UP -0.0 11.60
RUN UP-LEAN -0.0 29.90
RUN UP-RICH -0.0 31.60
T4KE-OFF -0.0 110. «0
CLINB -0.0 80.90
DESCENT -0.0 TO. 10
APPROACH -0.0 SI. 00
Till
TEST
NODE
1
2
10
TEST
NODE
1
2
3
4
5
6
T
A
9
10
TEST
NODE
2
6
T
9
10
TOTAL
TOT4L
EIH4UST
GAS
TENP
DEGREES F
482.00
T62.00
1199.00
1256.00
1222.00
1*46.00
1*80.00
-0.00
-0.00
-0.00
NASS ENI
CO
L8/U
L8 FUEL
434.il
8*1.27
712.09
971.81
560.97
679. 89
722.78
877.75
963.21
938.22
TINE IN
NODE
«IN.
12.00
0.30
5.00
6.00
4.00
FOR CTCLE
FOR CYCLE/IB
10
EIH4UST
G4S
PRESSURE
PSI4
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.co
-0.00
-0.00
NASS ENI
MC.
LB/IK
IB FUEL
263.65
T0.50
17.92
10.81
1*. 71
36.68
15.10
14.52
14.78
172.92
MEASURED
FUEL FLOM
L8/IW
17.60
110.00
10.90
51.00
14.10
FUEL
-0
CO
IOR»>
PERCENT V
.10
.40
.80
.60
.50
.70
.80
.70
8. SO
8.90
NASS ENI
N02
IB/ IK
IB FUFL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
3.52
O.SS
6.71
5.10
0.94
16.833
0
CO
2
(ORTI
PERCENT V
T.OO
8.90
10.40
11.50
11.50
10.70
10.20
9.80
9.10
7.40
NASS ENI
CO 2
LB/IK
L8 FUEL
1453.94
1627.56
2006.22
2246.12
2252.47
2005.34
1997.18
1755.27
1620.26
1225.71
CO
L8/U
LB FUEL
861.27
679.19
722.78
963.21
938.22
14.10
THC
IORVI
PPNV
34824.00
10577.00
2549.00
1519.00
2061.00
5370.00
2115.00
2224.00
22T8.00
28640.00
NASS ENI
NO
LB/1K
LS FUEL
1.69
1.01
5.02
3.59
4.03
10.56
7.63
3.60
3.18
0.36
LTD CTCLE
CO
IB/IK
HOURS
15158.42
75)32.00
51472.95
49123.95
13228.94
NI4SUREO C4LCUL4TEO
41* FLO* F/4
LI/NR
102.00 O.OTIOI
199.00 0.08006
401.00 0.07535
396.00 0.07403
420.00 0.07312
1409.00 0.07745
1023.00 0.07430
850.00 0.0814)
598.00 0.08219
134.00 0.
NO
IORTI
PPNV
71.00
5). 00
249.00
176.00
197.00
939.00
373.00
112.00
171.00
21.00
NASS ENI
KOI
IB/IK
L8 FUEL
1.69
1.01
5.02
3.59
4.03
10.56
7.63
3.60
3.18
0.36
ENISSIONS
CO
EMISSION
LBS.
3.032
0.3T7
4.153
4.912
0.886
14.060
0.835
NO
2
IDRT)
PPNV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS ENI
CO
LS/HR
6662.55
15158.42
22502.01
17097.24
17726.48
75332.00
58472.95
61705.70
49123.95
13228.94
HC
LB/U
IB FUEL
70.50
36.61
15.10
14.78
172.92
08V03
NO
X
(OUT)
PPNV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS ENI
HC
IB/MR
2768.37
1240.88
566.38
323.35
464.98
4064.66
1221.19
1020.74
754.00
2438.11
MC
LB/IK
HOURS
1240.88
4064.66
1221.19
754.00
2438.11
ALDEHYDES SMOKE
IDRYI
60.00
29.00
-0.00
-0.00
-0.00
-0.00
6.00
4.00
10.00
44.00
ASS ENI
H02
LB/KR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.248
0.020
O.I 01
0.075
0.163
0.609
0.036
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS ENI
C02
IB/MR
15266.37
21645.09
43)94.50
67159.06
71178.06
222191.31
161571.75
12)393.38
82633.00
1T2B2.44
NO
LB/IK
LB FUEL
1.01
10.56
T.63
3.18
0.36
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS ENI NASS ENI
NO NOI
L8/HR LB/HR
17.78 17.78
17.83 17.8)
158.68 191.68
107.45 107.45
127.47 127.47
1170.08 1170.08
617.67 617.67
292.73 252.73
162.33 162.33
5.13 5.13
NO NO
Lfl/lK EMISSION
HOURS IBS.
17.83 0.0036
1170.08 0.0059
617.67 0.0913
162.33 0.0162
9.13 0.0003
0.0773
0.0046
1-83
-------
DUE: e/17/Tl
TEST ORGANIIATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEDVNE-CONTINENTAL
ENGINE DATA
CAL 10 NUMBER) 382 ENGINE TYPE AND MODEL) IO-470-VO
HATED HORSEPOWER: 260.
ENGINE TOTAL TINE: 18S. MRS
FUEL: AV GAS 100/130 FUEL H/C RATIOl 1.840
OPERATIONAL DATA [[[
INLET AIR TENPERATUREf DEGREES F: START 90.00 FINISH 90.00
ATMOSPHERIC PRESSURE: START 30.0; FINISH 30.04
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.02
RELATIVE HUMIDITY: 55.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOU RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER) 49035VOA
9963
CARR. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOU
LB/HR
IDLE-LOU 1 -0.0 10.50
IDLE/TAXI 2 -0.0 15. 80
RUN UP 3 -0.0 33.40
RUN UP-LEAN » -0.0 26.40
RUN UP-RICH 5 -0.0 31.60
TAKE-OFF 6 -0.0 98.40
CLIMD 7 -0.0 77.40
DESCENT 8 -0.0 63.30
APPROACH 9 -0.0 31.00
TAXI
TEST
MODE
1
2
3
4
5
6
1
B
9
10
TEST
MODE
1
2
3
4
5
6
7
H
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
482.00
762.00
1099.00
1121.00
1143.00
1412.00
1435.00
1334.00
1256.00
471.00
MASS EMI
CO
LB/IK
L"> FUEL
470.94
863.69
997.91
1000.17
851.76
706.88
7*3. 73
909.31
994.62
908.40
TIME IN
MODE
MM.
12.00
0.30
3.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
355.59
87.14
27.12
28.00
22.91
36.96
15.68
15.32
15.94
215.61
xrASURf.o
FUtL FLOW
L8/HH
15.80
98.40
77.40
51.00
15.80
FUEL
-0.0
CO
IORY)
PERCENT V
1.50
7.60
8.70
6.90
7.20
6.00
6.40
7.80
8.50
8.40
MASS F.MI
N02
LO/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LOS.
3.16
0.49
6.42
5.10
1.06
16.235
CO
2
IORYI
PERCENT V
6.90
B. an
8.50
6.70
9.50
10.60
10.30
9.30
8.70
6. BO
MASS EMI
CO 2
LB/1K
LB FUEL
1458.75
1574.97
1531.89
1525.94
1769.96
1962.17
1931.24
1703.49
1583.46
1155.44
CO
LB/1K
Id FUEL
865.69
706.88
763.73
984.62
908.40
15.80
THC
(OitYl
PPMV
46144.00
13356.00
4129.00
3373.00
3373.00
547B.OO
2294.00
2294. 00
2402.00
34811.00
MASS EMI
NO
LB/1K
LB FUEL
4.09
0.67
1.28
1.74
1.32
9.15
5.16
3.83
2.78
0.34
LTD CYCLE
cn
LH/IK
HOUBS
13677.97
69556.75
59112.73
50215.70
14352.78
MEASURED CALCULATED
AIR FLOU F/A
LB/HR
96.00 0.06977
175.00 0.08185
384.00 0.08142
323.00 0.064*0
383.00 0.07837
124.10 0.07846
967.00 0.07757
756.00 0.07980
592.00 0.08055
146.00 0.
NO
(DRY)
PPMV
185.00
36.00
68.00
73.00
68.00
473.00
263.00
200.00
146.00
19.00
MASS EMI
NOX
LB/1K
LB FUEL
4.09
0.67
1.2B
1.74
1.32
9.15
5.16
3. 83
2.78
0.34
EMISSIONS
CO
EMISSION
LBS.
2.736
0.348
4.906
5.022
0.962
13.973
0.861
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
4944.82
13677.97
3333C.09
26404.37
26978.65
69556.75
59112.73
57559.41
50215.70
14352.78
HC
LB/IK
LB FUEL
B7.14
36.96
15.68
15.94 '
215.61
08701
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
MASS EMI
HC
LB/HR
3733.74
1376.88
405.96
739.25
723.85
3637.10
1213.50
969.53
812.72
3406.58
HC
LB/IK
HOURS
1376.88
3637.10
1213.50
812.72
3406. 58
ALDEHYDES SMOKE
IORY)
40.00
29.00
-0.00
-0.00
-0.00
-0.00
8.00
5.00
3.00
45.00
MASS EMI
NU2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0."
0.0
HC
EMISSION
LBS.
0.275
0.018
0.101
0.081
0.228
0.704
0.043
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
15316. 88
24884.49
51165.14
40284.68
55930.65
193077.75
149477.69
107830.81
80756.56
16255.92
N(I
L8/IK
LB FUEL
0.67
9.15
5.16
2.78
0.34
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
tin NOX
LB/HR Lfl/HR
42.93 42.93
10.64 10.64
42. F9 47.79
45.88 45.88
41.65 41.85
900.68 900.68
399.00 399.00
242.42 242.42
141.68 141.68
5.33 5.33
NO NO
LB/IK EMISSION
HOURS LdS.
10.64 0.0021
900.68 0.0045
399.00 0.0331
IM.66 0.0142
5.33 0.0004
0.0543
0.0033
-------
DATE! 8/17/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEDVNE-CONTINENTAL
ENGINE DATA
CAL 10 NUMBERS 363 ENGINE TYPE AND NOOEll IO-470-VO
RATED HORSEPOMERl 260.
ENGINE TOTAL TIMCl 111. MRS
FUEL! »V GAS 100/130 FUEL M/C RATIO! 1.940
OPERATIONAL DATA »««««»»«»».
INLET AIR TEMPERATURE. DE.GREES Fl START 77.90 FINISH 78.00
ATMOSPHERIC PRESSURE! START 30.04 FINISH 30.04
INLET AIR HUMIDITY, CRN H20/L8 AIR! 0.04
RELATIVE NimlDITVl 168.00 PERCENT
SAMPLE LINE! TEMPERATURE. DEGREES Cl -0.00. FLOK RATE. LITERS/MINI
SAMPLE LINE TRANSPORT TINE. SECl 1.60
NUMBER OF TESTSl 10
COMMENTS:
SERIAL NUMBER! 4905SVOB
9965
CARB. TEST ENGINE MEASURED
HEATER MODE RPN FUEL FLOW
LB/HR
IDLE-LOU 1 -0.0 12.30
IDLE/TAXI 2 -0.0 15.80
RUN UP 3 -0.0 33.40
RUN UP-LEAN 4 -0.0 26.40
RUN UP-RICH 5 -0.0 28.10
TAKE-OFF 6 -0.0 102.00
CLIMB 7 -0.0 72.10
DESCENT 8 -0.0 63.30
APPROACH 9 -0.0 49.20
TAXI
TEST
MODE
,
2
3
4
5
6
7
a
9
10
TEST
MODE
1
2
1
4
5
6
7
8
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
IENP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
1969.00
1424.00
1368.00
1300.00
767.00
MASS EMI
CO
LB/1K
LB FUEL
264.40
471.47
916.12
755.49
784.61
713.61
805.87
911.68
948.91
498.12
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PS1A
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
Lfl/lK
LB FUEL
225.18
30.66
20.23
19.48
16.34
38.1*
16.76
16.47
17.09
83.45
MEASURED
FUEL FLOH
LB/HR
15.80
102.00
72.10
49.20
15.80
FUEL
-0.
CO
IORYI
PERCENT V
1.30
3.50
7.80
6.20
6.50
6.10
6.80
8.00
8.20
1.80
MASS EMI
NQ2
LB/U
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
3.16
0.51
5.98
4.92
1.06
15.633
.0
CO
2
(ORVI
PERCENT V
6.70
11.10
9.10
10.10
10. DO
10.60
10.00
9.10
9.00
10.50
MASS EMI
C02
LB/1X
LB FUEL
2141.04
2349.35
1679.33
1933.74
1896.62
1948.38
1862.05
1665.16
1636.41
2162.63
CO
LB/1K
LB FUEL
471.47
713.61
805.87
948.91
498.12
15. BO
THC
(DRY)
PPMV
19332.00
3974.00
3007.00
2792.00
2363.00
5692.00
2470.00
2470.00
2578.00
11116.00
MASS EMI
NO
LB/IK
LB FUEL
0.90
1.39
2.20
1.92
1.78
9.55
4.19
3.19
3.04
i.oa
LTD CYCLE
CO
LB/IK
HOURS
7449.22
72787.94
58102.92
46686.49
7870.36
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
141.00 0.04616
213.00 0.06840
397.00 O.C7928
330.00 0.07603
329.00 0.07679
1282.00 0.07902
888.00 n. 07823
749.00 0.07996
579.00 0.08051
198.00 0.
NO
(DRY)
PPMV
27.00
63.00
114.00
96.00
90.00
497.00
215.00
167.00
160.00
50.00
MASS EMI
NOX
LB/IK
LB FUEL
0.90
1.39
2.20
1.92
1.78
9.55
4.19
3.19
3.04
1.08
EMISSIONS
CO
EMISSION
LBS.
1.490
0.364
4.823
4.669
0.527
11.872
0.759
KO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
3252.08
7449.22
30598.25
19944.98
22047.62
72787.94
58102.92
58975.40
46686.49
7870.36
HC
LB/U
LH FUEL
30.66
39.14
16.76
17.09
83.45
07049
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
2769.74
484.41
675.59
514.40
459.05
3889.91
1208.73
1042.85
840.63
1318.57
HC
LB/U
HOURS
484.41
3889.91
1208.73
840.63
1318.57
ALDEHYDES SMOKE
IDRYI
32.00
15.00
-0.00
-0.00
-0.00
-0.00
13.00
21.00
19.00
15.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.097
0.019
0.100
0.084
o.oea
0.309
0.025
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
26334.82
37119.69
56089.52
51050.69
53295.03
198734.75
134254.00
105404.75
80511.50
34169.49
NO
LB/1K
La FUEL
1.39
9.55
4.19
3.04
1.08
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO KOI
LB/HR LB/HR
11.09 11.09
22.02 22.02
73.46 73.46
50.73 50.73
50.14 50.14
974.11 974.11
301.75 301.75
202.22 202.22
149.63 149.63
17.01 17.01
NO NO
LB/IK EMISSION
HOURS LBS.
22.02 0.0044
974.11 0.0049
301.75 0.0250
149.63 0.0150
17.01 0.0011
0.0504
0.0032
1-85
-------
DATE: 7/15/71
TEST ORGANUATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: LYCUMING
ENGINE DATA
CAL ID NUMBER: 163 ENGINE TYPE AND MODEL: 0-470-R
RATED HORSEPOWER: 230.
ENGINE TOTAL TIME: 161. MRS
FUEL: AV GAS 80/87 FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA «»««»»»«»*»
INLET AIR TEMPERATURE, DEGREES Ft START 89.50 FINISH 89.00
ATMOSPHERIC PRESSURE: START 29.09 FINISH 29.09
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: «i.oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOU RATE, L1TERS/MIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER: 203247-70«»
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 10.60
IDLE/TAXI 2 -0.0 15.00
RUN UP 3 -0.0 35. 5P
RUN UP-LEAN 4 -0.0 35.50
RUN UP-RICH 5 -0.0 35.50
TAKE-OFF 6 -0.0 108.80
CLIMB 7 -0.0 101.00
DESCENT 8 -0.0 57.40
DFSCFNT ON 8 -0.0 49.60
APPROACH 9 -0.0 44.80
TAXI
TEST
MODE
1
2
3
it
5
6
7
a
a
9
10
TEST
MODf
1
i
3
4
5
6
7
fl
3
9
10
TEST
10DE
2
6
7
9
10
TOTAL
TOT«L
EXHAUST
GAS
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EHI
CD
LB/IK
LB FUEL
1001.11
873.37
608.11
661.05
634.90
1027.93
630.62
643.49
1279.11
744.28
816.17
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
HC
L9/1K
LB FUEL
72.49
16.87
8.07
6.38
6.80
13.05
7.19
7.19
20.28
8.29
13.61
MEASURED
FUEL FLOW
LB/HR
15.00
108.60
101.00
44. BO
12.40
FUEL
-0,
CO
IORYI
PERCENT V
4.30
6.80
4.70
5.10
4.90
a. ao
4.90
5.00
11.60
5.90
6.50
MASS FMI
N02
L3/1K
LB FUEL
0.0
n.o
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USFO
LBS.
3.00
0.54
B.3U
4.4B
0.83
17.238
.0
CO
2
IDRYI
PERCENT V
7.40
8.70
10.80
10.40
10.60
8.30
10.70
10.60
6.40
10.00
9.40
MASS EHI
C02
LB/IK
LB FUEL
1402.41
1755.69
2196.30
2118.06
2158.01
1523.34
2163.68
2143.46
1108.84
1982. 08
1854.53
CO
LB/IK
LB FUEL
873.37
1027.93
630.62
744.28
816.17
12.40
THC
IORY)
PPMV
10493.00
2294.00
1089.00
860.00
917.00
1950.00
975.00
975.00
3211.00
1147.00
1692.00
MASS EMI
NO
LR/1K
LB FUEL
0.32
1.01
3.59
2.11
1.75
3.45
4.21
3.57
0.3B
2.57
0.66
LTD T.YCLE
CO
LB/IK
HOURS
13100.56
111838.1)1
63692.52
33343.63
10120.51
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
115.00 0.07760
181.00 0.07260
470.00 0.07132
463.00 0.07135
467.00 0.07131
1253.00 0.08003
1330.00 0.07176
751.00 0.07180
508.00 0.08559
571.00 0.07346
153.
NO
IDRYI
PPMV
16.00
48.00
169.00
99.00
82.00
180.00
199.00
169.00
21.00
124.00
32.00
MASS EMI
NOX
LB/IK
LB FUEL
0.32
1.01
3.59
2. 11
1.75
3.45
4.21
3.57
0.38
2.57
0.66
EMISSIONS
CO
EMISSION
LBS.
2.620
0.559
5.2B6
3.334
0.678
12.478
0.724
00 0.
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
-0.00
MASS EMI
CO
LB/HR
10611.80
13100.56
21595.12
23467.44
22530.68
11183R. 81
63692.52
36936.26
63443.88
33341.63
10120.51
HC
LB/IK
LB FUEL
16.87
13.05
7.19
8.29
11.61
07402
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
766.34
253.12
286.57
226.64
241.57
1419.35
725.84
412.51
1005.81
371.25
168.72
HC
LB/IK
HOURS
253.12
1419.35
725.84
371.25
168.72
ALDEHYDES SMOKE
IDRYI
29.00
12.00
-0.00
-0.00
-0.00
-0.00
5.00
3.00
1.00
2.00
2.00
MASS FMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.051
0.007
0.060
0.037
0.011
0.166
0.010
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
14865.55
26335.29
77968.63
75191.19
76609.13
165739.56
218531.81
123034.56
54998.41
88797.19
22996.14
NO
LB/IK
LB FUEL
1.01
3.45
4.21
2.57
0.66
PARTICULATES
-0.00
-0.00
-O.CC
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
3.36 3.36
15.19 15.19
127.55 127.55
74.83 74.63
61.95 61.95
375.75 375.75
424.88 424.88
205.06 205.06
18.67 18.67
115. 11 115.11
B.18 8. IB
NO NO
LB/IK EMISSION
HCUKS LBS.
15.19 0.0030
375.75 0.0019
424.88 0.0353
115.11 0.0115
8.18 0.0005
0.0522
0.0030
1-86
-------
'3303
... I
DATEl 8/17/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIERl TELEDYNE-CONTINENTAL
ENGINE DATA ««*««»«««««»«»»»«»«««*»»«««
CAL 10 NUMBER! 390 ENGINE TYPE AND MODEL 1 0-470-R SERIAL NUMBER! 131110-6-R
RATED MORSEPOHERl 230.
ENGINE TOTAL TINCl t9. HKS
FUELI AV CAS 100/130 FUEL H/C RATIOI I.(40
OPERATIONAL DATA *»««»«««»«««««»««»«»«»»««
INLET AIR TEMPERATURE, DEGREES ft START 75.00 PINISN 74.30
ATMOSPHERIC PRESSUREI START 30.12 FINISH 30.II
INLET AIR HUMIDITY. GIN H20/LB AIRI 0.01
RELATIVE HUMIOITT1 47.00 PERCENT
SAMPLE LINE! UNMRATUtE. DEGREES Cl -0.00, FLO* RATEt LITIRI/NINl 7.00
SAMPLE LINE TRANSPORT TINE. SECt 1.60
NUM8ER OF TESTSI 11
CONNENTSl
I »***»**
CAR). IE1T ENGINE MEASURED
HCATCR NODE RPM FUEL FLOH
LB/MA
IDLE-LOW 1 -0.0 14.10
IDLE/TAXI I -0.0 14.70
RUN UP 3 -0.0 30.90
RUN UP-LEAN 4 -0.0 30.00
RUN UP-RICH » -0.0 30.00
TAKE-OFF 4 -0.0 97.70
CLIMB ' -0.0 71.30
DESCENT 1 -0.0 62.30
DESCENT 4 -0.0 66.30
APPROACH ') -O.D 42.00
TAXI
TEST
MODE
1
2
3
4
5
6
7
a
8
9
10
TEST
NODE
1
2
3
4
5
6
7
B
8
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DECREES F
62B.OO
930.00
1256.00
1390.00
1356.00
1536.00
1558.00
1513.00
1323.00
1323.00
964.00
MASS EMI
CO
LB/IK
LB FUEL
868.41
1095.35
754.37
531.41
574.88
997.49
599.25
677.00
1241.87
820.86
1133.33
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
42 8. 76
91.18
12.11
6.44
B.33
14.46
8.36
O.IB
14.18
9.37
91.09
MEASURED
FUEL FLOU
LB/HR
16.70
97.70
71.30
42.00
15.80
FUEL
-0.
CO
(DRY)
PERCENT V
8.40
10.30
6.00
4.10
4.50
9.00
4.90
5.50
11.70
6.80
10.90
MASS EMI
N02
IB/ IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
3.34
0.49
5.92
4.20
1.06
15.005
,0
CO
2
IORY)
PERCENT V
3.90
7.20
9.90
11.40
11.20
9.00
11.50
10.90
7.10
9.80
7.00
MASS EMI
C02
LB/1K
LB FUEL
633.50
1203:05
1955.73
2321.60
2248.12
1567.29
2209.77
2108.11
1184.10
1858.77
1143.60
CO
LB/IK
LB FUEL
1095.35
997.49
599.25
820.86
1133.33
15.80
THC
I DRY!
PPNV
72414.00
14971.00
1682.00
868.00
1139.00
2278.00
1193.00
124.80
2332.00
1356.00
15296.00
MASS EMI
NO
LB/1K
LB FUEL
0.05
0.14
3.45
2.13
1.99
0.69
2.29
1.80
0.30
5.27
0.10
LTD CYCLE
CO
LB/1K
HOURS
18292.30
97455.06
42726.32
34476.13
17906.95
NEASURED CALCULATED
AIR PLOD F/A
LB/KR
90.00 0.09221
168.00 0.08839
388.00 0.07375
403.00 0.07101
39T.OO 0.07212
1131.00 0.08409
937.00 0.07525
802.00 0.07498
696.00 0.08864
517.00 0.07687
156.00 0.
NO
(DRY)
PPNV
3.00
8.00
167.00
100.00
95.00
38.00
114.00
89.00
17.00
266.00
6.00
MASS EMI
NOX
LB/IK
LB FUEL
0.05
0.14
3.45
2.13
1.99
0.69
2.29
1.80
0.30
5.27
0.10
EMISSIONS
CO
EMISSION
LBS.
3.658
0.487
3.546
3.448
1.200
12.339
0.822
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
12244.59
18292.30
23310.10
15942.26
17246.30
97455.06
42726.32
42177.25
82335.94
34476.13
17906.95
HC
LB/IK
LB FUEL
91.18
14.46
8.36
9.37
91.09
09050
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
6045.51
1522.74
374.25
193.30
250.01
1412.74
595.78
54.81
939.89
393.74
1439.19
HC
LB/U
HOURS
1522.74
1412.74
595.78
393.74
1439.19
ALDEHYDES SMOKE
(DRY)
36.00
27.00
-0.00
-0.00
-0.00
-0.00
8.00
8.00
6.00
7.00
13.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.305
0.007
0.049
0.039
0.096
0.497
0.033
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
8932.40
20091.00
60431.95
69648.06
67443.50
153123.69
157556.25
131334.94
78505.50
78068.19
18068.88
NO
LB/1K
LB FUEL
0.14
0.69
2.29
5.27
0.10
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
0.72 0.72
2.33 2.33
106.57 106.57
63.87 63.87
59.80 59.80
67.59 67.59
163.28 163.28
112.11 112.11
19.65 19.65
221.52 221.52
1.62 1.62
NO NO
LB/U EMISSION
HOURS LBS.
2.33 0.0005
67.59 0.0003
163.28 0.0136
221.52 0.0222
1.62 0.0001
0.0366
0.0024
1-87
-------
DATE: 8/17/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEDYNE-CONTINENTAL
ENGINE DATA
C»L ID NUMBER: 366 ENGINE TYPE AND MODEL: TSIO-SZO-E
RATED MORSEPOHER! 300.
ENGINE TOTAL TIME: 214. MRS
FUEL: AV GAS 100/130 FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA »««»««»«««««««««««»
INLET AIR TEMPERATURE, DEGREES F: START 91.00 FINISH 89.50
ATMOSPHERIC PRESSURE! START 30.20 FINISH 30.20
INLET AIR HUMIDITY, GKN H20/LB AIR: 0.02
RELATIVE HUMIDITY: 53.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/KIN: 7.00
SAMPLE LINE TRANSPORT TIME. SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER! 206193-9-E
9973
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 16.70
IDLE/TAXI 2 -0.0 33:20
RUN UP 3 -0.0 49.20
RUN UP-LEAN 4 -0.0 43.90
RUN UP-RICH 5 -0.0 24.60
TAKE-OFF 6 -0.0 105.50
CLIMB 7 -0.0 84.40
DESCENT 8 -0.0 77.40
APPROACH 9 -0.0 58.00
TAXI 10 -0.0 40.40
TEST
MOnE
I
2
3
4
5
6
7
1
9
10
TFST
MODE
1
2
3
4
5
6
7
a
9
10
TFST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES f
504.00
594.00
642.00
908.00
964.00
1278.00
1312.00
1244.00
1110.00
1186.00
MASS EMI
CO
LB/IK
LB FUEL
510.25
526.54
665.54
553.01
593.54
270.50
495.30
671.60
993.84
360.18
TIME IN
none
Ml N.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
206.36
33.04
0.14
11.46
10.58
9.22
a. 85
9.63
13.52
48.59
MEASURED
FUEL FLOW
LB/HR
15.20
105.50
34.40
58.00
40.40
FUEL
CO
(DRY)
PERCENT V
4.60
4.40
5.70
4.70
5.10
2.20
4.20
5.90
7.70
7.60
MSSS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
US CO
LOS.
7.04
0.53
7.01
5.8C
2.71
23.079
CO
2
(DRY)
PERCENT
9.80
12.00
11.60
12.30
12.10
14.10
12.80
11.70
9.50
9.50
MASS EMI
C02
LB/IK
LB FUEL
1774.96
2256.29
2128.13
2273.92
2212.61
2723.93
2371.74
2092.59
1732.73
16U9.4I
CO
LB/IK
LB FUEL
526.54
270.50
495.30
893.84
n&o.ie
THC
(DRY)
PPMV
V
31258.00
4821.00
21.46
1700.00
1588.00
1310.00
1310.00
1477.00
2034.00
7496.00
MASS EMI
NO
LB/IK
LB FUEL
0.32
3.86
4.72
2.90
3.06
38.45
15.73
4.88
2.96
0.89
LTD CYCLE
CO
LB/IK
HOURS
185J4.05
21537.27
41803.28
51842.56
34751. OR
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
1044.00 0.08043
466.00 0.07672
635.00 0.07881
585.00 0.07794
324.00 0.07888
1504.00 0.07393
1142.00 0.07758
997.00 0.08081
697.00 O.OR007
483.00 0.08212
NO
(DRY)
PPMV
17.00
44.00
246.00
150.00
160.00
1904.00
812.00
261.00
155.00
48.00
MASS [MI
NOX
LB/IK
LB FUEL
0.32
0.86
4.7?
?.90
3.06
38.45
15.73
4.88
2.96
0.89
EMISSIONS
cn
EMISSION
IBS.
J.707
0.143
3.470
5.184
2.328
14.832
0.643
NO
2
(DRY)
PPMV
-C.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-C.OO
-0.00
-C.OO
MASS EMI
CO
LB/HR
51275.28
18534.05
32744.73
24776.91
14601.15
28537.27
41803. 2d
51981.91
51842.56
34751.08
MC
LB/IK
LB FUEL
33.04
9.22
8.85
13.52
48.59
NO
X
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
19955.23
1163.06
7.06
502.91
260.38
973.21
746.75
745.29
784.32
1963.04
HC
LB/IK
HOURS
1163.06
97J.21
746.75
784.32
1963.04
ALDEHYDES SMOKE
(DRY)
40.00
27.00
-0.00
-0.00
-0.00
-0.00
20.00
9.00
29.00
14.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.233
0.005
0.062
0.078
0.132
0.509
0.022
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
coz
LB/HR
171638.38
79421.38
104703.94
99825.00
54430.28
287374.00
200174.88
161966.31
100498.06
68252.13
NO
LB/IK
IB FUEL
C.Bt>
38. 45
15.73
2.96
0.89
PARTICULATES
-0
-0
-0
-0
-0
-0
-0
-0
-0
-0
MASS EMI
NO
LB/HR
31.13
30.44
232.13
127.26
75.24
4056.74
1327.51
377.71
171.41
36.05
NO
LU/1K
HOURS
30.44
4056.74
1327.51
171.41
36.05
.00
.00
.00
.00
.00
.00
.00
.00
.00
.00
MASS EMI
NOX
LB/HR
31.13
30.44
232.13
127.26
75.24
4056.74
1327.51
377.71
171.41
36.05
NO
EMISSION
LBS.
0.0061
0.0203
C.1I02
0.0171
0.0024
0.1561
0.0068
1-88
-------
DATE: e/17/Tl
TEST ORGANISATION! SCOTt/SEN AVIATION
ENGINE SUPPLIER: TELEOYNE-CONTINENTAL
ENGINE OAT*
C»L ID NUMBER: 367 ENGINE TYPE AND NOOELI TSIO-JZO-E
RATED HORSEPOWER: 3CO.
ENGINE TOTAL TIHEl 214. MRS
FUEL" AV G»S 100/110 FUEL H/C RATIO: 1.1*0
OPERATIONAL DATA «*««»»****«»«««
INLET AIR TEMPERATURE, DEGREES Fi START 76.50 FINISH 77.50
ATMOSPHERIC PRESSUREI START 30.16 FINISH 30.16
INLET AIR HUMIDITY, CRN H20/LS AIR1 0.02
RELATIVE HUMIDITY: 79.00 PERCENT
SAMPLE LINEl TENPERATURE, DEGREES C: -0.00, FLO* RATE, LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TIME, SECI 1.60
NUMBER OF TESTS! 10
COMMENTS:
SERIAL NUMBER: 206113-«-EA
3975
CARD. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 -0.00
IDLE/TAXI 2 -0.0 33.40
RUN UP 3 -0.0 51.00
DUN UP-LEAN 4 -0.0 45.70
RUN UP-RICH 5 -0.0 28.10
TAKE-OFF 6 -0.0 126.60
CLIMB 7 -0.0 98.40
DESCENT 8 -0.0 87.90
APPROACH 9 -0.0 58.00
TAXI
TEST
NODE
I
2
3
4
5
6
7
a
9
10
TEST
NODE
1
2
3
4
5
6
7
e
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
605.00
673.00
953.00
930.00
998.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/1K
L8 FUEL
5B9.42
591.12
602.07
724.42
749.40
497.14
713.13
826.89
901.48
844.00
TIME IN
MODE
MIN.
12. 00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
189.33
53.07
15.59
12.50
12. SO
10.64
10. 57
11.97
14.29
45.26
MEASURED
FUEL FLO"
LB/HR
33 .40
126.60
99.40
58.00
36.90
FUEL
-0
CO
IDRYI
PERCENT V
4.50
4.60
.60
.80
.00
.80
.70
.70
7.50
7.00
MASS EMI
ND2
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
6* 68
0.63
a. 17
5.30
2.47
23.752
0
CO
2
(ORY)
PERCENT V
a. 40
10.40
9.80
10.20
10.00
11.50
10.30
9.50
9.10
9.10
MASS EMI
CO 2
LB/IK
LB FUEL
1728.73
2099.86
1871.25
2001.71
1962.46
2363.93
2024.75
1842.19
1718.60
1723.95
CO
LB/1K
LB FUEL
591.12
497.14
713.13
901.48
844.00
36.90
THC
(DRYI
PPMV
25238.00
7211.00
2240.00
1746.00
1748.00
1420.00
1475.00
1693.00
2076.00
6555.00
MASS EMI
NO
LB/IK
LB FUEL
0.28
0.99
3.99
2.61
7.61
21.47
4.50
3.43
2.64
1.03
LTO CYCLE
CO
LB/IK
HOURS
62938.32
70172.31
52285.99
31143.60
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
-0.00 0.07122
431.00 0.07196
631.00 0.07635
579.00 0.07413
353.00 0.07420
1706.00 0.07032
1253.00 0.07397
1080.00 0.07528
695.00 0.07746
443.00 0.
NO
IDRY)
PPMV
13.00
47.00
200.00
127.00
127.00
999.00
219.00
169.00
144.00
52.00
MASS EMI
NOX
LB/IK
LB FUEL
0.26
0.99
3.99
2.61
2.61
21.47
4.50
3.43
2.84
1.03
EMISSIONS
CO
EMISSION
LBS.
0.315
5.624
5.229
2.087
17.403
0.733
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
-0.00
19743.44
40905.38
33106.02
21058.15
62938.32
70172.31
72663.36
52265.99
31143.60
HC
LB/IK
LB FUEL
53.07
10.64
10.57
14.29
45.26
07720
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
-0.00
1772.56
795.11
571.43
351.36
1346.99
1039.99
1051.87
828.89
1670.26
HC
LB/IK
HOURS
1772.58
1346.99
1039.99
828.89
1670.26
ALDEHYDES SMOKE
IO«Y)
29.00
12.00
-0.00
-0.00
-0.00
-0.00
5.00
4.00
6.00
10.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.355
0.007
0.066
0.083
0.112
0.642
0.027
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI
CU2
LB/HR
-0.00
70135.31
95433.50
91476.19
55145.17
299273.19
199235.50
161926.19
99679.00
63613.68
NO
LB/IK
LB FUEL
0. 99
21.47
4.50
2.84
1.03
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
-0.00 -0.00
33.13 33.13
203.60 203.60
119.07 119.07
73.21 73.21
2717.80 2717.80
442.85 442.85
301.14 301.14
164.69 164.69
36.00 36.00
NO NO
LB/IK EMISSION
HOUHS LBS.
33 .13 0. 0066
2717.60 0.0136
442.85 0.0368
164.69 0.0165
38.00 0.0025
0.0760
0.0032
1-89
-------
DATE: B/IT/TI
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEDYNE-CONTINENTAl
ENGINE DATA
CAL ID NUMBER: 168 ENGINE TYPE AND MODEL: TSIO-520-E
RATED HORSEPOWER: 300.
ENGINE TOTAL TIKE: 21*. MRS
FUEL: AV GAS 100/130 FUEL H/C RATIO: 1.840
OPERATIONAL DATA ««««»««««
INLET AIR TEMPERATURE, DEGREES F: START T8.00 FINISH
ATMOSPHERIC PRESSURE: START 30.I* FINISH
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.02
RELATIVE HUMIDITY: 77.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/KIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER! 206193-9-E
77.00
30.14
S977
CARB. TEST ENGINE MEASURER
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 -0.00
IDLE/TAXI 2 -0.0 33.40
RUN UP 3 -0.0 52.70
RUN UP-LEAN 4 -0.0 49.20
RUN UP-RICH 5 -0.0 29.90
TAKE-OFF 6 -0.0 110. 80
CLIMB 7 -0.0 102.00
DESCFNT 8 -0.0 93.20
APPROACH 1 -0.0 59. 80
TAXI
TEST
NODE
1
2
3
4
5
6
7
8
t
10
TEST
MODF
1
?
3
4
5
b
7
9
1
10
ifsr
HIIHE
2
b
r
i
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
404.00
583.00
942.00
897.00
986.00
1256.00
1244.00
1233.00
1076.00
852.00
1ASS EMI
CO
LB/1K
LB FUEL
577.48
717.83
954.60
815.28
711.39
316.23
625.71
740. 19
B62.23
820.21
TIME IN
H006
HIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLF/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
IB/ IK
LB FUEL
236.16
62.93
16.92
14.55
12.01
9.99
10.28
10.35
13.81
29.62
MEASURED
FUEL FLOH
LB/HR
33.40
110.80
102.00
59.80
38.70
FUEL
-0.
CO
(DRY)
PERCENT V
5.10
6.20
8.20
7.50
5.80
2.40
5.00
6.10
7.30
7.00
MASS EMI
N02
LB/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
6.68
0.55
8.47
5.98
2.59
24.273
.0
CO
2
(DRY)
PERCENT V
9.10
10.30
8.90
9.40
10.50
12.80
11.00
10.40
9.60
9.80
MASS EMI
C02
LB/1K
L8 FUEL
1619.00
1873.73
1627.93
1743.36
2023.53
2649.96
2162.89
1962.83
1781.59
1804.24
CO
LB/U
LB FUEL
717.83
316.23
625.71
862.23
820.21
38.70
THC
(DRY)
PPMV
36416.00
9490.00
2538.00
2152.00
1710.00
1324.00
1435.00
1490.00
2042.00
4414.00
MASS EMI
NO
LB/1K
LB FUEL
0.30
0.74
4.55
1.59
2.58
39.87
11.16
6.66
3.63
1.39
LTD CYCLE
CO
LB/1K
HOURS
23975.59
35038.24
63822.55
51561.20
31742.28
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
-0.00 0.08215
415.00 0.07995
619.00 0.08007
593.00 0.07677
381.00 O.C7539
1564.00 0.06939
1330.00 0.07371
1176.00 0.07675
725.00 0.07864
472.00 0.
NO
(DRY)
PPMV
16.00
39.00
238.00
82.00
128.00
1842.00
543.00
334.00
187.00
72.00
MASS EMI
NOX
LB/1K
LB FUEL
0.30
0.74
«.5S
1.59
2.58
39.87
11.16
6.66
3.63
1.39
EMISSIONS
CO
EMISSION
LBS.
4.795
0.175
5.2')7
5.156
2.127
17.550
0.723
NO
2
IDRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-c.oo
-0.00
-0.00
MASS EMI
CO
LB/HR
-C.OO
23975.59
50307.37
43555.82
2127C.66
35038.24
63822.55
68985.69
51561.20
31742.28
HC
LB/IK
LB FUEL
62.93
9.99
10.28
13.81
29.62
C7920
NO
X
IORVI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
-0.00
2101.79
891.77
715.77
359.17
1107.04
1C49.06
965.07
826.04
1146.35
HC
L9/1K
HOURS
?101.79
1107.04
1049.06
826.04
1146.35
ALDEHYDES SMOKE
IORYI
32.00
26.00
-0.00
-0.00
-0.00
-0.00
6.00
8.00
3.00
2.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.420
0.006
0.087
0.083
0.077
0.672
0.028
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/HR
-0.00
62582.52
85791.81
85773.00
60503.49
293615.69
220615.06
184799.56
106539.19
69823.94
NO
LB/U
LB FUEL
0.74
39.87
11.16
3.63
1.39
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NU NOX
LB/HR LB/HR
-0.00 -0.00
24.77 24.77
239.84 239.84
78.22 78.22
77.11 77.11
4417.14 4417.14
1138.48 1138.48
62C.43 620.43
216.95 216.95
53.63 53.63
NO NO
LB/1H EMISSION
HOURS LBS.
24.77 0.0050
4417.14 0.0221
1138.46 C.0945
216.95 0.0217
53.63 0.0036
O.I46B
0.0060
1-90
-------
DATE: 8/17/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER I TELEDYNE-CONTINENTAL
ENGINE DATA
C»L 10 NUMBER! 369 ENGINE TYPE »HO MODEL 1 ISIO-520-E
RATED HORSEPOMERl 300.
ENGINE TOTAL TINEl 21*. MRS
FUELl AV GAS 100/130 FUEL H/C «ATtOl 1.840
OPERATIONAL OATA «»*««!»*«»«««««»«»«««»».
INLET AIR TEMPERATURE. DEGREES Fl START 75.50 FINISH 75.50
ATMOSPHERIC PRESSURE! START 30.14 FINISH 30.14
INLET AIR HUNI01TV, GRII H20/L8 AIRl 0.01
RELATIVE HUM1DITTI 76.00 PERCENT
SAMPLE LINEi TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/NIK: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: l.t.0
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER! 206211-9-E
S979
CARB. TEST ENGINE MEASURED
HEATER NODE RPM FUEL FLOU
LB/HR
IDLE-LOU 1 -0.0 -0.00
IDLE/TAXI 2 -0.0 22.90
RUN UP 3 -0.0 45.70
RUN UP-LEAN 4 -0.0 45.70
RUN UP-RICH 5 -0.0 43.90
TAKE-OFF 6 -0.0 130.10
CLIMB 7 -0.0 116.00
DESCENT B -0.0 107.20
APPROACH 9 -0.0 59.80
TAXI
TEST
MODE
I
2
3
4
5
6
7
a
9
10
TEST
MODE
I
2
8
t
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
471.00
560.00
930.00
908.00
964.00
1289.00
1267.00
1267.00
1076.00
841.00
MASS EMI
CO
LB/1K
LB FUEL
659.08
909.71
1152.39
1094.58
1100.12
606.99
998.51
1016. 10
1195.97
978.25
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
333.46
173.55
22.86
20.79
20.32
12.73
13.29
13.22
17.57
105.75
MEASURED
FUEL FLOW
L8/HR
22.90
130.10
116.00
59.80
19.30
FUEL
-0
CO
IDRYI
PERCENT V
6.60
8.90
10.30
9.60
9.70
4.80
4.50
8. 70
10.70
8.90
MASS EMI
N02
LD/1K
LB FUEL
0.0
o.o
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
L3S.
4.58
0.65
9.63
5. 98
1.29
22.132
0
CO
2
IORY)
PERCENT
7.80
7.90
7.40
7.80
7. BO
11.00
8.50
8.40
7.10
7.80
MASS EMI
C02
LB/IK
LS FUEL
1223. B6
1268.76
1300.86
1397.37
1389.95
2185.61
1568.89
1541.46
1246.90
1347.07
CO
LB/IK
LB FUEL
909.71
606.99
998.51
1195.97
978.25
19.30
THC
IDRVI
PPMV
V
58304.00
29646.00
3568.00
3184.00
3129.00
1757.00
1976.00
1976.00
2745.00
16799.00
MASS EMI
NO
LB/IK
LB FUEL
0.25
0.37
0.99
0.86
0.89
14.87
2.80
2.5V
0.99
0.61
LTD CYCLE
CO
LB/IK
KOUKS
20832.38
7B969.63
115827.25
71518.81
18880.16
MEASURED CALCULATED
AIR FLOU F/A
LB/HR
-0.00 0.09374
223.00 0.09162
497.00 0.08394
509.00 0.08219
488.00 0.08264
1703.00 0.07293
1344.00 0.07950
1235.00 O.CBOOO
640.00 0.08414
200.00 0.
NO
IDRYI
PPMV
15.00
22.00
54.00
47.00
4B.OO
716.00
145.00
135.00
54.00
34.00
MASS EMI
NOX
LR/1K
LB FUEL
0.25
0.37
0.99
0.88
0.89
14.87
2.80
2.59
0.99
0.61
EMISSIONS
CO
EMISSION
(.85.
4.166
0.395
9.614
7.152
1.265
22.592
1.021
NO
2
IDRV)
PPMV
-n.oo
-0.00
-0.00
-c.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
-0.00
20832.38
52664.07
50022.43
48295.13
78969.63
115827.25
108925.56
71518.81
18880.16
HC
LB/IK
Lfl FUEL
173.55
12.73
13.29
17.57
10?. 75
08524
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EH|
HC
LB/HR
-0.00
3974.30
1044.83
950.19
892.24
1655.53
1542.14
1416.91
1050.81
2041.01
HC
IB/IK
HOURS
3974.30
1655.53
1542.14
1050. 81
2041.01
ALDEHYDES SMOKE
IORYI
27.00
6.00
-0.00
-0.00
-0.00
-0.00
5.00
19.00
55.00
46.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
L8S.
0.795
0.008
0.128
0.105
0.137
1.173
0.053
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MASS EMI
C02
LB/HR
-0.00
29054.56
59449.36
63859.60
61018.92
284347.88
181990.69
165244.88
74564.63
25998.50
NO
IB/IK
LB FUEL
0.37
14.87
2.80
0.99
0.61
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
L8/HR LB/*R
-0.00 -0.00
8.46 8.46
4J.3J 46.35
40.23 40.23
39.25 39.25
1934.87 1934.87
324.55 324.55
277.63 277.63
59.29 59.29
11.85 11.85
NO NO
LB/IK EMISSION
HCURS L8S.
II. 46 0.0017
1934.87 0.0097
324.55 0.0269
59.29 0.0059
11.85 O.OOOB
0.0450
0.0020
1-91
-------
DATE: e/ir/7i
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEOYNE-CONTINENTAL
ENGINE DATA
CAL ID NUMBER: 370 ENGINE TYPE AND MODEL: TSIO-520-E
RATED HORSEPOWER: 300.
ENGINE TOTAL TIME: 214. MRS
FUEL: «V GAS 100/UO FUEL H/C RATIO: 1.840
OPERATIONAL DATA »»»«»«»»««
INLET AIR TEMPERATUREt DEGREES F: START 75.00 FINISH 74.00
ATMOSPHERIC PRESSURE: START 3C.14 FINISH 30.14
INLET AIR HUMIDITY, CRN H20/LB AIR] 0.01
RELATIVE HUMIDITY: 78.oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOM RATE, LITERS/HIM: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER I 206211-9-EA
9981
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
L8/HR
IOLF.-LOW 1 -0.0 -0.00
IDLE/TAXI 2 -0.0 19.30
RUN UP 3 -0.0 47. SO
RUN UP-LEAN 4 -0.0 45.70
RUN UP-RICH 5 -0.0 45.70
TAKE-OFF 6 -0.0 128.30
CLIMB 7 -0.0 114.30
DFSCFNT 8 -0.0 105.50
APPROACH 9 -0.0 58.00
TAXI
TEST
MODE
I
2
3
4
5
6
7
8
)
10
TEST
MODE
1
2
3
4
5
6
« 7
3
9
10
TEST
MODE
2
6
7
1
10
TOTAL
TOTAL
EXHAUST
GAS
TFMP
OEGREES f
448.00
583.00
919.00
R97.00
164.00
1267.00
1278.00
1278.00
1087.00
B63.00
MASS EMI
CO
LB/IK
LO FUEL
669.94
229.25
1 1 5 5 . 46
1090.01
1170.43
568.27
905.21
974.07
1196.88
991.94
TIMF IN
MODE
MIN.
12.00
0.30
5.00
6.00
4. 00
FOR CYCLF
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
446.08
43.25
25.43
23.84
22.25
14.13
13.64
13.40
19.00
100.09
MEASURED
FUEL FLUW
LB/HR
19.30
128.30
114.30
58.00
19.30
FUEL
-0.
CO
(DRY!
PERCENT V
6.80
t.90
10.00
9.20
9.50
4.30
7.30
a. oo
10.30
8.60
MASS EMI
NU2
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUFL
USED
LBS.
1.B6
0.64
9.49
5.30
1.29
21.081
.0
CO
2
IDRY)
PERCENT V
5.80
66.60
7.10
7.50
7.30
10.80
8.80
8.40
6. BO
7.40
MASS EMI
C02
LB/IK
LB FUfL
897.83
2695.40
1288.99
1316.1 8
1352.76
2242.59
1714.53
1607.01
1241.54
1341.09
CO
LR/IK
Lfl FUEL
229.25
568.27
909.21
1 196. 8H
991.94
19.30
THC
(ORYI
PPMV
79056.00
29317.00
3843.00
3514.00
3294.00
1867.00
1921.00
1921.00
2855.00
15152.00
MASS [Ml
MO
LB/IK
LB FUEL
0.15
0.08
0.99
0.91
0.91
17. 13
4.22
2.96
0.94
0.70
LTD CYCLE
CO
LB/IK
HOURS
4424.43
72909.25
103465.00
69419.25
19144.41
MEASURED CALCULATED
AIR FLOU F/A
LB/HR
-0.00 0.09587
181.00 0.28822
514.00 0.08137
508.00 O.C7919
503.00 0.07964
1696.00 0.06984
1368.00 0.07518
1231.00 0.07672
619.00 0.08103
201.00 0.
NO
IORYI
PPNV
9.00
19.00
52.00
47.00
47.00
789.00
207.00
148.00
49.00
37.00
MASS EMI
NOX
LB/IK
L8 FUEL
0.15
0.08
0. 99
O.V1
0.91
17.11
4.72
2.96
0.94
0.70
EMISSIONS
CO
EMISSION
LBS.
0.865
0.365
8.588
6.942
1.283
18.062
0.857
NO
2
IDRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MASS EMI
CO
LB/HR
-c.oo
4424.43
548B4. 18
49813.35
51203.47
729C9.25
103465.00
102764.44
69419.25
19144.41
HT
LB/IK
19 FUEL
43.25
14.13
13.64
19.00
ICC. 09
08136
NO
X
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
-0.00
834.70
1207.99
1C89.69
1016.82
1813.03
1559.35
1413.27
1 102.03
1931.79
HC
LB/IK
HOURS
834.70
1H13.03
1559.35
1102.03
1931.79
ALDEHYDES SMOKE
(DRY )
19.00
5.00
-0.00
-0.00
-0.00
-0.00
8.00
17.00
53.00
62.00
MASS FHI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.167
0.009
0.129
O.UO
0.129
0.545
0.076
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/HR
-0.00
52021.16
61227. OR
63805.40
61821.13
287724.31
195971.00
169539.25
72009.44
258B2.93
NO
LB/IK
LB FUEL
0.03
17.13
4.22
0.94
0.70
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
-0.00 -0.00
1.55 1.55
46.88 46.88
41.80 41. BO
41.61 41.61
2197.41 2197.41
481.91 481.91
312.27 312.27
54.24 54.24
13.53 13.53
NO NO
LB/IK EMISSION
HOURS LBS.
1.55 0.0003
2197.41 0.0110
481.91 C.0400
54.24 0.0054
13.53 0.0009
0.0576
0.0027
1-92
-------
D»TEl 8/1T/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEDYNE-CONTINENTAL
ENGINE OAT*
CAL ID NUMBER! 171 ENGINE TYPE AND NOOELI TS10-520-E
RATED MORSEPOHERI 300.
ENGINE TOTAL TINEl 214. MRS
FUEL: AV GAS 100/110 FUEL H/C RATIOI 1.1*0
OPERAT10NAL OAT A ««»»»«»«»
INLET AIR TEMPERATUREt DEGREES Ft START 73.00 FINISH T3.00
ATMOSPHERIC PRESSURE! START 30.14 FINISH 30.1*
INLET AIR HUMIDITY, GRN H20/LB AIR! 0.01
RELATIVE HUMIDITY! 6.20 PERCENT
SAMPLE LINE! TEMPERATURE. DEGREES Ci -0.00, FLO* RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS!
SERIAL NUMBER: 20621I-«-EB
9983
CARS. TEST ENGINE MEASURED
HEATER MODE RPH FUEL FLOK
LB/HR
IDLE-LOU 1 -0.0 -0.00
IDLE/TAXI 2 -0.0 22.40
RUN UP 3 -0.0 47.50
RUN UP-LEAN 4 -0.0 45. TO
RUN UP-RICH 5 -0.0 43.90
TAKE-OFF 6 -0.0 128.30
CLIMB 7 -0.0 114.30
DESCENT 8 -0.0 105.50
APPROACH 9 -0.0 56.30
TAXI
TEST
NODE
1
2
3
4
5
6
7
a
9
10
TEST
MODE
1
2
3
4
5
6
7
e
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
FXHAUST
CAS
TEMP
DEGREES F
448.00
560.00
930.00
919.00
964.00
1334.00
1300.00
1278.00
1076.00
852.00
KISS EMI
CO
LB/IK
LB FUEL
577.27
642.26
1092.98
1045.66
1068.64
525.53
911. 18
976.24
1213.01
970.46
TINE IN
NODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSU
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
187.23
145.49
20.06
18.51
17.61
11.83
11.66
12.18
17.95
114.12
MEASURED
FUEL FLOU
LB/HR
22.90
128.30
114.30
56.30
21.10
FUEL
-0.
CO
(DRY)
PERCENT V
4.50
5.20
9.80
9.10
9.40
4.10
7. TO
8.40
11.10
8.90
MASS EMI
N02
LB/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
4.58
0.64
9.49
5.63
1.41
21.752
,0
CO
2
(DRY)
PERCENT V
8.70
9.10
8.00
8.20
8.10
11.50
9.20
8.80
7.10
7.80
MASS EMI
C02
L6/1K
LB FUEL
1753.58
1765.98
1401.89
1480.48
1446.86
2316. OT
1710.57
1606.93
1219.09
1336.36
CO
LB/1K
L8 FUEL
642.26
525.53
911.18
1213.01
970.46
21.10
THC
IORY)
PPMV
25483.00
20567.00
3141.00
2813.00
2704.00
1611.00
1721.00
1830.00
2868.00
18273.00
MASS EMI
NO
LB/IK
LB FUEL
0.38
0.65
1.30
1.09
1.06
22.28
4.02
2.75
0.84
0.61
LTD CYCLE
cn
LB/1K
HOURS
147C7.70
67425.69
104148.13
68292.19
20476. 11
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
-0.00 0.07262
256.00 O.OT531
529.00 0.08396
519.00 0.08140
495.00 0.08232
1720.00 0.07178
1367.00 0.07865
1233.00 0.08024
598.00 0.08608
218.00 0.
NO
IORY)
PPMV
18.00
32.00
71.00
58.00
57.00
1058.00
207.00
144.00
47.00
34. OU
MASS EMI
NOX
LB/IK
L6 FUEL
0.38
0.65
1.30
1.09
1.06
22.28
4.02
2.75
0.84
0.61
EMISSIONS
CO
EMISSION
LBS.
2.942
0.337
8.644
6.829
1.372
20.124
0.925
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
-C.OO
14707.70
51916.43
47786.85
46913.41
67425.69
104148.13
102993.19
68292.19
20476.79
HC
LB/1K
LB FUEL
145.49
11.83
11.66
17.95
114.12
08592
NO
X
(ORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
-0.00
3331.64
953.00
846.02
772.90
1517.34
1333.17
1285.07
1010.58
2407.84
HC
LB/1K
HOURS
3J3I.64
1517.34
1333.17
1010.58
2407.84
ALDEHYDES SMOKE
IORYI
27.00
23.00
-0.00
-0.00
-0.00
-0.00
25.00
29.00
8.00
19.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
o.o
0.0
HC
EMISSION
LBS.
0.666
0.008
0.111
0.101
0.161
1.047
0.048
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
-0.00
40440.92
66589.63
67658.00
63517.33
297151.31
195518.19
169531.38
68634.88
28197.11
NO
LB/1K
LB FUEL
0.65
22. 28
4.02
0.84
0.61
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LG/HR LB/HR
-0.00 -0.00
14.87 14.87
61.78 61.78
50.03 50.03
46.73 46.73
2857.90 2857.90
459.89 459.89
290.01 290.01
47.50 47.50
12.85 12.85
NO NO
LB/IK EMISSION
HOURS LBS.
14.87 0.0030
2857.90 0.0143
459.89 0.0382
47.50 0.0047
12.85 0.0009
0.0610
0.0028
1-93
-------
DATE: 7/28/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOMING
ENGINE OAT*
C«L ID NUMBER: 2»* ENGINE TYPE AND NODELl IO-540-C4B5
RATED HORSEPOWER: 250.
ENGINE TOTAL TINE: 17*7. HRS
FUEL: AV GAS 100/130 FUEL H/C RATIO: ua»o
OPERATIONAL DATA .«».«»....».».««««..»...«.»«»»»«»»«»»«
INLET AIR TEMPERATURE, DEGREES f. START 77.00 FINISH 77.00
ATMOSPHERIC PRESSURE: START 29.82 FINISH 29.82
INLET AIR HUMIDITY. CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 40.00 PERCENT
SAMPLE LINE: TEMPERATUREi OEGREES C: -0.00, FLOM RATE, LITERS/KIN: 7.00
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUNBERl L-6246-48AA
9999
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLO*
LB/HR
IOLE-LOH 1 -0.0 15.20
IDLE/TAXI 2 -0.0 17.60
RUN UP } -0.0 56.30
RUN UP-LEAN 4 -0.0 56.30
RUN UP-RICH 5 -0.0 57.40
TAKE-OFF 6 -0.0 117.20
CLIMB 7 -0.0 105.50
DESCENT 8 -0.0 78.50
APPROACH 9 -0.0 46.40
TAXI
TEST
NODE
1
2
3
4
5
6
7
a
i
10
TEST
MODE
1
2
)
',
5
6
7
a
9
10
fESI
Mtirjf
2
6
7
1
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
740.00
762.00
1211.00
1278.00
1256.00
1323.00
1244.00
1211.00
1121.00
795.00
MUSS EMI
CO
LB/1K
19 FUEL
1064. BO
1038.14
1175.55
1 142.66
1130.23
1188.48
1175.82
1 172. 86
1139. 71
1142.85
TIME IN
MUOE
M1N.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
HC
LB/IK
LB FUEL
187.72
65.83
23.48
22.23
17.77
17.05
19.41
21.34
23.71
184.76
MFASUREO
FUEL FLOM
LB/HR
17.60
117.20
105.50
46.90
17.60
FUEL
-0.
CO
IDRY)
PERCENT V
9.50
3.50
9.80
9.40
10.00
12.30
10.30
1.70
1.10
10.30
MASS EMI
N02
LB/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
L9S.
3.52
0.59
8.76
4.69
1.18
18.732
.0
CO
2
IDRY)
PERCENT
5.60
7.10
6.70
6.90
7.60
8.30
7.10
6.70
6.70
5.00
MASS EMI
C02
LB/IK
LB FUEL
986.21
1362.49
1262.78
1317.88
1349.65
1260.10
1271.51
1272.88
1318.46
871.69
CO
LB/IK
IB FUEL
1038.14
iiga.48
1175.82
1139.71
1142.85
17.60
THC
IORYI
PPMV
V
29243.00
9411.00
3417.00
3193.00
2745.00
3081.00
2969.00
3081.00
3305.00
29075.00
MASS EHI
NO
LB/IK
LB FUEL
0.13
0.4fl
1.28
1.06
0.93
1.33
1.09
1.19
1.38
0.18
LTO CYCLE
CO
L9/1K
HOURS
18271.27
139290.06
124049.25
53452.51
20114.12
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
135.00 0.08444
194.00 0.07694
605.00 0.07852
613.00 0.07740
632.00 0.08301
1261.00 0.09688
1138.00 0.08237
847.00 0.07789
512.00 0.07518
149.
NO
(DRY)
PPMV
7.00
24.00
65.00
53.00
50.00
84.00
58.00
60.00
67.00
10.00
MASS EMI
N0>
LB/IK
L,) FUEL
0.13
0.48
1.28
1.06
0.93
1.33
1.09
1.19
1.38
0.18
EMISSIONS
CO
EMISSION
LBS.
3.654
0.696
10.296
5.345
1.348
21.340
1.139
00 0.
NO
2
(DRY)
PPMV
-0.00
-C.OO
-0.00
-C.OO
-0.00
-0.00
-o.oo
-0.00
-0.00
-o.oo
MASS EMI
CO
LP/HR
16184.9?
18271.27
66183.56
64331.74
64875.35
139290.06
124049.25
92069.50
53452.51
20114.12
HC
LB/IK
LB FUEL
65.33
17.05
19.41
23.71
184.76
08SS5
NO
X
(DRV)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EHI
HC
LR/HR
2853.34
1158.59
1321.64
1251.53
1019.92
1998.26
2047.92
1674.87
1111.34
3251.84
HC
LA/IK
HOURS
1158.59
1998.26
2047.92
1111.84
3251.84
ALDEHYDES SMOKE
IORYI
28.00
5.00
-0.00
-0.00
-0.00
-0.00
7.00
6.00
6.00
22.00
MASS EMI
NO 2
LB/HR
o.n
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
UBS.
0.232
0.010
0.170
0.111
0.218
0.741
0.040
-0.00
-O.JO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HK
14990.40
23979.82
71094.63
74196.69
77469.56
147683.31
134354.88
99921.13
61835.74
15341. 6j
NO
LB/IK
LB FUEL
C.48
1.33
1.09
1.38
0.18
PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.ao
-o.oo
:iiS5 EMI '(SS EMI
NO NOX
LB/HR LB/HR
1.96 1.96
8.47 8.47
72. 1C 72.10
59.58 59.58
53.28 53.28
156.25 156.25
114.74 114.74
93.54 93.54
64.64 64.64
3.21 3.21
NO NO
LB/IK EMISSION
HOURS LBS.
8.47 0.0017
156.25 0.0008
114.74 0.0095
64.64 0.0065
3.21 0.0002
0.0167
0.0010
1-94
-------
DATEl 7/28/71
TEST ORGANIZATION! SCOTT/GEN »VI»TION '.
ENGINE SUPPLIERI LYCOMING
ENGINE D»I» «»»»«**»»
CtL ID NUNBERI 2*9 ENGINE TYPE >NO KOOELI IO-S40-C489 SERIAL NUMBERI L-6246-48B
RATED HQRSEPOMERl 250.
ENGINE TOTAL TINEl 1T««. MRS
FUEL: »v o»s too/no FUEL H/C RATIOI i.«*o
OPERATIONAL OAT* «***»««»*»»««««»»»«*«
INLET AIR TENPERATUREi DEGREES Ft START 82.00 FINISH 81.00
ATMOSPHERIC PRESSURE! START 29.82 FINISH 24.12
INLET AIR HUMIDITY. CRN H20/LB AIRI 0.01
RELATIVE HUMIOITYl 92.00 PERCENT
SAMPLE LINE) TEMPERATURE. DEGREES Ct -0.00, FLOM RATE, LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TINE, SECl 1.60
NUMBER OF TESTSl 10
COMMENTS:
0001
CARB. TCST ENGINE MEASURED
HEATER MODE RPM FUEL FLOU
IB/ KB
1 OLE-toy 1 -0.0 17.60
IDLE/TAXI 2 -0.0 14.90
RUN UP J -0.0 52.70
RUN UP-LEAN 4 -0.0 51.60
RUN UP-RICH S -0.0 51.60
TAKE-OFF 6 -0.0 140.60
CLIMB 7 -0.0 111.30
DESCENT B -0.0 94.60
APPROACH 4 -0.0 60.90
TAXI
TEST
NODE
1
2
3
*
5
6
7
S
9
10
TEST
MODE
1
2
3
4
5
6
7
B
9
10
TEST
OOF
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
572.00
684.00
1143.00
1143.00
1177.00
127B.OO
1278.00
1244.00
1087.00
762.00
MASS ENI
CO
LB/1K
LB FUEL
848.64
948.88
1142.66
1D94.03
1134.13
1217.57
1241.45
1227.75
1223.49
1154.62
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MASS EMI
HC
LB/1K
LB FUEL
371.21
157.09
26.66
51.07
24.12
18.28
16.87
15.15
16.77
205.02
MEASURED
FUEL FLCIB
LB/HR
19.90
140.60
111.30
60.90
15.20
FUEL
-0.
cn
(DRY)
PERCENT V
7.30
7.50
8. BO
8.40
8.60
10.90
11.10
11.70
11.00
11.60
MASS EMI
NO 2
LB/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
UBS.
3.48
0.70
4.24
6.04
1.02
21.029
,0
CO
2
IORYI
PERCENT V
4.50
6.30
6.40
6.40
6.40
6.90
6.70
7.30
6.90
5.10
MASS EMI
CO 2
LB/1K
LB FUEL
822.15
1252.36
1305.73
1309.68
1326.12
1211.03
1177.38
1203.61
1205.85
797.61
CO
LB/IK
IB FUEL
948.88
1217.57
1241.45
1223.49
1154.62
15.20
THC
(DRY)
PPMV
55740.00
21680.00
3585.00
7115.00
3193.00
2857.00
2633.00
2521.00
2633.00
35965.00
MASS EMI
NO
LB/1K
LB FUEL
0.29
0.83
1.62
1.26
1.32
1.43
0.79
O.B1
0.86
-0.00
LTD CYCLE
CO
LB/IK
HOURS
18882.75
171189.88
136172.81
74510.38
17550.20
MEASURED CALCULATED
AIR FLOH F/A
LB/HR
128.00 0.08173
195.00 0.07451
572.00 0.07261
562.00 0.07237
563.00 0.07148
1488.00 0.08428
1165.00 0.08426
1053.00 0.08958
644.00 0.08464
124.00 0.
NO
IDRYI
PPMV
15.00
40.00
76.00
59.00
61.00
78.00
43.00
47.00
47.00
-0.00
MASS EMI
NOX
LB/IK
LB FUEL
0.29
0.83
1.62
1.26
1.32
1.43
0.79
0.81
0.86
-0.00
EMISSIONS
CO
EMISSION
LBS.
3.777
0.856
11.468
7.451
1.176
24.728
1.176
NO
2
(ORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
ca
IB/MR
14939.54
18882.75
60218.15
56451.69
58520.89
171189.88
138172.81
122283.75
74510.38
17550.20
HC
LB/IK
LB FUEL
157.04
18.28
16.87
16.77
205.02
09538
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
6533.21
3126.14
1405.01
2738.53
1244.39
2569.85
1877.14
1509.04
1021.46
3116.38
MC
LB/IK
HOURS
3126.14
2569.85
1877.14
1021.46
3116.38
ALDEHYDES SMOKE
(ORYI
40.00
31.00
-0.00
-0.00
-0.00
-0.00
19.00
7.00
5.00
24.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.625
0.013
0.156
0.102
0.209
1.105
0.053
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
CO 2
LB/HR
14469.84
24922.01
68811.81
67574.63
68427.50
170270.31
131042.64
119879.31
73436.38
12123.64
NO
LB/IK
LB FUEL
0.83
1.43
0.79
0.36
-o.no
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MISS EMI
NO NOI
LU/HR LB/HR
5.04 5.04
1*.54 16.54
85.42 85.42
65.13 65.13
68.18 68.18
201.22 201.22
87.92 87.92
80.69 80.64
52.24 52.24
-0.00 -0.00
NO NO
LB/IK EMISSION
HOURS LBS.
16.54 0.0033
201.22 0.0010
87.42 0.0073
52.24 0.0052
-0.00 -0.0000
-0.0000
-0.0000
1-95
-------
DATE: 7/28/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: LYCOMING
ENGINE DAT*
CAL ID NUMBER: 2*6 ENGINE TYPE AND MODEL: IO-54O-C4B5
DATED HORSEPOMER: 290.
ENGINE TOTAL TIMEl 17*8. MRS
FUEL! AV GAS 100/130 FUEL H/C RATIQ1 1.640
OPERATIONAL DATA «««««»»««««*«»»«««««««.»»»«....»,
INLET AIR TEMPERATURE. DEGREES F: START S2.00 FINISH 82.00
ATMOSPHERIC PRESSURE! START 29.82 FINISH 29.82
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 55.00 PERCENT
SAMPLE LINE: TEMPERATURE, CEGREES C: -0.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER! L-62»fr-«SC
G003
CARS. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOM
LB/HR
IDLE-LOU 1 -0.0 17.60
IDLE/TAXI 2 -0.0 21.10
RUN UP 3 -0.0 56.30
RUN UP-LEAN 4 -0.0 56.30
DUN UP-RICH 5 -0.0 56.30
TAKE-OFF 6 -0.0 MO. 60
CLIMB 7 -0.0 111.30
DESCENT 8 -0.0 96.10
APPROACH 9 -0.0 63.30
TAXI 10 -0.0 15.20
TEST EXHAUST EXHAUST CD CO THC
WIDE CAS GAS I!)RY) 2 IORYI
TEMP PRESSURE PERCENT V (DRYI PPMV
1
2
3
4
5
6
7
a
9
10
TEST
NUDE
1
2
3
4
5
6
7
B
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
DEGREES F
560.00
650.00
1110.00
1110.00
1132.00
1289.00
1256.00
1256.00
1121.00
751.00
MASS EMI
CO
LB/1K
LB FUEL
706.12
765.03
1197.93
1148. ?5
1196.47
1257.70
1291.53
1249.88
1250.
-------
OATEl 7/28/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOMING
ENGINE 0»T»
C»L ID NUNBERl 2*7 ENGINE TYPE AND MODEL I IO-540-C4B9
RATED HORSEPOWER! 290.
ENGINE TOTAL TINEI 1760. HIS
FUELl »V G»S 100/130 FUEL H/C RATIO! 1.8*0
OPERATIONAL DATA «««««».
INLET AIR TENPERATURE. DEGREES Ft START 65.00 FINISH 70.00
ATMOSPHERIC PRESSURE! START 29.10 FINISH 24.10
INLET AIR HUMIDITY, CRN H20/LB AIRI 0.01
RELATIVE HUMIDITY! 95.00 PERCENT
SAMPLE LINE! TEMPERATURE, OEGREES Cl -0.00, FLOV RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTSi 10
COMMENTS:
SERIAL NUNBERl 1-623*-*8A
7.00
0005
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOH
LB/HR
IDLE-LOU 1 -0.0 19.30
IDLE/TAXI 2 -0.0 22.90
RUN UP 3 -0.0 61.50
RUN UP-LEAN * -0.0 61.50
RUN UP-RICH 5 -0.0 59.80
TAKE-OFF 6 -0.0 149. *0
CLIMB 7 -0.0 109.00
DESCENT 8 -0.0 96.70
APPROACH 9 -0.0 52.70
TAXI
TEST
MODE
1
2
3
*
5
6
7
S
1
10
TEST
MODE
1
2
3
*
5
&
7
a
9
10
TEST
HOOf
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TENP
OEGREES F
852.00
830.00
1267.00
1233.00
1390.00
1*46.00
1412.00
1345.00
1199.00
807.00
MASS EMI
CO
LB/IK
LB FUEL
1087. 78
1)07.10
1124.39
1131.75
1144.77
1150.73
1126.62
1133.00
1126.76
1055.21
TINE IN
MODE
KIN.
12.00
0.30
5.00
6.09
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS ENJ
HC
LB/IK
LB FUEL
127.45
24.53
18.23
17.60
16.50
14.28
16.46
16.55
19.05
59.49
MEASUREI1
FUEL FLOU
LB/HR
22.90
149.40
1 09. 00
52.70
22.90
FUEL
-0
CO
IORYI
PERCENT V
.50
.00
.50
.50
.60
1 .90
.90
.90
.30
.70
MASS EMI
ND2
LB/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
IBS.
4.58
0.75
9.05
5.27
1.53
21.178
0
CO
2
IORY)
PERCENT V
6.20
a. TO
7.30
7.20
7.10
8.00
7.60
7.50
7.10
7.10
MASS EMI
C02
LB/1K
LB FUEL
1115.44
1838.81
1357.55
1347.72
1330.28
1327.02
1358.92
1348.64
1351.59
1353.06
CO
L8/1K
LB FUEL
807.10
1150.73
1126.62
1126.76
IOS5. 21
22.90
THC
(ORYI
PPMV
19435.00
3184.00
2690.00
2580.00
2416.00
2361.00
2525.00
2525.00
2745.00
8564.00
MASS EMI
NO
IB/ IK
LB FUEL
0.15
.15
.46
.29
.06
.97
.21
.22
.09
0.72
LTD CYCLE
CO
LO/IK
HOURS
18482.66
171919.56
122601.56
59380.32
24164.35
MEASURED CALCULATED
AIR FLOH F/A
LB/HR
185.00 0.08243
280.00 0.06929
678.00 0.07936
677.00 0.07887
655.00 0.07884
1635.00 0.08874
1200.00 0.08244
1062.00 0.08201
579.00 0.07758
252.00 0.
NO
I DRY!
PPMV
e.oo
52.00
75.00
66.00
54.00
56.00
65.00
65.00
55.00
36.00
MASS Ell
NOX
LH/1K
LB FUEL
0.15
1.15
1.46
.29
.06
.97
.21
.22
.09
0.72
EMISSIONS
CO
EMISSION
LBS.
3.697
0.860
10.193
5.938
1.619
22.306
1.053
NO
2
IDRV)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS ENI
CO
LB/HR
20994.13
18482.66
69150.00
69602.69
68457.25
171919.56
122801.56
109561.25
59380.32
24164.35
HC
L8/1K
LB FUEL
24.53
14.28
16.46
19.05
59.49
07748
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
2459.82
561.74
1121.41
1C62.60
986.71
2132.75
1793.80
1600.40
1003.80
1362.32
HC
LB/1K
HOURS
561.74
2132.75
1793.80
1003.80
1362.32
ALDEHYDES SMOKE
(DRY)
8.00
10.00
-0.00
-0.00
-0.00
-0.00
9.00
7.00
13.00
8.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
o.n
0.0
0.0
0.0
HC
EMISSION
LBS.
0.112
0.011
0.149
0.100
0.091
0.464
0.022
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS E*l
CO 2
LB/HH
21528.01
42108.63
63*89.13
82884.4*
79550.88
198256.31
148122.25
130413.06
71228. 88
30985.06
NO
LB/1K
LB FUEL
1.15
0.9f
1.21
1.09
0.72
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI MASS EMI
NU NOX
LB/HR LB/HR
2.90 2.90
26.31 26.31
89.67 89.67
79.43 79.43
63.25 63.25
145.08 145. 08
132.43 132.43
118.16 118.16
57. 6B 57.68
16.42 16.42
NO NO
L8/1K EMISSION
HCURS LBS.
26.31 0.0053
145.08 0.0007
112.43 C.0110
57.68 0.0058
16.42 0.0011
0.0238
0.0011
1-97
-------
DATE: T/28/TI
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER: LYCOMING
ENGINE DATA
CAL ID NUMBER! 2*8 ENGINE TYPE »NO MODEL! IO-540-C4B5
RATED KORSEPOKER: 250.
ENGINE FOTAL TINE! 1761. MRS
FUEL: AV GAS 100/130 FUEL H/C RATIOI 1.840
OPERATIONAL DATA «««»..«»»««»««.«»««««..
INLET AIR TEMPERATURE, DEGREES F: START 71.00 FINISH Tl.OO
ATMOSPHERIC PRESSURE: START 29.eo FINISH 29.BO
INLET AIR HUMIDITY, CRN H2Q/LB AIR: 0.01
RELATIVE HUMIDITY: 84.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOM RATE, LITERS/NIN:
SAHPLE LINE TRANSPORT TINE, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER: L-62i«-*sB
0007
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOM 1 -0.0 24.60
IDLE/TAXI 2 -0.0 24.60
RUN UP 3 -0.0 59.80
RUN UP-LEAN 4 -0.0 61.50
RUN UP-RICH 5 -0.0 58.00
TAKE-OFF 6 -0.0 133.60
CLIMB 1 -0.0 105.50
DESCENT B -0.0 96.70
APPROACH 9 -0.0 58.00
TAXI
TEST
MODE
1
2
3
4
5
6
7
a
9
10
TEST
mot
i
2
3
4
5
6
7
8
9
10
TEST
MODE
2
IS
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
673.00
773.00
1300.00
1233.00
I368.no
1368.00
1356.00
1334.00
1222.00
POT. CO
MASS EMI
CO
LB/IK
LB FUEL
745.00
805.35
1141.27
1111.12
1076.27
1149.71
1134.41
1 149.17
1135.07
953.73
TIME IN
HOOE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOB CYCLE/LB
10
EXHAUST
GAS
PKESSUKF.
PSIA
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
237.48
115.26
20.28
19.76
18.02
17.38
16.74
17.13
17.65
162.63
MEASURED
FUEL FLOW
LR/HR
24.60
133.60
105.50
58.00
22.90
FUEL
-0
CO
(DRYI
PERCENT V
5.80
5.80
9.20
9.00
9.20
10.40
9.80
9.70
9.30
7.80
KASS EMI
NO 2
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
3.0
0.0
FUEL
USED
LRS.
4.92
0.67
8.76
5.80
1.53
21.679
0
CO
2
(DRY)
PERCENT
6.70
7.30
6.80
6.80
7.80
7.60
7.40
7.10
7.00
6.40
MASS FMI
C02
LB/IK
LB FUEL
1352.19
1592.64
1325.40
1342.80
1433.73
1320.10
1345.90
1321.63
1342.38
1229.56
CO
LB/IK
LB FUEL
805.35
1149.71
1134.41
1135.07
953.73
22.90
THC
IDRYI
PPNV
V
32281.00
14494.00
2855.00
2745.00
2690.00
2745.00
2525.00
2525.00
2525.00
23223.00
PASS EMI
NO
LB/IK
LB FUEL
0.68
.32
.75
.20
.10
.05
.29
.21
1.12
1.16
LTO CYCLE
CO
LB/IK
HOURS
19811.60
153601.69
119680.31
65833.81
21840.42
MEASURED CALCULATED
AIR FLO* F/A
LB/HH
235.00 0.07321
269.00 0.06754
653.00 0.07587
675.00 0.07488
651.00 O.CB010
1459.00 0.08488
1157.00 0.08111
1056.00 0.07936
636.00 0.07705
221.00 0.
NO
IDRYI
PPMV
32.00
58.00
86.00
58.00
57.00
58.00
68.00
62.00
56.00
58.00
MASS EMI
NOX
LB/IK
LB FUEL
0.68
.32
.75
.20
.10
.05
.29
.21
.12
.16
EMISSIONS
CO
EMISSION
LBS.
3.962
0.764
9.933
6.583
1.463
22.710
1.048
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-0.00
-c.oo
MASS EMI
CO
LB/HR
18326.87
19811.60
68247.94
69563.56
62423.84
153601.69
119680.31
111125.00
65633.81
21840.42
HC
LB/IK
LB FUEL
115.26
17. 38
16.74
17.65
162.63
07707
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS THI
HC
LB/HR
5841.88
2835.47
1212.98
1215.14
1045.35
2321.94
1766.05
1656.71
1023.70
3724.18
HC
LB/IK
HOURS
2835.47
2321.94
1766.05
1023.70
3724.18
ALDEHYDES SMOKE
IDRYI
18.00
14.00
-0.00
-0.00
-0.00
-0.00
8.00
6.00
6.00
14.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.567
0.012
0.147
0.102
0.250
1.077
0.050
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-n.oo
MASS FMI
CO 2
LB/HR
33263.93
39178.92
79259.00
82582.19
83156.31
176365.88
141992.61
127801.69
77857.68
28156.90
NO
L8/K
LB FUEL
1.32
1.05
1.29
1.12
1.16
PARIICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
1ASS EIM MASS EMI
NO NOX
LB/HR LB/HR
16.61 16.61
32.54 32.54
104.79 104.79
73.64 73.64
63.53 63.53
140. II 140.71
1)6. « 136.40
116.67 116.67
65.11 65.11
26.66 26.66
NO NO
LB/IK EMISSION
HOURS LBS.
32.54 0.0065
140.71 0.0007
136. 4C 0.0113
65.11 0.0065
26.68 0.0018
0.0268
0.0012
1-98
-------
DATE! 7/28/71
TEST ORGANIZATION: SCOTT/GEN »Vt»MON
ENGINE SUPPLIER! LYCONING
ENGINE 0»I»
C»L ID NUMBER: 2*9 ENGINE TYPE AND NOOELI io-»40-c*8»
RATED MORSEPOHERl 250.
ENGINE TOTAL TINE: 1741. H«S
FUELl AV GAS 100/130 FUEL H/C RATIO) 1.6*0
OPERATIONAL DATA »»*»»«»«»»*»«»
INLET AIR TEMPERATURE. DEGREES Fl START Tl.OO FINISH Tl.OO
ATMOSPHERIC PRESSUREl START 29.73 FINISH 29.7}
INLET AIR HUMIDITY, CRN H20/LB AIRl 0.02
RELATIVE HUMIDITY! It.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES Cl -0.00, FLOM RATE. LITERS/MINI T.OO
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER: L-62J9-48C
3009
CARB. TEST ENGINE MEASURED
HEATER NODE RPM FUEL FLOM
LB/HR
IOLE-LON 1 -0.0 2*. 60
IDLE/TAXI ;i -0.0 26. 40
RUN UP !1 -0.0 61.50
RUN UP-LEAN 4 -0.0 39.60
RUN UP-RICH -0.0 54.80
TAKE-OFF h -0.0 124.80
CLIMB 7 -0.0 109.00
DESCENT I) -0.0 98.40
APPROACH o -0.0 61.50
TAXI
TEST
MODE
1
2
3
4
5
6
7
8
9
10
TEST
MODE
1
2
3
4
5
6
7
a
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
673.00
762.00
1300.00
1211.00
1323.00
1369.00
1356.00
1334.00
1211.00
785.00
MASS EMI
CO
LB/1K
LB FUEL
960.29
856.63
1178.74
1172.70
1146.59
1204.08
1185.93
1184.86
1176.11
1034.10
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
in
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
IB/IK
LB FUEL
196.22
45.49
27.43
19.92
42.67
15.43
14.73
15.47
18.68
135.91
MEASURED
FUEL FLOW
LB/HR
26.40
124.80
109.00
61.50
24.60
FUEL
-0.
CO
(DRY)
PERCENT V
8.30
6.40
10.10
10.10
9.90
11.90
11.00
10. TO
10.00
8.70
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
5.28
0.62
9.05
6.15
1.65
22.749
.0
CO
2
(DRY)
PERCENT
6.20
8.10
6.80
7.00
6.90
7.80
7.50
7.30
6.90
6.30
MASS EMI
C02
LB/1K
LB FUEL
1127.08
1703.48
1246.93
1277.03
1255.63
1240.05
1270.48
1270.11
1275.07
1176.59
CO
LB/1K
LB FUEL
856.63
1204.08
1185.93
1176.11
1034.10
24.60
THC
(DRY)
PPMV
V
29613.00
5934.00
4104.00
2995.00
6433.00
2662.00
2385.00
2440.00
2773.00
19964.00
MASS EMI
NO
LB/1K
LB FUEL
0.27
1.03
1.34
1.58
1.05
0.78
0.96
0.98
1.00
0.72
LTD CYCLE
CO
L6/1K
HOURS
22615.09
150268.63
129266.56
72330.63
25438.93
MEASURED CALCULATED
AIR FLOM F/A
LB/HR
22T.OO 0.08154
315.00 O.C6984
659.00 0.08068
644.00 0.08102
643.00 0.08125
1334.00 0.09270
1173.00 0.08709
1061.00 O.OB486
662.00 0.08002
239.
NO
IDRY)
PPMV
14.00
47.00
70.00
83.00
55.00
47.00
54.00
54.00
52.00
37.00
MASS EMI
NOX
LB/IK
LB FUEL
0.27
1.03
1.34
1.58
1.05
0.78
0.96
0.98
1.00
0.72
EMISSIONS
CO
EMISSION
LBS.
4.523
0.751
10.729
7.233
1.704
24.941
1.096
00 0.
NO
2
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
23623.17
22615.09
72492.19
70127.31
66566.06
150268.63
129266.56
116589.75
72330.63
25438.93
HC
LB/IK
LB FUEL
4b.49
15.43
14.73
10.66
135.91
07935
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
HC
LB/HR
4827.12
1200.91
1687.03
1190.99
2551.72
1925.20
1605.19
1522.69
1148.73
3343.28
HC
LB/1K
HOURS
1200.91
1925.20
1605.19
1148.73
3343.26
ALDEHYDES SMOKE
(DRYI
25.00
14.00
-0.00
-0.00
-0.00
-0.00
9.00
9.00
9.00
17.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.240
0.010
0.133
0.115
0.224
0.722
0.032
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
27726.18
44971.97
76666.13
76366.38
75086.18
154758.31
138461.88
124979.13
78416.81
2B944.00
NO
LB/IK
LB FUEL
1.03
0.78
0.96
1.00
0.72
PtRMCULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI SASS EMI
NO NOX
LB/HR LB/HR
6.54 6.54
27.28 27.28
82.53 82.53
94.66 94.66
62.57 62.57
9T.49 97.49
104.23 104.23
96.65 96.65
61.78 61.76
17.77 17.77
NO NO
LB/IK EMISSION
HOURS IBS.
27.28 0.0055
97.49 0.0005
104.23 0.0087
61.78 0.0062
17.77 0.0012
0.0220
0.0010
1-99
-------
DATE: as 6/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER: LYCOMING
ENGINE DATA
CAL 10 NUMBER: 266 ENGINE TYPE AND MODELt io-S40-c4B5
RATED HORSEPOMER: 2!0.
ENGINE TOTAL TINE: 1305. HRS
FUEL: AV GAS 100/130 FUEL H/C RATIO: 1.840
OPERATIONAL DATA »«»»«»«««»«»»««««.««.
INLET AIR TEMPERATURE, DEGREES Ft START 8*.00 FINISH 84.00
ATMOSPHERIC PRESSURE: START 24.89 FINISH 29.as
INLET AIR HUMIDITY, GRN H2Q/LB AIR: 0.01
RELATIVE HUMIDITY: M.co PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLO* RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 9
COMMENTS:
SERIAL NUMBER: L-16JJ-48B
2011
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOU 1 -0.0 3.50
IDLE/TAXI 2 -0.0 15.80
RUN UP 3 -0.0 31.60
RUN UP-LEAN «! -0.0 29.90
RUN UP-RICH 5 -0.0 29.90
TAKE-OFF 6 -0.0 109.00
CLIMB T -0.0 49.20
APPROACH 9 -0.0 26.40
TAXI 10 -0.0 12.30
TEST EXHAUST EXHAUST Cn CO THC
MODE GAS GAS IORVI 2 (DRY)
TEMP PRESSURE PERCENT V ( DRY 1 PPHV
1
2
3
4
5
6
7
1
10
TEST
MODE
1
2
1
it
5
6
7
9
11
TfST
MODE
2
6
7
9
10
TOTAL
TOTSL
DEGREES F
650.no
762.00
1166.00
1289.00
1278.00
1289.00
1244.00
1121.00
eia.oo
MAIS EMI
CO
LB/IK
LB FUEL
919.61
1000.02
1380.59
12B3.B6
1359. 19
1410.52
13118.64
1372.31
1331.98
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FDR CYCLE/LB
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
345.37
200.31
35.35
84.23
35.35
24.92
26.86
32.52
44.25
MEASURED
FUEL FLOW
LB/HR
15.80
109.00
49.20
26.40
12.30
FUEL
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
26.00 0.08784
142.00 0.08315
306.00 0.08863
2T6.00 0.09003
292.00 0.08854
1047.00 0.09541
477.00 0.09078
256.00 O.C8978
121.00 0.07T70
NU NO NO
IDRYI 2 X
OPMV (ORY1 (DRY!
PERCENT V
B. 50
8. BO
12.90
12.20
12.70
14.20
13.30
13.00
10.90
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
3.16
0.14
4.06
2.64
0.82
11.251
4.60
5.90
5.40
5.60
5.60
5.70
5.60
5.60
5.00
MASS EMI
C02
LB/IK
LB FUEL
781.95
1053.46
908.05
925.94
941.611
889.62
916.68
928.82
960.02
CO
LB/IK
LB FUEL
1000.02
1410.52
1388.64
1372.31
1331.98
55732.00
30777.00
5767.00
13975.00
5767.00
4381.00
4492.00
5379.00
6322.00
MASS EMI
NO
LB/IK
L8 FUEL
0.23
0.52
0.16
0.21
0.12
0.26
0.21
0.19
0.22
LTD CYCLE
CO
LB/IK
HOURS
15800.33
153746.94
68321.19
36228.86
16383.33
13.00
28.00
9.00
12.00
7.00
16.00
12.00
11.00
11.00
MASS EMI
NQX
LB/IK
LB FUEL
0.23
0.52
0.16
0.21
0.12
0.26
0.21
0. 19
0.22
EMISSIONS
cn
EMISSION
LBS.
3.160
0.769
5.671
3.623
1.098
14.320
1.273
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
MASS EMI
co
LB/HR
3218.63
15800.33
43626.71
38387.34
40639.71
153746.94
68321.19
36228.86
16383.33
HC
LS/1K
LB FUEL
200.31
24.92
26.86
32.52
44.25
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
1208.65
3164.86
1117.01
2518.40
1056.9?
2716.67
1321.57
R58.53
544.22
HC
LB/IK
HOURS
3164.86
2716.67
1321.57
858.53
544.22
ALDEHYDES SMOKE
(DRY)
58.00
60.00
-0.00
-0.00
-0.00
-0.00
27.00
14.00
41.00
MASS EMI
N02
Lfl/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
L8S.
0.633
0.014
0.110
O.OK6
0.036
0.879
0.078
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oa
-o.on
-0.00
-0.00
MASS tMI
C02
LB/HR
2736. S3
16644.61
28694.24
27685.65
26156.14
96968.56
45199.16
24520.96
11806.22
NU
LD/IK
LB FUEL
0.52
0.26
0.21
0.19
0.22
PARTICULATES
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
MASS EMI
NO
LB/fR
0.81
6.26
5.00
6.20
3.68
28.45
10. 13
5.04
2.72
NO
LB/IK
HOURS
6.26
2X.45
10.13
5.04
2.72
00
00
00
00
00
00
00
00
CO
MASS EMI
NOX
LB/HR
0.81
8.26
5.00
6.20
3.68
28.45
10.13
5.04
2.72
NO
EMISSION
LBS.
0.0017
0.0001
c.cooa
0.0005
0.0002
0.0033
0.000)
1-100
-------
0»Tf: 8/ 6/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCONING
ENGINE DATA
C»L 10 NUMBER! 267 ENGINE TYPE AND MODEL! IO-540-C4B5
RATED HORSEPOHERI 290.
ENGINE TOTAL TIMEl 1218. MRS
FUEL" AV GAS 100/1)0 FUEL H/C RATIOI 1.1*0
OPERATIONAL DATA *»*»»»»*»«**««
INLET AIR TEMPERATURE) DECREES Fl START 62.00 FINISH 82.00
ATMOSPHERIC PRESSURE! START 21.«0 FINISH 29.90
INLET AIR HUMIDITY, CRN H20/LB AIRl 0.01
RELATIVE HUMIDITY! 32.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES Cl -0.00, FLO* RATE, LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TINE, SECl 1.60
NUMBER OF TESTSi 10
COMMENTS:
SERIAL NUMBER! L-1623-48C
0013
CARB. TEST ENGINE MEASURED
HEATER NODE RPN FUEL FLO*
LB/HR
IDLE-LOW 1 -0.0 8.80
IDLE/TAXI 2 -0.0 8.80
RUN UP J -0.0 29.90
RUN UP-LEAN 4 -0.0 22.90
RUN UP-RICH 5 -0.0 28.10
TAKE-OFF 6 -0.0 72.10
CLIMB 7 -0.0 52.70
DESCENT 8 -0.0 40. 40
APPROACH 9 -0.0 26.40
TAXI 10 -0.0 10. SO
TEST EXHAUST EXHAUST CO CO THC
MODE GAS GAS (DRY) 2 IORYI
TEMP PRESSURE PERCENT V 1 CRT I PPMV
(
2
3
4
5
6
7
a
9
10
TEST
MODE
1
2
3
4
5
6
7
8
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
DEGREES F
594.00
717.00
1166.00
1199.00
1256.00
1278.00
1244.00
1211.00
1099.00
773.00
MASS EMI
CO
LB/IK
LB FUEL
882.66
973.05
1378.34
1150.60
1356.35
1388.83
1399.10
1386.47
1384.08
1079.42
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
PSIA
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
386.72
249.09
40.17
186.55
39.62
26.14
27.15
27.70
94.05
267.28
MEASURED
FUEL FLOW
LB/HR
B.80
72.10
52.70
26.40
10.50
FUEL
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
61.00 0.09052
74.00 0.08654
289.00 0.09284
193.00 0.09070
275.00 0.09079
700.00 0.10011
509.00 0.09415
393.00 0.09225
255.00 0.09043
81.00 0.09424
NO NO NO
(DRYI 2 X
PPMV IORYI IORYI
PERCENT V
8.40
8.90
13.50
11.00
13.00
14.70
13.90
13.50
13.20
10.70
MASS EMI
N02
LR/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
1.76
0.36
4.37
2.64
0.70
9.838
4.40
5.60
5.60
5.20
5.70
6.20
5.70
5.70
5.50
4.70
MASS EMI
CO 2
LB/IK
LB FUEL
726.45
962.00
898.36
854.62
934.42
920.37
901.46
919.79
906.13
744.98
CO
LO/IK
LB FUEL
973.05
1388.83
1399.10
1384.08
1079.42
64260.00
39780.00
6870.00
31140.00
6630.00
4830.00
4710.00
4710.00
5670.00
46260.00
MASS EMI
NO
L8/1K
LB FUEL
0.45
0.40
0.25
0.26
0.15
0.25
0.18
0.20
0.17
0.15
LTD CYCLE
CO
LB/IK
HOURS
8562.88
100134.94
73732.38
36539.71
11333.93
26.00
22.00
15.00
15.00
9.00
16.00
11.00
12.00
I0.no
9.00
MASS EMI
NOX
LB/IK
LB FUEL
0.45
0.40
0.25
0.26
0.15
0.25
0.18
0.20
0.17
0.15
EMISSIONS
CO
EMISSION
LBS.
1.713
0.501
6.120
3.654
0.759
12.746
1.296
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
7767.38
8562.88
41212.29
26348.62
38113.43
100134.94
73732. 3B
56013.27
36539.71
11333.93
HC
L6/IK
LB FUEL
249.09
26.14
27.15
34.05
267.28
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
3403.15
2192.00
1201.14
4271.98
1113.25
1884.35
1430.90
1119.24
898.92
2906.39
HC
LB/IK
HOURS
2192.00
1884.35
1430.90
898.92
2806.39
ALDEHYDES SMOKE
(ORY)
70.00
66.00
-0.00
-0.00
-0.00
-0.00
26.00
18.00
15.00
42.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.438
0.009
0.119
0.090
o. ias
0.845
0.0116
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
-o.no
-o.no
MASS FMI
C02
LB/HR
6392.73
8465.56
26860. 32
19570.71
26257.20
66358.75
47506.91
37159.53
23921.72
7822.27
NO
LB/IK
LB FUEL
0.40
0.25
0.1B
0.17
0.15
PARTICUL4TES
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
MASS EMI
NO
LB/HR
3.95
3.48
7.52
5.9C
4.33
17.90
9.58
8.18
4.55
1.57
NO
LB/IK
HCURS
3.4A
17.90
9.58
4.55
1.57
00
oo
00
00
00
00
oo
00
00
00
MASS EMI
NOX
LB/HR
3.95
3.4B
7.52
5.90
4.33
17.90
9.58
8.18
4.55
1.57
NO
EMISSION
LBS.
0.0007
0.0001
0.0008
0.0005
0.0001
0.0021
0.0002
1-101
-------
DATE! B/IT/T1
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOMING
ENGINE DATA
CAL ID NUMBER: 972 ENGINE TYPE AND NODELI 0-5*0-AIBS
RATED HORSEPOWER: 290.
ENGINE TOTAL TIME: 1111. MRS
FUEL: AV GAS 100/110 FUEL H/C RATIOl 1.640
OPERATIONAL DATA »«««»»«««««««««»
INLET AIR TENPERATURE, DEGREES F: START T8.00 FINISH 78.00
ATMOSPHERIC PRESSURE: START 10.29 FINISH 10.29
INLET AIR HUMIDITY, GUN M20/LB AIR: 0.01
RELATIVE HUNIDITYI 41.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOM RATE, LITERS/NIN: 7.00
SAMPLE LINE TRANSPORT TINE. SEC: 1.60
NUMBER OF TESTSi 11
COMMENTS:
SERIAL NUMBER! L-JM1-40
CARS. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IOLE-LOM 1 -0.0 22.90
IDLE/TAXI 2 -0.0 26.40
RUN '1? 1 -0.0 59.60
RUN UP-LEAN 4 -0.0 56.30
RUN UP-RICH 5 -0.0 41.90
TAKE-OFF 6 -0.0 109.00
CLIMB 7 -0.0 91.40
DESCENT 6 -0.0 75.60
DESCENT ON 8 -0.0 87.90
APPROACH 9 -0.0 56.10
TAXI
TEST
NODE
1
2
3
4
5
6
I
a
n
4
10
TEST
MORE
I
2
a
a
9
10
TEST
MODE
2
6
7
9
in
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
619.00
650.00
852.00
729.00
B18.00
1480.00
1480.00
1446.00
1300.00
1222.00
796.00
MASS EMI
CO
Lfl/lK
LH FUEL
B57.19
917.85
952.11
953.96
960.50
964.09
885.33
710.85
1247.25
926.66
921.20
TIME IN
HOOF.
M!N.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
HC
LB/1K
16 FUEL
121.21
53.86
19.12
17.11
16.09
19.47
16.18
14.81
22.88
19.78
61.26
MEASURED
FUEL FLOW
LB/HR
26.40
109.00
91.40
56.10
26.40
FUFL
-0
CO
(DRY)
PERCENT V
6.40
7.10
a. 10
8.10
fl.10
8.10
r.AO
5.90
11.40
7.70
7.80
MASS EMI
N02
IB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
5.28
0.54
7.59
5.63
1.77
20.K10
0
CO
2
IORY)
PERCENT V
7.10
7.80
8.80
8.80
8.70
8.80
9.50
10.20
6.70
8.80
8.40
MASS EMI
C02
LB/1K
LB FUEL
1494.49
1584.34
1625.26
1628.42
1620.95
1606.05
1738.81
1985.24
1151.76
1663.99
1556.76
CO
LB/IK
LB FUEL
917.85
964.09
BB5.33
926.66
921.20
26.40
THC
IDRY)
PPNV
15801.00
7274.00
2870.00
2516.00
2369.00
2926.00
2425.00
2090.00
3651.00
2870.00
9057.00
MASS EMI
NO
LB/1K
LB FUEL
0.20
0.45
4.09
2.48
2.47
6.14
6.70
ia.79
2.79
5.24
0.62
LTO CYCLE
CO
LB/1K
HOURS
24231.32
105085.25
80918.81
52170.82
24319.76
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
244.00 0. C7009
307.00 0.07242
702.00 0.07931
661.00 0.07918
515.00 0.07867
1275.00 0.08028
1100.00 0.07978
956.00 0.07475
917.00 0.08614
665.00 0.07747
306.
NO
IORY)
PPMV
9.00
21.00
212.00
128.00
127.00
122.00
350.00
899.00
155.00
265.00
32.00
MASS EMI
NOX
LB/1K
LB FUEL
0.20
0.45
4.09
2.48
2.47
6.14
6.70
1B.?9
2.79
5.24
0.62
EMISSIONS
CO
EMISSION
LBS.
4.846
0.525
6.716
5.217
1.629
18.934
C.910
00 0.
NO
2
IORY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI
CO
LR/HR
1963'i. 18
24231.32
56936.13
537Ce.ll
42165.81
105085.25
80918.81
5S252.0I
109633.56
5217C.82
24111.76
HC
LB/1K
LB FUEL
53.86
19.47
16.18
19.78
61.26
07909
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
MASS EMI
HC
LB/HR
2776.28
1421.80
1155.19
961.05
706.29
2121.70
1478.74
1120.95
2010.93
1113.60
1617.31
HC
LB/1K
HOURS
1421.80
2121.70
1478.74
1111.69
1617.31
ALDEHYDES SMOKE
IDRYI
21.00
18.00
-0.00
-0.00
-0.00
-0.00
7.00
9.00
12.00
3.00
9.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
o.o
0.0
HC
EMISSION
LBS.
0.284
0.011
0.123
0.111
0.10B
0.637
0.031
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/HR
34223.89
41826.50
97190.44
91680.19
71159.50
175059.00
158927. 11
150084.00
101239.94
916ft;. 18
41151.20
NO
LB/1K
LB FUEL
0.45
6.14
6.70
5.24
0.62
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
Nil NOX
LB/HR LB/HR
4.54 4.54
11.77 11.77
244.77 244.77
139.41 139.41
ioa.59 ina.59
669.64 669.64
612.10 612.10
1382.85 1182.85
244.84 244.84
294.9? 294.92
16.39 16.39
NO NO
LB/IK EMISSION
HCUHS LBS.
11.77 O.OC24
669.64 0.0033
612.10 0.0508
294.92 0.0295
16.39 0.0011
0.0871
0.0042
1-102
-------
0»IE: 8/IT/T1
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENCINE SUPPLIER! LYCOMING
ENGINE OAT*
CAL 10 NUMBER! 373 ENGINE TYPE AND MODEL! 0-540-AIB5
RATED HORSEPOWER! 290.
ENGINE TOTAL TINE! 1133. MRS
FUEL! AV GAS 100/130 FUEL H/C RATIOI 1.8*0
OPERATIONAL DATA »«
INLET AIR TEMPERATURE, DEGREES Fl START 86.10 FINISH
ATMOSPHERIC PRESSURE! START 30.29 FINISH
INLET AIR HUMIDITY, CAN H20/19 AIR! 0.01
RELATIVE HUMIDITY! 36.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES Cl -O.OC, FLOW RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: II
COMMENTS:
SERIAL NUMBER! L-31M-40A
81.00
30.2*
CtRB. TtST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 19.30
IDLE/TAXI 2 -0.0 26.40
RUN UP 3 -0.0 39.80
RUN UP-LEAN 4 -0.0 99.80
RUN UP-RICH 5 -0.0 40.40
TAKE-OFF 6 -0.0 110. 80
CLIMB . 7 -0.0 84.40
DESCENT B -0.0 65.00
DESCENT ON 8 -0.0 77.40
APPROACH 9 -0.0 58.00
TAXI
TEST
MODE
1
2
]
4
5
6
7
B
a
9
10
TEST
MODE
1
2
3
4
5
&
7
8
a
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
-0.00
706.00
986.00
975.00
886.00
1457.00
1480.00
1390.00
1256.00
1110.00
796.00
MASS EMI
CO
LB/IK
LB FUEL
610.79
H63.4I
946.38
938.55
938.62
963.82
666.60
762.10
1250.36
1422. SI
936.08
IIME IN
MODE
Ml N.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/IB
10
EXHAUST
CAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
MASS EMI
HC
LB/IK
LB FUEL
99.26
53.38
24.99
21.50
20.65
26.42
19.04
19.35
26.34
39.05
57.66
MEASURED
FUEL FLOW
LR/HR
26.40
110.80
84.40
58.00
26.40
FUEL
-0.
CO
(DRY)
PERCENT V
4.20
6.90
7.90
8.00
7.90
8.30
5.20
6.10
11.40
13.70
7.90
MASS EMI
N02
LB/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUF.L
USED
L8S.
5.28
0.55
7.01
5.80
1.77
20.408
.0
CO
2
I DRY!
PERCENT V
8.50
8.50
B. 60
8.90
8.80
B.TO
10.30
9.80
6.60
5.10
B.30
MASS EMI
C02
LB/IK
LB FUEL
1942.23
1671.18
1618.72
1640.58
1642.80
1587.37
2074.63
1923.74
1137.39
832.04
1545.26
CO
LB/1K
LB FUEL
863.41
963.82
666.60
1422.51
936.08
26.40
THC
(ORYI
PPNV
11918.00
7449.00
3642.00
3200.00
3035.00
3973.00
2593.00
2704.00
4193.00
6566.00
8497.00
MASS EMI
NO
LB/IK
LB FUEL
0.31
0.51
5.10
2.87
2.71
5.40
42.66
17.46
2.83
0.58
0.68
LTD CYCLE
CO
LB/IK
HOURS
22793.93
106791.75
56261.37
82505.69
24712.46
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
230.00 0.06411
313.00 0.07458
402.00 0.07790
703.00 0.07944
477.00 0.07848
1291.00 0.08034
1082.00 0.07218
812.00 0.07425
804.00 0.08597
548.00 o: 09 150
305.00 0.
NO
(DRY)
PPMV
13.00
25.00
259.00
149.00
139.00
283.00
2026.00
851.00
157.00
34.00
35.00
MASS EMI
NDX
LB/IK
LB FUEL
0.31
0.51
5.10
2.87
2.71
5.40
42.66
17.46
2.83
0.58
0.68
EMISSIONS
CO
EMISSION
LBS.
4.559
0.534
4.670
8.251
1.656
19.669
0.964
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
11788.26
22793.93
56593.20
56125.43
37920.30
106791.75
56261.37
49S36.39
96777.44
82505.69
24712.46
HC
LB/IK
LB FUEL
53.38
26.42
19.04
39.05
57.66
07886
NO
X
IDRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
MC
LB/HR
1915.79
1409.33
1494.25
1285.77
834.35
2927.68
1606.77
1257.61
2038.63
2264.69
1522.30
HC
LB/IK
HOURS
1409.33
2927.68
1606.77
2264.69
1522.30
ALDEHYDES SMOKE
IORY)
18.00
10.00
-0.00
-0.00
-0.00
-0.00
4.00
5.00
11.00
5.00
B.OO
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.3
0.0
0.3
0.0
HC
EMISSION
LBS.
0.282
0.015
0.133
0.226
0.102
0.758
0.037
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
37484. 98
44119.20
96799.63
98106.50
66369.06
175880.25
175098.50
125042.75
88034.25
48258.27
40794.83
NO
LB/IK
LB FUEL
0.51
5.40
42.66
0.56
0.68
PARTICULATES
-O.CO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NQX
LB/HR LB/HR
5.99 5.99
13.57 13.57
304.76 304.76
171.70 171.70
109.59 109.59
598.09 598.09
3600.53 3600.53
1135.13 1135.13
218.92 218.92
33.63 33.63
17.98 17.98
N(l NO
LB/IK EMISSION
HOURS LBS.
13.57 0.0027
59B.09 0.0030
3600.53 0.29BB
33.6} 0.0034
17.98 0.0012
0.3091
0.0151
1-103
-------
OATEl 8/17/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOMING
ENGINE 0»T»
C»L 10 NUMBER! }T» ENGINE TYPE AND MODEL! 0-540-A1B5
IUTED HORSEPOKER: 290.
ENGINE TOTAL TIME: 11)3. Hits
FUEL: AV GAS ICO/DO FUEL H/C RATIO: i.e«o
OPERATIONAL DATA «»«««««»«»««««»«««»»««««»«
INLET AIR TEMPERATURE, DEGREES F: START 87.00 FINISH 85.00
ATMOSPHERIC PRESSURE: START 30.29 FINISH 30.2<)
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 38.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOH RATE, LITERS/KIN! 7.00
SAMPLE LINE TRANSPORT TIME, SF.C: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER! L-31«1-«OB
CARS. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOM
LB/HR
IDLE-LOU I -0.0 22.90
IDLE/TAXI 2 -0.0 2*. 60
RUN UP 3 -0.0 58.00
RUN UP-LEAN 4 -0.0 61. SO
RUN UP-RICH 5 -0.0 40.4C
TAKE-OFF 6 -0.0 11*. 30
CLIMB 7 -0.0 87.90
DESCENT 8 -0.0 75.90
DESCENT ON 8 -0.0 77.40
APPROACH 9 -0.0 58.00
TAXI
TEST
MODE
1
2
3
4
5
6
7
a
a
9
10
TEST
MODE
I
2
1
4
5
6
7
a
a
**
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
5.16
560.00
1076.00
1121.00
1121.00
1300.00
1188.00
12*4.00
1031.00
1031.00
-0.00
MASS EMI
CO
LB/1K
LR FUEL
525.81
801.57
936.79
928. 28
939.96
952.21
831.27
729.05
1262.94
998.09
943.15
TIME IN
MODE
HIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
52.85
46.37
20.45
16.79
16.61
18.62
17.31
16.25
23.19
20.83
62.85
MEASURED
FUEL FLOW
LB/HR
24.60
114.30
87.90
58.00
26.40
FUEL
-0,
CO
(DRY)
PERCENT V
3.60
6.20
7.60
7.60
7.60
a. no
6.60
5.60
11.10
a. 10
7.80
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LRS.
4.9Z
0.57
7.30
5.80
1.77
20.356
.0
CO
2
(DRY!
PERCENT V
9.60
8.80
8.50
a. 70
8.50
8.70
9.20
9.70
6.30
8.00
8.00
MASS EMI
C02
LB/IK
LB FUEL
2203.09
1787.60
1646.22
1669.64
1651.78
1627.04
1820.64
1984.17
1126.26
1548.86
1519.90
CO
LB/IK
LB FUEL
801.57
952.21
831.27
998.09
943.15
26.40
THC
(DRY)
PPMV
6318.00
6262.00
2897.00
2401.00
2345.00
2731.00
2400.00
2179.00
3559.00
2952.00
9076.00
MASS EM]
NO
LB/IK
LB FUEL
0.74
0.81
6.09
4.27
3.94
7.19
13.84
22.82
4.45
S.69
1.25
LTD CYCLF
CO
LB/IK
HOURS
19718.55
108837.00
73068.44
57889.28
24899.25
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
229.00 0.06351
299.00 0.07207
684.00 0.07574
730.00 0.07636
478.00 0.07548
1343.00 0.07837
1075.00 0.07386
954.00 0.07127
799.00 0.08297
670.00 0.07594
303.00 0.
NO
(DRY)
PPMV
31.00
38.00
301.00
213.00
194.00
368.00
669.00
1067.00
238.00
281.00
63.00
MASS EMI
NOX
LB/IK
LB FUEL
0.74
o.ai
6.09
4.27
3.94
7.19
13.84
22. B2
4.45
5.69
1.25
EMISSIONS
CO
EMISSION
LBS.
3.944
0.544
6.065
5.789
1.668
18.010
0.885
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-c.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS F«l
CO
LB/HR
12040.95
19718.55
54334.09
57089.34
37974.39
108837. CO
73068.44
55334.80
97751.31
57889.28
24899.25
HC
LB/IK
LB FUEL
46.37
18.62
17.31
20.8]
62.85
07738
N'J
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
1210.27
1140.62
1186.18
1032.52
671.07
2127.91
1521.75
1233.14
1795.04
1208.30
1659.32
HC
LB/IK
HOURS
1140.62
2127.91
1521.75
1208.30
1659.32
ALDEHYDES SMOKE
IDRVI
14.00
10.00
-0.00
-0.00
-0.00
-0.00
7.00
6.00
13.00
6.00
9.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.228
0.011
0.126
0.121
0.111
0.597
0.029
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
CO?
LB/HR
50450.79
43974.84
95480.75
102683.00
66732.00
185970.56
160034.00
150598.44
87172.31
89834.13
40125.44
NO
Ld/lK
LB FUEL
0.81
7.19
13.84
5.69
1.25
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NQX
LB/HR LB/HR
17.03 17.03
19. AS 19.85
353.46 353.46
262.81 262.81
I39.22 159.22
C22.35 822.35
1216.56 1216.56
1731.79 1731.79
344.27 344.27
329.87 329.87
33.03 33.03
ND NO
LB/IK EMISSION
HOURS LBS.
19.85 0.0040
822.35 0.0041
1216.56 0.1010
329.87 0.0330
33.03 0.0022
0.1443
0.0071
1-104
-------
0»TE: 6/17/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOMING
ENGINE DMA
CAL 10 NUMBER! 375 ENGINE TYPE AND NODELI 0-J40-A1B5
RATED HORSEPOMERl 250.
ENGINE TOTAL TINE! 932. MRS
FUEL: AV GAS loo/uo FUEL H/C RATIO: i.ato
OPERATIONAL DATA *«»***»**,
INLET AIR TEMPERATURE. DEGREES F: START 70.00 FINISH 74.00
ATMOSPHERIC PRESSURE! START 30.26 FINISH 30.28
INLET AIR HUMIDITY, GR* H20/LB AIR! 0.01
RELATIVE HUMIDITY: 57.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00. FLOH RATE. LITERS/MIN: 7.00
SAMPLE L1NF TRANSPORT TINE, SEC: 1.60
NUMBER OF TESTS: II
COMMENTS:
SERIAL NUMBER! L-3454-40
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IOLE-LOH I -0.0 21.10
IDLE/TAXI 2 -0.0 24.60
RUN UP 3 -0.0 52.70
RUN UP-LEAN 4 -0.0 47.50
RUN UP-RICH 5 -0.0 52.70
TAKE-OFF 6 -0.0 110.80
CLIMB 7 -0.0 110.80
DESCENT 8 -0.0 77.40
DESCENT ON B -0.0 B4.40
APPROACH 9 -0.0 58.00
TAXI 10 -0.0 22.90
TEST
HODE
|
2
3
4
5
6
7
a
a
9
10
TEST
NODE
1
2
3
4
5
6
7
a
a
9
10
TEST
MODE
2
6
7
9
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES f
706.00
773.00
1278.00
1334.00
1312.00
1379.00
1424.00
1558.00
1278.00
1614.00
1323.00
MASS EMI
CO
LB/IK
LB FUEL
704.81
707.25
824.39
773.83
766.26
1018.61
973.80
508.52
1233.05
838.12
695.81
TIME [N
MODE
NIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CYCLE/LB
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
173.93
83.99
39.84
32.01
29.52
55.10
41.60
33.68
60.42
45.78
80.37
MEASURED
FUEL FLOU
LB/HR
24.60
110.80
110.80
58.00
22.90
FUF.L
CO
IDRYI
PERCENT V
6.20
4.70
7.10
6.50
6.50
10.80
8.90
4.20
12.30
7.31
5.70
MASS EMI
N02
LB/IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
4.92
0.55
9.20
5.80
1.53
22.005
CO
2
IDRYI
PERCENT V
8.90
9.40
9.70
10.00
10.20
9.60
8.90
12.00
6.80
9.60
9.70
MASS EMI
C02
LB/IK
LB FUEL
1589.67
1832:58
1769.64
1870.56
1889.30
1422.63
1530.06
2282.85
1071.08
1731.78
1860.48
CD
LB/U
LB FUEL
707.25
1018.61
973.80
838.12
695.81
THC
(DRY)
PPMV
26715.00
11819.00
S99I.OO
4695.00
4372.00
10200.00
6638.00
4857.00
10524.00
6962.00
11496.00
MASS EMI
NO
LB/IK
LB FUEL
0.28
0.77
3.99
2.97
2.11
4.28
3.07
26.97
1.93
4.66
0.92
LTD CYCLE
CO
LB/IK
HOURS
17398.28
112861.63
107897.25
48610.91
15933.98
MEASURED CALCULATED
AIR FLO* F/A
LB/HR
224.00 0.08193
289.00 0.07488
641.00 O.C7996
587.00 0.07786
654.00 0.07956
1207.00 0.09862
1279.00 O.OB521
1032.00 0.07583
828.00 0.09400
70.00 0.08091
271.00 0.07601
NO
(DRY)
PPNV
15.00
38.00
209.00
152.00
109.00
276.00
171.00
1356.00
117.00
247.00
46.00
MASS EHI
NOX
LB/IK
LB FUEL
0.28
0.77
3.99
2.97
2.11
4.28
3.07
26.97
1.93
4.66
0.92
EMISSIONS
CO
EMISSION
LBS.
3.460
0.564
8.955
4.861
1.068
18.928
0.860
hO
2
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
14U7I.39
17198.28
43445.42
36756.97
40381.62
112861.63
107897.2!
39359.30
104069.25
48610.91
14933.98
HC
LB/IK
LB FUEL
83.99
55.10
41.60
45. 78
80.37
NO
X
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
3669.95
2066.13
2099.57
1520.57
1555.60
6104.75
4608.96
2606.82
5099.69
2655.16
1840.52
HC
LB/IK
HOURS
2066.13
6104.75
4608.96
2655.16
1840.52
ALDEHYDES SMOKE
(DRY)
14.00
10.00
-o.on
-0.00
-0.00
-0.00
4.00
7.00
7.00
6.00
9.00
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.413
0.031
0.383
0.266
0.123
1.215
0.055
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
33541.95
45081.43
93260.06
88851.44
99565.94
157627.44
169530.75
176692.31
90399.25
100443.13
42604.90
NO
LB/IK
LB FUEL
0.17
4.28
3.07
4.66
0.92
PARTICIPATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
4.91 5.91
19.05 19.05
210.06 210.06
1M.19 141.19
111.23 111.23
473.75 473.75
340.52 340.52
2087.27 2087.27
162.60 162.60
270.16 270.16
21.12 21.12
NO NO
LS/iK MISSION
HOUKS LBS.
19.05 0.0038
473.75 0.0024
340.52 0.0283
270.16 0.0270
21.12 0.0014
0.0629
0.0029
1-105
-------
0«TEl 6/17/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCOMING
ENGINE OAT*
CAL ID NUMBER! 376 ENGINE TYPE AND MODEL: 0-5*0-A1B5
RATED HORSEPOWER: 250.
ENGINE TOTAL TIME: 932. MRS
FUEII AV GAS 100/130 FUEL H/C RATIOI 1.840
OPERATIONAL DATA «««»«.«««»..««.»»««.«««»««..«.«..........,....».«..«
INLET AIR TEMPERATURE. DEGREES F: START 75.50 FINISH 78.50
ATMOSPHERIC PRESSURE: START 30.28 FINISH 30.20
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 50.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MM: 7.00
SAMPLE LINE TRANSPORT TIME. SEC: 1.60
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER: L-3»»*-40»
CARB. TEST ENGINE MEASURED
HEATER MODE KPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 22.90
IDLE/TAXI 2 -0.0 22.90
RUN UP 3 -0.0 52.70
RUN UP-LEAN 4 -0.0 47.50
RUN UP-RICH 5 -0.0 52.70
TAKE-OFF 6 -0.0 109.00
CLIMB 7 -0.0 80.90
DESCENT 8 -0.0 70.30
DESCENT ON 8 -0.0 72.10
APPROACH 9 -0.0 52.70
TAKI 10 -0.0 24.60
TEST
HOOE
,
2
3
4
5
6
7
a
a
9
10
TEST
MODE
,
2
3
4
5
6
7
a
a
9
10
TESt
MODE
2
6
7
9
10
TOTAL
TOT/VL
EXHAUST
CAS
TEMP
DEGREES F
493.00
684.00
1233.00
1267.00
1099.00
1273.00
1076.00
1211.00
1143.00
1166.00
919.00
MASS EMI
CO
LO/IK
LB FUEL
357.09
614. 72
D63.il
841.55
491.08
1005.26
583.49
549.61
1279.47
933.59
687.04
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FOR CVCLE/L8
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
L3/IK
LB FUEL
144.21
31.97
16.80
12.34
337.38
11.75
8.31
9.86
21.83
14.14
29.55
MEASURED
FUEL FLOW
LB/HR
22.90
109.00
80.90
52.70
24.60
FUEL
en
(DRY)
PERCENT V
2.10
4.60
7.50
7.20
3.50
9.30
4.80
4.50
12.20
8.00
5.20
MASS EMl
N02
IB/IK
LB FUEL
U.O
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
FUEL
USED
LBS.
4.5B
0.54
6.71
5.27
1.65
18.758
CO
2
IORY)
PERCENT
8.30
10.10
9.80
9.90
6.70
9.20
11.70
11.90
6.70
9.10
9.70
MASS EMI
C02
LB/IK
LB FUEL
2217.55
2120.68
1772.02
1818.11
1477.07
1562.51
2234.67
2283.63
1104.03
1668.58
2013.68
CO
LB/IK
LB FUEL
614.72
1005.26
583.49
933.59
687.04
THC
(DRY)
PPMV
V
14808.00
4177.00
2549.00
1844.00
41984.00
1898.00
1193.00
1410.00
3634.00
2115.00
3905.00
MASS EMI
NO
LB/IK
LB FUEL
0.50
0.92
3.65
2. 78
2.01
3.69
21.48
23.75
2.02
4.26
1.28
LTO CYCLE
CO
LB/IK
HtlUMS
14C76.17
109573.69
47201.95
49200.30
16901.23
MEASURED CALCULATED
AIR FLOW F/A
LB/HR
279.00 0.05483
295.00 0.06929
640.00 0.08065
580.00 0.07936
487.00 0.0669ft
1262.00 0.08615
1067.00 0.07564
935.00 0.07521
741.00 0.08989
625.00 0.07979
312.00 0.07022
NO
IDRY)
PPMV
ie.no
42.00
193.00
145.00
87.00
208.00
1076.00
1184.00
117.00
222.00
59.00
MASS EMI
NOX
LB/IK
LB FUEL
0.50
0.92
3.65
2.7H
2.01
3.69
21.48
23.75
2.02
4.26
1.28
EMISSIONS
CO
EMISSION
LBS.
2.815
0.548
3.918
4.970
1.132
13.334
0.711
NO
2
IDRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.00
MASS EMI
CO
LD/HR
8177.31
14076.97
45485.75
39971.63
25880.09
109573.69
47203.95
38637.39
92249.44
49200.30
16901.23
HC
LB/IK
LB FUEL
31.97
11.75
8.31
14. 14
29.55
NO
I
IDHY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
Lfl/HR
3302.43
732.08
885.38
586.34
17779.80
1280.75
671.93
693.36
1573.74
744.96
726.91
HC
LB/IK
HOURS
737.08
1280.75
671.93
744.96
726.91
ALDEHYDES SMOKE
(DRY)
11.00
7.00
-0.00
-0.00
-0.00
-0.00
4.00
9.00
5.00
4.00
7.00
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
HC
EMISSION
LBS.
0.146
0.006
0.056
0.074
0.049
0.332
0.018
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
en?
LB/HR
50781.77
48563.63
93385.25
86360.38
77841.50
170313.69
1807194. 56
160539.06
79600.75
87934.06
49536.45
NO
LB/IK
L8 FUEL
0.92
3.69
21.48
4.26
1.28
PARTICULUES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
Nil NOX
LP/HR LB/HR
11.51 11.51
21.11 21.11
192.26 192.26
132.23 132.23
105.67 105.67
402.54 402.54
1738.08 I73B.08
I66S.81 1669.81
145.31 145.31
224.26 224.26
31.50 31.50
Ml MO
LH/IK EMISSION
HOURS LBS.
21.11 0.0042
4U2.54 0.0020
1738. 08 0.1443
224.26 0.0224
31.50 0.0021
0.1750
0.0093
1-106
-------
DATE! 8/17/71
TEST ORGANIIATIONI $COTT/GI:N AVIATION
ENGINE SUPPLIER! LYCOMING
ENGINE DATA
CAL 10 NUMBER! 371 ENGINE TYPE «NO MODEL! 0-540-A1BS
RATED HORSEPOBERI 290.
ENGINE TOTAL TIHE1 9J2. HRS
FUEL! AV GAS 100/110 FUEL H/C RATIQI 1.840
OPERATIONAL DATA »*«»*»««*«»«»«»»**»»*«»»
INLET AIR TEMPERATURE, DEGREES Ft START 87.00 FINISH 84.00
ATMOSPHERIC PRESSURE! START 30.29 FINISH JO.29
INLET AIR HUMIDITY, CRN H20/LB AIRl 0.01
RELATIVE HUMIDITY! 38.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MINI T.OO
SAMPLE LINE TRANSPORT TIME. SEC: 1.60
NUMBER OF TESTS! II
COMMENTS!
SERIAL NUMBER! L-3434-40B
CARB. TEST ENGINE MEASURED
HEATER MODE RPM FUEL FLOW
LB/HR
IDLE-LOW 1 -0.0 22.90
IDLE/TAXI -0.0 24.60
RUN UP -0.0 56.30
HUN UP-LEAN -0.0 49.20
RUN UP-RICH -0.0 52.70
TAKE-OFF -0.0 110. 80
CLIMB -0.0 109.00
DESCENT 8 -0.0 70.30
DESCENT 8 -0.0 79.10
APPROACH 9 -0.0 51.00
TAXI
TEST
MODE
1
2
3
4
5
6
7
H
a
q
10
TEST
MODE
1
2
8
a
q
10
TEST
MOOE
2
6
7
1
10
TOTAL
TOTAL
EXHAUST
GAS
TEMP
DEGREES F
639.00
751.00
1200.00
1233.00
953.00
1412.00
1323.00
1412.00
1233.00
1166.00
684.00
MASS EMI
CO
LB/1K
LB FUEL
651.50
601.19
883.55
872.28
614.87
763.40
1015.77
552.16
1288.00
920.3$
503.00
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
FOR CYCLE
FDR CTCLE/LB
10
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS Eni
HC
LB/IK
LB FUEL
45.5
-------
SUMMARY 0 200A
3001
MODEL SUMMARY
SAMPLE NUMBER 19.
TEST
MODE
2
6
T
9
10
TOTAL
TOTAL
MEAN:
STO OEVl
ME AN I
STO OEV:
MEANl
STD OEV:
MEANl
STD DEV:
MEAN:
STO OEV.
FOR CYCLE
FOR CYCLE/LB
MEASURED
FUEL FIOH
IB/Hit
7.68
1.3*
48.41
4.2*
48.41
4.24
21.29
1.21
6.49
LOT
MEAN:
STD OEV:
FUEL
FUEL
USED
IBS.
1.54
0.27
0.24
0.02
4.02
0.35
2.13
0.12
0.44
0.07
8.161
0.639
CO
LB/1K
LB FUEL
967.65
136.25
1109.63
232.11
1109.63
232.11
1117.45
61.01
998.81
114. TO
CO
IB/IK
HOURS
7519.03
2147.27.
54600.71
12360.03
54600.71
12360.03
23841.52
2275.58
6536.55
1589.63
MEAN:
STO DEV:
CO
EMISSION
LBS.
1.504
0.429
0.273
0.062
4.532
1.026
2.384
0.228
0.438
0.107
9.131
1.524
1.084
0.135
SUMMARY
MODEL
TEST
MODE
2
6
T
1
10
TOTAL
TOT4L
SUMMARY
MEAN:
STD OEV:
MEAN:
STO DEV:
MEAN:
STD OEV:
MEAN:
STD OEV:
MEAN:
STD DEV:
FOR CYCLE
FOR CYCLE/LB
SAMPLE
MEASURED
FUEL FLO«
LB/HR
12.99
5.16
65.68
10.73
63.54
10.95
21.13
a. 59
13.48
6.70
MEAN:
STD OEV:
FUEL
NUMBER -
FUEL
USF.O
LBS.
2.60
1.03
0.33
0.05
5.27
0.91
2.31
0.86
C.90
0.45
11.415
2.364
28.
CO
LB/1K
LB FUEL
835.02
234.46
1075.71
156.55
1022.85
247.90
1027.34
124.59
714.86
228.47
CO
LB/1K
HOURS
11056.69
6014.22
70926.00
16345.73
65751.06
21934.26
24266.00
10546.54
10045.07
6281.34
MEAN:
STD DEV:
CO
EMISSION
LBS.
2.211
1.203
0.355
0.082
5.458
1.821
2.427
1.055
0.673
0.421
11.123
2.916
C.970
0.131
SUMMARY
MODEL
TFSt
IDE
2
6
7
9
10
TOTAL
TOTAL
SUHHARY
MEAN:
STO nev:
MEAN:
STD DEV:
MEAN:
STD DEV:
MEAN:
STO DEV:
MEAN:
STD DEv:
FOR CYCLE
FOR CYCLE/LB
SAMPLE
MEASURED
FUEL FLOK
LB/HR
15.87
4.76
an. 70
18.42
67.88
13.79
33.51
8.46
15.96
4.81
MEAN:
STD OEV:
FUEL
NUMBER
FUEL
USED
LOS.
3.17
0.95
0.44
0.09
5.63
1.14
3.35
0.85
1.07
0.32
13.671
2.441
15.
CO
Lfl/lK
LB FUEL
848.18
272.92
1031.25
1)3.90
971.97
210.70
980.66
23U.44
931.26
341.25
CO
IB/IK
HOURS
13001.87
5783.23
92088. 13
24629.55
67412.13
23895.07
34420.59
16140.19
14212.80
6210.09
MEAN:
STD DEV:
CO
EMISSION
LBS.
2.600
1.157
0.460
0.123
5.595
1.983
3.442
1.614
0.952
0.416
13.050
4.319
0.947
0.214
KC HC
LB/IK LB/1K
LB FUEL HOURS
27.07 211.94
10.67 111.95
14.67 719.60
4.82 246.42
14.67 719.60
4.82 246.42
17.86 379.68
4.02 87.55
21.75 140.58
5.49 45.30
0-320
HC HC
LS/IK LB/1K
LB FUEL HOURS
26.04 355.08
12.38 247.99
22.27 1490.02
14.82 1094.05
20.49 1109.65
13.72 971.72
2C.93 495.80
4.10 236.96
22.62 120.01
13.05 281.00
10 - 360
HC HC
LB/IK LB/1K
IB FUEL HOURS
144.50 22S9.32
136.44 2774.19
22.47 2014.49
5.96 7B4.61
17.40 1196.83
3.53 395.98
22.80 772.36
6.03 313.61
1H2.26 2905.61
126.99 2763.99
HC
EMISSION
LBS.
0.0428
0. 0264
0.0016
0.0012
O.C59T
0.0209
0.0380
0.0088
0.0094
0.0030
0.153
0.048
0.018
0.005
HC
EMISSION
LBS.
0.0710
0.0496
0.0075
0.0055
0.1087
0.0807
O.C496
0.0237
0.0214
0.0190
0.258
0.111
0.022
0.009
HC
EMISSION
LBS.
0.4519
0.5548
0.0102
0.0019
0.099]
0.0129
0.0772
0.0314
0.1947
0.1852
0.833
0.764
0.059
0.043
NO
IB/IK
LB FUEL
1.17
0.38
6.00
8.56
6.00
8.56
2.43
1.34
1.46
0.47
NO
LB/1K
LB FUEL
1.01
0.72
1.21
4.44
5.91
12.77
2.26
1.52
1.59
1. 11
NO
LB/1K
LB FUEL
1.09
0.87
5.32
4.97
6.60
6.11
4.74
2.9}
0.96
0.71
NO
LO/1K
HOURS
8.86
J.03
258.91
265.29
258.91
265.29
51.76
29.77
9.50
3.46
NO
LB/IK
HOURS
12.53
10.87
213.51
271.24
175.43
839.61
51.42
50.03
21.92
24.82
NO
LB/IK
HCUHS
17.8?
16.75
474.50
486.96
407.76
J39.78
141.54
73.86
13.57
12.34
NO
EMISSION
LBS.
0.0018
0.0006
0.0013
0.0011
0.021!
0.0220
0.0052
0.0030
0.0006
0.0002
0.0304
0.0239
0.0038
0.0038
NO
EMISSION
LBS.
0.0025
0.0022
0.0011
0.0014
0.0112
0.0697
0.0051
0.0050
0.0015
0.0017
0.0413
0.0742
0.0095
0.0056
NO
EMISSION
LBS.
0.0036
0.0033
0.0024
0.0024
0.0338
0.0282
0.0142
0.0074
0.0009
0.0008
0.0548
0.0356
0.0042
0.0029
1-108
-------
SUMMARY 10 470
MODEL SUMMARY
SAMPLE NUMBER * 12.
TEST
MODE
2 MEAN!
STD OEVl
6 MEAN!
STO OEVl
T MEANI
STO OEVl
9 MEANI
STO OEV:
10 MEAN:
sro DEVI
TOTAL FOR CYCLE
TOTAL FOR CYCLE/LB
MEASURED
FUEL FLOW
LB/HR
21.53
7.84
104.69
14.07
60.24
8.29
53.97
9.1}
21.6B
8.47
MEAHI
STO OEV:
FUEL
FUEL
USED
LBS.
4.31
1.57
0.52
0.07
6.66
0.69
5.40
0.91
1.45
0.57
IB. 340
3.511
CO
LB/U
L8 FUEL
724.07
175.94
800.73
123.41
792.44
72.98
965.91
42.75
B21.79
137.06
CO
IB/ IK
HOURS
15383.41
6843. 84
83614.44
16579.38
63485.63
8136.49
52267.35
9956.32
17858.19
7698.01
MEAN:
STD OEV:
CO
EMISSION
LBS.
3.077
1.369
0.418
0.083
5.269
0.675
5.227
0.996
1.196
0.516
15.187
3.215
0.830
0.075
SUMMARY
HOnEL SUMMARY
TEST
MODE
2 MEAN:
SIO DEVI
6 MEAN:
STD OEVl
7 MEAN:
STD f>EV:
9 MEAN:
STD OEv:
10 MEAN:
Sro DEV:
TOUL FOR CYCLE
TOTAL FOR CYCLE/LB
SAMPLE
MEASURED
FUEL FLOW
LB/HR
is. a;
1.20
103.25
7. as
86.15
21.00
43.40
1.98
14.10
2.40
MEAN:
STO OEV:
FUEL
NUMBER -
FUEL
USED
LBS.
3.17
0.24
0.52
0.04
7.15
1.74
4.34
0.20
0.94
0. 16
16.121
1.579
2.
CO
LB/U
LB FUEL
984.36
156.96
1012.71
21.52
614.93
22.19
762.57
54.15
974.76
224.28
CO
LB/1K
HOURS
15696.43
3671.08
104646.94
10170.77
53209.41
14825.50
33909. 8S
801.44
14013.73
5505.84
MEAN:
STD DEVI
CO
EMISSION
LBS.
3.139
0.734
0.52)
0.051
4.416
1.231
3.301
O.ORO
0.939
0.369
12.409
0.099
0.773
0.070
HC
L8/1K
LB FUEL
101.89
76.02
30.88
11.09
18.10
7.76
19.52
3.80
188.31
93.89
0-470
HC
LB/1K
LB FUEL
54.03
52.54
13.75
1. 00
7.77
0.83
8.83
0.77
52.35
54.79
KC
LB/U
HOURS
2065.28
1786. »«
3295.03
1375.73
1463.02
683.24
1058.83
313.66
3918.95
2759.22
HC
LB/U
HOURS
867.93
897.76
1416.04
4.69
660.81
91.97
382.50
15.90
803.95
898.36
HC
EMISSION
LSS.
0.4131
0.3574
0.0165
0.0069
0.1214
0.0567
0.1059
0.0314
0. 2626
0.1849
0.919
0.560
0.049
0.025
HC
EMISSION
LBS.
0.1776
0.1796
0.0071
0.0000
0.0548
0.0076
0.0382
0.0016
0.0539
0.0602
0.332
0.234
0.021
0.017
NO
LB/U
LB FUEL
0.95
0.96
6.86
4.31
5.90
3.02
3.40
1.35
0.64
0.36
NO
LB/U
LB FUEL
0.58
0.62
2.07
1.95
3.25
1.36
3.92
1.91
0.38
0.39
NO
LB/U
HOURS
20.87
24.30
712.99
477.38
467.62
237.77
177.68
69.10
14.97
10.66
NO
LB/1K
HOURS
8.76
9.09
221.67
217.91
294.08
164.98
168.31
75. P5
4.90
4.64
NO
EMISSION
LBS.
0.0042
0.0049
0.0036
0.0024
0.0386
0.0197
0.0178
0.0069
0.0010
0.0007
0.0653
0.0283
0.0037
0.0016
NO
EMISSION
LBS.
0.0018
0.0018
0.0011
0.0011
0.0244
0.0154
0.0168
0.0075
C.0003
0.0003
0.0444
0.0110
0.0027
0.0004
SUMMARY TSIO - 520
MODEL SUMMARY
TESI
MODE
2 MEANI
STO DEVI
6 MEAN:
sro OEV:
7 MEANI
STD nEV:
9 MEAN:
STO DEV:
10 MEAN:
STO OEV:
TOTAL FOR CYCLE
TOTAL FOR CYCLE/LB
SAMPLE
MEASURED
FUEL FLOM
LB/HB
27. as
A. 90
121.60
10.61
104.90
12.42
58.32
1.33
29.28
10.3d
ME«NI
STD OEV.
FUEL
NUMBER
FUEL
USED
LBS.
5.57
1.38
0.61
0.05
8.71
1.03
5.83
0.13
1.96
0.69
22.676
1.230
6.
CO
LB/1K
LB FUEL
602.78
225.60
464.11
138.19
774.84
194. D4
1043.90
173.74
910.84
77.37
CO
LB/U
HOURS
17036.25
6879.25
57636.38
20831.44
83206.38
28889.20
60819.99
9832.53
26023.02
7269.30
MEAN:
STD OEV:
CO
EMISSION
LBS.
3.407
1.376
0.288
0.104
6.906
2.398
6.082
0.983
1.744
0.487
18.427
2.650
0.817
0.142
HC
LB/1K
LB FUEL
65.22
59.07
11.42
1.83
11.38
1.85
16.02
2.41
73.91
36.71
HC
LB/U
HOURS
2196.34
1229.66
1402.19
322.62
1211.74
321.54
933.78
136.28
1860.05
422.84
HC
EMISSION
LBS.
0.4393
0.2459
0.0070
0.001')
0.1006
0.0267
0.0934
0.0136
0.1246
0.0283
0.765
0.277
0.034
0.013
NO
LB/U
LB FUEL
0.62
0.34
25.68
10. 80
7.07
5.18
2.03
1.25
0.87
0.30
NO
LB/IK
HOURS
18. R7
12.62
3030.31
999.79
695.86
423.85
119.05
73.92
27.65
17.44
NO
EMISSION
LBS.
0.0038
0.0025
0.0152
0.0050
n.0576
0.0352
0.0119
0.0074
0.0019
0.0012
0.0904
0.0464
0.0039
0.0020
1-109
-------
SUMMARY 10 540
MODEL SUMMARY
SIMPLE NUMBER 7.
TEST
MODE
2
6
7
9
10
ITAL FOR
ITAL FOR
MEAN:
STD DEVI
MEAN:
STD DEV:
MEAN:
STO DEV:
MEAN:
STD DEVI
MEAN:
STO OEV:
CYCLE
CYCLE/LB
MEASURED
FUEL FLOW
LB/HR
19.60
6.05
120.96
25.54
91.74
27.96
47.69
15.67
18.00
5.60
MEAN:
STD OEV:
FUEL
FUEL
USED
LBS.
3.92
1.21
0.60
0.13
7.61
2.32
4.79
1.57
1.21
0.36
18.134
5.339
CO
LB/IK
LB FUEL
692.19
109.31
1250.01
108.73
1241.15
116.23
1226.35
111.85
1099.37
118.20
CO
LB/IK
HOURS
17097.97
4407.29.
149399.25
25252.25
111656.88
28862.23
57559.49
16682.53
19424.22
4951.68
MFAN:
STD OEV:
CO
EMISSION
LBS.
3.420
0.881
0.747
0.126
9.268
2.396
5.756
1.668
1.301
0.332
20.491
4.964
1.151
0.099
HC
LB/IK
LB FUEL
129.00
88.48
19.31
4.62
19.69
5.19
23.30
7.15
153.39
81.07
HC
LB/IK
HOURS
2198.03
1316.39
2256.04
177.75
1685.16
249.79
1021.38
110.38
2623.89
1195.70
HC
EMISSION
LBS.
0.4196
0.2633
0.0113
0.0019
0. 1399
0.0207
0.1021
0.0110
0.1758
O.OflOl
0.869
0.283
0.053
0.024
NO
LB/1K
LB FUEL
0.87
0.39
0.74
0.41
0.74
0.50
0.76
0.51
0.47
0.40
NO
LB/IK
HOURS
18.71
11.57
94.67
56.36
76.88
57.64
40.04
26.42
10.06
10.11
NO
EMISSION
LBS.
0.0037
0.0023
0.0005
0.0003
0.0064
0.0048
0.0040
0.0028
0.0007
0.0007
0.0153
0.0100
0.0008
0.0004
SUMMARY 0 - 540
MODEL SUHNARY
SIMPLE NUMBER - 6.
TEST
MODE
2
6
7
9
10
1TAL FOR
IfiL FOR
MEAN:
SID OEV:
MEAN:
STD OEv:
MEAN:
STT> DEV:
MEAN:
STD DEVI
MEAN:
STD OEV:
CYCLE
CYCLE/LB
MEASURED
FUEL FLOH
LB/HR
24.92
1.32
110.78
1.94
94.07
12.77
55.67
3.03
26.10
2.33
MEAN:
STO DEV:
FUEL
FUEL
USED
LBS.
4.911
0.26
0.55
0.01
7.81
1.06
5.57
0.31
1. 75
0.16
20.660
1.143
CO
LB/U
LB FUEL
751.00
131.12
944.56
92.53
826.04
170.66
1006.55
210.05
731.05
180.76
CO
LB/1K
HOURS
18834.69
4162.94
104622.31
10164.48
79344.81
26105.00
56219.13
13442.22
20301.05
4797.29
MEAN:
STD REV:
CO
EMISSION
LBS.
3.767
0.833
0.523
0.051
6.586
2.167
5.622
1.344
1.360
0.321
17.053
2.291
0.86?
0.085
HC
IB/IK
LB FUEL
49.21
20.52
23.76
16.34
19.30
11.55
25.57
13.52
52.00
22.59
HC
LB/IK
HOURS
1233.77
525.50
2634.41
1811.92
1890.62
1374.78
1448.67
B17.24
1328.80
524.57
HC
MISSION
LBS.
0.2468
0.1051
0.0132
0.0091
0. 1569
0.1141
0.1449
0.0817
0.0690
0.0351
0.651
0.321
0.031
0.014
NO
LB/IK
LB FUEL
0.78
0.79
5.16
1.33
19.30
14.69
4.00
1.83
1.14
0.54
NO
LB/IK
HOURS
19.33
A. 67
573.04
15S.74
1760.37
1318.45
222.51
106.15
30.46
17.27
NO
EMISSION
LBS.
0.0039
0.0013
0.0029
0.0008
0.1461
0. 1094
0.0223
0.0106
0.0020
C.0012
0.1771
0.1012
0.0086
0.0049
1-110
-------
SERIAL NUNREit 1-UB44-27AA
DATEl ' 7/28/71
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCONING
ENGINE DATA «»»««««««*«««««
CAL 10 NUMBER! 250 ENGINE TYPE AND MODEL! 0-32O-E2A
RATED HORSEPOWER! 150.
ENGINE TOTAL TINE! 720. HRS
FUEL! AV GAS 80/87 FUEL H/C RATIO! 1.840
OPERATIONAL DATA »».»«»»»**«**«»
INLET AIR TEMPERATURE. DEGREES Fl START 74.00 FINISH 74.00
ATMOSPHERIC PRESSURE! START 29.84 FINISH 29.84
INLET AIR HUH 101TY, CRN H20/LB AIR! 0.01
RELATIVE HUMIDITY! 12.00 PERCENT
SAMPLE LINE! TEMPERATURE. DEGREES Cl -O.OOi FLOW RATE. LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TIME. SEC! 1.60
NUMBER OF TESTS! 5
COMMENTS!
CARS.
HEATER
IDLE-LOW
IDLE/TAXI
RUN UP
RUN UP-LEAN
RUN UP-RICH
TEST
NODE
ENGINE
RPN
-0.0
-0.0
-0.0
-0.0
-0.0
MEASURED
FUEL FLOW
LB/KR
15.20
18.80
35.20
35.20
34.00
MEASURED
AIR FLOW
LB/HR
181.00
223.00
397.00
401.00
388.00
CALCULATED
F/A
0.03369
0.04885
O.OT349
0.07286
0.07283
TEST
NODE
1
2
3
4
3
E«H»UST
GAS
TEMP
DEGREES F
314.00
449.00
1031.00
964.00
1099.00
FXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
CO CO THC
IDRYI 2 IDRVI
PERCENT V (DRY) PPMV
PERCENT V
3.10
4.70
8.30
8.10
8.10
3.90
5.60
7.30
7.40
7.40
1537.00
1482.00
2141.00
1867.00
1812.00
NO
IDRYI
PPMV
14.00
24.00
31.00
23.00
22.00
NO
2
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
NO
I
IDRYI
PPNV
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
(DRY)
6.00
5.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MtlOE
MASS EMI
cn
LB/1K
LB FUEL
875.45
908.78
1060.1?
1043.17
1043.54
MASS EMI
HC
LB/1K
LB FUEL
24.86
16.41
15.66
13.77
13.37
MASS EMI MASS EMI MASS EMI
N02 C02 NO
IB/IK LB/IK IB/IK
LB FUEL LB FUEL LB FUEL
0.0
0.0
0.0
0.0
0.0
1710.51
1701.32
1465.27
1497.41
1497.93
0.65
0.76
0.65
0.49
0.47
MASS EMI
NOI
LB/IK
IB FUEL
0.65
0.76
0.65
0.49
0.47
MASS EMI
CO
LB/HR
13306.88
17085.02
37323.13
36719.59
35480.24
MASS EMI
HC
LB/KR
37T.86
308.54
551.39
484.73
414.57
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
MASS EMI
C02
LB/HR
26303.74
31984.85
51577.57
52708.77
50929.73
NtSS EMI
NO
LB/KR
9.87
14.33
22.90
17.13
15.83
MASS EHI
NO*
LB/HR
9.87
14.33
22.90
17.13
15.83
1-111
-------
******<*»****«»******
SERIAL NIMBEftl L-W302-27AA
OtTEl 7/10/71
TEST ORGANIIATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER I LVCONING
ENGINE 0«I» «»**«*
C»L 10 NUMBER! 259 ENGINE TYPE ANO MODEL! 0-120-E2A
RATED HORSEPOTERI ISO.
ENGINE TOTAL TINEl 139. HRS
FUEL! »V GAS 80/87 FUEL H/C RATIO! I.MO
OPERATIONAL DATA «««»«»«»«»*
INLET AIR TENPERATUREt DEGREES Fl START 97.00 FINISH 86.00
ATMOSPHERIC PRESSURE: START JO.II FINISH 10.19
INLET AIR HUHIDITT, CRN H20/LB AIRI 0.01
RELATIVE HUMIDITY! 45.00 PERCENT
SAMPLE LINE: TEMPERATURE! DEGREES Cl -0.00. FLO* RATE. LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TIME, SECl 1.60
NUMBER OF TESTS) 8
COMMENTS!
CARB.
HEATER
RUN UP
RUN UP-LEAN
TAKE-OFF
CLIMS
DESCENT
DESCENT
APPROACH
TAXI
TEST
MODE
3
*
6
7
8
a
9
10
ENGINE
RPM
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
MEASURED
FUEL FLON
LB/HR
19.30
19.30
42.20
42.20
24.60
24.60
17.60
5.30
MEASURED
AIR FLON
LB/HR
220.00
221.00
4T2.00
472.00
395.00
298.00
196.00
65.00
CALCULATED
F/A
0.06862
0.06(07
0.07264
0.07264
0.06176
0.06121
0.061SO
0.06121
TEST
MODE
9
10
EXHAUST
GAS
TEMP
DEGREES F
1054.00
1076.00
1300.00
1300.00
1233.00
1211.00
942.00
471.00
EXHAUST
GAS
PRESSURE
PSU
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO CO THC
I DRY) 2 IDRYI
PERCENT V (DRY) PPNV
PERCENT V
7.50
7.40
8.40
8.40
6.30
6.00
7.90
S.30
7.00
7.00
7.00
7.00
7.70
7.90
6.50
7.70
3506.00
2337.00
2112.00
2112.00
1886.00
1830.00
2900.00
2112.00
NO
IDRYI
PPNV
104.00
80.00
8.00
8.00
40.00
108.00
66.00
68.00
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
X
I DRY I
PPNV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
(DRY)
-0.00
-0.00
-0.00
10.00
6.00
S.OO
7.00
4.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICIPATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
6
7
8
8
9
10
MASS EMI
CO
LB/IK
LB FUEL
1027.20
1031.60
1087.04
1087.04
897.02
860.71
1086.44
810.47
MASS EMI
HC
LB/IK
LB FUEL
19.66
18.48
15.65
I5.6S
15.38
15.03
22.84
16.50
MASS EMI MASS EM| MASS EMI
N02 C02 NO
LB/IK LB/1K LB/IK
LB FUEL LB FUEL LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
1506.36
1518.39
1423.32
1423.32
1722.63
1780.62
1404.S3
1850.07
2.34
1.81
0.17
0.17
0.94
2.54
1.49
1.71
MASS EMI
NOX
LB/IK
LB FUEL
2.34
1.81
0.17
0.17
0.94
2. 54
1.49
1.71
MASS EMI
CO
LB/HR
19824.87
19716.80
45873.02
45873.02
23066.71
21173.50
19121.38
429S.47
MASS EMI
HC
LB/KR
379.38
356.62
660.57
660.S7
378.34
369.86
402.01
9S.03
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
MASS EMI
CO?
LB/HR
29072.69
29304.96
60064.01
60064.01
42376.60
43803.31
24719.74
9805.38
MASS EMI
ND
LB/KR
45. 15
35.01
7.18
7.18
23.01
62.60
26.24
9.05
MASS EMI
NOX
LB/HR
45.15
35.01
7.18
7. IB
23.01
62.60
26.24
9.05
1-112
-------
DATE: 6/17/11
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEOYNE-CONTINENTAL
ENGINE DAT* «»««»««**
CAL ID NUMBER: 363 ENGINE TYPE AND MODEL I IO-36O-C
RATED HORSEPOHERI 210.
ENGINE TOTAL TINEl TOO. MRS
FUELt «v G»S 100/130 FUEL H/C KATIO: 1.8*0
OPERATIONAL D»t» **»*»»*»«*»*«*»»»»*
INLET AIR TEMPERATURE, DEGREES Fl START 8*.00 FINISH 84.00
ATMOSPHERIC PRESSURE: START 30.24 FINISH 30.24
INLET AIR HUMIDITY, CRN H20/LB AIR: 0.02
RELATIVE HUMIDITY: 66.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES Cl -0.00. FLO* RATEi LITERS/MINI T.OO
SAMPLE LINE TRANSPORT TINE. SECl 1.60
NUMBER OF TESTS: 8
COMMENTS)
APPROACH NODE MISSING
SERIAL NUMBER! MS9I-6CB
CARB.
HEATER
I OLE-LOU
IDLE/TAXI
RUN UP
RUN UP-LEAN
RUN UP-RICH
TAKE-OFF
CLIMB
DESCENT
TEST
MODE
ENGINE
RPM
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
MEASURED
FUEL FLOX
LB/HR
16.40
19.90
22.10
19.90
19.40
91.40
59.80
42.20
MEASURED
AIR FLOW
LB/HR
194.00
262.00
293.00
267.00
2T2.00
IOT6.00
T8I.OO
5)8.00
CALCULATED
F/A
0.06361
0.06765
O.OT01I
0.06789
0.06592
0.OTB59
0.07102
0.072*9
TEST
MODE
EXHAUST
GAS
TEMP
OEGRFES F
673.00
729.00
419.00
897.00
953.00
1289.00
1356.00
I26T.OO
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
(ORYI
PERCENT
2.80
3.40
4.30
3.50
3.20
7.80
4. TO
5. JO
CO
2
V IDRY)
PERCENT
9.40
10.40
10. TO
10.90
11.10
8.80
10.60
10.10
THC
IDRV)
PPMV
V
16*70.00
9882.00
3*0*. 00
4T21.00
153T.OO
4282.00
2306.00
2086.00
NO
«ORYI
PPMV
42.00
56.00
309.00
150.00
ITT.00
262.00
T96.00
564.00
NO
2
I DRY I
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
X
I DRY I
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
IDRYI
*2.00
35.00
-0.00
-0.00
-0.00
-0.00
18.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
MASS EMI
CO
LB/IK
LB FUEL
408.51
*6*.*B
566.28
*75.**
**7.27
925.*0
611.38
702.86
MASS EMI
HC
LB/IK
LB FUEL
137.62
77.32
25.67
36.73
12.30
29.10
17.18
15.27
MASS EMI MASS EMI MASS EMI
N02 C02 NO
LB/IK LB/IK LB/IK
L8 FUEL LB FUEL LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
215*.83
2232.33
221*.05
2326.45
243T.T2
16*0.42
2166.49
2028.00
1.01
1.26
6.68
3.35
4.06
5.11
IT.01
II. 6*
MASS EMI
NOX
LB/IK
LB FUEL
1.01
1.26
6.68
3.35
4.06
5.11
IT. 01
11. 8*
MASS EMI
CO
LB/HR
6699.58
92*3.11
12628.09
9*61.29
8900. T3
84581.13
36560.53
29660.84
MASS EMI
MC
LB/HR
2256.99
1538.61
5T2.54
T30.91
244.85
2659.32
102T.35
644.29
MASS EMI
NO 2
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
MASS EMI
C02
LB/HR
35339.13
44423.31
493T3.2T
46296.39
48510.62
149933.44
129556.31
85581.56
MASS EMI
NO
LB/HR
16.51
25.01
149.06
66.60
80.67
466.66
1017.06
499.60
MASS EMI
NOX
LB/HR
16.51
25.01
149.06
66.60
80.87
466.66
1017.06
494.60
1-113
-------
Omi 7/16/Tl
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEDVNE-CONTINENTAl
ENGINE f»TA ««»«««««*»»*»«*»«»*»
C»L ID NUMBER! 16* ENGINE TYPE AND HOD EL I O-4TO-0 $E»UL NUMBER! 20124T-7W6
RATED HORSEPOWER: 210.
ENGINE TOTAL TINE: 182. MRS
FUELt AV GAS BO/87 FUEL H/C RATIO! 1.1*0
INLET AIR TEMPERATURE, DEGREES Fl START 91.00 FINISH 91.00
ATMOSPHERIC PRESSURE! START 29.9$ FINISH 29.95
INLET AIR HUMIDITY, CRN H20/LB AIR1 0.01
RELATIVE HUMIDITY: 40.00 PERCENT
SAMPLE LINEl TEMPERATURE, DEGREES Cl -0.00. FLOW RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SECl 1.60
NUMBER OF TESTS) 10
COMMENTS:
APPROACH MODE MISSING
T.OO
CARB.
HEATER
TEST
MODE
I OLE-LOW
IDLE/TAXI
RUN UP
RUN UP-LEAN
RUN UP-RICH
TAKE-OFF
CLIMB
DESCENT
DESCENT
TAXI
ENGINE
RPN
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
MEASURED
FUEL FLOW
LB/HR
10.60
15.00
35.50
14.60
14.60
106.60
101.00
52.50
60.10
11.50
MEASURED
AIR FLOW
LB/HR
119.00
184.00
449.00
441.00
446.00
1240.00
1110.00
681.00
646.00
146.00
CALCULATED
F/A
0.07215
0.06879
0.0687S
0.06498
0.06624
0.07406
0.06864
0.06917
0.07646
0.06921
TEST
NODE
EXHAUST
GAS
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
149.00
133.00
128.00
EXHAUST CO
GAS IDRY)
CO
2
PRESSURE PERCENT V IORYI
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
.20
.10
.60
.10
.00
.90
.70
.10
.80
.50
PERCENT
7.40
8.60
9.20
8.90
9.10
7.90
10.20
9.90
6.40
9.40
THC
IORYI
PPMV
V
9195.00
2009.00
1359.00
1004.00
1004.00
1812.00
827.00
768.00
1771.00
1516.00
NO
IDRYI
PPMV
10.00
41.00
122.00
70.00
78.00
150.00
94.00
78.00
22.00
45.00
NO
2
IORVI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
IDRYI
30.00
11.00
-0.00
-0.00
-0.00
8.00
8.00
6.00
4.00
2.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PART1CULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
HOOF
2
3
4
5
6
7
8
8
10
MASS EMI
CO
LB/IK
LB FUEL
936.05
827.03
757.46
730.70
701.45
998.54
633.74
683.38
1208.89
738.12
MASS EMI
MC
LB/IK
LB FUEL
69.95
15.60
10.53
8.24
B. 07
13.26
6.39
5.89
12.53
11.81
MASS EMI MASS EMI MASS EMI
N02 C02 NO
LB/IK LB/IK LB/IK
LB FUEL LB FUEL LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
1511.59
1812.00
1955.22
2003.54
2049.97
1568.93
2160.98
2084.33
1240.45
1982.11
0.21
0.91
2.71
1.65
1.80
3.11
2.08
1.72
0.45
0.99
MASS EMI MASS EN
NOX CO
LB/IK LB/HR
LB FUEL
0.21
0.91
2.71
1.65
1.80
3.11
2.08
1.72
0.45
0.99
9922.09
12405.39
26889.74
25282.29
24270.18
106444.25
64007.48
35877.48
72895.81
8488.32
MASS EMI
HC
LB/HR
741.50
211.99
171.71
281.05
279.11
1411.71
645.04
109.4]
755.12
115.77
MASS EMI
N02
LB/HR
MASS EMI
C02
LB/HR
MASS EMI
NO
LB/HR
MASS EMI
NOX
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
16022.87
27480.02
69410.44
69122.56
70929.06
167247.88
218258.56
109427.19
74798.88
22794.23
2.26
13.70
96.22
57.00
62.19
331.98
210.27
90.13
26.88
11.41
2.26
13.70
96.22
57.00
62.19
311.98
210.27
90.13
26.88
11.41
1-114
-------
OATEl T/16/T1
TEST ORGANIZATION! SCOTT/CEN AVIATION
ENGINE SUPPLIERI TEIEOYNE-COICTINENTAL
FNCINE 0»T«
CAl 10 NUNBERl 16} ENGINE TYPE «NO HOTELI O-4TO-R
RATED MORSEPOUERl 230.
ENGINE TOTAL TINEl 182. HRS
FUEL) AV GAS BO/IT FUEL H/C RATIOI 1.8*0
OPERATIONAL DATA >»»»»»
INLET AIR TENPERATUXEi DEGREES Fl START 91.00 FINISH 91.00
ATMOSPHERIC PRESSUREl START 29.93 FINISH 29.91
INLET AIR HUMIDITY, GRN II20/LB AIRI 0.01
RELATIVE HUMIDITVI 40.00 PERCENT
SAMPLE LINEI TEMPERATURE. DEGREES Cl -0.00. FLOW RATE. LITERS/MINI T.OO
SAMPLE LINE TRANSPORT TIME. SEC: 1.60
NUMBER OF TESTSl 10
COMMENTS:
TAKE OFF MODE MISSING
SERIAL NUNBERI 20J4T-TORC
CARB.
HEATER
IOLE-LON
I OLE/Till
RUN UP
RUN UP-LEAN
RUN UP-RICH
CLIMB
DESCENT
OF SCENT
APPROACH
TAXI
TEST
MODE
1
2
1
4
5
7
8
a
9
10
ENGINE
RPM
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
MEASURED
FUEL FLOH
LB/HR
B.90
14.10
14.60
34.60
34.60
102.10
53.90
91.50
35.50
12.40
MEASURED
AIR FLO*
LB/HR
101.00
115.00
446.00
447.00
449.00
1U1.00
689.00
545.00
442.00
157.00
CALCULATED
F/A
0.07419
0.07091
0.07118
0.07019
O.OT058
0.07582
O.OT057
0.07903
0.06924
0.06842
TEST EXHAUST
NODE GAS
TEMP
DEGREES F
1 762.00
2 942.00
1323.00
1267.00
1334.00
1581.00
1569.00
1457.00
1278.00
10 1031.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
IORYI
PERCENT V
1
.30
.10
.40
.30
.20
.30
.40
.30
.00
.40
CO
2
IORYI
PERCENT V
7.90
9.10
10.00
9.90
10.10
7.90
9.90
6.40
B. 90
9.30
THC
(DRY)
PPNV
8569.00
1959.00
1199.00
963.00
965.00
1609.00
T90.00
2252.00
1199.00
1726.00
NO
IORVI
PPNV
13.00
32.00-
113.00
93.00
99.00
26.00
89.00
23.00
121.00
53.00
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
I
-------
ami 8/17/M
TEST ORGANIZATION! SCOTT/GEN AVIATION
ENGINE SUPPLIER! TELEDVNE-CONTINENTAL
ENGINE 0*r» «««««««««»*«««»»««»»«»«
01 ID NUNBERI 391 ENGINE TYPE MO RODEL> 0-«TO-fl SEOUL NUMBER! U15IO-6-RA
RATED HORSEPOWERl 210.
ENGINE TOTAL TINEl 69. MRS
FUEL: AV GAS lao/uo FUEL H/C RATIOS 1.940
OPERATIONAL DATA »*»««««»»»«»»»«»**»»»»«»'
INLET AIR TEMPERATURE, DEGREES Fl START 83.50 FINISH 81.90
ATMOSPHERIC PRESSURE! START 10.12 FINISH 10.12
INLET AIR HUMIDITY, CRN H20/LB AIRl 0.01
RELATIVE HUNIDITTl 18.00 PERCENT
SAMPLE LINE! TENPERATUREi DEGREES Cl -0.00. FLOW RATE, LITERS/MINI T.OO
SAMPLE LINE TRANSPORT TIME. SEC1 1.60
NUMBER OF TESTS! e
COMMENTSt
CARB.
HEATER
IDLE-LOW
IDLE/TAXI
RUN UP
RUN UP-LEAN
RUN UP-RICH
TAKE-OFF
CLIMB
DESCENT
TEST
MODE
ENGINE
RPM
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
MEASURED
FUEL FLOW
LB/HR
12.40
15.80
10.90
10.00
10.90
77.50
71.40
41.10
MEASURED
AIR FLOW
LB/HR
77.00
164.00
181.00
402.00
408.00
1148.00
10.9)
969.00
CALCULATED
F/A
0.08872
0.08667
0.07941
0.070)1
0.07088
0.06678
0.06497
0.07806
TEST
MODE
EXHAUST
GAS
TEMP
DEGREES F
918.00
fl97.00
1296.00
1390.00
1149.00
1681.00
1704.00
1592.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO CO THC
IDRT) 2 IORYI
PERCENT V I DRY I PPMV
PERCENT V
7.60
9.90
6.20
1.90
4.10
0.70
0.50
1.60
1.70
7.50
9.70
11.30
10.90
14.00
11.80
15.50
74911.00
12966.00
5199.00
2259.00
1222.00
1442.00
1289.00
1911.00
NO
(DRY)
PPMV
1.00
10.00
134.00
80.00
71.00
1281.00
4206.00
2681.00
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
(DRY)
16.00
24.00
-0.00
-0.00
-0.00
-0.00
12.00
12.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
MASS EMI
cn
Lfl/lK
LB FUEL
917.08
IOT2.0)
761.0]
910.77
559.65
95.27
70.01
420.56
MASS EMI
HC
LB/1K
LB FUEL
461.25
77.93
16.)]
16.91
24.02
11.24
10.14
12.9]
MASS EMI MASS EMI MASS EMI
N02 C02 NO
IB/IK LB/1K L8/1K
LB FUEL LB FUEL LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
625.01
1276.05
1879.68
2)29.10
2229.02
2991.72
1019.89
2477.97
0.05
0.18
2.71
1.72
1.56
73.15
96.7]
51.44
MASS EMI
NOX
LB/1K
LB FUEL
0.05
0.18
2.71
1.72
1.56
73.35
96.7)
51.44
MASS EMI
CO
LB/HR
10111.77
16917.99
21977.90
15)2). 16
17291.18
7)81.20
91)8.48
17284.94
MASS EMI
HC
LB/HR
9719.59
1231.31
1122.74
907.4)
742.1)
871.08
798.69
9)1.55
MASS EMI
N02
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
MASS EMI
C02
LB/HR
7750.17
20161.65
97998. )4
69759.00
68876.56
232013.38
2228)4.19
101844.56
MASS EMI
NO
IB/HR
0.66
2.81
8). 70
91.6)
48.22
9684.25
7099.9!
2114.18
MASS EMI
N0«
LB/HR
0.66
2.81
81.70
51.6)
48.22
5684.25
7099.91
2114.18
1-116
-------
OATEl 8/ 6/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: TELEOYNE-CONTINENTAL
ENGINE DATA »«**«««*»»»»«
CAl ID NUMBER! 268 ENGINE TYPE AND MODEL) IO-S20-P SERIAL NUNBERl 110140-3-AA
RATED HORSEPOKERI 300.
ENGINE TOTAL TINEI HJ6. MRS
FUEL: AV GAS 100/130 FUEL H/C RATIOI 1.8*0
OPERATIONAL DATA ««»»««»*«»«»««»«»»«««*«»«»»*«»«
INLET AIR TEMPERATURE, DEGREES Ft START T3.00 FINISH 11.00
ATMOSPHERIC PRESSURE: START 30.24 FINISH 30.24
INLET AIR HUNIOITV, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY: 49.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00. FLOW RATE. LITERS/MINI T.OO
SAMPLE LINE TRANSPORT TIME, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
NO FUEL FLOW DATA
CARB.
HEATER
IDLE-LOM
IDLE/TAXI
RUN UP
RUN UP-LEAN
RUN UP-RICH
TAKE-OFF
CLIHB
DESCENT
APPROACH
TAXI
TEST
NODE
1
2
3
4
5
6
7
B
9
10
ENGINE
RPN
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
MEASURED
FUEL FLO*
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MEASURED
AIR FLOW
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CALCULATED
F/A
0.07314
0.07797
0.07210
0.07178
0.07080
0.06335
0.06312
0.06386
0.06901
0.079S2
TEST
MODE
4
5
6
7
e
9
10
FKHAUST
GAS
TEMP
DEGREES F
5*1.00
684.00
1076.00
1041.00
1076.00
1469.00
1469. 00
1)90.00
1211.00
740.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
IORYI
PERCENT V
7.00
8.50
7.50
6.90
6.70
2.60
2.80
4.40
6. SO
8.30
CO
2
IORVI
PERCENT
7.70
7.10
7.90
8. 40
8.40
11.00
10.90
9.80
8.20
7.10
THC
IDRYI
PPNV
V
11621.00
11621.00
2480.00
2313.00
2202.00
2870.00
1310.00
1S33.00
2202.00
16972.00
NO
(DRY)
PPNV
12.00
15.00
47.00
35.00
32.00
359.00
213.00
-0.00
-0.00
-0.00
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
IDRYI
14.00
9.00
-0.00
-0.00
-0.00
-0.00
5.00
9.00
5.00
14.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
1-117
-------
OtTEl B/ 6/71
TEST ORGANItATIONI SCOTT/GEN AVIATION
ENGINf SUPPLIER! TELEDYNE-CONTINENTAl
ENGINE OATt »«*»*»»****»***********»*«*****»**
CAL ID NUMBER: 2*9 ENGINE TYPE AND MODEL I 10-520-P SERIAL NUMEItl I10I4O-1-AB
RATED HORSEPOWER: 300.
ENGINE TOTAL TINE. 15)6. MRS
FUEL I AV GAS 100/130 FUEL H/C RATIOI 1.8*0
OPERATIONAL DATA »««»«»«»««»
INLET AIR TEMPERATURE. DEGREES Fl START T9.00 FINISH 80.00
ATMOSPHERIC PRESSURE: START 30.24 FINISH 30.24
INLET AIR HUMIDITY, GRN H20/LB AIRl 0.01
RELATIVE HUMIDITY: 42.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES Cl -0.00, FLO* RATE, LITERS/MIN: T.OO
SAMPLE LINE TRANSPORT TIME, SECl 1.60
NUMBER OF TESTS: 10
COMMENTS:
NO FUEL FLOW DATA
CARB.
HEATER
IDLE-LOU
IDLE/TAXI
RUN UP
DUN UP-LEAN
RUN UP-RICH
TAKE-OFF
CLIMB
DESCENT
APPROACH
Tax I
TEST
NODE
6
T
8
9
10
ENGINE
RPM
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
MEASURED
FUEL FLON
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MEASURED
AIR FLOH
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CALCULATED
F/A
0.0751*
0.076)9
0.07666
0.07)91
0.07498
0.071)2
0.07127
0.07J39
0.07393
0.07718
TEST
MODE
1
2
3
4
5
6
7
a
9
10
EXHAUST
GAS
TEMP
DEGREES F
181.00
141).00
964.00
942.00
986.00
1390.00
1424.00
1278.00
1166.00
773.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO CO THC
IORYI 2 IORY)
PERCENT V I DRY I PPMV
PERCENT V
6.80
7.20
8.00
7.40
7.20
3.70
3.10
5.20
6.10
3. 30
4.60
7.00
8.30
8.80
8.80
12.20
12.50
10.70
9.60
6.70
4)8)1.00
22677.00
2731.00
2)11.00
2)11.00
29S2.00
1241.00
1)17.00
1848.00
1)642.00
NO
I DRV I
PPNV
-0.00
-o.oo-
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
2
IORYI
PPNV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO ALDEHYDES
» (DRYI
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
17.00
24.00
-0.00
-0.00
-0.00
-0.00
9.00
9.00
5.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
1-118
-------
DATE: 8/ 6/71
TEST ORGANIZATION: SCOTT/GEN »VI»TION
ENGINE SUPPLIER! TELEDVNE-CONTINENTAL
ENGINE 0»I»
SERIAL NUM8ER1 110I4O-JAC
C»l 10 NUNBERI 270 ENGINE TYPE (NO MODEL! 10-S20-P
RATED HORSEPOWER! 300.
ENGINE TOTAL TIME! 1556. MRS
FUEL I «V GAS 100/110 FUEL H/C RATIOl 1.8*0
OPERATIONAL DATA *««««««»««
INLET AIR TENPERATUKE. DEGREES Fl START 8J.OO FINISH 81.00
ATMOSPHERIC PRESSURF.I START 30.24 FINISH 10.1*
INLET AIR HUHIDIIY, CRN H20/LB AIR: 0.01
RELATIVE HUMIDITY! 40.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOW RATE. LITERS/MINI T.OO
SAMPLE LINE TRANSPORT TIME. SECt 1.60
NUMBER OF TESTS: 10
COMMENTS:
NO FUEL FLOW DATA
CARB.
HEATER
IDLE-LOW
IDLE/TAKI
RUN UP
RUN UP-LEAN
RUN UP-RICH
TAKE-OFF
CLIMB
DESCENT
APPROACH
TAKI
TEST
NODE
1
2
3
4
5
6
T
8
9
10
ENGINE
RPM
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
MEASURED
FUEL FLOW
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MEASURED
AIR FLO*
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CALCULATED
F/A
0.056*6
0.07501
0.07160
0.06958
0.07376
0.06777
0.06502
0.06629
0.06802
0.07531
TEST
MODE
2
1
*
5
6
7
8
9
10
EXHAUST
GAS
TEMP
DEGREES F
594.00
796.00
1099.00
1110.00
1054.00
1592.00
1592.00
1446.00
1300.00
942.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
(DRY)
PERCENT
4.20
6.10
6.50
5.30
6.20
1.20
2.40
4.60
5.70
7.70
CO
2
V IDRTI
PERCENT
4.40
8.00
8.80
9.70
9.70
11.40
11.80
9.70
8.90
7.00
THC
IDRY)
PPMV
V
34110.00
21068.00
2229.00
1505.00
1561.00
2787.00
1059.00
1393.00
1561.00
14882.00
NO
IDRTI
PPMV
0.0
30.00.
71.00
108.00
102.00
-0.00
90.00
418.00
256.00
29.00
NO
2
I DRY I
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO ALDEHYDES
X IDRYI
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
34.00
41.00
-0.00
-0.00
-0.00
-0.00
15.00
15.00
14.00
19.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
1-119
-------
DATE! S/ 6/71
TEST ORGANIIATIONI SCOTT/GEN AVIATION
ENGINE SUPPLIER! LYCONING
ENGINE OATA «««««««««»««»»»»«»
CAL ID NUMBER: 262 ENGINE TYPE AND MODEL1 IO-540-C485 SERIAL NURIERt L-401-48A
RATED HORSEPOMERI 250.
ENGINE TOTAL TINEl 1318. MRS
FUELl AV GAS 100/130 FUEL H/C RATIOl 1.8*0
OPERATIONAL DATA »»»»»»«««»»»»««*»»»»»««»
INLET AIR TEMPERATURE, DEGREES Ft START 82.00 FINISH 83.00
ATMOSPHERIC PRESSURE: START 29.40 FINISH 24.90
INLET AIR HUMIDITY, GRN H2O/LB All! 0.02
RELATIVE HUNIDITVl 63.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES Cl -0.00, FLOW RATE, LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TIME, SECI 1.60
NUMBER OF TESTS: 10
COMMENTS:
NO FUEL FLOM DATA
CARB.
HEATER
IOLE-LOM
IDLE/TAXI
RUN UP
RUN UP-LEAN
RUN UP-RICH
TAKE-OFF
CLIMB
DESCENT
APPROACH
TAXI
TEST
MODE
1
2
3
4
5
6
7
8
9
10
ENGINE
RPM
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
MEASURED
FUEL FLOW
LB/HR
-0.00
-0.00.
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MEASURED
AIR FLOK
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CALCULATED
0.08)67
0.08431
0.07848
0.07896
0.07827
0.04348
0.09578
0.09134
0.08322
O.OS587
TEST
MOOf
EXHAUST
GAS
TEMP
DEGREES F
628.00
740.00
1222.00
1143.00
1233.00
1300.00
1256.00
1256.00
1143.00
673.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
I DRY)
PERCENT
8.50
9.70
9.30
9.20
9.10
12.90
12.60
12.10
9.90
a. 40
CO
2
V IORYI
PERCENT
4.50
6.40
7.40
7.40
7.50
6.80
7.70
7.20
7.70
4.80
THC
IDRYI
PPMV
V
52045.00
19594.00
2965.00
3074.00
2525.00
3349.00
3129.00
3184.00
3294.00
50728.00
NO
IORYI
PPMV
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
IORVI
63.00
46.00
-0.00
-0.00
-0.00
-0.00
12.00
9.00
6.00
33.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
1-120
-------
DATE! 8/ 6/71
TEST ORGANIZATION! SCOTT/GEN IVIATION
ENGINE SUPPLIER! LTCONING
ENGINE OAT*
CAL ID NUMBER I 263 ENSINE TYPE AND NQOELI IO-5*O-C*BJ
RATED HORSEPOHERI 290.
ENGINE TOTAL TINEl HIS. MRS
FUEL I AV GAS 100/130 FUEL H/C RATIOI 1.8*0
OPERATIONAL DATA »»««»«««»««*
INLET AIR TEMPERATURE. DEGREES Ft START 03.00 FINISH 66.00
ATMOSPHERIC PRESSURE! START 29.40 FINISH 29.90
INLET AIR HUMIDITY, CRN H20/L8 AIR1 0.02
RELATIVE HUMIDITY! 61.00 PERCENT
SAMPLE LINE" TEMPERATURE, DEGREES Cl -0.00! FLO* RATE. LITERS/MINI T.OO
SAMPLE LINE TRANSPORT TIME. SECl 1.60
NUMBER OF TESTS: 10
COMMENTS!
NO FUEL FLOW DATA
SERIAL NUMBER! l-90l-»8S
CARB.
HEATER
(OLE-LOW
IDLE/TAXI
RUN UP
RUN UP-LEAN
RUN UP-RICH
TAKE-OFF
CLIMB
DESCENT
APPROACH
TAXI
TEST
MODE
ENGINE
RPN
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
MEASURED
FUEL FLO*
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MEASURED
AIR FLOH
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CALCULATED
F/A
0.08317
0.08091
0.07*52
0.07252
0.0750*
0.08789
O.OBII9
0.08823
0.08*32
0.08305
TEST
MODE
EXHAUST
GAS
TEMP
DEGREES F
516.00
650.00
1166.00
1177.00
12)3.00
1323.00
1289.00
1267.00
1166.00
7*0.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
IDRY)
PERCENT
6.*0
7.50
7.90
7.*0
a. oo
11. 80
10.30
10.90
9.50
9.30
CO
2
V IDRYI
PERCENT
*.50
5.»0
7. BO
7.90
7.90
6.70
6.80
7.80
8.40
5.*0
THC
IORV)
PPMV
V
67866.00
*3699.00
3752.00
3531.00
292*. 00
3366.00
3200.00
3090.00
3255.00
30126.00
NO
IORYI
PPNV
28.00
*3.00
115.00
87.00
71.00
131.00
*5.00
51.00
78.00
75.00
NO
2
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
X
IORYI
PPMV
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
IORVI
59.00
6T.OO
-0.00
-0.00
-0.00
-0.00
12.00
21.00
6.00
27.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
1-121
-------
OATEl B/ 6/71
TEST ORGANIZATION: SCOTT/GEN »VI«TION
ENGINE SUPPLIERl LYCOHING
ENGINE DATA
CM 10 NUMBER: 26* ENGINE TYPE AND MODELi io-S40-c*B5
RATED HORSEPOWER! 250.
ENGINE TOTAL TINE: 1319. MRS
FUEL! »V GAS 100/130 FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA *»
INLET AIR TEMPERATURE. DEGREES Ft START 66.00 FINISH 87.00
ATMOSPHERIC PRESSURE! START 29.90 FINISH 29.90
INLET AIR HUMIDITY, CRN H20/LB A1RI 0.02
RFLATIVE HUMIDITY: 60.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES Cl -0.00. FLOM RATE. LITERS/MINI T.OO
SAMPLE LINE TRANSPORT TIME. SEC: l.AO
NUMBER Of TESTS! 10
COMMENTS:
NO FUEL FLOW DATA
SERIAL MUMSERI L-901-4SC
»****»
CARS.
HFATER
IOLF-LQW
IDLE/TAXI
RUN UP
RUN UP-LEAN
RUN UP-RICH
TAKE-OFF
CLIMB
DESCENT
APPROACH
TAXI
TEST
MODE
1
2
3
4
5
6
7
a
9
10
ENGINE
RPN
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
MEASURED
FUEL FLOW
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MEASURED
AIR FLOM
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CALCULATED
F/A
0.08518
0.08220
0.07613
0.07185
0.07568
0.09024
0.09657
0.09267
0.08541
0.09229
TEST
MODE
EXHAUST
GAS
TEMP
DEGRFES F
538.00
661.00
1166.00
1188.00
1233.00
1289.00
1289.00
1267.00
1166.00
695.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO CO THC
(DRY) 2 IDRT)
PERCENT v IDRVI PPNV
PERCENT V
7.50
7.90
7.90
7.70
7.80
12.10
12.30
11.30
9.40
9.50
5.20
6.50
8.20
8.40
8.30
6.90
8.20
8.40
8.80
5.00
56141.00
32278.00
3504.00
3062.00
2621.00
3559.00
3338.00
3173.00
2952.00
51479.00
NO
IDRT I
PPMV
19.00
40.00
140.00
98.00
98.00
55.00
55.00
67.00
105.00
35.00
NO
2
I DRV)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO ALDEHYDES
X IORYI
I DRY I
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
84.00
62.00
-0.00
-0.00
-0.00
-0.00
15.00
10.00
9.00
32.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
1-122
-------
DATE: 8/ 6/71
TEST ORGANIZATION: SCOTT/GEN AVIATION
ENGINE SUPPLIER: LYCONING
ENGINE 0«T»
C*L ID NUMBER: 265 ENGINE TYPE AND MODEL: IO-540-C4B5
RATED HORSEPOMER: 250.
ENGINE TOTAL TIME: 130*. MRS
FUEL: FUEL M/C RATIO: 0.251
OPERATIONAL DATA «<.*«««»
INLFT AIR TEMPERATURE. DEGREES F: START 86.00 FINISH 86.00
ATMOSPHERIC PRESSURE: START 29.90 FINISH 29.90
INLFT AIR HUMIDITY, GUN HJO/LB AIR: 0.01
RELATIVE HUMIDITY: 52.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00. FLOM RATE. LITERS/MINI 7.00
SAMPLE LINE TRANSPORT TINi;, SEC: 1.60
NUMBER OF TESTS: 10
COMMENTS:
NO FURL FLOW OATt
SERIAL NUMBER: L-1623-48A
CARB.
HEATER
IDLE-LOW
IDLE/TAXI
RUN UP
RUN UP-LEAN
BUM UP-RICH
TAKE-OFF
CLINB
DESCENT
APPROACH
TA«I
TEST
MODE
I
2
3
4
5
6
7
e
9
10
ENGINE
RPM
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
-0.0
MEASURED
FUEL FLOM
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MEASURED
AIR FLOM
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CALCULATED
F/A
0.08279
0.07913
0.08267
0.08039
0.08298
0.12776
0.10178
0.09987
0.09340
0.07926
TEST
MODE
1
2
3
4
5
6
7
a
9
10
EXHAUST
GAS
TEMP
DEGREES F
78.00
830.00
1211.00
1256.00
1300.00
1334.00
1278.00
1276.00
1177.00
773.00
FXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CD CO
IDRYI 2
PERCENT V (DRY)
PERCENT
9.20 4.80
9.60 6.70
12.40 5.60
10.50 5.50
12.20 5.80
19.30
15.20
14.90
13.80
9.20
.00
.90
.80
.50
.80
THC
IDRYI
PPMV
V
48245.00
16803.00
5324.00
21794.00
5324.00
4769.00
44)6.00
4492.00
5157.00
37931.00
NO
IORYI
PPMV
5.00
16.00
18.00
19.00
11.00
11.00
10.00
11.00
11.00
14.00
NO
2
(OKYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
I DRY I
76.00
47.00
-0.00
-0.00
-0.00
-0.00
16.00
I).00
12.00
40.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
1-123
-------
TABLE H
LIGHT-UTILITY PISTON ENGINES
TELEDYIME/CONTINENTAL
CONTENTS:
11-2 TO 11-20 INDIVIDUAL ENGINE RUNS - COMPLETELY PROCESSED -
CLIMB LEAN MODE
11-21 MODEL SUMMARY - CLIMB LEAN MODE
II-22 TO 11-34 INDIVIDUAL ENGINE RUNS - CLIMB RICH MODE
II-35 MODEL SUMMARY - CLIMB RICH MODE
11-36 INDIVIDUAL RUN - MASS EMISSION CONVERSION ONLY
II-l
-------
Oittl 6/18/71
TEST ORGANIZATION:
ENGINE SUPPLIER: TFLEOYNE-CONTINENTAL
ENGINE 0*TA *
c»i ID NUMBER: 201 ENGINE TYPE AND MODEL: O-ZOO-A
RATED HORSEPCNER: 100.
ENGINE TOTAL TIME: -0. HRS
FUFL: «v CAS so/a? FUEL H/C RATIO: i.e«o
OPERATIONAL DATA ««**.««««««««««««..«««««.««»««««««««*«««««««
INLEI AIR TEMPERATUREi DEGREES F: START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: START 23.91 FINISH -0.00
INLET AIR HUMIDITY, GR N H2O/LR AIR: 73.00
RELATIVE HUMIDITY: -o.oo PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOW RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 9
COMMENTS:
1MIAL NUHBfKI
1U45TA
COLO START > 130 SEC
TAXI-IDLE LOW
TAXI-IDLF HIGH
RUN-UP
TAKE-OFF 100*
CLIMB-LI: AN
APPROACH
TAXI-IDLE
HOT START
TFST
MODE
1
2
3
4
6
9
10
11
13
POKER
SHAFT PERCENT
HP RATED
0.0
2.60
6.50
20.40
89.40
8S.60
30.00
7.20
0.0
0
2
6
20
B9
BH '
29
7
0
MEASURED
FUFL
FLOW
LP/HR
4.00
5.40
B.20
13. BO
53.00
51.00
23.00
9.00
4.00
AIK FLOW
LB/HR
27.00
45.00
72.00
153.00
558.00
558.00
216.00
72.00
27.00
CALCULATED
F/A
0.14815
0.12000
0.11389
0.09020
0.0949B
0.09140
0.10648
0.12500
0.14815
TEST
MI1DF
1
2
3
4
6
9
10
11
13
F XHAUST
GAS
TEMP
DEGREES *
-0.00
-0.00
-0.00
-0.00
-0.00
-O.on
-o.oo
-0.00
-0.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
-0.00
CJ
1 ORY I
PPMV
59000.00
62000.00
6-JOOO.OO
74000.00
102000.00
97500.00
54500.00
97500.00
97500.00
CO
2
IDRYI
PERCENT V
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
IhETI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-o.oo
NO
(ORYI
PPMV
40.00
25.00
30.00
35.00
59.00
59.00
25.00
25.00
35.00
NO
2
(CKYI
PPMV
-0.00
-C.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.on
NO
X
IDRYI
PPMV
-o.oo
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-o.oo
-C.OO
-0.00
-o.no
-o.oo
-o.oo
-o.oo
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-o.on
-0.00
-0.00
-O.OC
PARTICULATES
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-o.on
TFST
HOOF
10
11
13
MASS F.MI
CO
LB/IK
LB FUFL
3B2.KO
405.50
579.55
768.79
1012.19
1001 .IB
4B7.44
749. 14
632.60
MSS h.MI MASS EMI MASS EMI
HC N02 C02
LB/IK LI/IK Lt./lK
LB FUEL LB FUEL LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
-0.00
-3.00
-0.00
-0.00
-0.00
-0.00
-.1.00
-0.00
-0.00
-C.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
S EMI
NO
O/IK
1 FUEL
0.43
0.33
0.41
0.60
0.96
1.00
0.37
0.32
0.37
MASS EMI
NOX
LB/IK
LB FUFL
-0.00
-n.oo
-0.00
-11.00
-0.00
-o.on
-o.oo
-0.00
-0.00
Mass EMI
CO
Lrf/HM
1.53
2.6H
4.75
1C. 61
53.65
51.C-,
1 1.21
6.74
2.53
MASS E.MI
HC
LB/HK
-0.00
-0.00
-0.00
-0.00
-o.oo
-O.on
-C.OO
-0.00
-0.00
MASS mi MASS EMI rtASS EMI MASS FM1
ND2 C02 NO NOX
LB/HK L-J/HR LB/HR LB/HK
-U.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
-C.OO
-0.00
-0.00
-0.00
-C.OO
-0.00
0.00
0. 00
o.on
0.01
0.05
0.05
C.01
0.00
O.OP
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
M'JOF
LB/ IK HP-HI*
LB/IK HP-HP.
»*»*nnHSFPOWFR-H* DAilS NOT CALCULABLE****
2 1.079 -0.000
3 0.731 -0.000
4 0.520 -0.000
6 3.600 -0.000
9 0.575 -0.000
10 0.374 -0.000
11 C.936 -0.000
**»»»HOPS(:POKEP.-HR BASIS NOT CALCULABLE****
THC
LB/IK Itp-HK
-0.000
-0.000
-C.OOO
-C.OOO
-0.000
-0.000
-n.ooo
NO
LI/IK HP-H-)
0.001
0.001
0.000
0.001
0.001
0.000
0 .000
LI/IK HP-MR
-0.000
-c.ooo
-o.coo
-O.POO
-0.000
-0.000
-o.noo
NT
X
L9/1K HP-HH
0.001
0.001
0. TOO
0.001
O.OUI
0.000
o.oco
LTO CYCLF EMISSIONS
TFST
MODE
9
10
II
TIME IN rtF.ASU.1En
MODE FUFL FLU«
MIN. LB/HR
12.00
0.30
5.00
6.00
4. CO
6.20
53 .00
51.00
23.00
1.00
TOTAL FOR CYCLE
TOTAL FOB CYCLE/LB FUEL
FUEL
UStl)
L
-------
OtTEl 6/18/71
TEST ORGANIZATION! TELEDYNE-CONTINENTAL
ENGINE SUPPLIER: TELEOYNE-CONT1NENTAL
ENGINE DATA «»«««««««««»«»««««t««
CAL in NUMBER: 202 ENGINE TYPE AND MODEL: 0-200-A
RATED HORSEPOWER: 100.
ENGINE TOTAL TINE: -0. MRS
FUEL: AV GAS 80/87 FUEL H/C RATIO: 1.6*0
OPERATIONAL DATA «««....«
INLET AIR TEMPERATURE, DEGREES F: START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: START 28.92 FINISH -o.oo
INLET AIR HUMIDITY, CRN H20/LB AIR: 11.00
RELATIVE HUMIDITY: -o.oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER:
2I34STB
TF.ST POWER
MODF SHAFT
HP
COLO START > 130 SFC 1 0.0
TAXI-IDLE LOW 2 2.10
TAXI-IDLE HIGH 3 7.00
RUN-UP 4 20.10
TAKE-OFF 100' 6 89.60 '
CLIMB-HICH B H8.30
CLIMB-LFA.N 9 87.50
APPROACH 10 2R.OO
TAXI-IOLF 11 9.30
HOT START ' 13 o.o
TEST LXHAUSI EXHAUST CO CO
MllOt GAS GAS (ORYI 2
TF.MP PKFSSURF. I'PMV IORYI
PEGRFFS F I'SIA
1
2
)
4
«,
a
g
10
11
13
TEST
MIII)E
1
2
3
4
n
8
ARTICULATES
-0
-0
-0
-0
-0
-0
-0
-C
-0
-0
«SS F"l
.Nil
LO/hR
0.00
0.00
0.00
0.00
0.05
C.05
0.05
U.OI
0.00
0.00
.00
.00
.00
.00
.00
.00
.on
.00
.00
.00
MASS tMI
NUX
LB/HR
-0.00
-0.00
-O.CO
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
LB/IK HP-HK LH/IK HP-HK
CALCULABLE"*"
-0..100
-0.000
-0.000
-O.JOO
-0.000
-o.:ioo
-o.noo
-0.000
-c.oon
-c.ooo
-0.000
-0.000
-1.0OO
-c.ooc
-0.000
-o.oon
0.
0.
0.
0.
0.
0.
0.
o.
000
000
000
001
001
001
000
000
-0.000
-0.000
-0.000
-o.oon
-0.000
-o.ocn
-o.noo
-o.noo
0.000
0.000
0.000
-n.ooi
O. 001
0.001
0.000
0.000
CALCULABLE"'"*
F'JEL
'JSEO
L*S.
1.26
0.26
4. 15
'.30
0.1,1
8.640
cn
L»J/ |K
LB FUTL
681.86
957.53
9S1.29
454. -)8
416.32
Lid CYCLE
cn
LH/IK
HOURS
4295.69
49791 .52
49564.45
10464.45
4163.2)
EMISSIONS
cn
hMISSION
LRS.
O.H59
0.249
4.114
1.046
0.279
6. 54 1
0.751
HC
L ?/ 1 *
LS FUHL
-o.oo
-o.no
-0.0"
-o.oo
-C.OD
HC
LO/IK
HOURS
-0.00
-0.00
-n.no
-1.00
-0 . 00
HC
EM I SS ION
LHS.
-O.noo
-O.oon
-n .nno
-0.000
-0.000
-0.000
-0.000
Nil
LH/IK
i R CUEL
0.17
0.9-)
C.94
0. 15
0.25
Ml
l.rl/ IK
HCUKS
1 .10
51 .65
47. 13
8.11
2.4B
NO
EMISSION
LBS.
0.0002
C.0003
0.0039
O.OOOd
0.0002
0.0054
0.0006
II-3
-------
DATE!. 6/21/71
TEST ORGANUATIONI TELtOYNE-CONTINENTAL
ENGINE SUPPLIER I TELEOVNE-CONTINENTtl
ENGINE 0»T» *««««»»»»»»»»»»»«»»»»»«*
i
t»L ID NUMBER I 20) ENGINE TYPE AND MODEL I 0-200-A IERIAI NUMOU 2I1SOM
RATED HORSEPOMERI 100.
ENGINE TOTAL riHEl -0. MRS
FUEL I 4V G»S tO/87 FUEL H/C RATIOl 1.8*0
OPERATIONAL DATA *»»««««**»««»«
INLET AIR TEMPERATURE. DEGREES Fl START -D.OO FINISH -0.00 _
ATMOSPHERIC PRESSURE: START 28.91 FINISH -0.00
INLET AIR HUMIDITY, CRN H20/LB AIR: 69.00
RELATIVE HUHlOITYl -0.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLDK RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 9
COMMENTS:
COLO START » 130 SEC
TAXI-IDLE LOU
TAXI-IDLE HIGH
RUN-UP
TAKE-OFF lOOt
CLIMR-LFAN
APPROACH
TAXI-IDLE
HOT START
TEST
MODE
1
2
3
*
6
9
10
11
13
POKER
SHAFT PERCENT
HP RATED
0.0
2.80
8.00
20.30
91.30
91.10
29.30
7.40
0.0
0
2
7
20
91 .
91
29
7
0
MEASURED
FUEL
FLOW
LB/HR
3.90
4.60
8.20
15.50
53.00
51.00
22.00
7.50
3.50
AIR FLOW
LB/HR
27.00
40.50
76.50
157.50
576.00
567.00
207.00
67.50
22.50
CALCULATED
F/A
0.12963
0.11358
0.10719
0.09841
0.09201
0.08995
0.10628
0.11111
0.15556
TEST
MODE
1
2
3
4
6
9
10
II
13
EXHAUST
GAS
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
50000.00
64000.00
71500.00
87500.00
93000.00
87500.00
69000.00
54000.00
54000.00
CO
2
tORYl
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
[MET!
PPMV
V
25000.00
27500.00
17500.00
4000.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
I DRV I
PPMV
25.00
10.00
35.00
35.00
115.00
150.00
25.00
25.00
40.00
NO
2
I DOT I
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
NO
X
(DRVi
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
1
2
J
4
6
9
10
11
13
MASS EMI
CO
LB/IK
LB FUEL
371.66
540.20
654. R9
843.01
951.52
913.37
619.66
465.30
114.01
t«SS EMI
MC
LB/IK
LB FUEL
136.64
167.84
111.36
27.06
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FHI
N02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MASS EMI
C02
LB/IK
LB FUF.L
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NCI
LB/IK
LB FUEL
0.31
0.14
0.51
0.55
1.93
2.57
0.37
0.35
0.41
MASS EMI
NOX
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-C.OO
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
1.30
2. 48
5.37
13.07
50.43
46.58
13.61
3.49
1.17
MASS EMI
HC
LB/HR
0.49
0.77
0.91
0.42
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
N02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NO
LB/HR
0.00
0.00
0.00
0.01
0. 10
0.13
0.01
0.00
0.00
MASS EMI
NUX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TF.5T
MODE
10
11
CO
LB/IK HP-Hk
LB/IK HP-HR
R-Hu BASIS NOT CALCULABLE****
0.887 -0.000
0.671 -0.000
0.644 -0.000
0.552 -0.000
0.511 -0.000
0.465 -0.000
0.472 -0.000
MHRSEPOMER-HR BASIS NOT CALCULABLE****
THC
L8/1K HP-HR
0.276
0.114
0.021
-0.000
-0.000
-0.000
-0.000
NO
LB/IK HP-MR
0.000
0.001
0.000
0.001
0.001
o.ooo
0.000
Lfl/lK HP-HR
-0.000
-0.000
-0.000
-0.000
-O.oon
-0.000
-0.000
LB/IK HP-HR
0.000
0.001
0.000
o.ooi
0.001
0.000
0.000
LTD CYCLE EMISSIONS
TEST
MODE
10
II
TIME IN MEASURED
MODE FUEL FLOW
HIN. LB/HR
12.00
0.30
5.00
6.00
4.00
8.20
53.00
51.00
22.00
7.50
TOTAL FOR CTCLf
TOTAL FOR CYCLE/LA FUEL
FUEL
USED
LBS.
1.64
0.26
4.23
2.20
0.50
8.840
CO
LB/IK
LB FUEL
654.89
951.52
913.37
619.66
465.30
CO
LB/IK
HOURS
5370.07
50430.65
46581.89
13632.48
3489.76
CO
EMISSION
LRS.
1.074
0.252
3.866
1.363
0.234
6.790
0.768
HC
LB/IK
LB FUEL
111.36
-0.00
-o.oo
-0.00
-0.00
HC HC
LB/IK EMISSION
HOURS LBS.
913.12
-0.00
-0.00
-0.00
-0.00
0.183
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
NO
LB/IK
LB FUEL
0.51
1.93
2.57
0.17
0.35
NO
LB/IK
HOURS
4.20
102.43
131.17
8.11
2.65
NO
EMISSION
LBS.
0.0008
0.0005
0.0109
0.0008
0.0002
0.0132
0.0015
II-4
-------
DATE! 6/21/71
TEST ORGANIZATION! TELEDTNE-CONT INENTAL
ENGINE SUPPLIER: TELEDYNE-CONTINENTAL
ENGINE 0»T» »»«
C»L 10 NUMBER: 20* ENGINE TYPE AND MODEL: 0-200-*
(UTEO HOB Sf POKER I 100.
ENGINE TOTAL TIME: -0. MRS
FUFL: 4V GAS 80/67 FUEL H/C RATIC: 1.840
OPERATIONAL DATA ««.««««.«««.......»..................».».........»...........
INLET AIR TEMPERATUREt DEGREES f- START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: STAPT 28.91 FINISH -0.00
INLET AIP HUMIDITY, GRN H20/LB AIR: 65.00
RELATIVE HUMIDITY: -0.00 PERCENT
SAMPLE LINE: TEMPERATURE. CEGREFS C: -0.00, FLOU RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF IESTS: 10
COMMENTS:
SERIAL NUMBER:
21350*8
TEST POWER
MODE SHAFT
HP
COLD START » 130 SEC 1 0.0
TAXI-IDLE LOW 2 2.00
TAXI-IDLE HIGH 3 6. BO
PUN-UP 4 19.60
IAKF-OFF 100» 6 91.10
CLIMB-KICH 8 91.10
CLIMB-LF4N 9 90.30
APPROACH 10 28.80
TAXI-IDLE 11 7.00
HOT START 13 0.0
IEST FXHftUST FXHAUST CO CO
MODE GAS GAS IfJRYl 2
IEMP PRESSURE PPMV IDRYI
DEGREES F PSIA
1
t
3
4
6
8
9
10
11
13
TCST
MOOF
1
2
|
4
6
8
t
10
1 1
13
TFST
fdOF
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
MASS Ell MASS FMI
cn HC
LH/1K LB/1K
LR FltFl LP FUEL
612.95 -0.00
595. If, -0.00
455.08 -0.00
64.9? -O.DO
649.97 -0.00
649.97 -0.00
563.42 -0.00
147.60 -0.00
486. 10 -0.00
482.71 -C.OO
CO
L8/IK HP-HH
«*««Ha»SEP']*FH-HR BASIS NO!
2
J
4
6
H
9
10
11
l.2«0
0.509
0.044
0.178
0.378
0.318
0.571
0.451
HrmSFPHWEH-HP BASIS NUT
Tf.St
(lint
1
6
1
10
11
TOTAL TOH
TOTAL FOK
TIMF IN MEASURED
MUOF FUCL FLOU
MIN. LB/HH
12.00 7.60
O.JO 53.00
5.00 51.00
6.00 22.00
4 . 00 6 . 50
CVCIF
CYCLE/LI FUEL
82500.00
74000.00
53500.00
0000.00
64003.00
64000.00
54000.00
85010.00
49SOO.OO
79000.00
MASS EMI
NU2
H/1K
L» FUFL
-0.00
-0.00
-1.00
-0.00
-0.00
-d. 00
-O.CO
-O.CO
-o.oo
-0.00
cn
2
LP/K HP-HH
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-O.JO
-0.00
-0.00
MASS EMI
C02
LB/IK
LO FUEL
-0.00
-C.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PERCENT
RATED
0
1
6
19
91
91
90
28
6
0
THC
IKFTI
PPMV
V
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
Nil
LB/1K
LP FUEL
0.31
0.11
0.35
2.31
1.50
1 .50
2.23
C.29
0.4H
0.41
IHC
LB/1K HP-HO
MEASURED AIR FLOI, CALCULATED
FUEL Lfl/HR F/A
FLOW
LB/MR
3.50 27.00 0.12963
4.30 36.00 0.11944
7.60 67.50 0.11259
13.20 153.00 0.08627
53.00 571.50 0.09274
53.00 571.50 0.09274
51.00 567.00 0.08995
22.00 202.50 0.10864
6.50 67.50 0.09610
3.50 22.50 0.15556
NO NO Nn ALDEHYDES
IDRYI 2 X
PPMV (DRY) (DRY)
25.00
10.00
25.00
130.00
90.00
90.00
110.00
20.00
30.00
40.00
MASS FMI
NOX
LB/IK
LB FUEL
-0.00
-O.CO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
LB/ IK
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-C.OO
-0.00
MASS FM|
CD
LB/HH
2.15
2.56
3.46
0.86
34.45
34.45
23. '3
16.45
3.16
1.69
NO
HP-HP
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS FWI
HC
LB/HK
-0.00
-0.0"
-O.CO
-0.00
-0.00
-0.00
-0.00
-o.oc
-0.00
-0.00
NC
?
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
M«SS EMI
NU2
Lrt/HR
-0.00
-0.00
-0.00
-C.OO
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
SMOKE
-0.00
-o.oo
-3.00
-u.oo
-0.00
-0.00
-0.00
-o.ao
-0.00
-0.00
MASS EMI
C02
LR/HU
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-C.OO
-0.00
Ml)
X
PARTICULARS
-0
-0
-0
-0
-0
-0
-0
-0
-0
-0
MASS FMI
Nil
LB/HK
0.00
0.00
0.00
0.03
C.OB
0.08
0. 11
C.OI
P. 00
C.OO
.00
.00
.00
.00
.00
.00
.00
.00
.00
.CO
MASS EMI
NOX
LB/HH
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
LB/1K HP-HK L3/IK CP-HR
CALCULABLE****
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-o.ooo
-[1.000
-c.ooo
-0.000
-u.ooo
-o.ooo
-0.000
0.
0.
0.
0.
0.
0.
0.
0.
000
OOC
002
001
001
001
000
000
-0.100
-0.000
-0.000
-O.OPO
-0.000
-0.000
-0.000
-0.000
o.ooo
o.ooo
0.002
0.001
o.ooi
0.001
0.000
0.000
CALCULABLE****
FUEL
tisro
L.IS.
1.52
0. 26
4.21
2.20
0.44
8.653
cn
HI/ IK
18 FUFL
455.08
649.97
563.42
747.60
4H6.10
LTO CVCLT
cn
LB/IK
HOUKS
3451.64
344', H. 51
28734.33
1644'. 10
3159.63
EMISSIONS
Ctl
HC
EMISSION LB/1*.
LRS.
0.692
0.172
2.385
1 .645
0.212
5.105
0.590
L.I FUt-L
-0.00
-0.00
-0.00
-0.00
-0.00
HC
IB/IK
HOURS
-0.00
-0.00
-0.00
-0.00
-0.00
HC
EMISS1IIN
LBS.
-o.oco
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
NO
LB/IA
LO FUEL
0.35
1.50
2.23
0.29
0.48
Ml
Lb/IK
HUUPS
2.65
79.57
1 13.62
6.36
3.15
NO
FMISSIQN
LHS.
0.0005
0.0004
0.0094
0.0006
0.0002
0.0112
0.0013
II-5
-------
DATE!. 6/22/71
TCST OAGANIIATIONI TEL (DYNE-CONTINENTAL . '
EN6INE SUPPLIERI TELEOYNf-COMTlNENTAL ''
ENGINE DATA »«««««»«»»»»»«»«*«»
CAL ID NUNIERI 209 ENGINE TYPE (NO NOOELI O-JOO-A IHUl MMIftl illtM
RATED HORSEPOUERl 100.
ENGINE TOTAL TINEl -0. KRS
FUEL I AV GAS 80/8T FUEL H/C RATIO! 1.1*0
OPERATIONAL DATA »»««»«««»«««»»««»«»«»«»»
INLET AIR TEMPERATURE, DEGREES Fl START -0.00 FINISH -0.00 ^
ATMOSPHERIC PRESSURE! START 26.91 FINISH -0.00
INLET AIR HUMIDITY, CRN H20/LB AIR! 6*.00
RELATIVE HUMIDITY! -0.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES C: -0.00, FLO* RATE, LITERS/MINI -0.00
SAMPLE LINE TRANSPORT TIME, SECi -0.00
NUMBER OF TESTS: 9
COMMENTSi
COLD START 110 SEC
TAXI-IDLE LOU
TAXI-IOLF HIGH
RUN-UP
TAKE-OFF lOOt
CLIMB-LEAN
APPROACH
TAXI-IOLE
HOT START
TEST
MODE
1
2
3
4
ft
9
10
11
1)
POKER
SHAFT PERCENT
HP RATED
0.0
2.70
7.50
20.90
93.30
92.10
29.00
7.10
0.0
0
2
T
20
93
92
28
7
0
MEASURED
FUEL
FLO*
LB/HR
3.50
4.00
7.50
12.60
32.00
51.00
21.50
6.30
3.30
AIR FLOU
LB/HR
22.30
45.00
81.00
171.00
574.00
561.00
207.00
63.00
22.50
CALCULATED
F/A
0.15556
0.08889
0.09259
0.07368
0.09026
0.06995
0.10386
0.10000
0.15556
TESl
MODE
1
2
3
4
6
9
10
II
1]
EXHAUST
C«S
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-o.no
-o.on
-0.00
-0.00
-0.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
(DRY)
PPMV
10000.00
61500.00
59000.00
sooo.oo
88000.00
86000.00
53000.00
61500.00
74OOO.OO
CO
2
lour)
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THU
(NET)
PPMV
V
20000.00
4000.00
3100.00
500.00
1250.00
2250.00
1500.00
3000.00
25000.00
NO
IORYI
PPMV
42.00
42.00
70.00
445.00
225.00
2AO.OO
40.00
65.00
42.00
NO
2
IDRYI
PPMV
-a.oo
-a.oo
-o.oo
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
NO
X
i Dim
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
1
2
3
4
6
9
10
II
13
MASS EMI
cn
LB/IK
LA FUEL
61.84
648.52
600.17
61. M
915.42
897.50
486.04
503.86
457.61
MASS EMI
HC
LB/1K
LB FUEL
97.10
29.08
21.90
4.14
8.99
16.22
9.76
20.06
121.37
MASS EMI
ua 2
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.00
MASS T.MI
C02
LB/IK
L8 FUFL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
MO
LB/IK
LB FUEL
0.43
0.73
1.17
9.04
3.84
4.46
0.60
1.01
0.43
MASS EMI
NOX
LB/1K
LS FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
0.22
2.59
4.50
0.78
41.60
45.77
10.45
3.6U
1.60
MASS CM
HC
LB/HR
0.34
0.12
0.16
0.05
0.47
0.83
0.21
0.13
0.42
MASS EMI
K02
LB/HR
MASS EMI
CO 2
LB/HR
MASS EMI
NO
LB/HR
MASS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-o.oo
-o.oo
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
0.00
o.oo
0.01
0.11
0.20
0.23
o.oi
0.01
0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
co
LB/IK MP-HR
LB/1K HP-HR
****HORSEPOUER-HR BASIS NOT CALCULABLE****
2 0.961 -0.000
3 0.600 -0.000
4 0.037 -0.000
6 0.510 -0.000
9 0.497 -0.000
10 0.360 -0.000
II 0.518 -0.000
HURSEPOKER-MR BASIS NOT CALCULABLE****
THC
LB/IK HP-HR
0.043
0.022
0.002
0.005
0.009
0.007
0.018
NO
IB/IK HP-HR
0.001
0.001
o.oo;
o.oo;
0.002
0.000
0.001
L8/1K HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
IB/IK HP-HR
o.ooi
0.001
0.005
0.002
0.002
0.000
0.001
LTO CYCLE EMISSIONS
TEST
Mone
3
6
9
10
1 I
TIME IN MEASURED
MODE FUEL FLOW
MIN. LB/HR
12.00
0.30
5.00
6.00
4.00
7.50
52.00
51 .00
21.50
6.30
TOTAL FOR CYCLE
TOTAL FOR CYCLE/LB FUEL
FUEL
USED
LBS.
1.50
0.26
4.23
2.15
0.42
8.565
CO
LB/IK
LB FUEL
600.17
915.42
897.50
466.04
563.66
CO
LB/IK
HUURS
4501.27
47601.64
45772.69
10449.95
3678.31
CO
EMISSION
LBS.
0.900
0.238
3.799
1.045
0.246
6.229
0.727
HC
LB/IK
LB FUEL
21.90
B.99
16.22
9.76
20.06
HC
LB/IK
HUURS
164.23
467.43
827.34
209.91
126.40
HC
EMISSION
LBS.
0.033
0.002
0.06><
0.021
0.006
0.133
0.016
NO
LB/IK
LB FUEL
1.17
3.84
4.46
0.60
I. 01
NO
LB/IK
HOURS
8.77
199.91
227.30
12.95
6.39
NO
EMISSION
LBS.
0.0018
0.0010
0.0189
0.001)
0.0004
0.0233
0.0027
II-6
-------
OATEl 6/2J/71
TEST ORGANUATIONI TELEOYNE-CONTIHENTAL
ENGINE SUPPLIER! TEIEDYNE-CONTINENTAl
ENGINE DATA **>.»****
CAL 10 NUKBERl 206 ENGINE TYPE AND HDDELt 0-200-A
RATED HORSEPOWER: 100.
ENGINE TOTAL riNE: -0. MRS
FUEL: AV GAS 80/87 FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA »»«»»«««««««««.»»«
INLET AIR TENPERATUREi DEGREES F: START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: START 28.71 FINISH -0.00
INLET AIR HUMIDITY, CRN H20/LB AIR: 83.00
RELATIVE HUMIDITY: -0.00 PERCENT
SAMPLE LINE: IFMPFRATURE, DEGREES C: -0.00. FLOW RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TINE, SEC: -0.00
NUMBER OF TESTS: 9
COMMENTS:
SERIAL NUMBERI
2USOOA
cntn STARI » no SEC.
TAXI-IOLF LOW
TAXI-IDLE HIGH
RUN-UP
TAKE-OFf lOOt
CLIMB-LFiN
APPROACH
TAXI-IDLE
HOT START
TEST
MODE
2
3
4
6
9
10
II
13
POWER
SHAFT PERCENT
HP RATED
0.0
2.10
6.60
18.60
09.10
68.80
28.10
6.60
0.0
0
2
6
IB
89
88
78
6
0
MEASURED
FUEL
FLOW
LB/HR
3.50
4.00
10.50
15.70
51.50
51.00
21.50
11. SO
3.50
AIR FLOW
LB/HR
22.50
45.00
81.00
153.00
562.50
558.00
207.00
67.50
27.00
CALCULATED
F/A
0.15556
O.OBH89
0.12463
0.10261
0.09156
0.09140
0.10386
0.17481
0.12963
TEST
MOOE
1
2
1
4
6
9
10
11
11
tXHAUST
GAS
TFMP
nEGKEFS F
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
-0.00
-o.no
EXHAUST CO
GAS (DRY)
PRESSURE PPMV
PSIA
-0.00
-0.00
-o.on
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
35000.00
64000.00
97500.00
61500.00
82500.00
86000.00
52000.00
112000.00
54000.00
CO
2
1 CRYI
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
THC
IbETI
PPMV
V
32500.00
3500.00
7000.00
1550.00
2100.00
1750.00
900.00
750.00
35000.00
NO
(DRY)
PPMV
55.00
60.00
45.00
85.00
175.00
195.00
70.00
15.00
60.01)
NO
IDOY)
PPMV
-C.OO
-0.00
-0.00
-o.oo
-0.00
-o.oo
-0.30
-0.00
-C.OO
Nfl
X
(DRY)
PPMV
-0.00
-0.00
-o.oo
-o.oo
-o.oo
-o.oo
-0.00
-0.00
-0.00
ALDFHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-o.oo
-c.ro
-0.00
-0.00
-0.00
TFST
Mont
in
11
13
MISS EMI
CO
Lfl/IK
LH FI/FL
215.46
671.91
771.12
567. 77
843.90
881 .04
474. 76
609.52
199.50
HSSS EMI
HC
LB/IK
Lfl FUEL
I5T.7S
25.45
IB. 82
10. Id
14.95
12.48
5.86
3.34
194.09
MASS EMI
NCI2
LI/ IK
10 FUEL
-n.oo
-0.00
-o.on
-0.00
-o.oo
-o.on
-o.oo
-o.oo
-0.00
"A iS EMI
CQ2
LH/IK
L4 FUEL
-n.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NO
LH/1K
LB FUEL
0.56
1.03
0.55
1.29
2.94
3.28
1.05
0.31
0.73
MASS EMI
NOX
LB/IK
LH FUEL
-0.00
-0.00
-n.oo
-C.OO
-o.oo
-o.oo
-o.oo
-o.oo
-0.00
MASS EMI
CO
LH/H8
C.75
2.69
7.57
8.91
43. 4h
44.93
10.21
7.19
1.40
MASS E«
HC
LB/HO
0.55
0.10
0.41
0.16
0.77
0.64
0. 13
0.04
0.68
MASS FMI
NO?.
LB/HR
-0.00
-o.on
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
MASS fM
C02
LB/HR
-o.no
-0.00
-n.oo
-c.oo
-o.oo
-0.00
-0.00
-0.00
-n.n.)
MASS EMI MASS EMI
NO NOK
LB/HH Lfl/HR
n.oo
0.00
0.01
0.07
0. 11
0.17
0.0?
0.00
o.on
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
TFST
MUOI-
C"
LH/IK HP-HR
HnKSFPOUFR-HR BASIS NUI
2
1
4
<>
q
10
11
1.280
1.I4U
a. 4 79
0.488
0.506
0.161
1.090
CO
2
i HMX HP-HW
CALCULA«LC«
-0.000
-0.000
-0.000
-O.OOO
-0.000
-0.000
-0.000
IHC
LB/IK HP-HK
0.062
0.009
0.009
0.007
0.004
o.r>r>6
NO
LB/IK HP-HR
0.002
0.001
n.oo i
0.007
0.002
0.001
o.oni
LO/IK H"-HR
-o.ooo
-0.000
-o.ooo
-o.oon
-o.uuo
-0.0(10
-o.oon
NO
X
LH/IK HP-HR
0.00?
0.001
0.001
0.002
0.032
0.001
0.001
IPflwEH-HP OASIS NOT CALCULABLE»
LTD CYCLt EMISSIONS
TFSI
DOE
)
6
9
10
11
THIAL FOR
TOTAL FOR
TIME IN
MOOE
Ml\.
12.00
0.10
S.OO
6.00
4.00
CYCLE
CYCLt/LB
MFASURED
FUhL FLOW
LB/HO
10. 50
il.50
51.00
7.1.50
1 1 .80
FUEL
FUEL
USED
L1S.
2. 10
0.26
4.21
2. 15
0.79
9.511
cn
LB/IK
LH FUEL
721.12
843.90
fltH.O*
474.76
609.52
CO
LH/IK
HOURS
7571.91
41460.84
44933. IB
10207.40
7192.29
CO
FMISSIIIN
LRS.
1.515
0.217
3.729
1.021
0.4B2
6.9ft4
0.731
IIC
LB/IK
IH FUEL
3E.87
14.95
12.48
5.8!>
3. Ji
HC HC
LH/IK C-MISSIIIN
HOURS LHS.
40f.5 0.087
770.0
636. P
125.9
39.4
0.004
0.053
0.013
0.003
0.153
0.016
NO
Lfl/lK
Lrt FUEL
C.55
2.94
3.28
1.05
0.31
NO
LB/IK
HOURS
5.74
151.4)
167.35
?2.57
3.69
NO
EMISSION
i ns.
0.0011
o.oooe
0.0139
0.0073
0.0002
0.018)
0.0019
11-7
-------
DATEl 4/24/71
TEST ORCAM1IAT10NI TELIDYNE-CONTININTAL
ENGINE SUPPLIER! TEIEDYNE-CONTIMNTAl '
ENGINE DATA «»»*»»«»»*»«»»»»»»»»»«««»»»»»«»«»»«»»»»*»
CU ID NUNBEAI 207 EN6INE lift AND ROOEU 0-200-A SERIAL NUWHl 21IIOO«
RATED HORSEPOWER I 100.
ENGINE TOTAL TINEI -0. H«J
FUEll AV GAS 80/87 FUEL H/C RATIOI 1.8*0
OPERATIONAL DATA ««*»«»**»«»»»«»»«««««»»««
INLET AIR TEMPERATURE. DEGREES Fl START -0.00 FINISH -0.00
^
ATMOSPHERIC PRESSURE! START 28.66 FINISH -0.00
INLET AIR HUMIDITY, CRN H20/LB AIRI 91.00
RELATIVE HUNIOITYl -0.00 PERCENT
SAMPLE LINEl TEMPERATURE. DEGREES C: -0.00, FLO* RATE. LITERS/NIN: -0.00
SAMPLE LINE TRANSPORT TIME. SECi -0.00
NUMBER OF TESTS: 9
CONNENTSl
COLO START » 130 SEC
TAII-IOLE LOW
TAXI-IDLE HIGH
RUN-UP
TAKE-OFF 1001
CLIMB-LEAN
APPROACH
TAXI-IDLE
HOT START
TEST
MODE
1
2
3
4
6
9
10
11
13
POWER
SHAFT PERCENT
HP RATED
0.0
2.00
7.00
19.10
86.60
88.90
28.70
7.00
0.0
0
1
6
19
88
88
28
6
0
MEASURED
FUEL
FLOW
LB/HR
3.50
4.50
9.00
16.70
52.50
51.00
22.50
10.00
3.50
AIR FLOW
LB/HR
31.90
45.00
85.50
166.50
580.50
576.00
216.00
67.50
27.00
CALCULATED
F/A
0.11111
0.10000
0.10526
0.10030
0.090**
0.08654
0.10*17
0.14819
0.12963
TEST
MODE
2
3
*
6
9
10
II
13
EXHAUST
GAS
T6HP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
IORYI
PPNV
86000.00
7ROOO.OO
92500.00
6*000. no
86000.00
83000.00
52000.00
107000.00
52000.00
CO
2
IDRTj
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
(MET)
PPMV
V
25000.00
5000.00
8500.00
2200.00
2600.00
2000.00
2100.00
*000. 00
35000.00
NO
IORYI
PPNV
50.00
",5.00
50.00
65.00
150.00
180.00
55.00
42.00
55.00
NO
2
IORVI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
NODE
1
2
3
*
6
9
10
11
13
MISS EMI
CO
LR/IK
LB FUEL
736.19
735.66
8)2.65
602.1*
B87.63
872.76
*72.62
691.27
383.98
MASS EMI
HC
LB/IK
LB FUEL
155.02
31.4*
5*. 80
14.66
16.67
14.58
13.64
20.12
194.09
MASS EMI
N02
L«/IK
L8 FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS Efl
C02
LB/IK
IB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oc
-0.00
MISS EMI
NO
LB/IK
LB FUEL
0.70
0.70
0.74
1.00
2.5*
3.11
0.82
0.45
0.67
MASS EMI
NUX
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
2.58
3.31
7.49
10.06
46.60
44.51
10.63
6.91
1.34
MASS EMI
HC
LB/HR
0.54
0.15
0.49
0.25
0.98
0.74
0.31
0.20
0.68
MASS EMI
NO 2
LB/HK
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NO
LB/HR
0.00
0.00
0.01
0.02
0.13
0.16
0.02
0.00
0.00
MASS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
LB/IK HP-HP.
LB/IK HP-Hq
HORSEPQUER-HR BASIS NOT CALCULA8LF****
2 1.656 -0.000
3 1.071 -0.000
4 0.526 -0.000
6 0.526 -0.000
9 0.501 -0.000
10 0.371 -0.000
II 0.968 -0.000
HORSEPOHER-HR BASIS NOT CALCULABLE'
THC
LB/IK HP-HR
0.075
0.070
0.013
0.011
O.OOB
0.011
0.029
NU
LB/IK HP-HR
0.002
0.001
0.001
0.002
0.002
0.001
0.001
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-o.ooo
-o.ooo
-0.000
Nl)
X
LB/IK HP-HR
0.002
0.001
0.001
0.002
0.002
0.001
0.001
LTO CYCLE EMISSIONS
TEST
MODE
3
6
9
10
II
TIME IN MEASURED
MODE FUEL FLO*
MIN. LB/HR
12.00
0.30
5.00
6.00
4.00
9.00
52.50
51.00
22.50
10.00
TOTAL FOR CYCLE
TOTAL FOR CYCLE/LB FUEL
FUEL
USED
LBS.
1.80
0.26
4.23
2.25
0.67
9.215
CO
LB/IK
LB FUEL
832.65
697.63
872.76
472.62
691.27
CO
LB/IK
HOURS
7493.63
46600.59
44510.95
10633.89
6912.66
CO
EMISSION
LBS.
1.491
0.233
3.694
1.063
0.463
6.953
0,754
HC
LB/IK
LB FUEL
54.80
16.67
14.58
13.64
20.12
HC
LB/IK
HOURS
493.17
980.38
743.62
306.90
201.24
HC
EMISSION
LBS.
0.099
0.005
0.062
0.031
0.013
0.209
0.023
NO
LB/IK
LB FUEL
O.F4
2.54
1. II
0.82
0.45
NO
LB/IK
HOURS
6.65
133.51
156.56
18.47
4.46
NO
EMISSION
LBS.
0.0013
0.0007
0.0132
0.0018
0.0003
0.0173
0.0019
II-8
-------
0«TE1 6/24/71
TEST ORGANIZATION! TELEDYNE-CONTI MENTAL
ENGINE SUPPLIER! IELEDYNE-CONTINENTAL
ENGINE DATA **«.
CAL ID NUMBER: 208 ENGINE TYPE AND HODELI 0-200-*
RATED HORSEPOWER: too.
ENGINE TOTAL TIME: -0. MRS
FUEL: sv GAS so/a? FUEL H/C RATIO: i.a<,o
OPERATIONAL DATA «....«........«... ».«.,,.>,...*,...«.
INLET AIR TEMPERATURE, DEGREES F: START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: START 26.68 FINISH -0.00
INLET AIR HUMIDITY, CRN H20/LB AIR: 91.00
RELATIVE HUMIDITY: -0.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/M1N: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 9
COMMENTS:
SERIAL NUMBER I
21J500L
COLO START » 150 SF.C
T4XI-IDLF LOU
TAXI-IDLE HIGH
RUN-UP
TAKE-OFF lOOt
CLIMH-LE4N
APPROACH
TAXI-10LE
HOT STAR!
TEST
MODE
10
II
13
POWER
SHAFT PERCENT
HP RATED
0.0
2.10
6.60
19.60
89.00
88.50
28.50
6.60
0.0
0
2
6
19
MEASURED
FUEL
FLOW
LB/HR
3.50
4.00
9.00
13.30
52.30
51.00
22.50
10.50
3.60
AIR FLOW
LB/HR
27.00
40.50
76.50
144.00
562.50
562.50
211.50
72.00
27.00
CALCULATED
F/A
0.12963
0.09877
0. 11765
0.09236
0.09298
0.09067
0.10638
0.14583
0.13333
TEST
MODE
i
2
3
4
6
9
10
11
13
FXHAUST
GAS
TEMP
OEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
EXHAUST CO
r,AS (DRY)
PRESSURE PPMV
PSIA
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.03
76000.00
74000.00
97500.00
64000.00
86000.00
86000.00
52000.00
102000.00
54000.00
CO
2
ICHY)
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
IhFT)
PPMV
V
39000.00
5000.00
9000.00
2100.00
2800.00
2000.00
2000.00
9500.00
42000.00
NO
IORY)
PPMV
50.00
42.00
42.00
55.00
185.00
155.00
50.00
35.00
45.00
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
X
IOB VI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
TEST
HOOF
10
II
13
MASS EMI
CO
LB/IK
LB FUEL
561 .20
706.03
790. 75
648 .40
866. 16
d85.67
463.51
669.62
3H7.34
MASS EMI
HC
LB/IK
LB FUEL
216.77
33. 74
53.55
14.86
19. 72
14.34
12.80
4B.35
228.18
MASS CMI
Nil 7
La/iK
Lfl FUtL
-0.00
-0.00
-o.on
-o.oo
-o.oo
-0.00
-0.00
-n.oo
-o.oo
MASS EMI
C02
LH/IK
LI) FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NO
Lfl/lK
LR FUEL
0.61
0.66
0.56
C.92
3.06
7.62
0.73
0.38
0.53
M«SS Ell
NOX
LB/IK
L8 FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MASS EMI
CO
LE/HR
1.96
2.H2
7.17
8.67
45.30
45.17
10.43
7.03
1.40
MASS tMI
HC
LB/HR
0.76
0.13
0.43
0.20
1.C3
0.71
0.29
0.51
O.P2
MASS EMI
NO 2
LR/HR
-0.00
-C.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
C02
L3/MH
-0.00
-0.30
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
MASS EMI
Ml
LH/HR
C.OO
r.cc
0.31
C.OI
0. 16
o.u
0.02
o.oc
0.00
MASS EMI
NOX
ia/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
tFST
MIIDE
cn
LB/IK HP-HR
.HIJRSEPOWER-HR BASIS NOT
2
3
4
6
9
10
11
1.345
1.078
0.440
0.509
n.5io
0.366
1.065
CO
2
Lrt/K HP-HR
CALCULABLE***
-1.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
THC
LB/IK HP-HR
0.064
0.073
0.010
0.017
0.008
0.010
0.077
NO
LH/IK HP-HR
0.001
0.001
1.001
0.002
0.007
0.001
0.001
LS/1K HP-HR
-0.000
-o.noo
-o.coo
-0.000
-o.noo
-0.000
-0.000
MO
X
LB/IK HP-HR
0.001
0.001
0.001
0.002
0.002
o.oni
0.001
HftSIS NOI CALCULfl
LTD CYCLE EMISSIONS
lEsr
MCII1E
3
6
4
10
11
ItlTHL FUR
TOTAL FOP
TIME IN
MODE
MI N.
12.110
0.30
5.00
6.00
4.00
CYCLE
CYf.LE/LB
MEASURED
fUf.L FLUW
LB/HR
9.00
>2.30
51 .00
22.50
10.50
FUEL
FUfcL
USED
L»S.
1.80
0.26
4.23
2.25
0. 70
9.24K
CO
LI/IK
L" FUEL
79U.75
866.16
H85. 67
463.53
669.67
CO
LD/IK
HOURS
7116.79
45300.20
45169. nq
10429.46
7031.06
CO
EMISSION
LBS.
1.423
0.7? 1
3. 741
1.043
0.471
6.913
0.748
HC
LB/IK
LB FUtL
53. 55
19.77
14.34
12.80
46. 3*
HC
LB/IK.
HOURS
481.95
1031.39
731.29
2B7.90
507.6*
HC
EMISSION
LRS.
0.09(,
0.005
0.061
0.02S
0.034
0.225
0.024
NO
Lfl/lK
LB FUCL
C.56
3.06
2.62
0. M
0. in
N;)
L8/1H
HOURS
5.04
160.06
133.77
16.47
3.96
NO
EMISSION
LBS.
0.0010
0.0008
0.0111
0.0016
0.0003
0.0148
0.0016
II-9
-------
OATEI 6/25/71
TEST ORGANIZATION! TELEOYNE-CONTINENTAL
ENGINE SU>n I Ml TELEDYNE-CONTINENTAL
ENGINE DATA »»»»»«»«»*«»»..»....
CM. ID NUMBER! 204 ENGINE TYPE AND NOOEtl 0-20O-A
RATED HORSEPOMER! 100.
ENGINE TOTAL TINEl -0. MRS
FUEL I AV GAS SO/87 FUEL H/C RATIOi 1.8*0
OPERATIONAL DATA *******»*»«»*»»*****
INLET AIR TEMPERATUREi DEGREES Fl START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: START 28.63 FINISH -0.00
INLET AIR HUMIDITY, CRN H20/LB AIRl 87.00
RELATIVE HUMIDITY! -0.00 PERCENT
SAMPLE LINEl TEMPERATURE, DEGREES Cl -0.00, FLO* RATE, LITERS/MINI -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS' 1
COMMENTS!
SERIAL NuniRt
»11*7*
COLO START » 130 SEC
TAXI-IDLE LOU
TAXI-IDLE HIGH
RUN-UP
TAKE-OFF lOOt
CLIMB-LEAN
APPROACH
TAXI-IDLE
HOT START
TEST
MODE
9
10
11
1)
POWER
SHAFT PERCENT
HP RATED
0.0
2.60
T.50
19.50
91.00
91.50
29. 10
7.50
0.0
0
2
7
19
90
91
29
7
0
MEASURED
FUEL
FLOW
LB/HR
3.50
3.70
9.00
13.20
52.50
51.00
21.50
10.30
3.50
AIR FLdM
LB/HR
27.00
40.50
81.00
153.00
562.50
562.50
202.50
67.50
27.00
CALCULATED
F/A
0.12963
0.09136
0.1U1I
0.08627
0.09333
0.09067
0.10617
0.15259
0.12963
TEST
MODE
1
2
3
*
6
9
10
11
11
EXHAUST
CIS
TFMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
FXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
(DRY)
PPMV
76000.00
57000.00
74000.00
9000.00
92500.00
B6000.00
52000.00
74000.00
53000.00
CO
2
1CRYI
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
(UET)
PPMV
V
27500.00
7500.00
42CO.OO
900.00
1000.00
1800.00
1500.00
4000.00
40000.00
NO
IORVI
PPMV
40.00
35.00
55.00
325.00
140.00
170.00
55.00
55.00
80.00
NO
2
(ORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.oo
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
NODE
9
10
II
13
n«ss EMI
CO
LB/IK
LB FUEL
561.73
583.63
614.06
96.89
929.33
1)86. 49
464. Bl
464.24
191.74
MASS EMI
HC
IB/IK
LB FUF.L
152.50
53.48
26.04
6.68
7.02
12.91
9.61
19.69
221.82
MISS EMI
N02
LB/IK
LB FUEL
-0.00
-1.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
H«SS EMI
C02
LR/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-0.00
-0.00
-0.00
MASS EMI
N')
LB/1K
LB FUEL
0.49
0.59
0.77
5.75
2.31
2.88
0.81
0.57
C.97
MASS fMI
NOX
Lfl/lK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
1.97
2.16
5.71
1.28
48.79
45.21
9.99
4.78
1.37
MASS EMI
HC
LB/HR
0.53
0.20
0.21
0.09
0.37
0.66
0.21
0.20
0.7H
MISS EMI
NO 2
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NO
LB/HR
0.00
0.00
0.01
O.OU
0.12
0.15
0.02
0.01
0.00
MASS EM
NOX
L6/MR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
LB/1K MP-HR
LB/1K HP-HR
HORSEPOUER-HR BASIS NOT CALCULABLE****
2 0.811 -0.000
3 0.761 -0.000
4 0.066 -0.000
6 0.536 -0.000
9 0.49* -0.000
10 0.1*3 -0.000
II 0.638 -0.000
HORSEPOUFR-HR BASIS NOT CALCULABLE****
THC
LB/1K HP-HH
0.076
0.031
0.005
0.004
0.007
0.007
0.027
NO
LB/1K HP-HR
0.001
0.001
0.004
0.001
0.002
0.001
0.001
L8/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
NO
X
LB/IK HP-HR
0.001
0.001
0.004
0.001
0.002
0.001
0.001
LTD CYCLE EMISSIONS
TEST
HOOF
10
11
TIME IN MEASURED
MODE FUEL FLOU
MIN. LB/HR
12.00
0.30
5.00
6.00
4.00
TOTAL FOR CYCLE
9.00
52.50
51.00
21.50
10.30
FUEL
USED
LBS.
1.30
0.26
4.23
2.15
0.69
CO
L8/IK
LB FUEL
634.06
929.33
886.49
464.81
464.24
CO
LB/IK
HOURS
5706.56
48789.93
45210.91
9993.48
4781.61
CO HC
EMISSION LB/IK
LBS. L3 FUEL
1.141
0.244
J.753
0.999
0.320
6.457
26.04
7.02
12.91
9.61
19.69
HC
LB/IK
HOURS
234.19
368.76
656.16
206.62
202.B5
TOTAL FOR CYCLE/LB FUEL
HC
EMISSION
LBS.
0.047
0.002
0.055
0.021
0.014
0.118
0.015
NO
LB/IK
LB FUEL
0.77
2.31
2.88
0.81
0.57
NO
LB/IK
HOURS
6.97
121.29
146.BO
17.36
5.84
NO
EMISSION
LBS.
0.0014
0.0006
0.0122
0.0017
0.0004
0.0163
0.0018
11-10
-------
DUE! 6/25/71
TEST ORGANIZATION! TELEOYNE-CONTINENTAL
ENGINE SUPPLIER! TELEOYNE-CONtINENTtL
ENGINE DATA »»»»»
CAL 10 NUMBER: 21? ENGINE TYPE AND MODEL: O-»TO-R
RATED HORSEPOMERl 230.
ENGINE TOTAL TINE: -0. HRS
FUEL: AV GAS 80/87 FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA «.««««»
INLFT AIR TENPERATUREt DEGREES f: START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: START 29.05 FINISH -0.00
INLET AIR HUMIDITY, CRN H2Q/LS AIR: 84.00
RELATIVE HUMIDITY: -o.oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLON RATE, LITERS/NIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER:
211305
COLO START » 130
TAXI-IDLE LOV.
TAXI-IDLE HIGH
RUN-UP
I4KE-OFF I00«
CLIMB-RICH
CLIMB-LEAN
APPROACH
TAXl-IOLE
HOI START
TFST EXHAUST
MODE GAS
TEMP
1
2
3
4
b
a
9
in
1 1
13
usr
MUOC
OEGRFES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST POMFP
MODE SHAFT PERCENT
HP RATEO
SEC 1 0.0 0
.? 2.00 0
3 4.60 1
4 23.90 10
6 191. 1C 83
II 152.70 66
9 153.80 66
10 39.00 16
11 4.30 1
11 0.0 0
EXHAUST CO CO IHC
GAS IURYI 2 (WEI)
PRESSURE PPMV IORYI PPMV
F PSIA
-0.00
-0.00
-0.00
-0.00
-o.on
-o.oo
-o.oo
-o.oo
-o.oo
-0.00
MASS EMI MASS FMI
co
LB/IK
HC
LB/IK
LO FUEL LB FUEL
1
2
1
4
h
3
9
in
u
13
TCSt
MOOt
372.66
463. 11
767. 15
776.52
1145.91
626.54
602.12
6.12. 14
620.06
525.01
c
I.O/1K
233.52
258.31
775.93
28.51
22.93
9.06
7.75
17.87
779.34
219.09
HP-HR
HORSEPOWFR-HP HftSIS NOT
2
3
4
6
1
9
10
1 1
4.
3.
1.
0.
0.
0.
0.
2.
HORSOPONEfi-H
TEST
MUlIt
1
6
9
10
11
IIHE IN
MODE
M1N.
12.00
0.30
5.00
s. no
4.00
170
786
040
790
J61
339
551
581
° BASIS NOT
MFASUREO
FUCL FLOW
LB/HH
19. 70
133.00
06.50
14.00
17.90
PERCENT V
64000.00
69000.00
97500.00
98000.00
120000.00
57000.00
53000.00
61500.00
63000.00
99000.00
MASS EMI
ND7
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-o.on
-o.oo
-o.oo
-o.oo
CO
7
LB/IK HP-HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
C02
LB/IK
LO FUFL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-n.no
-o.on
-o.oo
50000.00
50000.00
47500.00
4500.00
3400.00
1200.00
1000.00
2500.00
50000.00
50000.00
MASS EMI
NO
LP/IK
LB FUEL
1.05
1.3B
1.29
1.30
1 .44
6.32
7.74
2.03
1.41
1 .39
IHC
LB/IK HP-HR
MEASURED AIR FLON CALCULATED
FUEL LB/HR F/A
FLOU
LB/HR
15.50 94.50 0.16402
18.00 126.00 0.14286
19.70 162.00 0.12160
32.00 297.00 0.10774
133.00 1345.50 0.09885
88.00 1044.00 0.08429
86.50 1066.50 0.08111
34.00 373.50 0.09103
17.90 139.50 0.12832
14.50 81.00 0.17901
NO NO NO ALOCHYOES
(DRYI 2 X
PPMV (OHY) (DRYI
PPMV
110.00 -0.00
125.00 -0.00
100.00 -0.00
90.00 -0.00
92.00 -0.00
350.00 -C.OO
415.00 -0.00
12C.OO -C.OO
115.00 -0.00
160.00 -G.OO
MASS FMI MASS [Ml
NOX CO
LB/IK LB/HP
L3 FUEL
-0.00 5.78
-0.00 8.14
-0.00 15.12
-C.OO 2'i.85
-0.00 152.41
-0.00 55.14
-C.OO 52. OS
-0.00 21.49
-0.00 11.10
-O.on 7.61
Nil
LB/IK HP-Hk
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS fMI
HC
LB/HR
3.62
4.65
5.44
0.91
3.05
0.80
0.67
O.M
5.00
3. IB
Mil
2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-o.oo
-o.oo
MASS EMI
NO?
Lfl/HR
-0.00
-o.no
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
C'I2
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
NO
X
PART1CULATES
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
MASS FMI
NO
LB/HR
0.02
n.o?
0.03
0.04
0.19
0.56
0.67
0.07
0.03
0.02
CO
00
00
00
00
00
00
00
00
00
MASS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
LB/IK HP-HR LB/IK HP-HR
CALCULABLE"**
-0.000
-0.000
-o.oon
-0.000
-n.oon
-n.ooo
-0.000
-0.000
CALCULABLE*
FU6L
USfO
L'IS.
3.94
0.66
7. 18
3.40
1.20
*
CO
LB/IK
Lrt FUEL
767.35
1145.91
602.12
632.14
62C.06
2.3?!>
1.1H2
o.oin
G.016
0.005
0.004
0.016
1. 163
LIO CYCLE
CO
LP/IK
HOURS
151 16.75
152405.68
52083.31
21492.89
11099.14
'1.012
0.006
0.002
0.001
0.004
0.004
0.002
0.006
[MISSIONS
CO MC
EMISSION L8/1K
LHS. L» FUFL
3.023 2/5.93
0.762 22.93
4.323 7.75
7. 149 17.87
0.74', 279.14
-0.000
-C.oon
-o.nun
-o.oon
-o.nno
-0.000
-O.DOO
-0.000
HC
LB/IK
IIUUFS
5455. 76
3049.29
670.51
607.69
5000.1 1
HC
EMISSION
LBS.
1 .087
0.015
O.ns6
0.061
0.335
n.oi2
0.006
0.007
o.nci
0.004
0.004
0.002
0.006
N!l
LB/IK
LU FUFL
1 .79
1.44
7.74
2.01
1.41
NO
LH/IK
HOURS
25.47
191 .92
669.87
68. SA
25.26
NO
EMISSION
LBS.
0.0051
0.0010
0.0556
0.0069
C.OOI7
IOIAL FOR CYCLE
TUTAL FOR CYCLE/LB FUEL
11.001
0.671
1.554
0.095
0.0702
0.0043
11-11
-------
own- 6/2e/7i
TEST OtfiANIlATIONI TCLEDYNt-COirTINnTAL
ENGINE SUPPLItRI TELEDYNt-CONTKrtNTAl
ENGINE 0»T» «»*»*»»****»
CAL 10 NUMBER! 21* ENGINE TYPE MO NDOELI 0-4TO-*
RATED HOUSEPOKERI 210.
ENGINE TOTAL riNEi -o. HIIS
FUEL I »V GAS 80/87 FUEL M/C RATIOl 1.840
OPERATIONAL DATA «*«»»»
INLET AIR TEMPERATURE, DEGREES Fl START -0.00 FINISH -0.00
ATMOSPHFRIC PRESSUREI START 2S.51 FINISH -0.00
INLET AIR HUMIDITY. CRN H20/LB AIRl 109.00
RELATIVE HUNIOITTl -0.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES C: -0.00. FLOM RATE. LITERS/MINI
SAMPLE LINE TRANSPORT TIME. SECl -0.00
NUMBER OF TESTS: 10
COMMENTS!
I**********************************
k
SERIAL NUMBERl lit Ml A
COLD START . 130 SEC
TAXI-IDLE LOW
TAXI-IDLE HIGH
RUN-UP
TAKE-OFF lOOt
CLIMB-RICH
CLIMB-LEAN
APPROACH
TAXI-IDLE
HOT START
TEST
MODE
1
2
3
4
6
a
9
10
n
11
POWER
SHAFT PERCENT
HP RATED
0.0
1.50
4.20
23.10
158.7C
155.30
156.80
52.60
4.00
0.0
0
0
1
10
68
67
68
22
1
0
MEASURED
.FUEL
FLOM
LB/HR
15.40
16.70
14.00
33.00
110.00
90.00
86.50
42.00
17.10
15.50
AIR FLOW
LB/HR
99.00
117.00
153.00
101.50
1123.00
1012.50
1035.00
495.00
119.50
101.50
CALCULATED
F/A
0.15556
0.14274
0.09150
O.I 0945
0.09826
0.08889
0.08357
0.08485
0.12258
0.14976
TEST
MODE
1
2
1
4
6
9
9
10
11
13
EXHAUST
GAS
TEMP
DEGREES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
EXHAUST
GAS
PRESSURE
PSI*
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CD
loon
PPHV
76500.00
78000.00
97500.00
110000.00
122000.00
61500.00
54000.00
51000.00
74000.00
59000.00
CO
2
IORYI
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
(NET)
PPMV
V
50000.00
50000.00
48000.00
5000.00
1000.00
1500.00
1100.00
1600.00
50000.00
50000.00
NO
I OR VI
PPMV
120.00
110.00
89.00
50.00
62.00
265.00
360.00
260.00
90.00
122.00
NO
2
I DRY I
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
X
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICIPATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TFST
MODE
1
2
3
4
6
8
9
10
11
11
MASS EMI
CO
LB/IK
L9 FUEL
468.01
521.10
991.86
950.98
1144.52
641.80
594.51
575.94
574.55
J75.17
MASS EMI
HC
LB/IK
LB FUEL
242.74
258.48
141.91
31.34
20.32
10.91
9.87
12.02
288.77
249.57
MASS EMI
urn
LB/IK
LB FUFL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MISS EMI
C02
LB/IK
L8 FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI MASS EMI
NO NOX CO
LB/IK LB/IK LB/hft
Lfl FUFL LB FUEL
MASS EMI
HC
L8/HR
MASS EMI
N02
LB/HR
HISS EMI
CO 2
LB/HR
MASS EM
NO
LB/HR
1.21
1.21
1.49
0.71
C.97
4.54
6.51
4.64
1.15
1.27
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
7.21
8.70
13.89
31.38
151.39
57.76
51.43
24.19
9.82
5.82
3.74
4.32
4.79
1.03
2.64
0.98
0.85
0.50
4.94
3.87
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
0.02
0.02
0.0?
0.02
0.13
0.41
0.56
0.19
0.02
0.02
MASS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
CO
L6/1K HP-HR
LB/IK HP-HH
HORSEPOWER-HR BASIS NOT CALCULABLE«»««
2 5.802 -0.000
3 1.306 -0.000
4 1.359 -0.000
6 0.954 -0.000
1 0.372 -0.000
9 0.128 -0.000
10 0.460 -0.000
II 2.456 -0.000
HORSFPQUER-HR BASIS NUT CALCULABLE**"
7HC
LB/IK HP-HR
2.878
1. 140
0.045
0.017
0.006
0.005
0.010
1.234
NO
LU/1K HP-HI)
0.011
0.005
0.001
0.001
0.003
0.004
0.004
0.005
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-o.ooo
-0.000
NO
X
LB/IK HP-HR
0.011
0.005
0.001
o.ooi
0.001
0.004
0.004
0.005
LTQ CYCLE EMISSIONS
TEST
MODF
3
6
9
10
11
TOTAL FOR
TOTAL FOR
I ME IN
NODE
KIN.
12.00
0.10
5.00
6.00
4.00
CYCLE
CYCLE/LB
MEASURED
FUEL FLOM
LB/HR
14.00
110.00
86.50
42.00
17.10
FUEL
FUFL
USED
LBS.
2.80
0.65
7.18
4.20
1.15
15.975
CO
LB/IK
L9 FUEL
991.86
1164.52
594.51
575.94
574.55
CO
LB/IK
HOURS
13886.05
151188.06
51425.15
24189.66
9824.86
CO
EMISSION
LBS.
2.777
0.757
4.268
2.419
0.658
10.880
0.681
HC
LB/IK
IB FUEL
141.91
20.32
9.87
12.02
288.77
HC
LB/IK
HOURS
1786.76
2641.04
851.65
504.78
4917.97
HC
EMISSION
LBS.
0.957
0.011
0.071
0.050
0.111
1.421
0.089
NO
LB/IK
LB FUEL
1.49
0.97
6.51
4.64
1.15
NO
LB/IK
HOURS
20.82
126.37
563.12
194.92
19.61
NO
EMISSION
LBS.
0.0042
0.0006
0.0467
0.0195
0.0013
0.0723
0.0045
11-12
-------
DATE: 6/28/71
TEST ORGANIZATION! TELEOYNE-CONTINENTAL
ENGINE SUPPLIER! TELEDYNE-CONTINENTAL
ENGINE DATA
CAL ID NUMBER: 219 ENGINE TTPE AND NQDEL: 0-470-R
RATED HORSEPOWER! 230.
ENGINE TOTAL TINE: -0. MRS
FUEL: AV GAS 90/87 FUEL H/C RATIO: 1.840
OPERATIONAL DATA »«««««»»»«««»««««
INLET AIR TEMPERATUREt DEGREES F: START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: START 28.5a FINISH -o.oo
INLET AIR HUMIDITY, CRN H20/LB AIR: 114.00
RELATIVE HUMIDITY: -O.CO PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITCRS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 11
COMMENTS:
SERIAL NUMBER: 470-R-21U028
TEST POWER
MODE SHAFT PERCENT
HP RATED
COLD START . 1)0 SEC 1 0.0 0
TAXI-IOLE LOW 2 1.60 0
TAXI-IDLE HIGH 3 4.00 |
RUN-UP 4 22.00 9
TAKE-OFF lOOt 6 186.30 80
TAKE-OFF TO CLIMB 7 I 52. SO 66
CLIMB-RICH 8 150.60 65
CLIMB-LEAN 9 154.00 66
APPROACH 10 17.00 16
TAXI-iniE 11 4.40 1
HOI START 13 0.0 0
TEST FXHAUST FXHAUST CO CC IHC
MODE GAS GAS IORYI 2 IUFTI
TFMP PRESSURE PPMV IOHY) PPMV
UEGKEFS F PSU
1
2
3
4
*»
7
8
9
10
11
U
TEST
MODE
,
2
3
4
6
7
3
9
10
11
It
TEST
POOF
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -C.OO
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-o.oo -o.oo
MASS'FMI M*SS EMI
en HC
LB/IK LB/lr.
LR FUEL I* FUEL
466.92 129.22
4V.lt> 126.04
549.69 66.50
624.77 16.20
1148.84 20.79
665.41 10.92
HHfl.11 H.25
585.01 9.90
715.57 13. 45
507.5* 37.94
418.09 17.21
CO
LB/IK HP-HR
HORSFPOWFt-HK BASIS NOT
2
)
4
6
7
q
9
10
11
2.4H7
1. 745
0.625
0.802
0.3')8
0.437
0.329
0.619
1.292
*****HOHSFPOWbR-HR BASIS NUT
TFST
MDIIF
3
6
9
10
11
TOTAL FOR
TOTAL FOR
TIMF IN MFASURFn
MODE FUEL FLOW
Mln. LB/HH
12.00 12.70
n.JO 130.00
5.00 S6.50
6.00 32.00
4.00 11.70
CYCUF
CYC.LE/LS FUEL
52000.00
52000.00
59000.00
59000.00
177000.00
64000.00
73000.00
5)000.00
71000.00
52000.00
52000.00
"JSS FM
W2
LI1/1K
LS FUEL
-3.00
-o.no
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
LB/IK HP-HR
MEASURED AIR FLOW CALCULATED
FUEL LB/HR F/A .
FLCW
LB/HR
8.50 81.00 0.10494
8.80 81.00 0.10864
12.70 126.00 0.10079
22.00 252.00 0.08730
130.00 1305.00 0.09962
91.00 1026.00 0.08869
74.00 999.00 0.07407
86.50 1039.50 0.08)21
32.00 346.50 0.09735
11.20 117.00 0.09573
8.50 72.00 0.11806
NO NO NO ALOEHYDFS
(PRYI 2 X
PPMV IDRY)
PERCENT V
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/IK
Lfl FUEL
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-o.oc
-0.00
-0.00
-0.00
-0.00
20000.00
20000.00
10000.00
2200.00
3100.00
1500.00
1000.00
1300.00
1900.00
5500.00
2900.00
MASS EMI
NO
LB/IK
LB FUEL
0. HH
0.64
0.61
1.57
0.93
3. 77
21.00
6.07
1 .32
0.77
0.53
THC
LH/1K HP-H'4
60.00
45.00
40.00
90.00
6C.OO
220.00
1050.00
330.00
80.00
48.00
40.00
MASS EMI
NOX
LB/IK
LI FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
LH/1K
PPMV
-C.OO
-0.00
-0.00
-0.00
-0.00
-O.on
-0.00
-o.oo
-0.00
-0.00 .
-0.00
MOSS EMI
CO
LO/HR
3.97
3.9H
6.98
13.74
149.35
60.8)
65.77
50.60
22.90
5.68
).55
NO
HP-HK
PPMV
-0.00
-0.00
-o.oo
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MASS FMI
HC
LB/HR
1.10
1. 1 1
0.84
0.36
2.70
0.99
0.61
n.Sft
0.43
0.47
0.15
NO
2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
N02
LB/HP
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
CO?
L3/HK
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
NO
X
BAHTICULATFS
-0
-0
-0
-0
-0
-0
-0
-0
-0
-0
-0
MASS EMI
Nfl
LH/HX
0.01
0.01
0.01
0.03
0.12
11.34
1.55
0.53
0.04
C.OI
0.00
.00
.00
.00
.00
.00
.00
.00
.00
.00
.00
.00
M4SS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
LH/1K HP-HR Lfl/IK HP-HR
f.ALCULAHLF»»««
-0.000
-0.000
-o.ooo
-0.000
-0.000
-0.000
-0.000
-0.101)
-o.ooo
0.69)
0.21 1
0.010
0.015
0.007
0.004
0.006
C.OI2
0.097
3.
a.
0.
0.
0.
0.
0.
0.
1.
004
002
002
001
00?
01C
013
001
002
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
0.004
0.002
0.002
o.oci
0.002
0.010
0.003
0.001
0.002
CALCULABLE"*'
FUEL
USED
L'IS.
2.54
0.65
7.18
3.20
0. 75
14.370
CO
Lil/lK
LB FUEL
549.69
1148.84
585.01
715.57
507.58
LTC CYCLE
cn
Lfl/ IK
HOURS
6961.07
149349.50
50603.19
22898.30
5684. 9C
EMISSIONS
CO
EMISSION
LBS.
1.396
0.747
4.200
2.290
0.3bl
9.014
0.679
HC
LR/1K
LO FUCu
66.50
20.79
9.90
1 J.45
37.94
HC
IB/ IK
HOIIMS
941.56
2702.54
R56.74
430.27
424.98
HC
EMISSION
LPS.
0.169
0.014
0.071
0.043
0.02H
0.325
0.023
NO
L*/IK
LO FUEL
O.M
0.9)
6.07
1. )2
C.77
NO
LB/IK
HGllrtS
7.77
120.65
525.37
42. JB
8.62
NU
EMISSION
LBS.
0.0016
0.0006
0.0436
0.0042
0.0006
0.0506
0.0035
11-13
-------
OtTCt. 6/21/Tl
TEST ORGANIIATKMl TELEOYNE-CDNTINENTtL
ENGINE SUPPLIER: TELEDYNE-CONTINENTAL
ENGINE 0»T» ***»*»««»*««**«**««»«**«**»****
* -
CAL ID NUMBEAI 210 ENGINE TYPE AND HOOELI IO-S20-P SERIAL WHIMS ' 151I50A
RATED HORSEPOHER: 900.
ENGINE TOTAL TINEl -0. MRS
FUEL I »V GAS 100/130 FUEL H/C RATIO! 1.840
OPERATION*!. DATA «««««««««»««««««.«««»««.«««««»«».»«««»««.
INLET AIR TEMPERATURE. DEGREES Ft START -0.00 FINISH -0.00 _,
ATMOSPHERIC PRESSURE: START 28.96 FINISH -0.00
INLET AIR HUMIDITY, CRN H20/LB AIRI 6).00
RELATIVE HUMIDITVl -0.00 PERCENT
SAMPLE LINEl TEMPERATURE, DEGREES C: -0.00, FLOW RATE. LITERS/MINI -0.00
SAMPLE LINE TRANSPORT TIME, SECl -0.00
NUMBER OF TESTS: 10
COMMENTS:
TEST POWER
MODF SHAFT PERCENT
HP RATED
COLD START « 130 SEC 1 0.0 0
TAXI-IDLE LOU 2 1.40 0
TAXI-IOLE HIGH 3 4.60 1
RUN-UP 4 ?4.00 7
TAKE-OFF 1001 6 263.70 87
CLIMB-RICH a 202.10 67
CLIMB-LEAN 9 202.90 67
APPROACH 10 35.40 11
TAKI-IOLE 11 4.60 1
HOT START 13 0.0 0
TEST EXHAUST EXHAUST CO CO THC
MODE GAS GAS IORV) 2 IWETI
TEMP PRESSURE PPMV I DRY I PPMV
OEGRFES F PSIA PERCENT V
I -0.00 -0.00 74000.00 -0.00 -0.00
2 -0.00 -0.00 69000.00 -0.00 -0.00
3 -0.00 -0.00 59000.00 -0.00 -0.00
4 -0.00 -0.00 54000.00 -0.00 -0.00
6 -0.00 -0.00 61500.00 -0.00 -0.00
8 -0.00 -0.00 61500.00 -0.00 -0.00
9 -0.00 -0.00 10000.00 -0.00 -0.00
10 -0.00 -0.00 81000.00 -0.00 -0.00
11 -0.00 -0.00 59000.00 -0.00 -0.00
13 -0.00 -0.00 81000.00 -0.00 -0.00
TFST MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI
MODE CO' HC N02 C02 NO
LB/IK LB/IK LB/1K IB/ IK LB/IK
L8 FUEL LB FUEL L8 FUEL LB FUEL LB FUEL
I 544.96 -0.00 -0.00 -0.00 0.57
2 516.70 -0.00 -0.00 -0.00 0.43
3 462.48 -0.00 -0.00 -0.00 0.32
4 440.84 -0.00 -0.00 -0.00 0.40
» 625.75 -0.00 -0.00 -0.00 7.69
» 625.75 -0.00 -0.00 -0.00 7.85
9 118.33 -0.00 -0.00 -0.00 -0.00
10 653.84 -0.00 -0.00 -0.00 -0.00
11 415.48 -0.00 -0.00 -0.00 0.35
11 602.04 -0.00 -0.00 -0.00 0.31
IEST CO CO THC
MOOF 2
LB/IK HP-HU LB/IK HP-HH LB/IK HP-HR
HORSePUWER-HR BASIS NOT CALCULABLE****
2 2.991 -0.000 -0.000
3 1.610 -0.000 -0.000
t, 0.661 -0.000 -0.000
6 0.344 -0.000 -0.000
8 0.341 -0.000 -0.000
9 0.054 -0.000 -0.000
10 0.831 -0.000 -0.000
11 1.447 -0.000 -0.000
HORSEPDNER-HR BASIS NOT CALCULABLE****
LTD CYCLE
TEST TIME IN MEASURED FUEL CO CO
MODE MODE FUEL FLOW USED LB/IK LB/IK
MIN. LB/HR LBS. LB FUEL HOURS
3 12.00 16.00 3.20 462.98 7407.62
6 0.30 145.00 0.72 625.75 90733.19
9 5.00 92.00 7.64 11B.33 10886.68
10 6.00 45.00 4.50 653.84 29422.80
11 4.00 16.00 1.07 415.98 6655.64
TOTAL FOR CYCLE 17.133
TOTAL FOR CYCLE/L8 FUEL
MEASURED AIR FLOW CALCULATED
FUEL LB/HR F/A
FLOW
LB/HR
10.60 81.00
11.00 85.50
16.00 130. SO
36.00 306.00
145.00 1566.00
110.00 1188.00
92.00 1183.50
45.00 378.00
16.00 117.00
10.50 81.00
NO NO NO
IORYI 2 X
PPMV (DRY) IORYI
PPMV PPMV
47.00 -0.00 -0.00
35.00 -0.00 -0.00
25.00 -C.OO -0.00
30.00 -0.00 -0.00
460.00 -0.00 -0.00
470.00 -0.00 -0.00
-0.00 -0.00 -0.00
-0.00 -0.00 -0.00
10.00 -0.00 -0.00
25.00 -0.00 -0.00
MASS EMI MASS EMI MASS EMI
NOX CO HC
LB/IK LB/HR LB/KR
LB FUEL
-0.00 5.78 -0.00
-0.00 5.68 -0.00
-0.00 7.41 -0.00
-0.00 15.87 -0.00
-0.00 90.73 -0.00
-0.00 60.83 -0.00
-0.00 10.89 -0.00
-0.00 29.42 -0.00
-0.00 6.66 -0.00
-0.00 6.32 -0.00
NO NO
i
LB/IK HP-HR LB/IK HP-
0.002 -0.000
0.001 -0.000
0.001 -0.000
0.004 -0.000
0.004 -0.000
-0.000 -0.000
-0.000 -0.000
o.ooi -o.ooo
(MISSIONS
CO HC HC
EMISSION LB/IK LB/U
LBS. Lt) FUEL HOURS
1.482 -0.00 -0.00
0.454 -0.00 -0.00
0.904 -0.00 -0.00
2.942 -0.00 -0.00
0.446 -0.00 -0.00
6.227
0.363
0.13086
0.12865
0.12261
0.11765
0.09259
0.09259
0.07774
O.I 1405
0.13675
0.12963
ALDEHYDES SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EM]
N02
LB/HR
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.ob
-0.00
-0.00
MASS EMI
C02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
X
PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
0.01 -0.00
0.00 -0.00
o.oi -o.oo
0.01 -0.00
1.11 -0.00
0.86 -0.00
-0.00 -0.00
-0.00 -0.00
0.01 -0.00
0.00 -0.00
HR IB/ IK HP-HR
HC
EMISSION
LBS.
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
0.002
o.ooi
0.001
0.004
0.004
-0.000
-o.ooo
0.001
NO
LB/IK
LB FUEL
0.32
7.69
-0.00
-0.00
0.35
NO NO
LB/IK EMISSION
HOURS LBS.
5.16 0.0010
1114.73 0.0056
-0.00 -0.0000
-0.00 -0.0000
5.56 0.0004
-0.0000
-0.0000
11-14
-------
D«TE: 6/21/71
TEST ORGANIZATION: TELEOYNE-CIW1 MENTAL
ENGINE SUPPLIER: TELEDYNE-CONTINENTAL
ENGINE DATA ««««»««««»»««««««
C»L ID NUMBER: 211 ENGINE TYPE AND MODEL: io-520-p
RATED HORSEPOWER: 300.
ENGINE TOTAL TIME: -0. MRS
FUEL: AV GAS 100/130 FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA ««««««««««««««*«
INLET AIR TEMPERATURE, DEGREES F: START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: START 28.96 FINISH -0.00
INLET AIR HUMIDITY, CRN H20/LB AIR: 63.00
RELATIVE HUMIDITY: -0.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLO* RATE, LITERS/M1N: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER!
159850B
TES1 POWER
MODE SHAFT
HP
COLD START t 130 SEC 1 0.0
TAXI-IOLE LOW 2 1.90
TAXI-IOLF HIGH 3 4.80
RUN-UP 4 2*. 20
TAKE-OFF 1001 6 264.20
CLIMB-RICH B 202.30
CLIMB-LEAN 9 203.10
APPROACH 10 35.80
TAXI-IDLE 11 4.50
HOT STAR! 13 0.0
1EST EXHAUST EXHAUST CO CO
MURE GAS GAS lOftrt 2
TEMP PRESSURE PPMV (DRY!
nEGRF.ES F PS1S
I
2
1
4
b
i
9
10
1 1
1 1
IFST
Mtinr-
i
2
3
4
6
A
9
10
11
13
TFSI
MODE
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-o.no -o.oo
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
MASS FMI MASS EMI
CIJ HC
LB/1K LH/1K
LR FUFL LR FUFL
553.09 -0.30
462.35 -G.OO
477.12 -0.10
419.36 -0.00
570.25 -0.00
599.51 -0.00
95.27 -0.00
'.59.29 -0.00
441.01 -0.00
579.79 -0.00
r.n
LB/IK HP-MR
»*«*»Hr)RSFf UHFH-HR BASIS NOT
t
3
4
1,
8
9
10
11
2.991
1.51 1
0.641
0.31 }
0.329
0.043
0.616
1.421
HDRSEPnuFR-HR BASIS NUT
TEST
HOOF
3
6
9
10
1 1
TOTAL FOR
TOTAL FOR
TIKE IN MEASURED
10DF FUEL FLOh
MIN. LB/HR
12.00 15.20
0.10 145.00
5.00 92.00
6.00 4B.OO
4.00 14.50
CYCLE
CYCLE/LB FUEL
76500.00
69000.00
62000.00
52000.00
54000.00
59000.00
8003. OC
62000.00
59000.00
78000.00
MASS EMI
MO?
LB/IK
LB FUFL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-1.00
-0.00
-0.00
en
?
LP/IK H(>-HR
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
C02
LB/1K
LB FUEL
-0.00
-0.00
-0.00
-C.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PERCENT
RATED
0
0
8
88
67
67
11
1
0
THC
IkFTI
PPMV
V
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS F.MI
NO
LR/IK
Lfl FUEL
0.65
0.39
0.53
0.62
7.11
6.84
-0.00
0.43
0.52
0.67
THC
LH/1K HP-HR
MEASURED AIK FLOW CALCULATED
FUEL LB/HR F/A
FLO*
LB/HR
10. BO 81.00 0.13333
12.30 85.50 0.14386
15.20 121.50 0.12510
37.00 310.50 0.11916
145.00 1633.50 0.08877
111.00 1197.00 0.09P73
92.00 1192.50 0.07715
48.00 369.00 0.13008
14.50 112.50 0.12889
10.50 81.00 0.12963
NO NO NO ALDEHYDES SMOKE
(DRYI 2 X
PPMV ICHYI IORYI
55.00
35.00
42.00
47.00
410.00
410.00
-0.00
35.00
42.00
55.00
MASS CMI
NOX
LB/IK
L3 FUEL
-0.00
-0.00
-0.00
-0.00
-0.0')
-0.00
-0.00
-0.00
-0.00
-0.00
LB/IK
PPPV
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-C.OO
MASS F.MI
Cll
Lfl/HR
5.97
5.69
7.25
15.52
02.69
66.55
8.76
22. C5
6.39
6.C9
VO
HP -MM
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS I-MI
HC
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-O.PO
-0.00
MASS FMI
Nil?
LB/HS
-0.00
-0.00
-0.00
-0.00
-o.oc
-o.oo
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FKI
CU2
LB/HR
-0.00
-C.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.03
-C.OO
NO
X
PARTICULATES
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
MASS rcl
NH
LB/HS
0.01
0.00
0.01
0.02
1.03
0.76
-0.00
C.02
0.01
0.01
00
00
00
CO
00
CO
00
00
CO
CO
MASS FMI
NQX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
Lrt/lK HP-HR LB/IK HP-HR
CALCULABLE'"*
-0.000
-0.000
-o.oon
-0.000
-0.000
-0.000
-0.000
-o.ooo
-0.000
-C.OOO
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
0.
0.
0.
0.
0.
-0.
0.
0.
002
002
001
004
004
000
001
002
-0.000
-0.000
-0.000
-o.oon
-0.000
-0.000
-0.000
-O.OIQ
0.002
0.002
0.001
1.004
0.004
-0.000
0.001
0.002
CALCULABLE****
FUFL
USED
L3S.
3.04
0.12
7.64
4.80
0.97
17. 172
CC
Irt/lK
LU FUEL
477.12
5J0.25
95.27
459.29
441 .03
LTI1 CYCLE
CO
LB/1K
HOUKS
7252.21
G2686.61
8764.89
22045.99
6394.95
EMISSIONS
CO
EMISSION
LBS.
1.450
0.413
0.727
2.205
0.47*
5.274
0.304
hC
LB/IK
Li3 FUF.L
-0.00
-0.00
-0.00
-0.00
-0.00
HC
LB/IK
HOURS
-0.00
-0.00
-0.00
-0.00
-0.00
HC.
FfMSSION
LBS.
-0.000
-o.ooo
-0.000
-0.000
-0.000
-0.000
-0.000
NO
LB/IK
LB FUFL
0.53
7.11
-0.00
0.43
0.52
NO
Lfl/lK
HOURS
8.C7
1031.21
-O.OO
20.44
7.4H
NO
EMISSION
LUS.
0.0016
0.0052
-C.OOOO
0.0020
0.0005
-0.0000
-0.0000
11-15
-------
01TCI. 4/22/71
TEST ORGANIZATION! TEL (DYNE-CONTINENTAL
ENGINf SUPPLIER! TfltDVM-CIMTINEIITM.
ENGINE DATA «»«»«»«*»«»*»»»»«»**««*»*»«»«»»«
« ' .
C»L 10 NUMBER! 112 ENGINE TYPE AND MODEL! 10-MO-P SERIAL KUMCRI lf««TU
RATED HORSEPOWER! 100.
ENGINE TOTAL TINEI -0. MRS
FUEL I AV GAS 100/110 FUEL H/C RAT10I l.t»0
OPERATIONAL OAT A »**»***»**»»»»*»*»»**«***»**«**»*»*********««
INLET All TEMPERATURE, DEGREES F: START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE! START 28.94 FINISH -0.00
INLET AIR HUMIDITY, GRN H20/LB AIRl 63.00 " .
RELATIVE HUNIDITYl -0.00 PERCENT ;
SAMPLE LINE) TEMPERATURE. DEGREES Ci -0.00. FLON RATE. LITERS/MINI -0.00
SANPLE LINE TRANSPORT TINE, SECl -0.00
NUMBER OF TESTS! 9
COMMENTS!
COLD START 130 SEC
TAXI-IDLE HIGH
RUN-UP
TAKE-OFF 100»
CLIMB-RICH
CLIMB-LEAN
APPROACH
TAXI-IDLE
HOT START
TEST
MODE
3
4
6
8
9
10
11
13
POWER
SHAFT PERCENT
HP RATED
0.0
4.60
23.60
261.40
200.00
204.80
37.30
4.20
0.0
0
1
7
B7
66
68
12
1
0
MEASURED
FUEL
FLOW
LB/HR
11.30
18.10
J9.00
154.00
123.00
92.00
46.00
14.60
8.10
AIR FLOW
LB/HR
81.00
144.00
315.00
1597.50
1192.50
1183.50
396.00
117.00
67.50
CALCULATED
F/A
0.14198
0.12569
0.1Z381
0.09640
0.10314
0.07774
0.11616
0.12479
0.12000
TEST
MODE
9
10
11
13
EXHAUST
GAS
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
EXHAUST
GAS
PRESSURF
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
en
IDRY)
PPMV
87500.00
52000.00
116000.00
87500.00
97500.00
9000.00
122000.00
54000.00
73500.00
CO
2
I DRV I
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
(MET)
PPMV
V
47500.00
42500.00
9000.00
2400.00
2400.00
1300.00
11000.00
37500.00
45000.00
NO
(DRY)
PPMV
145.00
177.00
129.00
205.00
175.00
2250.00
55.00
60.00
60.00
NO
2
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
9
10
11
u
MASS EM|
CO
LB/IK
LB FUEL
594.18
398.34
901.71
858. 84
900.07
106.50
1008.09
416.58
588.79
MASS FMI
HC
L9/IK
Lfl FUEL
246.51
241.02
51.60
16.48
15.70
10.38
66.05
213.79
261.93
MASS EMI
N02
L8/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
co2
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI MASS EMI
NO NOX CO
LB/IK LB/IK LB/HR
LB FUEL LB FUEL
1.62
2.23
1.60
3.31
2.65
43.73
0.75
0.76
0.79
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
6.83
7.21
35.17
132.26
110.71
9.80
46.37
6.08
4.77
MASS EMI
HC
LB/HK
MASS EMI
N02
LB/HK
MASS EMI
CU2
LB/HR
MASS EMI
NO
LB/HR
MASS EMI
NOX
LB/HR
2.83
4.36
2.01
2.54
1.93
0.95
3.04
3.12
2.14
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
0.02
0.04
0.06
0.51
0.33
4.02
0.03
0.01
0.01
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
CU
LB/IK HP-HR
LB/K HP-HR
HORSFPOuER-HR BASIS NOT CALCULABLE**"
3 1.567 -0.000
4 1.490 -0.000
6 0.506 -0.000
8 0.554 -0.000
9 0.04B -0.000
10 1.243 -0.000
11 1.448 -0.000
HORSEPOWER-HR BASIS NOT CALCULABLE****
THC
LB/IK HP-HR
0.448
0.085
0.010
0.010
0.005
0.081
0.743
NO
LB/IK HP-HR
0.009
0.003
0.002
0.002
0.020
0.001
0.003
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
0.009
0.003
0.002
0.002
0.020
0.001
0.003
LTD CYCLE EMISSIONS
TEST
MODE
10
11
TIME IN MEASURED
MODE FUEL FLOU
MIN. Lfl/HR
12.00
0.30
5.00
6.00
4.00
18.10
154.00
92.00
46.00
14.60
IOTAL FOR CYCLE
TOTAL FOR CVCLE/LB FUEL
FUEL
USED
LBS.
3.62
0.77
7.64
4.60
0.98
17.604
CO
LB/IK
Lfl FUFL
398.34
858.84
106.50
1008.09
416.58
CO
LB/IK
HOURS
7209. 811
132261.56
9798.02
46372.05
6082.04
CO
EMISSION
LBS.
1.442
0.661
0.813
4.637
0.407
7.961
0.452
HC
LB/IK
LB FUFL
241.02
16.48
10.38
66.05
213.79
HC
LB/1K
HOURS
4362.54
2537. 19
954.74
303U.48
3121.36
HC
EMISSION
LBS.
0.873
0.013
0.079
0.304
0.209
1.477
0.084
NO
LB/IK
LB FUEL
2.23
3.31
43.73
0.75
0.76
NO
LB/IK
HOURS
40.31
508.98
4023.45
34.34
11.10
NO
EMISSION
LBS.
O.C081
0.0025
0.3339
0.0034
0.0007
0.3487
0.0198
11-16
-------
DATE: 6/22/71
TEST ORGANIZATION! TELEDYNE-CONTINENTAL
ENGINE SUPPLIER) TELEOYNE-CONTINENTAL
ENGINE 0»T» ****»«»*»*»»**»*
CAL to NUMBER: 213 ENGINE TYPE AND MODEL: io-520-p
RATED HORSEPOWER: soo.
ENGINE TOTAL TIME: -0. HRS
FUEL: AV GAS 100/130 FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA ..............P[[[
INLET AIR TEMPERATURE, DECREES F: START -0.00 FINISH '0.00
ATMOSPHERIC PRESSURE: START 26.94 FINISH -0.00
INLFT AIR HUMIDITY, CRN H20/LB AIR: 63.00
RELATIVE HUMIDITY: -0.00 PERCENT
SAMPLE LINE: TEMPERATURE, OEGREES C: -0.00, FLON RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUMBER!
TEST POWER
MODE SHAFT PERCENT
HP RATED
COLD START DO SEC 1 0.0 0
TAXI-IDLE LOW ? 2.60 0
TAXI-IOLF HIGH 3 6.10 2
RUN-UP 4 26.60 6
TAKE-UFF 100% 6 262.80 87
CLIMB-RICH 8 206.20 66
CLIMB-LEAN 9 209.20 69
APPROACH 10 40.00 13
TAXI-IDLE 11 5.70 1
HOT START 13 0.0 0
TEST EXHAUST EXHAUST CO CO THC
M00[ GAS GAS IDRVI 2 IUETI
TEMP PRESSURE PPMV ( DRY } PPMV
DECREES F PSIA
1
2
3
4
6
8
9
10
II
13
TEST
MODE
i
2
>
4
6
a
4
10
1 1
19
TFSI
MOOE
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-o.oo -n.oo
-0.00 -0.00
-o.on -o.oo
MASS EMI MASS EMI
en HC
Lfl/K LB/IK
LB ruEL LB FUFL
72.89 283. "9
fi2fi.ll 277.27
446.04 238.66
956.61 56.59
849. 56 16.94
862.75 15.17
9K.53 9.60
917. 19 6.55
417.05 790.86
4BI.77 751.55
CO
LH/1K HP-HR
*«*«HURSFPOWER-HR BASIS NOT
2
3
4
D
8
9
10
11
2.537
1.25R
I. Ill
0.491
0.515
0.043
1. 147
1.027
HOHSFP'.JWFR-IO BASIS NOT
TF.SI
MODE
3
b
q
10
11
TOTAL FOR
TOTAL Fflrf
TIMF IN MEASURED
MOOE FUEL FLOW
M1N. LR/HR
12.00 17.20
0.10 152.00
5.00 92.00
6.00 46.00
4.00 14.20
CYCLE
CYCLE/LB FUFL
9500.00
84500.00
59000.00
117000.00
88000.00
92500.00
8330.00
122000.00
52000.00
74000.00
MASS EMI
NO 2
LI/IK
LB FUEL
-0.00
-0.00
-T.OO
-0.00
-0. 00
-1.00
-a. On
-0.00
-D.OO
-0.00
CO
2
LB/IK HP-MR
MEASURED AIR FLOW CALCULATED
FUEL LB/HR F/A
FLOW
LB/HR
9.60 76.50 0.12549
10.50 81.00 0.12963
17.20 135.00 0.12741
37.00 315.00 0.11746
152.00 1548.00 0.09H19
123.00 1706.00 0.10199
92.00 1188.00 0.07744
46.00 391.50 0.11750
14.20 117.00 0.12137
10.00 67.50 0.14815
NO NO NO ALDEHYDES
IDRYI 2 X
PPMV IORY) (DRY)
PERCENT V
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
.MASS EMI
C02
Lb/ln
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
50000.00
50000.00
42500.00
9500.00
2500.00
2100.00
1700.00
11CO.OO
50000.00
50000.00
PASS EMI
NCI
LB/1K
LB FUEL
3.72
1.37
1.06
0.91
3.41
2.91
55. OB
1. 17
1.30
1 . 1 B
THC
LB/1K HP-HK
295.00
112.00
85.00
6B.OO
215.00
190.00
2825.00
87.00
100.00
110.00
MASS CM]
NUX
LO/IK
Lfl FUFL
-0.00
-0.00
-0.00
-C.OO
-0.00
-0.00
-0.00
-C.OO
-0.00
-0.00
IB/ IK
PPMV
-C.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
C.70
6.60
7.67
35.39
129.13
1C6.12
9.06
45.87
5.B5
4.81
NC
hP-HR
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
.MASS Erl
HC
LB/HR
2.73
2.91
4.11
2.09
2.57
1.B7
0.88
0.30
4. 13
2.52
NU
2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MASS EMI
N02
LB/HR
-0.00
-0.00
-o.ro
-0.00
-o.no
-o.oo
-o.oo
-C.OO
-o.oo
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS tMI
CD?
LO/HH
-0.00
-o.no
-0.00
-0.00
-O.dO
-o.oo
-0.00
-C.OO
-C.OO
-0.00
Nil
X
PARTICUIATES
-0
-0
-0
-0
-0
-n
-0
-0
-0
-0
MASS EMI
NO
LB/HR
0.04
0.01
0.0?
C.03
0.52
0.36
5.07
0.05
0.0?
0.01
.00
.00
.00
.00
.00
.00
.00
.00
.00
.00
MASS EMI
NOX
L8/HR
-U.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
LR/1K HP-MR LR/1K HP-HR
CALCULABLE"**
-0.000
-0.000
-n.oon
-0.000
-0.000
-0.000
-n.ooo
-0.000
1.120
0.673
0.079
0.010
0.009
0.004
0.001!
0.725
0.
0.
0.
0.
0.
0.
0.
0.
006
003
001
002
002
024
001
003
-0.000
-0.000
-0.000
-0.000
-O.OCO
-0.000
-0.000
-0.000
n.006
0.003
0.001
O.OC2
0.002
0.024
0.001
O.OC1
CALCULABLE****
FUEL
USED
L1S.
3.44
0. 76
7.64
4. 60
0.95
17. 187
CO
LB/IK
LB FUFL
446.04
849. 56
98.53
997.19
412.05
LTC1 CYCLE
CO
Lfl/lK
HOURS
7671.91
129132.56
9064.78
45870.94
5B51. 16
EM1SSKINS
cn
EMISSION
LPS.
1.134
0.646
0.752
4.587
0.392
7.912
0.455
HC
H/IK
LB FUFL
23G.66
16.94
-------
tmti 6/n/Tt
TEST ORGANUATION: TELEOYNE-CONTINENTAL
ENGINE SUPPLIER: TELEDYHS-CONTINENTAL '
ENGINE DATA »»»»*»*****»»»*
I
CM. 10 NUMBER: Zl« ENGINE TYPE AND NODEll 10-SM-P SERIAL NUMBER: 1499I2A
RATED HORSEPOWER! 300.
ENGINE TOTAL TIME! -0. KRS
FUELl AV GAS 100/130 FUEL H/C RATIOl 1.840
OPERATIONAL DATA ««»««*»»»«**»«»»«*««««»*«»«»«»»«'
INLET AIR TEMPERATURE. DEGREES ft START -0.00 FINISH -0.00 _.
ATMOSPHERIC PRESSURE: START 28.60 FINISH -0.00
INLET AIR HUMIDITY, CRN WO/LB AIR: 95.00
RELATIVE HUMIDITY: -o.oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MINI -0.00
SAMPLE LINE TRANSPORT TINE, SEC: -0.00
NUMBER OF TESTS: 10
COMMENTS:
COLO START » 130 SEC
TAKI-IOLE LOU
TAXI-IDLE HIGH
RUN-UP
TAKE-OFF 1001
CLIMB-RICH
CLIMB-LEAN
APPROACH
TAXI-IDLE
HOT START
TEST
MODE
10
11
13
POKER
SHAFT PERCENT
HP RATED
0.0
2.30
5.40
25.40
259.BO
205.90
207.70
32.30
5.00
0.0
0
0
1
a
86
68
69
10
1
0
MEASURED
FUEL
FLOW
LB/HR
10.00
10.90
14.30
31.00
144.00
112.00
92.00
34.50
13.00
8.30
AIR FLON
LB/HR
81.00
99.00
130.90
238.00
1534.50
1206.00
11118.00
306.00
112.50
63.00
CALCULATED
F/A
0.12346
0.10606
0.10958
0.10764
0.09384
0.09287
0.07744
0.11275
0.11556
0.13175
TEST
MODE
9
10
11
EXHAUST
GAS
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
CO
(DRY I
PPMV
52000.00
90000.00
78000.00
54000.00
66500.00
57000.00
8000.00
81000.00
5)000.00
66500.00
CO
2
IDRY)
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
(WED
PPMV
V
20000.00
10000.00
3500.00
2900.00
2000.00
2000.00
1600.00
3600.00
7500.00
37500.00
NO
(DRV I
PPMV
100.00
150.00
110.00
140.00
310.00
420.00
2875.00
115.00
85.00
90.00
NO
2
I DRY I
PPMV
-0.00
-0.00
-0.00
-0.00
-C.OO
-0.00
-0.00
-0.00
-0.00
-0.00
NO
X
(DRV)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
TEST
MODF
1
2
3
4
6
8
9
10
11
13
MASS EMI
CO
LB/IK
LB FUEL
403.23
805.64
677.19
476.82
665.20
575.48
94.49
694.91
437.85
483.98
MASS EMI MASS FMI MASS EMI
HC N02 C02
LB/IK LB/IK LB/IK
LB FUEL LB FUEL LB FUEL
114.91
64.12
21.92
ia.40
13.99
14.10
12.81
22.09
45.21
205.52
-0.00
-0.00
-0.00
-0.00
-0.00
-a.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI MASS EMI
NO NOX CO
LB/IK LB/IK LB/HR
LB FUEL LB FUEL
1.27
2.21
1.57
2.03
5.09
6.97
55.78
1.60
1.15
l.Ofl
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
4.03
9.69
14.78
95.79
64.45
8.69
23.63
5.69
4.02
MASS tMI
HC
LB/HR
1.15
0.67
0.11
0.57
2.02
1.58
1.18
0.76
0.59
1.71
MASS EMI MASS EMI
N02 C02
LB/HR LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NO
Lfl/MR
0.01
0.02
0.02
0.06
0.73
0.78
5.13
0.06
0.01
0.01
MASS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
2
3
4
6
8
9
10
11
CO
LB/IK HP-HR
LB/IK HP-HR
ft-HR BASIS NOT CALCULABLE**"
3.678 -0.000
1.794 -0.000
0.5S2 -0.000
0.369 -0.000
0.313 -0.000
0.042 -0.000
0.732 -0.000
1.136 -0.000
HORSEPnuER-HR BASIS NOT CALCULABLE*
THC
LB/1K HP-HR
0.293
0.058
0.022
0.008
0.008
0.006
0.024
0.11B
NO
LB/IK HP-HR
0.010
0.004
0.002
0.003
0.004
0.025
0.002
0.003
LB/1K HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-o.noo
LB/1K HP-HR
0.010
0.004
0.002
0.003
0.004
0.025
0.002
0.003
LTD CYCLE EMISSIONS
TEST
MODE
10
11
TIME IN MEASURED FUEL
MODE FUEL FLC1K USED
MIN. L8/HR LBS.
12.00 14.30
0.30 144.00
5.00 92.00
6.00 34.50
4.00 13.00
TOTAL FOR CYCLE
TOTAL FOR CYCLE/LB FUEL
2.96
0. II
7.64
3.45
0.87
15.537
CO
LB/1K
LB FUEL
cn
LB/1K
HOUBS
CO
EMISSION
L8S.
677.39
665.20
94.49
684.91
437.85
9686.64
95788.94
8692.87
23629.47
5692.07
1.937
0.479
0.772
2.363
0.381
5.882
0.379
HC
LB/IK
L8 FUEL
21.92
13.99
12.81
22.09
45.21
HC
LB/U
HOURS
313.47
2015.16
1178.14
762.07
587.70
HC
EMISSION
LBS.
0.063
o.oio
0.098
0.076
0.039
0.286
0.018
NO
LB/IK
L8 FUEL
1.57
5.09
55.78
1.60
1.15
NO NO
LB/IK EMISSION
HOURS L8S.
22.44 0.0045
733.46 0.0037
5131.35 0.4259
55.10 0.0055
14.99 0.0010
0.4406
0.02B4
11-18
-------
DATEI 6/21/T1
TEST ORGANIZATION: TELEOVNE-CONTINENTU
ENGINE SUPPLIER! TELEOYNE-CONTINENTAl
ENGINE OAT A c»»»....»».»»»»..»...,.......»»..»«»..,.
CAL 10 NUMBER: 21 s ENGINE TYPE AND MODEL: IO-SZO-P
RATED HORSEPOHERt 300.
ENGINE TOTAL TINE: -0. MRS
FUEL: AV GAS 100/110 FUEL H/C RATIO: i.e»o
OPERATIONAL DATA «.«»«...«.«.....»..«.«»««....«».........«.«........«.....»..
INLET AIR TENPERATUREi DEGREES F: START -0.00 FINISH -0.00
ATNOSPHERIC PRESSURE: START 28.60 FINISH -0.00
INLET AIR HUMIDITY, CRN H20/L8 AIR: 85.00
RELATIVE HUMIDITY: -o.oo PERCENT
SAMPLE LINE: TEMPERATURE, CEGREES C: -0.00, FLOU RATE, LITERS/KIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF lESIS: 10
COMMENTS:
SERIAL NUMBER!
1599826
COLD START * 130 SEC
TAXI-IDLE LOU
TAXI-IDLE HIGH
RUN-UP
TAKF-OFF 1001
CLIMB-RICH
CLIMB-LEAN
APPROACH
MO-IDLE
HOT START
TEST
MODE
1
2
3
4
6
a
9
10
II
13
POWER
SHAFT PFRCfNT
HP RATED
0.0
1.80
4.80
23.50
263.00
207.10
209.50
19.00
5.00
0.0
0
0
1
7
87
69
69
12
1
0
MEASURED
FUEL
FLOU
LB/HR
6.10
10.30
13.40
30.50
146.00
112.00
92.00
37.00
12.80
7.50
AIR FLOH
LB/HR
63.00
ai.oo
121.50
279.00
1561.50
1224.00
1210.50
360.00
117.00
63.00
CALCULATED
F/A
0.12857
0.12716
0.11029
0.10932
0.09350
0.09150
0.07600
0.10278
0.10940
0.11905
TEST
MODE
2
3
4
6
3
9
in
11
13
EXHAUST
GAS
TEMP
DFGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
FXHAUST
GAS
PRESSURE
»SIA
-0.00
-o.oo
-0.00
-o.oo
-o.oo
-o.oo
-o.oo
-n.OO
-0.00
-0.00
cn
(nay i
PPMV
10000.00
54000.00
66500.00
66500.00
71500.00
57000.00
10000.00
83000.00
52000.00
66510.OU
CO
2
IORVI
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
IkETI
PPMV
V
35000.00
22500.00
7300.00
33000.00
2300.00
2000.00
1500.00
3800.00
7500.00
17500.00
NO
(DRY)
PPMV
165.00
208.00
70.00
10.00
295.00
400.00
2625.00
115.00
75.00
BC.OO
NO
2
(CRY)
PPMV
-0.00
-0.00
-0.00
-O.OP
-0.00
-o.oo
-0.10
-0.00
-c.oo
-0.00
IDRYI
PPMV
-0.00
-0.0')
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-3.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PAHTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
TKST
MUDE
B
9
in
II
13
MASS EMI
r.n
LB/IK
LB FUEL
74.54
406.90
574.05
578.79
7 1 7 . 54
5H3.08
119.98
764. 7H
452.27
514.01
MASS EMI
HC
LB/IK
LB FUEL
195.25
176.53
46.76
207.04
16.13
14.25
12. 16
24.92
47.03
221.22
IASS EMI
N32
LB/IK
LR FUEL
-0.00
-1.00
-0.00
-3.00
-0.00
-n.oo
-0.00
-0.00
-0.00
-o.oo
MASS EMI
C02
LB/U
LB FUEL
-0.00
-0.00
-c.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MASS EMI
Nf)
LB/IK
LB FUEL
2.02
2.57
0.99
1.29
4. 86
6.72
51.73
1. 74
1.07
1.06
MASS EMI
NDX
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.0(1
-0.00
-0.00
-0.00
-r.oo
-0.03
MASS FMI
CO
LB/H«
0.60
4.19
7.69
1 7.65
104.76
65.31
1 1.04
28.30
5. 79
4.01
MASS EMI
HC
LB/HR
1.58
1.30
0.63
0.31
2.36
1.60
1.12
0.92
0.60
1.66
MASS hMI
HC17
Lfl/HK
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EM
C02
Lfl/MK
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
0.02
0.03
0.01
0.04
0.71
0.75
4. 76
0.06
0.01
0.01
MASS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TFSI
MODE
CO
Ld/IK HP-MO
IB/IK HP-HR
««««Hn«SFPauC«-HR BASIS NOT CALCULABLE*'**
2 2.32H -0.000
J 1.603 -0.000
4 0.751 -0.000
6 0.398 -0.000
9 0.315 -0.000
9 0.053 -0.000
10 0.745 -0.000
II 1.15D -O.f)00
.....HORSEPOWER-HP BASIS NOT CALCUL4RLt««««
THC
LB/IK HP-HR
0.724
0. 131
0.269
O.C09
O.OOB
C.005
0.024
C.120
NO
LB/1H HP-HB
0.015
0.003
0.002
O.OOJ
0.004
0.023
0.002
0.003
Lfl/IK HP-HH
-0.000
-O.non
-o.noc
-o.ooo
-0.000
-0.000
-o.ooo
-0.000
NO
X
Lrt/lK HP-HH
0.015
0.003
0.002
0.001
0.00',
0.32J
0.002
0.301
LTH CYCLH EMISSIONS
TEST
MflOfc
9
10
11
TIMf IN MEASURED FUEL
MODE FUEL ELUW USED
MIN. LB/HR LOS.
12.00
0.30
5.00
6.00
4. 00
II . 40
146.00
92.00
37.00
12.BO
TOTAL FflR CYCLE
TOTAL FOR CYCIE/LB FUEL
2.6«
0. 73
7.64
1. '0
0.86
15.604
cn
Lt)/lK
LB FUEL
574.05
717.54
119.98
764.78
45?. 27
r.o
LB/IK
HOURS
7692.21
104761.31
11039.04
28296.92
57B9.10
CO
EMISSION
LBS.
I.53H
0.52'
0.916
2.830
0.1BH
6.196
0.397
HC
LB/IK
LB FUEL
46.76
16.13
12.16
24.92
47.01
HC
Lrt/lK
HIJUPS
626.52
2355.70
1118.87
922.05
601.91,
HC
EMISSION
L9S.
0.125
0.012
0.091
0.092
0.040
0. J62
0.023
NO
L3/IK
LB FUEL
C.9T
4. Ho
51.71
1.74
1.07
NO
LO/IK
HOURS
13.10
7 09 . 9 7
4759.28
64 .40
13.71
NO
FMISSICN
LOS.
0.0027
0.0035
0.3950
0.0064
0.0009
0.4086
0.0262
11-19
-------
04TI1 4/24/71
TEST ORGANUATIONI TELEDYNE-COKTINENTAL
ENGINE SUPPLIER! TELEDYNE-CONTINENTAL
ENGINE DATA «»»»»»»»»»»«*»
CAL 10 NUNBERI 216 ENGINE TYPE AND KOOEll 10-520-P SHUL NUWERI
RATED HORSEPOWER I 300.
ENGINE TOTAL TINEI -0. MRS
FUEL! AV GAS 100/130 FUEL H/C RATIOl 1.840
OPERATIONAL DATA »»«««.»«««««««««««
INLET AIR TENPERATUREi DEGREES ft START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE! START 26.76 FINISH -0.00
INLET AIR HUMIDITY. CRN M20/L9 AIRl 13.00
RELATIVE HUNIDITTI -0.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES Cl -0.00, FLOW RATE, LITERS/NIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTSl 10
COMMENTS:
!*!
Uttil
****»****
TEST
MODE
COLD START » 130 SEC
TAXI-IDLE LOU
TAXI-IDLE HIGH
RUN-UP
TAKE-OFF lOOt
CLIMB-RICH
CLIMB-LEAN
APPROACH
TAXI-IOLF
HOT START
10
11
13
POKER
SHAFT PERCENT
HP RATED
0.0
1.70
4.80
23.70
255.70
201.60
204.60
35.80
4.00
0.0
0
0
7
85
67
66
II
I
0
MEASURED
.FUEL
FLON
LB/MR
10.50
11.30
16.00
34.50
150.00
117.00
92.00
43.00
13.30
8.70
AIR FLOH
LB/HR
90.00
106.00
148.50
306.00
1534.50
1174.50
1161.00
387.00
126.00
63.00
CALCULATED
F/A
0.11667
0.10463
0.10774
0.11279
0.09775
0.09962
0.07924
0.11111
0.10556
0.13810
TEST
HOOF
10
II
13
EXHAUST
GAS
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
IORT)
PPMV
54000.00
67000.00
81000.00
76000.00
99000.00
76000.00
61500.00
116000.00
88000.00
9000.00
CO
2
(DRY)
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
(NET)
PPMV
V
42500.00
36500.00
23000.00
7500.00
2600.00
2400.00
1600.00
9500.00
42500.00
50000.00
NO
IORYI
PPMV
90.00
90.00
105.00
125.00
160.00
250.00
2100.00
80.00
108.00
116.00
NO
2
(DRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
X
(ORVI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MOUF
9
10
II
13
MASS FMI
cn
LB/IK
LB FUEL
442.29
607.60
714.92
642.93
955.17
720.93
712.77
994.17
791.59
62.54
MASS EMI
HC
LB/IK
LB FUEL
254.41
236.32
145.81
46.02
17.67
16.09
12.60
58.91
273.44
2*4.78
MASS EMI
N02
L9/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
CQ2
L6/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NO
LB/IK
LB FUEL
1.21
1.34
1.52
1.74
2.54
3.69
39.96
1.13
1.60
1.32
MASS EMI
NOX
LB/IK
LB FUEL
-0.00
-o.on
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EM
CO
LB/HR
4.64
6. 87
11.44
22.18
143.28
64.34
65.58
42.78
10.53
0.54
MASS EMI
HC
LB/HR
MASS EMI
NO 2
LB/HR
MASS EMI
C02
LB/HR
MASS EMI
NO
LB/HR
MASS EMI
NOX
LB/HR
2.67
2.67
2.33
1.59
2.65
1.88
1.16
2.53
3.64
2.30
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-o.oo
0.01
0.02
0.02
0.06
0.38
0.46
3.68
0.05
0.0?
0.01
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
NODE
cn
LB/IK HP-HR
LB/IK HP-HR
HORSEPOUER-HR OASIS NOT CALCULABLE»»»»
2 4.039 -0.000
3 2.363 -0.000
4 0.936 -0.000
6 0.560 -0.000
8 0.416 -0.000
9 0.320 -0.000
10 1.195 -0.000
11 2.632 -0.000
HORSFPOUER-HR BASIS NOT CALCULABLE""
THC
LB/IK HP-HK
1.571
G.486
0.067
C.010
0.009
0.006
0.071
0.909
NO
LB/IK HP-HR
0.009
0.005
0.003
0.001
0.002
0.016
0.001
0.005
LH/1K HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
Lfl/lK HP-HR
0.009
0.005
0.003
0.001
0.002
0.018
0.001
0.005
LTD CYCLE EMISSIONS
TEST
MODE
10
II
TIME IN MEASURED FUEL
MODE FUEL FLOW USED
MIN. LB/HR LBS.
12.00
0.30
5.00
6.00
4.00
16.00
150.00
92.00
43.00
13.30
TOTAL FOR CYCLE
TOTAL FOR CYCLE/LB FUEL
3.20
0.75
7.64
4.30
0.89
16.777
CO
LB/IK
LB FUEL
714.92
955.17
712.77
994.87
791.59
CO
LR/1K
HOURS
11438.64
143275.38
65575.13
42779.22
10528.16
CO
EMISSION
LBS.
2.268
0.716
5.443
4.276
0.705
13.430
0.801
HC
LB/IK
LB FUEL
145.81
17.67
12.60
58.91
273.44
HC
LB/IK
HOURS
2333.00
2650.84
1159.56
2533.01
3636.72
HC
EMISSION
LBS.
0.467
0.013
0.096
0.253
0.244
1.073
0.064
NO
LB/IK
LB FUEL
1.52
2.54
39.98
1.13
1.60
NO
LB/IK
HOURS
24.36
360.34
3677.93
48.46
21.22
NO
EMISSION
LBS.
0.0049
0.0019
0.3053
0.0048
0.0014
0.3183
0.0190
11-20
-------
O-200-A SUMMARY - CLIMB LEAN MODE
MODEL SUMMARY
SAMPLE NUMBED 5.
TEST
MODt
1
6
9
10
11
TOTAL FOR
TOTAL FOP
MEAN:
STD DEV:
MEAN:
STO OEV:
MEAN:
srn DEV:
MEAN:
sro OEV:
MEAN:
sro DEV:
CYCLE
CYCLE/LB
MEASURED
FUEL FLOW
LB/HR
9.00
1.06
52.16
0.42
51.00
0.0
21. 10
0.55
9.78
2.06
MEAN:
srn OEV:
FUEL
FUEL
USED
LBS.
1.80
0.21
0.26
0.00
4.23
0.01
2.19
0.05
0.66
0.14
I.U9
(1.154
CO CO CO
LB/LK LB/1K EMISSION
LB FUEL HOURS LBS.
715.79 6478.47
99.19 1136.37
888.49 46350.61
34.94 2063.94
884.69 45119.34
9.10 459.29
472.35 10342.64
9.06 246.97
601.70 5919.19
B9.29 1593.71
MEAN:
sro nev:
O-470-R SUMMARY
MODEL SUMMARY
FESI
MODE
3
6
9
10
II
inlAL FOR
TOTAL FOR
HFAN:
sro DEV:
MEAN:
srn HEV:
MCAN:
srn OEV:
MEAN:
sro OEV:
MFAN:
srn DF.V:
CYCLF
CYCLF./LB
SAMPLE
MEASURED
FUEL FLDW
LO/HR
15.47
1.7?
131 .00
1.74
86.50
0.04
16.00
5.29
15.40
3.66
MCAN:
srn ncv:
FUEL
NUMBER
FUEL
IJSEU
LBS.
3.09
0.74
0.65
0.01
7.18
0.01
3.60
0.53
1.03
0.25
15.560
1 .093
j.
1.296
0.267
0.232
0.010
3.745
0.038
1.034
0.025
0.397
0.107
6.703
0.3)9
0.733
0.019
HC
LB/1K
LB FUEL
39.02
15.18
13.67
5.68
14.10
1.49
10.33
3.oa
22.31
16.23
HC
LB/IK
HOURS
356.26
149.08
723.60
297.64
719.33
75.90
227.46
72.48
215.52
176.52
HC
EMISSION
LBS.
0.0713
0.0298
0.0036
0.0015
0.0597
0.0063
0.0227
0.0072
0.0144
0.0118
0.172
0.043
0.019
0.004
NO
LB/IK
Lfl FUEL
0.76
0.25
2.94
0.59
3.27
0.71
0.80
0.16
0.54
0.29
NO
LB/IK
HOURS
6.63
1.42
153.24
30.16
166.74
36.14
17.57
3.48
4.H7
1.18
NO
EMISSION
LBS.
0.001)
0.0003
0.0008
0.0002
0.0138
0.0030
C.OOI8
0.000)
0.0003
0.0001
0.0180
0.0032
0.0020
0.0004
- CLIMB LEAN MODE
r.o co co
LI/ IK LR/IK EMISSION
LB FUEL HOURS LBS.
769.63 11994.62
221.09 43H5.25
1153.09 151047.81
9.97 1555.87
593.68 51370.54
H.57 742.23
641.22 22860.27
70.25 1349.11
567.40 8869.63
56.56 2830.70
"FAN:
sro OEV:
2.399
0.877
0.755
0.008
4.264
0.062
2.266
0.135
0.594
0.190
10.298
1.114
0.661
0.027
HC
LB/IK
LB FUEL
27fl.ll
143.80
21.34
1. 19
9.17
1.2)
14.45
3.05
202.02
142.17
MC
LB/IK
HOURS
3689.03
2484.66
2797.62
220.1)
791.47
106.49
514.24
89.09
3454. )5
7.623.70
HC
EMISSION
LBS.
0.7378
0.4969
0.0140
0.0011
0.0659
0.0086
0.0514
0.00(19
0.7)14
0.1758
1.101
0.675
0.069
0.040
NO
LB/IK
LB FUEL
1.1)
0.46
1.11
0.29
6.78
0.87
2.66
1.75
1.11
0.32
NO
LB/ U
HOURS
IH.02
9.17
140.31
19.60
5B6.I2
74 .95
102.00
81.50
I'.H4
6 .46
NO
FMISSION
LBS.
0.00)6
0.0018
0.0007
0.0002
0.0466
0.0062
0.0102
0.0082
0.0012
0.0006
0.0644
O.C120
0.0041
0.0005
IO-520-P SUMMARY - CLIMB LEAN MODE
MODEL SUMMA
2426.70
754.34
IOSJ.99
I3I.85
I5II.39
H98.B3
2415.59
1699. 9e
HC
EMISSION
L BS.
0.4696
0. 3775
0.0121
0.0013
0.0679
0.0109
0. 1511
0.1199
0. 1618
0. 1139
0.61)1
0.531
0.052
0.029
N)
LO/IK
LH FUEL
1.47
0.50
1.84
1.09
49.26
7.06
l.2d
0.40
1.13
0.11
NO
11/lK
HOURS
23.71
10.21
570.19
148.90
4531.96
64
-------
I
MTU t/ll/TI
TEST ORGANIZATION! TELEOYNE-CONTINENTAL
ENGINE SUPPLIER! TELEOYNf-CONTINENTAL
ENGINE DATA ***»*»»**«*»«***»»»********»»»*»»
i
Ctl ID NUMBER! 202 ENGINE TYPE AND NODELI 0-200-A SERIAL MUNICH 2IS«»TI
RATED HORSEPOKERl 100.
ENGINE TOTAL TINEl -0. MRS
FUEL I AV GAS 80/8T FUEL H/C RATIOl 1.840
OPERATIONAL DATA *»»*»»»»»«*«««*«»*«**«»»*««*«»
INLET AIR TENPERATUREf DEGREES FI START -0.00 FINISH -0.00 ,.
ATMOSPHERIC PRESSURE! START 28.92 FINISH -0.00
INLET AIR HUMIOirr, GUN H20/L8 AIR! T9.00
RELATIVE HUMIDITY! -0.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES Ct -0.00, FLOH RATE, LITERS/MINI -0.00
SAMPLE LINE TRANSPORT TIME, SEC I -0.00
NUMBER OF TESTS! 10
COMMENTS!
COLO START t 130 SEC
Till-IDLE LOW
TAXI-IOLE HIGH
RUN-UP
TAKE-OFF lOOt
CLIMB-RICH
CLIMB-LEAN
APPROACH
TAXI-IDLE
HOT START
TEST
MODE
1
2
3
4
6
a
9
10
11
13
POKER
SHAFT PERCENT
HP RATED
0.0
2.10
T.OO
20.10
89.60
88.30
87.50
28.00
9.30
0.0
0
2
6
20
89
88
87
27
9
0
MEASURED
FUEL
FLOM
LB/HR
4.00
5.30
6.30
15.00
52.00
50.00
50.00
23.00
10.00
4.00
AIK FLOH
LB/HR
27.00
45.00
72.00
162.00
558.00
558.00
558.00
207.00
63.00
18.00
CALCULATED
F/A
0.14815
0.11778
0.08750
0.09259
0.09319
0.08961
0.08961
0.11111
0.15873
0.22222
TEST
KOOE
9
10
11
13
EXHAUST
GAS
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
I DRV I
PPHV
54000.00
54000.00
64000.00
78000.00
95000.00
95000.00
95000.00
53000.00
69000.00
54000.00
CO
2
I DRY I
PERCENT V
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
IMETI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
I DRV I
PPMV
25.00
10.00
10.00
20.00
60.00
55.00
55.00
25.00
25.00
40.00
NO
2
IDRVI
PPHV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
X
I DRV I
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
1
2
3
4
6
B
9
10
11
13
MASS EMI
CO
LB/IK
LB FUEL
349.86
438.72
681.86
790.68
957.53
991.29
991.29
454.98
416.32
224.91
MASS EH1
HC
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
HISS EHI
N02
IB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-o.oo
-0.00
HASS EMI
C02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
NO
LB/IK
LB FUEL
0.27
0.13
0.17
0.33
0.99
0.94
0.94
0.35
0.25
0.27
MASS EHI
NOX
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
1.40
2.33
4.30
1I.B&
49.79
49.56
49.56
10. 4(,
4.16
0.90
MASS EMI
HC
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EHI
N02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EHI
C02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EHI
NO
LB/KR
0.00
0.00
0.00
0.00
0.05
0.05
0.05
0.01
0.00
0.00
MASS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MOOE
LR/1K HP-HR
LB/IK HP-HR
THC
LB/IK HP-HR
NO
LB/IK HP-HR
LB/IK HP-HR
LB/IK HP-HR
HDRSEPOMER-HR BASIS NOT CALCULABl£
2 1.117 -0.000 -0.000
3 0.614 -0.000 -0.000
4 0.590 -0.300 -0.000
6 0.556 -0.000 -0.000
a 0.561 -0.000 -0.000
9 0.566 -0.000 -0.000
10 0.374 -0.000 -0.000
11 0.448 -0.000 -0.000
HORSEPOUER-HR BASIS NOT CALCULABLE****
0.000
0.000
0.000
0.001
0.001
0.001
0.000
0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
o.ooo
0.000
0.000
0.001
0.001
0.001
0.000
0.000
LTO CYCLE EMISSIONS
TEST
MODE
10
11
MMF IN MEASURED
MC10E FUEL FLOH
UN. LB/HR
12.00
0.30
5.00
6.00
4.00
6.30
52.00
50.00
23.00
10.00
TOTAL FOR CVCLE
TOTAL FOR CYCLE/Lrt FUEL
FUEL
USED
LBS.
1.26
0.26
4.15
2.30
0.67
CO
LB/IK
LB FUEL
CO
LB/IK
HOURS
CO
EMISSION
LBS.
681.86
957.53
991.29
454.98
416.32
4295.69
49791.52
49564.45
10464.45
4163.23
0.859
0.249
4.114
1.046
0.279
6.547
0.758
HC
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
HC
LB/IK
HOURS
-0.00
-0.00
-0.00
-0.00
-0.00
HC
EMISSION
LBS.
-0.000
-0.000
-0.000
-0.000
-0.000
-o.ooo
-0.000
NO
LB/IK
LB FUEL
o.i r
0.99
0.94
0.35
0.25
NO NO
LB/IK EMISSION
HOURS LBS.
I.10
51.65
47.13
a.ii
2.48
0.0002
0.0003
0.0039
0.0008
0.0002
0.0054
0.0006
11-22
-------
0«IEt 6/21/71
TEST ORGANIZATION! TF.LEDYNE-CONT 1NEHTM.
ENGINE SUPPLIER: TELEDYNE-CONTINENTAL
ENGINE 0»T» ».«..«..
CAL to NUMBED: 20* ENGINE TYPE AND MODEL: 0-200-4
RATED MORSEPOMERl 100.
ENGINE TOTAL TIKE: -0. MRS
FUEL: IV GAS 80/87 FUEL H/C RATIO: 1.840
OPERATIONAL DATA »«««««««««»«»»»««««
INLET AIR TEMPERATURE, DEGREES F: START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: START 28.11 FINISH -o.oo
INLET AIR HUMIDITY, CRN H20/LB AIR: 65.00
RELATIVE HUHIDITr: -0.00 PERCENT
SAMPLE LINE: TEMPERATURE. CEGRECS C: -0.00. FLOW RATE, LITEHS/M1N: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER flF TESTS: 10
COMMENTS:
SERIAL NUMBER!
COLD START « HO S6C
TAXI-IDLE LCU
TAKI-IOLE HIGH
RUN-UP
FAKE-OFF lOOt
CLIMB-RICH
CLIMB-LEAN
APPROACH
TAXI-IDLE
HOT START
TEST
MODI;
9
10
u
13
POWER
SHAFT PERCENT
HP RATED
0.0
2.00
6.80
19.60
91 .10
91. 10
90.10
28.80
7.00
0.0
0
1
6
19
91
91
90
28
A
0
MEASURED
FUEL
FLOW
L8/HR
3.50
4.30
7.60
13.20
53.00
53.00
51.00
22.00
6.50
3.50
AIR FLOW
LB/MR
27.00
36.00
67.50
153.00
571.50
571.50
567.00
202.50
67.50
22.50
CALCULATED
F/A
0.12963
0.11944
0.11259
0.08627
0.09274
0.09274
0.08995
0.1C864
0.09630
0.15556
TFST
MODE
1
2
3
4
6
a
9
10
u
n
LXHAUSI
GAS
TF*P
tlEGRCES ^
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
-0.00
-0.00
FXHAUST
GAS
PRFSSURE
PSIA
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
IDRV)
PPMV
112500.00
74000.00
'1)500.00
6000.00
h4000.00
o
-------
OATEI 6/25/71
TEST ORGANIZATION! TELEDYNE-CONTINENTAL
ENGINE SUPPLIERI TELEDYNE-CONTINENTAL
ENGINE DATA *****t*******
i
CAL 10 NUMBER: 217 ENGINE TYPE AND NOOELt 0-47O-R SERIAL NUNtEII 211103
RATED HORSEPOWER! 230.
ENGINE TOTAL TINE! -0. MRS
FUELi AV GAS 80/87 FUEL H/C RATIOl 1.6*0
OPERATIONAL DATA »»«»«»».«»»««.«»««»«»«»««»»«««
INLET AIR TENPERATUREt DEGREES f: START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: START 29.05 FINISH -q.oo
INLET AIR HUMIDITY, CRN H20/LB AIR1 84.00
RELATIVE HUMIDITY: -o.oo PERCENT
SAMPLE LINEl TEMPERATURE, DEGREES C: -0.00, FLO* RATE, LITERS/MINI -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 10
COMMENTS:
»>*
TEST POKER
MODE SHAFT PERCENT
HP RATED
COLO START t |30 SEC 1 0.0 0
TAXI-IOLE LOW ? 2.00 0
TAXI-IDLE HIGH 3 4.60 1
RUN-UP 4 21.90 10
TAKE-OFF 100« 6 191.10 83
CLIMB-RICH 8 152.70 66
CLIMB-LEAN 9 153.80 66
APPROACH 10 39.00 16
TAXI-COLE 11 4.30 1
HOT START 13 0.0 0
TEST EXHAUST EXHAUST CO CO THC
MODE GAS CIS IORYI 2 (MET)
TEMP PRESSURE PPMV IDRY) PPMV
DEGREES F PSIA
,
2
3
4
6
a
q
10
11
13
TEST
MODE
I
2
3
4
6
8
9
10
1 1
13
TEST
MODE
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
MASS EMI MASS EMI
CO HC
LB/1K LB/1K
LB FUEL LB FUEL
17?. 66 233.52
463.31 258.31
767.35 275.93
776.52 28.51
1145.91 22.93
626.54 9.06
602.12 7.75
632.14 17.87
620.06 279.34
575.01 219.09
CO
LB/1K HP-HR
...HORSFPOWER-HR BASIS NOT
2
3
4
6
8
9
10
11
4.170
3.286
1.040
0.79B
0.361
0.339
0.551
2.581
HQRSEPOWER-HR BASIS NOT
TEST
MdOE
3
t,
8
ID
11
TOTAL FOR
TOTAL FOR
TIME IN MEASURED
MODE FUEL FLO*
MIN. L8/HR
12.00 19.70
0.30 133.00
5.00 B8.00
6.00 34.00
4.00 17.90
CYCLE
CrCLF/LB FUEL
64000.00
69000.00
97500.00
88000.00
120000.00
57000.00
53000.00
61500.00
83000.00
99000. 00
MASS EMI
N02
L9/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-3.00
-0.00
CO
2
LB/IK HP-HR
MEASURED AIR FLOW CALCULATED
FUEL LB/HR F/A
FLOW
LB/HR
15.50 94.50 0.16402
18.00 126.00 0.14286
19.70 162.00 0.12160
32.00 297.00 0.10774
133.00 1345.50 0.09885
88.00 1044.00 0.08429
86.50 1066.50 0.08111
34.00 173.50 0.09103
IT. 90 139.50 0.12832
14.50 Bl.OO 0.17901
NO NO NO ALDEHYDES
IORYI 2 X
PPMV ICRYI IORY)
PERCENT V
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/IK
L9 FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
50000.00
50000.00
47500.00
4500.00
3400.00
1200.00
1000.00
2500.00
50000.00
SOOOO.OO
MASS EMI
NO
LB/IK
LB FUEL
1.05
1.38
1.29
1.30
1.44
6.32
7.74
2.03
1.41
1.39
THC
LB/IK HP-HR
110.00
125.00
100.00
90.00
92.00
350.00
415.00
120.00
115.00
160.00
MASS tMI
NOX
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
LB/U
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
5.78
8.34
15.12
24.85
152.41
55.14
52. OB
21.49
1 1.10
7.61
NO
HP-HR
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
3.62
4.65
5.44
0.91
3.05
O.BO
0.67
0.61
5.0C
3. IB
NO
2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
N02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
NO
X
PARTICULATES
-0.
-0.
-0.
00
00
00
-0.00
-0.
-0.
-0.
-0.
-0.
00
00
00
00
00
-0.00
MASS EMI
NO
LB/HR
0.02
0.02
0.03
0.04
0.19
0.56
0.67
0.07
0.03
0.02
MASS EMI
NOX
LB/KR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
LB/IK HP-HR LB/IK HP-HR
CALCULABLE""
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
2.325
1.182
0.038
0.016
0.005
0.004
0.016
1.163
0.
0.
0.
0.
0.
0.
0.
0.
012
006
002
001
004
004
002
006
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
0.012
0.006
0.002
0.001
0.004
0.004
0.002
0.006
CALCULABLE"**
FUEL
USED
LBS.
3.94
0.66
7.30
3.40
1.20
16.508
cn
L8/1K
L8 FUEL
767.35
1145.91
626.54
632.14
620.06
LTD CYCLE
CO
LB/IK
HOURS
15116.75
152405.88
55135.82
21492.89
11099.14
EMISSIONS
CO
EMISSION
LBS.
3.023
0.762
4.576
2.149
0. 744
11.255
0.682
HC
LB/1K
LB FUEL
275.93
22.93
9.06
17.87
279.34
HC
LB/IK
HOURS
5435.76
3049.29
796.89
607.69
5000.11
HC
EMISSION
LBS.
1.087
0.015
0.066
0.061
0.335
1.564
0.095
NO
L8/1K
LB FUEL
1.29
1.44
6.32
2.03
1.41
NO
LB/IK
HOURS
25.47
191.92
556. C9
68.88
25.26
NO
EMISSION
LBS.
0.0051
0.0010
0.0462
0.0069
0.0017
0.0608
0.0037
11-24
-------
D»T6I 4/21/71
TEST ORGANIZATION! TELEDYNE-COIITINENTAl
ENGINE SUPPLIER! TELEOVNE-CONTINENTAl
ENGINE 0»T» "«»»«««.
CAL ID NUMBER: 218 ENGINE TYPE AND MODEL: O-»TO-R
RATED HORSEPOUERl 230.
ENGINE TOTAL TIME: -0. HRS
FUEL: AV GAS 80/87 FUEL N/C RATIO: 1.840
OPERATIONAL DATA «»«««««*«»««««««««««*«««*«*««««*«
INLET AIR TEMPERATURE, DEGREES F: START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: START 28.93 FINISH -0.00
INLET AIR HUMIDITY, CRN H20/L8 AIR: 109.00
RELATIVE HUMIDITY: -o.oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOH RATE, LIFERS/KIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 10
COMMENTS:
SERIAL NUH8ERI
211302*
TEST POWER
MODE SHAFT PERCENT
HP RATED
COLD START » 110 SEC 1 0.0 0
TAXI-IDLF LOW 2 1.50 0
TAXI-IDLE HIGH 3 4.20 1
RUN-UP 4 23.10 10
TAKF-OFF lOOt 6 158.70 68
CLIMB-RICH a 155.30 67
CLIMB-LEAN 1 156.80 68
APPROACH 10 52.60 22
TAXI-IDLE 11 4.00 1
HOT START 13 0.0 0
TFST FXHAUST EXHAUST CO CO THC
MODE GAS GAS (DRY) 2 (WET)
TEMP PRESSURE PPMV (DRY) PPMV
OEGREFS F PSIA
I
2
3
4
6
8
9
10
11
11
TFST
1UDE
1
>
3
4
IS
H
9
in
11
1 )
TESl
MODE
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
MASS FMI MASS EMI
CO HC
LB/IK LB/1K
Lfl FUEL LB FUEL
468.01 24?. 74
5?1.IO 756.46
191.86 341.91
950. 98 31.34
1164.52 20.32
641.DO 10.91
504.51 9.87
575.94 12.02
574.55 288.77
175.37 249.57
CO
LB/IK HP-HR
»*»»tHnRSFPOyFR-HR BASIS NOT
2
3
4
6
q
1
10
11
5.RD2
3.306
1.359
0.954
0.372
0.328
0.460
2.456
HORSFPOHtR-HR BASIS NOT
TFST
MUOF
3
6
a
10
11
TOTAL FOR
TOTAL FOR
TIMT. IN MFASURED
MOIE Furi FLOW
MN. LB/HR
12.00 14.00
0.30 130.00
5.00 90.00
6.00 42.00
4.00 17.10
CYCLE
CYCLE/LB FUEI
76500.00
78000.00
97500.00
110000.00
122000.00
61500.00
S4000.00
53000.00
74000.00
S9000.00
MASS EMI
NO 2
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
LB/IK HP-HR
MEASURED AIR FLOW CALCULATED
FUEL LB/HR F/A
FLOW
LB/HR
15.40 99.00 0.15556
16.70 117.00 0.14274
14.00 153.00 0.09150
33.00 301.50 0.10945
130.00 1323.00 0.09826
90.00 1012.50 0.08889
86.50 1035.00 0.08357
42.00 495.00 0.06485
17.10 139.50 0.12258
15.50 103.50 0.14976
NO NO NO ALDEHYDES
(DRY) 2 X
PPMV (DRY) (DRY)
PERCENT V
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
C02
LB/IK
LB FUFL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
50000.00
50000.00
48000.00
5000.00
3000.00
1500.00
1300.00
1600.00
5COOO.OO
50000.00
MASS EMI
NO
Lfl/U
LP FUEL
1.21
1.21
1.49
0.71
0.97
4.54
6.51
4 .64
1.15
1.27
THC
Lfl/lK HP-HR
120.00
110.00
89.00
50.00
62.00
265.00
360.00
260.00
90.00
122.00
MASS EMI
NOX
LB/IK
L8 FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
LO/1K
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS E'H
CO
LB/HR
7.21
8.70
13.89
31.38
151.39
57.76
51.43
24.19
9.82
5.8?
NO
HP-MR
PPMV
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HK
3.74
4.3?
4.71?
1.03
2.64
0.98
0.85
0.50
4.94
3.67
NO
2
Lfl/lK HP-
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
NO 2
LH/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
S.HOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.oo
-0.00
-c.oo
NO
X
PARTICULATES
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
MASS Efl
NO
LB/Hk
0.02
0.0?
0.02
0.02
0. 13
0.41
0.56
0. 19
0.02
0.02
00
00
00
00
00
00
00
00
00
00
MASS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
HR LB/IK HP-HR
CALCULABLE****
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
2.87B
1. 140
0.045
0.017
0.006
0.005
0.010
1.234
0.
0.
0.
0.
3.
0.
0.
0.
013
005
001
001
00.1
004
004
005
-0.000
-0.000
-0.000
-o.ono
-o.ooo
-o.oon
-0.000
-0.000
0.013
0.005
0.001
0.001
0.003
0.004
0.004
0.005
CALCULABLE'***
FUEL
I/SCO
L'3S.
2.80
0.65
7.47
4.20
1.15
16.266
CO
L8/IK
LB FUEL
991 .86
1164.52
641.80
575.94
574.55
LTD CYCLL
CO
LD/IK
HOURS
13886.05
151388.06
57762.31
241B9.66
9824.86
EMISSIONS
CO
HC
EMISSION LB/IK
LBS.
2.777
0.757
4. 794
2.419
0.65K
11.406
0.701
LB FUEL
341.91
20.32
1C. 91
12.02
289. 77
HC
LB/IK
HOURS
47d6. 7*>
^641.04
981.49
504.73
4937.97
HC
EMISSION
LOS.
0.957
0.011
0.081
0.050
0.331
1.433
O.OBR
HU
LB/IK
LB FUEL
1.49
0.97
4.54
4.44
1.15
NO
LB/IK
HOURS
20.62
126.37
40B.R2
194.92
19.63
NO
EMISSION
LBS.
0.0042
0.0006
0.0339
0.0195
0.0013
0.0595
0.0037
11-25
-------
DATEI- »/I*/TI :
TEST ORCANIlATtOm TElEDVNE-COMTINENTtl . _ .
ENGINE SUPPLieRl TELEOYNE-COWTIWNTAL ''
ENGINE DAT* »»«»»»«»»»»»»«»»»*«»««»»«»»»*«»»»««««»»»»««»»
«
CM. 10 NUMBERI 219 ENGINE TYPE AND WO El I 0-4TOHI JM1AI NtMIEH 470-1-211101*
RATED KORSEPMERI 230.
ENGINE TOTAL TIKE I -0. MRS
FUEL' »V GAS aa/(T FUEL H/C RATIQI I.MO
OPERATIONAL DATA ******«*»»******
INLET AIR TEMPERATUREi DEGREES Fl START -0.00 FINISH -0.00 _
ATMOSPHERIC PRESSUREl START 28.18 FINISH -0.00
INLET AIR HUMIDITY, CRN H20/LB AIRl 114.00
RELATIVE HUNIOITYl -0.00 PERCENT
SANPLE LINEI TEMPERATURE! DEGREES Cl -0.00, FLO* RATE, LITERS/MINI -0.00
SAMPLE LINE TRANSPORT TIME, SECl -0.00
NUMBER OF TESTSl 11
COMMENTSi
TEST POKER
MODE SHAFT PERCENT
HP RATED
COLO START » 1)0 SEC 1 0.0 0
TAXI-IDLE LOW 2 1.60 0
TAXi-IOLE HIGH 4.00 1
RUN-UP 22.00 9
TAKE-OFF 1001 166.30 80
TAKE-OFF TO CLIMB 192.90 66
CLIMB-RICH 150.60 6?
CLIMB-LEAN 154.00 66
APPROACH 10 37.00 16
TAXI-IDLE 11 4.40 1
HOT START 13 0.0 0
TEST EXHAUST EXHAUST CO CO THC
MODE GAS GAS IORYI 2 (hETI
TEMP PRESSURE PPMV IDRVI PPMV
DEGREES F PSIA
1
2
10
11
13
TFST
NODE
1
2
3
4
6
7
a
i
10
11
i)
TEST
MODE
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
MASS EMI MASS EMI
CO HC
IB/ IK LB/IK
LB FUEL LB FUEL
466. 92 129.22
452.16 126.04
549.69 66.50
624.77 16.20
1146.84 20.79
66B.41 10.92
BBS. 81 8.25
5BS.01 9.90
715.57 13.45
507.58 37.94
418.09 17.21
CU
LB/IH HP-HR
HORSEPHHER-HR BASIS NOT
2
3
4
6
7
a
9
10
11
2.487
1.745
0.625
O.B02
0.398
0.437
0.329
0.619
1.292
HORSEPOHER-HR BASIS NOT
TEST
MODE
3
6
B
10
11
TOTAL FOR
TOTAL FOR
TINF IN MEASURED
MODE FUEL FLOW
MIN. LB/HR
12.00 12.70
0.30 130.00
5.00 74.00
6.00 32.00
4.00 11.20
CYCLE
CYCLE/LB FUEL
52000.00
52000.00
59000.00
59000.00
122000.00
64000.00
73000.00
53000.00
71000.00
52000.00
52000.00
MASS EMI
N02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
en
2
LB/IK HP-HR
MEASURED AIR FLOM CALCULATED
FUEL LB/HR F/A
I OK
LB/HR
(.90 81.00 0.10494
8.80 81.00 0.10864
12.70 126.00 0.10079
22.00 292.00 0.08730
110.00 1303.00 0.09962
91.00 1026.00 0.08869
74.00 999.00 0.07407
86.50 1039.50 0.08321
32.00 346.50 0.09235
11.20 117.00 0.09573
8.90 72.00 0.11806
NO NO NO ALDEHYDES
IORYI 2 X
PPMV (ORYI IORYI
PERCENT V
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
20000.00
20000.00
10000.00
2200.00
3100.00
1500.00
1000.00
1300.00
1900.00
5500.00
2900.00
MASS EMI
NO
LB/IK
LB FUEL
0.88
0.64
0.61
1.57
0.93
3.77
21.00
6.07
1.32
0.77
0.53
THC
LB/IK HP-HR
60.00
45.00
40. or
90.00
60.00
220.00
1050.00
335.00
80.00
48.00
40.00
MASS EMI
NOX
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
LB/IK
PPMV
-0.00
-0.00
"~ -OiOO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00.
-0.00
MASS EMI
CO
LB/HR
3.97
3.98
6.98
13.74
149.35
60.83
65.77
50.60
22.90
5.68
3.55
NO
HP-HR
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HR
1. 10
1.11
0.84
0.36
2.70
0.99
0.61
0.66
0.43
0.42
0.15
NO
2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EHI
NO 2
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
X
PARTICULATES
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
MASS EMI
NO
LB/HR
0.01
0.01
0.01
0.03
0.12
0.34
1.55
0.53
0.04
0.01
0.00
00
00
00
00
00
00
00
00
00
00
00
MASS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
LB/IK HP-HR LB/IK HP-HR
CALCULABLE'***
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-o.ooo
0.693
0.211
0.016
0.015
0.007
0.004
0.006
0.012
0.097
0.
0.
0.
0.
0.
0.
0.
0.
0.
004
002
002
001
002
010
003
001
002
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
0.004
0.002
0.002
0.001
0.002
0.010
0.003
0.001
0.002
CALCULABLE****
FUEL
USED
Las.
2.54
0.65
6.14
3.20
0.75
13.282
CO
LB/IK
LB FUEL
549.69
1148.84
888.81
715.57
507.58
LTD CYCLE
CO
LB/IK
HOURS
6981.07
149349.50
65771.75
22898.30
5684.90
EMISSIONS
CO
EMISSION
LBS.
1.396
0.747
5.459
2.290
0.381
10.273
0.77J
HC
LB/IK
LB FUEL
66.50
20.79
B.25
13.45
37.94
HC
LB/IK
HOURS
844.56
2702.54
610.64
430.27
424.98
HC
EMISSION
LBS.
0.169
0.014
0.051
0.043
0.028
O.S05
0.023
NO
LB/IK
LB FUEL
0.61
0.93
21.00
1.32
0.77
NO
LB/IK
HOURS
7.77
120.65
1553.91
42.38
B.62
NO
EMISSION
LBS.
0.0016
0.0006
0.1290
0.0042
0.0006
0.1359
0.0102
11-26
-------
OUTEl 6/29/71
TEST ORGANIIATIONI TELEDYNE-CONTINEKTAL
ENGINE SUPPLIER! TELEDYNE-CONTINENTAL
ENGINE OAT* »***»»»»«*»»*
C»L ID NUMBER I 221 ENGINE TYPE AND NOOELI 0-*TO-R
RATED HORSFPOMERI 230.
ENGINE TOTAL TIME: -0. HRS
FUEL: IV GAS 80/87 FUEL H/C RATIO: 1.840
OPERATIONAL DATA <«««««««««««««««*»«»««««**
INLET AIR TEMPERATURE, DEGREES F: START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: START 26.77 FINISH -0.00
INLET AIR HUMIDITY, CRN H20/LB AIR: 103.00
RELATIVE HUMIDITY: -o.oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -O.OC, FLOM RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 9
COMMENTS:
SERIAL NUMBER! 47O-K-311302B
COLD START 130 SEC
TAXI-IDLE LOM
TAXI-IDLE MICH
RUN-UP
TAKE-OFF 1001
CLIMK-RICH
APPROACH
TAXI-IDLE
HOT START
TESI
MODI
10
11
13
POWER
SHAFT PERCENT
HP RATED
0.0
1.90
4.90
24.00
193.60
158.00
38.90
5.00
1.40
0
0
2
10
64
69
16
2
0
MEASURED
FUEL
FLOW
LB/HR
9.80
10.70
14.10
30.00
132.00
90.00
33.00
14.80
8.90
AIR FLON
LB/HR
81.00
94.50
126.00
263.50
1341.00
1039.50
360.00
117.00
76.50
CALCULATED
F/A
0.12099
0.11323
0.11190
0.10502
0.09B43
0.06656
0.09167
0.12650
0.11634
TEST
MODE
1
2
3
4
b
a
10
11
11
FXH4UST
GAS
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
EXHAUST
GAS
PRESSURE
PSI A
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
(DRY)
PPMV
bISOO.OO
71000.00
78000.00
78000.00
l.!2000.00
57000.00
r>4000.00
71000.00
STOOD. 00
CO
2
(DRY)
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
(WEI)
PPMV
V
32500.00
30000.00
13220.00
3300.00
2600.00
1300.00
1900.00
12000.00
37500.00
NO
(DRY I
PPMV
60.00
55.00
50.00
60.00
70.00
320.00
100.50
40.00
70.00
NO
2
-------
OATEl 4/21/71
TEST ORGANIZATION: TELEDtNE-CONTINCNTAl
ENGINE SUPPLIER: TEIEOYNE-CONTINENTAL
ENGINE DATA **»*»***«**«****»*********»*****************
C»L 10 NUMBER: 110 ENGINE TYPE MO HOOCH 10-MO-P IRIU NUMf«l lf«*IOA
RATED HORSEPOUERI 100.
ENGINE TOTAL TINEl -0. Has
FUEL: AV GAS 100/110 FUEL H/C RATIOl 1.8*0
OPERATIONAL DATA «««»«««««««««»«««««««**«.».«».«««««««««»«««»«««
INLET AIR TEMPERATURE. DEGREES Ft START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: START 21.96 FINISH -0.00
INLET AIR HUMIDITY, GRN H20/LB AIRI 63.00
RELATIVE HUMIDITY: -0.00 PERCENT
SANPLE LINE: TENPERATUREt DEGREES Cl -0.00. FLOV RATEi LITERS/MINI -0.00
SAMPLE LINE TRANSPORT TIMEt SEC: -0.00
NUMBER OF TESTS: 10
COMMENTS:
COLD START t 130 SEC
TAXI-IDLE LOW
TAXI-IDLE HIGH
RUN-UP
TAKE-OFF lOOt
CLIMB-RICH
CLIMB-LEAN
APPROACH
TAXI-IDLE
HOT START
TEST
MODE
1
2
3
4
6
e
9
10
11
13
POKER
SHAFT PERCENT
HP RATED
0.0
1.10
4.60
24.00
263.70
202.10
202.90
35.40
4.60
0.0
0
0
I
7
87
67
67
11
1
0
MEASURED
FUEL
FLOW
LB/HR
10.60
11.00
16.00
36.00
143.00
110.00
92.00
45.00
16.00
10.50
AIR FLOW
LB/HR
81.00
85.50
130.50
306.00
1566.00
1188.00
1183.50
378.00
117.00
81.00
CALCULATED
F/t
0.13086
0.12B65
0.12261
0.11765
0.09259
0.09259
0.07774
0.11905
0.13675
0.12963
TEST
MODE
9
10
11
13
EXHAUST
GAS
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
CO
I DRY I
PPMV
74000.00
69000.00
59000.00
54000.00
61500.00
61500.00
10000.00
B 1000.00
59000.00
81000.00
CO
2
I CRY I
PERCENT V
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
(MET)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
(DRY)
PPMV
47.00
35.00
25.00
30.00
460.00
470.00
-0.00
-0.00
30.00
25.00
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
10
II
11
MASS EMI
CO
LB/IK
LR FUEL
544.96
5 1 6 . 70
462.98
440.84
625.75
625.75
118.33
651.84
415.98
602.09
MASS FMI
HC
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
N02
LB/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
Lfl/lK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NO
LB/IK
LB FUEL
0.57
0.43
0.32
0.40
7.69
7.85
-0.00
-0.00
0.35
0.11
MASS EMI
NOX
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
5.78
5.68
7.41
15.87
90.73
68.83
10.89
29.42
6.66
6.32
MASS EMI
HC
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI
N02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CU2
Lfl/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NO
LB/HR
0.01
0.00
0.01
0.01
1.11
0.86
-0.00
-0.00
0.01
0.00
MASS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
cn
LB/IK HP-MR
HORSEPOUEH-HR BASIS NOT
2
3
4
6
R
9
10
11
2.991
1.610
0.661
0.344
0.341
0.054
0.831
1.447
CO
2
LB/1K HP-HR
CALCULABLE'*"
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
THC
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
NO
LB/IK HP-HR
0.002
0.001
0.001
0.004
0.004
-0.000
-0.000
o.ooi
LB/1K HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
NO
X
LB/IK HP-HR
0.002
0.001
o.ooi
0.004
0.004
-0.000
-0.000
0.001
HORSEPOUER-HR BASIS NOT CALCULABLE****
TEST
MODE
10
II
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
MEASURED
FUEL FLOW
LB/HR
16.00
145.00
110.00
45.00
16.00
TOTAL FOR CYCLE
TOTAL FOR CYCLE/LB FUEL
LTD CYCLE EMISSIONS
FUEL CO CO CO
USED LB/IK LB/IK EMISSION
LBS. La FUEL HOURS LBS.
3.20
0.72
9.13
4.50
1.07
18.627
462.98
625.75
625.75
651.84
415.98
7407.62
90731.19
68832.06
29422.80
6655.64
1.482
0.454
5.711
2.942
0.446
11.036
0.592
HC
LB/IK
HOURS
-0.00
-0.00
-0.00
-0.00
-0.00
HC NO
EMISSION LB/1K
LBS. LB FUEL
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
0.32
7.69
7.85
-0.00
0.35
NO NO
LB/IK EMISSION
HOURS LBS.
5.16
1114.73
864.04
-0.00
5.56
0.0010
0.0056
0.0717
-0.0000
0.0004
-0.0000
-0.0000
11-28
-------
OATEl 6/M/71
TEST ORGANUATIONI TELEOYNE-CONTINENTU
ENGINE SUPPLIER:
ENGINE 0«T» ««»«»«»«»«..«»»««
C*L ID NUMBER: 211 ENGINE TYPE AND NOOELI io-*20-p
RATED HORSEPOUER: 300.
ENGINE TOTAL TINE: -0. MRS
FUEL: AV GAS 100/130 FUEL H/C RATIO: 1.8*0
OPERATIONAL DATA t**««««»»**«««*«*«««««««««*««««»«»««»«*«««.««*«««««
INLET AIR TEMPERATURE. DEGREES F: START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: START 28.96 FINISH -0.00
INLET AIR HUMIDITY, CRN H20/LB AIR: 63.00
RELATIVE HUHIDITr: -0.00 PFRCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RAIE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME. SEC: -0.00
NUMBER CF TESTS: 10
COMMENTS:
SERIAL NUMBER!
159850B
TEST POWER
MODE SHAFT
HP
COLD START » 130 SEC 1 0.0
TAXI-IDLF LOW 2 1.90
TAXI-IDLF HIGH 3 4.80
RUN-UP 4 24.20
TAKE-OFF IOOJ 6 264.20
CLIMB-RICH 8 202.30
CLIMB-LFAN 9 203.30
APPROACH 10 35.80
TAXI-IDLE . 11 4.50
HOT START 13 0.
TEST
MODE
,
2
3
^
6
a
9
10
11
13
TFST
MflDF
1
2
3
4
6
8
9
10
11
13
TEST
MODE
fXHAUST EXHAUST
GAS GAS
TEMP PRESSURE
nF.GREES F PSIA
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
MASS EMI MASS EMI
CO HC
LR/1K LO/1K
I.B FUEL LB FUEL
553.09 -0.00
462.35 -0.00
477.12 -0.00
419.36 -0.00
570.25 -0.00
599.51 -0.00
95. ?7 -0.00
459.29 -0.00
441.03 -0.00
579. (9 -0.00
CO
LR/1K HP-H4
HORSFPONIR-MR HASIS NOT
2
.1
4
6
u
9
10
11
2.993
1.511
0.641
0.313
0.329
0.043
0.616
1.421
....OHOKSf PO..FR-HB BASIS NOT
CO
(DRY)
PPMV
70500.00
69000.00
62000.00
52000.00
54000.00
59000.00
8000.00
62000.00
59000.00
78000.00
MASS FMI
N02
LD/1K
LR FUHL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-1.00
-0.00
-0.00
-0.00
CO
2
LH/IK HP-HR
0
CO
2
(DRY)
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PFRCENT
RATED
0
0
I
8
8fl
67
67
11
1
0
THC
(WET)
PPMV
V
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NO
LB/IK
LB FUEL
0.65
0.39
0.53
0.62
7. II
6.84
-0.00
0.43
0.52
0.67
THC
LH/IK HP-HR
MEASURED AIR FLOW CALCULATED
FUEL LB/HR F/A
FLOW
LB/HR
10.80 HI. 00 0.13333
12.30 85.50 0.143B6
15.20 121.50 0.12510
37.00 310.50 0.11916
145.00 1633.50 0.08877
111.00 1197.00 0.09273
92.00 1192.50 0.07715
48.00 369.00 0.13008
14.50 112.50 0.12889
10.50 81
NO NO
IDRY1 2
PPMV IDRYI
PPMV
55.00 -0.00
35.00 -0.00
42.00 -0.00
47.00 -0.00
410.00 -0.00
410.00 -0.00
-0.00 -0.00
35.00 -0.00
42.00 -0.00
55.00 -0.00
MASS EMI MASS EMI
NOX CO
LB/IK LB/HK
LB FUEL
-0.00 5.97
-0.00 5.69
-0.00 7.25
-O.CO 15.52
-0.00 82.69
-0.00 66.55
-0.00 8.76
-0.00 22.05
-0.00 6.39
-0.00 6.09
NO
LB/IK HP-HR
.00
NO
X
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HK
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
2
0.12963
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NO 2
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LJ/H^
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
Nil
X
PARTICULARS
-0
-0
-0
-0
-0
-0
-0
-0
-0
-0
MASS EMI
NO
LH/HK
0.01
0.00
0.01
0.0?
1.03
0. 70
-0.00
0.02
0.01
0.01
.00
.00
.00
.00
.00
.00
.00
.00
.00
.00
MASS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
LB/IK HP-HR LB/IK HP-HK
CALCULABLE****
-0.000
-0.001
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-o.ooo
0.002
0.002
0.001
0.004
0.004
-0.000
0.001
0.002
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-o.ooo
-0.000
0.002
0.002
0.001
0.004
0.004
-O.OOO
0.001
0.002
CALCULABLE****
LTD CYCLE EMISSIONS
TFST
MIIOE
3
6
a
10
11
TOTAL FOP
I1TAL FOR
TIME IN
MODE
MIN.
12.00
0.30
5.00
6.00
4.00
CVCLF
CYCLE/L8
MEASURED
FUtL FLOW
LB/HK
15.20
I 45.00
111.00
4P.OO
14.50
FUEL
FUEL
USEn
L1S.
1.04
0.72
9.21
4.80
0.97
18. 749
CO
LR/1K
LU FUK
477.12
570.25
599.51
459.29
441 .03
CU
LB/IK
HOUPS
l?52.21
82686.63
66545.63
22045.99
6394.95
CO
FMISSION
LI'S.
1 .450
0.413
5.523
2.205
0.428
10.020
0.534
HC
LB/IK
L3 FUEL
-o.oo
-c.oo
-o.oo
-0.00
-0.00
HC
LB/IK
HOURS
-0.00
-0.00
-0.00
-0.00
-0.00
HC
EMISSION
LBS.
-o.ooo
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
NO
LB/IK
LB FUFL
0.53
7.11
6.H4
0.41
C.52
NO
LH/IK
HCUKS
a. 07
1031 .21
759.58
20.44
7.48
NO
EMISSION
L6S.
0.0016
0.0052
C.0630
0.00?0
0.0005
0.0724
0.0039
11-29
-------
SIIIAL NUNtfRI
it«rm
0»TEl 6/12/71
TEST OAGANIJATIONI TELEDYNE-COWTINENTAL
ENGINE SUPPLIEAl TELEOTWE-CONTINENTAL
C»L 10 NUNBERI 212 ENGINE TVM AND MDELI IO-S10-P
HATED HORSEPOMERI 300.
ENGINE TOTAL TINEl -0. H»S
FUELI AV GAS 100/110 FUEL H/C lit 1101 1.840
OPERATIONAL DATA «»«««»»»»»»«»»»»»»»
INLET AIR TEMPERATURE! DEGREES Fl START -0.00 FINISH -0.00 _,
ATMOSPHERIC PRESSURE! START 28.9* FINISH -0.00
INLET AIR HUMIDITY, CRN H2Q/LB AIRI 6}.00
RELATIVE HUMIDITVI -0.00 PERCENT
SAMPLE LINEl TEMPERATURE, DEGREES Cl -0.00, FLOK RATE, LITERS/MINI -0.00
SAMPLE LINE TRANSPORT TIME, SECl -0.00
NUMBER OF TESTS: 1
COMMENTS:
COLD START 130 SEC
TAXI-IDLE HISH
RUN-UP
TAKE-OFF 100X
CLIMB-RICH
CLIMB-LEAN
APPROACH
TAXI-IDLE
HOT START
TEST
MODE
3
4
6
a
9
10
11
13
POKER
SHAFT PERCENT
HP RATED
0.0
4.60
23.60
261.40
200.00
204.80
3T.30
4.20
0.0
0
1
T
87
66
68
12
1
0
MEASURED
.FUEL
FLOH
IB/MR
11.50
18.10
39.00
194.00
123.00
92.00
46.00
14.60
8.10
AIR FLOM
LB/HR
81.00
144.00
315.00
159T.50
1192.50
1183.50
396.00
117.00
6T.50
CALCULATED
F/A
0.14198
0.12569
0.12381
0.09640
0.10314
O.OT7T4
0.11616
0.12479
0.12000
TEST
MODE
1
3
4
6
a
9
10
11
1)
EXHAUST
CAS
TFMP
DECREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
EXHAUST CO
CAS (ORVI
PRESSURE PPMV
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
87500.00
52000.00
116000.00
87500.00
97500.00
9000.00
122000.00
54000.00
73500.00
CO
2
(ORV)
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
IWET)
PPMV
V
47500.00
42500.00
9000.00
2400.00
2400.00
1300.00
11000.00
37500.00
45000.00
NO
IDRVI
PPMV
145.00
177.00
125.00
205.00
175.00
2250.00
55.00
60.00
60.00
NO
2
(CRT)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.oo
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TFST
"ODE
1
3
fc
6
B
9
10
11
13
MASS EMI
CO
LB/IK
LR FUEL
594.18
398.34
901.71
958.84
900.07
106.50
100H.09
416. 5B
198.79
MASS EM
HC
LB/IK
LR FJEI
246.51
241.02
51.60
16.48
15.70
10.36
66.05
213.79
263.93
MASS CMI MASS EMI
NO? C02
LB/IK LP/1K
LB FUEL LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI MASS EMI
NO NO I CO
LB/IK LB/IK LB/HR
LB FUEL LB FUEL
1.62
2.23
1.60
3.31
2.65
43.73
0.75
0.76
0.79
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
6.63
7.21
35.17
132.26
110.71
9.80
46.37
6.08
4.77
MASS EMI
HC
LB/HR
MASS EMI
N02
LB/HR
MASS EMI
C02
LB/HR
MASS EH
NO
LB/HR
2.83
4.36
2.01
2.54
1.9)
0.95
3.04
3.12
2.14
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
0.02
0.04
0.06
0.51
0.33
4.02
0.03
0.01
0.01
MASS EMI
HO*
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
LB/IK HP-HR
LB/IK HP-HR
HORSEP04ER-HR BASIS NOT CALCULARLF****
3 1.567 -0.000
» 1.490 -0.000
6 0.506 -0.000
B 0.554 -0.000
9 0.048 -0.000
10 1.243 -0.000
II 1.448 -0.000
HORSEPOUFR-HR BASIS NOT CALCULABLE****
THC
LB/IK HP-HR
0.948
0.065
0.010
0.010
0.005
0.081
0.743
HO
LB/IK HP-HR
0.009
0.003
0.002
0.002
0.020
0.001
0.003
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
NO
X
LB/IK HP-HR
0.009
0.003
0.002
0.002
0.020
0.001
0.003
LTD CYCLE EMISSIONS
TEST
MODE
3
6
8
10
II
TOTAL FOR
TOTAL FOR
TIME IN
MODE
HIN.
12.00
0.30
5.00
6.00
4.00
CYCLE
CYCLE/LB
MEASURED
FUEL FLOH
LB/HR
IB. 10
154.00
123.00
46.00
14.60
FUEL
FUEL
USED
LBS.
3.62
0.77
10.21
4.60
0.98
20.177
CO
LB/IK
LB FUEL
398.34
858.84
900.07
1006.09
416.58
CO
LB/IK
HOURS
72C9.88
132261.56
110708.69
46372.05
6082.04
CO
EMISSION
LBS.
1.442
0.661
9. 189
4.637
0.407
16.337
0.810
HC
LB/IK
LB FUEL
241.02
16.48
15.70
66.05
213.79
HC
LB/IK
HOURS
4362.54
2537.19
1930.99
3038. -.8
3121.36
HC
EMISSION
LBS.
0.873
0.013
0.160
0.304
0.209
1.55B
0.077
NO
LB/IK
LB FUEL
2.23
3.31
2.65
0.75
0.76
NO
LB/IK
HOURS
40.31
508.98
326.39
34.34
11.10
NO
EMISSION
LBS.
0.0081
0.0025
0.0271
0.0034
0.0007
0.0419
0.0021
11-30
-------
OtTEl 6/22/71
TEST ORGANIZATION: TELEDYNE-CONTINtNTAl
ENGINE SUPPLIER! TELEOYNE-CON11NENTAL
ENGINE DATA »«»«*«»**
i
C*L ID NUMBER: 213 ENGINE TYPE AND MODEL: 10-920-P SERIAL NUMBER: I»«9TTB
RATED HORSEPOMERI JOO.
ENGINE TOTAL TINE: -0. HRS
FUEL: AV GAS 100/130 FUEL H/C RATIO: 1.6*0
OPERATIONAL DATA »«<.»....»««
INLET AIR TENPERATURE, DECREES F: START -0.00 FINISH -0.00 _
ATMOSPHERIC PRESSURE: START 28.94 FINISH -0.00
INLET AIR HUMIDITY, CRN H20/LB AIR: 63.00
RELATIVE HUMIDITY: -0.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/NIN: -0.00
SAMPLE LINE IRANSPORT TINE, SEC: -0.00
NUMBER OF TESTS: 10
COMMENTS:
COLO START . 130 SEC
TAXI-IDLF LOU
TAXI-IDLF HIGH
RUN-UP
TAKE-OFT 1001
CLIMB-RICH
CLI MR-LEAN
APPROACH
TAKI-tOLE
HOT START
TESI
MODI
10
II
13
POWER
SHAFT PERCENT
HP RATED
0.0
2.60
6.10
26.60
262.80
206.20
209.20
tO.00
5.70
0.0
0
0
2
e
87
68
69
13
1
0
MEASURED
FUEL
FLOW
LB/HR
9.60
10.50
17.20
37.00
152.00
123.00
92.00
46.00
14.20
10.00
AIR FLOW
LB/HR
76.50
81.00
135.00
315.00
1548.00
1206.00
1188.00
391.50
117.00
67.50
CALCULATED
F/A
0.12549
0.12963
0.12741
0.11746
0.09819
0.10199
0.077*4
0.11750
0.12137
0.14815
TFST
MODE
1
10
II
13
fXHAUST
r,AS
IEMP
OFGREFS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
(ORfl
PPMV
9500.00
£4500.00
59000.00
117000.00
88000.00
92500.00
8300.00
122000.00
52000.00
74000.00
cn
2
(DRY)
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
THC
(WETI
PPMV
V
50000.00
50000.00
42500.00
9500.00
2500.00
2300.00
1200.00
1100.00
50000.00
50000.00
NO
(DRY)
PPMV
295.00
112.00
35.00
68.00
215.00
190.00
2825.00
87.00
100.00
110.00
NO
2
lORtl
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
(DRY)
PPMV
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARIICULATES
-0.00
-0.00
-0.00
-0.00
-o.co
-0.00
-o.oo
-0.00
-0.00
-0.00
tEST
MODE
10
11
u
MASS F.M1 MASS EMI MASS EMI
CO HC N )2
LB/IK LB/IK 19/lK
LR FUEL LB FUEL LH FUEL
72.89
628.II
446.04
956.61
949.56
862.75
98.53
997.19
412.05
431.27
283.89
277.27
238.66
56.59
16.94
15.17
9.60
6.55
290.86
251.55
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
C02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
MASS EMI
Nil
LB/IK
LB FUEL
3.72
1.37
1.06
0.91
3.41
2.91
55.08
1.17
1.30
1. Id
MUSS EMI
NOX
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
0.70
6.60
7.67
35.39
129.13
106.12
9.06
45.87
5. (15
4.81
MASS FMI
HC
LB/HR
2.73
2.91
4.11
2.T9
2.57
1.87
0.8H
0.30
4.13
2.52
MASS EMI
NO 2
LB/HR
-0.00
-O.CO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS tMI
CC12
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.00
-0.00
MASS E«!
NO
L8/HB
0.04
0.01
0.02
0.03
0.52
0.36
5.07
0.05
0.02
0.01
MASS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TFST
MODE
LB/IK HP-HR
«*»««HOHSEPOWf R-HO RASIS NOT
2 2.53f
> 1.258
4 1.331
6 0.491
K 0.515
9 0.043
10
II
1.147
1.027
LR/IK HP-HR
CALCULABLE'*"
-0.100
-0.000
-11.000
-0.000
-0.000
-0.000
-o.ooo
-0.000
THC
LB/IK HP-H«
1.120
0.673
0.079
0.010
0.009
0.004
O.OCfl
0.725
NO
LB/IK HP-HR
0.006
0.003
o.mi
0.002
0.002
0.024
0.001
0.003
L9/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
NO
X
LR/IK HC-HR
0.006
0.003
0.001
0.002
0.002
0.0?4
0.001
0.003
HOHSFPCIUCR-HR BASIS NO! CALCUL AriLF* »
L10 CYCLE EMISSIONS
10
u
TIME IN MEASURED FUEL
MODE FUEL FLOW USF.D
4
0. 7(,
10.21
4.60
0.95
19.960
CO
LB/1K
L9 FUEL
446.04
849.56
662.75
997.19
412.05
CO
LB/IK
HOURS
7671.91
129132.56
106118.31
45870.9*
5S51.16
CO
EMISSION
LBS.
1.534
0.6*6
n.aon
4.587
0.392
15.967
0.800
HC
Lfl/ln
LB FUhL
2 18.66
16.94
15.17
6.55
290.86
HC
LB/IK
HOURS
4105.03
2574.63
1865.50
301.35
4130.23
HC
EMISSION
LBS.
0.821
0.013
0.155
O.C30
0.277
1 .296
0.065
Nn
LB/IK
LB FUEL
1.06
3.41
2.91
1.17
1.30
Nil
LB/IK
HOURS
Id. 15
518.22
358.03
53.73
18.48
NO
EMISSION
LBS.
0.0036
0.0026
0.0297
0.0054
0.0012
0.0426
0.0021
11-31
-------
I
0*Til 4/21/71
TEST OAGANIlATIWl TEL !DYNE-COirn MENTAL
ENGINE SUPPLIER! TELEOVNE-CO*TINfNTAL
ENGINE D»T» **********»
I
CU ID NUMIEU (I* ENGINE TYM MO NOOfU 10-MB-P tllltl NU»MI 1IMMA
RATED HORSEPOHERl 100.
ENGINE TOTAL TINE! -0. MRS
FUELI «V CM 100/110 FUEL H/C RATIOI l.»40
OPERATIONAL OAT A *»»«»»»»»»»»»»
INLET AIR TENPERATUREt DEGREES Ft START -0.00 FINISH -0.00 _
ATHOSPHERIC PRESSUREl START 28.60 FINISH -0.00
INLET AIR HUMIDITY. GRN H2Q/L8 AlRl 89.00
RELATIVE HUMIDITY! -0.00 PERCENT
SAMPLE LINE' TENPERATUREi DEGREES Cl -0.00. FLOM RATE. LITERS/MINI -0.00
SAMPLE LINE TRANSPORT TIME. SECl -0.00
NUMBER OF TESTS: 10
COMMENTS!
TEST POUER
MODE SHAFT PERCFNT
HP RATED
COLD START < 110 SEC 1 0.0 0
TAXI-IDLE LOW 2 2.10 0
TAXI-IDLE HIGH 1 5.40 1
RUN-UP * 21.40 8
TtKE-OFF [001 6 259.90 86
CL (MS-RICH 6 205.1)0 68
CLIMB-LEAN 9 207.70 69
APPROACH 10 12.10 10
TAXI-IOLE 11 5.00 i
HOT START 11 0.0 0
TEST EXHAUST EXHAUST CO CO THC
MODE GAS GAS IORTI 2 INETI
TEHP PRESSURE PPNV IORYI PPMV
DEGREES F PSIA
1
2
3
4
6
8
9
10
11
1)
TEST
MODE
1
2
1
4
6
8
9
10
11
1]
TEST
MODE
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
MASS EMI MASS EMI
CO HC
LB/IK LB/1K
LB FUEL LH FUEL
403.21 114.91
SOS. 64 64.12
ATT. 19 21.92
476.82 IB. 40
665.20 13.99
575.48 14.10
94.49 12.81
664.91 22.09
437,85 45.21
483.98 205.52
CO
LB/1K HP-HP
HORSFPOHER-HR BASIS NOT
2
3
4
b
9
9
10
11
3.67B
1.794
0.5B2
0.169
0.311
0.042
0.732
1.138
HORSEPOtfER-HR BASIS NOT
TEST
NODE
3
6
8
10
11
TOTAL FOR
TOTAL FOR
TIMF IN MEASURED
MODE FUEL FLOW
MlN. LB/HR
12.00 14.30
0.10 144.00
5.00 112.00
6.00 14.50
4.00 13.00
CYCLE
CYCLE/LB FUEL
52000.00
90000.00
78000.00
54000.00
66500.00
57000.00
8000.00
81000.00
53000.00
66500.00
MASS EMI
N02
L9/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
CO
2
LB/IK HP-HR
MEASURED
FUEL
FLO*
LB/HR
10.00
10.30
14.10
11.00
144.00
112.00
92.00
14.50
11.00
8.30
MO
(DRYI
PPMV
PERCENT V
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/IK
L8 FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
20000.00
10000.00
3500.00
2900.00
2000.00
2000.00
1600.00
3600.00
7500.00
37500.00
MASS EMI
NO
L6/1K
LB FUEL
1.27
2.21
1.57
2.03
5.09
6.97
55.78
1.60
1.15
1.08
THC
LB/IK HP-HR
100.00
190.00
110.00
140.00
110.00
420.00
2875.00
115.00
85.00
90.00
AIR FLOM CALCULATED
LB/HR F/A
81.00 0.12346
99.00 0.10606
110.50 0.10958
288.00 0.10764
1514.50 0.09184
1206.00 0.09287
1188.00 O.OT744
306.00 0.11275
112.50 0.11556
63.00 0.11175
NO NO ALDEHYDES
2 X
(DRY) (DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NOX
LB/IK
L9 FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
CO
L8/HS
4.03
8.46
9.69
14.78
95.79
64.45
8.69
23.63
5.69
4.02
LB/lK HP-HR
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
L8/H8
1.15
0.67
0.31
0.57
2.02
1.58
1.18
0.76
0.59
1.71
NU
2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
N02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
NO
X
PARTICULATES
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
MASS EMI
NO
LB/HR
0.01
0.02
0.02
0.06
0.73
0.78
5.13
0.06
0.01
0.01
00
00
00
00
00
00
00
00
00
00
MASS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
LB/IK HP-HR LB/IK HP-HR
CALCULABLE*"*
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
0.293
0.058
0.022
0.008
0.008
0.006
0.024
0.118
o.oio
0.004
0.002
0.003
0.004
0.025
0.002
0.003
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-o.ooo
0.010
0.004
0.002
0.003
0.004
0.025
0.002
0.003
CALCULABLE****
FUEL
USED
LAS.
2.86
0.72
9.30
3.45
0.87
17.197
CO
LB/IK
L8 FUEL
677.39
665.20
575.48
684.91
437.85
LTO CYCLE
CO
LB/IK
HOURS
9686.64
95788.94
64453.72
23629.47
5692.07
EMISSIONS
CO
EMISSION
HC
LB/IK
LBS. LB FUEL
1.937
0.479
5.150
2.161
0.381
10.510
0.611
21.92
13.99
14.10
22.09
45.21
HC
LB/IK
HOURS
311.47
2015.16
1578.95
762.07
587.70
MC
EMISSION
LBS.
0.061
0.010
0.111
0.076
0.019
0.319
0.019
NO
LB/IK
Lfl FUEL
1.57
5.09
6.97
1.60
1.15
NO
LB/IK
HOURS
22.44
733.46
780.09
55.10
14.99
NO
EMISSION
LBS.
0.0045
0.0017
0.0647
0.0053
0.0010
0.0794
0.0046
11-32
-------
0*1(1 4/S1/TI '
TCtT mCANIUTlONI TELIOTNt-COKTIMITU
ENGINE SUMLICKI TELEOVNC-COMTININTAl
ENGINE 0«T» »««««»»»»««»«»»»««o»»«»«t«««««««««««««»««««««»««««««»»«»«««««»»«««»«»»««««««««««»«»««»»»
t
C»L ID NUMBER! 21} ENGINE TY« MO MJOELt IO-S20-P UIIAL *MiM> ItMUl
IUTED MOISEPOHERI 100.
ENGINE TOTAL TINEl -0. MRS
FUFL: AV GAS loo/no FUEL H/C RATIO: i.e»o
OPERATIONAL DATA «o[[[
INLET AIR TEMPERATURE. DEGREES F: START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: START 28.60 FINISH -o.oo
INLET AIR HUMIDITY, CRN HJQ/LB AIR: 85.00
RELATIVE HUMIDITY: -O.CO PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00. FLOM RATE, LITERS/KIN: -0.00
SAMPLE LINE TRANSPORT TINf, SEC: -0.00
NUMBER OF TESTS: 10
COMMENTS:
COLO START 130 SEC
TAKI-IDLF LOU
TAKI-IOLE HIGH
RUN-UP
IAKE-UFF 100T
CLIMB-RICH
CLIMB-LEAN
APPROACH
TAXI-IOLf
HOT START
TESI
MODE
1
2
3
4
6
a
9
10
11
13
POKER
SHAFT PERCENT
HP RATED
0.0
1.60
4.60
23.50
263.CO
207.30
209.50
36.00
5.00
0.0
0
0
7
67
69
69
12
1
0
MEASURED
FUEL
FLOU
LB/HR
8.10
10.30
13.40
30.50
146.00
112.00
92.00
37.00
12.80
7.50
AIR FLQM
LB/HR
63.00
61.00
121.50
279.00
1561.50
1224.00
1210.50
360.00
117.00
63.00
CALCULATED
F/A
0.12657
0.12716
0.11029
0.10932
0.09350
0.09150
0.07600
0.10278
0.10940
0.11905
IESI
MODE
10
II
MHAUST EXHAUST
GAS GAS
TE"P PRESSURE
I1EGREES F PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
CO
(DRY)
PPMV
10000.00
54000.00
66500.00
66500.00
71500.00
57000.00
10000.00
83000.00
52000.00
66500.00
CO IHC
2 IKF.TI
(DRY I PPMV
PERCENT V
NO
IORYI
PPMV
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00
35000.00
22500.00
7500.00
33000.00
2300.00
2000.00
1500.00
3800.00
7500.00
37500.00
165.00
208.00
70.00
90.00
295.00
400.00
2625.00
115.00
75.00
80.00
NO
2
ICRYI
PPMV
-0.00
-0.00
-C.OO
-0.00
-0.00
-0.00
-C.OO
-0.00
-0.00
-0.00
IORYI
PPMV
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
-o.oo
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ThST
(DDE
R
9
10
II
13
MASS EMI
cn
LB/U
LB FUFL
74.54
4C6.90
574.05
57H.79
717.54
5R3.08
119. 98
764.78
452.27
514.03
MASS 6M1
HC
L6/1K
Lfl FUEL
195.25
126.53
46.76
207.04
16.13
14.25
12.16
24.92
47.03
221.22
MASS FM1
N02
LH/1K
LB FUEL
-0.00
-0.00
-0.00
-a. oo
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
MASS EMI
C02
Lfl/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
ND
IB/ IK
LB FUEL
2.02
2.57
C.99
1.29
4.86
6.72
51.73
1.74
1.07
1.06
MASS EMI
NOX
LB/IK
LR FUEL
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
L8/HR
0.60
4.19
7.69
17.65
104.7'.
65.31
11.04
28.30
5. 79
4.01
MASS EMI
HC
LB/HR
1.5B
1.30
0.61
6.31
2.36
1.60
1.12
0.92
0.60
1.66
MASS tMI
NO 2
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/MR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
MASS EMI
NO
LH/HB
0.02
0.0)
0.01
0.04
0.71
0. 75
4. 76
0.06
0.01
C.OI
MASS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TFST
MHOE
L8/1K HP-HP
L8MK HP-HR
L8/1K HP-Hrt
NO
LH/1K HP-Hi*
L3/IK HP-HR
Ull
X
LB/IK HP-HR
HORSJ-PQWCR-HR BASIS NOT CALCULABLE****
2 2.328 -0.000 0.724
.1 1.603 -0.000 0.131
4 0.751 -0.000 0.269
n 0.398 -0.000 0.009
» 0.315 -0.000 O.OOB
9 0.053 -0.000 0.005
10 0.745 -0.000 0.024
II I.158 -0.000 0.120
HORSFPOJER-HR BASIS NtlT CALCULABLE»«*«
0.015
0.003
0.00?
0.00)
0.004
0.023
0.002
0.003
-0.000
-o.oon
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
0.015
0.00)
0.002
O.OC3
0.004
0.023
0.002
0.003
LTU CYCLE EMISSIONS
TEST
HUGE
TIME IN MEASURED FUEL
MUOE FUEL FLOW USED
MIN. LB/HR LOS.
12. OT
0.30
5.00
6.00
4.00
13.40
146.00
112.00
37.00
12.BO
TOTAL FOR CYCLE
TOTU FOR CYCLE/LB FUEL
2.68
0.71
9.30
3.70
O.B6
I 7.264
CO
L8/IK
LS FUFL
CO
IB/IK
HOURS
574.05
717.54
583.08
764. 78
452.27
7692.21
104761.31
65305.21
2829<,.92
5789.10
1.538
0.524
5.420
2.830
0.388
10.700
0.620
CO HC
EMISSION LR/IK
LBS. LB FUEL
46.76
16.11
14.25
24.92
47.0!
HC
LB/IK
HOURS
626.52
2355.70
1595.59
922.05
601.96
HC
EMISSION
LBS.
0.125
0.012
0.132
0.092
0.040
0.402
0.023
NO
Lrt/IK
LB FUEL
0.99
4.86
6.72
I. 74
1.07
NO
LR/1H
HOURS
11.30
7 T.9. 9 7
752.75
64.40
13.71
NO
EMISSION
LBS.
0.0027
0.0035
0.0625
0.0064
0.0009
0.0760
-------
(UTEl 6/14/71
TEST OIGANimiONI TCLIDVNE-CONTINfNTAL
ENGINE SUPPLIER! TELtOYIW-CONTINENTAL
ENGINE DATA »«»«»»»«»»»««»»»«».«*»«»
CAL ID NUMBER: 216 ENGINE T»« AND KOOIL1 IO-520-P
RATED HOASEPOMEA1 100.
ENGINE TOTM. TINEI -0. MRS
FUEL I AV GAS 100/130 FUEL N/C RATIO! 1.140
OPERATIONAL DATA «»«««*»««««««««
SIIIAL
INLET AIR TENPERATUREi DEGREES Fl .START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE! START 2B.76 FINISH -0.00
INLET AIR HUMIDITY, CRN H20/LB AIR! 63.00
RELATIVE HUMIDITY! -0.00 PERCENT
SAMPLE LINE) TEMPERATURE. DEGREES Cl -0.00. FLOM RATE. LITERS/MINI
SAMPLE LINE TRANSPORT TINE. SEC: -0.00
NUMBER OF TESTS: 10
COMMENTS:
TEST POKER
MODE SHAFT PERCENT
HP RATED
COLD START » 130 SEC 1 0.0 0
TAII-IDLE LOU 2 1.70 0
TAXI-IDLE HIGH 3 4. 90 1
RUN-UP 4 23.70 7
TAKE-OFF lOOt 6 255.70 85
CLIMB-RICH B 201.60 67
CLIMB-LEAN 4 204.80 66
APPROACH 10 35.80 II
TAXI-IDLE 11 4.00 1
HOT START 13 0.0 0
TEST EXHAUST EXHAUST CO CO THC
MODE GAS GAS IDRV) 2 (MET)
TEMP PRESSURE PPNV IORY) PPNV
DEGREES F PSIA
1
2
3
4
6
a
9
10
11
13
TEST
NUDE
!
2
1
4
6
e
i
10
11
13
rest
MODE
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
MASS EMI MASS EMI
CO HC
LB/1K LB/IK
Id FUEL LB FUEL
442.21 234.41
607.60 236.32
714.92 145.81
642.93 46.02
55. 17 17.67
120.8} 16.09
712.77 12.60
994.87 58.91
791.59 273.44
62.54 264.78
cn
LB/1K HP-HR
HORSEPOUER-HR BASIS NOT
2
3
4
6
8
9
10
11
4.019
2.3H3
0.936
0.560
0.41B
0.320
1.195
2.612
.....HORSEPOuER-HR BASIS NOT
TEST
MODE
3
6
8
10
11
TOTAL FOR
TOTAL FOR
TIME IN MEASURED
NODE FUFL FLOM
MIN. LB/HR
12.00 16.00
0.30 150.00
5.00 117.00
6.00 43.00
4.00 13.30
CYCLE
CYCLE/LB FUEL
54000.00
67000.00
61000.00
76000.00
99000.00
76000.00
61300.00
116000.00
aaooo.oo
9000.00
MASS EMI
N02
LB/IK
Lfl FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
LB/IK HP-HR
MEASURED AIR FLOM CALCULATED
FUEL Lfl/HR F/A
FLOW
LB/HR
10. SO 90.00 0.11667
11.30 106.00 0.10463
16.00 146.50 0.10774
34.50 306.00 0.11275
150.00 1534.50 0.09775
117.00 1174.50 0.09962
92.00 1161.00 0.07924
43.00 387.00 O.IIIII
13.30 126.00 0.10356
6.70 63.00 0.13810
NO NO NO ALDEHYDES
IORYI 2 X
PPNV (DRY) (DRY)
PERCENT V
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
42500.00
36500.00
23000.00
7500.00
2600.00
2400.00
1600.00
9500.00
42500.00
50000.00
MASS EMI
NO
LB/IK
LB FUEL
1.21
1.34
1.52
1.74
2.54
3.89
39.96
1.13
1.60
1.32
THC
LA/ IK HP-HR
90.00
90.00
105.00
125.00
160.00
250.00
2100.00
80.00
108.00
116.00
MASS FMI
NOX
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
LB/IK
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
4.64
6.67
11.44
22.16
143.28
84.34
65.58
42. '«
10.53
0.54
NO
HP-HR
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/HK
2.67
2.67
2.33
1.59
2.65
i.ae
1.16
2.53
3.64
2.30
NU
2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
N02
Lfl/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
NO
X
PARTICULATES
-0
-0
-0
-0
-0
-0
-0
-0
-0
-0
MASS EMI
NO
LB/HR
0.01
0.02
0.02
0.06
0.38
0.46
3.66
0.05
0.02
0.01
.00
.00
.00
.00
.00
.00
.00
.00
.00
.00
MASS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
L8/1K HP-HR LB/IK MP-HR
CALCULABLE*"*
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
1.571
0.486
0.067
0.010
0.009
C.006
0.071
0.909
0.
0.
0.
009
005
003
0.001
0.
0.
0.
0.
002
018
001
005
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
0.009
0.005
0.003
0.001
0.002
0.01B
0.001
0.005
CALCULABLE**"
FUEL
USED
LBS.
1.20
0.75
9.71
4.30
0.89
18.832
CO
LB/IK
LB FUEL
714.92
955.17
720. SJ
994.87
791.59
LTD CYCLE
cn
LB/IK
HOURS
11438.64
143275.36
64337.63
42779.22
10528. 16
EMISSIONS
cn
EMISSION
LBS.
2.286
0.716
7.000
4.278
0.705
14.987
0.795
HC
LB/IK
LB FUFL
145.61
17.67
16. 09
58.91
273.44
HC
LB/IK
HOURS
2333.00
2650.84
1383.06
2533.01
3636.72
HC
EMISSION
LBS.
0.467
0.013
0.156
0.253
0.244
1.133
0.060
NO
LB/IK
LB FUEL
1.52
2.54
3.89
1.13
1.60
Ntl
LB/IK
HOURS
24.36
380.34
455.69
46.46
21.22
NO
EMISSION
LBS.
0.0049
0.0019
0.0378
0.0048
0.0014
0.0509
0.0027
11-34
-------
SUMMARY 0 470-R - CLIMB RICH MODE
MODEL SUMMARY
SIMPLE NUMBER
TEST
MODE
3
6
a
10
11
1TAL FOR
HAL FOR
MEAN:
SID OEV:
MEAN:
sro OEV:
MEAN:
STD DEV:
MEAN:
sro OEV:
MFAN:
SID DEv:
CYCLE
CYCLE/LB
MEASURED
FUEL FLOH
LB/HR
15.12
3.12
131.29
I .51
85.50
T.72
35.25
4.57
15.25
3.00
MEAN:
Sro OEV:
FUEL
FUEL
USED
LBS.
3.02
0.62
0.66
0.01
7.10
0.64
1.52
0.46
1.02
0.20
15.324
1.468
CO
L8/1K
LB FUEL
742.58
188.46
1155.89
9.12
691.66
132.09
618.22
73.52
559.42
48.88
CO
LB/1K
HOURS
11327.45
3621.09
151707.56
1834.17
58381.31
5097.82
21676.36
2611.55
8633.44
2359.03
MEAN:
STD DEVI
CO
EMISSION
LBS.
2.265
0.764
0.759
0.009
4.846
0.423
2.168
0.261
0.578
0.158
10.616
0.881
0.695
0.061
HC
LB/1K
LB FUEL
191.47
138.40
20.40
2.20
9.46
1.12
14.21
2.54
168.45
134.10
HC
LB/1K
HOURS
3054.25
2393.21
2678.52
298.41
ei3.ee
155.41
497.20
80.33
2841.40
2*69.20
HC
EMISSION
LBS.
0.6108
0.4786
0.0134
0.0015
0.0676
0.0129
0.0497
0.0080
0.1904
0.1654
0.932
0.659
0.058
0.038
NO
L8/IK
LB FUEL
1.02
0.43
LIT
0.23
9.37
7.79
2.42
1.51
0.96
0.40
NO
LB/IK
HOURS
15.97
8.54
145.95
32.34
756.17
535.33
90.40
70.51
15.21
8. 68
NO
EMISSION
IBS.
0.0032
0.0017
0.0007
0.0002
0.0628
0.0444
0.0090
0.0071
0.0010
0.0006
0.0767
0.0397
0.0052
0.0033
SUMMARY IO-520-P - CLIMB RICH MODE
MODEL SUMMARY
SAMPLE NUMBER
TESI
.10DF
3
6
e
10
11
1! »L FOR
ITAL FOR
MEAN:
STf) DEV:
HFAN:
sro OEV:
MEAN:
srn OEV:
MFAN:
srn OEV:
HE AN:
srn OEV:
CYCLE
CYCLE/IB
MEASURER
FUEL FLOW
LB/HH
15.80
1.96
149.20
4.15
11 7. 40
5.51
41.30
5.29
13.58
0.78
MEAN:
sro DEV:
FUFl
FUEL
USED
LSS.
3.16
0. 39
0.75
0.02
9.74
0.46
4. 13
0.53
0.91
0.05
IB. 690
1.424
CO
LB/1K
LB FUEL
562.15
138.81
809.26
116.76
728.44
151.72
889.97
153.44
502.07
162.66
CO
LB/1K
HOURS
8739.86
17B5.97
121043.94
19927.34
86184.69
21853.98
37389.69
10650.04
678K.50
2095.45
«EAN:
srn OEV:
CO
EMISSION
LBS.
1.748
0.357
0.605
0.100
7.143
1.814
3.739
1.065
0.455
0.140
13.700
2.869
0. J27
0. 102
HC
LO/1K
LB FUEL
118.84
103.20
16.24
1.36
15.06
0.88
35.70
25.55
174.07
120.25
HC
L6/1K
HOURS
2348.11
1887.36
2426.70
254.14
1770.82
169.37
1511.39
1198.83
2415.59
1699.98
HC
EMISSION
LBS.
0.4696
0.3775
0.0121
0.0013
0.1470
0.0141
0.1511
0.1199
0. 1618
C.1119
0.942
0.552
0.049
0.026
MO
LB/IK
L8 FUEL
1.47
0.50
3.84
1.09
4.63
2.08
1.28
0.40
1.1H
0.31
NO
LU/1K
HOURS
21.71
10.21
570. 19
148.90
534.59
217.15
51.21
11.04
15.90
3.99
NO
EMISSION
LBS.
0.0047
0.0020
0.0029
0.0007
0.0444
0.0180
0.0051
0.0011
0.0011
0.0001
0.0582
0.0183
0.0032
0.0012
H-35
-------
umti »/</*!
TEST ORGANKATIOMI TELEDYNE-CONTINENTIL
ENGINE SUPPLIERI TELBDYNE-COPJTINENTAL
ENGINE 0»T» *»»»»«»«»»
***»****
CAL ID NUNBEAI 220 ENGINE TYPE AND NODE LI 0-4TO-* IH
RATED HORSEPOMERI 230.
ENGINE TOTAL TINEI -0. HRS
FUELl AV GAS 80/87 FUEL H/C RATIOI 1.8*0
OPERATIONAL DATA *****«**'
INLET AIR TEMPERATURE. DEGREES Ft START -0.00 FINISH -0.00
ATMOSPHERIC PRESSURE: START 28.93 FINISH -0.00
INLET AIR HUMIDITY, CRN H20/LB AIRt 114.00
RELATIVE HUMIDITY! -0.00 PERCENT
SAMPLE LINEI TEMPERATURE. DEGREES C! -0.00. FLOM RATE. LITERS/KIN! -0.00
SAMPLE LINE TRANSPORT TIME. SECl -0.00
NUMBER OF TESTS: 5
COMMENTSl
> «r»-«-iiuou
***
COLD START » 1)0 SEC
TAXI-IDLF LOW
TAXI-IDLE HIGH
RUN-UP
TAKE-OFF mot
TEST
MODE
POHER
SHAFT PERCENT
HP RATED
0.0
1.90
5.00
24. 00
189.60
0
0
2
10
82
MEASURED
FUEL
FIOM
LB/HR
7.80
8.30
13.00
21.50
130.00
AIR FLOM
LB/HR
T2.00
81.00
117.00
261.00
1318.90
CALCULATED
F/A
0.10833
0.102*7
0.11111
0.08238
0.09860
TEST
MODE
1
2
3
4
6
EXHAUST
GAS
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
EXHAUST CO
GAS IDRYI
PRESSURE PPNV
PSU
-0.00
-0.00
-0.00
-0.00
-0.00
49000.00
31000.00
69000.00
78000.00
122000.00
CO
2
IDRYI
PERCENT
-0.00
-0.00
-0.00
-0.00
-0.00
THC
IHETI
PPMV
V
23500.00
20000.00
2700.00
2000.00
2100.00
NO
IDRVI
PPMV
73.00
69.00
80.00
145.00
100.50
NO
2
I DRV)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
NO
I
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
MASS EMI
CO
LB/IK
IB FUEL
427.20
284.51
587.51
ade.45
1150.60
MASS EMI
HC
IB/ IK
IB FUEL
148.40
111.44
16.74
15.34
16.89
MASS EMI
N02
LB/1K
L8 FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NO
LB/IK
LB FUEL
1.05
1.04
1.12
2.65
1.57
MASS EMI
N0>
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/HR
3.33
2.36
7.64
18.67
150.75
MASS EMI
KC
LB/HR
1.16
1.09
0.22
0.33
2.20
MASS EMI
NO 2
IB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NO
LB/HR
0.01
0.01
0.01
0.06
0.20
MASS EMI
NOX
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
NODE
CO
LB/IK HP-HR
LB/IK HP-HR
R-H" BASIS NOT CALCULABLE****
1.243 -0.000
1.528 -0.000
0.778 -0.000
0.795 -0.000
THC
LB/IK HP-HR
0.574
0.044
0.014
0.012
NO
LB/IK HP-HR
0.005
0.003
0.002
0.001
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
0.005
0.003
0.002
0.001
11-36
-------
TABLE IE
AUXILIARY POWER UNITS
AIRESEARCH MFG.
CONTENTS:
111-2 TO 111-54 INDIVIDUAL ENGINE RUNS - MASS EMISSION CONVERSIONS
ONLY (INCLUDES AIR HORSEPOWER CALCULATED DATA)
III-l
-------
DATE: 5/17/Ti
TEST ORGANIZATION: AIRESEARCH
ENGINE SUPPLIER: AIRESEARCH
ENGINE DATA «««»««.
CAL 10 NUMBER: 35 ENGINE TYPE AND KODEL: GTCP30-92
RATED SHAFT HORSEPOWER: 40.
ENGINE TOTAL TIME:
TIME SINCE HOT SECTION OVERHAUL:
TIME SINCE:
SERIAL NUMBER:
0. HRS
0. HRS
NI COMPRESSOR OVERHAUL: o. HRS
NZ COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: o. HRS
FUEL H/C RATIO: 1.928
FINISH
FINISH
95.00
28.56
FUEL: AV HERDS
OPERATIONAL DATA «»*«»«
INLET AIR TEMPERATURE, DEGREES F: START 95.00
ATMOSPHERIC PRESSURE: START 2B.56
INLET AIR HUMIDITYt LBS H20/LB AIR: 0.0012
RELATIVE HUMIDITY: 5.00 PERCENT
SAMPLE LINE: TEMPERATUREi DEGREES C: -0.00. FLOW RATE, LITERS/MIN:
SANPLF LINE TRANSPORT TIMF, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
SHP LOADING ONLY
-o.oo
TEST
MODE
I/ 0
6/ 1
ll/ 6
16/11
20/16
POWER
PERCENT
RATED
SHP
0
75
50
76
101
POWER
PERCENT
RATEO
SHP
0
25
50
76
101
POWER
PERCENT
RATEO
SHP
SHAFT
HP
0.0
10.20
20.30
30.50
40.70
EXHAUST
GAS
TEMP
OEGREFS F
640.00
675.00
710.00
745.00
795.00
MASS EMI
CO
LB/1K
LB FUEL
37.14
27.47
21.65
17.49
14.30
CO
LB/1K
.....HORSEPOWER-HP
25
50
76
101
100.
43.
24.
16.
POWER
AIR
HP
0.0
0.0
0.0
0.0
0.0
EXHAUST
GAS
ENGINE CORRECTEC
SPEED FUEL
RPM FLOW
NI N2 LB/HR
59200.00 -0.00 35.40
59200.00 -0.00 37.40
59100.00 -0.00 40.40
59100.00 -0.00 43.40
59100.00 -0.00 47.40
CO CO
1 WETI
THC
2 (WFTI
PRESSURE PPMV (WET) PPMV
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
3.37
1.44
0.75
0.50
0.32
HP-HR
BASIS NOT
738
083
892
654
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
NO
I WETI
PPMV
PERCENT V
331.40 1.
266.30 1.
224.50 2.
193.00 2.
170.30 2.
MASS EMI MASS EMI
N02 C02
LB/IK LB/1K
IB FUEL LB FUEL
-0.00 3030.00
-0.00 3050.00
-0.00 3050.00
-0.00 3060.00
-0.00 3060.00
CO
2
LR/1K HP-HR Lfl/1
CALCULABLE*****
11183.374
6069.949
4354.227
3563.733
72 52.60
88 24.50
02 13.50
15 9.70
32 6.60
7.70
9.20
11.30
14.00
16.30
MASS EMI MASS FMI MASS
Nfl
LB/IK
NOX CO
F/A COMPRESSOR COMPRESSOR
CALC INLET DISCHARGE
FRdM TEMP PRESSURE
FMISS10NS DEGREES f PSIA
O.OCB600 83.00 J9.30
0.009300 96.00 39.10
0.009900 100.00 39.40
0.010600 96.00 39.60
0.011400 98
NO NO
2 X
iwfTi iHcri
PPMV PPMV
5.10 12. 7n
5.10 14. 30
5.00 16.30
5.20 19.20
5.30 71.60
.00 39.70
ALOFHYDFS SMOKE
-o.nn -o.oo
-n.no -o.no
-o.oo -o.oo
-n.oo -o.no
-o.oo -o.oo
EMI MASS EMI MASS EMI MASS FMI MASS
HC
LB/IK LB/HR LB/HR
Nfl2 CII7 NO
BLEED
FLOW
L3/MIN
0.0
0.0
0.0
0.0
0.0
PART1CUL ATFS
-o.no
-0.00
-0.00
-0.00
-0.00
FMI M^SS EMI
NOX
LB/HP LB/HR Lfl/HM LH/HR
LB FUEL LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
THC
K HP-HR
5.298
1.485
0.713
0.370
2.34 1.
7.43 1.
7.58 0.
7.86 0.
2.98 0.
NO
Lfl/IK HP-HR
-0.000
-0.000
-0.000
-0.000
31 0.12
03 0.05
87 0.03
76 0.07
68 0.0?
NO
2
IB/IK HP-HR
-0.000
-0.000
-n.ooo
-0.000
-0.00 107.26 -0.
-0.00 114.07 -0.
-0.00 123.22 -0.
-0.00 137.80 -0.
-0.00 145.04 -0.
NO
X
LB/IK HP-MR
8.903
5.1J1
4. 064
3.469
30 0.08
no 0.09
on o.io
00 0.12
no 0.14
III-2
-------
DATE! 5/17/71
TEST ORGANIZATION: AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE DATA ««»««
CAL ID NUMBER! 80 ENGINE TYPE AND MODEL! GTCP30-92
RATED SHAFT HORSEPOWER: 40.
ENGINE TOTAL TIME! 0. HRS
TIME SINCE HOT SECTION OVERHAUL! 0. HRS
TIME SINCE!
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.928
^t*****
SERIAL NUMBER: P-28794
FINISH
FINISH
98.00
FUEL: AV KEROS
OPERATIONAL DATA «««««
INLET AIR TEMPERATURE, DEGREES F: START 98.00
ATMOSPHERIC PRESSURE: START 28.56
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0012
RELATIVE HUMIDITY: 5.00 PERCENT
SANPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/BIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
COMBINATION SHP/BLEED LOADING
TEST
NODE
22/ 0
19/22
15/19
10/15
5/10
POWER
PERCENT
RATED
SHP
101
75
50
25
0
POWER
PERCENT
DATED
SHP
101
75
50
25
0
POKED
PERCENT
RATF.O
SHP
101
75
50
25
0
SHAFT
HP
40.40
30.40
20.10
10.20
0.0
EXHAUST
GAS
TEMP
DEGREES F
1MB. 00
1320.00
1320.00
1320.00
1320.00
MASS EMI
CO
LB/IK
LB FUEL
5.04
5.32
5.35
5.91
6.14
CO
LB/IK
5.
6.
7.
10.
13.
POMER
AIR
HP
24.30
25.7*
27.00
27.79
28.62
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/U
LB FUEL
0.13
0.13
0.10
0.10
0.09
ENGINE
Nl
58900.
58900.
59000.
59000.
59000.
SPEED
RPM
00
00
00
00
00
CO
(UETI
PPHV
107.
111.
111.
121.
123.
MASS EMI
N02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
MP-HR LB/IK HP-K
361
5<><>
636
195
738
3210.677
3712.036
4309.762
5206.340
6752.922
00
50
50
30
90
MASS
C
N2
-0.00
-0.00
-0.00
-0.00
-o.oo
en
2
(WET!
PERCENT
4.07
4.02
4.00
3.94
3.88
CORRECTED
FUEL
FLOW
LB/HR
69.00
69.00
67.50
65.50
64.00
THC
(WET)
PPNV
V
4.90
4.90
3.80
3.50
3.20
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
NO
(WET)
PPMV
41.80
40.40
39.20
37.60
36.00
EMI MASS EMI MASS EMI MASS
02
LB/IK
LB
3020
3020
3020
3020
NO
LB/IK
NOX C
F/A COMPRESSOR
CALC INLET
FROM TEMP
EMISSIONS DEGREES f
0.020100 97.00
0.019900 98.00
0.019800 99.00
0.019500 98.00
0.019100 98.00
COMPRESSOR
DISCHARGE
PRESSURE
PSIA
37.00
36.40
35.80
35.10
34.70
NO NU ALOEHVOES SMOKE
2 X
(UETI (HET)
PPMV PPMV
4.10 45.90 -0
3.90 44.30 -0
1.50 42.70 -0
3.70 41.30 -0
4.30 40.30 -0
EMI MASS EMI MASS EMI
0 HC N02
LB/IK LB/HB LB/HR LB/HR
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
BLFED
FLOW
LB/MIN
25.51
27.52
29.43
31.13
32.54
OARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
MASS Ell MASS EMI MASS
CO 2
LB/HH
NO NO
EMI
X
LB/HR LB/HR
FUEL LR FUEL LB FUEL
.00
.00
.00
.00
3020.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
at
LB/IK
0.
0.
0.
0.
0.
HP-HR
141
163
150
171
201
3.55 0
3.47 0
3.36 0
3.31 0
3. 28 0
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
.35 0.01 -0.00
.37 0.01 -0.00
.36 0.01 -0.00
.39 0.01 -0.00
.19 0.01 -0.00
NO
2
208.38
208.38
203.85
197.81
191.23
NO
X
-0.00 0.
-0.00 0.
-0.00 0.
-0.00 0.
-0.00 0.
25
24
23
22
21
LR/1K HP-HR L8/IK HP-HO
-0.000
-0.000
-0.000
-0.000
-0.000
3.777
4.270
4.802
5.705
7.339
III-3
-------
DATE* S/1B/T1
TEST OtSANUAUOJtl A1RESEARCH
F.NCI WE SUPPLIER! AIREJEAACH '.
EN6INE DATA »»»»»»»«»»»»»««»»»««*»«*«»
C»L 10 NUMURI lil ENGINE TYPE MO KOOILI CTCPIO-*2 SERIAL NUMEkl' P-2«T»4
RATED SHAFT HORSEPOWER! 40.
0. MRS
0. HIS
ENGINE TOTAL TINEl
TINE SINCE HOT SECTION OVERHAUL!
TINE SINCEl
Nl COMPRESSOR OVERHAUL! 0. MRS
NZ COMPRESSOR OVERHAUll 0. HRS
COMSUSTOR CAN REPLACENENTl 0. HRS
FIRST STAGE NOZILE GUIDE VANE OVERHAUL! 0. HRS
Nl TURBINE OVERHAUL! 0. HRS
NZ TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIOl 1.92)
FINISH
FINISH
85.00
28.8*
FUILI AV KEROS
OPERATIONAL DATA »«««««»
INLET AIR TENPERATUREt DEGREES Fl START 85.00
ATMOSPHERIC PRESSURE: START 28.8*
INLET AIR HUMIDITY. LBS H20/LB AIR> 0.0020
RELATIVE HUMIDITY! 15.00 PERCENT
SAMPLE LINEl TEMPERATURE. DEGREES Cl -0.00, FLOW RATE. LITERS/MINI
SAMPLE LINE TRANSPORT TIME. SECi -0.00
NUMBER OF TESTS! 5
COMMENTS:
SHP LOADING ONLY
TEST
MODE
I/ 0
6/ 1
III 6
16/11
20/16
POKER
SHAFT
HP
0.0
10.20
20.40
90.50
40.60
AIR
HP
0.0
0.0
0.0
0.0
0.0
ENGINE
SPEED
RPM
Nl N2
59200.00 -0
59200.00 -0.
59200.00 -0.
59000.00 -0.
58900.00 -0,
CORRECTED
FUEL
FLOW
LB/HR
36.40
19.40
42.40
46.40
50.30
GAS GEN
AIR FLOW
LB/SK
-0.00
-0.00
-0.00
-0.00
-0.00
F/A COMPRESSOR
CALC INLET
FROM TEMP
EMISSIONS DEGREES F
0.008600
0.009400
0.009900
0.010300
0.010900
82.00
85.00
85.00
93.00
88.00
COMPRESSOR BLEED
DISCHARGE FLOH
PRESSURE LB/MIN
PSIA
40.20
40.20
40.30
40.50
40.50
0.0
0.0
0.0
0.0
0.0
POKED EXHAUST
PERCENT GAS
RATED TEMP
SHP DEGREES F
0
25
50
76
101
610.00
650.00
695.00
765.00
050.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-o.oo
-o.oo
-o.oo
CO
(MET)
PPMY
234.50
257.10
271.40
309.50
332.80
CO
2
I MET)
PERCENT V
1.74
1.90
2.01
2.08
2.20
THC
IUETI
PPMY
7.30
5.30
5.60
7.10
6.50
NO
IWETI
PPMV
12.00
13.10
14.00
15. 90
16.60
NO
2
(MET)
PPMV
7.20
7.60
8.00
B.60
9.60
NO
X
(MET)
PPMV
19.20
20.80
22.10
24.50
26.20
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICIPATES
-0.00
-0.00
-0.00
-0.00
-0.00
POKED
PERCENT
RATED
SHP
0
25
50
76
101
MASS EMI
CO
LB/IK
LB FUEL
26.19
26.25
26.21
28.87
29.22
MASS EMI
HC
LB/IK
LB FUEL
0.47
0.31
0.31
0.38
0.33
MASS EMI
N02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/IK
LB FUEL
3060.00
3050.00
3050.00
3040.00
3040.00
MASS EMI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/IK
LB FUEL
3.52
3.48
3.50
3.76
3.78
MASS EMI
CO
LB/HR
0.95
1.03
1.11
1.34
1.47
MASS EMI
HC
LB/HR
0.02
0.01
0.01
0.02
0.02
MASS EM
ND2
IB/MR
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/HR
111.38
120.17
129.32
141.06
152.91
MASS EMI
NO
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/HR
0.13
0.14
0.15
0.17
0.19
POWER CO
PERCENT
RATED IB/IK HP-HR
SHP
LB/IK HP-HR
HORSEPOWER-HR BASIS NOT CALCULABLE*""
25 101.409 11781.367
50 54.4B4 6339.211
76 43.922 4624.785
101 36.199 3766.305
THC
LB/IK HP-HR
1.186
0.640
0.572
0.408
NO
LB/IK HP-MR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
13.454
7.279
5.719
4.688
111-4
-------
OATfl 5/18/71
TEST ORGANIZATION: AIRESEARCH
ENGINE SUPPIIERI AIRESEARCH
ENGINE D»T» »»»*«««»»*»»«»«»
CAL 10 NUMBER! 86 ENGINE TYPE AND MODEL: GTCP3O-92
RATED SHAFT HORSEPOWER! 40.
ENGINE TOTAL TINE:
TINE SINCE HOT SECTION OVERHAUL:
TINE SINCE:
SERIAL NUMBER:
P-Z8794
0. HRS
0. HRS
HI COMPRESSOR OVERHAUL: 0. HRS
N2 CONPRESSOR OVERHAUL: 0. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N; TURBINE OVERHAUL: o. HRS
FUEL H/C RATIO: 1.928
FINISH
FINISH
93.00
28.84
FUEL: AV KERns
OPERATIONAL DATA «»«»
INLET AIR TEMPERATURE. DEGREES F: START 9).00
ATMOSPHERIC PRESSURE: START 28.84
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0020
RELATIVE HUMIDITY: 15.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 0.0 , FLOW RATE, LITERS/KIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.0
NUMBER OF TESTS: 5
COMMENTS:
COMBINATION SHP/BLEED LOADING
22/ 0
19/22
IS/19
10/15
5/10
POWFR
SHAFT AIR
HP HP
40.30
30.30
20.20
10.10
0.0
19. 65
22.92
25.56
28.14
29.15
ENGINE
SPEED
RPM
Nl
58600.00
58600.00
58600.00
58600.00
59600.00
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CORRECTED
FUEL
FLOW
LB/HR
68.00
68.00
67.00
67.00
66.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
CALC
FROM
EMISSIONS
0.015700
0.015900
0.017100
0.017700
0.017900
COMPRESSOR
INLET
TEMP
DEGREES F
89.00
91.00
95.00
96.00
95.00
COMPRESSOR BLEED
DISCHARGE FLOW
PRESSURE LR/HIN
PSIA
IS. 30
37.40
36.50
35.70
35.10
20.07
24.00
77.39
30.95
32.82
POWER EXHAUST
PERCENT GAS
RATED TEMP
SHP DEGREES F
100
75
50
25
0
1315.00
1320.00
1120.00
1)35.00
1330.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
CO
I WET)
PPMV
341.20
345.40
342.30
346.80
341.10
CO THC
2 (MET)
IWET) PPHV
PERCENT V
3.17
3.21
3.44
3.56
3.60
3.10
2.60
I.00
1.50
1.00
NO
IWETI
PPMV
28.90
29.50
31.60
34.50
35.30
NO
2
(WET)
PPMV
9.90
9.20
8.90
9.30
9.40
ALDEHYDES SMPKE PASTICULATFS
IWET)
PPMV
3B.flO
38.70
40.50
43.10
44.70
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-o.oo
POWER
PERCENT
RATED
SHP
100
75
50
25
0
MASS EMI
CO
LB/IK
LB FUEL
20.70
20.67
19.09
18. 65
18.15
MASS EMI
MC
LB/IK
LB FUEL
0.11
0.09
0.06
0.05
0.03
MASS EMI
N02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0,00
-0.00
MASS EMI
C02
LB/IK
L8 FUEL
3020.00
3020.00
3010.00
3010.00
3010.00
MASS EM|
NO
IB/ IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/IK
LB FUEL
3.87
3. OS
3.71
3.86
3.90
MASS EM
cn
LB/HR
.41
.41
.29
.25
.20
MASS EMI
HC
Lfl/HB
MASS EMI
NO 2
IB/MR
MASS EMI
C'l?
LB/HH
MASS EMI
NO
L8/H»
ASS FHI
NHX
LR/HR
0.01
0.01
0.00
0.00
0.00
-0.00
-0.00
-0.00
-0.00
-0.00
205.36
205.36
201.67
201. >>7
lift.66
-0.00
-0.00
-0.00
-0.00
-0.00
0.26
0.21
0.25
0.26
0.26
POWFR
PFRCENT
RATED
SHP
100
75
50
25
0
CO
LB/IK HP-MR
23.477
26.418
27.944
32.681
41.092
LP./IK HP-HR
3425.472
3858.880
4406.688
5273.629
6816.168
THC
LB/IK HP-HR
0.121
O.I I?
0.085
0.061
0.070
NO
LO/1K HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
-0.000
-0.000
-0.000
-o.ooo
-0.000
MO
t
LR/1K HP-HR
4.38B
3.916
5.429
6.777
8. 814
III-5
-------
DATE! 5/14/T1
TEST OR GAD HAT I ON I AIRCSEARCH
ENGINE SUPPLIER! AIRISEAACH
ENGINE DATA ^^^^^A***********
i
CAL ID HUNBERl. 14 ENGINE TYPf AND MODEL I GTCPI4-4 SERIAL NUMBERI P-»44«6
RATED SHAFT HORSEPOWER! 160.
0. N1S
0. HRS
ENGINE TOTAL TINEI
TINE SINCE HOT SECTION OVERHAUL!
TINE SINCE I
Nl COMPRESSOR OVERHAUL! 0. HRS
12 COMPRESSOR OVERHAULl 0. HRS
CONBUSTOR CAN REPLACEMENT! 0. KRS
FIP.ST STAGE NOIUE GUIDE VANE OVERHAULl 0. HIS
Nl TURBINE OVERHAUL I 0. HRS
HZ TURBINE OVERHAULl 0. HRS
FUEL H/C RATI01 1.677
FINISH
FINISH
98.00
28.6!
FUEL I JP-1
OPERATIONAL DATA ««««
INLET AIR TEMPERATURE. DEGREES Ft START 91.00
ATMOSPHERIC PRESSUREl START 26.65
INLET AIR HUMIDITY. LBS H20/LB AIRI 0.0050
RELATIVE HUMIDITY! 14.00 PERCENT
SAMPLE LINE! TEMPERATURE. DEGREES Cl -0.00. FLOW RATE. LITERS/MINI
SAMPLE LINE TRANSPORT TIME. SECl -0.00
NUMBER OF TESTS! )
COMMENTS:
SHP LOADING ONLY
TEST
NODE
I/ 0
6/ 1
ll/ 6
POWER
PERCENT
RATED
SHP
0
25
33
POWER
PERCENT
RATED
SHP
0
J5
33
POWER
PERCENT
RATED
SHP
SHAFT
HP
POWER
AIR
HP
0.0 0.0
41.00 0.0
53. TO 0.0
EXHAUST
GAS
TEMP
DEGREES F
600.00
715.00
750.00
MASS EMI
CO
LB/IK
LB FUFL
18.79
20.56
20.15
CO
LB/1K
HORSEPOWER-HR
25 34.
33 35.
ENGINE
SPEED
RPM
Nl
59200.00
59100.00
59000.00
EXHAUST CO
GAS I VET)
PRESSURE PPHV
PS1»
-o.oo
-0.00
-0.00
MASS EM]
HC
L6/IK
LB FUEL
1.05
0.86
0.77
HP-MR
BASIS NOT
250
311
1*5.60
206.50
218.80
N2
-0
-0
-0
.00
.00
.00
CO
2
(WETI
PERCENT
MASS EMI MASS EMI
N02 C02
LB/IK LB/1K
LB FUEL LB FUEL
-0.00 3090.
-0.00 3070.
-0.00 3070.
CO
2
Lfl/U HP-HB
CALCULABLE**"*
5114.164
5379.641
00
00
00
1.52
1.96
2.12
CORRECTED
FUEL
FLOW
LB/HR
64.50
68.30
94.10
TKC
IWETI
PPMV
V
14.20
15.20
14.60
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
NO
IWET)
PPNV
11.30
18.90
20.20
F/A
CALC
FROM
EMISSIONS
0.007400
0.009600
0.010400
NO
2
IWETI
PPMV
6. BO
10.30
12.10
COMPRESSOR
INLET
TEMP
DEGREES F
98.00
98.00
98.00
COMPRESSOR
DISCHARGE
PRESSURE
PSIA
53.00
53.20
53.20
NO 4LOEMYOES SMOKE
X
IWET)
PPMV
18.10
29.20
32.30
-0.00 -0.00
-o.no -o.oo
-0.00 -0.00
BLEED
FLOW
LR/MIN
0.0
0.0
0.0
PART ICUl «TES
-0.00
-0.00
-0.00
MASS EMI M«SS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI
NO NOX CO HC N02 CD? NO NOX
LB/1K LB/1K LB/HR LB/HR LB/KR LB/HR LB/HR LB/HR
LB FUEL LB FUEL
-0.00
-0.00
-0.00
IMC
LB/U HP-HR
1.
1.
438
346
3.84 1
4.77 I
4.89 1
NO
LB/U MP-HR
-0.000
-0.000
.21 0.
.40 0.
.90 0.
LB/IK
-0
-0
07 -0.00
06 -0.00
07 -0.00
NO
2
HP-MR
.000
.000
199.30 -0.
209.68 -0.
288.89 -0.
NO
X
LB/1K HP-HR
7.954
8.565
00 0.25
00 0.51
00 0.46
III-6
-------
DiTE! 3/14/71
TEST ORGANIZATION! »IRESE»RCH
ENGINE SUPPLIER! AIRCSEARCH
ENGINE DAT* ««»««»««»««
CAL ID NUNBERI 81 ENGINE TYPE AND MODEL: GTCP36-6
RATED SHAFT HDRSEPOMER: ISO.
ENGINE TOTAL TINE:
TIME SINCE HOT SECTION OVERHAUL:
TIME SINCE:
SERIAL NUMBER:
0. MRS
0. MRS
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL! 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOIZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.S77
FINISH 101.00
FINISH 28.65
FUEL: JP-S
OPERATIONAL DATA ««««««««««
INLET AIR TENPERATUREi DEGREES F: START 101.00
ATMOSPHERIC PRESSURE: START 20.65
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0050
RELATIVE HUMIDITY: 14.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN:
SAMPLE. LINE TRANSPORT TIME, SFC: -0.00
NUMBER OF TESTS: 3
COMMENTS:
COMBINATION SHP/BLEEO LOADING
TEST
MODE
15/ 0
10/15
5/10
POWER
PERCENT
RATED
SHP
56
25
0
POWER
PERCENT
HATED
SHP
56
25
0
POWER
PERCENT
RATED
SHP
S6
25
0
POWER ENGINE CORRECTED
SHAFT AIR SPEED FUEL
HP HP RPH FLOW
Nl N2 LB/HR
41.10 56.30 58400.00 -0.00 144. 40
40.60 73.93 58600.00 -0.00 137.00
0.0 96.41 59900.00 -0.00 123.90
EXHAUST EXHAUST CO CO THC
GAS GAS (UETI 2 IWETI
TEMP PRESSURE PPMV (WET) PPMV
DEGREES f PSIA PERCENT V
1200.00 -0.00 243.30 3.79 3.90
1195.00 -0.00 291.90 3.58 7.20
1IT5.00 -0.00 259.00 3.65 9.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
NO
I WETI
PPMV
47.50
40.90
41.30
F/A COMPRESSOR
CALC INLET
FROM TEMP
EMISSIONS DEGREES F
O.OIBTOO 100.00
0.017600 101.00
0.016000 102.00
COMPRESSOR
DISCHARGE
PRESSURE
PSIA
50. 10
47.00
44.30
NO Nl) ALDEHYDES SMOKE
2 X
IWF.T) IkFT)
PPMV PPMV
12.20 59. 7P -0
13.40 54.30 -0
12.60 53.90 -0
MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS FHI MASS EMI MASS FMI
CO HC N02 C02 NO NOX CO HC Nf)2
LB/IK LB/IK LB/1K LB/IK LB/IK LB/IK LB/HR L8/HR IB/HH
LB FUEL 18 FUEL LB FUEL LB FUEL LB FUEL LB FUEL
12.38 0.11 -0.00 3030.00 -0.00
15.72 0.22 -0.00 3030.00 -0.00
13.68 0.27 -0.00 3030.00 -0.00
CO CO THC
2
LB/IK HP-HR LB/IK HP-HH IB/IK MP-HH
12.540 3069.376 0.115
18. BIO 3624.527 0.266
17.586 3694.060 0.348
4.98 1
4.81 2
4.61 1
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
.65 0.0? -0.00
.15 0.03 -0.00
.70 0.03 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
BLEED
FLOW
LB/MIN
42.35
59.04
61.70
PARTICULATES
-0.00
-o.oo
-0.00
"ASS F.MI MASS 6"! MASS EMI
C02 ND NOX
LB/HS Lfl/HP. LB/HR
452.66
415.11
375.4?
-0.00 0.74
-0.00 0.66
-0.00 0.56
NO NO
? X
Lfl/lK HP-HR LK/1K HP-HR
-0.000
-0.000
-0.000
5.050
5.749
r>.OI >
III-7
-------
IMfEl 5/14/Tl
TEIT ORGAN11ATIONI A(RESEARCH
ENGINE SUPPHERl AIRCIEAACM
ENGINE OAT* **»*****»«***»**»»****»»****************
C»L 10 NUNBERI IT ENGINE TTM AND MODEL I GTCPM-* SERIAL NIMBEm P-»«TTI
RATED SHAFT HORSEPOWER! 160.
ENGINE TOTAL TIKEI , 0. MRS
TINE SINCE HOT SECTION OVERHAUL! 0. HIS
TINE SINCE!
Nl COMPRESSOR OVERHAULl
N2 COMPRESSOR OVERHAULl
CONBUSTOR CAN REPLACENENTl
FIRST STAGE NOZZLE GUIDE VANE OVERHAULl
Nl TURBINE OVERHAULl
N2 TURBINE OVERHAULl
FUEL H/C RATIOl 1.877
0. HRS
0. HRS
0. HRS
0. HRS
0. HRS
0. HRS
FINISH
FINISH
B7.00
28.70
FUELl JP-5
OPERATIONAL DATA *«»
INLET AIR TENPERATURE. DEGREES Fi START ST.00
ATMOSPHERIC PRESSURE: START 28.70
INLET AIR HUMIDITY, LBS H20/LB AIRI 0.0048
RELATIVE HUNIOITYi 17.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES Cl -0.00, FLOW RATE, LITERS/MINI -0.00
SAMPLE LINE TRANSPORT TIME, SECl -0.00
NUMBER OF TESTSl 5
COMMENTS:
SHP LOADING ONLY
TEST
MODE
I/ 0
6/ 1
lit 6
16/11
20/16
POKER
SHAFT AIR
HP HP
0.0
39.50
T8.70
114.00
118.70
0.0
0.0
0.0
0.0
0.0
ENGINE
SPEED
RPM
Nl N2
29100.00
98900.00
58600.00
58500.00
28100.00
-0.00
-0.00
-0.00
-0.00
-0.00
CORRECTED
FUEL
FLOW
LB/HR
72.60
90.60
109.60
128.70
132.90
GAS GEN
AIR FLOW
L8/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
F/A COMPRESSOR
CALC INLET
FROM TEMP
EMISSIONS DEGREES F
0.008000
0.010100
0.012200
0.014300
0.015000
84.00
86.00
88.00
89.00
90.00
COMPRESSOR
DISCHARGE
PRESSURE
PSIA
52.90
53.40
54.40
54.40
54.10
BLEED
FLOW
LB/NIN
0.0
0.0
0.0
0.0
0.0
POKER
PERCENT
RATED
SHP
0
24
49
71
74
EXHAUST
GAS
TEMP
DEGREES F
540. 00
6)5.00
740.00
860.00
905.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
CO
I WET I
PPMV
114.10
130.10
1)0.70
122.80
120.20
CO
2
I MET I
PERCENT V
1.63
2.06
2.50
2.93
3.07
THC
(MET)
PPMV
3.50
1.80
1.40
0.50
0.30
NO
IUET)
PPMV
16.00
21.10
27.40
37.60
41.40
NO
2
IKETI
PPMV
5.20
8.10
9.70
9.20
8.70
ALDEHYDES SMOKE PARTICULATES
IHET)
PPMV
21.30
29.20
37.10
46.80
50.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
SHP
0
24
49
71
74
MASS EMI
CO
LB/1K
LB FUEL
13.75
12.38
10.21
8.17
7.62
MASS EMI
HC
LB/1K
LB FUEL
0.24
0.10
0.06
0.02
0.01
MASS EMI
NQ2
LB/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/1K
LB FUEL
3090.00
3080.00
3070.00
3060.00
3060.00
MASS EMI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/IK
LB FUEL
4.21
4.56
4.76
5.12
5.21
MASS EMI
CO
LB/HR
.00
.12
.12
.05
.01
MASS EMI
HC
LB/HR
0.02
0.01
0.01
0.00
0.00
MASS EMI
NO 2
LB/HR
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
C02
LB/HR
224.33
279.05
336.47
393. 62
406.67
MASS EMI
NO
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/HR
0.31
0.41
0.52
0.66
0.69
POWER
PERCENT
RATED
SHP
LB/IK HP-HR
CO
LB/IK HP-HR
MORSFPDWER-HR BASIS NOT CALCULABLE*****
24 28.389 7064.496
49 14.222 4275.371
71 9.226 3454.578
74 8.528 3426.063
THC
LB/IK HP-HR
0.225
0.089
0.024
0.011
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
10.464
6.630
5.777
5.8)2
III-8.
-------
0»T6I 5/14/71
TEST ORGANIZATION: AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE 0»I»
CAL ID NUNBERl 82 ENGINE TYPE AND MODEL: GTCP36-6
RATED SHAFT HORSEPOWER: 160.
ENGINE TOTAL TINEl 0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: o. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZUE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO: 1.877
SERIAL NUMBER:
P-34TT2
FINISH
FINISH
93.00
28.70
FUEL: JP-5
OPERATIONAL DATA «««»
INLET AIR TEMPERATURE. DEGREES F: START 93.00
ATMOSPHERIC PRESSURE: START 28.TO
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.00*8
RELATIVE HUMIDITr: 17.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 3
COMMENTS:
COMBINATION SHP/HLEED LOADING
!
i>
{
s
i
ji
5
5
I
0
TFST
NODE
15/ 0
10/15
5/10
POKER
PERCENT
KITED
SHP
48
24
0
POWER
PERCENI
RATED
SHP
48
24
0
POWER
PFRCENT
RATED
SHP
48
2t
0
SHAFT
HP
POWER
AIR
HP
78.20 64.63
39.10 80.39
0.0
EXHAUST
GAS
TEMP
DEGREES F
1145.00
1155.00
1155.00
MASS EMI
CO
LB/IK
LB FUEL
5.95
5.59
5. 78
to
LB/IK
5.
6.
8.
86.25
EXHAUST
CAS
PRESSURE
PSIA
-0.00
-0.00
-o.no
MASS EMI
HC
LB/IK
LB FUEL
0.01
0.02
0.01
ENGINE
SPEED
RPM
NI
58200.00
58300.00
58500.00
CO
(WET)
PPMV
116.90
100.00
106.90
MASS EMI MASS
CORRECTED
N2
-0.00
-0.00
-0.00
CO
2
IWETI
PERCENT V
3. BO
3.47
3.59
ENI MASS
FUEL
FLOW
LB/HR
139. BO
112.90
122.70
THC
IWET)
PPMV
0.40
0.60
0.50
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
NO
IWETI
PPMV
47.40
54.70
50.50
EMI MASS EMI MASS
N02 C02 NO
LB/IK LB
/IK LB/
IK L
LB FUEL LB FUEL LB FUEL LB
-0.00 3040
-0.00 3050
-0.00 3050
CO
2
HP-HR LB/IK HP-HR
820
223
220
2975.469
339Z.153
4119.047
.00 -0.
.00 -0.
.00 -0.
THC
00
00
00
LB/IK HP-HR
0.010
O.OJO
O.OZI
NOX CO
fl/lK LB/
FUFl
4.57 0.
5.66 0.
5.04 0.
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
F/A
CALC
FROM
EMISSIONS
0.018700
0.017000
0.017600
NO
2
IWETI
PPMV
7.30
6.90
6.30
EMI MASS
HC
HR LB/
»3 0.
74 0.
71 0.
LB/IK
-0
-0
-n
COMPRESSOR
INLET
TEMP
DEGRFES F
93.00
94.00
93.00
CCMPRESSOR
DISCHARGE
PRESSURE
PSIA
50.10
47.30
44.30
NO ALDEHYDES SMOKE
X
IWFT)
PPMV
54.70
61.50
56.80
-0.00 -0.00
-o.oo -o.oo
-0.00 -0.00
EMI MASS FMI "ASS EMI MASS
NH2
HR LB/HR
00 -0.00
00 -0.00
00 -0.00
nn
2
HP-HR
.000
.000
.000
en 2 N»
LB/HR LB/
424.99 -0.
405.34 -1.
374.21 -0.
NO
X
LR/IK HP-HR
4.477
6.291
7.l<>9
BLEED
FLOW
LB/MIN
49. 16
64.60
74.28
PARUCULATES
-0.00
-n. oo
-0.00
EMI MASS TMI
NO*
HR LB/MK
00 0.64
00 0.75
00 0.62
III-9
-------
OATEt
TEST ORGANIZATION I A1RESEARCH
ENGINE SUPPLIER I AIRESEARCH
ENGINE DATA »»»»»»«»»««»»
i
CAL ID NUMBER! 38 ENGINE TYPE AND HOOCH GTCM60-4 SERIAL NUMBER! P-37596
RATED SHAFT HORSEPOWER! 300.
ENGINE TOTAL TINEl 0. HRS
TINE SINCE HOT SECTION OVERHAUL! 0. HRS
TINE SINCEl
Nl CONPRESSOR OVERHAUL! 0. HRS
N2 CONPRESSOR OVERHAUL' 0. HRS
CONBUSTOR CAN REPLACENENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAULl 0. HRS
Nl TURBINE OVERHAUL! 0. HRS
N2 TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO! 1.B7T
FINISH
FINISH
ea.oo
28.69
FUEL! JP-3
OPERATIONAL DATA »»*«»»
INLET AIR TENPERATURE, DEGREES F: START 88.00
ATMOSPHERIC PRESSURE: START 28.69
INLET AIR HUNIOITYf LBS H20/L8 AIR: 0.0037
RELATIVE HUMIDITY: 15.00 PERCENT
SANPLE LINE! TENPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/KIN: -0.00
SAMPLE LINE TRANSPORT TINE, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
SHP ONLY. SURGE VALVE OPEN
TEST
NODE
I/ 0
(,/ I
ll/ 6
16/11
20/16
POMES
SHAFT AIR
HP HP
0.0
7*.90
ISO.10
224.90
102.30
0.0
0.0
0.0
0.0
0.0
ENGINE
SPEED
RPN
Nl N2
20020.00
20010.00
20010.00
20020.00
20010.00
CORRECTED GAS GEN
FUEL AIR FLOW
FLOW LB/SEC
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
596.00
641.50
6B6.00
725.00
773.00
-0.00
-0.00
-0.00
-0.00
-0.00
F/A COMPRESSOR
CALC INLET
FROM TEMP
EMISSIONS DEGREES f
o.ooaooo
0.008400
0.009)00
0.009700
0.010500
86.00
87.00
88.00
88.00
89.00
CONPRESSOR BLEED
DISCHARGE FLOW
PRESSURE Lfl/NIN
PSIA
55.10
55.70
56.20
56.80
57.10
0.0
0.0
0.0
0.0
0.0
POWER
PERCENT
RATED
SHP
0
24
50
74
100
EXHAUST
GAS
TEMP
DEGREES F
681.00
723.00
763.00
801.00
849.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
CO
(WET)
PPNV
116.70
114.00
117.20
112.50
117.80
CO
2
IWETI
PERCENT V
1.63
1.72
1.90
1.98
2.16
THC
(WET)
PPMV
11.20
9.60
9.40
8.50
9.30
NO
IWETI
PPMV
18.40
20.60
22.30
24.60
27.20
NO
2
IWETI
PPMV
5.20
5.40
5.90
5.80
6.10
ALDEHYDES SMOKE PARTICULATES
I WET I
PPMV
23.50
26.00
28.20
30.40
33.40
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
SHP
0
24
50
74
100
MASS EMI
CO
16/11
LB FUEL
14.08
13.04
12.12
11.17
10.72
MASS EMI
HC
L8/1K
LB FUEL
0.77
0.63
0.56
0.48
0.48
MASS EMI
N02
L8/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
NASS EHI
C02
LB/IK
LB FUEL
3090.00
3090.00
3090.00
3090.00
3080.00
MASS EHI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/IK
LB FUEL
4.«7
4.89
4.78
4.95
4.99
MASS EMI
CO
LB/HR
fl.39
8.36
8.31
8.10
8.29
MASS EMI
HC
LB/HR
0.46
0.40
0.38
0.15
0.37
MASS EHI
NO 2
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/MR
1841.64
1982.23
2119.74
2240.25
2180.84
MASS EHI
NO
LO/HR
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EHI
NO X
LB/HR
2.78
3.13
3.28
3.59
3.85
POWER CO
PERCENT
RATED LB/IK HP-HR
SHP
LB/IK HP-HR
HORSFPOWER-HR BASIS NOT CALCULABLE**"*
24 111.650 26465.082
50 55.374 14122.184
74 36.002 9961.090
100 27.407 7875.758
THC
LB/IK HP-HR
5.353
2.546
1.563
1.230
NO
IB/IX HP-HR
-0.000
-0.000
-0.000
-0.000
L8/1K HP-HR
-0.000
-0.000
-0.000
-o.ooo
LB/IK HP-HR
41.847
21.860
15.970
12.750
111-10
-------
OATEl S/26/71
TEST ORGANUATIONI AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE DAT*
C»L 10 NUMBER: 63 ENGINE TYPE AND MODEL: GTCP660-4
RATED SHAFT HORSEPOWER: 300.
ENGINE TOTAL TINEi 0. HRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
H2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOIZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.877
SERIAL NUMBER:
FINISH
FINISH
91.00
28.69
FUEL I JP-5
OPERATIONAL DATA »
INLET AIR TEMPERATUREi DEGREES F: START 91.00
ATMOSPHERIC PRESSURE: START 28.69
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0037
RELATIVE HUMIDITY: 15.00 PERCENT
SAMPLE LINF.: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIHE, SEC: -0.00
NUMBER OF TESTS: 6
COMMENTS:
COMBINATION SMP/BLFED LOADING
TEST
MODE
22/ 0
19/22
15/19
10/15
5/10
3/ 5
POWER
PERCENT
RATED
<;HP
100
75
50
24
0
1
POWER
PERCENT
RATED
SHP
100
75
50
74
0
0
POWER
PERCENT
RATED
SHP
100
75
50
24
0
0
SHAFT
HP
902.40
227.30
150.10
74.90
0.0
0.0
EXHAUST
GAS
TEMP
DEGREES F
1209.00
1202.00
1194.00
1187.00
1180.00
953.00
MASS EMI
CO
LB/U
LB FUEL
8. 24
8.53
B.43
8.96
9.38
9.76
CO
LB/IK
8.
4.
9.
10.
12.
13.
POWER
AIR
HP
630.10
637.51
651.15
659.68
665.27
564.58
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
0.29
0.41
0.34
0.43
0.40
0.58
ENGINE
SPEED
RPM
Nl
20020.00
20010.00
20010.00
20010.00
20020.00
20010.00
CO
IWETI
PPMV
146.60
146.70
143.50
154.10
156.80
129.40
MASS EMI MASS
N2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
IWETI
PERCENT
3.45
3.34
3.30
3.34
3.25
CORRECTED
FUEL
FLOW
LB/HR
970.00
442.00
914.00
885.00
872.00
757.00
THC
IWETI
PPMV
V
9.00
12.30
10.00
13.00
11.80
2.59 13.40
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
IWETI
PPMV
49.30
48.70
46.50
47.60
45.10
34.30
EMI MASS FMI MASS EMI MASS
N02 C02
LB/IK LB/IK
LB FUEL LB
-0.00 3050
-0.00 3050
-0.00 3050
-0.00 3050
-0.00 3050
-0.00 3070
CO
2
HP-HR LB/IK HP-HR
574
360
609
794
288
093
3172.655
1551.845
3478.325
3674.553
3997.783
4116.340
Nfl
NQX CO
F/A
CALC
FROM
EMISSIONS
0.016900
0.016400
0.016200
0.016400
0.015900
0.012700
NO
1
IWFTI
PPMV
8.80
8.20
8.50
7.90
8.50
6.90
FMI MASS
HC
COMPRESSOR
INLET
TEMP
DEGREES F
89.00
90.00
90.00
92.00
92.00
95.00
COMPRESSOR
DISCHARGE
PRESSURE
PSIA
51.70
50.50
49.40
48.00
46.90
49.60
NO ALDEHYDES SMOKF
X
IWFT)
PPMV
58.10 -0
56.80 -0
55.00 -0
55.50 -0
53.60 -0
41.30 -0
EMI MASS EMI
N02
LB/IK LB/IK LB/HR LB/Hfl LB/HR
FUEL IB CUEL LB
.00
.00
.00
.00
.00
.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
LB/IK
0.
0.
0.
0.
0.
0.
HP-HR
301
208
383
522
530
774
FUEL
5.36 8.
5.43 3.
5.31 7.
5.30 7.
5.26 8.
5.11 7.
NO
IB/ IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
00 0.
77 0.
70 0.
93 0.
17 0.
39 0.
LI/IK
-0
-0
-0
2fl -0.00
\i -0.00
31 -0.00
3D -0.00
35 -0.00
44 -0.00
NO
2
.00 -0.00
.00 -0.00
.00 -o.oo
.00 -0.00
.00 -0.00
.00 -o.oo
MASS EMI MASS
Cfl2 ND
BLEED
FLOW
Lfl/MIN
468.46
483.82
504.98
524.23
541.12
432.06
PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
FMI MASS
EMI
NOX
L8/HR LB/HR LB/HR
295H.50 -n.
1348.10 -0.
27J7.70 -0.
2699.25 -0.
2659.60 -0.
2321.99 -0.
NO
X
00 5
00 7
00 4
00 4
00 4
00 3
.20
.40
.85
. 69
.59
.87
HM-MR LH/1K HP-HR
.000
.000
.000
-0.000
-0
-n
.000
.000
5.579
2.773
6.057
6.39)
6.900
6.859
III-ll
-------
omt
TEST OAGANIIATIONI A1RESEARCH
ENGINE SUPPLIER! AUESEAACH
ENGINE 0*1* *»«»»«»»»»»»»»»»«««»»««
t
CAL 10 NUMBER! 14 ENGINE TYM MO MODEL! GTCM40-* SERIAL NUMBER! P-JTTOi
RATED SHAFT HORSEPOWER! )00.
0. MRS
0. MRS
ENGINE TOTAL TINE I
TINE SINCE HOT SECTION OVERHAUL!
TINE SINCE I
Nl COMPRESSOR OVERHAUL! 0. MRS
HZ COMPRESSOR OVERHAUL) 0. MRS
CONBUSTOR CAN REPLACEMENT I 0. MRS
FIRST STAGE NOZILE GUIDE VANE OVERHAUL! 0. HRS
Nl TURBINE OVERHAUL! 0. HRS
N2 TURBINE OVERHAUL I 0. HRS
FUEL H/C RATIO! 1.8TT
FINISH
FINISH
96.00
28.58
FUEL! JP-3
OPERATIONAL DATA »«««««
INLET AIR TENPERATUREt DEGREES Fl START 96.00
ATMOSPHERIC PRESSURE! START 28.56
INLET AIR HUMIDITY. LBS H2Q/LB AIRi 0.00)1
RELATIVE HUMIDITY! 9.00 PERCENT
SAMPLE LINE! TEMPERATURE. DEGREES Cl -0.00. FLOW RATE. LITERS/MIN:
SAMPLE LINE TRANSPORT TIME. SEC! -0.00
NUMBER OF TESTS! 1
COMMENTS:
SHP ONLY, SURGE VALVE OPEN
-0.00
TEST
MODE
I/ 0
6/ 1
llf 6
16/11
20/16
POWER
SHAFT
HP
0.0
T4.90
151.10
2Z5.90
302.30
AIR
HP
0.0
0.0
0.0
0.0
0.0
ENGINE
SPEED
RPM
Nl
20010.00
20010.00
20000.00
2000.00
20010.00
Hi
-0.00
-0.00
-0.00
-0.00
-0.00
CORRECTED
FUEL
FLOW
LB/HR
396.00
636. SO
685.00
T2J.OO
757.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
F/A
CALC
FROM
EMISSIONS
0.007700
0.008200
0.009000
0.009600
0.010100
COMPRESSOR
INLET
TEMP
DEGREES F
96.00
96.00
96.00
97.00
96.00
COMPRESSOR BLEED
DISCHARGE FLOM
PRESSURE LH/MIN
PSIA
54.70
55.30
S6.00
56.60
0.0
0.0
0.0
0.0
0.0
POWER
PERCENT
RATED
SHP
0
24
50
75
100
EXHAUST
GAS
TEMP
DEGREES F
691.00
719.00
767.00
BOO.00
823.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
CO
(HEM
PPMV
77.10
BO.40
87.40
92.80
103.80
CO
2
(UETI
PERCENT V
1.58
1.68
1.85
1.96
2.06
THC
IWEII
PPMV
21.30
10.60
28.50
8.40
19.00
NO
I WET I
PPMV
17.00
20.50
23.10
25.20
27.40
NO
2
(WET)
PPMV
3.80
4.80
5.20
5.90
6.30
NO
X
IWETI
PPMV
20.80
2S.20
28.30
31.10
33.70
ALDEHYDES SMOKE P4RTICULATFS
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
SHP
0
24
50
75
100
MASS EMI
CO
LB/IK
LB FUEL
9.61
9.41
9.28
9.30
9.87
MASS EMI
HC
LB/IK
LB FUEL
1.52
0.71
1.73
0.48
1.03
MASS EMI
N02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-n.no
-0.00
MASS EMI
C02
LB/IK
IB FUEL
3100.00
3100.00
3090.00
3090.00
3080.00
MASS EMI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/IK
LB FUEL
4.26
4.85
4.93
5.12
5.27
MASS EMI
CO
L6/HR
5.73
5.99
6.36
6.73
7.47
MASS EM
HC
LB/HR
0.90
0.45
1.18
0.35
0.78
MASS EMI
NO 2
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
1847.60
1973.15
2116.65
2234.07
2131.56
MASS EMI
NO
LB/HB
-0.00
-0.00
-0. 00
-0.00
-0.00
MASS EMI
NOX
LB/HR
2.54
3.09
3.38
3.70
3.99
POWER
PERCENT
RATED
SHP
LB/IK HP-MR
LB/1K HP-HR
HORSEPOWER-HR BASIS NOT CALCULABLE"*
24 80.009 263*3.789
50 42.070 14008.266
75 29.771 9889.637
100 24.723 7712.738
THC
LB/IK HP-KR
6.008
7.838
1.549
2.579
NO
LB/IK HP-HB
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
41.258
22.363
16.390
13.192
111-12
-------
OATEl
TEST ORGANIZATION: AIRESEARCH
ENGINE SUPPLIER! AIRESEARCM
ENGINE 0»t»
CAL 10 NUMBER: 84
ENGINE TOTAL TIME:
TINE SINCE HOT SECTION OVERHAUL:
TINE SINCE:
ENGINE TYPE AND MODEL: 6TCP660-*
RATED SHAFT HORSEPOWER: 300.
0. HXS
0. HRS
SERIAL NUMBER:
P-J7T05
HI COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.877
FINISH
FINISH
58.00
2B.S6
FUEL: JP-5
OPERATIONAL DATA »««««««««
INLET AIR TEMPERATUREt DEGREES F: START 98.00
ATMOSPHERIC PRESSURE: START 28.58
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0031
RELATIVE HUMIDITY; 9.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITFRS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
COMBINATION SHP/BLEEO LOADING
TEST
MODE
22/ 0
19/22
15/19
10/15
5/10
POWER
SHAFT AIR
HP HP
302.10
225.90
1*9.80
7*.90
0.0
669.65
676.99
685.29
618.22
698.09
ENGINE
SPEED
RPM
NI N2
20000.00
20000.00
20000.00
2000.00
20000.00
CORRECTED GAS GEN
FUEL AIR FLOW
FLOW LB/SFC
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
962.00
932.00
907.00
895.00
S57.00
-0.00
-0.00
-0.00
-0.00
-0.00
F/A COMPRESSOR
CALC INLET
FROM TEMP
EMISSIONS DEGREES f
0.015900
0.016200
0.016300
0.016700
0.016400
93.00
97.00
98.00
100.00
99.00
COMPRESSOR
DISCHARGE
PRESSURE
PSIA
51.00
49.90
48. 70
47.10
46.00
BLEEI1
FLOW
LB/MIN
49(1.2?
511.21
531.06
555.03
571.89
PUUER
PERCENT
RATED
SHP
100
75
49
74
0
EXHAUST
GAS
TEMP
DEGREES F
1202.00
1192.00
1183.00
1172.00
1162.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
en co
IWET) 2
PPMV IBETI
PERCENT V
167.50
174.20
177.10
191.40
197.30
3.23
3.30
3.32
3.39
3.34
THC
(MET)
PPMV
13.90
26.70
15.00
28.40
23.90
HO NO
I MET I 2
PPMV IKETI
PPMV
ALDEHYDES SMOKE PABTICULATES
51.00
50.40
53.90
56.80
54.60
9.30
9.90
10.90
1 1.00
11.40
(WET I
PPMV
60.30
60.20
64.f)0
67.80
66.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
POWER
PERCENT
RATED
SHP
100
75
49
24
0
MASS EMI
cn
IB/IK
LB FUEL
10.05
10.24
10.34
10.93
11.45
MASS EMI
HC
LB/1K
LB FUFL
0.48
0.90
0.50
0.93
0.79
MASS FMI
NO?
L8/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
cn2
LB/IK
LB FUEL
3050.00
3050.00
3050.00
3040.00
3040.00
MASS EMI
NO
LB/IK
LR FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NDX
LB/IK
LB FUEL
5.94
5.81
6.22
6.36
6.29
MASS EMI
CO
LR/MR
9.67
9.54
S.38
9.68
9.H1
MASS fHI
HC
LR/HS
0.46
0.84
0.45
0.82
0.6*
MASS E«l
N02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
cn?
LB/HR
2934.10
2342.60
2766.35
2690.40
2605. ?8
««SS EMI
N<1
18/HK
-o.no
-o.oo
-o.no
-o.oo
-o.oo
MASS FMI
NOX
LR/HK
5.7?.
5.42
5.64
5.63
5.39
POWER
PERCENT
RATED
SHP
100
75
49
24
0
CO
19/IK HP-HR
9.952
10.569
11.236
12.517
14.054
LR/K HP-HR
3019.409
3148.351
3312.624
3479.941
3732.031
THC
LB/IK HP-HR
0.471
0.927
0.544
1.061
0.972
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
LB/IK HP-MR
-0.000
-o.ooo
-o.ooo
-o.ono
-o.ooo
NO
X
LI/IK HP-MR
5.8'4
6.001
6.756
7.285
7.721
111-13
-------
OAU't 5/25/T1
TEST ORGANI1ATIONI AIREStARCK
ENCIM SUPPLIER! AIAESEARCM
EN6INE OAT* *»******»*******»**********»**,*««***
CAl ID NUMBER! 40 ENGINE TY« am NODELI TKPTOO-4 SERIAL NUNBEll P~«OIM
ATED SHIFT HORSEPOKERI 1«J.
ENGINE TOT*L TINil 0. MRS
TIME SINCE HOT SECTION OVERHAUL I 0. MRS
TINE sincei
Nl COMPRESSOR OVERHAUL" 0. HRS
N2 COMPRESSOR OVERHAULl 0. HRS
COMBUSTOR CAN REPLACEMENT! 0. HRS
FIRST STA6E N01ZLE GUIDE VANE OVERHAULl 0. HRS
Nl TURBINE OVERHAULl 0. HRS
NZ TURBINE OVERHAUL) 0. HRS
FUEL H/C RATIO! I.8T7
FINISH
FINISH
91.00
ZB.66
FUEL I JP-S
OPERATIONAL DATA ««»«««««««»««
INLET AIR TEMPERATURE. DEGREES Ft START 91.00
ATMOSPHERIC PRESSUREl START 21.66
INLET AIR HUMIDITY, LBS H20/LB AIRl 0.0037
RELATIVE HUMIOtTYl 18.00 PERCENT
SAMPLE LINEl TEMPERATURE, DEGREES Ct -0.00, FLOM RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SECl -0.00
NUMBER OF TESTS! 6
CONMENTSI
STANDBY MODE. SHP ONLY, SURGE VALVE OPEN
TEST
MODE
I/ 0
21 1
6/ 2
III «
16/11
20/16
POWER
PERCENT
RATED
SHP
0
0
25
49
73
99
POKER
PERCENT
RATED
SHP
0
0
25
49
73
99
POWER
PERCENT
RATED
SHP
SHAFT
HP
0.0
0.0
36.00
70.70
104.00
141.00
EXHAUST
GAS
TEMP
DEGREES F
819.00
777.00
800.00
813.00
858.00
893.00
MASS EMI
CD
LB/1K
L8 FUEL
21.33
6.64
4.52
3.17
2.29
1.76
CO
L8/IK
HORSEPOUER-HR
HORSEPOMER-HR
25
49
71
99
46.
17.
POWER ENGINE CORRECTED
AIR SPEED FUEL
HP RPK FLOW
Nl N2 LB/HR
0.0 17680.00 35350.00 225.00
0.0 24890.00 15910.00 317.00
0.0 25000.00 15830.00 171.00
0.0 25600.00 35800.00 394.00
0.0 25900.00 35750.00 417.50
0.0
EXHAUST
GAS
PRESSUR
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
KC
18/lK
LB FUEL
7.75
2.82
2.96
2.40
2.65
2.44
HP-HR
BASIS NOT
BASIS NOT
602
644
9.201
5.
5JO
26400.00 15690.00 442.00
CO
(WETI
E PPMV
251.70
78.70
55.80
40.40
30.50
25.00
MASS EMI MASS
CO THC
2 (MET)
IMETI PPMV
PERCENT V
2.28 160.00
2.32 58.40
2.41 63.80
2.50 53.60
2.60 61.60
2.77 60.50
GAS GEN
AIR FLOW
L8/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
(MET)
PPMV
F/A COMPRESSOR COMPRESSOR
CALC INLET DISCHARGE
FROM TEMP PRESSURE
EMISSIONS DEGREES F PSIA
0.011300 78.00 37.70
0.011300 89.00 101.00
0.011800 92.00 104.00
0.012200 99.00 106.90
0.012700 100.00 108.90
0.013500
NO NO
2
(MET! (WE
98.00 110.80
ALDEHYDES SMOKE
X
T)
BLEED
FLOW
L8/NIN
0.0
0.0
0.0
0.0
0.0
0.0
PARTICULARS
PPMV PPMV
22.50
52.60
53.60
62.80
71.20
72.80
EMI MASS EMI MASS EMI MASS
N02 C02 NO
L8/1K LB/IK IB/IK
L6 FUEL LB
-0.00 3040
-0.00 3080
-0.00 3080
-0.00 3080
-0.00 3080
-0.00 3070
CO
2
LB/1K HP-HR
CALCULABLE*****
CALCULABLE*****
31741.105
17164.352
12364.422
9623.684
NOX CO
12.90 35.
11.70 64.
B. 40 62.
7.00 69.
6.20 77.
16.50 89.
EMI MASS EMI
HC
L8/IK LB/HR LB/HR
40 -0.00 -0.00
30 -0.00 -0.00
00 -0.00 -0.00
80 -0.00 -0.00
40 -0.00 -0.00
30 -0.00 -0.00
MASS EMI MASS Ell MASS
N02 C02 NO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
EMI MASS EM
NOX
LB/HS LB/HR IB/MR 18/HR
FUEL LB FUEL LA FUEL
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
THC
LB/1K HP-HR
10.494
13.369
10.634
7.661
4.93 4.
8.91 2.
8.26 1.
8.98 1.
9.56 0.
10.36 0.
NO
LB/1K HP-HR
-0.000
-0.000
-0.000
-0.000
80 1.74
24 0.95
68 1.10
25 0.95
96 1.11
78 1.08
NO
2
LB/IK MP-H
-0.000
-0.000
-0.000
-0.000
-0.00 684.00 -0.
-0.00 1037.96 -0.
-0.00 1142.68 -0.
-0.00 1213.52 -0.
-0.00 1285.90 -0.
-0.00 1356.94 -0.
NO
X
ft LB/IK HP-HR
85.124
50.050
38.386
32.489
00 1.11
00 3.00
00 3.06
00 3.54
00 3.99
00 4.58
111-14
-------
0»TE: 5/25/T1
TEST ORGANIZATION! AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE 0»T» ««
C»L ID NUMBER
85 ENSINE TYPE AND MODEL> TSCP700-*
RATED SHAFT HORSEPOWER: U2.
ENGINE TOTAL TINE: 0. MRS
TIME SINCE HOT SECTION OVERHAUL! 0. MRS
TINE SINCEl
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.877
SERIAL NUMBER!
FINISH
FINISH
89.00
28.66
FUFL: JP-S
OPERATIONAL DATA ««««
INLET AIR TENPERATUDEf DEGREES F: START 88.00
ATMOSPHERIC PRESSURE: START 28.66
INLET AIR HUMIDITY> LBS H20/LR AIR: 0.0037
RELATIVE HUMIDITY: is.oo PERCENT
SAMPLE LINE: TEMPERATUREi DEGREES C: -0.00, FLOW RATE. LITERS/MIN:
SAMPLE LINE TRANSPORT TIME. SEC: -0.00
NUMBER OF TESTS: 6
COMMENTS:
NORMAL NODE, COMBINATION LOAD
TEST
MODE
22/ 0
19/22
IS/I*
10/15
5/10
25/ 5
POWER
PERCENT
RATEP
SHP
98
72
49
25
0
0
POWER
PERCENT
RATED
SHP
18
72
49
25
0
n
POWER
PERCENT
RATEn
SHP
98
72
49
25
0
0
SHAFT
HP
139.60
102.80
69.80
15.50
0.0
0.0
EXHAUST
GAS
TEMP
DEGREES F
1005.00
1005.00
1005.00
1005.00
1005.00
887.00
MASS EMI
CO
LB/IK
LB FUEL
.49
.28
.28
.41
.19
.92
CO
LB/IK
0.
0.
0.
0.
0.
0.
POWER ENGINE CORRECTED GAS GEN
AIR SPEED FUEL AIR FLOW
HP RPN FLOW LB/SEC
Nl N2 LB/HR
1171. 89 27300.00 15350.00 495.50 -0.00
1191.55 27300.00 35350.00 487.00 -0.00
1198.68 27300.00 35350.00 477.00 -0.00
1203.58 27300.00 35350.00 469.00 -0.00
1197.28 27300.00 25250.00 467.00 -0.00
1033.62 28100.00 35350.00 467.00 -0
FXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
2.35
2.70
2.50
2.90
2.18
3.15
HP-HR
563
483
481
535
541
868
MASS
CU
(WETI
PPMV
23.80
20.40
20.40
22.70
22.60
26.10
EMI MASS
cn
2
IUETI
PERCENT V
1.11
3.10
1.10
1.12
3.18
2.66
EMI MASS EM
ND2 C02 NO
LB
LB
-0
-0
-0
-0
-0
-0
LB/IK
1156
1151
1150
1158
1205
1387
/IK LB
FUEL LS
.00 3060
.00 3060
.00 3060
.00 3060
.00 3090
.00 1070
CO
2
HP-HR
.111
.326
.686
.211
.256
.052
/IK LA/IK
.00
THC NO
(WET) (WETI
PPMV PPMV
65.50 97
75.30 109
69.60 90
81.50 95
62.10 92
74.90 9.1
1 MASS EMI
NOX
LB/IK
.50
.30
.80
.70
.10
.20
MASS
cn
LB/
F/A COMPRESSOR CCMPRESSOP
CALC INLET DISCHARGE
FROM TFMP PRESSURE
EMISSIONS DFGREES F PSIA
0.015200 90.00 111.30
0.015200 89.00 109.40
0.015200 87.00 108.50
0.015100 86.00 106.90
0.015500 85.00 104.50
0.013000 91.00 125
NO NO
2 X
-------
MTU 5/17/71
TEST ORGANIZATION! AIRESEAACH
ENGINE SUPPLIER! AIRESEAACH
EN6INE OAT* »**»**»*«**»******»»*»**»***»»»»»***»*»**»***»*********»
i
CAL 10 NUMBER! 41 ENGINE TYPE MO HODEL I TSCPTOO-4 SERIAL NUNBERI P-901M
RATED SHAFT HORSEPOWER: 142.
0. MRS
0. MRS
ENGINE TOTAL TINEl
TINE SINCE HOT SECTION OVERHAUL!
TINE SINCEl
Nl COMPRESSOR OVERHAUL: 0. MRS
HZ CONPRESSOR OVERHAUL: 0. HRS
COHBUSTOR CAN REPLACEMENT! 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.8TT
FINISH
FINISH
97.00
28.11
FUEL: jp-5
OPERATIONAL DATA ««»»»
INLET AIR TEMPERATURE. DEGREES Fi START 97.00
ATMOSPHERIC PRESSURE! START 28.72
INLET AIR HUMIDITY, LBS H20/LB AIR! 0.0041
RELATIVE HUMIDITY! 18.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MINI -0.00
SAMPLE LINE TRANSPORT TINE, SECi -0.00
NUMBER OF TESTS! 6
COMMENTS!
STANDBY MODE, SHP ONLY, SURGE VALVE OPEN
TEST
MODE
I/ 0
II I
6/ 2
ll/ 6
16/11
20/16
POWER
SHAFT AIR
HP HP
0.0
0.0
34.80
68.40
103.90
141.10
0.0
0.0
0.0
0.0
0.0
0.0
ENGINE
SPEED
RPM
Nl N2
17650.00
28100.00
27800.00
25990.00
26270.00
26750.00
35440.00
35000.00
34650.00
34650.00
35730.00
35720.00
CORRECTED
FUEL
FLOW
LB/HR
228.00
481.00
482.00
409.00
436.00
469.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
F/A COMPRESSOR
CALC INLET
FROM TEMP
EMISSIONS DEGREES F
0.011600
0.014000
0.014600
0.012700
0.013300
0.014300
82.00
100.00
103.00
96.00
102.00
100.00
COMPRESSOR BLEED
DISCHARGE FLOW
PRESSURE LB/MIN
PSIA
59.10
115.10
114.00
102.10
106.10
110.10
0.0
0.0
0.0
0.0
0.0
0.0
POWEB EXHAUST
PERCENT GAS
RATED TEMP
SHP DEGREES f
0
0
24
46
73
99
842.00
939.00
979.00
884.00
929.00
956.00
EXHAUST
GAS
PRESSURE
PSI>
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO CO
I WET) 2
PPMV (WET)
PERCENT V
193.20
16.00
18.80
22.20
18.90
14.80
2.35
2.88
2.99
2.61
2.73
2.92
THC
IWETI
PPMV
69.50
31.00
55.60
18.10
40.90
43.60
NO NO
(WET) 2
PPMV IWETI
PPMV
ALDEHYDES SMOKE P»RT ICULHTF.S
20.80
45.20
46.50
44.60
52.10
60.40
12.60
1.40
2.10
3.70
2.80
3.30
X
IWETI
PPMV
33.40
46.50
48.60
48.30
54.90
63.70
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
SHP
0
0
24
48
73
99
MASS EMI
CO
LB/IK
LB FUEL
15.98
1.09
1.23
1.67
1.35
0.99
MASS EMI
HC
LB/IK
LB FUEL
3.28
1.20
2.07
0.78
1.68
1.67
MASS EMI
N02
LB/IK
Lfl FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/IK
LB FUEL
3060.00
3070.00
3070.00
3080.00
3080.00
3070.00
MASS EMI
NO
LB/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/IK
LB FUEL
4.54
5.20
5. ?l
5.96
6.48
6.99
MASS EMI
CO
LB/HR
3.64
0.52
0.59
0.68
0.59
0.46
MASS EMI
HC
LB/HR
0.75
0.58
1.00
0.32
0.73
0.78
MASS EMI
N02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
697.68
1476.67
1479.74
1259.72
1342.88
1439.83
MASS EMI
NO
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/HR
1.04
2.50
2.51
2.44
2.82
3.28
POWER
PERCENT
RATED
SHP
LB/IK HP-MR
LB/IK HP-HR
KORSEPOWER-HR BASIS NOT CALCULABLE*****
HORSEPOWER-HR BASIS NOT CALCULABLE*****
24 17.022 42521.270
48 9.998 18416.957
73 5.686 12924.734
99 3.291 10204.320
THC
LB/IK HP-HR
28.740
4.658
7.050
5.541
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
NO
X
LB/IK HP-HR
72.203
35.644
27.188
23.241
111-16
-------
OUJ3
DATE: S/Z7/T1
TEST ORGANIZATION) AIRESEARCH
ENGINE SUPPLIERl AIRESEARCH
ENGINE DAT*
CAL ID NUMBER! 96 ENGINE TrPE AND MODEL! TSCP700-*
RATED SHAFT HORSEPOWER: 142.
FNGINE TOTAL TIMEi 0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
NZ COMPRESSOR OVERHAUL! 0. HRS
CONSUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.677
SERIAL NUMBER:
P-90123
FINISH
FINISH
89.00
26.72
FUEL: JP-S
OPERATIONAL DATA «»«»
INLET AIR TEMPERATURE. DEGREES F: START 89.00
ATMOSPHERIC PRESSURE: START 28.72
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0041
RELATIVE HUMIDITY: ta.oo PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00. FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 6
COMMENTS:
NORMAL MODE, COMBINATION LOAD
TEST
MODE
22/ 0
19/22
15/19
10/15
5/10
25/ 5
POWER
SHAFT
HP
140.00
103.10
70.00
35.60
0.0
0.0
AIR
HP
1083.37
1113.33
1131.67
1117.60
1097.85
1058.37
ENGINE CORRECTED
SPEED
RPM
Nl
27300.00
27300.00
27300.00
27300.00
27340.00
28100.00
N2
35440.00
35440.00
35440.00
35440.00
35440.00
35440.00
FUEL
FLOW
LB/HR
497.00
489.00
481.00
471.00
460.00
474.00
GAS GEN
AIR FLOW
IB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
F/A
CALC
FROM
EMISSIONS
0.015300
0.014900
0.014900
0.015100
0.015200
0.013700
COMPRESSOR
INLET
TEMP
DFGREES F
89.00
99.00
89.00
87.00
87.00
91.00
COMPRESSOR BLEED
DISCHARGE FLOW
PRESSURE LB/MIN
PSIA
109.80
108.60
107.90
104.40
102.60
116.50
448.74
464.4fl
474. 14
4BK.92
477.35
420.39
POWER
PERCENT
RATED
SHP
98
72
49
25
0
0
EXHAUST
GAS
TEMP
DEGREES F
1005.00
1005.00
1005.00
1005.00
1005.00
908.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO CO THC
IWETI 2 (WFTI
PPMV (WET) PPMV
PERCENT V
21.00
19.40
22.10
19.30
48.60
27. 10
3.14
3.04
3.06
3.09
3.11
2.81
24.50
31.40
28.80
38.80
39.90
23.60
NO
[MET I
PPMV
83.70
79.10
76.10
75.80
76.60
75.00
NO
2
IWETI
PPMV
0.40
3.4C
3.60
3.40
3.20
4.10
ALDEHYDES SMOKE PARTICULARS
I WET I
PPMV
84.10
"2.50
79.70
79.20
79.80
79. 10
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
SHP
9H
72
49
25
0
0
MASS EMI
CO
LB/IK
LB FUEL
.30
.24
.41
.22
.05
.93
MASS EMI
HC
LB/IK
LB FUEL
0.87
1.15
1.05
1.40
1.43
0.94
MASS EMI
N02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/IK
LB FUEL
3070.00
3070.00
3070.00
3070.00
3060.00
3070.00
MASS EMI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/IK
LB FUEL
8.58
8.69
B.36
8.20
8.21
9.05
MASS EMI
cn
LB/HR
0.65
0.61
0.68
0.57
1.40
0.91
MASS EMI
HC
LB/HR
0.43
0.56
0.51
0.66
0.66
0.44
MASS EMI
NO 2
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
Cl)2
L8/HR
1525. 79
1501.23
1476.67
1445.97
1407.60
1455. 13
XASS EMI
ND
LB/HR
-0.00
-0.00
-o.no
-0.00
-0.00
-0.00
MASS EM
NOX
LB/HR
4.26
4.25
4.02
3.86
3. 77
4.29
POWER
PERCENT
RATF.O
SHP
99
72
CO
LB/IK HP-HR
0.530
0.499
0.566
0.490
1.276
0.863
LR/IK HP-HR
1247.206
1234.129
1228.853
1232.504
1282.145
1374.920
THC
LB/IK HP-HR
0.353
0.463
0.421
0.562
0.598
0.420
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
-0.000
-0.000
-0.000
-o.ono
-c.ooo
-0.000
LB/IK HP-HR
3. 414
3.493
3.347
3.292
3.438
4.051
111-17
-------
DATE! ./14/T1
TEST ORGANIZATION! AIREICARCH
ENGINE SUPPLIER I AIRESEARCH
ENGINE DATA «»***»«»*»*»»»*»»»«»»*»»
CAL ID NUMBER! 42 ENGINE TYPE AND NOOIll GTCPtV-UO SERIAL NUMBER!
RATED SHAFT HORSEPOWER! 160.
ENGINE TOTAL TINE! 0. MRS
TINE SINCE HOT SECTION OVERHAUL! 0. HRS
TIME SINCE!
Nl COMPRESSOR OVERHAUL! 0. HRS
N2 COMPRESSOR OVERHAUL! 0. HRS
COMBUSTOR CAN REPLACEMENT! 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL! 0. HRS
Nl TURBINE OVERHAUL I 0. HRS
N2 TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO! 1.928
«»»»»»»»»
FINISH 101.00
FINISH 28.TO
FUEL! AV KEROS
OPERATIONAL DATA «»«««»
INLET AIR TEMPERATURE, DEGREES Fl START 101.00
ATMOSPHERIC PRESSURE! START 28.70
INLET AIR HUMIDITY. LBS H20/L8 AIRl 0.0030
RELATIVE HUMIDITY! 12.00 PERCENT
SAMPLE LINE! TEMPERATURE. DEGREES C! -0.00. FLOW RATE. LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SEC! -0.00
NUMBER OF TESTS! 5
COMMENTS!
SHP LOADING ONLY
TEST
MODE
I/ 0
6/ I
ll/ 6
16/11
20/16
SHAFT
HP
0.0
39.90
78.50
116.90
15*.90
AIR
HP
0.0
0.0
0.0
0.0
0.0
ENGINE
SPEED
RPM
Nl
41700.00
41600.00
41400.00
41300.00
41100.00
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CORRECTED
FUEL
FLOW
LB/HR
122.80
137.00
155.00
177.00
207.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
F/A
CALC
FROM
EMISSIONS
0.006900
0.007900
0.009100
0.010500
0.011900
COMPRESSOR
INLET
TEMP
DEGREES F
95.00
100.00
102.00
102.00
104.00
COMPRESSOR BLEED
DISCHARGE FLON
PRESSURE LB/KIN
PSIA
55.60
55. 10
54.80
54.40
53.60
0.0
0.0
0.0
0.0
0.0
POKER
PERCENT
RATED
SHP
0
24
49
73
96
EXHAUST
GAS
TEMP
DEGREES F
515.00
585.00
655.00
730.00
815.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
CO
I WET I
PPNV
146.80
160.90
180.80
200.20
235.70
CO
2
IHETI
PERCENT
1.41
1.62
1.85
2.13
2.42
THC
IWFT)
PPMV
26.30
24.70
20.80
18.20
27.30
NO
(WET)
PPMV
12.00
14.40
20.10
22.00
26.50
NO
2
(WET)
PPMV
6.70
8.20
0.40
10.40
11.60
NO
X
IWET)
PPMV
18.70
22.70
28.50
32.40
38.00
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-o.no
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
SHP
0
24
49
73
96
MASS EMI
CO
L8/1K
LB FUEL
20.29
19.42
19.01
19.33
18.92
MASS EMI
MC
LB/IK
LB FUEL
2.07
1.70
1.25
0.95
1.25
MASS EMI
N02
IB/ IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/1K
IB FUEL
3070.00
3070.00
3060.00
3060.00
3050.00
MASS EMI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/IK
LB FUEL
4.25
4.49
4.92
4. as
5.01
IASS EMI
CO
LB/HR
MISS EMI
HC
LB/HR
MASS ENI
HQ2
LB/HR
MASS EMI
CO 2
LB/HR
MASS EM
NO
LB/HR
2.49
2.66
2.95
3.24
3.92
0.25
0.23
0.19
0.17
0.26
-0.00
-0.00
-0.00
-0.00
-0.00
377.00
420.59
474.30
541.62
631.35
-0.00
-0.00
-0.00
-0.00
-0.00
MASS ENI
NOX
LB/HR
0.52
0.62
0.76
0.86
1.04
POWER
PERCENT
RATED
SHP
LB/IK HP-HR
LB/IK HP-HR
HORSEPOWER-HR BASIS NOT CALCULABLE*****
24 66.694 10541.094
49 37.538 6042.031
73 27.748 4633.188
96 25.278 4075.854
THC
LB/IK HP-HR
5.841
2.470
1.444
1.674
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-MR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
15.431
9.723
7.3S4
6.702
111-18
-------
OATEI 6/U/71
TEST ORGANIZATION: AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
FNG1NE DATA
CAI ID NUMBER: if ENGINE TYPE AND MODEL:
RATED SHAFT HORSEPOWER: 160.
ENGINE TOTAL TINEl 0. MRS
TINE SINCE HOT SECTION OVERHAUL: 0. HRS
TINE SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
NZ COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.428
SERIAL NUMBFRl
P-567
FINISH 110.00
FINISH 28.70
FUEL: AV KEROS
OPERATIONAL DATA *«»»«»»«»»«»««»»»«»«
INLET AIR TEMPERATUREi DECREES F: START 110.00
ATMOSPHERIC PRESSURE: START 28.70
INLET SIB HUMIDITY, LBS H20/LB AIR: 0.0050
RELATIVE HUMIDITY: 12.00 PERCENT
SAMPLE LINE: TEMPERATUREt DEGREES C: -0.00, FLON RATE, LITFRS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUM8ER OF TESTS: 5
COMMENTS:
COMBINATION SHP/BLEEO LOADING
TFST
MODE
22/ 0
11/22
IS/ 19
10/15
5/10
POWER
PERCENT
RATFO
SHP
96
12
48
24
0
POWER
PERCFNT
RATED
SHP
06
72
48
24
0
POWER
PERCENT
RATED
SMP
96
72
48
24
0
SHAFT
HP
154.50
115.60
77.90
39.00
0.0
EXHAUST
GAS
TFMP
DEGREES f
1150.00
1150.00
11 SO. 00
USD. 00
1 ISO. 00
MASS EMI
CO
LR/1K
LB FUEL
12.64
15.33
16.93
IS. 40
14.11
POWER ENGINE CORRECTED GAS GFN
AIR SPEED FUEL AIR FLOW
HP RPM FLOW LS/SEC
Nl 12 LB/HR
88.96 41000.00 -0.00 279.50 -0.00
114.77 41000.00 -0.00 272.50 -0.00
129.21 41100.00 -0.00 262.50 -0.00
144.10 41200.00 -0.00 251.50 -0.00
159.30 41200.00 -0.00 241.50 -0.00
EXHAUST CO CO THC NO
GAS (WET) 2 IWET) IWET)
PRESSURE PPMV IWFTI PPMV PPMV
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
0.22
0.26
0.30
0.22
0.18
CO
LB/1K
14.
18.
21.
21.
21.
HP-HR
514
132
455
156
421
PERCENT V
222
252
577
261
248
MASS EMI
NH2
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
CD
2
.90
.10
.90
.80
.40
MASS EMI
C02
LR/1K
Lfl FUEL
3030.00
3030.00
3030.00
3030.00
3020.00
3.40 6.
3.17 7.
3.16 8.
3.?7 6.
3.38 5.
MASS FMI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
THC
LB/IK HP-HR LB/IK HP-HR
3478.560
3584.189
3040.286
4161.965
4578.332
0.253
0.311
0.376
0.306
0.279
80 44.70
60 40.30
50 37.30
60 42.10
60 44.60
MASS EMI MASS
NOX CO
LR/1K LB/
LB FUEL
5.14 ).
5.21 4.
5.11 4.
5.22 3.
5.19 3.
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
F/A COMPRESSOR COMPRESSOR BLEFO
CALC INLET DISCHARGE FLOW
FROM TEMP PRFSSURF LB/MIN
EMISSIONS DEGREES f PSIA
0.016800 107.00 50.00 66.12
0.015700 110. 00 49.00 R6.54
1.015600 111.00 47.50 100.31
0.016200 110.00 46.00 US. 77
0.01IS700 114.00 44.10 132.81
NO NO ALDEHYDES SMOKE "ARTICULATES
? X
IWET) IHET)
PP"V PPMV
10
11
13
1 1
11
FMI
H«
53
18
44
87
41
.50 55
.BO 52
.80 51
.90 54
.90 55
MASS CMI
HC
LB/HR
0.06
0.07
0.08
0.06
0.04
ND
2
L8/1K HP-
-0.000
-0.000
-o.ooo
-0.000
-0.000
.10 -0.00
.10 -0.00
.50 -0.00
.00 -0.00
.50 -0.00
-0
-n
-0
-0
-0
MASS EMI MASS EMI
NO 2
LR/HR
-0.00
-0.00
-0.00
-0.00
-0.00
C02
LVHR
846.88
825.67
795.37
767.04
729.11
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
MASS EMI MASS EMI
NU NOX
LB/HB Lfl/HR
-0.00 1.44
-0.00 1.42
-0.00 1.34
-0.00 1.31
-0.00 1.25
NO
MR IH/1K
5
6
6
7
7
X
HP-MR
.897
.161
.480
.149
.862
111-19
-------
OATEi 6/14/71
TEST ORGANIZATION I AIRESEAACH
ENGINE SUPPLIER! AIRESEAUCH
ENGINE 0»T» »»»«»»«**»«
C»L 10 NUMBER! *» ENGINE TYPE MO MODEL! GTCP85-180
RATED SHAFT HORSEPOWER! 160.
ENGINE TOTAL TINEl
TINE SINCE HOT SECTION OVERHAUL!
TINE SINCE!
SERIAL NUNBERl
P-JOT
0. MRS
0. MRS
Nl CONPRESSOR OVERHAULl 0. MRS
N2 CONPRESSOR OVERHAUL: 0. MRS
CONDUCTOR CAN REPLACENENTl 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL! 0. HRS
Nl TURBINE OVERHAUL! 0. HRS
NZ TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO: 1.928
FINISH 10*.00
FINISH 28.58
FUEL: AV KEROS
OPERATIONAL DATA ««*»*«»«««**
INLET AIR TEMPERATURE, DEGREES ft START 104.00
ATMOSPHERIC PRESSURE! START 28.58
INLET AIR HUMIDITY, LBS H20/LB AIR! 0.0052
RELATIVE HUMIDITY! 12.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOW RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME. SEC" -0.00
NUMBER OF TESTS! 5
COMMENTS!
SHP LOADING ONLY
TEST
MODE
I/ 0
6/ I
ll/ 6
16/11
20/16
POWER
SHAFT
HP
0.0
39.50
79.00
119.30
157.80
AIR
HP
0.0
0.0
0.0
0.0
0.0
ENGINE
SPEED
RPN
Nl
41700.00
41400.00
41400.00
41100.00
41000.00
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CORRECTED
FUEL
FLOW
LB/HR
116.00
134.00
153.00
175.00
194.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
F/A
CALC
FROM
EMISSIONS
0.006500
0.007700
0.008700
0.010200
0.011600
COMPRESSOR
INLET
TEMP
DEGREES F
105.00
104.00
104.00
104.00
104.00
COMPRESSOR BLEED
DISCHARGE FLOM
PRESSURE LB/MIN
PSIA
54.20
53.JO
53.20
53.30
53.30
0.0
o.o
0.0
0.0
0.0
POWER EXHAUST
PERCENT GAS
RATED TEMP
SHP DEGREES F
0
24
49
74
96
510.00
580.00
645.00
710.00
790.00
EXHAUST
GAS
PRESSURE
PSU
-0.00
-0.00
-0.00
-0.00
-o.oo
CO
(WET)
PPMV
125.30
128.10
140.40
152.80
177.30
CO
2
(WET)
PERCENT
1.33
1.56
1.78
2.07
2.35
THC
(MET)
PPMV
16.90
12.40
11.50
8.70
7.10
NO
INETI
PPMV
11.40
14.90
17.70
22.40
27.20
NO
2
(wen
PPMV
5.90
7.30
8.50
10.30
10.90
NO
X
(WET)
PPMV
17.30
22.20
26.20
32.60
38.10
ALDEHYDES SMOKE P4RTICULATES
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
SHP
0
24
49
74
98
MASS EMI
CO
LB/U
LB FUEL
16.45
16.05
15.44
14.38
14.66
MASS EMI
KC
LB/IK
LB FUEL
1.42
0.89
0.72
0.47
0.33
MASS EMI
N02
LB/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/IK
LB FUEL
3080.00
3080.00
3070.00
3070.00
3060.00
MASS EMI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/U
LB FUEL
4.19
4.57
4.73
5.04
5.17
MASS EM
CO
LB/HR
2.14
2.15
2.36
2.52
2.84
MASS EMI
HC
LB/HR
0.17
0.12
0.11
0.08
0.06
MASS EMI
Nri2
LB/HR
-0.00
-0.00
-o.oo
-0.00
-0.00
MASS EMI
CD2
L8/HR
357.28
412.72
469.71
537.25
593.64
MASS EMI
NO
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
IB/MR
0.49
0.61
0.72
0.68
1.00
POWER
PERCENT
RATED
SHP
LB/U MP-HR
LB/IK HI>-HR
HORSEPOWER-MR BASIS NOT CALCULABLE**"*
24 54.434 10448.60?
49 29.903 5945.695
74 21.091 4503.352
98 18.018 3761.976
THC
LB/IK HP-MR
3.012
1.398
0.684
0.409
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
LR/1K HP-HR
-0.000
-0.000
-0.000
-0.000
NO
X
LB/U HP-HR
15.507
9.168
7.396
6.354
111-20
-------
OtTEl 6/14/71
TEST ORGANIZATION: AIRESEARCH
ENGINE SUPPLIER I AIRESEARCH
ENGINE 0»T» *****
CAL 10 NUMBER: »« ENGINE TYPE AND NODELI GTCPBJ-IBO
R»TED SHIFT HORSEPOWER: 160.
ENGINE TOTAL TINE:
TIME SINCE HOT SECTION OVERHAUL!
TIME SINCE:
SERIAL NUMBER:
o. HRS
o. HRS
NI COMPRESSOR OVERHAUL: o. MRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.928
FINISH IOT.OO
FINISH 28.5B
FUEL: AV HERDS
OPERATIONAL DATA «««««
INLET AIR TEMPERATURE, DEGREES F: START IOT.OO
ATMOSPHERIC PRESSURE: START 26.58
INLET AIR HUMIDITY, L8S H20/LB AIR: 0.0052
RELATIVE HUMIDITY: 12.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
CnMBINATION SUP/BLEED LOADING
TEST
MODE
22/ 0
19/22
15/19
10/15
5/10
POWER
PERCENT
RATED
SHP
97
71
49
24
0
POWER
PERCENT
RATED
SHO
97
71
48
24
0
POWER
PERCENT
RATED
SHP
97
71
46
24
0
SHAFT
HP
156.10
117.90
77.40
38.90
0.0
EXHAUST
GAS
TEMP
DEGREES F
1150.00
1150.00
1 150.00
1150.00
U50.00
MASS EMI
CO
LB/IK
LB FUEL
10.08
11.16
11.42
11.48
10.95
CO
LB/IK
10.
11.
11.
15.
15.
POWER
AIR
HP
93.41
117.17
115.59
152.47
161.62
EXHAUST
GAS
PRESSURE
PSI A
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
0.01
0.07
0.09
0.07
0.06
ENGINE
SPEED
RPM
NI
40600.00
40600.00
40600.00
40700.00
40800.00
CO
(WETI
PPMV
174.10
194.50
194.60
198.70
191.10
MASS EMI MASS
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
IbETI
PERCENT
11.40
3.30
3.29
1.34
3.4}
CORRECTED
FUEL
FLOW
LB/HR
271.50
271.50
260.50
252.50
235.00
THC
IWET)
PPMV
V
1.00
2.10
2.50
2.20
2.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
NO
IWET1
PPMV
44.40
43.50
41.70
41.00
41.20
EMI MASS EMI MASS fl MASS
N02 C02
LB/IK LB/IK
LB FUEL LB
-0.00 3010
-0.00 1010
-0.00 1010
-0.00 1030
-0.00 1030
CO
2
HP-HR LB/IK HP-HR
964
124
971
142
780
1294.440
1501.055
1705.881
1997.856
4405.586
NO
LB/IK
NOX CO
F/A
CALC
FROM
EMISSIONS
0.016400
0.016300
0.016200
0.016500
0.016900
NO
2
(ucri
PPMV
10.00
9.40
10.00
9. 10
9.50
EMI MASS
HC
COMPRESSOR CCMPRESSOR
INLET
TEMP
DEGREES
105.00
107.00
108.00
108.00
107.00
NO
X
IWET)
PPMV
54.40
53.00
51.70
52.10
52.70
EMI MASS
DISCHARGE
PRESSURE
F PSIA
49.70
48.60
46.90
45.60
41. 70
ALDEHYDES SMOKF
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
FMI MASS EMI »ASS
N02 C02 NO
BLEED
FLOW
LB/HIN
70.08
89.54
107. 18
174.04
137.74
PAPMCUIATES
-o.no
-0.00
-0.00
-0.00
-n.oo
EMI MASS
EM
NOX
LB/IK LB/HR LB/HP LB/HP Lfl/HR I.R/H8 LB/HR
FUEL LB FUEL LB FUEL
.00
.00
.00
.00
.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
LR/1K
0.
0.
0.
0.
0.
HP-HR
035
081
104
099
091
5.16 2.
5.03 1.
4.98 2.
4.94 2.
4.87 2.
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
74 0.
08 0.
93 0.
90 0.
55 0.
LB/1K
-0
-0
01 -0.
02 -0.
02 -0.
02 -0.
02 -0.
NO
2
HP-HR
.000
.000
-0.000
-0
-0
.000
.000
00 922.64 -0.
00 822.64 -0.
00 789.11 -0.
00 765.07 -0.
00 712.05 -0.
NO
K
LB/IK HP-HR
5.M6
5.S71
6.09h
6.515
7.078
00
00
00
00
on
.40
.18
.30
.25
. 14
111-21
-------
OATH 6/lVTl
TSSI ORGANISATION! AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE DATA »«»»»»»»
CAL 10 NUNSERl »» ENGINE TTPE IND MODELS GTCP85-UO
RATED SHAFT HORSEPOWER! 160.
ENGINE TOTAL TINEl
TINE SINCE HOT SECTION OVERHAUL!
TINE SINCE!
SERIAL NUNSERl
P-SIB
0. HRS
0. HRS
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 CONPRESSOR OVERHAUL! 0. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL! 0. HRS
Nl TURBINE OVERHAULI 0. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO! 1.929
FINISH
FINISH
97.00
28.69
FUEL! AV KEROS
OPERATIONAL DATA »«»««»««
INLET AIR TEMPERATURE. DEGREES F: START 97.00
ATMOSPHERIC PRESSURE: START 28.63
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.00*6
RELATIVE HUMIDITY! 13.00 PERCENT
SAMPLE LINE! TEMPERATURE. DEGREES C: -0.00, FLOM RATE, LITERS/NIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS! 5
COMMENTS:
SHP LOADING ONLY
7EST
NODE
II 0
6/ 1
ll/ 6
16/11
20/16
POKER
SHAFT MR
HP HP
0.0
*0.80
79.30
118.30
158.30
0.0
0.0
0.0
0.0
0.0
ENGINE
SPEED
RPN
Nl N2
41600.00
41500.00
41300.00
41100.00
41000.00
-0.00
-0.00
-0.00
-0.00
-0.00
CORRECTED
FUEL
FLOW
LB/HR
119.00
138.00
157.00
176.00
201.JO
GAS GEN
AIR FLOW
L8/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
F/A COMPRESSOR
CALC INLET
FROM TEMP
EMISSIONS DEGREES f
0.006800
0.007900
0.009200
0.010400
0.012200
96.00
96.00
98.00
98.00
99.00
CONPRESSOR
DISCHARGE
PRESSURE
PSIA
54.80
54.60
53.90
53.50
53.00
BLEED
FLOW
L8/NIN
0.0
0.0
0.0
0.0
0.0
POWER
PERCENT
RATED
SHP
0
25
49
73
98
EXHAUST
GAS
TEMP
DEGREES F
490.00
565.00
635.00
710.00
905.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
CO
(WET I
PPMV
160.80
199.00
255.30
266.10
311.50
CO
2
1METI
PERCENT
1.39
1.61
1.87
2.10
2.47
THC
(wen
PPMV
4.00
5.10
6.30
5.30
4.30
NO
(WET)
PPMV
8.40
10.20
12.50
15.40
19.50
NO
2
(KFTI
PPNV
8.80
11.50
12.70
15.50
14.40
ALDEHYDES SNOKF PARTICULATES
I MET I
PPHV
17.20
21.70
25.20
30.90
14.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
SHP
0
25
49
73
98
MASS EMI
CO
L8/1K
IB FUEL
22.59
24.06
26.48
24.53
24.37
MASS EMI
HC
LB/IK
LB FUEL
0.32
0.35
0.38
0.28
0.19
MASS EMI
N02
LB/1K
L8 FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/IK
LB FUEL
3070.00
3060.00
3050.00
3050.00
3040.00
MASS EMI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
NASS FMI
ND<
LB/IK
LB FUEL
3.97
4.31
4.29
4.68
4.36
MASS F.M1
CO
LB/HR
2.69
3.32
4.16
4.32
4.91
MASS EMI
HC
LB/HR
0.04
0.05
0.06
0.05
0.04
MASS EMI
NO 2
LB/HR
-0.00
-0.00
-o.no
-o.oo
-0.00
MASS EM!
C02
LB/HR
365.33
422.28
476.85
536.80
612.56
MASS EMI
NO
LB/HB
-0.00
-o.no
-0.00
-0.00
-0.00
NASS EMI
NOX
LB/HR
0.47
0.59
0.67
0.82
0.88
POWER
PERCENT
RATED
SHP
LB/IK HP-HR
LB/IK HP-HR
HORSEPOUER-HR BASIS NOT CALCULABLE*"**
25 81.369 10349.992
49 52.422 6038.461
73 36.496 4537.613
98 31.015 3869.614
THC
LB/IK HP-HR
1.197
0.744
0.412
0.247
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
NO
K
LB/IK HP-HR
14.581
8.503
6.963
5.554
111-22
-------
OiTEl 6/13/71
resr ORSANIIATIONI AIRESEARCH
ENGINE SUPPLIER" AIRESEARCH
ENGINE OAT« *»»**«
CAL ID NUMBER: «j ENGINE TYPE AND MODEL: GTCPBS-UO
RATED SHAFT HORSEPOWER: 160.
ENGINE TOTAL TINEl
TINE SINCE HOT SECTION OVERHAUL:
TINE SINCE:
SERIAL NUMBER:
o. HRS
o. HRS
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
HZ TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.928
FINISH 109.00
FINISH 28.63
FUEL: AV HERDS
OPERATIONAL DATA »««»«««««««««««««
INLET AIR TEMPERATURE, DEGREES F: START 109.00
ATMOSPHERIC PRESSURE: START 28.63
INLET AIR HUMIDITY. LBS H2D/LB AIR: 0.00*6
RELATIVE HUMIDITY: 13.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TINE. SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
COMBINATION SHP/BLEED LOADING
TEST
MODE
22/ 0
19/22
15/19
10/15
5/10
POWER
PFRCENT
RATED
SHP
97
7»
48
24
0
POWER
PERCENT
RATED
SHP
97
73
48
24
0
POWFR
PERCENT
HATED
SMP
97
73
48
24
0
SHAFT
HP
156.80
117.20
78.30
39.10
0.0
EXHAUST
GAS
TEMP
DEGREES F
1150.00
1150.00
1150.00
1150.00
1150.00
MASS EMI
cn
LB/IK
L8 FUEL
9.74
15.93
17.04
17.64
17.05
cn
L8/1K
10.
18.
20.
23.
25.
POWER
AIR
HP
97.61
117.67
134.40
151.38
163.84
FXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
0.02
0.23
0.32
0.35
0.31
ENGINE
SPEED
RPM
Nl
40600.00
40700.00
40600.00
40800.00
40900.00
CO
IWEM
PPMV
187.20
282.90
298.20
314.60
309.40
MASS EMI MASS
CORRECTED
FUEL
FLOW
GAS GEN
AIR FLOW
LB/SEC
N2 LB/HR
-0.00 281
-0.00 268
-0.00 261
-0.00 253
-0.00 248
CO
2 1
IWET)
PERCENT V
3.70
3.41
3.36
1.42 1
1.48
EMI MASS EMI
.50
.50
.50
.50
.50
THC
WET)
PPMV
0.60
7.10
9.70
1. 10
9. BO
-0.00
-0.00
-0.00
-0.00
-0.00
NO
IWET)
PPMV
48.30
39.80
36.80
37.00
37.80
MASS EMI 1ASS
ND2 C02 NO
IB/IK LB/IK LB/IK
L8 FUEL LB
-0.00 3020
-0.00 3020
-0.00 3020
-0.00 3020
-0.00 3020
CO
2
HP-HR LR/1S HP-HR
778
210
956
480
855
3141.578
3452.418
3712.895
4019.110
4580.398
FUFL LB FUEL
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
IHC
LB/IK HP-HR
0.019
0.262
0.390
0.472
0.469
NDX CO
F/A
CALC
FROM
EMISSIONS
o.oiRioo
0.016900
0.016600
0.017000
0.017300
NO
2
IWET)
PPMV
9.40
10.20
12.40
12.10
11.50
EMI MASS
HC
COMPRESSOR
INLET
TF.MP
DEGREES F
103.00
1 10.00
110.00
1 10.00
110.00
CCMPRFSSOR
DISCHARGE
PRESSURE
BLEED
FLOW
LB/PIN
PSIA
9
9
7
6
4
NO ALDEHYDES
X
IWET)
PPMV
57.70
50.00
49.30
49. 10
49.30
F.rl MASS FM
NO 2
LB/IK LB/HR LB/HB LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
.80
.00
. 7(1
.40
.70
SMOKE
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
I MASS EM 1ASS
C02
NO
71.35
an. 73
104.08
120.55
135.61
P«»IICULArES
-0.00
-0.00
-0.00
-0.00
-0.00
EMI 14SS EMI
NOX
LB/HR LB/HP LB/HR
LB FUEL
4.93 2.
4.63 4.
4.63 4.
4.53 4.
4.4S 4.
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
74 0.
28 0.
46 0.
47 0.
24 0.
L3/1K
-0
-0
-0
-0
-0
00 -0.00
06 -0.00
08 -0.00
09 -0.00
08 -0.00
NO
2
HP-HR
.000
.000
.000
.000
.000
850.
aio.
789.
765.
750.
Nl
X
11 -0.
87 -0.
7) -0.
57 -0.
47 -0.
00 1.39
00 1.24
00 1.21
00 1.15
OC I. II
LS/1K HP-HR
5.454
5.287
5.637
6.025
6.770
111-23
-------
DATEl 6/15/71
TEST ORGANIZATION! AIRESEARCH
ENGINE SUPPLIER! AIRESEARCM
ENGINE DATA *»*»********«»*»»»
C»L ID NUMBER I 4S ENGINE TYPE AND NOOELl GTCP85-I80
RATED SHAFT HORSEPOWER 1 160.
ENGINE TOTAL TIHEl
TINE SINCE HOT SECTION OVERHAULi
TINE SINCEl
SERIAL NUNBERl
0. MRS
0. HRS
HI COMPRESSOR OVERHAULi 0. HRS
N2 CONPRESSOR OVERHAULI 0. MRS
CONBUSTOR CAN REPLACENENTI 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL! 0. HRS
Nl TURBINE OVERHAULI 0. HRS
N2 TURBINE OVERHAULI 0. HRS
FUEL H/C RATIOl 1.928
FINISH 106.00
FINISH 28.64
FUELl AV KEROS
OPERATIONAL DATA «««»»««»«»»««»»»*
INLET AIR TENPERATURE, DEGREES F: START 106.00
ATMOSPHERIC PRESSURE! START 28.6*
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.00*6
RELATIVE HUNIDITVI 9.00 PERCENT
SAMPLE LINE! TEMPERATURE! DEGREES C: -0.00, FLOW RATE. LITERS/KIN: -0.00
SAMPLE LINE TRANSPORT TINE, SECl -0.00
NUMBER OF TESTS: 5
COMMENTS:
SHP LOADING ONLY
TEST
MODE
I/ 0
6/ 1
ll/ 6
16/11
20/16
POWER
SHAFT
HP
0.0
40.70
79.10
118.30
157.90
AIR
HP
0.0
0.0
0.0
0.0
0.0
ENGINE
SPEED
RPM
NI
41600.00
41400.00
41200.00
41100.00
40900.00
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CORRECTED
FUEL
FLOW
L6/HR
114.00
131.00
153.00
174.00
205.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
F/A
CALC
FROM
EMISSIONS
0.006800
0.007700
0.009100
0.010300
0.012000
COMPRESSOR
INLET
TEMP
DEGREES F
105.00
106.00
107.00
107.00
107.00
COMPRESSOR BLEED
DISCHARGE FLOW
PRESSURE LB/NIN
PSIA
53.40
52.90
52.60
52.40
51.90
0.0
0.0
0.0
0.0
0.0
POWER
PERCENT
RATED
SMP
0
25
49
73
98
EXHAUST
GAS
TEMP
DEGREES F
580.00
580.00
660.00
740.00
850.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
CO CO
IWETI 2
PPNV (WET)
PERCENT V
190.90
227.30
273.00
261.20
288.30
1.38
1.55
1.83
2.08
2.42
THC
(WETI
PPNV
50.80
55.50
56.30
49.00
36.90
NO NO
(WETI 2
PPHV IWETI
PPMV
8.70
11.20
13.10
17.30
23.30
8.70
11.20
12.50
14.10
15.30
NO
X
(WET)
PPMV
17.40
22.40
25.60
31.30
38.60
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
BATED
SHP
0
25
49
71
98
MASS EMI
CO
L8/IK
LB FUEL
27.00
28.51
28.88
24.17
22.98
MASS EMI
HC
IB/IK
LB FUEL
4.10
3.98
3.19
2.61
1.68
MASS ENI
N02
IR/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/IK
LB FUEL
3060.00
3050.00
3040.00
3040.00
3040.00
MASS EMI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/IK
LB FUEL
4.03
4.63
4.44
4.80
5.06
MASS EMI
CO
IB/ HI)
3.08
3.79
4.42
4.24
4.71
MASS EMI
HC
L8/HR
0.47
0.53
0.52
0.46
0.35
MASS EMI
N02
Lfl/HR
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EHI
C02
LB/HH
348.84
405.65
465.12
528.96
623.20
MASS EMI
NO
18/HR
-0.00
-0.00
-0.00
-0.00
-0.00
MASS ENI
NOX
LB/HR
0.46
0.62
0.68
0.84
1.04
POWEP
PERCENT
RATED
SMP
LB/IK HP-HR
LB/IK HP-HR
HORSEPOWER-HR BASIS NOT CALCULABLE*****
25 9).169 9966.820
49 55.856 5880.148
73 15.846 4471.140
98 29.841 1946.800
THC
LB/IK HP-MR
12.999
6.567
3.846
2.186
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
NO
X
LB/IK HP-HR
15.117
8.592
7.066
6.567
111-24
-------
OtTEl 6/15/71
TEST ORGANIZATION: AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE OAT*
CAL ID NUMBER: 92 ENGINE TYPE AND MODEL: GTCPes-ieo
RATED SHAFT HORSEPOWER: 160.
ENGINE TOTAL TINE: 0. HRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: o. HRS
N2 COMPRESSOR OVERHAUL: o. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
M TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
SERIAL NUMBER:
FUEL: AV KEROS
FUEL H/C RATIO: 1.928
OPERATIONA
INLET AIR TEHPFRATURE, DECREES F : START 111.00 FINISH 111.00
ATMOSPHERIC PRESSURE: START 28.6* FINISH 28.6*
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0046
RELATIVE HUMIDITY: 9.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/NIN:
SAMPLE LINE TRANSPORT TIMF. SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
COMBINATION SHP/BLEEO LOADING
TFST
MODE
22/ 0
19/22
15/19
10/15
5/10
POWER
PFRCFNT
RAIED
SHP
9fl
71
48
25
0
POKER
PERCENT
RATED
SHP
96
71
48
25
0
POHFB
PERCENT
RATED
SHP
9fl
73
48
25
0
SHAFT
HP
157.20
117.20
7B.30
40.10
0.0
EXHAUST
GAS
TEMP
DEGREES F
1150.00
1150.00
1150.00
1150.00
1150. On
MASS EMI
CO
L6/IK
LB FUEL
10.68
15.49
17.24
19.20
19.20
CO
LB/IK
11.
17.
21.
25.
20.
POKER ENGINE
AIR SPEED
HP RPM
NI
85.18 40700.00
116.26 40700.00
117.73 40BOO.OO
149.20 40800.00
164.95 40800.
EXHAUST
GAS
00
CO
(HEM
PRESSURE PPMV
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
0.19
0.19
0.27
0.44
0.49
HP-HR
716
151
108
507
111
197.
265.
289.
324.
331.
MASS EMI
NO?
LB/IK
L9 FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
L6/1K HP-H
3317.750
13X2.688
1697.595
4012.324
4421. 4BO
10
70
60
10
50
MASS
CORRECTED GAS GEN
FUEL AIR FLOK
FLOW LB/SEC
N2 LB/HR
-0.00 266.50 -0.00
-0.00 261.50 -0.00
-0.00 264.50 -0.00
-0.00 251.50 -0.00
-0.00 241.50 -0.00
CD
2
IHET]
PFRCENT V
3.55
1.10
1.21
3.25
3.32
EMI MASS EM
C02 NO
LB/IK LR/1K
LB
3020
1020
3020
1020
1020
[R
THC NO
IUET) IHETI
PPMV PPMV
6.10 51.60
5.7Q 43.10
7.90 37.90
11.00 35.40
14.80 15.60
1 MASS EMI MASS
NOX CO
F/A COMPRESSOR COMPRESSOR
CALC INLET DISCHARGE
FROM TEMP PHFSSUKE
EMISSIONS OEGRFFS F PSIA
0.017600 112.00 49.60
0.016300 112.00 49.70
0.016000 110.00 48.50
0.016100 110.00 47.20
0.016400 110.00
NO
2
(yen
PPMV
8.80
11. 10
15.00
14.70
14.60
NO
X
IHCT)
PPMV
00.40
54.20
52.10
50.10
50.20
EMI MASS FNI MASS
45
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
.70
SMOKE
-n.oo
-0.00
-0.00
-0.00
-0.00
FMI MASS EMI MASS
HC N02 Ul?
LB/IK IB/HR
ND
BLEED
FLOM
LB/MIN
63.40
06. 16
104.91
116.77
133.42
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
FMI MASS FMI
Nnx
LB/MR LB/HR LO/HK LB/HB LB/HR
FUFL LB FUEL LB FUEL
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
THC
LB/IK HP-HR
0.211
0.212
0.128
0.586
0.717
5.17 2.
5.19 4.
5.17 4.
4.87 4.
4. 7H 4.
NO
LB/IK HP-HR
-0.000
-0.000
-o.ono
-0.000
-0.000
85
05
56
83
64
0.05 -0.
0.05 -0.
0.07 -0.
0.11 -0.
0.12 -0.
NO
2
IH/1K HP-MH
-0.000
-0.000
-0.000
-o.ono
-0.000
00 304.
00 739.
00 79H.
00 759.
00 729.
NO
X
81 -0.
73 -0.
79 -0.
53 -0.
31 -0.
00 1.43
00 1.16
00 1.37
00 1.22
00 1.15
LB/IK HP-HR
5.90?
5.416
6. 125
6.466
6.995
111-25
-------
DATE! 6/14/71
TEST ORGANIIATIONl AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE DAT*
C*L ID NUMBER! 46 ENGINE TYPE AND MODEL! GTCP85-1BO
RATED SHAFT HORSEPOWER! 160.
ENGINE TOTAL TINEl 0. MRS
TINE SINCE HOT SECTION OVERHAULi 0. HRS
TIME SINCE!
Nl COMPRESSOR OVERHAUL! 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COM8USTOR CAN REPLACEMENT! 0. HRS
FIRST STAGE NOZ1LE GUIDE VANE OVERHAUL! 0. HRS
Nl TURBINE OVERHAUL! 0. HRS
N2 TURBINE OVERHAULI 0. HRS
FUEL H/C RATIO: 1.428
SERIAL NUMBER!
FINISH
FINISH
97.00
28.62
FUEL: AV KEROS
OPERATIONAL DATA «*»««««»«»»
INLET AIR TEMPERATURE, DEGREES f. START 97.00
ATMOSPHERIC PRESSURE! START 28.62
INLET AIR HUMCOITr, LBS H20/LB AIR: 0.0042
RELATIVE HUMIDITY: 15.00 PERCENT
SAMPLE LINE: TEMPERATURE! DEGREES C: -0.00. FLOW RATEi LITERS/MIN:
SAMPLE LINE TRANSPORT TIME. SEC: -0.00
NUMBER OF TESTS! 5
COMMENTS!
SHP LOADING ONLY
TEST
MODE
I/ 0
6/ 1
ll/ 6
16/11
20/16
POKER
SHAFT
HP
0.0
39.70
79.10
118.60
198.30
AIR
HP
0.0
0.0
0.0
0.0
0.0
FNGINE
SPEED
RPM
Nl
41600.00
41400.00
41200.00
41200.00
41000.00
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CORRECTE1
FUEL
FLOW
L8/HR
118.00
139.00
156.00
180.00
208.00
GAS GEN
AIR FLOW
IB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
F/A COMPRESSOR
CALC INLET
FROM TEMP
EMISSIONS DEGREES F
0.006700
0.008100
0.009200
0.010400
0.012000
94.00
95.00
98.00
98.00
98.00
COMPRESSOR BLEED
DISCHARGE FLOW
PRESSURE LB/MIN
PSIA
55.40
54.40
54.10
54.20
54.00
0.0
0.0
0.0
0.0
0.0
POWER EXHAUST
PERCENT GAS
RATED TEMP
SMP OEGREES F
0
24
49
74
98
500.00
585.00
655.00
740.00
850.00
FXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-o.oo
-0.00
-0.00
CO
IWETI
PPMV
143.50
164.80
185.70
206.70
236.90
CO
2
(WET)
PERCENT V
1.36
1.64
1.87
2.12
2.45
THC
(WET)
PPMV
25.00
26.40
24.50
22.40
19.00
NO
(WET!
PPNV
10.10
14.70
17.70
21.30
25.80
NO
2
IUET)
PPMV
7.40
9.80
11.00
12.20
13.00
ALDEHYDES SMOKF PARTICULATES
IWFT)
PPMV
17.50
24.50
28.70
33.60
38.80
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
SHP
0
24
49
74
98
MASS EMI
CO
IB/ IK
LB FUEL
20.58
19.60
19.39
IB. 96
IB. 75
MASS EMI
HC
LB/1K
LB FUEL
2.05
1.79
1.46
1.18
0.86
MASS EMI
N02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/IK
LB FUEL
3070.00
3070.00
3060.00
3050.00
3050.00
MASS EMI
NO
LB/IK
16 FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS ENI
NOX
LB/IK
LB FUEL
4.12
4.80
4.92
5.06
5.04
MASS EMI
CO
LR/HR
2.43
2.72
3.02
3.41
3.90
MASS ENI
HC
LB/HR
MASS FMI
NH2
LB/HR
MASS EMI
CO 2
LB/HR
MASS EMI
NO
L8/HR
MASS EMI
NOX
LB/HR
0.24
0.25
0.23
0.21
0. IB
-0.00
-0.00
-0.00
-0.00
-0.00
362.26
426.73
477.36
549.00
634.40
-0.00
-0.00
-0.00
-0.00
-0.00
0.49
0.67
0.77
0.91
1.05
POWER
PERCENT
RATED
SHP
LB/IK HP-HR
LB/IK HP-HR
HORSEPOVER-HR BASIS NOT CALCULABLE»*»*«
24 68.635 10748.859
49 38.243 6034.891
74 28.783 4629.000
98 24.641 4007.579
THC
LB/IK HP-HR
6.281
2.887
1.786
1.131
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
Lfl/lK HP-HR
16.799
9.713
7.677
6.625
111-26
-------
DATE! 6/16/71
TEST ORGANIZATION: AIRESEARCH
ENGINE SUPPLIERl AIRESEARCH
ENGINE DATA
CAL ID NUMBER! 63 ENGINE TYPE AND MODELl GTCP85-160
RATED SHAFT HORSEPOWER: 160.
ENGINE TOTAL TINE: 0. KRS
TINE SINCE HOT SECTION OVERHAUL: 0. KRS
TINE SINCE:
NI COMPRESSOR OVERHAUL: o. HRS
N2 CONPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOULE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
NZ TURBINE OVERHAUL: o. HRS
FUEL H/C RATIO: 1.928
SERIAL NUMBER:
FINISH 10*.00
FINISH 28.62
FUEL: AV KEROS
OPERATIONAL DATA
INLET AIR TEMPERATURE, DEGREES F: START 104.00
ATMOSPHERIC PRESSURE: START 28.62
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.00*2
RELATIVE HUMIDITY: 15.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/KIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 6
COMMENTS:
COMBINATION SHP/BLEEO LOADING
TFST
NODE
22/ 0
19/22
15/19
10/15
5/10
3/ >
POWER
PERCENT
RATED
SHP
98
71
49
24
0
0
POWER
PERCENT
RATED
SHP
98
71
49
24
0
0
POWER
PF.RCENT
RATED
SHP
98
71
49
24
0
0
SHAFT
HP
157.50
117.70
78.50
39.30
0.0
0.0
EXHAUST
GAS
TEMP
DEGREES F
1150.00
1150.00
1150.00
1150.00
1150.00
950.00
MASS EMI
CO
LB/IK
LB FUFL
11.55
12.50
14.59
15.44
15.28
22.62
CO
LB/IK
12.
14.
17.
20.
22.
35.
POWER ENGINE
AIR SPEED
HP RPM
NI
89.64 40800.00
118.21 40900.00
134.60 40900.00
151.98 41000.00
167.56 4100.00
132.95 41300.00
EXHAUST
GAS
PRESSUR
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
0.14
0.11
0.16
0.22
0.26
1.11
HP-HR
922
229
558
054
020
135
CO
(UETI
E PPMV
200.60
214.30
247.70
258.70
265.70
300.00
MASS EMI MASS
CORRECTED GAS GEN
FUEL AIR FLOW
FLOW LB/SEC
N2 LB/HR
-0.00 276.50 -0.00
-0.00 268.50 -0.00
-0.00 256.50 -0.00
-0.00 248.50 -0.00
-0.00 241.50 -0.00
-0.00 206
CD
.50 -0.00
THC NO
F/A COMPRESSOR COMPRESSOR
CALC INLET DISCHARGE
FROM TEMP PRESSURE
EMISSIONS DEGREES F PSIA
0.016500 100.00 52.50
0.016300 101.00 51.60
n. 016200 IOB.OO 49.90
0.016000 106.00 4R.90
0.016500 105.00 47.10
0.
012700 104.00 49
NO
2 IWETI IWFTI
(WET)
PERCENT V
1.35
3.10
3.27
3.21
3.15
PPMV PPMV
(W
2
ETI
PPMV
4.20 44.90
1.10 44.50
4.30 19.80
6.40 39.00
B. 10 38.90
2.56 25.80 24.20
EMI MASS EMI
402 CD2 NO
LB/IK LB/IK LB/IK
LB FUEL LB
-0.00 3030
-0.00 3030
-0.00 3030
-0.00 3030
-0.00 3020
-0.00 1030
CO
2
LB/IK HP-HR
33B9.917
3448.653
3647.128
3916.4B6
4152.762
4706.230
FUEL LB FUEL
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
THC
Lfl/lK HP-HR
0.151
0.126
0.196
0.281
0.182
1.724
MASS EMI MASS
NOX CO
10
9
12
1 1
11
14
FMI
.10
.70
.10
.80
.90
.00
NO
X
iwm
PPMV
55.00
54.20
51.90
50.90
50.80
38.20
MASS EMI MASS
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
.80
SMdKF
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
FMI MASS FMI 14SS
HC N02 C02
LR/IK LB/HR
Lfl FUEL
5.20 3.
5.19 1.
5.02 3.
4.98 3.
4.80 3.
4.73 4.
NU
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
19
36
74
84
69
6F
Nn
BLFED
FLOW
LB/MIN
64.40
B*. 16
100.06
115.64
132. 56
99. 71
PARI ICULSTFS
-0.00
-0.00
-n.oo
-0.00
-0.00
-0.00
FMI MASS FNI
NOX
LB/HR LB/HR LB/HR L5/HR Lfl/MR
0.04 -0
o.m -o
0.04 -0
0.05 -0
0.06 -0
0.21 -0
HO
^
L6/1K HP-HR
-0.000
-0.000
-0.000
-O.fOO
-n.ooo
-0.000
.00 817.
.00 813.
.00 777.
.00 752.
.00 729.
.00 625.
NO
X
79 -0.
55 -0.
19 -
-------
TEST ORGANIZATION! AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE DATA «««««««»«««»«
CAL ID NUMBER! 47 ENGINE TYPE AND MODEL! GTCP85-98CK
RATED SHAFT HORSEPOWER I 160.
ENGINE TOTAL TINE! 0. HRS
TINE SINCE HOT SECTION OVERHAULI 0. HRS
TINE SINCE!
Nl COMPRESSOR OVERHAUL! 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAULI 0. HRS
N2 TURBINE OVERHAULI 0. HRS
FUEL H/C RATIO! 1.926
SERIAL NUMBER!
FINISH
FINISH
96.00
26.65
FUEL! AV HERDS
OPERATIONAL DATA »»««»»
INLET AIR TEMPERATURE. DEGREES F: START 96.00
ATMOSPHERIC PRESSURE: START 26.65
INLFT AID HUMIDITY, LBS H20/LB AIR1 0.0019
RELATIVE HUMIDITY! 6.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES Ci -0.00, FLOW RATE. LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SECi -0.00
NUMBER OF TESTS: 5
COMMENTS:
SHP LOADING ONLY
resi
MODE
II 0
6/ 1
ll/ 6
16/11
20/16
POMER
SHAFT
HP
0.0
39.70
78.30
117.30
155.40
AIR
HP
0.0
0.0
0.0
0.0
0.0
ENGINE
SPEED
RPM
Nl
41500.00
41400.00
41300.00
41100.00
41000.00
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CORRECT El
FUEL
FLOW
LB/HR
122.00
141.60
161.60
164.00
214.00
GAS GEN
>IR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
F/A COMPRESSOR
CALC INLET
FROM TEMP
EMISSIONS DEGREES F
0.007200
0.008400
0.009600
0.010900
0.013100
90.00
93.00
95.00
98.00
104.00
COMPRESSOR BLEED
DISCHARGE FLOW
PRESSURE LR/HIN
PSIA
53.90
53.40
52.90
52.40
51.90
0.0
0.0
0.0
0.0
0.0
POMER EXHAUST
PERCENT GAS
DATED TEMP
SHP DEGREES F
0
24
48
73
97
560.00
630.00
700.00
905.00
930.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
CO
(MET)
PPMV
160.70
164.90
168.70
179.80
212.90
CO
2
IWETI
PERCENT
1.45
1.71
1.96
2.22
2.66
THC
IUET)
PPMV
61.10
41.50
29.20
22.00
19.60
NO
IUET)
PPMV
1.20
9.50
12.80
1 7.40
22.40
NO
2
IKETI
PPMV
6.50
7.70
7.80
8.00
a. 20
NO
X
I NET I
PPMV
7.70
17.20
20.60
25.40
30.60
-0.00
-0.00
-o.no
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
SHP
0
24
48
73
97
MASS EMI
CO
LB/1K
IB FUEL
21.55
18.83
16.81
15.79
15.53
MASS EMI
HC
LB/1K
LB FUEL
4.68
2.71
1.66
1.10
0.82
MASS EMI
NO 2
LB/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/U
LA FUEL
3060.00
3060.00
3060.00
3060.00
3040.00
MASS EMI
NO
LB/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
L6/1K
LB FUEL
1.69
3.22
3.36
3.66
3.67
MASS EMI
CO
LB/HR
2.63
2.67
2.72
2.90
3.32
MASS EMI
HC
LB/HR
0.57
0.38
0.27
0.20
0.17
MASS EMI
N02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CC12
LB/HR
373.32
433.30
495.11
563.04
650.56
MASS EMI
NO
LB/HR
-0.00
-n.oo
-0.00
-0.00
-0.00
MASS FM1
NOX
LB/HR
0.21
0.46
0.54
0.67
0.78
POWER
PERCENT
RATED
SHP
CO
LB/U HP-MR
LB/1K HP-MR
HORSFPOWER-HR BASIS NOT CALCULABLE"***
24 67.180 10914.246
46 34.728 6323.219
73 24.750 4799.996
97 21.392 4166.355
THC
LB/1K HP-HR
9.669
3.434
1.729
1.124
NO
LB/1K HP-HR
-0.000
-0.000
-0.000
-0.000
LB/1K HP-HR
-0.000
-0.000
-0.000
-0.000
NO
X
LB/1K HP-HR
11.479
6.951
5.738
5.050
111-28
-------
DATE! 6/ T/T1
TEST ORGANIIATIONI AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE OAtA
C»L 10 NUMBER! 66 ENGINE TYPE AND KDDEL1 GTCP8S-98CK
RATED SHAFT HORSEPOWER: 160.
ENGINE TOTAL TINE! 0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TINE SINCE!
NI COMPRESSOR OVERHAUL: o. MRS
N2 COMPRESSOR OVERHAUL: 0. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE N02ZLF GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.928
SERIAL NUMBER!
FINISH 123.00
FINISH 28.65
FUEL: AV HERDS
OPERATIONAL DATA »
INLET AIR TENPERATUREt DEGREES F: START 123.00
ATMOSPHERIC PRESSURE: START 28.65
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0019
RELATIVE HUMIDITY: 6.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOW RATE, LITERS/HIM:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
COMBINATION SHP/BLEEO LOADING
TEST
NODE
22/ 0
19/22
15/19
10/15
5/10
SHAFT
HP
154.30
116.50
77.30
39.10
0.0
AIR
HP
51.97
73.63
104.85
128.35
144.48
ENGINE
SPEED
RPH
NI
40700.00
40800.00
40800.00
40800.00
40800.00
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CORRECTED
FUEL
FLOW
LB/HR
258.00
244.00
244.00
242.00
234.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
F/» COMPRESSOR
CALC INLET
FROM TEMP
EMISSIONS DEGREES F
0.017800
0.017100
0.017300
0.017300
0.016800
130.30
125.00
126.00
120.00
114.00
COMPRESSOR BLEED
DISCHARGE FLOW
PRESSURE LB/MIN
PSU
48.20
47.70
46.50
46.00
45.On
38.46
55.56
81.04
101.34
117.92
POWER
PERCENT
RATED
SHP
96
72
4B
24
0
EXHAUST
GAS
TEMP
DEGREES F
1210.00
1150.00
1155.00
1160.00
1160.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
CO
(METI
PPMV
196.20
212.30
216.90
216.00
235.10
CO
2
(WET)
PERCENT
3.59
3.46
3.49
3.50
3.40
THC
IWETI
PPMV
15.70
26.30
24.20
24.20
25.60
NO
I HEM
PPMV
35.30
31.60
30.20
30.50
29.30
NO
2
I WE 11
PPMV
6.70
7.60
8.50
a. 10
9.00
ALDEHYDES SMOKE PARTICULARS
IKFU
PPMV
42.00
39.20
Jfl.80
38.60
38.30
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
SHP
96
72
48
24
MASS EMI
CO
LB/IK
LB FUEL
10.50
11.80
11.95
11.87
13.32
MASS EMI
HC
LB/IK
LB FUEL
0.48
0.84
0.76
0.76
0.83
MASS EMI
N02
LB/IK
L4 FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/IK
LB FUEL
3020.00
3020.00
3020.00
3020.00
3020.00
MASS EMI
NCI
LflMK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/IK
LR FUEL
3.69
3.58
3.51
3.49
3.57
MASS CM
CO
LB/HR
2.71
2. 88
2.92
2.87
3.12
MUSS FHI
HC
LB/HR
MASS EMI
NO 2
LB/HR
MASS EHI
C02
LD/HR
MASS EM
NO
LO/HP
0.12
0.70
0.19
0.18
0.19
-0.00
-0.00
-0.00
-0.00
-0.00
779.16
736.88
736.nn
730.84
706.61
-0.00
-0.00
-0.00
-C.OO
-0.00
HUSS EMI
NOX
Lfl/HR
0.95
0.87
0.86
0.84
0.81
POWER
PERCENT
RATED
SHP
96
12
48
24
0
CO
IB/IK HP-HR
II.136
15.147
16.006
17.155
21.572
LB/IK HP-HR
3777.388
3875.601
4045.375
4364.539
4891.250
THC
LB/IK HP-HR
0.599
1.073
1.022
I. 100
1.341
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
LB/IK HP-MR
-0.000
-0.000
-0.000
-0.000
-0.000
IB/IK HP-HR
4.617
4.592
4.700
5.019
5.777
111-29
-------
DATE I S/ 1/T1
TEST ORGANIZATION! AIAESEARCH
ENGINE SUPPLIER! A1RESEAACM
ENGINE OAT* «»«
CAL ID NUMBER!
4»
ENGINE TYPE »ND MODEL I GTCP85-9SD
RATED SHAFT HORSEPOMERI 160.
ENGINE TOTAL TIME)
TINE SINCE HOT SECTION OVERHAUL:
TINE SINCEi
SERIAL NUMBER I
P-2T692
0. MRS
0. MRS
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZILE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAULl 0. HRS
H2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.877
FINISH
FINISH
78.00
28.72
FUEL: JP-1
OPERATIONAL DATA «»»«
INLET AIR TEMPERATURE. DEGREES F: START 78.00
ATMOSPHERIC PRESSURE! START 28.72
INLET AIR HUMIDITY. IBS H20/L8 AIR: 0.0026
RELATIVE HUMIDITY: 10.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOU RATE, LITERS/NIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 3
COMMENTS:
SHP LOADING ONLY
TEST
MODE
I/ 0
6/ 1
ll/ 6
16/11
20/16
POWER
PERCENT
RArEO
SHP
0
25
50
75
88
POKER
PERCENT
HATED
SHP
0
25
50
75
88
POKE"
PERCENT
RATED
SHP
SHAFT
HP
0.0
40.40
80.60
120.90
141.70
EKHAUST
GAS
TEMP
DEGREES F
615.00
680.00
750.00
865.00
985.00
MASS EMI
CO
IB/IK
L8 FUEL
27.85
25.82
24.80
22.16
17.71
CO
LB/IK
HORSFPOUER-HR
25
50
75
88
97.
51.
16.
28.
POWER
AIR
HP
0.0
0.0
0.0
0.0
0.0
EXHAUST
GAS
PRESSUR
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
4.01
3.19
2.35
1.55
0.63
HP-HR
BASIS NOT
144
053
258
991
ENGINE
SPEED
RPM
Nl
41200.00
41100.00
41000.00
41000.00
40900.00
CO
IHETI
E PPMV
212.90
229.40
262.10
275.00
260.80
MASS EMI HASS
CORRECTED
FUEL
FLOU
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
IWET)
PERCENT V
1.49
1.71
2.06
2.4|
2.86
EMI HASS
LB/HR
125.50
152.00
172.40
197.80
212.00
THC
IHETI
PPMV
53.60
49.60
41.50
11.70
16.30
GAS GEN
AIR FLOU
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
NO
IUETI
PPMV
a. 10
10.10
14.40
21.90
32.40
EHI MASS EMI HASS
N02 C02 NO
Lfl/IK LB
L8 FUEL LB
-0.00 3070
-0.00 1060
-0.00 3060
-0.00 3050
-0.00 3050
CO
2
L8/1K HP-HR
CALCULABLE*****
11512.861
6545.207
4989.988
4991. 645
/IK IB/
IK L
FUEL LB FUEL LB
.00 -0.
.00 -0.
.00 -0.
.00 -0.
.00 -0.
THC
00
00
00
00
00
LB/IK HP-HR
11.998
5.033
2.542
1.013
NOX CO
B/1K LB/
FUEL
4.60 3.
4.42 1.
4.54 4.
4.76 4.
5.04 4.
NO
LB/1K HP-HR
-0.000
-0.000
-0.000
-0.000
F/A
CALC
FROM
EMISSIONS
0.007300
0.008500
0.010100
0.011900
0.014100
NO
?.
(WET)
PPMV
11.30
13.80
14.80
14.00
12.80
EMI HASS
HC
HR LB/
50 0.
92 0.
28 0.
38 0.
11 0.
LB/IK
-0
-0
-0
-0
COMPRESSOR
INLET
TEMP
DEGREES F
92.00
74.00
74.00
74.00
75.00
COMPRESSOR
DISCHARGE
PRESSURE
BLEED
FLOU
LB/MIN
PSIA
51
51
51
51
51
ND ALDFHYDES
X
IWET)
PPMV
21.40
23.90
29.20
35.90
45.20
FMI MASS EM
N02
HR LB/HR
50 -0.00
48 -0.00
41 -0.00
31 -0.00
15 -0.00
NO
2
HP-HR
.000
.000
.000
.000
-0.00
-0.00
-0.00
-0.00
-0.00
.90
.40
.70
.70
.60
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
1 MASS EMI MASS
C02
L8/H
385.
465.
527.
603.
707.
NO
X
NO
R LB/
28 -0.
12 -0.
54 -0.
29 -0.
60 -0.
0.0
0.0
0.0
0.0
0.0
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
FMI MASS EMI
NOX
HR LB/HR
00 0.5B
00 0.67
00 0.78
00 0.94
00 1.17
LB/IK HP-HR
16.626
9.709
7. 781
8.252
111-30
-------
OATEI s/ »m
TEST ORGANIIAMONI AIRESEARCM
ENGINE SUPPLIER: AIRESEARCH
ENGINE DAT* «»«*«*********
i
CAL ID NUNBERI »T ENGINE TYPE AND NODElI GTCP8S-9BO SERIAL NUKBERl P-27692
RATED SHAFT HORSEPOWER: 160.
0. MRS
0. MRS
ENGINE TOTAL TINEl
TIME SINCE HOT SECTION OVERHAUL 1
TINE SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 CONPRESSOR OVERHAUL: 0. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
NZ TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO: 1.877
FINISH
FINISH
48.00
28. 72
FUEL: JP-5
OPERATIONAL DATA »»»
INLET AIR TEMPERATURE. DEGREES f. START 98.00
ATMOSPHERIC PRESSURE: START 28.72
INLET AIR HUN I OUT, LBS H20/LB AIR: 0.0026
RELATIVE HUMIDIFY: 10.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: *
COMMENTS:
COMBINATION SHP/BLEED LOADING
TEST
NODE
22/ 0
19/22
15/19
10/15
5/10
POWER
PERCENT
RATED
SHP
50
37
25
25
0
POWER
PERCENT
RATED
SHP
50
17
25
25
0
POWER
PERCENT
HATED
SHP
50
37
75
SHAFT
HP
81.00
60.00
40.10
40.00
0.0
EXHAUST
GAS
TEMP
DEGREES F
1250.00
1250.00
1250.00
1235.00
1200.00
MASS EMI
CD
LB/IK
LB FUEL
6.6B
7.52
7.56
8.74
11.81
POWER
AIR
HP
49.01
73.55
98.04
-0.00
-0.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
0.04
0.06
0.05
0.01
0.15
CO
LB/IK
14.
14.
14.
Nl
40700
40700
40800
40700
40800
ENGINE
SPEED
RPM
.00
.00
.00
.00
.00
CO
(WET)
P
130
142
146
171
214
MASS EMI
N02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
PHV
.70
.50
.00
.40
.60
MASS
CORRECTED
FUEL
FLOW
N2 LB/HR
-0.00 277.50
-0.00 258.00
-0.00 267.00
-0.00 206.00
-0.00 201.00
CO THC
2 (WETI
IWETI PPMV
PERCENT V
3.78 1.30
3.67 2.10
3.74 1.70
3.79 0.30
3.51 4.70
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
NO
IWETI
PPMV
60.90
58.90
56.50
55.20
48.30
EMI MASS EMI MASS FMI MASS
C02 NO
LB
LB
3040
3040
3040
3030
3040
HP-MR LB/IK HP-MR
251
521
608
6489.590
5872.707
5875.594
/IK LB/IK
NOX CO
LB/IK LB/
F/A
CALC
FROM
EMISSIONS
0.018600
0.018000
0.018300
0.018600
0.017300
NO
2
IWETI
PPMV
8.60
9.00
9.70
9.10
11.50
EMI MASS
HC
HR Lfl/
COMPRESSOR
INLET
TEMP
DEGREES F
96.00
96.00
98.00
100.00
100.00
COMPRESSOR
DISCHARGE
PRESSURE
PSIA
52.10
50.70
49.10
45. 10
43.80
NO ALDEHYDES SMOKE
X
IWFT)
PPMV
69.50
67.90
66.20
64.30
59.80
CHI MASS EM
NO 2
H9 Ifl/HK
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
1 MASS EMI MASS
BLEED
FLOW
LB/MIN
35.72
55.01
75.37
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
f.fl MASS
EM
C32 Wl NOX
L8/HH in/
HP LB/
HR
FUEL LB FUEL LB FUEL
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
THC
LB/IK MP-HR
0.079
0.124
0.099
5.81 1.
5.88 1.
5.63 2.
5.39 1.
5.41 2.
NO
LB/IK HP-MR
-0.000
-0.000
-0.000
85 0.
94 0.
02 0.
80 0.
17 0.
Lfl/lK
-0
-0
-0
01 -0.00
02 -0.00
01 -0.00
CO -0.00
01 -0.00
NO
2
MP-HR
.000
.000
.000
843.60 -0.
784.32 -0.
811.68 -0.
624.13 -0.
611.04 -0.
NO
X
LB/IK HP-MR
12.448
11. 365
10.BK
00 1.
00 I.
00 1 .
00 1.
00 1.
62
52
50
11
09
HORSFPOWER-HR BASIS NOT CALCULABLE*****
****HORSFPOWER-HR BASIS NOT CALCULABLE"***
111-31
-------
DAT6I 5/ 6/71
TEST ORGANIZATION! AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE DATA *»**«*»»««»*»»«*«,»««**
C»L ID NUMBER: *9 ENGINE TYPE »ND MODEL I GTCP85-9BO SERIAL NUMBER 1 P-27857
RATED SHAFT HORSEPOUER: 160.
0. MRS
0. HRS
ENGINE TOTAL TINEt
TINE SINCE HOT SECTION OVERHAUL:
TINE SINCEl
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE KOIKE GUIDE VANE OVERHAUL: D. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.877
FINISH
FINISH
77.00
Z8.78
FUEL: JP-5
OPERATIONAL DATA «»««»»««
INLET AIR TEMPERATURE. DEGREES F: START 77.00
ATMOSPHERIC PRESSURE: START 2B.T8
INLET AIR HUMIDITY, LBS H2O/LB AIR: 0.0061
RELATIVE HUMIDITY: 40.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/KIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
SHP LOADING ONLY
TEST
NODE
I/ 0
6/ 1
ll/ 6
16/11
20/16
POWER
SHAFT
HP
0.0
39.30
77.90
116.70
155.80
AIR
HP
0.0
0.0
0.0
0.0
0.0
ENGINE
SPEED
RPM
Nl
41100.00
40950.00
40850.00
40700.00
40600.00
H2
-0.00
-0.00
-0.00
-0.00
-0.00
CORRECTED
FUEL
FLOM
LB/HR
112.50
137.00
159.50
184.50
211.00
GAS GEN
AIR FLOM
IB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
F/A
CALC
FROM
EMISSIONS
0.009600
0.007900
0.009400
0.010200
0.012700
COMPRESSOR
INLET
TEMP
DEGREES F
79.00
78.00
77.00
77.00
76.00
COMPRESSOR BLEED
DISCHARGE FLOW
PRESSURE LB/HIN
PSIA
57.90
56.60
56.90
56.50
56.40
0.0
0.0
0.0
0.0
0.0
POHfR
PERCENT
RATED
SHP
0
24
48
72
97
EXHAUST
GAS
TEMP
DEGREES F
540.00
605.00
670.00
7IS5.00
870.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
CO
IUET)
PPMV
182.20
246.90
289.70
355.20
334.30
CO
2
(MET)
PERCENT V
1.96
1.61
1.90
2.05
2.57
THC
IUET)
PPMV
63.60
84. BO
79.40
71.40
41.40
NO
(MET)
PPMV
1.60
7.00
10.10
13.30
20.90
NO
2
IHETI
PPMV
11.80
13.50
14.50
17.00
16.50
MO
X
I MET I
PPMV
15.50
20.50
24.60
30.30
37.40
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-o.oo
-o.oo
POMER
PERCENT
RATED
SHP
0
24
48
72
97
MASS ENI
CO
LB/IK
LB FUEL
18.19
29.86
29.66
33.48
25.14
MASS ENI
HC
LB/IK
La FUEL
3.63
5.86
4.63
3.84
1.76
MASS EMI
N02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-o.on
-0.00
MASS EMI
C02
LB/IK
LB FUEL
3070.00
3050.00
3050.00
3040.00
3040.00
MASS EMI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/IK
LB FUEL
2.53
4.07
4.12
4.69
4.62
MASS EM
CO
LB/HR
2.05
4.09
4.73
6. I*
5.30
MASS EMI
HC
LB/HR
MASS EMI
NO 2
LB/HR
MASS EMI
C02
LB/HR
MASS EMI
NO
LB/HR
MASS EMI
NOX
LB/HR
0.41
0.80
0.74
0.71
0.37
-0.00
-0.00
-0.00
-0.00
-0.00
345.37
417.85
486.47
560.S8
641.44
-0.00
-0.00
-0.00
-0.00
-0.00
0.29
0.56
0.66
0.81
0.97
POWER
PERCENT
RATED
SHP
LB/IK HP-HR
LB/IK HP-HR
HORSEPOHER-HR BASIS NOT CALCULABLE**"*
24 104.082 10632.309
48 60.723 6244.863
72 52.928 4806.168
97 J4.046 4117.070
THC
IB/IK HP-HR
20.445
9.484
6.077
2.390
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-MR
-0.000
-0.000
-0.000
-0.000
NO
X
Lfl/lK HP-HR
14.198
8.444
7.416
6.253
111-32
-------
DATE I 5/ 6/71
TEST ORGANIiATIONI AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE DATA ***
CAL ID NUNBERl
68 ENGINE TYPE AND HODEU GTCP85-98D
RATED SHAFT HORSEPOWERI 160.
ENGINE TOTAL TINEl 0. MRS
TINE SINCE HOT SECTION OVERHAUL: 0. MRS
TINE SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: l.BTT
SERIAL NUNBERl
P-Z7B57
FINISH
FINISH
76.00
28.78
FUEL: JP-S
OPERATIONAL DATA «««
INLET AIR TF.KPERATURE. DEGREES F: START 76.00
ATMOSPHERIC PRESSURE: START 28.78
INLET AIR HUMIDITT, IBS H20/LB AIR: 0.0061
RELATIVE HUMIDITY: 40.00 PERCENT
SAMPLE LINE: TEMPERATUREi DEGREES C: -0.00, FLOW RATEt LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
COMBINATION SHP/BLEED LOADING
TEST
MODE
22/ 0
19/22
15/19
10/15
5/10
POUER
SHAFT AIR
HP HP
153.90
US.50
76.90
38.80
0.0
96.03
106.58
125.06
139.40
150.48
ENGINE
SPEED
RPH
Nl N2
40100.00
40300.00
40300.00
40400.00
40500.00
-0.00
-0.00
-0.00
-o.on
-0.00
CORRECTED
FUEL
FLOW
LB/HR
284.50
273.00
264.00
255.00
234.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
F/» COMPRESSOB
CALC INLET
FROM TFMP
EMISSIONS DEGREES F
0.019700
0.018400
0.018100
0.017500
0.017700
78.00
75.00
74.00
73.00
SI.00
COMPRESSOR BLEED
DISCHARGE FLOW
PRESSURE LK/HIN
PSIA
51.40
52.70
51.70
50.50
49.00
64.79
79.06
95.59
109.17
119.55
POWER
PfRCFNT
RATED
SHP
96
72
48
24
0
EXHAUST
GAS
TEMP
DEGREES F
1230.00
1195.00
1185.00
1175.00
1170.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
CO
(UETI
PPMV
138.10
201.00
212.30
240.50
202.80
CO
2
IUETI
PERCENT
4.00
3.73
3.68
3.56
3.59
THC
IHETI
PPMV
41.40
40.60
73.30
76.20
13.80
NO
(WET)
PPNV
60.30
56.70
50.60
47.50
42.80
NO
2
IUETI
PPMV
9.00
9. 60
11.90
11.70
12.80
Nil
X
IHETI
PPMV
69.30
66.30
62.50
59.20
55.60
ALDEHYDES SMOKF PARTICULAUS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.oo
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
POKER
PERCENT
1ATED
SHP
96
72
48
24
0
MASS EMI
CO
LB/1K
IB FUEL
6.64
10.40
11.13
13.04
10.90
MASS EMI
HC
LB/1K
LB FUEL
1.14
1.20
2.20
2.36
0.42
MASS FMI
102
LB/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/1K
LB FUEL
3030.00
3030.00
3030.00
3030.00
3040.00
MASS FMI
NO
LB/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LR/1K
LB FUEL
5.41)
5.64
5.38
5.27
4.91
MASS FMI
CO
LB/HR
1.89
2.84
2.94
3.33
2.55
MASS EMI
HC
LB/HR
0.12
0.33
0.5H
0.60
0.10
MASS tMI
NO 2
LB/HP
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
862.03
827.19
799.92
772.65
711.36
MASS FM
NO
IB/ MO
-O.CO
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/HR
1.56
1.54
1.42
1.34
1.15
POWER
PERCENT
RATED
SHP
96
72
48
24
0
cn
LB/IK HP-HR
7.814
12.788
14.546
18.663
16.956
LB/IK HP-HR
3563.224
3724.758
3960.786
4315.809
4727.387
THC
LB/IK HP-HR
1.138
1.476
2.872
1.378
0.659
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
-0.000
-n.ooo
-0.000
-o.ono
-0.000
NO
X
LI/IK HP-HR
6.442
6.913
7.03B
7.538
7.611
111-33
-------
DATE: »/ 1/71
TEST ORGANIZATION! AIMSEARCH
ENGINE SUPPLIER! AIRESEARCH
ENCINE 0»T»
CAL 10 NUMBER! 50 ENGINE TYPE AND MODEL: GTCP85-98
RATED SHIFT HORSEPOWER! 160.
ENGINE TOTAL TIME! 0. MRS
TIKE SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE!
Nl COMPRESSOR OVERHAUL I 0. HRS
N2 COMPRESSOR OVERHAUL! 0. HRS
COXBUSTOR CAN REPLACEMENT 1 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL I 0. HRS
H2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: I.8TT
SERIAL NUMBER!
FINISH
FINISH
68.00
28.65
FUELS JP-5
OPERATIONAL OATA »
INLET AIR TEMPERATUREt DEGREES F: START 88.00
ATMOSPHERIC PRESSURE: START 28.6$
INLET AIR HUMIDITY, LBS M2D/LB AIR: 0.0019
RELATIVE HUMIDITY: is.oo PERCENT
SAMPLE LINE! TEMPERATURE. DEGREES C: -0.00. FLOW RATE. LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME. SECi -0.00
NUMBER OF TESTS! 5
COMMENTS:
SHP LOADING ONLY
TEST
MODE
I/ 0
6/ 1
ll/ 6
16/11
20/16
POWER
PERCENT
RATED
SHP
0
23
47
71
94
POWER
PERCENT
RATED
SHP
0
23
47
71
94
POWER
PERCENT
RATED
SHP
SHAFT
HP
0.0
38.30
76.40
114.30
151.60
EXHAUST
GAS
TEMP
DEGREES F
550.00
600.00
690.00
BOO. 00
950.00
MASS EMI
CO
LB/IK
LB FUEL
39.82
34.68
29.71
23.99
16.82
CO
LR/IK
HORSEPHWER-HR
23
47
71
94
119.
59.
37.
23.
POWER
AIR
HP
0.0
0.0
0.0
0.0
0.0
EXHAUST
GAS
PRESSUR
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
9.14
5.50
2.92
1.46
0.43
HP-HR
BASIS NOT
527
891
158
172
ENGINE
SPEED
RPM
Nl
41000.00
40900.00
40800.00
40700.00
40500.00
CO
IWET)
E PPHV
279.20
291.90
298.00
282.50
243.50
MASS EMI MASS
CORRECTED
FUEL
FLOW
N2 LB/HR
-0.00 113.00
-0.00 132.00
-0.00 154.00
-0.00 177.00
-0.00 208.80
CO THC
2 IWETI
IWETI PPMV
PERCENT V
1.36 112.10
1.63 81.00
1.95 51.20
2.29 30.10
2.81 10.80
GAS GEN F/A COMPRESSOR COMPRESSOR BLEED
AIR FLOW CALC INLET DISCHARGE FLOW
LB/SEC FROM TEMP PRESSURE Lfl/MIN
EMISSIONS DEGREES F PSIA
-0.00 0.006700 85.00 54.20 0.0
-0.00 0.008100 85.00 53.90 0.0
-0.00 0.009600 88.00 53.60 0.0
-0.00 0.011300 90.00 53.10 0.0
-0.00
NO
IWET)
PPMV
2.50
4.90
8.50
13.60
22.50
0.013800 94.00
NO NO
2 X
IWETI IWET)
PPMV PPMV
9.40 11.90
10.40 15.20
11.10 19.60
10.60 24.30
9.00 31.60
EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS
N02 C02 NO
NOX
LB/IK LB/IK LB/IK LB/IK
LB FUEL LB
-0.00 3040
-0.00 3050
-0.00 3050
-0.00 3050
-0.00 3050
CO
2
LB/IK HP-HR
CALCULABLE*****
10511.742
6147.902
4723.094
4200.789
FUEL LB FUEL LB
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -o.oo
THC
LB/IK HP-HR
18.949
5.878
2.262
0.589
FUEL
2.80
2.98
3.20
3.39
3.58
NO
LB/IK HP-
-0.000
-0.000
-0.000
-0.000
52.50
0.0
ALDEHYDES SMOKE PARTICULATES
-0.00 -0.
-0.00 -0.
-0.00 -0.
-o.no -o.
-0.00 -0.
EMI MASS EMI
CO HC N02 CCU
LB/HR LB/HR LB/HR LB/HH
4.50 1.03 -0.
4.58 0.73 -0.
4.58 0.45 -0.
4.25 0.26 -0.
3.51 0.09 -0.
NO
2
MR L8/1K HP-HR
-0.000
-0.000
-0.000
-0.000
00 343.52
00 402.60
00 469.70
00 539.85
00 636.84
NO
X
LB/IK MP-HR
10.257
6.458
5.245
4.932
00 -0.00
00 -0.00
00 -0.00
no -o.oo
00 -0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
-0.00 0.32
-0.00 0.39
-0.00 0.49
-0.00 0.60
-0.00 0.75
111-34
-------
DATE! V 1/Tl
TEST ORGANIZATION! AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE OAT*
CAL ID NUMBER: 69 ENGINE TYPE AND MODELi GTCPBS-^S
RATED SHAFT HORSEPOWERi 160.
ENGINE TOTAL TINEl 0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
HZ TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.877
SERIAL NUMBER!
P-1545*
FINISH
FINISH
59.00
28.65
FUEL: JP-S
OPERATIONAL DATA «««
INLET AIR TEMPERATURE. DEGREES F: START 95.00
ATMOSPHERIC PRESSURE: START 26.65
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0019
RELATIVE HUMIDITY: 18.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOH RATE, LITERS/HIM:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
COMBINATION SHP/BLEED LOADING
TEST
MODE
22/ 0
19/22
15/19
10/15
5/10
POWER
PFRCENT
RATED
SHP
94
70
47
23
0
POWER
PERCENT
RATED
SHP
94
70
47
23
0
POWER
PERCENT
RATED
SHP
94
70
47
23
0
SHAFT
HP
150.50
113.20
75.50
37.60
0.0
EXHAUST
GAS
TEMP
DFGREES f
1200.00
1200.00
1200.00
1200.00
1200.00
MASS EMI
CO
LB/IK
LB FUEL
6.94
7.53
9.04
10.20
11.59
CO
POWER ENGINE CORRECTED GAS GEN F/A COMPRESSOR COMPRESSOR BLfFO
AIR SPEED FUEL AIR FLOW CALC INLET DISCHARGE FLOW
HP RPH FLOW LB/SEC FROM TEMP PRESSURE LB/MIN
Nl N2 LB/HR EMISSIONS DEGREES F PSIA
67.56 40200.00 -0.00 261.50 -0.00 0.018300 96.00 51.60 49.69
95.10 40300.00 -0.00 251.50 -0.00 0.01B200 96.00 50.40 71.53
116.97 40300.00 -0.00 246.50 -0.00 0.017900 95.00 49.40 89.87
131.65 40400.00 -0.00 241.50 -0.00 0.017900 94.00 47.70 106.65
14B.43 40400.00 -0.00 231.70 -0.00 0.017600 92.00 46.40 122.05
EXHAUST CO CO THC NO NO NO ALOFHYDES SMOKF PARTICULARS
GAS (WET) 2 IWED IWETI 2 X
PRESSURE PPMV (WET) PPMV PPNV IWFTI (WETI
PSIA
-0
-0
-0
-0
-0
MASS
MC
.00
.00
.00
.00
.00
EMI
LB/IK
LB FUEL
0.
0.
0.
0.
0.
06
10
11
09
13
LB/IK HP-HR
6.
9.
11.
14.
18.
319
099
560
.355
099
134.
144.
170.
171.
214.
MASS EMI
NO 2
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
PERCENT V
00 3
40 3
00 3
80 3
10 3
MASS EMI
C02
LU/1K
LB FUEL
3040.00
3040.00
3040.00
3040.00
3040.00
.74 2
.71 3
.64 3
.63 3
.57 4
MASS EMI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
THC
LB/IK HP-HR LB/IK HP-HR
3645.544
3670.501
3893.331
4277.020
4745. 57B
0.078
0.117
0.141
0.127
0.209
.20 39
.30 39
.60 37
.00 36
.30 34
MASS EMI
NOX
LB/IK
LB FUEL
3.75
3.80
3.79
1.70
3.71
PPMV PPMV
.20 4.
.30 5.
.60 5.
.40 5.
.70 7.
MASS EMI
CO
LB/HR
l.BI
1.90
2.23
2.46
2.69
NO
LB/IK
-0.
-0.
-0.
-0.
-0.
HP-HR
000
000
000
000
000
90 4.
10 4.
90 3.
90 2.
10 1.
MASS FMI
HC
LB/HP
0.02
0.07
0.03
0.02
0.03
NO
2
10 -0.00 -0
40 -0.00 -0
50 -0.00 -0
30 -0.00 -0
70 -0.00 -0
MASS EMI MASS EMI
N02 C32
LB/HR LB/HR
-0.00 794.96
-0.00 764.56
-0.00 749.36
-0.00 734.16
-0.00 704.37
NO
X
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
-0.00 0.98
-0.00 0.96
-0.00 0.93
-n.on 0.89
-0.00 0.86
LB/IK HP-HR LB/IK HP-HR
-O.COO
-0.000
-0.000
-0.000
-O.POO
4.496
4.594
4.B56
5.204
5.79S
111-35
-------
omi S/H/TI
TEST ORGAN!IATIONI AIRJSEAACH
ENGINE SUPPLIER! AIRESEAACH
ENGINE DATA ««
C»L 10 NUMBER:
»l ENGINE TYPE AND MODEL I GTCP8S-98
RATED SHAFT HORSEPOWER: 160.
ENGINE TOTAL TIME I 0. HRS
TIME SINCE HOT SECTION OVERHAUL' 0. MRS
TINE SINCE:
Nl COMPRESSOR OVERHAUL) 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE N02ILE GUIDE VANE OVERHAUL! 0. HRS
Nl TURBINE OVERHAUL: o. HRS
NZ TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO: 1.928
SERIAL NUMBER:
P-1525T
FINISH
FINISH
86.00
28.8*
FUEL: AV HERDS
I1PERATIONAL DATA »»»»«»»«
INLET AIR TEMPERATUREt DEGREES F: START 86.00
ATMOSPHERIC PRESSURE: START 28.84
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0013
RELATIVE HUMIDITY: 8.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
SHf> LOADING ONLY
TEST
MODE
I/ 0
6/ I
ll/ 6
16/11
20/16
POWER
SHAFT AIR
HP HP
0.0
38.30
T6.40
114.30
152.00
0.0
0.0
0.0
0.0
0.0
ENGINE
SPEED
RPM
Nl
41000.00
40900.00
40800.00
40TOO.OO
40600.00
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CORRECTED
FUEL
FLOW
LB/HR
116.80
136.50
158.80
182.00
219.50
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
F/A
CALC
FROM
EMISSIONS
0.007300
0.008500
0.010000
0.011700
0.013700
COMPRESSOR
INLET
TEMP
DEGREES F
84.00
84.00
85.00
85.00
90.90
COMPRESSOR BLEED
DISCHARGE FLOW
PRESSURE LB/MIN
PSIA
54.90
55.20
54.90
54.60
54.00
0.0
0.0
0.0
0.0
0.0
POWER EXHAUST
PERCENT GAS
RATED TEMP
SHP DEGREES f
0
23
47
71
94
530.00
610.00
695.00
785.00
910.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
CO CO THC
IWETI 2 IWET)
PPMV (WET) PPMV
PERCENT V
288.60
269.10
263.50
253.80
219.10
1.47
1.71
2.02
2.37
2.78
158.90
89.30
37.30
16.80
3.30
NO
IWETI
PPMV
7.10
9.30
18.70
26.80
36.70
NO
2
IWETI
PPMV
12.80
17.00
14.10
13.50
12.20
ALDEHYDES SMOKE PARTICULATES
IWETI
PPMV
19.90
26.40
32.80
40.20
48.90
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
SHP
0
23
47
71
94
MASS EMI
CD
LB/IK
LB FUEL
37. T3
30.50
25.27
20.76
15.27
MASS EMI
KG
LB/IK
LB FUEL
11.88
5.79
2.04
0.79
0.13
MASS EMI
N02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/IK
LB FUEL
3020.00
3040.00
3050.00
3040.00
3040.00
MASS EMI
ND
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/IK
LB FUEL
4.27
4.91
5.16
5.40
5.60
MASS EMI
CO
LB/HR
4.41
4.16
4.01
3.70
3.35
MASS EMI
HC
LB/HR
1.39
0.79
0.32
0.14
0.03
MASS FMI
N02
LB/HR
-0.00
-o.no
-o.no
-o.no
-0.00
MASS EMI
CO 2
LB/HR
352.74
414.96
484.34
553.28
667.28
MASS EMI
NCI
LB/HR
-0.00
-o.on
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/HR
0.50
0.67
0.82
0.98
1.23
POWER
PERCENT
RATED
SHP
LB/IK HP-HR
LB/IK HP-HR
HORSEPOWER-HR BASIS NOT CALCULABLE*****
23 108.708 10834.461
47 52.525 6339.523
71 33.050 4840.594
94 22.057 4389.996
THC
LB/IK HP-HH
20.621
4.249
1.253
0.189
NO
Lfl/lK HP-HR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
17.492
10.731
8.606
8.088
111-36
-------
om< 5/18/7i
TCST ORGANIZATION! AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE D»T»
C»L 10 NUMBER: TO ENGINE TYPE *HD MODEL: GTCPas-98
RATED SHAFT HORSEPOWER! 160.
ENGINE TOTAL TINE: 0. MRS
TIKE SINCE HOT SECTION OVERHAUL: 0. HRS
TINE SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO: 1.928
SERIAL NUMBER:
P-15257
FINISH
FINISH
87.00
26.84
FUEL: AV KEROS
OPERATIONAL DATA ««»»»«»»*«««»
INLET AIR TEMPERATUREi DEGREES F: START 87.00
ATMOSPHERIC PRESSURE: START 28.64
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0013
RELATIVE HUMIDITY: B.OO PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00. FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER Of TESTS: 5
COMMENTS:
COMBINATION SHP/BLEEO LOADING
TEST
MODE
22/ 0
19/22
15/19
10/15
5/10
POWER
PERCENT
RATED
SHP
94
70
4 7
23
0
POWER
PERCENT
RATED
SHP
94
70
47
23
0
POWER
PERCENT
RATED
SHP
94
70
47
23
0
SHAFT
HP
151.30
113.50
75.60
37.90
0.0
EXHAUST
GAS
TEMP
DEGREES F
1200.00
1200.00
1200.00
1200.00
1200.00
MASS EMI
CO
LB/1K
LB FUEL
6.22
6.13
5.88
5.82
6.92
CO
LB/IK
7.
7.
11.
10.
11.
POWER
AIR
HP
62.92
95.29
63.42
109.73
146.13
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
Lfl/lK
LB FUEL
0.08
0.02
0.03
0.02
0.02
ENGINE
SPEED
RPM
Nl
40400.00
40400.00
40400.00
40500.00
40560.00
CO
(WET)
PPMV
120.60
122.70
125.50
117.00
137.70
MASS FMI MASS
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
(WET)
PERCENT
3.74
3.85
3.78
3.87
3.63
CORRECTED
FUEL
FLOW
LB/HR
270.00
270.00
274.00
262.00
242.no
THC
(WET)
PPMV
V
2.70
0.70
1.10
0.60
0.80
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
NO
(WET)
PPHV
59.90
58.00
60.10
59.30
54.20
EMI MASS EMI MASS FMI MASS
N02 C02
LB/IK LR/IK
NO
LR/IK
NOX CO
F/A
CALC
FROM
EMISSIONS
0.016400
0.019000
0.018600
0.019100
0.018900
NO
2
IWET)
PPMV
5.40
5.40
6.30
5.40
5.00
EMI MASS
HC
COMPRESSOR
INLET
TEMP
DEGREES F
85.00
86.00
88.00
SB. 00
88.00
COMPRESSOR
DISCHARGE
PRESSURE
PSIA
51.50
52.00
53.20
50.60
48.20
NO ALDEHYDES SMOKF
X
IWETI
PPMV
65.30 -0
63.40 -0
66.40 -0
64.60 -0
59.30 -0
FMI MASS EMI
ND2
LB/IK Lfl/HR LB/HR LB/HR
.00 -n.oo
.00 -0.00
.00 -0.00
.00 -o.oo
.no -o.oo
MASS EMI MASS
C02 NO
BLEED
FLOW
LB/HN
45.64
70.85
45.99
83.42
116.49
PARTICUIATES
-0.00
-0.00
-0.00
-0.00
-0.00
FMI MASS
EMI
NOX
LB/HR LB/HR LR/HR
Lfl FUEL LB FUEL LB FUEL LB FUEL
-0.00 3030.
00
-0.00 3020.00
-0.00 3020.
-0.00 3020.
-0.00 3020.
CO
2
HP-HR LR/IK HP-HR
636
927
585
331
457
3818.908
3905.266
5952. OB2
5359.71 I
5001.332
00
00
00
-0.00
-0.00
-0.00
-0.00
-o.on
THC
LB/IK
0.
0.
0.
0.
0.
HP-HR
098
027
061
032
051
5.52 1.
5.20 1.
5.55 I.
5.28 1.
4.69 1.
NO
LB/IK HP-HR
-0.000
-o.noo
-o.oon
-0.000
-0.000
68 0.
66 0.
61 0.
53 0.
67 0.
02 -0.00
01 -0.00
01 -0.00
00 -0.00
01 -0.00
Nl)
2
8IB.10 -0.
BIS. 40 -0.
82 7.49 -0.
791.24 -0.
730. fl4 -0.
NO
X
no i
00 1
00 1
00 1
00 1
.49
.41
.52
.38
.18
LB/IK HP-HR LR/IK HP-HR
-0
-n
-0
-0
.000
.000
.000
.000
-o.noo
6.951
6.729
10.942
1. )78
8.09B
111-37
-------
DATE! 5/21/71
TEST ORGANIZATION! AIIESEAItCH
ENGINE SUPPllEm »IR6SE»RCM
ENGINE DATA «*»««**«**««*»««».»«.
CAL 10 NUMBERl 52 ENGINE TYPE AND MODEL! GTCPS5-98
RATED SHAFT HOISEPOMERl 160.
ENGINE TOTAL TINE! 0. HRS
TINE SINCE HOT SECTION OVERHAUL! 0. HRS
TINE SINCE!
Nl COMPRESSOR OVERHAUL! 0. HRS
N2 COMPRESSOR OVERHAUL! 0. HRS
COMBUSTOR CAN REPLACEMENT! 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nt TURBINE OVERHAUL! 0. HRS
N2 TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO! 1.428
SERIAL NUMBER!
P-I5S41
FINISH
FINISH
91.00
2B.SS
FUEL! AV HERDS
OPERATIONAL DATA «««««««
INLET AIR TEMPERATURE, DEGREES Fl START 93.00
ATMOSPHERIC PRESSURE! START 28.58
INLET AIR HUH 101TT, LBS H20/LB AIR: 0.0013
RELATIVE HUMIOim 13.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES C: -0.00, FLO* RATE, LITERS/KIN:
SAMPLE LINE TRANSPORT TIME. SEC! -0.00
NUMBER OF TESTS: 5
COMMENTSl
SHP LOADING ONLY
TEST
MODE
I/ 0
6/ I
ll/ 6
16/11
20/16
POKER
SHAFT
HP
0.0
30.10
76.00
111.50
150.90
AIR
HP
0.0
0.0
0.0
0.0
0.0
ENGINE
SPEED
RPH
Nl
41000.00
40700.00
40600.00
40400.00
40100.00
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CORRECTED
FUEL
FLOK
LB/HR
117.00
125.00
158.00
182.00
213.40
GAS GEN
AIR FLOM
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
F/A
CALC
FROM
FMISSIONS
0.007000
0.008400
0.009900
0.012000
0.014500
COMPRESSOR
INLET
TEMP
DEGREES f
88.00
92.00
95.00
96.00
95.00
COMPRESSOR
DISCHARGE
PRESSURE
PSIA
51.90
51.40
51.30
51.20
51.00
BLEED
FLOU
LB/HIN
0.0
0.0
0.0
0.0
0.0
POKER
PERCENT
RATED
SHP
0
23
47
70
94
F.XHAUST
GAS
TEMP
OFGREES F
550.00
615.00
740.00
865.00
995.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
CO CO
I MET I 2
PPMV (METI
PERCENT V
282.10
119.90
128.00
296.40
196.10
1.18
1.68
1.49
2.42
2.91
THC
IUETI
PPMV
222.10
169.80
121.90
71.60
54.10
NO NO
I MET I 2
PPMV (METI
PPMV
ALDEHYDES SMOKE PARTICIPATES
8.20
9.20
14.70
23.40
40.40
11.10
15.00
15.10
11.80
7.70
IUFTI
PPMV
18.30
24.20
10.00
17.70
48.10
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POKER
PERCENT
RAfEO
SHP
0
21
47
70
94
MASS EMI
CO
IB/IK
LB FUEL
39.00
36.52
31.77
23.60
12.91
MASS EMI
HC
LB/1K
LB FUEL
17.55
11.08
6.75
1.35
2.04
MASS EMI
NO 2
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
IB/IK
LB FUEL
3000.00
3010.00
3020.00
1010.00
3040.00
MASS EMI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/IK
LB FUEL
4.15
4.54
4.78
4.91
5.20
MASS EMI
CO
LB/HR
4.56
4.56
5.02
4.30
2.76
MASS EMI
HC
LB/HR
2.05
1.38
1.07
0.61
0.43
MASS FMI
N02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO 2
LB/HR
151.00
176.25
477.16
551.46
648.74
MASS EMI
NO
IB/KB
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/HR
0.49
0.57
0.75
0.90
1.11
POWER
PERCENT
RATED
SHP
LB/IK HP-HR
CO
2
LB/IK HP-HR
HORSFPOKER-HR BASIS NOT CALCULABLE"***
21 119.801 9875.116
47 66.056 6278.418
70 17.848 4858.676
94 18.264 4299.109
TMC
LB/IK HP-HR
36.148
14.027
5.172
2.882
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
LB/IK HP-HR
14.905
4.429
7.907
7.354
111-38
-------
5/ZI/71
TEST ORGANIIATIONI AIRESEARCH
ENGINE SUPPIIERI AIRESEARCH
ENGINE DATA «*»***
C»L ID NUN8ERI 71 ENGINE TYPE AND HOOELl GTCP8f-48 SERIAL NUMBER: P-H541
RATED SHAFT HORSEPOWER I 160.
ENGINE TOTAL TINE: 0. HRS
TINE SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
HZ COMPRESSOR OVERHAUL: 0. HRS
COKBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZILE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
HZ TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.928
FINISH
FINISH
97.00
ze.se
FUEL: AV KEROS
OPERATIONAL DATA «»««»»««»«*
IMLFT AIR TEMPERATURE. DEGREES F: START 97.00
ATMOSPHERIC PRESSURE: START 28.58
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0033
RELATIVE HUMIDITY: 13.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
COMBINATION SHP/BLEED LOADING
TEST
MODE
22/ 0
19/22
15/14
10/15
5/10
POWER
PERCENT
RATED
SHP
93
70
46
23
0
POWER
PERCENT
RATED
SHP
93
70
46
23
0
POWER
PERCF.NT
RATED
SHP
93
70
46
23
0
SHAFT
HP
149.80
112.10
74.70
37.40
0.0
EXHAUST
GAS
TEMP
DEGREES F
1250.00
1250.00
1250.00
1250.00
1250.00
MASS EMI
CO
LB/IK
LB FUEL
4.37
4.90
5.32
5.65
6.35
CO
LB/IK
5.
6.
7.
8.
11.
POWER
AIR
HP
52.05
83.87
104.11
122.03
1)4.53
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
HC
LB/IK
LB FUEL
1.25
1.90
1.60
2.26
1.61
Nl
40000
39900
39900
40000
40000
ENGINE
SPFED
RPM
.00
.00
.00
.00
.00
CO
IWETI
P
90
100
109
114
127
MASS EMI
N02
Lfl/lK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
HP-HR LB/IK MP-
593
333
385
619
022
3864.502
3905.093
4195.363
4610.492
5239.453
PMV
.10
.90
.20
.50
.60
MASS
CORRECTED
FUEL
FLOW
N2 LB/HR
-0.00 258.30
-0.00 253.40
-0.00 248.40
-0.00 243.40
'0.00 233.40
CO THC
2 IWETI
(WET) PPMV
PERCENT V
3.96 45.20
3.95 68.30
3.94 57.60
3.89 80. 10
3.86 56.60
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
NO
IWETI
PPMV
61.10
61.30
59.80
59.60
56.30
EMI MASS EMI MASS EMI MASS
C02 NO
LB/IK Lfl/IK
LB
3020
3020
3020
3020
3020
HR
NOX CO
F/A
CALC
FROM
EMISSIONS
0.019500
0.019500
0.019500
0.019200
0.019100
NO
2
IWETI
PPMV
4.90
5.10
4.60
4.10
4.60
FHI MASS
HC
COMPRESSOR COMPRESSOR
INLET DISCHARGE
TEMP PRESSURE
DEGREFS
NO
IWE
96.00
98.00
98.00
97.00
96.00
X
Tl
F PSIA
49. 00
48.00
46.90
45.70
44.00
ALDEHYDES SMOKE
BLEED
FLOW
LB/MIN
40.24
65. V3
83.77
101.01
116.07
^ARTICULATES
PPMV
66.
66.
64.
63.
60.
EMI
00
40
40
70
90
MASS
-o.oo -o.on
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
FH1 MASS F«l MASS
N02 CO? NO
LB/IK L8/HR LS/HR
-0.00
-0.00
-0.00
-0.00
-0.00
FMI MASS EMI
NOX
LB/HR L8/MR LB/hR LO/HR
FUEL LB FUEL LB FUEL
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
THC
LB/IK HP-HR
1.606
2.453
2.228
3.446
2.791
5.26 1.
5.30 I.
5.15 1.
5.16 1.
4.99 1.
NO
LB/IK HP-MR
-0.000
-0.000
-0.000
-0.000
-0.000
13 0.
74 0.
32 0.
37 0.
48 0.
LB/IK
-0
-0
-0
-n
32
48
40
55
38
NO
2
-0.
-0.
-0.
-0.
-0.
HP-HR
.000
.000
.000
.000
-o.noo
00 780.06 -0.
00 765.27 -0.
00 750.17 -0.
no 735.07 -0.
00 704.17 -0.
NO
X
Lfl/IK HP-HR
6.71?
6.851
7.156
7.876
1. 652
00 1.36
00 1.34
no 1.28
00 1.26
00 1.16
111-39
-------
OATEI 5/11/71
TEST ORGANIZATION! AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE DAT* »******»*»**««»*»»*»*»**«**»»««*»«»*
C»L ID NUMBER! 53 ENGINE TYPE AND MODEL! GTCP85-U5 SERIAL NUMBER! P-18T25
SATED SHAFT HORSEPOWER! 160.
0. MRS
0. MRS
ENGINE TOTAL TINE!
TINE SINCE HOT SECTION OVERHAUL:
TINE SINCE!
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL! 0. HRS
NI TURBINE OVERHAUL: a. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.877
FINISH
FINISH
42.00
26.7B
FUEL: jp-5
OPERATIONAL DATA «««»»««
INLET AIR TEMPERATURE, DEGREES F: START 92.00
ATMOSPHERIC PRESSURE: START 20.TB
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.0059
RELATIVE HUMIDITY: 25.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00. FLOW RATE. LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
SHP LOADING ONLY
TEST
MODE
I/ 0
6/ 1
ll/ 6
16/11
20/16
SHAFT
HP
0.0
38.20
76.00
111.70
151.30
AIR
HP
0.0
0.0
0.0
0.0
0.0
ENGINE
SPEED
RPM
Nl N2
41100.00
40800.00
40600.00
40500.00
40400.00
-0.00
-0.00
-0.00
-0.00
-0.00
CORRECTED
FUEL
FLOW
LB/HR
110.60
121.70
155.90
185.30
215.80
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
F/A COMPRESSOR
CALC INLET
FROM TEMP
EMISSIONS DEGREES F
0.006400
0.007700
0.009700
0.012400
0.014000
82.00
85.00
93.00
105.00
96.00
COMPRESSOR BLEED
DISCHARGE FLOW
PRESSURE LB/MIN
PSIA
64.10
62.90
61.00
58.10
61.90
0.0
0.0
0.0
0.0
0.0
POWER
PERCENT
RATED
SHP
0
23
47
71
94
EXHAUST
GAS
TEMP
DEGREES f
520.00
615.00
740.00
900.00
1010.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-o.oo
-o.oo
-o.oo
-o.oo
CO
IWET)
PPMV
196.10
215.90
211.40
221.10
217.20
CO
2
-------
omi 5/um
TEST ORGANIZATION! AIRESEARCH
ENGINE SUPPLIER I AIRESEARCH
ENGINE 0»T» «««»«»»«»««
CM. 10 NUMBER) T2 ENGINE TYPE AND MODEL! GTCP85-115
RATED SHAFT HORSEPOWER: 160.
ENGINE TOTAL TINEl
TIME SINCE HOT SECTION OVERHAUL!
TINE SINCEl
SERIAL NUMBER I
P-1872S
0. HRS
0. HRS
Nl COMPRESSOR OVERHAUL! 0. HRS
N2 COMPRESSOR OVERHAUL! 0. HRS
CONBUSTOR CAN REPLACEMENT! 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: o. HRS
FUEL H/C RATIO: 1.677
FINISH 107.00
FINISH 28.78
FUEL: JP-S
OPERATIONAL DATA »«
INLF.T AIR TEMPERATURE* DEGREES F: START 107.00
ATMOSPHERIC PRESSURE: START 26.78
INLET AIR HUMIDITY, L8S H20/LB AIR: 0.0059
RELATIVE HUMIDITY: 25.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOM RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
COMBINATION SHP/BLEED LOADING
fEST
MODE
22/ 0
11/22
15/19
10/15
5/10
POWER
PERCENT
BATED
SHP
94
70
47
23
0
POWER
PERCENT
RATED
SHP
94
70
47
23
0
POWER
PERCENT
RATED
SHP
94
70
47
23
SHAFT
HP
150.90
113.20
75.60
57.80
0.0
EXHAUST
GAS
TEMP
DEGREES F
1200.00
1200.00
1195.00
1200.00
0.0
MASS EMI
CO
LB/1K
LB FUEL
8.74
10.95
12. BO
13.26
14.65
CO
LB/1K
11.
14.
17.
20.
POWER
AIR
HP
49.73
Tl.74
93.73
116.13
0.0
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
0.09
0.10
0.14
0.16
0.25
ENGINE
SPEED
RPM
Nl
40300.00
40300.00
40400.00
40400.00
0.0
CO
1 WETI
PPMV
161.80
200.40
226.70
243.10
264.30
MASS EMI MASS
NZ
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
(WETI
PERCENT
3.58
3.54
3.43
3.54
3.48
CORRECTED GAS GEN
FUEL AIR FLOW
FLOW LB/SEC
LB/HR
254.50 -0.00
246.40 -0.00
234.20 -0.00
233.20 -0.00
-0
.00 -0.00
THC NO
IWETI IWETI
V
EMI MASS FMI
N02 C02
L3/1K LB/1K
LB FUEL IB
-0.00 3040
-0.00 3040
-0.00 3040
-0.00 3030
-0.00 3030
CO
2
HP-HR LB/IK HP-HR
085
594
700
084
3856.163
4050.261
4204.504
4590.340
NO
LB/IK
FUEL LB FUEL
.00
.00
.00
.00
.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
LB/IK
0.
0.
0.
0.
HP-HR
119
139
198
236
PPMV PPMV
3.00 48.50
3.30 49.90
4.40 46.60
5.00 48.40
8.00 45.10
MASS FMI MASS
NO* CO
F/A COMPRESSOR COMPRFSSOP
CALC INLET DISCHARGE
FROM IEMP PRESSURE
EMISSIONS DEGREES F PSIA
0.017600 102.00 56.90
0.017400 102.00 54.20
0.016900 114.00 52.60
0.017400 109.00 50.60
0.017200 -0.00 -0
NO
2
IWET)
PPMV
5.70
5.60
5.80
6.70
7.50
NO
X
IWFTI
PPMV
54.10
55.50
52.40
55.10
52.60
EMI MASS EMI MASS
ALOEHVOES
-0.00
-0.00
-0.00
-0.00
-0.00
.00
SMOKF
-0.00
-0.00
-0.00
-0.00
-0.00
EMI MASS EMI MASS
HC Nfl2 C02
LB/1K Lfl/HR
LB FUEL
4.80 2.
4.98 2.
4.86 3.
4.93 3.
4.79 -0.
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
22
70
00
09
00
NO
PLEED
FLOW
LB/MIN
3.1.08
49.86
65.58
85.03
1.0
PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
EMI MASS FMI
Ndx
LB/HP Lfl/HR Lfl/HR LB/HR LR/HR
0.02 -0
0.03 -0
0.03 -0
0.0* -0
-0.00 -0
NO
2
LB/IK HP-Ha
-0.000
-o.oon
-0.000
-0.000
.00 771.
.00 749.
.00 711.
.00 706.
.00 -0.
NO
X
68 -0.
06 -0.
97 -0.
60 -0.
00 -0.
00 1.22
00 1.23
00 1.14
00 1.15
00 -0.00
LB/IK HP-HR
6.092
6.618
6.772
7.47S
*HnRSEPQWEft-HR BASIS NOT CALCULABLE*****
111-41
-------
DATE! 6/ 8/71
TEST ORGANIZATION! AIRESEARCH
ENGINE SUPPLIER) AIRESEARCH
ENGINE DAT*
CAL 10 NUMBER! S» ENGINE TYPE AND MODEL: GTCP85-115
RATED SHAFT HORSEPONERl 160.
ENGINE TOTAL TINEl 0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCEl
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL! 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAULl 0. HRS
HZ TURBINE OVERHAULl 0. HRS
FUEL H/C RATIO: 1.926
SERIAL NUMBER:
P-I8T81
FINISH
FINISH
93.00
26.72
FUEL: AV KEROS
OPERATIONAL DATA «»»«*«»»*»«
INLET AIR TEMPERATURE. DEGREES F: START 93.00
ATMOSPHERIC PRESSURE: START 26.72
INLET MR HUMIDITY, LBS H20/LB AIR: 0.0046
RELATIVE HUMIDITY: 15.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER (IF TESTS: 5
COMMENTS:
SHP LOADING ONLY
TEST
MODE
I/ 0
6/ 1
ii/ e
16/11
20/16
POKER
PFRCENT
RATED
SHP
0
24
48
71
95
POWER
PERCENT
RATED
SHP
0
24
48
71
95
POWER
PERCENT
RATED
SHP
SHAFT
HP
0.0
38.60
77.10
115.10
153.10
EXHAUST
GAS
TEMP
DEGREES f
545.00
620.00
710.00
820.00
960.00
MASS EMI
CO
LB/IK
LB FUEL
28.33
25.51
24.30
22.38
18.15
CO
Lfl/lK
HHRSFPOWER-HR
24
48
71
95
91.
50.
36.
25.
POWER ENGINE CORRECTED GAS GEN F/A
AIR SPEED FUEL AIR FLOW CALC
HP RPM FLOW LB/SEC FROM
Nl N2 LB/HR EMISSIONS
0.0 41200.00 -0.00 121.60 -0.00 0.006600
0.0 41200.00 -0.00 139.00 -0.00 0.008300
0.0 41200.00 -0.00 161.00 -0.00 0.010000
0.0 41000.00 -0.00 186.20 -0.00 0.011800
0.0 40900.00 -0.00 216.50 -0.00 0.013600
EXHAUST CO CO THC NO NO
GAS IWET) 2 IWET) (MET) 2
PRESSURE PPMV (WET) PPMV PPMV (WET)
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
5.16
4.25
2.93
1.79
0.91
HP-HR
BASIS NOT
870
735
213
662
PFRCENT V
194.
221.
254.
275.
259.
MASS EMI
N02
LB/IK
L8 FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
cn
2
60 I
20 1
70 2
20 2
50 2
MASS EMI
C02
LB/IK
LB FUEL
3050.00
3050.00
3040.00
3040.00
3040.00
.33 62
.68 6
.03 53
.38 38
.76 22
MASS EMI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
THC
LB/IK HP-HR LB/IK HP-HR
.00 3
.45 5
.80 10
.50 14
.70 22
MASS EMI
NOX
LB/IK
LB FUEL
2.66
2.79
3.44
3.40
3.71
PPMV
.70 7.
.80 8.
.60 11.
.70 10.
.80 9.
MASS EMI
CO
LB/HR
3.44
3.55
3.91
4.17
3.93
50
90
40
80
50
MASS
HC
COMPRESSOR COMPRESSOR BLEED
INLET DISCHARGE FLOW
TEMP PRESSURE LB/MIN
DEGREES F PSIA
92.00 53.50 0.0
91.00 54.40 0.0
91.00 54.40 0.0
94.00 54.10 0.0
96.00 53.90 0.0
NO ALDEHYDES SMOKE PARTICULATES
X
IWET I
PPMV
11.10
14.70
22.00
25.40
32.30
EMI MASS EM
N02
LB/HR LB/HR
0.
0.
0.
0.
0.
NO
LB/IK
HP-HR
LB/IK
63 -0.00
59 -0.00
47 -0.00
33 -0.00
20 -0.00
NO
2
HP-HR
-0.00 -0
-0.00 -0
-0.00 -0
-0.00 -0
-o.oo -o
I "ASS EMI
C02
LB/HR
370. aa
423.95
489.44
566.05
658.16
NO
X
LB/IK HP-HR
.00 -0.00
.00 -0.00
.00 -o.oo
.00 -o.oo
.00 -o.oo
MASS EMI MASS EMI
NO NQX
LB/HR LB/HR
-0.00 0.32
-0.00 0.39
-0.00 0.55
-0.00 0.63
-0.00 0.80
CALCULABLE*****
10983.148
6349.113
4917.875
4298.887
15.319
6. 127
2.899
1.281
-0.
-0.
-0.
-0.
000
000
000
000
-0
-0
-0
-0
.000
.000
.000
.000
10.036
7.188
5.500
5.246
111-42
-------
omt 6/ a/Ti
TEST ORGANIIITKMI AIRESEARCH
ENGINE SUPPLIER: AIRESEARCH
ENGINE DATA **«*
CM. ID NUMBER:
73 ENGINE TYPE AND MODEL: GTCPB3-I1S
RATED SHAFT HORSEPONERl 160.
ENGINE TOTAL TINE: 0. MRS
TIKE SINCE HOT SECTION OVERHAUL: 0. HRS
TINE SINCE:
NI COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: o. HRS
FUEL H/C RATIO: 1.928
SERIAL NUMBER:
P-18781
FINISH 107.00
FINISH 28.72
FUEL: AV KEROS
OPERATIONAL DATA »«»«»««»*»««
INLET AIR TEMPERATURE, DEGREES F: START 107.00
ATMOSPHERIC PRESSURE: START 28.72
INLET AIR HUMIDITY. LBS H20/L8 AIR: 0.0046
RELATIVE HUMIDITY: 15.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
COMBINATION SHP/BLEEO LOADING
TEST
MODE
22/ 0
19/22
15/19
10/15
5/10
POWER
PFRCFNT
RATED
SHP
95
71
47
23
0
POWER
PERCENT
BATED
SHP
95
71
»7
23
0
POWER
PERCENT
RATED
SHP
95
71
47
23
0
SHAFT
HP
152.40
114.30
76.20
38.20
0.0
EXHAUST
GAS
TEMP
DEGREES F
1250.00
1250.00
1250.00
1250.00
1250.00
MASS EMI
CO
LB/1K
LB FUEL
7.49
8.69
9.61
11.38
13.99
CO
LB/1K
9.
II.
13.
17.
24.
POWER
AIR
HP
61.69
80.08
104.53
121.75
136.45
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
Lfl FUEL
0.16
0.39
0.43
0.58
0.71
ENGINE
SPEED
RPM
NI
40700.00
40700.00
40700.00
40800.00
40800.00
CO
(WET)
PPMV
144.80
164.60
181.50
213.70
261.00
MASS EMI MASS
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
(WET)
PERCENT
3.72
3.65
3.63
3.61
3.58
CORRECTED
FUEL
FLOW
LB/HR
2B1.50
266.50
256.50
251.50
241.50
THC
(NET)
PPMV
V
5.30
12.80
14.30
19.00
23.20
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
NO
(WETI
PPMV
37.50
37.00
35.30
34.90
32.00
EMI MASS EMI MASS FMI MASS
N02 C02
LB/IK LB
LB FUEL La
-0.00 3020
-0.00 3020
-0.00 3020
-0.00 3020
/IK
NO
LB/IK
NOX CO
LB/IK LB/
F/A
CALC
FROM
MISSIONS
0.018300
0.018000
0.017900
0.017800
0.017700
NO
2
(WETI
PPMV
4.90
5.20
6.70
6.70
a. 10
FMI M^SS
HC
HR LB/
COMPRESSOR
INLET
TFMP
DEGREES F
100.00
110.00
108.00
108.00
108.00
COMPRESSOR
DISCHARGE
PRFSSURE
PSIA
51.90
50.20
48.70
47.00
4-i. 30
NO ALDEHYDES SMOKE
X
(WET)
PPMV
42.40 -0
42.30 -0
41.90 -0
41.60 -0
40.10 -0
EMI MASS EMI
NO 2
HR LB/HR
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
MASS FMI MASS
cnz NO
LH/HR Lfl/
RLEEO
FLOW
LB/MIN
44.80
58.98
79.58
96.03
1 11.77
PaOIICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
FMI MASS
EMI
NOX
HR LH
/HR
FUFL LB FUEL LB FUEL
.00
.00
.00
.00
-0.00 3020.00
CO
2
HP-HR LB/IK HP-HR
850
910
644
892
753
3970.900
4140.488
4286.059
4749.660
5144.934
-0.00
-0.00
-0.00
-0.00
-0.00
THC
LB/IK
0.
0.
0.
0.
1.
HP-HR
205
531
613
907
260
3.60 2.
3.67 2.
3.65 2.
3.64 2.
3.51 3.
NO
LB/IK HP-H«
-0.000
-0.000
-0.000
-0.000
-0.000
11 0.
32 0.
47 0.
86 0.
38 0.
LB/IK
-0
-0
-0
04 -0.00
10 -0.00
II -0.00
15 -0.00
17 -0.00
NO
2
H50.13 -0.
804.13 -0.
774.61 -0.
759.53 -0.
729.31 -0.
NO
X
no i
00 0
00 0
00 0
00 0
.01
.98
.94
.91
.AS
HP-HR LB/IK HP-HR
.000
.000
.000
-o.ocn
-0
.000
4. M6
5.02*
5.177
5.717
6.249
111-43
-------
DtTCl 6/11/71
TEST ORGANIZATION! AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE OAT*
CAL ID NUMBER: 55 ENGINE TYPE AND MODEL: GTCPBS-IIS
RATED SHAFT HORSEPOWER: 160.
ENGINE TOTAL TIME: 0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: o. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
HZ TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1,990
SERIAL NUMBER:
FINISH
FINISH
94.00
28.00
FUEL: jp-4
OPERATIONAL DATA «««»««»«*
INLET AIR TEMPERATURE, DEGREES f. START 94.00
ATMOSPHERIC PRESSURE: START 29.00
INLET AIR HUH 101TT, LBS H20/LB AIR: 0.0045
RELATIVE HUMIDITY: 17.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOH RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
SHP LOADING ONLY
TEST
MODE
I/ 0
6/ 1
ll/ 6
16/11
20/16
POWER
PERCENT
RATED
SHP
0
24
48
M
95
POWER
PERCENT
RATED
SHP
0
24
48
71
95
POWER
PERCENT
RATED
SHP
SHAFT
HP
0.0
38.60
76.90
115.10
153.50
EXHAUST
GAS
TEMP
DEGREES F
540.00
620.00
705.00
130.00
955.00
MASS EMI
CO
LB/IK
LB FUEL
27.47
28.44
27.84
24.65
18.57
CO
LB/IK
HORSEPOWER-HR
24
48
71
95
101.
57.
39.
25.
POWER
AIR
HP
0.0
0.0
0.0
0.0
0.0
EXHAUST
GAS
PRESSUR
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
4.49
3.79
2.74
1.46
0.75
HP-HR
BASIS NOT
684
209
236
646
ENGINE
SPEED
RPM
NI
41200.00
41200.00
41100.00
41000.00
41000.00
CO
IWET)
E PPMV
195.00
235.40
279.10
301.60
259.10
MASS EMI MASS
N02 C
CORRECTED
FUEL
FLOW
N2 Lfl/HR
-0.00 116.40
-0.00 138.00
-0.00 158.00
-0.00 183.20
-0.00 212.00
CO THC
2 IWET)
(WET) PPMV
PERCENT V
1.37 55.80
1.60 54.90
1.93 48.10
2.35 31.20
2.69 18.30
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
NO
IWETI
PPMV
7.70
10.80
18.20
27.00
35.30
EMI MASS EMI MASS EMI MASS
02 NO
LB/IK LB/IK LB/IK
LB FUEL LB
-0.00 3040
-0.00 3030
-0.00 3030
-0.00 3020
-0.00 3020
CO
2
Lfl/lK HP-HR
CALCULABLE*****
10832.637
6225.484
4806.809
4170.941
NOX CO
F/A COMPRESSOR
CALC INLET
FROM TEMP
EMISSIONS OEGREFS F
0.006800 87.00
0.007900 90.00
0.009600 94.00
0.011700 98.00
0.011300 103.00
COMPRESSOR BLEED
DISCHARGE FLOW
PRESSURE LB/MIN
PSIA
53.50 0.0
53.30 0.0
53.00 0.0
52.60 0.0
52.30
0.0
NO NO ALDEHYDES SMOKE PARTICULARS
2 X
IWET) IWET)
PPMV PPMV
7. HO 15.50 -0
9. BO 20.60 -0
8.00 26.20 -0
6.80 33.80 -0
6.60 41.90 -0
FMI MASS EMI MASS EMI
HC N02
LB/IK LB/HR LB/HR LB/HR
.00 -0
.00 -0
.00 -0
.00 -0
.00 -0
"ASS EMI
CO 2
Lfl/HR
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
MASS F.MI MASS EMI
NO NOX
LP/HR LB/HR
FUEL LB FUEL LB FUEL
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
THC
LB/IK HP-HR
11,557
5.630
2,319
1.034
3.59 3.
4.10 3.
4.30 4.
4.53 4.
4.93 3.
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
20 0.52 -0.00
92 0.52 -0.00
40 0.43 -0.00
57 0.27 -0.00
94 0.16 -0.00
NO
2
353.86
418.14
478.74
553.26
640.24
NO
X
-0.00 0.42
-0.00 0.57
-0.00 0.68
-0.00 O.B3
-0.00 1.05
Lfl/lK HP-HH Lfl/lK HP-HR
-0.000
-0.000
-0.000
-o.ooo
14.644
8.835
7.218
6.314
111-44
-------
6/ll/TI
TEST ORGANIZATION! AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE 0»T» »««»»«»»»»»«»««»««««««»«»«»;««««««»«*
CAL ID NUMBER! 7* ENGINE TTPE AND MOOELl GTCPBS-II* SERIAL NUMBER! P-18 702
RATED SHAFT HORSEPOWER! 160.
0. MRS
0. MRS
ENGINE TOTAL TINE)
TINE SINCE HOT SECTION OVERHAUL!
TINE SINCEt
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.990
FINISH 112.00
FINISH 28.00
FUEL: JP-4
OPERATIONAL DATA «»»»»»»
INLET AIR TEMPERATURE, DEGREES F: START 112.00
ATMOSPHERIC PRESSURE! START 28.00
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0045
RELATIVE HUMIDITY: 17.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/HIM:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
COMBINATION SHP/BLEED LOADING
TEST
MODE
22/ 0
19/22
15/19
10/15
5/10
POWER
PERCENT
RATED
SHP
95
71
47
23
0
POWER
PFRCENT
RATED
SHP
95
71
47
21
0
POWER
PERCENT
RATED
SMC
95
71
47
21
0
SHAFT
HP
152.40
114.30
76.40
38.10
0.0
EXHAUST
GAS
TEMP
DEGREES F
1250.00
1250.00
1250.00
1250.00
1248.00
MASS EMI
CO
LB/IK
LB FUFL
9.70
10.49
12.50
12.68
12.42
CO
LB/1K
12.
13.
16.
19.
20.
POWER
AIR
HP
56.88
87.22
107.13
121.16
139.03
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EHI
HC
LB/IK
LB FUEL
0.28
0.34
0.39
0.41
0.36
ENGINE
SPEED
RPM
Nl
40700.00
40700.00
40800.00
40700.00
40800.00
CO
IUETI
PPMV
192.20
206.60
245.50
243.40
245.60
MASS EHI MASS
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
IWET)
PERCENT
3.78
3.76
3.74
3.66
3.77
CORRECTED GAS GEN F/A
FUEL AIR FLOW CALC
FLOW LB/SEC FROM
LB/HR EMISSIONS
266.50 -0.00 0.018800
262.50 -0.00 0.018700
246.50 -0.00 0.018600
241.50 -0.00 0.018200
232.50 -0.00
V
THC NO
IWET) IUETI
PPMV PPMV
9.90 58.30
11.80 56.80
13.40 58.10
13.90 54.40
12.50 54.10
0.019800
NO
2
IWET)
PPMV
5.60
5.80
4.70
7.10
6.20
EMI MASS EMI MASS EMI MASS EMI MASS
N02 C02
LB/IK LA/IK
LB FUEL LB
-0.00 3000
-0.00 1000
-0.00 3000
-0.00 3000
-0.00 3000
CO
2
HP-HR LB/IK HP-HR
157
669
795
236
761
3820.327
3907.790
4029.263
4549.227
5016.887
NO
LR/IK
NOX
LB/IK
CO
LB/HK
HC
COMPRESSOR COMPRESSOR BLEED
INLET DISCHARGE FLOW
TEMP PRESSURE IB/PIN
DEGREES F PSIA
110.00 50.10 41.97
112.00 48.60 66.07
114.00 46.90 81.80
110.00 45.10 99.35
114.00 43.70
NH
t
IWFT)
PPMV
63.90
62.50
62.80
61.50
60.10
E"I MASS
117.04
ALDEHYDES SMOKE PARTICULATES
-0.00 -0.
-o.oo -a.
-n.no -o.
-0.00 -0.
-0.00 -0.
EMI 1ASS Fll
ND2 CO?
LR/HR LH/MR LI/MO
00 -0.00
oo -o.oo
oo -o.oo
00 -0.00
00 -0.00
MASS EMI MASS EM
Nil NOX
LB/H» LB/HR
FUEL LB FUEL LB FUEL
.00
.00
.00
.00
.00
-0.00
-0.00
-0.00
-0.00
-o.oo
THC
LB/IK
0.
0.
0.
0.
0.
HP-HR
162
447
525
620
604
5.30
5.22
5.25
5.26
5.01
NO
LB/IK HP-
-0.000
-0.000
-0.000
-0.000
-0.000
2.59
2.75
3.08
1.06
2.89
0.
0.
0.
0.
0.
HR LB/IK
-0
-0
-0
-0
08 -0
09 -0
10 -0
10 -0
08 -0
NO
2
hP-HR
.000
.000
.000
.000
-0.000
.00 799.50
.00 787.50
.00 719.50
.00 724.50
.00 697.50
NO
X
LH/1K HP-HR
6. 744
6.797
7.058
7.984
8.180
-0.00 1.41
-0.00 1.37
-C.OP 1.10
-0.00 1.27
-0.00 1.1'
111-45
-------
OATE1 4/21/71
TEST ORGAN1IATIO.N: AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE DATA «««»»««»««*»«*«
CAL 10 NUMBER: 56 ENGINE TYPE AND MODEL: GTCPas-i29
RATED SHAFT HORSEPOWER: 160.
ENGINE TOTAL TIME: 0. HRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZ2LE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.990
SERIAL NUMBER!
FINISH
FINISH
65.00
28.66
FUEL: JP-*
OPERATIONAL DATA **»«**»«*»»««»«»
INLET AIR TEMPERATURE, DEGREES F: START 85.00
ATMOSPHERIC PRESSURE: START 28.68
INLET AIR HUM 101rr, LBS H20/LB AIR: 0.0036
RELATIVE HUMIDITY: 23.00 PERCFNT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOH RATE, LITERS/MIS:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTSi 5
COMMENTS!
SHP LOADING ONLY
TEST
MODE
I/ 0
6/ 1
ll/ 6
16/11
20/16
POKER
PERCENT
RATED
SHP
0
25
49
73
96
POHER
PERCENT
RATED
SHP
0
25
49
73
96
POWER
PERCENT
RATED
SHP
SHAFT
HP
0.0
40.60
T8.50
116.90
155.20
EXHAUST
GAS
TEMP
DEGREES f
530.00
590.00
655.00
735.00
850.00
MASS EMI
cn
LB/IK
L» FUEL
23.68
22.00
19.88
21.01
15.17
CO
LB/IK
HORSEPOWER-HR
25
41
73
96
69.
37.
30.
19.
POMER
AIR
HP
0.0
0.0
0.0
0.0
0.0
EXHAUST
GAS
ENGINE
SPEED
RPM
Nl
41400.00
41500.00
41400.00
41300.00
41200.00
CO
(MET)
PRESSURE PPMV
PSIA
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
3.94
2.70
1.74
1.41
0.59
HP-HR
BASIS NOT
562
475
377
886
149.20
172.80
181.00
194.60
187.50
MASS EMI MASS
CORRECTED
FUEL
FLOM
N2 LB/HR
-0.00 111.00
-0.00 129.00
-0.00 148.00
-0.00 169.00
-0.00 203.50
CO THC
2 IUET)
IWET) PPMV
PERCENT V
1.22 43.50
1.52 37.10
1.77 27.80
1.80 22.90
2.39 12.70
GAS
AIR
GEN
FLOM
LB/SEC
-0
-0
-0
-0
-0
.00
.00
.00
.00
.00
NO
IUET)
PPMV
7
9
13
17
24
EMI MASS EMI MASS EMI
N02 C02 NO
LB/IK LB/IK LR/1K
NOX
LB/IK
.50
.10
.20
.30
.90
MASS
CO
F/A
CALC
FROM
EMISSIONS
0.006100
0.007500
0.008700
0.008900
0.011800
NO
2
(WET)
PPMV
13.80
13.50
14.20
15.40
15.20
EMI MASS
HC
COMPRESSOR
INLET
TEMP
DEGREES T
82.00
84.00
84.00
87.00
89.00
COMPRESSOR
DISCHARGE
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
NO ALDEHYDES SMOKE
X
BLEED
FLOM
LB/MIN
0.0
n.o
0.0
0.0
0.0
PARTICULATES
IME7I
PPNV
21
22
27
32
40
EMI
LB/HR LB/HR
.30 -0.
.50 -0.
.40 -0.
.70 -0.
.10 -0.
MASS EMI
HO 2
IB/MR
00 -0.00
00 -0.00
00 -0.00
00 -0.00
oo -o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI MASS EMI
CO 2
LB/HR
NO NOX
LB/HP LB/HR
LR FUEL IB FUEL LB FUEL LB FUEL
-0.00 3050.
-0.00 3050.
-0.00 3050.
-0.00 3050.
-0.00 3040.
CO
2
LB/IK HP-HR
CALCULABLE*****
9643.379
5750.313
4409.320
3986.082
00 -0.00
00 -0.00
00 -0.00
00 -0.00
00 -0.00
THC
LB/IK HP-HR
B.540
1.286
2.046
0.768
5.56
4.71
4.94
5.80
5.33
2.
2.
2.
3.
3.
63 0.
84 0.
94 0.
55 0.
09 0.
Nl)
LB/IK
-0.
-0.
-0.
-0.
HP-MR
000
000
000
000
L8/1K
-0
-0
-0
-0
44
35
26
24
12
NO
J
HP-
.000
.000
.000
.000
-0.00
-0.00
-0.00
-0.00
-0.00
338.55
393.45
451.40
515.45
618.64
NO
X
-0.00 0.62
-0.00 0.61
-0.00 0.73
-0.00 0.98
-0.00 1.08
HR LB/IK HP-HR
t4.t)9B
9.308
8.382
6.990
111-46
-------
OtTEl 4/28/Tl
TST ORGANIZATION! AIRESEARCH
ENGINE SUPPLIER! AIRESEARCN
ENGINE DATA «««*«««**«««»»«««««««««»«««««*««*««**«*i«**«**«»*»«»**«***«*«*««******
CAl ID NUMBER! 73 ENGINE TYPE AND NQDEL1 GTCPB5-I29 SERIAL NUMBER I P-34,763
RATED SHAFT HORSEPOVERl 160.
0. MRS
0. MRS
ENGINE TOTAL TINE:
TINE SINCE HOT .SECTION OVERHAUL:
TINE SINCE!
NI COMPRESSOR OVERHAUL: o. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO: 1.990
FINISH
FINISH
88.00
28.68
FUEL: JP-4
OPERATIONAL DATA ««»«
INLET AIR TEMPERATURE, DEGREES F: START 88.00
ATMOSPHERIC PRESSURE: START 28.68
INLET AIR HUMIDITY. IBS H20/LB AIR: 0.0036
RELATIVE HUMIDITY! 23.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
COMBINATION SHP/BLEED LOADING
TEST
NODE
22/ 0
19/22
15/19
9/15
4/ 9
POMER
PERCENT
RATED
SHP
95
72
49
24
0
POKER
PERCENT
RATED
SHP
95
72
49
24
0
POKER
PERCENT
RATED
SHP
SHAFT
HP
153.40
115.50
T8.50
39.20
0.0
EXHAUST
GAS
TEMP
DEGREES f
1250.00
1230.00
1175.00
1130.00
1100.00
MASS EMI
CO
LB/IK
LB FUEL
6.63
7.09
8. 80
11.77
13. 17
CO
POWER ENGINE CORRECTED GAS GEN F/» CdHPRESSOR COMPRESSOR BLFEn
AIR SPEED FUEL AIR FLOW CALC INLET DISCHARGE FLOW
HP RPN FLOW LB/SEC FROM TEMP PRFSSURE LB/MIN
Nl N2 LB/HR EMISSIONS DEGREES F PSIA
-0.00 10700.00 -0.00 283.20 -0.00 0.018600 88.00 -0.00 58.12
-0.00 40800.00 -0.00 276.20 -0.00 0.018500 88.00 -0.00 79. 6«
-0.00 40900.00 -0.00 259.40 -0.00 0.017400 88.00 -0.00 88.84
-0.00 40900.00 -0.00 239.50 -0.00 0.016400 in. 00 -O.OO 98.34
-0.00 40900.00 -0.00 226.50 -0.00 0.016100 86.00 -0.00 108.91
EXHAUST CO CO THC NO NO Nn ALDEHYDES SMOKE PARTICULATES
GAS (WET) 2 (WETI (KETI 2 X
PRESSURE PPMV (WET! PPMV PPMV IWETI (WETI
PSIA
-0.00
-0.00
-o.oo
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
0.06
0.09
0.09
o.ia
0.18
LB/IK -HP-MR
'HORSEPOWER-HR
*HRR
SEPOWER-MR
*HnRSEPOW£R-HR
*W1R
SEPOHER-HR
*HnRSEPOWfR-HR
BASIS NOT
BASIS NOT
BASIS NOT
BASIS NOT
BASIS NOT
PERCENT V PPM» PPMV
130.10
138.40
160.80
203.10
222.20
MASS EMI H&SS EMI
NH2 C02
LB/IK LB/IK
LB FUEL LB FUEL
-0.00 3010.00
-0.00 3010.00
-0.00 3010.00
-0.00 3010.00
-0.00 3010.00
CO
2
3.75 2.10 61.00 9.
3.74 3.00 59.30 9.
3.50 3.00 51.60 11.
3.31 5.40 44.50 14.
3.24 5.40 41.50 14.
MASS FMI MASS EMI MASS FMI
NO NOX CO
LB/IK LB/IK LB/HR
LB FUEL LB FUEL
-0.00 5.96 1.88
-0.00 5.77 1.96
-0.00 5.68 2.28
-0.00 5.56 2.82
-0.00 5.49 2.98
TMC NO
Lfl/IK MP-HR LB/IK HP-HR LB/IK HP-HR
CALCULABLE*
CALCULABLE*
CALCULABLE*
CALCULABLE*
CALCULABLE*
50 71.20 -0.00 -0.
40 68.60 -0.00 -0.
60 63.20 -0.00 -0.
00 58.40 -0.00 -0.
90 56.40 -0.00 -0.
MASS EMI MASS EMI MASS EMI
HC N02 Cn2
LB/HR LB/HR IB/HP
0.02 -0.00 852.43
0.02 -0.00 831.16
0.02 -0.00 780.79
0.04 -0.00 720.89
O.fl4 -0.00 681.76
NO NO
2 X
L9/IK HP-HR LB/IK MP-HR
00 -0.00
00 -0.00
00 -0.00
00 -0.00
00 -0.00
MASS CMI MASS EMI
NO NOX
LB/HR LB/HR
-0.00 .69
-0.00 .59
-0.00 .47
-0.00 .33
-n.oo .74
111-47
-------
0»TEI 5/IB/TI
TEST ORGANIZATION: AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE 0»T» »*»*»
CAL 10 NUMBER:
57 ENGINE TYPE »ND NOOELt 6TC85-90
RATED SHAFT HORSEPOWER: 0.
ENGINE TOTAL TINEl 0. MRS
TINE SINCE MOT SECTION OVERHAUL: 0. HRS
TINE SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
MI TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL HSC RATIO: 1.377
SERIAL NUMBER:
P-5T86
FUEL: JP-S
OPERATIONAL DATA ««««««««»«»
INLET AIR TEMPERATURE. DEGREES F: START 83.00 FINISH 83.00
ATMOSPHERIC PRESSURE: START 28.79 FINISH 28.79
INLET AIR HUMIOITT. LBS H20/LR AIR: 0.0026
RELATIVE HUMIDITY: 16.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -O.OOi FLOW RATE. LITERS/KIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
NO SHP DATA
PROBE LOCATIONS 1-10
TEST
MODE
I/ 0
2/ 1
3/ 2
4/ 3
5/ 4
POWER
PERCENT
RATER
SHP
0
0
0
0
0
POWER
PERCENT
RATED
SHP
0
0
0
0
0
POWFR
PERCENT
RATED
SHP
SHAFT
HP
0.0
0.0
0.0
0.0
0.0
EXHAUST
GAS
TEMP
DEGREES f
565.00
710.00
850.00
1000.00
1170.00
MASS EMI
CO
LB/1K
L8 FUEL
53.68
39.80
30.26
21.10
14.05
CO
LB/IK
HORSEPOWER-HR
0
n
0
0
99.
57.
36.
26.
POWER
AIR
HP
0.0
55. 84
85.92
106.99
114.34
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
10.57
3.01
0.81
0.16
0.14
ENGINE
SPEED
RPM
Nl
41200.00
41100.00
40900.00
40800.00
40700.00
CO
IWETI
PPMV
418.90
419.50
389.10
327.80
266.90
MASS EMI MASS
CORRECTED
FUEL
FLOW
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
IWET)
PERCENT V
1.49
2.03
2.49
3.00
3.66
EMI MASS
LB/HR
107.90
139.20
164.20
184.50
216.20
THC
IWET)
PPMV
GAS GEN
AIR FLOW
LB/SEC
F/A COMPRESSOR
CALC INLET
FROM TEMP
EMISSIONS DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
NO
IWET)
PPMV
0.
0.
0.
0.
0.
IW
007500
010100
012300
014BOO
018100
NO ND
2
IET) IWE
78.00
80.00
80.00
85.00
92.00
COMPRESSOR BLEFD
DISCHARGE FLOW
PRESSURE LB/MIN
PSIA
51.70
50.20
48.70
46.80
40.20
0.0
43.41
68.80
88.33
109.76
ALDEHYDES SMOKE PARTICULATES
X
T)
PPMV PPMV
144.30
55.60
18.20
4.40
4.50
3.50
11.30
20.20
30.30
43.60
FMI MASS EMI MASS
N02 C02 NO
LB/IK Lfl/IK LB/IK
LB FUEL L8
-0.00 3010
-0.00 3030
-0.00 3040
-0.00 3040
-0.00 3030
cn
2
HP-HR LB/IK HP-HR
NOX CO
11
13
13
11
a
EMI
LB/IK L8/HR
.80 15.
.70 25.
.30 33.
.50 41.
.50 52.
"ASS FMI
HC
LB/HR
30 -0.
00 -0.
50 -0.
90 -0.
10 -0.
MASS EMI
N02
IB/ MR
00 -0
00 -0
00 -0
00 -0
00 -0
MASS EMI
C02
LB/HR
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
MASS EMI MASS EMI
NO NOX
LB/HR LB/HR
FUEL Lfl FUEL LB FUEL
.00 -0.
.00 -0.
.00 -0.
.00 -0.
.00 -0.
THC
LB/IK HP-
00
00
00
00
00
HP
3.21 5.
3.90 5.
4.28 4.
4.43 3.
4.51 3.
NO
LB/IK HP-HR
79
54
97
89
04
1.14
0.42
0.13
0.03
0.03
NO
2
-0.00
-o.oo
-0.00
-0.00
-0.00
324.78
421.78
499.17
560.88
655.09
NO
X
-0.00 0.35
-0.00 0.54
-0.00 0.70
-0.00 0.82
-0.00 0.97
LB/IK HP-HR LB/IK MP-HR
BASIS NOT CALCULABLE*""
216
823
387
562
7553.566
5809.855
5242.527
5729.234
7.514
1.548
0.279
0.257
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
9.715
B. 189
7.636
8.522
111-48
-------
OATEI s/um
TEST ORGANIZATION! AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE 0»T»
CAL ID NUMBER: it ENGINE TYPE AND MODEL: ctce5-9o
RATED SHAFT HORSEPOKERl 0.
ENGINE TOTAL TINE: 0. MRS
TINE SINCE HOT SECTION OVERHAUL! 0. HRS
TINE SINCE:
Nl CONPRESSOR OVERHAUL: 0. HRS
N2 CONPRESSOR OVERHAUL: 0. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOIRE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.1177
SERIAL NUMBER:
FUEL: JP-5
OPERATIONAL DATA ****<
INLET AIR TENPERATURE> DEGREES F: START 88.00 FINISH 68.00
ATMOSPHERIC PRESSURE: START 28.74 FINISH 28.79
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.0026
RELATIVE HUMIDITY: 16.00 PERCENT
SAMPLE LIME: TEMPERATURE. DEGREES C: -0.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME. SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
NO SHP DATA
PROBE LOCATIONS 11-20
TEST
MODE
I/ 0
2/ 1
3/ 2
4/ 1
>/ 4
POWER
PERCENT
RATED
SHP
0
0
0
0
0
POWER
PERCENT
RATED
SHP
0
0
0
0
0
POKER
PERCENT
RATED
SHP
SHAFT
HP
0.0
0.0
0.0
0.0
0.0
EXHAUST
GAS
TEMP
DEGREES F
569.00
710.00
850.00
1000.00
1170.00
MASS EMI
CO
L8/IK
L8 FUEL
55.20
14.12
29.21
19.28
11.26
CO
LB/IK
HORSEPOUER-HR
0
0
0
0
91.
55.
12.
25.
POWER
AIR
HP
0.0
57.68
86.06
109.02
111.35
EXHAUST
GAS
PRESSURE
PSU
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
12.26
3.12
0.76
0.18
0.08
ENGINE
Nl
41200.
41100.
40900.
40800.
40700.
SPEED
RPM
00
00
00
00
00
CO
IHETI
PP
405.
398.
164.
MV
70
50
00
290.10
211.
MASS Ell
N<12
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
HP-HR LB/IK HP-H
80
MASS
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
(WET)
PERCENT
1.40
1.96
2.41
2.92
1.38
CORRECTED
FUEL
FLOW
LB/HR
107.90
137. 10
162.10
185.50
211.00
THC
(HETI
PPMV
V
157.70
55.10
16.60
4.80
2.60
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
NO
(WETI
PPMV
7.00
17.20
27.30
37.30
44.20
EMI MASS EMI MASS FMI MASS
CO 2
LB/IK
LB
3000
3040
3040
3040
3040
NO
la/iK
MIX CO
F/A COMPRESSOR
CALC INLET
FROM TEMP
EMISSIONS DEGREES F
0.007100 84.00
0.009700 86.00
0. 011900 87.00
0.014300 90.00
0.016600 92.00
COMPRESSOR
DISCHARGE
PRESSURE
PSU
51.70
50.00
48. tO
46.00
19.70
NO NO ALDEHYDES SMOKE
2 X
(WEI) IWET)
PPMV PPMV
9.00 16.00 -0
8.90 26.10 -0
7.90 35.10 -0
5.90 43.20 -0
6.10 50.50 -0
EMI MASS FM1 MASS FM 1
HC N02
LB/IK LB/HR LB/HR LB/HR
.00 -0.00
.00 -o.oo
.00 -o.oo
.00 -0.00
.00 -0.00
MASS F1I MASS
r.n2 NU
BLEFD
FLOW
IB/Ml
o.n
44.52
68.59
89.19
IOH. 44
N
PAPTICULATES
-0.
-0.
-0.
-0.
-0.
00
00
00
00
00
FWI 1ASS EMI
LB/HS LP/HB
NOX
LB/HR
FUEL LB FUEL LB FUEL
.00
.00
.00
.00
.00
-n.oo
-0.00
-0.00
-0.00
-0.00
THt
IR
LB/IK
HP-HR
1.57 5.
4.J1 5.
4.64 4.
4.71 1.
4.75 2.
NU
LR/1K HP-HR
96 1.32 -1.00
39 0.41 -0.00
74 0.12 -0.00
5H 0.03 -0.00
80 0.02 -0.00
NO
?
121.70 -0.
416.78 -0.
492.78 -0.
563.92 -0.
641.44 -0.
Nl)
X
00
00
00
00
on
0.18
0.58
0.75
0.87
1.00
L3/1K HP-HR L9/1K HO-HR
BASIS NOT CALCULABLE**"*
469
056
81*
126
7225.906
5725.965
5172.656
5760.457
7.
1.
0.
0.
411
431
111
161
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
1 0. 059
B.712
8.02!
8.995
111-49
-------
DATE! 6/16/71
TEST ORGANUATION! AIRESEARCH
ENGINE SUPPLIER I AIRESEARCH
ENGINE DATA
CAL ID NUMBER! 59 ENGINE TYPE AND MODEL! GTC85-90-2
RATED SHAFT HORSEPOWER! 0.
ENGINE TOTAL TIMEl 0. HRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOIZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO! 1.928
SERIAL NUMBER'
FINISH 108.00
FINISH 28.70
FUEL: JP-5
OPERATIONAL DATA «»»»»»«»*«
INLET AIR TEMPERATURE, DEGREES F: START 108.00
ATMOSPHERIC PRESSURE: START 28.TO
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0046
RELATIVE HUMIDITY: 9.00 PERCENT
SAMPLE LINE! TEMPERATUREt DEGREES C: -0.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
NO SHP DAT*
PROBE LOCATIONS 1-10
-0.00
TEST
MODE
I/ 0
2/ 1
11 2
4/ 3
5/ 4
POWER
PERCENT
RATED
SHP
0
0
0
0
0
PDWFR
PERCENT
RATED
SHP
0
0
0
0
0
POWER
PERCENT
RATED
SHP
POWER ENGINE CORRECTED
SHAFT AIR SPEED FUEL
HP HP RPM FLOW
Nl N2 LB/HR
0.0 0.0 41200.00 -0.00 -0.00
0.0 47.65 41100.00 -0.00 -0.00
0.0 80.90 40800.00 -0.00 -0.00
0.0 106.25 40700.00 -0.00 -0.00
0.0 70.88 40500.00 -0.00 -0.00
EXHAUST EXHAUST CO CO THC
GAS GAS (WETI 2 IWFTI
TEMP PRESSURE PPMV IWET) PPMV
DEGREES F PSIA PERCENT V
602.00 -0.00 381.60 1.47 22.70
745.00 -0.00 461.10 1.93 11.10
900.00 -0.00 494.60 2.38 4.50
1052.00 -0.00 438.80 2.93 0.60
11TO.OO -0.00 385.50 1.38 0.50
GAS GEN F/A COMPRESSOR
AIR FLOW CALC INLET
LB/SEC FROM TEMP
EMISSIONS DEGREES F
28.00 0.007300 109.00
-0.00 0.009600 107.00
-0.00 0.011900 108.00
-0.00 0.014500 108.00
-0.00 0.016800 108.00
COMPRESSOR BLEED
DISCHARGE FLOW
PRESSURE LB/MIN
PSIA
-0.00
49.20
47.30
45.80
29.30
0.0
35. 9R
63.40
B6.05
101.07
NO NO NO ALDEHYDES SMOKE PARTICULATES
IWETI 2 X
PPMV (WETI IWETI
PPMV PPMV
B.40 8.10 16.50 -0.
12.70 11.20 23.90 -0.
17.30 11.90 29.20 -0.
25.20 11.50 36.70 -0.
34.00 9.40 43.40 -0.
MASS EMI MASS EMI KASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS FMI MASS EMI
CO HC N02 C02 NO
LB/IK LB/IK LB/IK LB/IK LB/IK
NOX CO HC N02
LB/IK LB/HR LB/HR LB/HR
00 -0
00 -0
00 -0
00 -0
00 -0
MASS EMI
CO 2
LB/HH
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
MASS FMI MASS EMI
NO NOX
LB/HR LB/HR
LB FUEL L8 FUEL LB FUEL LB FUEL LB FUEL LB FUEL
49.93 1.69 -0.00 1020.00 -0.00
45.83 0.63 -0.00 3020.00 -0.00
39.83 0.21 -0.00 3020.00 -0.00
28.77 0.02 -0.00 3020.00 -0.00
21. B8 0.01 -0.00 3010.00 -0.00
CO CO THC
7
LB/IK HP-HR Lfl/lK HP-HR LB/IK HP-HR
3.54 -0.00 -0.00 -0.00
3.90 -0.00 -0.00 -0.00
3.86 -0.00 -0.00 -0.00
3.95 -0.00 -0.00 -0.00
4.05 -0.00 -0.00 -0.00
NO NO
2
LB/IK HP-HH LB/IK HP-HR L6/
-0.00
-0.00
-0.00
-0.00
-0.00
NO
X
IK HP-HR
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
HORSEPOWER-HR BASIS NOT CALCULABLE*****
0
0
0
0
-0.000 -0.000 -0.000
-0.000 -0.000 -0.000
-0.000 -0.000 -0.000
-0.000 -0.000 -0.000
-0.000 -0.000
-0.000 -0.000
-0.000 -0.000
-0.000 -0.000
-0.000
-0.000
-0.000
-o.ooo
111-50
-------
OATH 6/U/TI
TEST ORGANIZATION! AIRESEARCH
ENGINE SUPPLIERl AIRESEARCH
ENGINE OUT* »»«»»«««»«»»»
CAl ID NUMBER: TT ENGINE TYPE AND MODELl GTC8S-90-2
RATED SHAFT MORSEPOWERl 0.
ENGINE TOTAL TINE)
TINE SINCE HOT SECTION OVERHAUL:
TINE SINCE:
SERIAL NUMBER:
P-34276B
0. HRS
0. HRS
NI COMPRESSOR OVERHAUL: o. HRS
HZ COMPRESSOR OVERHAUL! 0. HRS
COKBUStOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: o. HRS
FUEL H/C RATIO: 1.928
FINISH 108.00
FINISH 29.70
FUEL: JP-S
OPERATIONAL DATA »«
INLET AIR TEMPERATURE. DEGREES F: START 108.00
ATMOSPHERIC PRESSURE: START 28.70
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.0046
RELATIVE HUMIDITY: 9.00 PERCENT
SAMPLE LINF: TEMPERATUREi DEGREES C: -0.00. FLOM RATE, LITERS/MIN:
SAHPLE LINE TRANSPORT TINE. SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
NO SHP DATA
PROBE LOCATIONS 11-20
TEST
NODE
I/ 0
2/ 1
3/ 2
4/ 3
5/ 4
POWER
PF.RCFNT
RATED
SHP
0
0
0
0
0
POWER
PERCENT
RATED
SHP
0
0
0
0
0
POWER
PERCENT
RATED
SHP
SHAFT
HP
0.0
0.0
0.0
0.0
0.0
EXHAUST
GAS
TEMP
DEGREES F
602.00
750.00
900.00
1050.00
1167.00
MASS ENI
CO
LB/IK
LB FUEL
52.35
46.23
40.12
28.81
21.21
CO
POWER
AIR
HP
0.0
48.10
81.69
107.09
70.96
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
in FUEL
2.02
0.88
0.39
0.07
0.02
ENGINE
SPEED
RPM
NI
41300.00
41100.00
40800.00
40600.00
40500.00
CO
IWETI
PPMV
398.50
457.90
500.30
448.50
381.60
MASS EMI MASS
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
(WET)
PERCENT
1.47
1.90
2.39
2.99
3.45
CORRECTED
FUEL
FLOW
LB/MR
101.00
127.00
157.00
179.00
198.00
THC
IWEU
PPMV
V
27.00
15.30
8.60
1.80
0.80
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
NO
IWEt)
PPMV
13.60
17.80
25.30
34.10
39.80
EMI HASS EMI MASS EMI MASS
N02 C02
LB/IK LB/IK
LB FUEL 18
-0.00 3020
-0.00 3020
-0.00 3010
-0.00 3010
-0.00 3010
CO
2
LB/IK HP-HR LB/IK HP-HR
HORSEP(ttlER-HR
0
0
0
0
122.
77.
48.
S9.
NO
LB/IK
F/A
CALC
FROM
EMISSIONS
0.007300
0.009500
0.011900
0.014800
0.017100
NO
2
IWET)
PPMV
4.50
5.40
4.30
2.60
3.60
EMI MASS
NOX CO HC
COMPRESSOR
INLET
TEMP
DEGREES F
107.00
108.00
109.00
108.00
108.00
COMPRESSOR
DISCHARGE
PRESSURE
PSIA
-0.00
49.20
47.50
46.00
29.30
NO ALDEHYDES SMOKE
X
IWETI
PPMV
IS. 10 -0
23.20 -0
29.60 -0
36.70 -0
43.50 -0
FMI HASS EMI
N02
LB/IK LB/HR LB/HR LB/HR
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
MASS Fll MASS
cn? NO
BLEED
FLOW
LB/MIN
0.0
36.75
63.64
86. 34
101.21
PART1CULATES
-0.00
-0.00
-0.00
-0.00
-0.00
EMI MASS
F«
NOI
LH/HR LB/HR LB/HR
FUEL LB FUFL LB FUEL
.00
.00
.00
.00
.00
-0.00
-0.00
-o.oo
-0.00
-0.00
THC
LB/IK
HP-HR
3.90 5
3.85 5
3.90 6
3.88 5
3.97 4
NO
LB/IK HP-HR
.29 0.
.87 0.
.30 0.
.16 0.
.20 0.
LB/IK
20 -0.00
11 -0.00
06 -0.00
01 -0.00
00 -0.00
NO
2
105.0? -0.
393.54 -0.
472.57 -0.
538.79 -0.
595.98 -0.
NO
X
00 0
00 0
00 0
oo o
00 0
.39
.49
.61
.69
.79
HP-HR LB/IK HP-HR
BASIS NOT CALCULABLE*****
077
105
161
175
7974.418
5784.902
5031.230
BJ97.004
2.
0.
0.
0.
337
757
112
070
-0.000
-0.000
-0.000
-0.000
-d
1.000
-0.010
-0
1.000
-0.000
10. I5fl
7.49?
6. 477
11.072
111-51
-------
DATE: 6/16/T1
TEST ORGANIZATION: AIRESEARCH
ENGINE SUPPLIER! AIRESEARCM
ENGINE DATA
c»i 10 NUMBER:
78
ENGINE TYPE »NO MODEL: GTC85-90-2
RATED SHAFT HORSEPOWER: 0.
ENGINE TOTAL TINE:
TINE SINCE HOT SECTION OVERHAUL:
TINE SINCE:
SERIAL NUMBER! P-243T6C
0. HRS
0. HRS
Nl COMPRESSOR OVERHAUL: 0. HRS
NZ COMPRESSOR OVERHAUL: o. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO: 1.928
FINISH 105.00
FINISH 28.70
FUEL: jp-5
OPERATIONAL DATA ««««««»«*««
INLET AIR TEMPERATURE. DEGREES F: START IDS.00
ATMOSPHERIC PRESSURE: START 28.70
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0046
RELATIVE HUMIDITY: 9.00 PERCENT
SAMPLE LINE: TENPERATUREi DEGREES C: -0.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TINE, SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
NO SHP DATA
12 POINT F1IED PROBE
-0.00
TEST
MODE
I/ 0
2/ 1
3/ 2
4/ 3
5/ 4
POMER
PFRCENT
RATED
SHP
0
0
0
0
0
POWER
PERCENT
RATED
SHP
0
0
0
0
0
POWER
PFRCFNT
BATED
SHP
SHAFT
HP
0.0
0.0
0.0
0.0
0.0
EXHAUST
GAS
TEMP
DEGREES F
605.00
742 . 00
400.00
1045.00
1156.00
MASS EMI
CO
LB/IK
LB FUEL
51.00
46.90
39.47
30.24
23.05
CO
LB/IK
HORSEPOUER-HR
0
0
0
0
125.
76.
51.
19.
POWER
AIR
HP
0.0
47.60
80.37
104.33
114.45
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-o.on
-0.00
MASS EMI
HC
IB/IK
LB FUEL
2.29
1.05
0.59
0.21
o.ia
ENGINE
SPEED
RPM
Nl
41300.00
41100.00
40900.00
40700.00
40500.00
CO
IWETI
PPMV
394.00
462.30
488.90
451.60
405.40
MASS EMI MASS
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
(WETI
PERCENT
1.45
1.84
2.38
2.87
3.37
CORRECTED
FUEL
FLOW
LB/HR
101.50
127.00
155.00
179.00
198.00
THC
IWET)
PPMV
V
30.00
18.00
12.80
5.60
5.60
GAS GEN
AIR FLOW
L8/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
NO
IWET)
PPMV
10.60
17.60
18.10
25.20
30.90
EMI MASS EM] MASS EMI MASS
N02 C02
LB/IK LB/
IK
NO
LB/IK
NOX CO
LB/IK LB/
F/A
CALC
FROM
EMISSIONS
0.007200
0.009400
0.011800
0.014200
0.016700
NO
2
(WETI
PPMV
6.00
4.80
10.10
-0.00
8.90
EMI MASS
HC
HR LB/
COMPRESSOR
INLET
IEMP
DEGREES F
104.00
106.00
105.00
105.00
105.00
COMPRESSOR
DISCHARGE
PRESSURE
PSIA
51.10
49.40
48.00
46.50
43.60
NO ALDEHYDES SMOKE
X
(WFT)
PPMV
16.60 -0.
22.50 -0.
28.20 -0.
35.00 -0.
39.80 -0.
EMI MASS EMI
N02
HR L8/HR
00 -0.00
00 -0.00
00 -0.00
00 -0.00
00 -0.00
BLEED
FLOW
LB/MIN
C.O
35.86
62.40
83.63
98. 12
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
MASS F*4! MASS EMI MASS
CO?
LB/HR
EM
NO Nttt
LB/HR LB/
HR
LB FUEL LB FUEL LB FUEL LB FUEL
-0.00 3030.
-0.00 3020.
-0.00 3010.
-0.00 3010.
-0.00 3010.
CO
2
HP-HR IB/ IK HP-HR
00
00
00
00
00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
Lfl/lK
HP-HH
3.63 5.
3.74 5.
3.74 6.
3.88 5.
3.72 4.
NO
LB/IK HP-HR
18 0.
96 0.
12 0.
41 0.
56 0.
L8/1K
23 -0.00
13 -0.00
09 -0.00
04 -0.00
04 -o.on
NO
1
307.54
383.54
466.55
538.79
595.99
NO
X
-0.00 0.
-0.00 0.
-0.00 0.
-0.00 0.
-0.00 0.
37
48
58
69
74
HP-MR LB/IK HP-HH
BASIS NOT CALCULABLE"'*'
147
129
885
8T4
H057.625
5804.875
5164.426
5207.453
2.
1.
0.
0.
801
144
367
315
-0.000
-0.000
-0.000
-0.000
-0
-0
-0
-0
.000
.000
.000
.COO
9.992
7.217
6.657
6.431
111-52
-------
OtTEl 4/16/71
TEST ORGANIZATION! AIRESEARCH
ENGINE SUPPLIER! AIRESEARCH
ENGINE 0»TA
CAl ID NUMBER! T9 ENGINE TYPE AND NOOELI GTC85-90-2
RATED SHAFT HORSEPOWER! 0.
ENGINE TOTAL TIME) 0. MRS
TINE SINCE HOT SECTION OVERHAUL! 0. HRS
TINE SINCE"
NI COMPRESSOR OVERHAUL: o. HRS
N2 CONPRESSOR OVERHAUL! 0. HRS
COM8USTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL! 0. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: I.92B
SERIAL NUMBER!
FINISH 108.00
FINISH 26.70
FUEL: JP-5
OPERATIONAL DATA «««
INLET AIR TENPERATURE. DEGREES F: START 108.00
ATMOSPHERIC PRESSURE: START 28.70
INLET AIR HUHIDITT, LBS H20/LB AIR: 0.0046
RELATIVE HUMIDITY: 9.00 PERCENT
SAMPLE LINE: TENPERATURE. DEGREES C: -0.00, FLOW KITE. LITERS/MINI
SAMPLE LINE TRANSPORT TIME. SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
NO SHP
12 POINT MOVABLE PROBEIAVERAGE OF LOCATIONS 1-201
EMISSION RATES NOT CALCULATED BY TEST ORGANIZATION
TEST
MODE
I/ 0
21 1
3/ 2
4/ 3
5/ 4
POWER
PERCENT
RATED
SHP
0
0
0
0
0
POWER
PERCENT
RATED
SHP
0
0
0
0
0
POWER
PERCENT
RATED
SHP
SHAFT
HP
0.0
0.0
0.0
0.0
0.0
EXHAUST
GAS
TEMP
DEGREES F
602.00
750.00
900.00
1050.00
1167.00
MASS EMI
CO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
CO
LR/IK
HORSEPOWER-HR
0
0
0
0
-0.
-0.
-0.
-0.
POWER ENGINE CORRECTED GAS GEN F/A COMPRESSOR COMPRESSOR BLEED
AIR SPEED FUEL AIR FLOW CALC INLFT DISCHARGE FLOW
HP RPM FLOW LB/SEC FROM TEMP PRESSURE LB/MIN
Nl N2 LB/HR EMISSIONS DEGREES F PSU
0.0 41300.00 '0.00 101.00 -0.00 0.007300 107.00 I'l.lO 0.0
48.10 41100.00 -0.00 127.00 -0.00 0.009500 10B.OO 49.20 16.25
81.69 40800.00 -0.00 157.00 -0.00 0.011900 109.00 47.50 61.64
107.09 40600.00 '0.00 179.00 -0.00 0. 014X00 108.00 46.00 66.34
70.98 40500.00 -0.00 198.00 -0.00 0.017100 106.00 29. .10 101.71
EXHAUST CO CO THC NO NO NO ALDEHYDES SMOXF P4RT ICUL ATF.S
GAS IWET) 2 IWETI IWET) 2 X
PRESSURE PPMV IWET) PPMV PPMV IWET) (WFTI
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
HP-HR
BASIS NOT
000
000
000
ooo
PERCENT V
390.00
459.50
497.50
443.70
393.50
MASS EMI MASS EMI
N02 C02
LB/IK LB/IK
LB FUEL LB FUEL
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-o.oo -o.oo
-0.00 -0.00
CO
2
1.47 24.
1.91 13.
2.39 6.
2.96 1.
3.42 0.
MASS EHI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
THC
LB/IK HP-HR LB/IK HP-HR
CALCULABLE'****
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-o.ooo
-0.000
80 II
50 15
50 21
20 29
65 36
MASS EMI
NOX
LB/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
PPMV PPMV
.00 6
.30 8
.30 8
.70 6
.90 6
MASS EMI
cn
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
NO
LB/IK
-0.
-0.
-0.
-0.
HP-HR
000
000
000
000
.10 17.
.30 21.
.10 29.
.60 36.
.50 41.
MASS EMI
HC
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
HO
?
30 -0.00
50 -0.00
40 -0.00
70 -0.00
40 -0.00
-0
-0
-0
-0
-0
MASS fMI MASS EMI
N02
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
C02
LB/HR
-0.00
-0.10
-0.00
-o.no
-o.oo
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
MASS EMI MASS
EMI
MO NOX
LB/HR Lfl/HR
-0.00 -0
-0.00 -0
-0.90 -0
-0.00 -0
-o.no -o
.00
.00
.00
.00
.00
NO
LB/IK HP-HR LB/IK
-0.000
-0.000
-0.000
-0.000
-0
-0
-0
-0
X
HP-MR
.000
.000
.000
.000
111-53
-------
DATEl S/ 5/71
TEST ORGANIZATION: AIRESEARCH
ENGINE SUPPLIER: AIRESEARCH
ENGINE OAT*
CAL ID NUMBER: SB ENGINE TYPE AND HODELI GTcas-90-2
RATED SHAFT HORSEPOUER: 0.
ENGINE TOTAL TINE: 0. MRS
TINE SINCE HOT SECTION OVERHAUL: 0. HRS
TINE SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
HZ COMPRESSOR OVERHAUL: 0. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.990
SERIAL NUMBER:
P-2450*
FINISH
FINISH
79.00
0.0
FUEL: jp-4
OPERATIONAL DATA «««»**»*««»«
INLET AIR TEMPERATURE, DEGREES F: START T9.00
ATMOSPHERIC PRESSURE: START 28.5*
INLET AIR HUMIDITY. LBS H2O/LB AIR: 0.004;
RELATIVE HUMIDITY: 23.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00. FLOM RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME. SEC: -0.00
NUMBER DF TESTS: 5
COMMENTS:
TEST
MODE
I/ 0
21 1
I/ 2
4/ 3
5/ 4
POKER
PERCENT
RATED
SHP
0
0
0
0
0
POKER
PERCENT
RATED
SHP
0
0
0
0
0
POKER
PERCENT
RATED
SHP
SHAFT
HP
0.0
0.0
0.0
0.0
0.0
EXHAUST
GAS
TEMP
DEGREES f
5*5.00
675.00
825.00
975.00
1125.00
MASS EMI
CO
LB/U
LB FUEL
50.12
46.89
43.99
35.39
23. 42
CO
LB/1H
HORSEPONER-HR
0
0
0
0
-0.
-0.
-0.
-0.
POKER
AIR
HP
0.0
42.31
82.57
107.97
127.37
EXHAUST
GAS
PRESSURE
PSIA
-o. on
-0.00
-o.oo
-0.00
-0.00
MASS EMI
HC
LB/1K
LB FUEL
4.86
2.92
1.65
0.99
0.20
ENGINE
SPEED
RPM
Nl
40850.00
40760.00
40660.00
40580.00
40450.00
CO
IKET)
PPMV
341.50
429.90
501.90
49B.OO
419.50
MASS EMI MASS
N02 C
N2
-0.00
-0.00
-0.00
-0.00
-0.00
CO
2
IKET)
PERCENT
1.30
1.75
2.17
2.68
3.41
CORRECTED
FUEL
Finn
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
THC
IKET)
PPMV
V
58.00
46.80
36.90
24.50
6.30
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
NO
IUETI
PPMV
3.10
6.20
12.70
20.70
30.60
EMI MASS EMI MASS EMI MASS
02
LB/1K LB/IK
LB FUEL LB
-0.00 3010
-0.00 3000
-0.00 2990
-0.00 2990
-0.00 2990
CO
2
HP-HR LB/1K HP-HR
NO
LB/IK
NOX C
F/A
CALC
FROM
EMISSIONS
0.006500
0.008800
0.010900
0.013400
0.017000
NO
2
(MET)
PPMV
12.90
14.30
15.30
11.70
12.60
EMI MASS
0 HC
COMPRESSOR
INLET
TEMP
DEGREES F
77.00
76.00
91.00
62.00
77.00
COMPRESSOR
DISCHARGE
PRESSURE
PSIA
S3. 50
52.50
51.20
50.00
49.30
NO ALDEHYDES SMOKE
X
IKET)
PPMV
16.10
20.60
27.90
34.40
43.20
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
EMI MUSS EMI M»SS EMI MASS
N02
Lfl/IK LB/HR LR/HR LB/HR
C02 Nn
BLEED
FLOH
LB/MIN
0.0
31.76
62.87
83.95
101.34
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
EMI MASS
N
EMI
ox
LB/H« LB/HR LB/HR
FUEL LB FUEL LB FUEL
.00
.00
.00
.00
.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
LB/IK
HP-HR
3.67 -0
3.69 -0
4.02 -0
4.02 -0
3.96 -0
NCI
L8/1K HP-HR
.00 -0.
.00 -0.
.00 -0.
.00 -0.
.00 -0.
Lfl/IK
00 -0.00
no -o.oo
on -o.oo
00 -0.00
00 -0.00
Nil
2
HP-HR
-0.00 -0.
-0.00 -0.
-0.00 -0.
-0.00 -0.
-0.00 -0.
NO
X
Lfl/IK MP-Hfl
00 -0
00 -0
00 -0
00 -0
00 -0
.00
.00
.00
.00
.00
BASIS MOI CALCULABLE"*"
000
000
000
000
-0.000
-o.ooo
-0.000
-0.000
-0.
-0.
-0.
-0.
000
000
000
000
-0.000
-0.000
-0.000
-0.000
-0
-0
-0
-0
.000
.000
.000
.000
-0.000
-0.000
-0.000
-0.000
111-54
-------
TABLE nr
TURBINE/TURBOPROP ENGINES
(UNWEIGHTED PROCESSING)
CONTENTS:
IV-2 TO IV-299 INDIVIDUAL ENGINE RUNS - COMPLETELY PROCESSED
IV-300 TO IV-312 MODEL SUMMARIES
IV-313 TO IV-361 INDIVIDUAL ENGINE RUNS - MASS EMISSION
CONVERSIONS ONLY
IV-362 INDIVIDUAL RUN - INPUT DATA REPRODUCED ONLY
IV-1
-------
01TCI ' 4/11/71
TEST OKGANIUTIONl S K I I KELLY
ENGINE SUPPLIFRI USAF, KELLY Ufa
ENGINE DATA »»»««»»»«»»««»»»»»»»»»»»«»»»»««««»»»»»»»»«»»»«»»»«»»»»«««»»»«»»«»»««»»«»»»«»»»«««»
t
CAL ID NUMBER: 2 ENGINE TYPE AND MOOELI n*-»r« IERIAL numim
R.ATEO KORJEPOKfKt ITU.
ENGINE TOTAL TIMEl til*. MRS
TIKE SINCE Mfif sFcrinN OVERHAUL: o. MRS
TINE SINCE!
Nl COMPRESSOR OVERHAUL: 0. MRS
N2 COMPRESSOR OVERHtULi -0. MRS
COMfluSTOR ON REPLACEMENT: 0. MRS
FIRST STAGE NOmf GUIDE VANE OVERHAUL! 0. MRS
XI TURBINE OVERHAUL! 0. MRS
N2 TURBINE OVERHAUL: -o. MRS
FUEL! JP-4 FUEL H/C RAT In: 1.991
OPERATIONAL DATA «««»»
INLET AIR TF"PFOATURE, DEGREES f : START 80.00 FINISH ID. 00
ATMOSPHERIC PRESSURE! START 29. 26 FINISH 29.26
INLET AIR HUMIDITY, LBS H2Q/LB AIR: 0.021*
RELATIVE HUMIDITY: 63.00 PERCENT
SAMPLE LINE: TEMPERATURE, OEGRFFS C: ISO. 00, FLOW RATE, LITERS/MIN: 42.50
SAMPLE LINF TUANSPORT TIME, SEC: 0.50
NUMBER OF TESTS: a
COMMENTS:
F/A CALCUIAUC1N B4SFO ON EXHAUST CHMPflSITION FOR LAST RUN
»»«»«»«»»»»«»»»»»»»
FLAPSEO
IIMF
0.0
5.30
11.00
16.10
19.30
71.10
7.4.00
76.30
IEST
MPDE
I/ 0
71 1
I/ 2
4/ 1
5/ 4
4/ S
8/ 4
11 R
POWER
THRUST, IBS
OR
SHP
7175.00
120?. 00
3553.00
h65.00
3684.00
865.00
777.00
1 19.00
PE'CFNT
RATED
T.O.
61
85
94
21
IS
21
;
3
ENC
SI
*
Nl
[3800. OC
1)800.00
13800. 00
11100.00
14200.00
13100.00
11430.00
99RO.OO
RPM
N?
-o.oo
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MEASURED
FUEL
FLOW
LB/HR
1*6*.00
mo.oo
19*5.00
910.00
1980.00
90S.00
711.00
555.00
GAS GEN
AIR FLOW
LB/SEC
30.80
30.80
30.80
78. 7P
37.60
78.70
29.20
15.00
CALC
F/A
0.013200
0.016300
0.017500
0.009SOO
0.016800
0.008800
0.006800
0.010300
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURF
RATIO
FPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
TURBINF
INLET
TEMP
OEGRFES F
1505.00
1710.00
1780.00
1169.00
1900.00
1170.00
1046.00
1128.00
PQUF.D
"ERCENT
ft ATFn
T.O.
61
«5
94
73
SB
?3
7
3
F. xMiusr
OS
TCWP
OFGRFFS ^
-n. oo
-0.00
-n.on
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
F XM4UST
GAS
PRESSURF.
PSU
-0.00
-0.00
-o.on
-o.oo
-o.oo
-o.oo
-0.00
-0.00
en
(WET)
ppwy
78.00
26.00
24.00
77.00
23.00
30.00
27.00
771.00
(WETI
PEHCENT
2.17
3.08
3.78
1.66
3.54
1.64
1.1?
2.07
THC
IWFTI
PPMV
0.0
0.0
0.0
o.n
0.0
5.00
2.00
275.00
NCI
(WEt|
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
2
IWEII
PPMV
-0.00
-0.00
-0.00
-0.00
-O.on
-0.00
-0.00
-0.00
ALOEHYOFS SMOKE PARTICULATFS
(WEII
PPMV
A8.00
96.00
102.00
32.00
102.00
32.00
74.00
25.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
POHFR
PERCENT
DATED
T.l.
M
BS
M4
?1
98
?1
T
3
MASS EMI
cn
1. P/ IK
Ln FUEL
2. IK
1 .64
1.46
3.24
1.30
1.65
'..08
7S.54
.MASS EMI
HC
LR/1K
LB FUEL
0.0
0.0
0.0
n.O
0.0
0.35
0.17
12.15
MASS E»l
N02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C07
LB/IK
L1 FUEL
3135.17
1136.22
3136.56
3133.77
3136. B3
3132.19
11 31.99
1065.42
MASS EMI
NO
LH/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00 '
-0.00
-0.00
-0.00
MASS EMI
SDK
LB/IK
L8 FUEL
9.40
10.72
10.70
6.32
9.45
6.39
5.95
3.87
MASS EMI
cn
Lfl/HR
1.45
1.05
7.84
2.95
7.57
3.30
7.92
14. IB
MASS EMI
HC
LB/HR
0.0
0.0
0.0
0.0
0.0
0.32
0.12
6.74
MASS EMI
NO 2
LB/HK
-0.00
-0.00
-o.on
-0.00
-0.00
-0.00
-o.on
-0.00
MASS [Ml
C02
LB/HR
4593.0?
5676.56
6100.64
2851.73
6210. 9J
2B34.63
2239.17
1701.31
MASS EMI
NO
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
N0>
LB/HR
13.78
18.50
19.8]
5.75
18.71
5.7fl
4.26
2.15
POWER
PFRCFNT
RATFO
T.O.
61
85
94
73
9<
23
7
1
cn
LRMK HP-HM
1.4B5
O.T52
0.500
3.413
O.i97
3.315
10.S24
119.123
L6/IK HP-HH
1975.491
1772.81H
1717.039
1296.804
16H5.919
3277.030
8014.383
14296.711
THC
LB/IK HP-HK
0.0
0.0
0.0
0.0
0.0
0. 364
0.446
56.644
un
LB/IK HP-19
-0.000
-0.000
-0.000
-0.000
-0.000
-O.OOT
-o.oo.i
-0.000
LB/IK HP-HR
-0.000
-o.ooo
-0.100
-0.000
-o.ooo
-0.000
-0.000
-0.000
NO
X
LB/IK MP-HR
5.975
5.777
5.5B2
6.644
5.078
6.665
15.366
IB.050
IV-2
-------
CAL 10 NUNBERl 2 ENGINE TYPE AND MODEL I T56-A7B
TEST ORGANIZATION! S W R I KELLY
SERIAL NUMBER! AE-103141
NODE
FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIHROUT
APPROACH
TAXI-IDLE
0.030
1.000
0.900
0.300
0.030
POWER
HP
112.6
3755.0
1179.5
1126.9
112.6
EMISSION
RATE
Lfl/HR
20.406
2.500
2.81*
3.438
20.906
FUEL
RATE
LB/HR
979.903
2032.360
1891.819
1071.003
979.903
USAGE TIME IN
MT FACTOR MODE
MIN.
1.000
1.000
1.000
1.000
I.000
19.00
0.90
2.90
4.90
7.00
TOTAL FOR CVCLEl
LBS POLLUTANT/IK LB FUEl/CYCLEl
LBS POLLUTANT/IK HP-MR/CVCLEl
LBS POILUTANT/1000K HP AT T.O.I
CO
MASS
LBS.
6.620
0.021
0.117
0.299
2.439
9.496
22.226
30.964
0.999
FUEL
MASS
LBS.
182.24
16.94
78.83
80.33
67.14
LB CO /
IK LB FUEL
36.326
1.230
1.487
3.229
36.326
ENERGY
HP-HR
39.67
11.29
140.81
94.49
13.14
LB CO /
HP-HR
0.18598
0.00067
0.00081
0.00307
0.18998
425.47
MODE
FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
0.030
1.000
0.900
0.300
0.030
POWER
HP
112.6
3755.0
3379.3
1126.9
112.6
EMISSION FUEL
RATE RATE
LB/HR LB/HR
8.487
0.059
0.065
0.081
8.487
USAGE TIME IN
HT FACTOR MODE
MIN.
575.901
2032.160
1891.B39
1071.003
9T9.903
1.000
1.000
1.000
1.000
1.000
19.00
0.50
2.90
4.90
7.00
TOTAL FOR CYCLEl
LBS POLLUTANT/IK LB FUEL/CYCLEl
LBS POLLUTANT/IK MP-HR/CYCLEI
LBS POLLUTANT/1000K HP AT T.O.I
HC
MASS
LBS.
2.688
0.000
0.003
0.006
0.990
1.687
8.665
12.072
0.110
FUEL
MASS
LBS.
182.24
16.94
78.81
80.11
67.14
L8 HC /
IK LB FUEL
14.747
0.029
0.019
0.079
14.747
ENERGY
MR-KR
19.67
11.29
140.B1
84.49
11.14
LB KC /
HP-HR
0.07514
0.00002
0.00002
0.00007
0.07534
FRACTIONAL
POWER
TAXI-IOLE
TAKEOFF
CLtMBOUT
APPROACH
TAXI-IDLE
0.010
1.000
0.900
0.300
0.030
POWER
HP
112.6
3759.0
3179.5
1126.5
112.6
EMISSION
RATE
LB/MR
2.084
18.149
19.766
7.281
2.084
FUEL
RATE
LB/HR
979.901
2032.160
1841.«14
1071.001
979.903
USAGE
WT FACTOR
.000
.000
.000
.000
.000
TIME IN
MODE
MIN.
19.00
0.50
2.50
4.50
7.00
TOTAL FOR CYCLEl
LBS POLLUTANT/IK LB FUEL/CVCLEl
IBS POLLUTANT/IK HP-HR/CYCLEl
LBS POLLUTANT/1000K HP AT T.O.t
N0«
Mass
LBS.
0.660
0.151
0.824
0.546
0.241
2.424
5.697
7.917
40.278
FUEL
MASS
IBS.
112.24
16.44
71.81
10.11
67.14
425.47
LB NOX/
IK LB FUEL
1.620
8.410
10.448
6.100
1.620
ENERGY
HP-HR
15.67
11.29
140.81
84.4*
11.14
109.41
L8 NOX/
HP-HR
0.01850
0.00481
0.00189
0.00647
0.01890
IV-3
-------
DATE! ' 6/18/71
TEST ORGANIZATION: S W R I KELLY
ENGINE SUPPLIER: USAF. KELLY AFB
ENGINE DATA
CAL ID NUMBED: 3 ENGINE TYPE AND MODEL: T56-ATB
RATED HORSEPOWER: 37;;.
ENGINE TOTAL TIME: 4865. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
THE SINCF:
Nl COMPRESSOR UVERHAUL: 0. HRS
NZ COMPRESSOR OVERHAUL: -o. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: -o. HRS
FUEL: jp-4 FUEL H/C HAT in: 1.995
OPERATIONAL DATA ««««««««»««»««»
INLET AIR TEMPERATURE, DEGREES F: START 90.00 FINISH 68.00
ATMOSPHERIC PRESSURE: START 29.27 FINISH 29.27
INLET Al° HUMIDITY, L8S H20/LB AIR: 0.0186
RELATIVE HUMIDITY: 12.00 PERCENT
SAMPLE LINE: TEMPERATURE, OEGRFES C: 150,00, FLOW RATE, LITERS/MINI
SAMPLE LINE HANSPOUT TIME, S F.C: 0.50
NUMBER OF TESTS: 8
COMMENTS:
F/A CALCULATION BASFD ON F.XHAUST COMPOSITION FOR LAST RUN
SERIAL NUMBER:
ELAPSED
TIME
0.0
4.00
9.00
15.00
17.00
I8.oo
20.00
22.30
TFST
MOPE
I/ 0
;>/ i
>/ 2
4/ i
5/ 4
4/ 5
ft/ 4
POWER
THKUST, LBS
OR
SHP
2191.00
3P70.00
1421.00
821.00
3H08.00
P 2 1.00
299.00
1 19.00
PERCENT
RATED
T.O.
58
81
91
21
101
21
7
1
EN(
SI
1
Nl
13780.00
13800.00
13800.00
132BO.OC
14200.00
11280.00
13440.00
9970.00
MEASURED
FUEL
RPM FLOW
N2 LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
1430.00
1755.00
1835.00
875.00
2055.00
PRO.00
705.00
565.00
GAS GEN
AIR FLOW
LB/SEC
30.10
30.10
30.10
28.00
31.80
2ft.00
28.50
15.40
CALC
F/A
0.013200
0.016200
0.017400
0.008700
0.018000
0.008700
0.006900
0.010200
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.oo
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
OEGRFtS F
1506.00
I 7 10.00
1780.00
1178.00
1910.00
1182.00
1062.00
1IA6.00
POWER
PERCENT
RATED
T.O.
58
81
91
21
101
21
7
1
FXHAUST
GAS
TEMP
-0.00
-0.10
-0.00
-o.or>
-0.00
-0.00
-0.00
-0.00
F XHHUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
(HFTI
PPMV
40.00
39.00
59.00
45.00
11.00
45.00
45.00
287.00
cn
_>
IKFTI
PERCENT V
2.42
.07
.25
.bO
.48
.62
.30
2.05
THC
IUEII
PPMV
0.0
1.00
I. 00
2.00
n.O
2.00
2.00
221.00
Nil
IHFTI
PPMV
-0.00
-0.00
-O.OP
-0.00
-0.00
-0.00
-O.OP
-o.or
NO
2
(HFTI
DPMV
-0.00
-0.00
-0.00
-O.OD
-0.00
-0.00
-0.00
-0.00
NO
X
I MET I
PPMV
73.00
103.00
33.00
31.00
1 I 1.00
33.00
24.00
26.00
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
BATED
T.O.
58
81
91
21
101
21
7
3
MASS EMI
CO
LB/IK
LB FUEI
3. in
2.53
2.39
5 .60
2.18
5.53
6.89
27.21
MASS FMI
HC
LB/IK
LB FUEL
0.0
0.04
0.04
0.14
0.0
0. 14
O.ld
12.41
MASS EMI
M02
LB/IK
LB FUEL
-o.oo
-o.oo
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
C02
LB/IK
LI FUFL
1113.69
3134.79
1115.01
3129.68
1135.45
3129.79
3127.57
3061.95
MASS FMI
NO
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
NI1X
LB/IK
LB FUFL
9.88
10.99
3.11
6.75
10.46
6.66
6.04
4.06
MASS EMI
C1
LB/HB
4.71
4.45
4.51
4.90
4.4°
4.87
4.86
15.41
MASS EMI
HC
LB/HR
0.0
0.07
0.07
0. 1 '?
0.0
0.12
0.12
7.01
MASS tMI
Nfl2
IB/HR
-0.00
-0.00
-O.OP
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
C02
LB/HR
4481.18
5501.55
5909.50
2738.47
6443.34
2754.22
2204.94
1730.00
MASS EMI
NO
LR/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EM
NQX
LB/HR
14.11
19.30
6.27
5.90
21.49
5.87
4.26
2.29
POUER
PEKCFNT
RATED
T.O.
58
81
91
21
101
21
7
3
cn
LB/IK HP-Hfl
2.150
I .449
1.319
5.971
1. I 76
5.911
16.246
129.516
LB/IK HP-Hk
2043.400
1792.035
1727.418
3335.530
lf.92.055
3354.709
7374.167
1451 7. B4U
THC
LB/IK HP-HH
0.0
0.021
0.019
0. 152
0.0
0. 151
0.414
58.917
LD/1K HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-o.ooo
-0.000
Lfl/lK IIP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
NO
X
LB/IK HP-HR
6.444
6.28S
1.834
J.192
5.642
7.144
14.212
19.275
IV-4
-------
CAl ID NUMBER: 3 ENGINE TYPE AND MODEL! T56-A7B
TEST ORGANIZATION! S H R I KELLY
SERIAL NUNBF.KI AE-104B86
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
NODE
r<«l-IOLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.030
1.000
0.400
0.300
0.030
FRACTIONAL
POKER
0.030
1.000
0.400
0.300
0.030
FRACTIONAL
POKER
0.030
1.000
0.900
0.300
0.030
POKES
HP
112.6
3755.0
3374.)
1126.5
112.6
POKER
HP
112.6
3755.0
3379.5
1126.5
112.6
POKER
HP
112.6
3755.0
3379.5
1126.5
112.6
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR MODE
LB/HR L8/HR MIN.
15.642 555.406 .000 14.00
4.254 2038.633 .000 0.50
4.416 1891.581 .000 2.50
5.229 1053.412 .000 4.50
15.642 555.406 .000 7.00
TOTAL FOR CTCLE:
LBS POLLUTANT/IK LB FUEL/CYCLEl
LBS POLLUTANT/IK HP-HR/CYCLEl
LBS POLLUTANT/IOOOK HP AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR MODE
LB/HR LB/HR MIN.
7.971 555.406 .000 14.00
0.065 2038.633 .000 0.50
0.087 1891.581 .000 2.50
0.135 1053.412 .000 4.50
7.971 555.406 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLEl
LBS POLLUTANT/IOOOK HP AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR MODE
LB/HR LB/HR MIN.
2.239 555.406 .000 19.00
21.551 2038.633 .000 0.50
20.763 1841.581 .000 2.50
7.660 1053.412 .000 4.50
2.234 555.406 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK MP-MR/CYCLE:
LBS POLLUTANT/IOOOK HP AT T.O.:
CO
MASS
LBS.
4.453
0.035
0.184
0.342
1.825
7.390
17.787
24.197
0.944
HC
MASS
LBS.
2.524
0.001
0.004
0.010
0.930
3.464
8.348
11.357
0.144
KOI
MASS
LBS.
0.709
0.180
0.865
0.574
0.261
2.589
6.232
B.478
47.827
FUEL
MASS
LBS.
175. BB
16.99
78.82
79.01
64.80
415.44
FUEL
MASS
LBS.
175.88
16.44
78.82
79.01
64.80
415.44
FUEL
MASS
LBS.
175. B8
16.49
78.82
74.01
64.80
413.44
LB CO /
IK LB FUEL
28.164
2.087
2.335
4.964
28.164
LB HC /
IK LB FUEL
14.353
0.032
0.046
O.I2B
14.353
LB NOX/
IK LB FUEL
4.031
10.571
10.976
7.272
4.031
ENERGY
HP-MR
35.67
31.29
140.81
84.49
13.14
305.41
ENERGY
HP-HR
35.67
31.29
140.81
84.49
13.14
305.41
ENERGY
HP-HR
35.67
31.29
140.81
84.44
13.14
305.41
LB CO /
HP-HR
0.13886
0.00113
0.00131
0.00464
0.13886
LB HC /
HP-HR
0.07076
0.00002
0.00003
0.00012
0.07076
LB NOX/
HP-HR
0.01987
0.00574
0.00614
0.00680
0.01487
IV-5
-------
0»TEl 6/ia/Tl
TEST ORGANIIATION: S W R 1 KELLY
ENGINE SUPPLIER! USAF, KELLY AFB
ENGINE n»T« »*»»**»
C«L in NUMBER: * ENGINE TYPE AND HOOElI TS6-ATB
RATED HORSEPOWER! 3749.
ENGINE TOTAL THE: 779). HRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TINE SINCE:
Nl COMPRESSOR OVERHAUL! 0. HRS
N2 COMPRESSOR OVERHAUL: -o. HRS
COMBUSTOR CAN REPLACEMENT! 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL! 0. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL! JP-4 FUEL H/C RATIO: I.195
OPERATIONAL DATA «««««««««««««««««««
INLET AIR TEMPERATURE, DEGREES F: START 82.00 FINISH SI.00
ATMOSPHERIC PRESSURE: START 28.90 FINISH 28.90
INLET AIR HUMIDITY, IBS H20/LB AIRI 0.0107
RELATIVE HUMIDITY: -o.oo PERCENT
SAMPLE LINE: TEMPERATURE, OFGRFES C: 150.00, FLOW RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SEC: 0.50
NUMBER OF TESTS: S
COMMENTS:
F/A CALCULATION BASED ON EXHAUST COMPOSITION FOR LAST RUN
SERIAL NUMBER!
AE-10IB54
ELAPSED
TIMF
0.0
10.50
16.55
21.20
26.05
26.15
27.50
10.50
TEST
MODE
I/ 0
2/ I
3/ 2
4/ 1
5/ 4
4/ 5
I/ 4
7/ B
THRUST
OR
SHP
2214.
1092.
3399.
823.
1618.
821.
?S6.
87.
POWER
,LBS
00
00
00
00
00
00
00
on
PERCENT
RATED
T.O.
58
87
90
21
96
21
6
2
Nl
11800.
13800.
11800.
13300.
14240.
11270.
13450.
9940.
ENGINE
SPEEO
RPM
00
00
00
00
00
00
00
00
N2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MEASURED
FUEL
FLOW
LB/HR
1440.00
1770.00
1910.00
890.00
2000.00
895.00
705.00
555.00
GAS GEN
AIR FLOW
LB/SFC
.10.80
10.80
10.80
28.70
32.60
28.70
28. 10
14.90
CALC
F/A
0.011000
0.016000
0.017200
0.008600
0.017000
0.008700
0.007000
0.010300
COMPRESSOR
OISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
ENGINE
PRESSURE
RATIO
EPR
-0.00
-o.oo
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
TURBINE
INLET
TFMP
DEGREES F
1510.00
1710.00
1780.00
1180.00
1890.00
1180.00
1052.00
1155.00
POWER
PERCENT
HAIED
T.n.
58
82
90
21
96
21
6
EXHAUST
GAS
TFMP
DECREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.no
F XHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.00
-0.00
-n.oo
CO
I MET I
PPMV
12.00
28.00
25.00
12.00
26.00
31.00
34.00
300.00
CO
2
I WET I
PERCENT V
2.28
2.98
1.21
1.67
1.60
1.67
1.33
2.08
THC
I WET I
PPMV
0.0
o.o
0.0
0.0
o.n
o.n
o.o
348.00
NO
IWETI
PPMV
61.00
89.00
9B.OO
0.0
95.00
25.00
in.oo
10.00
ALDEHYDES SMOKE PARTICULATES
IWETI
PPMV
5.00
1.00
3.00
0.0
0.0
5.00
4.00
0.0
I WET I
PPMV
66.00
90.00
101.00
31.00
0.0
10.00
22.00
0.0
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-n.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
PUWER
PERCENT
RATED
T.O.
58
H2
90
21
96
21
6
MASS FMI
cn
LIVIK
LB FUEL
2.80
1.88
1.55
3.02
1.44
3.14
5.09
77.94
MASS EMI
HC
LR/1K
LR FUEL
0.0
n.o
n.o
0.0
o.n
0.0
o.n
10.56
MASS EMI
NO 2
LB/IK
LB FUFL
1.72
0.11
0.11
0.0
1.0
0.9H
0.9H
0.0
MASS HMI
CC12
LB/1K
LB FUFL
1134.47
3115. "2
3136.43
3112. B7
3116.61
11 12.I.B
3110.117
3044.04
MASS fcMI
NO
LB/IK
LB FUEL
8. 77
9. 79
10.01
0.0
R.65
4.00
4.41
1.53
MASS EMI
NOX
LB/IK
LB FUEL
9.49
9.90
10.12
6.08
0.0
5.88
5.41
0.0
MASS FM
co
LB/HR
4.03
1.12
2.97
3.40
2.88
*.53
3.59
15.51
MASS FMI
HC
L8/HP
0.0
0.0
0.0
0.0
0.0
0.0
0.0
10.1C
MASS EMI
N02
LB/HR
1.01
0.19
0.59
n.o
0.0
0.81
0.69
0.0
MASS EMI
C02
LB/HR
4511.64
5550.58
5990.58
2788.25
6271.21
2801. 75
2207.26
1689.44
MASS EMI
NO
LB/HR
12.62
17.11
19.12
0.0
17.11
4.19
1.12
0.85
MASS EMI
NOX
LR/MR
11.66
17.52
19.70
5.41
0.0
5.27
1.82
0.0
PQWFR
PERCENT
OSIEO
T.O.
5B
12
90
21
96
21
6
2
cn
LO/1K HP-HR
I.H2I
1.D74
0. H74
4.117
0. 797
4 . 79*i
14.178
178.756
LB/IK HP-HR
2038.680
1795.143
U62.451
1387.915
l7(3.flB9
3415.043
8422.117
19418.879
THC
LB/IK HP-HR
0.0
n.o
o.n
n.o
o.o
o.o
o.n
118.426
Nil
LB/IK HP-HR
5.702
5.605
5.625
0.0
4.783
5.344
12.199
9.76n
LB/IK HP-HR
0.467
0.061
0.177
0.0
0.0
1.069
2.711
0.0
LB/IK HP-HR
6.169
5.668
5.797
6.574
0.0
6.411
14.910
0.0
IV-6
-------
CAL 10 NUMBER: 4 ENGINE TYPE AND MODEL: T56-A7B
TEST ORGANIZATION: s w R I KELLY
SERIAL NUMBER:
AE-101854
MOOF FRACTIONAL
POWER
TAXI-IDLE 0.030
TAKEOFF 1.000
CLIMBOUT 0.900
APPROACH 0.300
TAXI-IDLE 0.030
MODE FRACTIONAL
POKER
TAXI-IDLE 0.030
TAKEOFF 1.000
CLIMBOUT 0.900
APPROACH 0.300
TAXI-IOLE 0.030
MODE FRACTIONAL
POWER
TAXI-IDLE 0.030
TAKEOFF I. 000
CLIMBOUT 0.900
APPROACH 0.300
TAXI-IOLE 0.010
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
EMISSION FUEL USAGE TIME IN
RATE RATE XT FACTOR MODE
LB/HR LB/HR MIN.
12.931 576.902 .000 19.00
2.701 2083.368 .000 0.50
3.141 1924.923 .000 2. SO
3.703 1031.957 .000 4.50
12.931 576.902 .000 T.OO
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE1
LBS POLLUTANT/1000K HP AT T.O.l
EMISSION FUEL USAGE TIKE IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
7.534 576.902 .000 19.00
0.007 2083.368 .000 0.50
0.0 1924.923 .000 2.50
0.0 1031.957 .000 4.50
7.534 576.902 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK HP-HR/CYCLE:
LBS POLLUTANT/ 1000K HP AT T.O. :
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
1.474 576.902 .000 19.00
21.849 2083.368 .000 0.50
19.881 1924.923 .000 2.50
6.952 1031.957 .000 4.50
1.474 576.902 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
CO
MASS
LBS.
4.095
0.023
0.131
0.276
1.509
6.034
14.200
19.758
0.599
HC
MASS
LBS.
2.386
0.000
0.0
0.0
0.879
3.265
7.683
10.690
0.016
N0>
MASS
LBS.
0.467
0.182
0.828
0.521
0.172
2.171
5.108
7.107
48.488
FUEL
MASS
LBS.
182.69
17.36
80.21
77.40
67.31
424.95
FUEL
MASS
LBS.
182.69
17.36
80.21
77.40
67.31
424.95
FUEL
MASS
LBS.
182.69
17.36
80.21
77.40
67.31
424.95
LB CO /
IK LB FUEL
22.414
1.296
1.632
3.588
22.414
LB HC /
IK LB FUEL
13.060
0.003
0.0
0.0
13.060
LB NOX/
IK LB FUEL
2.555
10.487
10.328
6.737
2.555
ENERGY
HP-HR
35.67
31.29
140.81
84.49
13.14
305.41
ENERGY
HP-HR
39.67
31.29
140.81
84.49
13.14
305.41
ENERGY
HP-HR
35.67
31.29
140.81
84.49
13.14
305.41
LB CO /
HP-HR
0.11479
0.00072
0.00093
0.00329
0.11479
LB HC /
HP-HR
0.06688
0.00000
0.0
0.0
0.06688
LB NOX/
HP-HR
0.01308
0.00582
0.00588
0.00617
0.01308
IV-7
-------
DtTEt 6/21/n
TEST ORGANIZATION: S W » I KELLY
ENGINE SUPPLIER: US»F, KELLV AFB
ENGINE DATA «»«««««»«««««»
CAL in NUMBER: 5 ENGINE TYPE AND MODEL: T56-A7B
RATED HORSEPOWER: 3755.
ENGINE TOTAL TIME: 7751. HRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
SERIAL NUMBER:
AE-101776
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: -o. HRS
FUEL H/C RATIO:
1.915
FUEL: jp-4
OPERATIONAL DATA »««««.«.««.««««««»«««
INLET AIR TEMPERATURE, DEGREES F: START 81.00 FINISH 83.00
ATMOSPHERIC PRESSURE: START 29.21 FINISH 29.21
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0184
RELATIVE HUMIDITY: 67.oo PERCENT
SAMPLE LINE: TE'PFRATURF, DEGREES C: 150.00, FLOW RATE, LITERS/KIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.50
NUMBER OF TESTS: 8
COMMFNTS:
F/A CALCULATION BASED ON F.XHAUST COMPOSITION FOR LAST RUN
42.50
ELAPSFO
TIMF
0.0
5.00
10.10
15.10
18.10
19.10
21.00
23.00
TFST
MODE
I/ 0
2/ 1
I/ 2
4/ 1
5/ <<
4/ 5
H/ 4
7/ 0
THRUST
OR
SHP
2? 59.
§202.
1511.
838.
idle.
818.
2)2.
9*.
POWFR
,LBS
00
00
00
00
00
00
no
00
PERCENT
RATED
T.O.
60
85
94
22
96
22
6
2
Nl
13820.
13800.
13800.
13200.
14200.
13110.
13320.
9840.
ENGINF
SPEED
RPH
00
00
00
00
00
00
00
00
N2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MEASURED
FUEL
FLOW
LB/HR
1450.00
1795.00
1925.00
900.00
2010.00
885.00
685.00
555.00
GAS GEN
AIR FLOU
L8/SfC
10.60
10.60
30.60
28.00
32.40
27.60
28.SO
13.40
CALC
F/A
0.013200
0.016300
0.017500
O.OOR900
0.017200
0.008900
0.006700
0.011500
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
1505.00
1705.00
1780.00
1160.00
1850.00
1175.00
1040.00
1175.00
POKER EXHAUST
PERCENT GAS
RATED TFMP
T.O. OEC.REFS F
60
85
94
22
96
?2
-o.no
-o.oo
-0.30
-0.00
-0.00
-0.00
-0.00
-0.00
F XHAUST
GAS
PRCSSURF
PSIA
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
en
(UEII
PPMV
11 .00
26.00
23.00
27.00
21.00
77.00
27.00
123.00
CU
2
IWFT)
PEUCFNt V
2.54
1.17
1.42
1.67
1.64
1.70
1.11
2.12
THC
(NET)
PPMV
42.00
46.00
44.00
17.00
46.00
17.00
46.00
315.00
NO NO
IHET) 2
PPMV (HEM
PPMV
62.00
93.00
102.00
0.0
0.0
0.0
0.0
0.0
5.00
2.00
3.00
0.0
0.0
0.0
o.o
0.0
NO
X
I WET I
PPMV
69.00
95.00
105.00
31.00
105.00
11.00
22.00
26.00
ALDEHYDES SMOKE PART1CULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
POWFR
PEKCFNT
RATFD
T.n.
60
85
94
22
96
2?
MASS FVI
CO
LB/IK
Lfl FUFL
2.41
1.61
1.14
3.72
1.15
3. 16
4.03
77.07
MASS EMI
HC
LB/IK
LB FUEL
1.89
1.66
1.47
2.51
1.44
2.48
3.94
15.12
MASS EMI
N02
LO/IK
LD FUEL
0.64
0.21
0.29
0.0
0.0
0.0
0.0
0.0
MASS fMI
C02
LB/IK
LB FUEL
3129.88
3131.76
3132.74
3126.89
3133.11
3127.10
3121.74
3054.86
MASS FMI MASS FMI
NO NOX
LB/IK LB/IK
LB FUEL LB FUEl
7.99 ,H9
9.60
9.77 I
0.0
0.0
0.0
.81
.05
.07
.45
.96
0.0 5.40
0.0 3.58
MASS EMI
CO
L8/KR
1.51
2.91
2.50
2.90
2.11
2.80
2. 76
15.02
MASS EMI
HC
LB/HR
2.74
2.97
2.81
2.27
2.90
2.20
2.70
8.19
MASS EMI
NO 2
LB/HR
0.91
0.17
0.55
0.0
0.0
0.0
0.0
0.0
MASS FMI
C02
LB/HR
4518.12
5621.50
6010.51
2814.20
6297.44
2767.48
2118.39
1695.45
MASS EMI
NO
LB/HR
11.58
17.24
18.80
0.0
0.0
0.0
0.0
0.0
MASS EMI
NOX
LB/HR
12.89
17.61
19.36
5.46
18.99
5.28
1.70
1.99
POWFR
"ERCENT
PAT ED
T.O.
60
85
94
72
96
22
6
2
CO
LB/IK HP-HP
1.561
0.916
0.711
1.456
0.619
3.31D
11.909
159.121
LB/IK HP-H!<
2008.994
1755.621
1707.877
3358.215
1740.614
3302.487
9217.201
18016.691
THC
LB/IK HP-MR
1.211
0.929
0.801
2.712
O.H02
2.620
11.620
89.266
NO
L8/1K HP-HR
5.126
5.184
5.125
0.0
0.0
0.0
0.0
0.0
LB/IK HP-«R
0.411
0. 116
0.157
0.0
0.0
0.0
0.0
0.0
LB/IK HP-HR
5.705
5.500
5.482
6.517
5.249
6.296
15.919
21.111
IV-8
-------
CAL to NUMBED: 5 ENGINE TYPE AND MODEL: T56-A7B
TEST ORGANIZATION! S W R I KELLY
SERIAL NUMBER: AE-10177&
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TA«I-10LE
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TA>I-IDLE
FRACTIONAL
POKER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POKER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.010
1.000
0.900
0.300
0.030
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR NIN.
15.074 56«.752 .000 19.00
2.0*9 2084.54* .000 0.50
2.498 1897.624 .000 2.50
3.041 1043.322 .000 4.50
15.074 564.752 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/ 1000K HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
6.711 564.752 .000 19.00
2.760 20B4.544 .000 0.50
2.758 1897.624 .000 2.50
2.38) 1043.322 .000 4.50
6.711 564.752 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/ IOOOK HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
L8/MR LB/HR MIN.
2.292 564.752 .000 19.00
20.240 2084.544 .000 0.50
18.988 1897.624 .000 2.50
6.983 1043.322 .000 4.50
2.292 564.752 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK HP-HR/CYCLE:
LBS POLLUTANT/ IOOOK HP AT T.O.:
CO
MASS
LBS.
4.773
0.017
0.104
0.228
1.759
6.881
16.407
22.532
0.455
HC
MASS
LBS.
2.125
0.023
0.115
0.179
0.783
3.225
7.688
10.558
6.126
NOX
MASS
LBS.
0.726
0.169
0.791
0.524
0.267
2.477
5.905
8.110
44.917
FUEL
MASS
LBS.
178.84
17.37
79.07
78.25
65.89
419.41
FUEL
MASS
LBS.
178.84
17.37
79.07
78.25
65.89
419.41
FUEL
MASS
L8S.
178.84
17.37
79.07
78.25
65.89
419.41
LB CO /
IK LB FUEL
26.691
0.983
1.317
2.915
26.691
LB HC /
IK LB FUEL
11.882
1.324
1.454
2.284
11.882
LB NOX/
IK LB FUEL
4.059
9.709
10.006
6.693
4.059
ENERGY
HP-HR
35.67
31.29
140.81
84.49
13.14
305.41
ENERGY
HP-HR
35.67
31.29
140.81
84.49
11.14
305.41
ENERGY
HP-HR
35.67
31.29
140.81
84.49
13.14
305.41
LB CO /
HP-HR
0.13381
0.00055
0.00074
0.00270
0.13381
LB HC /
HP-HR
0.05957
0.00074
0.00082
0.00212
0.05957
LB NOX/
HP-HR
0.02035
0.00539
0.00562
0.00620
0.02035
IV-9
-------
OtTEl ' 6/21/71
TEST ORGANIZATION: S w R I KELLY
ENGINE SUPPLIER: USAF, KELLY AFB
ENGINE DATA «..«.
CAL ID NUMBER: 6 ENGINE TYPE AND MODEL: 156-473
RATF.O HORSEPOWER: 375;.
ENGINE TOTAL TIME: 6027. HKS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
Nl COMPRESSOR OVERHAULl. 0. HRS
N?. COMPRESSOR OVERHAUL: -o. HRS
CHHBUSTOB CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL: JP-4 FUEL H/C RATIO: I.995
OPERATIONAL DATA «««««««.«.«««...«..........«««......
INLET AIR TEMPERATURE, DEGREES F: START 74.00 FINISH 74.00
ATMOSPHERIC PRESSURE: START 11.19 FINISH 2<).i<)
INLFT AIR HUMIDITY, IBS HZ(VI8 AIR: 0.0176
RELATIVE HUMI-IITY: 66.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOM RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.50
NUMBER OF TESTS: 8
COMMENTS:
F/A CALCULATION BASEO ON EXHAUST COMPOSITION FOR LAST RUN
SERIAL NUMBER I
ELAPSED
TIME
0.0
6.30
10.30
17.30
19.00
21.00
72.00
24.00
TEST
MODE
I/ 0
2/ 1
3/ 2
4/ 3
>! 4
4/ 5
B/ 4
II 8
THRUST
OR
SHP
2456.
3355.
3662.
fl34.
372B.
B40.
241.
111.
POWER
,LBS
00
00
00
00
00
00
00
00
PERCENT
RATED
T.O.
65
81
97
22
99
22
6
2
Nl
13800.
13800.
1.1800.
13100.
14220.
13200.
I342C.
9980.
ENGINE
SPEED
RPM
oc
00
00
00
00
no
00
00
N2
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
00
00
00
00
00
00
no
00
MEASURED
FUtL
FLOW
Lfl/HR
1510.00
1665.00
1980.00
895.00
2045.00
870.00
720.00
550.00
GAS GEN
AIR FLOW
Lfl/SEC
31.20
31.20
31.20
28.10
33.00
2B.60
29.50
15.90
CALC
F/A
0.013400
0.016600
0.017600
0.008BPO
0.017200
O.OOB400
0.006800
0.009600
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
1850.00
1712.00
1775.00
1146.00
1860.00
1132.00
1026.00
1084.00
POWFR
PERCENT
RATED
T.O.
65
B9
97
22
99
27
EXHAUST
GAS
TFMP
DEGRFFS F
-0.00
-0.00
-0.00
-o.on
-0.00
-0.00
-0.00
-P.00
FXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
IWETI
PPMV
40.00
26.00
21.00
25.00
17.00
24.00
21.00
217.00
CO
2
(MET)
PFP.CFNT V
2.52
3.10
3.34
1.60
3.74
1.5B
1.26
1.94
THC
(WFTI
PPMV
0.0
0.0
0.0
0.0
0.0
o.n
0.0
2SO.OO
NO
IWETI
PPHV
63.00
90.00
97.00
24.00
0.0
0.0
17.00
7.00
NO
2
IWET)
PPMV
9. no
8.00
I. 00
5.00
0.0
0.0
6.00
15.00
ALDEHYDES SMOKE PARTICULATES
IWFT)
PPMV
72.00
98.00
104.00
29.00
96.00
79.00
23.00
22.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
POWFR
PERCENT
RATED
r.o.
65
R9
97
22
99
27
6
2
MASS FMI
cn
Lfl/IK
LB FIIFI
3.17
1.67
1 .76
3.12
0.91
3.03
3.32
21.82
MASS FMI
HC
IB/IK
Lfl F-UFL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
14.40
MASS EMI
N02
I.B/1K
LB FUFL
1.17
O.B5
0.69
1.02
0.0
0.0
1.56
2.48
MASS EMI
C02
LB/1K
LB FUEL
3133.90
3136.24
3136.90
3133.98
3137.45
3134.11
3133.65
3065.09
MASS EMI
NO
LR/1K
LP FUEL
B.19
9.52
9.52
4.91
O.n
0.0
4.42
1. 16
MASS EMI
NDX
LB/IK
LB FUEL
9.36
10.36
10.21
5.94
6.42
6.01
5.98
3.63
MASS EMI
CO
LB/HR
4.78
3.12
2.49
2.79
1.86
2.64
2.39
12.00
MASS EM
HC
LB/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
7.92
MASS EMI
NO 2
LB/HR
1.77
1.58
1.36
0.97
0.0
0.0
1.12
1.36
MASS EMI
C02
LB/HR
4732.18
5849.09
6211.06
2804.91
6416.07
2726.68
2256.23
16B5.BO
MASS EMI
NO
LB/HR
12.17
17.75
18.86
4.40
0.0
0.0
3.18
0.64
MASS EMI
Nnx
LB/HR
14.13
19.33
20.22
5.31
17.22
5.23
4.31
2.00
POVIER
PERCENT
RATED
T.n.
65
89
97
22
94
27
6
2
CU
Lfi/lK HP-HP
1.946
0.931
0.679
3.145
0.49B
3.13H
9.931
108.119
LB/IK HP-HR
1926.7H4
1741.395
1696.084
3361.199
1721.049
3246.041
9361.945
15187.37S
THC
LB/IK HP-HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
71.319
NO
IB/IK HP-HR
5.036
5.291
5.149
5.774
0.0
0.0
13.205
5.729
Lfl/IK HP-HR
0.719
0.470
0.372
1.099
0.0
0.0
4.660
12.276
NO
X
LB/IK hP-HR
5.755
5.762
5.521
6.373
4.618
6.22B
17.865
18.005
IV-10
-------
C»L ID NUNBERl 6 ENGINE TYPE >NO MODEL: T56-ATB
TEST ORGANIZATION: s w R I KELLY
SERIAL NUMBER! AE-104313
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLIMROUT
APPROACH
TAXI-IDLE
MODE
TAXI-IOLF
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POHER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
POWER
HP
112.6
3755.0
3379.5
1126. 5
112.6
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR NODE
LB/HR LB/HR MIN.
14.231 536.639 .000 19.00
1.863 2079.368 .000 0.50
3.296 1695.471 .000 2.50
3.389 1076.472 .000 4.50
14.231 536.839 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
L8S POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE UT FACTOR MODE
LB/HR LB/HR MIN.
6.377 536.839 .000 19.00
0.064 2079.368 .000 0.50
0.044 1895.471 .000 2.50
0.0 1076.472 .000 4.50
6.377 936.839 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLEl
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
2.108 536.839 .000 19.00
22.T90 2079.368 .000 0.50
20.198 1895.471 .000 2.50
7.037 1076.472 .000 4.50
2.106 536.839 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
CO
MASS
LBS.
4.506
0.016
0.137
0.254
1.660
6.574
16.046
21.525
0.414
HC
MASS
LBS.
2.019
0.001
0.002
0.0
0.744
2.766
6.751
9.056
0.143
NOD
MASS
LBS.
0.667
0.190
0.842
0.526
0.246
2.473
6.036
8.096
50.577
FUEL
MASS
LBS.
170.00
17.33
78.98
80.74
62.63
409.67
FUEL
MASS
LBS.
170.00
17.33
78.98
80.74
62.63
409.67
FUEL
MASS
LBS.
170.00
17.33
78.96
80.74
62.63
409.67
LB CO /
IK LB FUEL
26.909
0.696
1.739
3.146
26.509
LB HC /
IK LB FUEL
11.878
0.031
0.023
0.0
11.676
LB NOX/
IK LB FUEL
3.926
10.960
10.656
6.537
3.926
ENERGY
HP-HR
35.67
31.29
140.81
84.49
13.14
305.41
ENERGY
HP-HR
35.67
31.29
140.81
64.49
13.14
305.41
ENERGY
HP-HR
35.67
31.29
140.81
84.49
13.14
305.41
LB CO /
HP-HR
0.12633
0.00050
0.00098
0.00301
0.12633
LB HC /
HP-HR
0.05661
0.00002
0.00001
0.0
0.05661
L8 NOX/
MP-HR
0.01871
0. 00607
0.00598
0.00625
0.01871
IV-11
-------
DATE: 6/22/71
TFST ORGANIZATION: S w R I KELLY
ENCINE SUPPLIER: USAF, KELLY AFB
ENGINE 0114 .>.>>>.>.«>..»*>.««««.«.«...........«........
C«L 10 NUMBER: 7 ENGINE TYPE AND MOOELi T56-A7B
RATED HORSEPOWER: 3755.
ENGINE TOTAL THE:
TIME SINCE HOT SECTION OVERHAUL:
TIME SINCE:
SERIAL NUMBER:
«E-ioiea<>
8488. MRS
0. HRS
NI COMPRESSOR OVERHAUL: o. MRS
NZ COMPRESSOR OVERHAUL: -o. HRS
crmeusTnR CAN REPLACEMENT: o. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINF OVERHAUL: o. MRS
HZ TURBINE OVERHAUL: -o. HRS
FUEL: JP-» FUEL H/C RATIO! 1.995
OPERATIONAL DATA «««««««
INLET AIR TEMPERATURE, DEGREES F: START 83.00 FINISH
ATMOSPHERIC PRESSURE: START 29.01 FINISH
INLFI AIR HUMIDITY, LBS H20/LB AIR: 0.0199
RELATIVE HU'IDHY: 7?.00 PERCENT
SAMPLF LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.50
NUMBER OF TESTS: 6
COMMENTS:
F/A CALCULATION BASED ON EXHAUST COMPOSITION FOR 2ND LAST RUN
83.00
29.01
ELAPSED
TIHF
0.0
7.35
13.35
19.35
21.37
22.15
73.15
21.50
TFST
MODE
If 0
Zl \
»/ 2
4/ 3
5/ 4
4/ 5
7/ 4
8/ 7
1 HP US T
OR
SHP
?28i.
1180.
34B7.
B40.
3510.
820.
lie.
328.
POWER
,LBS
00
00
00
00
00
on
00
00
PERCENT
RATED
T.O.
60
B4
92
2!
93
21
3
8
NI
13800.
13800.
13800.
13240.
14260.
13250.
9910.
13330.
ENGINE
SPEED
RPM
00
00
00
00
00
00
00
00
N2
-0.00
-tl.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MF.ASUOEO
FUEL
FLOW
IB/HR
I4BO.OO
1825.00
1960.00
890.00
1975.00
895.00
575.00
745.00
GAS GEN
AIR FLOW
LB/SEC
30.60
30.60
30.60
28.20
32.40
2B.20
14.60
78.60
CALC
F/A
0.013400
0.016&00
0.017800
0.COB800
0.016900
o.coaeoo
0.010900
0.007200
COMPRESSOR
DISCHARGE
TEMP
DCGRFtS F
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
ENGINF
PRFSSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
1510.00
1710.00
1780.00
1164.00
1858.00
1164.00
1130.00
1055.00
POWER
PERCENT
RATED
T ,n.
60
84
92
22
93
7.1
3
FXHAUST
GAS
TEMP
-0.00
-0.10
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
FXHAUST
GAS
PRFSSUHF
PSI4
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-o.on
co
1WFD
PPMV
27.00
26.00
24.00
29.00
25.10
29.00
299.00
12.00
CO
7
IWFII
PFBCENT V
2.53
3.16
3.47
1.71
3.76
1.71
2.15
1.40
THC
IWET)
PPNV
43.00
41.00
4.10
41.00
42.00
42.00
250.00
45.00
NO
IWETI
PPMV
60.00
83.00
93. OC
0.0
0.0
0.0
9.00
0.0
NO
2
IWETI
PPMV
7.00
7.00
6.00
0.0
0.0
0.0
16.00
0.0
ALDEHYDES SMUKE PARTICULATFS
(WFTI
PPMV
(7.00
90.00
99.00
32.00
100.00
31.00
25.00
75.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWFR
PERCENT
RATED
T.n.
60
H4
92
7?
U3
71
3
8
MASS EMI
CO
LB/1K
L« FUEL
7. 13
1 .64
1.40
3.37
1 .33
3.37
27.09
4.54
MASS E.HI
HC
1 B/IK
LP FUEL
1 .94
1 .48
0.14
2.73
1.28
7. HO
12.97
3.66
MASS EMI
N02
L')/IK
LB FUEL
0.91
0.73
1.58
0.0
0.0
0.0
2.38
0.0
MASS EMI
C(12
LI/IK
LB FUEL
3130.21
3132.23
3136.30
3126.08
3133.2')
3125.89
3060.72
3121.71
MASS EMI
Nil
LB/IK
LB rutL
7.76
8.60
8.9?
0.0
0.0
0.0
1.34
0.0
MASS EMI
not
LR/1K
LB FUEL
8.67
9.33
9.49
6.12
B.71
5.92
3.72
5.83
MASS EMI
CO
LR/HR
3.15
2.99
2.75
3.00
2.62
3.02
15.58
3.38
MASS EM
HC
Lfl/HR
2. 87
2.71
0.27
2.43
2.57
2.50
7.46
2.77
MASS EMI
N02
LH/HR
1.34
1.32
1.13
0.0
0.0
0.0
1.37
0.0
MASS CMI
C07
LB/HR
4632.71
5716.32
6147.14
2782.21
6188.24
2797.68
1759.91
2325.67
MASS EMI
NO
LB/HR
11.49
15.70
17.47
0.0
0.0
0.0
0.77
0.0
MASS EM|
NO I
LB/HR
12.83
17.02
18.60
5.44
17.21
5.30
2.14
4.34
POWER
PERCENT
RATED
T.n.
60
84
92
22
93
21
3
CD
LB/IK HP-HP
I . 179
0.141
0. T87
3.575
0.746
3.683
I 32.009
10.315
LBMK HP-HK
2111.000
1791.585
1762.?73
3312.153
1763.032
341I.ROO
14914.516
(090.457
THC
I H/IK HP-HR
1.258
0.850
0.077
2.895
0.718
3.055
63.215
8.307
NO
IB/IK HP-HR
5.035
4.936
5.011
C.O
0.0
0.0
6.527
0.0
LB/IK HP-HR
0.5B7
0.416
0.323
0.0
0.0
0.0
11.603
0.0
NO
X
LB/IK HP-HR
5.623
5.352
5.335
6.480
4.907
6.466
16.130
13.236
IV-12
-------
CAL 10 NUMBER: 7 ENGINE TYPE »ND MODEL: t56-»7B
TEST ORGANIZATION: s K R i KELLY
SERIAL NUMBER! AE-101889
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TIKI-IDLE
FRACTIONAL
POKER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POKER
0.030
1.000
0.900
0.300
0.030
POKER
HP
112.6
3755.0
3379.5
1126.5
112.6
POKER
HP
112.6
3755.0
3379.5
1126.5
112.6
POKER
HP
112.6
3755.0
3379.5
1126.5
112.6
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR MODE
LB/HR LB/HR NIN.
14.701 427.346 .000 19.00
2.436 2070.004 .000 0.50
2.752 1920.723 .000 2.50
3.251 1063.044 .000 4.50
14.701 427.346 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR MODE
LB/HR LB/HR MIN.
6.051 427.346 .000 19.00
1.637 2070.004 .000 0.50
2.091 1920.723 .000 2.50
2.694 1063.044 .000 4.50
6.051 427.346 .000 7.00
TOTAL FOR CVCLEl
LBS POLLUTANT/IK LB FUEL/CYCLEl
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR NODE
LB/HR LB/HR MIN.
1.519 427.346 .000 19.00
19.136 2070.004 .000 0.50
17.872 1920.723 .000 2.50
7.004 1063.044 .000 4.50
1.519 427.346 .000 7.00
TOTAL FOR CYCLE1
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
CO
MASS
LBS.
4.655
0.020
0.115
0.244
1.715
6.749
18.634
22.099
0.541
HC
MASS
LBS.
1.916
0.014
0.087
0.202
0.706
2.92S
a. 076
9.577
3.634
MOX
MASS
LBS.
0.481
0.159
0.745
0.525
0.177
2.088
5.764
6.836
42.471
FUEL
MASS
LBS.
135.33
17.25
80.03
79.73
49.86
362.19
FUEL
MASS
LBS.
135.33
17.25
80.03
79.73
49.86
362.19
FUEL
MASS
LBS.
135.33
17.25
80.03
79.73
49.86
362.19
LB CO /
IK LB FUEL
34.400
1.177
1.433
3. 058
34.400
LB HC /
IK LB FUEL
14.160
0.791
1.089
2.535
14.160
LB NOX/
IK LB FUEL
3.554
9.245
9.305
6.589
3.554
ENERGY
HP-HR
35.67
31.29
140.81
84.49
13.14
305.41
ENERGY
HP-HR
35.67
31.29
140.81
64.49
13.14
305.41
ENERGY
HP-HR
35.67
31.29
140.81
84.49
13.14
305.41
LB CO /
HP-HR
0.13050
0.00065
0.00081
0.00289
0.13050
LB HC /
HP-HR
0.05372
0.00044
0.00062
0.00239
0.05372
LB NOX/
HP-HR
0.01348
0.00510
0.00529
0.00622
0.01348
IV-13
-------
DATE: 6/22/71
TEST ORGANIZATION:
ENGINE SUPPLIER:
ENGINE DATS ...«..«
CAL in NUMBER:
s * K I KELLY
USAF, KELLY AFB
ENGINE TYPE »ND MODEL: T56-A7B
RATED HORSEPOWER: 3755.
TOM. MRS
SERIAL NUKBFR:
ENGINE TOTAL TIME:
TIME SINCE HOT SECTION OVERHAUL:
TIMF SINCE:
Nl COMPRESSOR OVERHAUL:
N2 COMPRESSOR OVERHAUL:
COMBUSTOP. CAN REPLACEMENT:
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL:
NI TURBINE OVERHAUL:
N2 TURBINE OVERHAUL:
FUEL H/C RATIO:
0. HRS
0. HRS
-0. HRS
0. HRS
0. HRS
0. HRS
-0. HRS
90.00
29.OB
fUEL: JP-4
OPFRATIONAL DATA ««««
INLET AIR TEMPERATURE, DEGREES F: START 90.00 FINISH
ATMOSPHERIC PRESSURE: START 29.OB FINISH
INLET AIR HUMIDITY, LBS H20/L? AIR: 0.016",
RELATIVE MUMI.'UTY: 49.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 150.00. FLOW RATF, LITERS/MIN:
SAMPLF LINE TRANSPORT TIME, SEC: 0.50
NUMBER OF TESTS: B
COMMENTS:
F/A CALCULATION HASFfl ON EXHAUST FOR LAST RUN
ELAPSED
TIMF
0.0
7.00
u.no
15.00
17.52
19.30
21.00
23. on
TTST
MODE
I/ n
7/ I
3/ ?
'/ 3
5/ 4
4/ 5
8/ 4
7/ 1
POWER
THRUST. LBS
OR
SHP
2105.nO
3C04.00
3155.00
040.00
3533.00
676.00
404.00
142.00
PERCENT
RATED
T.O.
56
79
R9
22
94
11
10
3
ENGINE
SPEEO
RPM
Nl
13800. 00
mno.no
13800.00
13240.00
14000.00
13300.00
13400.00
9930.00
N?
-0.00
-0.00
-n.oo
-0.00
-0.00
-0.00
-0.00
-n.oo
MEASURED
FUEL
FLOW
LB/HR
1410.00
1755.00
leno.oo
905.00
1910.00
845.00
765.00
585.00
GAS GEN
AIR FLOW
Lfl/SEC
30.10
30.10
30. 10
27.80
30.90
78.00
28.40
15.30
CALC
F/A
0.013000
0.016700
0.017300
0.009000
0.017200
O.OOB400
O.OC7500
0.010600
COMPRESSOR
DISCHARGE
TFMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
OEGREES F
1505.00
1710.00
1780.00
1206.00
1900.00
1152.00
1094.00
1178.00
POWER
PFRCENT
RATED
T.O.
56
79
P9
22
94
IB
10
1
FXHMIST
GAS
TF IP
OEGRFF5 f
-o.nn
-0.00
-o.no
-0.00
-0.00
-0.00
-1.00
-0.00
EXHAUST
GAS
PRFSSURF
PSIA
-0.00
-0.00
-o.on
-0.00
-o. no
-o.on
-o.on
-o.oo
CO
(WET)
PPMV
34.00
34.00
13.00
14.00
10.00
13.10
13.01
269.00
cn
2
(WET)
PFRCENT V
2.35
2.35
3.20
1 .67
3.60
1.55
1.38
2. 14
THC
(WFTI
PPMV
0.0
0.0
0.0
0.0
0.0
0.0
n.o
215.00
NU
IWET)
PPMV
71.00
71.00
113.00
27.00
O.C
o.n
0.0
12.00
NO
2
IWETI
PPMV
8.00
8.00
5.00
10.00
0.0
0.0
0.0
16 .00
Nl)
X
IWFTI
PPMV
79.00
79.00
1 19.00
37.00
1 19.00
32.00
2B.OO
2R.OO
ALDEHYDES SMOKE PART1CULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-0.00
-0.00
-0.00
-o.on
-n.oo
-o.no
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
-0.00
-c.oo
POWER
PERCENT
KAIEO
T.fl.
56
79
R9
22
94
ia
10
3
MASS EMI
CIJ
LK/1K
L'J HIH
7.H9
? . 11
0. »l
1 .67
C.55
1.67
1 .98
74.56
MASS £11
HC
LH/1K
LK FUEL
o.n
0.0
0.0
0.0
1.0
P.O
0.0
1 1.24
MASS FMI
N02
I.'1/1K
LO FUEL
i.i?
1.12
0.51
1.96
0.0
0.0
1.0
2.40
MASS KM!
C(J2
LB/IK
LS FlltL
3134. 14
3134. )4
3137.60
1136.24
3138.00
3136.24
3135.12
3069.45
MASS EMI
NO
IB/IK
IP FIIFL
9.90
9.90
11. 5«
5.31
0.0
0.0
O.C
1.80
MASS EMI
NOX
LP/1K
LB FUEL
11.02
11.02
12.10
7.26
10. «4
6.77
6.65
4.20
MASS EMI
CO
LB/HR
4.07
5.07
1.53
1.51
1 .06
1.41
1 .44
14.37
MASS EMI
HC
LB/HP
0.0
0.0
0.0
0.0
0.0
0.0
0.0
6.58
MASS EMI
NC12
LB/HR
1.57
1.96
0.96
1.78
0.0
0.0
0.0
1.40
MASS EMI
C12
LB/HR
4419.41
5500.76
589D.68
23311.30
5993.58
7650.13
239D.9H
1795.63
MASS EMI
NO
LH/HR
13.96
17.37
21.7B
4. BO
0.0
0.0
0.0
1.05
MASS EMI
NHX
LB/HR
15.53
19.33
22.74
6.57
20.71
5.72
5.09
2.46
PERCENT
RATEO
T.n.
56
79
89
22
94
18
10
3
1.933
I . 6H6
0.455
1 .303
0. 100
7.093
3.560
101.165
LH/I* HP-MR
2099.484
1811.145
175H.175
3378.927
1696.456
3920.303
5938.063
12645.273
THC
LB/K HP-HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
46.30K
Nil
LB/1K HP-HK
6.631
5.784
6.490
5.711
0.0
0.0
o.o
7.413
LB/IK HP-HR
0. 74 7
0.652
0.287
2. 115
0.0
0.0
0.0
9.884
NO
X
LB/IK HP-HR
7.376
6.435
6.778
7.826
5.867
8.461
12.595
17.296
IV-14
-------
CAL ID NUMBER! 8 ENGINE TYPE AND MODEL I T56->7B
TEST ORGANIZATION: s w R I KELLY
SERIAL NUMBER! AE-101743
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBQUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIM80UT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.010
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.0)0
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
16.345 470.568 .000 19.00
0.0 1960.124 .000 0.50
2.413 1664.996 .000 2.50
2.007 1039.307 .000 4.50
16.345 470.566 .000 7.00
TOTAL FOR CYCLEi
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/ 1000K HP AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE HT FACTOR NODE
LB/HR LB/HR MIN.
7.052 470.566 .000 19.00
0.0 1960.124 .000 0.50
0.009 1864.996 .000 2.50
0.047 1039.307 .000 4.50
7.092 470.568 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE HT FACTOR MODE
LB/HR LB/HR MIN.
1.652 470.568 1.000 19.00
21.094 1960.124 1.000 0.50
20.368 1864.946 1.000 2.50
8.484 1039.307 I. 000 4.50
1.652 470.566 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
CO
MASS
LBS.
5.176
0.0
0.101
0.151
1.907
7.334
19.510
24.014
0.0
HC
MASS
LBS.
2.233
0.0
0.000
0.004
0.623
3.060
6.140
10.014
0.0
NOX
MASS
LBS.
0.523
0.176
0.849
0.636
0.193
2.377
6.323
7.782
46.812
FUEL
MASS
LBS.
149.01
16.33
77.71
77.95
54.90
375.90
FUEL
MASS
LBS.
149.01
16.33
77.71
77.95
94.90
375.90
FUEL
MASS
LBS.
149.01
16.33
77.71
77.95
54.90
375.40
LB CO /
IK LB FUEL
34.735
0.0
1.294
1.931
34.735
LB HC /
IK LB FUEL
14.987
0.0
0.005
0.045
14.987
LB NOX/
IK LB FUEL
3.511
10.761
10.921
8.163
3.511
ENERGY
HP-HR
35.67
31.29
140.61
64.49
13.14
305.41
ENERGY
HP-HR
35.67
31.29
140.81
64.49
13.14
305.41
ENERGY
HP-HR
35.67
31.29
140.81
84.49
13.14
305.41
LB CO /
HP-HR
0.14510
0.0
0.00071
0.00178
0.14510
LB HC /
HP-HR
0.06260
0.0
0.00000
0.00004
0.06260
LB NOX/
HP-HR
0.01467
0.00562
0.00603
0.00753
0.01467
IV-15
-------
DATE: 6/21/71
TEST ORGANIZATION: S V R I KELLY
ENGINE SUPPLIER: USAF, KELLY AFB
ENGINE DMA
CAL 10 NUMBER: 9 ENGINE TYPE AND MODEL: T56-A7B
RATED HORSEPOWER: 3755.
ENGINE TOTAL TIME: 4628. MRS
TIKE SINCE HOT SECTION OVERHAUL: 0. HRS
TINE SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
NZ COMPRESSOR OVERHAUL: -o. HRS
COMBUSTflR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TUKRINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: -o. HRS
FUEL: JP-4 FUEL H/C RATIO: 0.995
OPERATIONAL DATA ««»»»««««»
INLET AIR TEMPERATURE. DEGREES F: START 85.00 FINISH R5.00
ATMOSPHERIC PRESSURE: START 29.12 FINISH 29.12
INLET AIR HUMIDITY, IBS H20/LB AIR: 0.0170
RELATIVE HUMIDITY: 58.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/MIN:
SAMPLE LINF TRANSPORT TIME, SEC: 0.50
NUMBER OF TESTS: 9
COMMENTS:
F/A CALCULATION BUSED ON FXHAUST COMPOSITION FOR LAST THREE RUNS
SERIAL NUMBER:
AE-101695
ELAPSED
TIME
0.0
5.00
10.00
15.10
17.00
in. 30
20.30
22.00
29.30
I/ 0
71 I
I/ 2
4/ 1
5/ 4
R/ 5
7/ B
7/ 7
THRUST
OR
SMP
2237.
31 14.
3*41.
641.
3548.
363.
I2t>.
I2b.
176.
POWER
,LBS
00
00
00
00
00
00
00
no
00
PERCENT
RATED
T.O.
59
82
91
17
94
9
3
3
1
Nl
13BOO.
13800.
13800.
13210.
13800.
13430.
9.
9.
9.
ENGINE
SPEED
RPM
OC
00
00
00
00
00
92
91
90
N2
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-0.00
-0.00
-0.00
MEASURED
FUEL
FLOW
LB/HR
1450.00
1795.00
1930.00
815.00
1945.00
750.00
565.00
580.00
570.00
GAS GEN
AIR FLOW
LB/S6C
30.50
»0. 50
10.50
28.00
30.50
28.90
14.90
15.00
14.60
CALC
F/A
0.013200
0.016300
0.017600
o.ooaioo
0.017700
0.007200
0.010500
0.010700
0.010900
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TFNP
DEGREES F
1505.00
1710.00
1775.00
1132.00
1760.00
1080.00
1152.00
1150.00
1150.00
POWER EXHAUST
PERCENT GAS
RATED TEMP
T.O. DEGREE F
59
82
91
-0.00
-o.on
-o.oo
-o.oo
-o.oo
-o.no
-o.oo
-o.on
-o.on
EXHAUST
GAS
PBtSSIIPF
PSIA
-0.00
-o.on
-o.oo
-n.oo
-n.oo
-o.oo
-o.oo
-0.00
-0.00
CO
(WET)
PPMV
42.00
35.00
30.00
30.00
29.00
11 .00
261 .00
270.00
270.00
CT
2
IUETI
PERCENT V
2.44
3.07
3.2B
1.67
3.38
1.46
2.12
2.16
2.19
THC
IWET)
PPMV
4.00
4.00
2.00
3.00
3.00
4.00
162.00
175.00
171.00
NO
(MEM
PPMV
71.00
103.00
109.00
28.00
0.0
23.00
13.00
12.00
12.00
NO
2
IWETI
PPMV
7.00
5.00
5.00
4.00
0.0
5.00
16.00
17.00
17.00
NO
X
IWET)
PPMV
78.00
109.00
114.00
32.00
1 17.00
26.00
29.00
29.00
29.00
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-o.oo
-o.oo
-o.oo
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POUEP
PERCENT
BATED
T.O.
59
B2
91
17
94
t
1
3
3
MASS EMI 'HASS FMI MASS E^I
cn
0
5
2
1
1
FUEL
.
.
.
.
.
.
.
77
(15
74
92
0
56
13
92
90
MASS
N
EMI
OX
LB/IK
LB
11
12
12
6
17
6
4
4
4
FUEL
.28
.42
.28
.76
.23
.76
.74
.65
.59
MASS
C
EM
0
LB/HR
5
4
3
3
3
3
14
15
14
.36
.40
.80
.15
.59
.4?
.68
.29
.U3
MASS EMI MASS EMI MASS EMI
HC N02 C02
LB/HR LB/HR LB/HR
0.29
0.29
0.14
0.1S
0.21
0.25
5.22
5.68
5.IB
1.47
1.03
1.04
0.69
0.0
0.91
1.4B
I. 58
1.53
MASS EMI MASS FMI
NO NOX
LB/HR LB/HR
4B94.69
6063.00
6520.92
2750.91
6571.79
2530.45
1873.46
1921.97
1889.70
14.89
21.27
22.65
4.82
0.0
4.17
1.20
1.12
1.08
16.36
22.30
23.69
5.51
23.78
5.07
2.68
2.70
2.62
POWER
PERCENT
RATED
T.O.
59
R2
91
Ch
I.P/IK HP-MR
2.397
I.',11
1.101
4.831
1.011
9.420
1 16.504
171.352
117.680
LRMK HP-HR
2188.059
1947.015
1893.966
4225.660
1852.253
6970.926
14(168.703
15253.746
14997.578
THC
LB/IK HP-HR
0. 131
0.092
0.042
0.277
0.060
0.696
41.415
45.047
42.685
Nil
LB/IK HP-HR
6.656
6.829
6.580
7.407
0.0
11.480
9.532
8.859
8.591
LB/IK HP-HR
0.656
0.131
0.302
1.058
0.0
2.496
11.731
12.550
12.170
NO
V
LB/IK HP-HR
7.312
7.160
6. 882
8.465
6.703
13.976
21.263
21.409
20.761
IV-16
-------
CAL ID NUMBER! 9 ENGINE TYPE AND MODEL: T56-A7B
TEST ORGANIZATION: s w R I KELLY
SERIAL NUMBER: AE-101695
MODE FRACTIONAL
POWER
TAXI-IDLE 0.030
TAKEOFF 1. 000
CLIMBOUT 0.900
APPROACH 0.300
TAXI-IDLE 0.030
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
EMISSION
RATE
LB/HR
14.147
2.680
3.626
*.2U
14.147
FUEL
RATE
LB/HR
540.310
2016.737
1893. BB4
1046.024
540.310
USAGE
WT FACTOR
1.000
I. 000
1.000
1.000
1.000
TIME IN
MODE
NIN.
19.00
0.50
2.50
4.50
7.00
TOTAL FOR CVCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLEI
LBS POLLUTANT/1000K HP AT T.O.t
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.030
1.000
0.900
0.300
0.030
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
EMISSION
RATE
LB/HR
4.685
0.139
0.161
0.171
4.685
FUEL
RATE
LB/HR
540.310
2016.737
1893.884
1046.024
540.310
USAGE
WT FACTOR
.000
.000
.000
.000
.000
TIME IN
MODE
MIN.
19.00
0.50
2.50
4.50
7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
MODE
TAXI-IDLE
TAKF.OFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
EMISSION
RATE
LB/HR
2.537
24.308
23.462
8.529
2.537
FUEL
RATE
LB/HR
540.310
2016.737
1893. 884
1046.024
540.310
USAGE
WT FACTOR
.000
.000
.000
.000
.000
TINE IN
MODE
MIN.
19.00
0.50
2.50
4.50
7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
CO
MASS
LBS.
4.480
0.022
0.151
0.316
1.651
6.620
16.213
21.676
0.595
HC
MASS
LBS.
1.483
0.001
0.007
0.013
0.547
2.051
5.022
6.715
0.309
NOX
MASS
LBS.
0.803
0.203
0.978
0.640
0.296
2.919
7.149
9.558
53.945
FUEL
MASS
LBS.
171.10
16.81
78.91
78. 45
63.04
408.30
FUEL
MASS
LBS.
171.10
16. 81
78.91
78.45
63.04
408.30
FUEL
MASS
LBS.
171.10
16. Bl
7B.91
78.45
63.04
408.30
LB CO /
IK LB FUEL
26.IB4
1.329
1.915
4.028
26.184
LB HC /
IK LB FUEL
8.670
0.069
0.085
0.163
8.670
LB NOX/
IK LB FUEL
4.695
12.053
12.388
8.152
4.695
ENERGY
HP-MR
35.67
31.29
140.81
84.49
13.14
305.41
ENERGY
HP-HR
35.67
31.29
140.81
84.49
13.14
305.41
ENERGY
HP-HR
35.67
31.29
140.81
84.49
13.14
305.41
LB CO /
HP-HR
0.12559
0.00071
0.00107
0.00374
0.12559
LB HC /
HP-HR
0.04159
0.00004
0.00005
0.00015
0.04159
LB NOX/
HP-HR
0.02252
0.00647
0.00694
0.00757
0.02252
IV-17
-------
DATE: 6/23/71
TEST ORGANIZATION: s w R i KFLLY
FNGINF SUPPLIER: USAF, KELLY AF9
ENGINE DATA
CAL ID NUMBFR:
in ENGINE TYPE AND MODEL: T56-A7B
BATED HORSEPOWER: 1755.
ENGINE TOTAL TIME: 5381. MRS
TIME SINCE HOT SECTION OVFRHAUL: 0. MRS
TIME SINCE:
SERIAL NUHBERi
NI COMPRESSOR OVERHAUL: o. HRS
NZ COMPRESSOR OVERHAUL: -o. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVFRHAUL: 0. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUFL: JP-4 FUEL H/C RATIO: 1.995
OPERATIONAL DATA »»»*««««««««««
INLET AIR TEMPERATURE, DEGREES F: START 93.00 FINISH 9*.00
ATMOSPHERIC PRESSURE: START 29.05 FINISH 29.05
INLFT MR HUMIDITY, IBS H20/LB AIR: 0.013;
RELATIVE HUMIDITY: 37.00 PERCENT
SAMPLE LINE: TEMPFPATURF, DEGREES C: 150.00, FLOW RATE, LITERS/HIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.50
NUMBER OF TESTS: t
COMMENTS;
F/A CALCULATION BASFO ON EXHAUST COMPOSITION FOR LAST RUN
ELAPSED
TIMF
0.0
5.00
10.00
15.10
17.15
IS. 45
19.30
22.00
TEST
MODE
I/ 0
2/ I
3/ 2
4/ 1
5/ 4
4/ 5
8/ 4
7/ 8
THRUST
OR
ShP
2083.
2939.
1216.
720.
1458.
721.
236.
63.
POWER
,LBS
00
00
00
00
00
00
00
00
PERCENT
RATFO
T.O.
55
79
85
19
92
19
6
1
Nl
13900.
13880.
13900.
133*0.
14320.
13J50.
13490.
9990.
ENGINE
SPEED
RPM
00
oc
00
00
00
00
00
00
N2
-o.oo
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MEASURED
FUEL
FLOW
LB/HR
1405.00
1740.00
1860.00
860.00
1980.00
860.00
715.00
565.00
GAS GEN
AIR FLOW
LB/SEC
29.90
29.90
29.90
28.00
32.10
28.00
26.60
15.20
CALC
F/A
0.013100
0.016200
0.01 MOO
O.OOB500
0.017100
0.008500
0.006900
0.010300
COMPRESSOR
DISCHARGE
IEMP
DEGRESS F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
FPR
-fl.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
1508.00
1710.00
1782.00
1180.00
1852.00
1178.00
1076.00
1170.00
POWER
PERCENT
RATED
T.O.
55
78
85
19
92
19
6
EXHAUST
C.AS
TEMP
PEGPFES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0. 00
-0.00
EXHAUST
GAS
P°ESSURF
rsi A
-d. 00
-n.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-(I.00
CM
(WFTI
PPMV
44.00
29.00
24.00
29.00
22.00
26.00
24 .00
312.00
CO
2
IWETI
\>f PCENT
2.39
.02
.22
.66
.52
.59
.33
2.10
THC
IWETI
PPMV
0.0
0.0
0.0
0.0
0.0
0.0
0.0
NO
IUETI
PPMV
73.00
110.00
119.00
0.0
0.0
0.0
0.0
0.0
NO
2
IUET)
POMV
9.00
6.00
I.no
0.0
0.0
0.0
0.0
0.0
ALDEHYDES SMOKE PARTICULATFS
IHET)
PPMV
81.00
116.00
126.00
39.00
128.00
15.00
29.00
11.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POrtFR
PERCENT
RATED
T.n.
55
79
85
19
92
19
MASS FM1
cn
L6/1K
L9 FUFL
1.67
1.92
1.49
3. 36
1.25
1.26
3.60
28. KB
MASS EMI
HC
IB/ IK
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
0.0
1 4.31
MASS EMI
NII2
LS/1K
Lfl FUEL
1.10
0.65
0.71
0.0
0.0
0.0
0.0
0.0
MASS FMI
C02
LB/1K
1. B FUEL
1133.10
3135.86
3136.53
3133.59
3136.91
1113.75
31 13.22
3054.23
MASS EMI
NO
LB/1K
LB FUEL
10.00
11.94
12.12
0.0
0.0
0.0
0.0
0.0
MASS EMI
NOX
LP/IK
LB FUEL
11.10
12.59
17.83
7.70
11.92
7.21
7.14
4.71
MASS EMI
CO
LB/HR
5.16
3.33
2.77
2.89
2.47
2.90
2.57
16.1?
MASS EMI
HC
Lfl/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
8.09
MASS EM
NO 2
LB/HR
1.54
1.13
1.33
0.0
0.0
0.0
0.0
0.0
MASS EMI
CO 2
LB/HR
4402.01
5456.39
5833.95
7694.88
6211.08
2695.02
2240.25
1725.64
MASS EMI
NO
Lfl/HR
14.06
20.78
22.54
0.0
0.0
0.0
0.0
0.0
MASS EMI
NOX
LB/HR
15.60
21.91
23.86
6.62
23.61
6.20
5.11
2.66
POWER
PERCENT
RATEO
T.O.
55
78
B5
19
92
19
CO
LB/IK HP-MR
2.476
1.115
0.861
4.018
0.714
1. B90
10.902
259.004
LB/IK HP-HR
2113.302
1956.548
1814.040
1742.895
1796.149
3717.B95
9492.598
27391.109
THC
LB/IK HP-HH
0.0
0.0
0.0
0.0
0.0
0.0
0.0
128.369
NO
LB/IK HP-HR
6.749
7.069
7.008
0.0
0.0
0.0
0.0
0.0
LB/IK HP-HR
0.739
0.386
0.412
0.0
0.0
0.0
0.0
0.0
LB/IK HP-HR
7.487
7.455
7.421
9. 193
6.028
8.602
21.638
42.270
IV-18
-------
CAL ID NUMBER: 10 ENGINE TYPE AND MODEL: TS6-A7B
TEST ORGANIZATION: s w R I KELLY
SERIAL NUMBER! AE-104192
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
POWER
HP
112.6
3755.0
3379.5
1126.5
11Z.6
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR NODE
LB/HR LB/HR MIN.
9.139 588.560 1.000 19.00
1.700 2160.290 1.000 0.50
2.475 1941.074 1.000 2.50
3.811 1068.830 1.000 4.50
9.139 58B.560 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/ 1000K HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
3.138 588.560 .000 19.00
0.0 2160.290 .000 0.50
0.002 1941.074 .000 2.50
0.019 1068. 830 .000 4.50
3.138 588.560 .000 T.OO
TOTAL FOR CYCLE:
L9S POLLUTANT/ IK LB FUEL/CYCLE!
LBS POLLUTANT/IK HP-HR/CYCLE:
IBS POLLUTANT/ 1000K HP AT T.O. :
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/KR LB/HR MIN.
2.8B9 588.560 .000 19.00
10.241 2160.290 .000 0.50
25.268 1941.074 .000 2.50
9.101 1068.830 .000 4.50
2.889 588.560 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.I
CO
MASS
LBS.
2.894
0.014
0.101
0.286
1.066
4.363
10.051
14.286
0.377
HC
MASS
LBS.
0.994
0.0
0.000
0.001
0.366
1.361
3.136
4.458
0.0
NOI
MASS
IBS.
0.915
0.252
1.053
0.683
0.337
3.219
7.461
10.607
67.112
FUEL
MASS
LBS.
186.38
18.00
80.88
80.16
68.67
434.09
FUEL
MASS
LBS.
186.38
18.00
80.88
80.16
68.67
434.09
FUEL
MASS
LBS.
186.38
18.00
80.88
80.16
68.67
434.09
LB CO /
IK LB FUEL
15.527
0.787
1.275
3.565
15.527
LB HC /
IK LB FUEL
5.332
0.0
0.001
0.018
5.332
LB NOX/
IK LB FUEL
4.909
13.998
13.018
B. 515
4.909
ENERGY
HP-HR
35.67
11.29
140.81
84.49
13.14
305.41
ENERGY
HP -MR
35.67
31.29
140.81
84.49
13.14
305.41
ENERGY
HP-HR
35.67
31.29
140. Bl
84.49
13.14
305.41
LB CO /
HP-HR
0.08112
0.00045
0.00073
0.00338
0.08112
LB HC /
HP-HR
0.02786
0.0
0.00000
0.00002
0.02786
LB NOX/
HP-HR
0.02565
0.00805
0.00748
0.00808
0.02565
IV-19
-------
DATE: 6/24/71
TEST ORGANIZATION: S U R I KELLY
ENGINE SUPPLIER: USAF, KELLY AFB
ENGINE DATA «.
CAL ID NUMBER: 13 ENGINE TYPE AND MODEL: T56-A7B
RATED HORSEPOWER: 5755.
ENGINE TOTAL TIME: 4R79. MBS
TINE SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
NI CCHPRESSOR OVERHAUL: o. MRS
N2 COMPRESSOR OVERHAUL: -o. HRS
COHBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE HQllLf GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: -0. HRS
SERIAL NUMBER:
AE-103202
FUEL! JP-4 FUEL H/C RATIO: 1.995
OPERATIONAL DATA «»«««««««««««««»*»««
INLET AIR Tf«PERATURE, DEGREES F: START 82.00 FINISH 81.00
ATMOSPHERIC PRESSURE: START 2».I2 FINISH 29.12
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0153
RELATIVE HUMIDITY: 48.00 PERCENT
SAMPLE LINF: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.50
NUMBER OF TESTS: B
COMMENTS:
F/A CALCULATION RASED ON FXHAUST COMPOSITION FOR LAST RUN
ELAPSED
TIME
0.0
4.30
9.50
15.30
17.00
IB.45
20.30
21.30
TEST
MODE
4/
S/
4/
B/
II
THRUST
OR
SHP
2281.
3202.
1465.
504.
1710.
442.
274.
79.
POWER
,185
00
00
00
00
on
00
00
00
PERCENT
HATED
T.O.
60
B5
92
13
98
11
7
2
NI
1379.
11800.
13800.
13240.
14250.
11250.
13300.
9920.
ENGINE
SPEED
flPM
00
00
00
00
00
00
00
00
N2
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-0.00
MEASURED
FUEL
FLOW
LB/HR
1465.00
1820.00
1950.00
790.00
2070.00
770.00
715.00
555.00
GAS GEN
AIR FLON
L3/SEC
30.70
30.70
30.70
28.30
32.70
28.30
28.50
15.30
CALC
F/A
0.013300
0.016500
0.0)7600
0.007700
0.017600
0.007600
0.007000
0.010100
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
1505.00
1710.00
I7BO.OO
1100.00
1900.00
1082.00
1040.00
1124.00
POWER
PERCENT
RATED
T.I).
60
85
92
13
98
II
7
2
EXHAUST EXHAUST
C.AS GAS
T£»P PRESSURE
DEGREES r °SI«
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
co
(HETI
PPMV
49.00
IX. 00
12.00
36.00
31.00
35.00
35.00
279.00
CO
2
IhETI
PERCENT V
?.53
3.11
3.31
1.51
3.45
1.43
1.34
2.04
THC
(WETI
PPMV
0.0
0.0
0.0
4.00
0.0
4.00
4.00
NO NO
I WE II ?
PPMV (HETI
PPMV
ALDEHYDES SMOKE PARTICULATES
78.00
109.00
118.00
0.0
1 1 7.00
23.00
0.0
13.00
9.00
9.00
a.oo
0.0
0.0
7.00
0.0
17.00
IUETI
PPMV
87.00
118.00
126.00
32.00
0.0
30.00
27.00
30.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
1.0.
60
85
92
13
98
11
7
2
MASS EMI
CO
L6/1K
LR FUFL
1.86
2.44
.93
.75
. 79
.88
.20
2 .65
MASS EMI
HC
LB/1K
LB FUEL
0.0
0.0
0.0
0.30
0.0
0.12
0.14
12.69
MASS FMI
N02
LF1/IK
LB FUEL
1.17
0.95
0.79
0.0
0.0
1 .60
0.0
2.67
MASS EMI
C02
LB/IK
LO FUEL
1132.80
1135.04
3135.84
3130. 5H
1116.05
3110.34
3129. 16
1062.17
MASS FMI
NO
LK/IK
LR FUEL
10.10
11.49
1 1.69
0.0
11.12
5.26
0.0
2.04
MASS EMI
NOt
LB/IK
LB FUEL
11.26
12.44
12.48
6.94
0.0
6.87
6.59
4.71
MASS EMI
CO
Lfl/HR
5.66
4.44
3.76
1.75
3. 71
1.75
3.72
14. 79
MASS FMI
MC
LB/HR
0.0
0.0
0.0
0.24
0.0
0.25
0.24
7.05
MASS EMI
NO 2
LB/HR
1.71
1.73
1.55
0.0
0.0
1.23
0.0
1.4B
MASS EMI
C02
LR/HR
4589.55
5705.77
6114.88
2473.16
6491.61
2410.16
2217.78
1699.50
MASS EMI
NO
LB/HP
14.79
20.91
22.79
0.0
21.01
4.05
0.0
1.13
MASS EM
NOX
LB/HH
16.50
22.63
24.33
5.48
0.0
5.29
4.71
2.61
POWER
PERCENT
HATED
T.D.
60
85
92
13
9B
11
7
2
CO
LR/1K HP-HH
2.4BO
1.386
1.086
7. 446
1.001
8.495
13.577
IH7.254
LB/IK HP-MH
2012.081
1781.940
1764.757
4907.059
1749.766
5451.297
BUT.066
21512.723
THC
LB/IK HP-HH
0.0
0.0
0.0
0.474
0.0
0.556
O.BR9
89.178
NO
LB/IK HP-HR
6.485
6.529
6.577
0.0
6.2C1
9.169
0.0
14.331
LB/IK HP-HR
0.74R
0.539
0.446
0.0
0.0
2.791
0.0
18.741
NO
X
LB/IK HP-HR
7.233
7.068
7.023
10.871
0.0
11.960
17.203
31.073
IV-20
-------
CAl 10 NUMBERi 13 ENGINE TVPE AND MODEL: T56-ATB
TEST ORGANIZATION: s w R I KELLY
SERIAL NUMBER: AE-103202
NODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IOLE
HODE
TAXI-IOLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IOLE
HODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POKER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POKER
0.030
1.000
0.900
0.300
0.030
POWER
HP
112.6
37S5.0
3379.5
1126.5
112.6
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
POWER
HP
112.6
3755.0
3379.5
1126.5
112.6
ENISSION FUEL USACE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
13.183 562.6*9 .000 19.00
3.472 2091.033 .000 0.50
4.006 1916.847 .000 2.50
4.604 1086.378 .000 4.50
13.183 582.649 .000 T.OO
TOTAL FOR CYCLEl
IBS POLLUTANT/ IK LB FUEL/CYCLEl
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000X HP AT T.O.I
ENISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR 16/HR KIN.
5.238 582.649 .000 19.00
0.0 2091.033 .000 0.50
0.013 1916.647 .000 2.50
0.162 1086.378 .000 4.50
5.238 582.649 .000 7.00
TOTAL FOR CYCLEl
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLEl
LBS POLLUTANT/ 1000K HP AT T.O.I
EMISSION FUEL USAGE TIHE IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
2.949 582.649 .000 19.00
26.433 2091.033 .000 0.50
23.969 1916.847 .000 2.50
9.336 1086.378 .000 4.50
2.949 582.649 .000 T.OO
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLEl
LBS POLLUTANT/ IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
CO
MASS
L8S.
4.175
0.029
0.167
0.343
1.538
6.254
14.501
20.477
0.770
' HC
MASS
LBS.
1.663
0.0
0.001
0.012
0.613
2.291
5.313
7.502
0.0
NOX
MASS
LBS.
0.934
0.220
0.999
0.700
0.344
3.197
7.414
10.469
38.661
FUEL
MASS
LBS.
184.51
17.43
79.87
81.48
67.98
431.25
FUEL
MASS
LBS.
184.51
17.43
79.87
81.48
67.98
431.25
FUEL
MASS
LBS.
184.51
17.43
79.87
81.48
67.98
431.25
LB CO /
IK LB FUEL
22.626
1.660
2.090
4.23B
22.626
LB HC /
IK LB FUEL
9.023
0.0
0.007
0.149
9.025
LB NOX/
IK LB FUEL
5.062
12.641
12.504
8.594
5.062
ENERGY
HP-HR
35.67
31.29
140.81
84.49
13.14
305.41
ENERGY
HP-HR
33.67
31.29
140.81
84.49
13.14
303.41
ENERGY
HP-HR
35.67
31.29
140.81
64.49
13.14
305.41
LB CO /
HP-HR
0.11703
0.00092
0.00119
0.00409
0.11703
LB HC /
HP-HR
0.04668
0.0
0.00000
0.00014
0.04668
LB NOX/
HP-HR
0.02618
0.00704
0.00709
0.00829
0.02618
IV-21
-------
DATE: 6/24/71
TEST ORGANISATION: 5 w B [ KELLY
ENGINE SUPPLIER! USAF , KELLY AFB
ENGINE DATA
CAL ID NUMBER: 12 ENGINF TYPF ANO MODEL: T56-A7KB
RATED HORSEPOWER: 3755.
fNCINE TOTAL TIME: 5743. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
SERIAL NUMBER:
AF-IO«15
NI COMPRESSOR OVERHAUL: o. HRS
«2 COMPRESSOR OVERHAUL: -o. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NUZ/LC GUIDE VANF. OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: -o. HRS
FUEL: jp-4 FUEL H/C RATIM: 1.995
OPERATIONAL OAT A «««**««»«»«»«»«««.««««.««««..«.*....«....
INLET AIR TEMPERATURE, DEGREES F: START 90.00 FINISH 90.00
ATMOSPHERIC PRESSURE: START 29.14 FINISH 29.14
INLET AIR HUMIDITY, LBS H20/L9 AIR: 0.0147
RELATIVE HUMIDITY: 43.00 PERCENT
SAMPLE LINE: TEMPFBATURE, DEGREES C: 150.00. FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIMF, SEC: 0.50
NUMBER OF TESTS: 8
COMMENTS:
F/A CALCULATION HASCO ON EXHAUST COMPOSITION TOR LAST RUN
ELAPSED
TIMF
0.0
5.30
10.00
16.15
17.30
19.00
19.45
72.00
TEST
MPPE
I/ 0
?/ 1
I/ 2
4/1
5/ 4
4/ 5
R/ 4
7/ 8
POWER
THRUST, LBS
OR
SHP
2115.00
2982.00
126R.OO
840.00
1470.00
B40.00
423.00
141.00
PERCENT
»ATEU
T.O.
56
79
87
27
97
22
11
1
EN(
SI
F
NI
13810.00
11780.00
13800.00
11240.00
14200.00
13240.00
13340.00
9890.00
MEASURED
FUEL
FLOW
LB/HR
GAS GEN
AIR FLOW
LB/SEC
CALC
F/A
0.00
0.00
o.oo
0.00
0.00
0.00
0.00
0.00
1410.00
1740.00
1850.00
895.00
2052.00
895.00
765.00
585.00
30.10
30.10
10.10
27.80
il.80
27.80
28.10
15.00
0.011000
0.016100
0.017000
0.008900
0.017900
0.009900
0.007500
0.010800
COMPRESSOR
DISCHARGF
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-C.OO
-0.00
-0.00
TURBINE
INLET
TEMP
OEGREFS f
1508.00
1710.00
1775.00
1204.00
1952.00
I20B.OO
1108.00
1202.00
POWER
PERCENT
RATED
T.O.
56
79
87
2?
92
22
11
t
Exi'aiisr
GAS
TCMP
-o. no
-o.oo
-o.oo
-n.oo
-o.oo
-o.oo
-o.oo
-o.oo
E XHAUST
GAS
PRESSURE
PSIa
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.00
-0.00
cn
IWET)
PPMV
41.00
37.00
13.00
34.00
31.00
33.00
32.00
311.00
CO
2
IWET)
PERCENT V
2.18
2.93
1. 16
1.71
3.46
1.73
1.43
2.19
THC
IWET)
PPMV
0.0
0.0
0.0
0.0
0.0
0.0
0.0
228.00
NO
(WET)
PPMV
66.00
98. OC
108.00
0.0
0.0
0.0
0.0
11.00
NO
2
(WET)
PPMV
7.00
7.00
5.00
0.0
0.0
0.0
0.0
18.00
NO
X
IWET)
PPMV
73. OC
105.00
113.00
15.00
1 13.00
35.00
78.00
29.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PAHTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
56
79
87
22
92
2?
II
3
ASS PHI
r.n
IB/IK
LF\ FIJFI.
3.44
2.57
7.03
3.96
1.79
3.80
4.46
77.69
IASS E«!
HC
LR/1K
LB IUFL
0.0
0.0
n.o
0.0
0.0
0.0
0.0
11.61
MASS EMI
102
LFf/lK
LR FUEL
0.96
0. 7fl
0.52
0.0
0.0
0.0
0.0
2.63
MASS KM I
r.07
LB/IK
LB F'.ITL
3133.47
JM4.'M
3135.60
3132.64
1136.06
3132.90
31 11 .86
3063. 48
MASS EMI
NO
LB/IK
LB FUEL
9.08
10.96
11.70
0.0
0.0
0.0
O.O
1.61
MASS EMI
NOX
LB/IK
LB FUEL
10.05
11.74
11.72
6.70
10.71
6.61
6.41
4.24
MASS EMI
cn
LB/HR
4.84
4.1H
1.86
1.55
1.67
1.40
3.41
16.20
MASS EMI
HC
Lfl/HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
6.80
MASS EMI
NCI 2
I.D/HR
1.16
1.36
0.96
0.0
0.0
0.0
0.0
1.54
MASS EMI
C02
LB/HR
4418.20
5454.75
5800.85
2803.72
6435.20
2803.94
7395.88
1792.13
NASS EMI
NO
LB/HR
12.81
19.07
20.73
0.0
0.0
0.0
0.0
0.94
MASS EMI
NOX
LB/HR
14.17
20.44
21.69
6.00
21.97
5.93
4.90
2.48
PDWFR
PERCENT
RATED
T.O.
56
79
87
72
9?
22
II
3
cn
LP/IK HP-HR
2.101
I .470
I . 180
4.724
1 .057
4.052
8. 067
I 14.H76
LB/IK HP-HS
2098.906
1879.274
17 75.046
3117.757
1854.523
1318.027
5664.008
12710.164
THC
LB/IK HP-HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
46.214
NO
LB/IK HP-HR
6.085
6.196
6.342
0.0
0.0
0.0
0.0
6.674
LB/IK HP-HR
0.645
0.457
0.294
0.0
0.0
0.0
0.0
10.921
NO
X
LB/IK MP-HR
6.710
6.851
6.636
7.142
6.312
7.060
11.594
17.595
IV-22
-------
c»i 10 NUMBER: 12 ENGINE TYPE »ND MODELi T56-«TKB
TEST ORGANIZATION: S V R I KELLY
SERIAL NUMBER! AE-104215
NODE FRACTIONAL
POWER
TAXI-IDLE 0.030
TAKEOFF 1.000
CLIMBOUT 0.400
APPROACH 0.300
TAXI-IOLE 0.030
POWER
HP
112.6
3755.0
33T9.5
1126.9
112.6
EMISSION FUEL
RATE RATE
LB/HR LB/HR
21.649 609.222
0.0 2256.038
1.666 1933.967
3.642 1002.166
21.649 609.222
USAGE
NT FACTOR
1.000
1.000
1.000
1.000
1.000
TIME IN
MODE
MIN.
19.00
0.50
2.50
4.50
7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
POWER
HP
112.
3T55.
3379.
1126.
112.
6
0
5
5
6
EMISSION FUEL
RATE RATE
LB/HR LB/HR
7.955 609.222
0.0 2296.038
0.004 19S1.967
0.0 1002.166
7.955 604.222
USAGE
WT FACTOR
.000
.000
.000
.000
.000
TIME IN
MODE
MIN.
19.00
0.90
2. SO
4.50
7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
185 POLLUTANT/IK HP-HR/CYCLE:
LBS PQLLUTANT/1000K HP AT T.O.:
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
POWER
HP
112.
3755.
3379.
1126.
112.
6
0
5
5
6
EMISSION FUEL
RATE RATE
LB/HR LB/HR
2.027 609.222
2S.B69 2256.038
22.794 1953.967
7.169 1002.166
2.027 609.222
USAGE
UT FACTOR
1.000
1.000
1.000
1.000
1.000
TIME IN
MODE
MIN.
14.00
O.SO
2.50
4. SO
7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE i
LBS POLLUTANT/1000K HP AT T.O.:
CO
MASS
LBS.
6. ess
0.0
0.064
0.273
2.526
9.724
22.131
31.634
0.0
HC
MASS
LBS.
2.519
0.0
0.000
0.0
0.928
3.447
7.B46
11.287
0.0
NOX
MASS
LBS.
0.642
0.216
C.950
O.S3B
0.236
2.581
5.875
B.4S2
57. 411
FUEL
MASS
LBS.
192.92
18.80
81.42
75.16
71.08
439.37
FUEL
MASS
LBS.
192.92
18.80
81.42
75.16
71.08
439.37
FUEL
MASS
LBS.
192.92
18.80
81.42
75.16
71.08
439.37
LB CO /
IK LB FUEL
35.535
0.0
0.853
3.635
35.535
LB HC /
IK LB FUEL
13.057
0.0
0.002
0.0
13.057
LB NOX/
IK LB FUEL
3.327
11.467
11.665
7.154
3.327
ENERGY
HP-HR
35.67
31.29
140.81
84.49
13.14
305.41
ENERGY
HP-HR
35.67
31.29
140.81
B4.49
13.14
305.41
ENERGY
HP-HR
35.67
31.29
140.81
84.49
13.14
305.41
LB CO /
HP-HR
0.19218
0.0
0.00049
0.00323
0.19218
LB HC /
HP-HR
0.07062
0.0
0.00000
0.0
0.07062
LB NOX/
HP-HR
0.01799
0. 00689
0.00674
0.00636
0.01799
IV-23
-------
DATEI 6/24/71
TEST ORGANIZATION: S H R I KELLY
SUPPLIER: USAF, KELLY APR
ENGINE DATA
CAL ID NUMBER:
II ENGINE TVPf AND HODEL: T56-A15
RATED HORSEPOWER: 4591.
ENGINE TOTAL TIME: 2779. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 0. MRS
NZ COMPRESSOR OVERHAUL: -o. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOKLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE (1VFRHAUL: 0. HRS
HZ TURBINE OVERHAUL: -0. HRS
FUEL: JP-4 fuEL H/C RATIO: 1.995
OPERATIONAL OATA ««»««««»»«««
INLET AIR TEMPERATURE, DEGREES F: START 79.00 FINISH
ATMOSPHERIC PRESSURE: START 29.29 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0167
RELATIVE HUMIDITY: 76.oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/KIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.50
NUMBER OF TF.STS: 10
COMMENTS:
F/A CALCULATION BASED ON EXHAUST COMPOSITION FOR ALL RUNS
SERIAL NUMBER:
60.00
29.29
".2.50
ELAPSED
TIME
0.0
6.00
11.00
16.30
19.00
21.00
22.00
25.00
27.00
28.30
POWER
PERCENT
RAIEO
T.O.
56
83
89
95
18
96
94
19
2
5
POHFR
PERCENT
RATED
r.n.
56
83
89
95
18
96
94
19
2
5
POWER
PERCENT
RATED
T.O.
56
83
R9
95
IB
96
94
19
2
5
TEST
MODE
I/ 0
2/ 1
3/ 2
6/ 3
4/ 6
5/ 4
6/ 5
4/ 6
7/ 4
R/ 7
EXHAUST
C.AS
TFMP
UEGRCFS F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MASS FMI
rn
LP/IK
LR FDFL
-7,
.27
7. 1
.04
.46
.04
.04
3.40
10.01
5.68
CO
L'/IK
1.
0.
0.
0.
3.
0.
0.
3.
138.
18.
POWER
THRUST, LBS
OR
SHP
2610.00
1838.00
4173.00
4386.00
848.00
4452.00
4120.00
911.00
127.00
713.00
FXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
»ASS FMI
PERCENT
RATED
ENGINE
SPEED
RPM
T.O. Nl
56 13820
83 13800
R9 13820
95 13800
18 13360
96 13820
94 13800
19 13350
2 9990
5 13350
Cll
IWETI
PPMV
21.00
22.00
77.00
21.00
29.00
71 .00
21.00
29.00
378.00
40.00
MASS KMI MUSS
.00
.00
.00
.00
.00
.00
.00
.00
.00
.00
en
2
IWETI
PEPCENT
2.69
3.45
I.t2
4.04
1.67
4.04
4.04
1.70
2.44
1.40
MEASURFn GAS GEN
N2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.oo
-0.00
FUEL
FLOW
LB/HR
AIR FLOW
LB/SEC
1600.00 13.40
2085.00 33.90
2180.00 13.60
2275.00 11.40
930.00 31.10
2295.00 31.70
2275.00 31.40
955.00 31.60
585.0
0 11.40
750.00 30.20
THC
IW
ETI IW
NO NO
FTI 2
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
PPMV PPMV IUET)
V
n
8
9
11
9
12
11
9
185
18
CMI MASS tMI
Hr NO? Cfl2
LR/1K
LP FUEL
0.34
0.27
0.78
0.31
0.62
0.34
0.31
0.60
17.51
1 .46
LR/IK LB/IK.
LR FUEL LR F1IFI L
O.R5 3135.
0.3H 1136.
0.54 3136.
0.73 3136.
0.0 3131.
0.0 1136.
0.73 3136.
0.0 3131.
2.48 3043.
O.n 3I7S.
CO
2
HP-HB LH/U HP-HR
04b
691
641
538
796
535
546
565
235
297
1921.996
1701. 716
1658.230
1626.830
3434.584
1616. 762
1651.685
3281.139
14020.164
10061.988
76
15
19
19
75
31
.19
fl7
69
01
NO
IB/IK
H TUEL
7.43
H.R4
8.42
S.28
0.0
0.0
R.7R
0.0
1.17
o.n
PPMV
.00 61.00 7.00
.00 93.00 4.00
.00 9
3.00 6.00
.00 102.00 9.00
.00
.00
0.0 0.0
0.0 0.0
.00 107.00 9.00
.00
.00
.00
MASS FMI
NOX
LB/IK
LR FUEL
8.29
9.72
R.97
9.01
6.47
0.01
9.01
6.74
1.65
6.77
THC
LR/IK
0
0
0
0
0
0
0
HP-HP.
.208
. 144
.150
.161
.675
.175
. 164
LR/IK
0.614
HO
4
.616
.716
0.0 0.0
9.00 19.00
0.0 0.0
MASS FMI MASS
CO
LG/HR
2.73
2.65
2.64
2.16
3.22
2.38
2.36
3.25
17.56
4.26
NO
HC
CALC
F/A
01 3300
017100
018000
070100
008300
020100
020100
008400
012100
006900
NO
X
IWETI
PPMV
68.00
97.00
99.00
111.00
33.00
111.00
111.00
35.00
28.00
29.00
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIO
DEGREES F FPR
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
ALDEHYDES SMOKE
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
FMI MASS EMI MASS EMI MASS
L8/HR
0.
0.
0.
0.
0.
0.
0.
0.
10.
1.
HP-HR LR/IK
4.556
4.801
4.451
4.294
0.0
0.0
4.359
0.0
5.406
0.0
1
54
55
62
71
57
78
71
5fl
24
10
NO
2
HP-HR
0.523
0.207
0.787
0.379
0.0
0.0
0.3B5
0.0
1.413
0.0
N02 C(12 NO
TURBINE
INLET
TEMP
DEGREES f
1605.00
1872.00
1920.00
1968.00
1212.00
2035.00
1970.00
1210.00
1218.00
1124.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
EMI MASS EMI
NOX
LB/HR LB/HR LB/HR LB/HR
1.36 5016.41 11.
0.79 6538.86 18.
1.18 6816.88 18.
1.66 7135.23 16.
0.0 2912.51 0.
0.0 7197.82 0.
1.66 7115.28 18.
0.0 2990.94 0.
1.45 1780.56 0.
0.0 2344.44 0.
NO
X
1 R/ IK HP-HR
5.079
.008
.741
.673
.095
.644
.744
.066
16.819
21.789
89 13.26
43 19.22
36 19.55
B.I 20.49
0 6.02
0 20.67
81 20.49
0 6.44
69 2.14
0 5.08
IV-24
-------
CAL ID NUMBER: 11 ENGINE TYPE AND MODEL: T56-A15
TEST ORGANIZATION: s w R i KELLY
SERIAL NUMBERl A£-106634
NODE
TAXI-IOLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKFOFF
CLIHBOUT
APPROACH
TAXI-IOLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.0)0
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
POKER
HP
137.7
4591.0
4131.9
1377.3
137. T
POWER
HP
137.7
4591.0
4)31.9
1377. 3
137.7
POWER
HP
137.7
4591.0
4131.9
1377.3
137.7
EMISSION FUEL USAGE TIME IN
RATE RATE *T FACTOR MODE
LB/HR LB/HR HIN.
30.255 575.225 .000 19.00
2.112 2358. 710 .000 0.50
2.345 2164.557 .000 2.50
3.149 1135.413 .000 4.50
30.255 575.225 .000 1.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CVCLE1
LBS POLLUTANT/ 1000K HP AT T.Q.I
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
18.507 575.225 .000 19.00
0.557 2398.710 .000 0.50
0.511 2164.557 .000 2.50
0.544 1135.413 .000 4.50
18.507 575.225 .000 7.00
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB FUEL /CYCLE 1
LBS POLLUTANT/IK HP-HR/CYCL6:
LBS POLLUTANT/1000K HP AT T.O. :
EMISSION FUEL USAGE TIME IN
RATE RATE MT FACTOR MODE
LB/HR LB/HR MIN.
1.660 575.225 .000 19.00
21.327 2358.710 .000 0.50
19.560 2164.557 .000 2.50
B.398 1135.413 .000 4.50
1.660 575.225 .000 7.00
TOTAL FOR CYCLE I
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE>
LBS POLLUTANT/ 1000K HP AT T.O.t
CO
MASS
LBS.
9.581
0.018
0.098
0.236
3.530
13.462
30.302
36.053
0.383
HC
MASS
LBS.
5.861
0.005
0.021
0.041
2.159
8.086
18.202
21.656
1.010
NOX
MASS
LBS.
0.526
0.178
0.815
0.630
0.194
2.342
5.271
6.271
38.712
FUEL
MASS
LBS.
182.15
19.66
90.19
85.16
67.11
444.27
FUEL
MASS
LBS.
182.15
19.66
90.19
85.16
67.11
444.27
FUEL
MASS
LBS.
182.15
19.66
90.19
85.16
67.11
444.27
LB CO /
IK LB FUEL
52.598
0.895
1.083
2.TT4
52.59B
LB HC /
IK LB FUEL
32.174
0.236
0.236
0.479
32.174
LB NOX/
IK LB FUEL
2.885
9.042
9.036
7.397
2.885
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
LB CO /
HP-HR
0.21967
0.00046
0.00057
0.00229
0.21967
LB HC /
HP-HR
0.13437
0.00012
0.00012
0.00039
0.13437
LB NOX/
HP-HR
0.01205
0.00465
0.00473
0.00610
0.01205
IV-25
-------
041f: 6/16/71
TEST ORGANIZATION: ALLISON DIVISION
ENGINE SUPPLIER: ALLISON DIVISION
ENGINE DATA
cu ID NUNBFR:
IB
ENGINE TYPE AND MODEL: T56-M5
RATEO HORSEPOWER: 4591.
ENGINE TOTAL TIME:
TIME SINCF HOT SECTION OVERHAUL:
TIME SINCF:
SERIAL NUMBER:
0. HRS
0. HRS
Nl COMPRESSOR OVERHAUL: 0. HRS
NZ COMPRESSOR OVERHAUL: o. HRS
COMRUSTOR CAN REPLACEMENT: 0. HRS
FIRSI STAGF NOZZLE GUIDE VANF OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: o. HRS
FUEL: JP-S FUEL H/C RATIO: 1.970
OPERATIONAL nATA «««»»»«
INLET AIR TEMPERATURE. DEGREES F: START 90.00 FINISH
ATMOSPHFRIC PRESSURE: START 28.70 FINISH
INLET AIR HUMIDITY, IBS H20/LB AIR: 0.0096
RELATIVE HUMIOITY: 10.00 PERCENT
SAMPLE LINE: TEMPERATURE. OEGREFS C: 15*.**, FLOW RATE, LITERS/MIN:
SAMPLF LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 7
COMMENTS:
FINAL RUN
98.00
2D.90
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TCST
MOOE
I/ 0
II 1
3/ 2
5/ 1
6/ 5
I/ 6
15/ 7
THRUST
OR
SHP
235.
2342.
1590.
4160.
1081.
829.
257.
POHFR
,LBS
60
90
90
10
50
20
00
PERCENT
RATED
T.O.
5
51
78
90
21
18
5
Nl
11500.
11800.
13800.
13300.
14200.
11200.
13500.
ENGINE
SPFED
RPM
00
00
cc
00
00
00
00
N2
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
N2
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MEASURED
FUEL
FLOW
LB/HR
721.00
1522.00
1925.00
2152.00
1058.00
900.00
710.00
GAS GEN
AIR FLOW
LD/SEC
29.83
29.79
2972.00
29.72
27.17
29.58
29.97
CALC
F/A
O.OC6700
0. 014200
0.017990
0.020100
O.OIOBOO
0.008500
0.006100
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
1090.00
1610.00
1850.00
1970.00
1385.00
1175.00
1085.00
POWER
PERCENT
RATED
T.O.
5
51
78
90
21
18
5
EXHAUST
GAS
TFMP
DEGREES F
-0.00
-0.00
-0.00
-1). 00
-0.00
-0.00
-n.oo
FXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
IORYI
PP"V
50.00
10.00
32.00
34. 10
15.00
52.00
50.00
cn
2
ICRY1
PERCENT V
1.42
3.23
4, 10
4.43
1.07
2.08
1.42
THC
IHETI
PPMV
40.00
13.00
2.00
2.00
1.00
1.00
21.00
NU
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES SMOKE PART1CULATES
IORYI
PPMV
12.00
91.00
129.00
152.00
129.00
71.00
30.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-n.oo
-0.00
62.00
59.00
60.00
60.00
57.00
62.00
67.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
5
51
78
90
23
IB
MASS EMI
cn
LB/IK
LB FUFL
7.00
1.16
1.56
1.51
2.71
4. 94
7.01
MASS EK[
HC
Lrt/lK
LP FUEL
1.75
0.48
0.06
0.05
0.12
0. 17
1.87
MASS FMI
ND2
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
C02
L6/1K
L6 FUEL
1124.60
1140.10
1141.91
1141.17
3140.63
1116.27
1128. 17
MASS FMI
10
LB/IK
LB F»PL
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
MASS FMI MASS FMI MASS EM
NOX r.o HC
LB/IK LB/HR L3/H5
LR FUEL
7.16
9.86
10.13
1 1.27
M.80
II. 19
6.91
5.05
2.81
1.00
1.10
2.41
4.49
5.12
2.15
0.72
0.11
0.12
0.12
0.15
1.37
MASS EMI MASS tMI
N02 C02
LB/HR LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
2252.84
4779.54
6048.18
6761.50
1322.78
2827.60
2281.71
MASS EMI
NO
L°/HP
-0.00
-0.00
-0.00
-0.00
-O.on
-0.00
-0.00
MASS EMI
NOX
LB/HR
5.11
15.01
19.69
24.25
14.60
10.07
5.04
POWER
PERCENT
RATEO
T.O.
51
7B
90
21
18
5
cn
Lfl/IK HP-KP
7.1.".79
1.206
0.117
0.794
2.'29
5 . ', 16
19.414
CO
!
LB/IK HP-HR
9562.121
2040.010
1634.108
1625.246
1072.185
1404.004
8886.015
THC
L8/l« HP-HR
9.956
0. 309
0.011
0.028
0.111
0.183
5.170
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-O.OPO
-0.000
-0.000
LB/IK HP-HR
-0.000
-0.000
-o.oon
-0.000
-0.000
-0.000
-0.000
L8/IK HP-HR
22.527
6.404
5.540
5.830
11.496
12.147
19.626
IV-26
-------
C»L ID NUMBER: IB ENGINE TYPE AND MODEL! 156-415
TEST ORGANIZATION: ALLISON DIVISION
SERIAL NUMBER: 8506
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POKER
0.030
1.000
0.900
0.300
0.030
POWER
HP
137.7
4591.0
4131.9
1377.3
137.7
POWER
HP
137.7
4591.0
4131.9
1377.3
137.7
POWER
HP
137.7
4591.0
4131.9
1377.3
137.7
EMISSION FUEL USAGE TIME IN
RATE RATE MT FACTOR MODE
LB/HR LB/HR MIN.
2.987 406.335 .000 19.00
3.867 2334.892 .000 0.50
3.535 2134.571 .000 2.50
2.604 1184.325 .000 4.50
2.987 406.335 .000 7.00
TOTAL FOR CVCLEl
LQS POLLUTANT/IK LB FUEL/CTCLE:
LBS POLLUTANT/IK HP-HR/CTCLE:
LBS POLLUTANT/ 1000K HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE UT FACTOR MODE
LB/HR LB/HR MIN.
6.425 406.335 .000 19.00
0.044 2334.892 .000 0.50
0.058 2134.571 .000 2.50
0.045 1184.325 .000 4.50
6.425 406.335 .000 7.00
TOTAL FOR CYCLEl
LBS POLLUTANT/IK LB FUEL/CTCLEl
IBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O. :
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
1.633 406.335 .000 19.00
30.075 2334.892 .000 0.50
23.783 2134.571 .000 2.50
10.357 1184.325 .000 4.50
1.633 406.335 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
CO
MASS
LBS.
0.946
0.032
0.147
0.195
0.348
1.669
4.471
4.470
0.702
HC
MASS
LBS.
2.035
0.000
0.002
0.007
0.750
2.794
7.485
7.483
0.081
NOX
MASS
LBS.
0.517
0.251
0.991
0.777
0.191
2.726
7.303
7.301
54.591
FUEL
MASS
LBS.
128.67
19.46
88.94
88.82
47.41
373.30
FUEL
MASS
LBS.
128.67
19.46
88.94
88.82
47.41
373.30
FUEL
MASS
LBS.
128.67
19.46
88.94
88.82
47.41
373.30
LB CO /
IK LB FUEL
7.351
1.656
1.656
2.198
7.351
LB HC /
IK LB FUEL
15.813
0.019
0.027
0.080
15.813
LB NOX/
IK LB FUEL
4.020
12.881
11.142
8.745
4.020
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
LB CO /
HP-HR
0.02169
0.00084
0.00086
0.00189
0.02169
LB HC /
HP-HR
0.04665
0.00001
0.00001
0.00007
0.04665
LB NOX/
HP-HR
0.01186
0.00655
0.00576
0.00752
0.01186
IV-27
-------
DATEl 6/21/71
TEST ORGANIZATION: ALLISON DIVISION
ENGINE SUPPLIER: ALLISON DIVISION
ENGINE DATA ««..............«.........,,....................
CAL ID NUMBER: 19 ENGINF ITPE AND MODEL: T56-A15
RATED HORSEPOWER: 4591.
ENGINE TOTAL TINE: 0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TINE SINCF:
NI COMPRESSOR OVERHAUL: o. HRS
N2 COMPRESSOR OVERHAUL: o. HRS
COMBUSTUR CAN REPLACEMENT: 0. HRS
FIRST STAGE N022LF GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL: JP-5 FUEL H/C RATIO: 1.970
OPERATIONAL DATA «*«««««««««»»»
INLET AIR TEMPERATURE, DEGREES F: START 90.00 FINISH 91.00
ATMOSPHERIC PRESSURE: START 7.8.70 FINISH 23.90
INLET AIR HUMIDirv, L8S H20/LR AIR: 0.009*
RFLATIVE HUMIDITY: 29.00 PERCENT
SAMPLE LINF: TEMPERATURE, CFGREES C: 154.44, FLOW RATE, LITERS/HIM:
SAMPLE LINE TRANSPORT T1MF, SEC: 1.00
NUMBER GF TESTS: 8
COMMENTS:
FINAL RUN
SERIAL NUMBER:
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
TEST
MODE
I/ 0
21 I
I/ ?.
4/ 1
5/ 4
If 5
II 7
I4/ 9
THRUST
OR
SHP
235.
2519.
1591.
J8-i3.
4335.
829.
4116.
95.
POUCR
.IBS
60
90
00
70
40
20
50
20
PERCENT
RATED
T.O.
5
55
7fl
83
94
IB
89
2
M
13500.
13800.
13800.
13800.
13800.
13400.
13BOO.
10000.
ENGINE
SPEED
QPM
00
00
00
00
00
00
00
00
N2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MEASURED
FUEL
FLOW
LB/HR
7 18 . 00
1544.00
1940.00
2045.00
2128.00
908.00
2150.00
572.00
GAS GEN
MR FLOW
LB/SEC
29.73
-0.00
29.62
29.72
29.65
29. 48
79.59
20.08
CALC
F/A
0.006700
0.014400
0.018200
0.019100
O.CI9900
O.OOS600
0.020200
0.003800
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
PATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
990.00
1610.00
1B50.00
1920.00
1970.00
1250.00
1970.00
1205.00
POWER
PERCENT
RATED
T.O.
5
55
78
83
94
18
R9
2
E XHAUST
GAS
DFC.PFES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
EXHAUST
GAS
PRESSURE
PSI A
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
(DRY I
PPMV
52.00
37.00
37.00
35.00
35.10
37.00
35.00
450.00
CO
2
ICRTI
PERCENT V
1.70
3.46
4.42
4.55
4.70
2.18
4.90
3.06
THC
(WETI
PPMV
32.00
5.00
3.00
2.00
1.00
8.00
3.00
180.00
NO
IDRVI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-O.OC
-0.00
NO
2
IORYI
PPMV
-0.00
-0.00
-o.oo
-o.oo
-0.00
-0.00
-0.00
-0.00
ALDEHYDES SMOKE PARTICIPATES
IDRYI
PPMV
46.00
107.00
142.00
145.00
150.00
32. OC
150.00
79.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
52.00
53.00
53.00
53.00
53.00
54.00
53.00
41.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
POWER
PFRCFNT
RATED
T.O.
5
55
78
fll
94
18
MASS EMI
r.n
LB/IK
LP FUEL
6.09
7.14
.67
.54
.49
.19
28.46
KSS FMI
HC
LB/IK
LP FUEL
2.18
0.17
0.08
0.05
0.08
0.41
0.07
14. 19
MASS E.1I
urn
LO/IK
LN FUF.L
-0.00
-o.on
-0.00
-0.00
-3.00
-0.00
-0.00
-0.00
MASS EMI
C07
LB/1K
LH FUEL
3128.97
1140.70
3141.67
3141.96
3141.97
3138.1)2
3142.00
1060. HH
MASS tMI
Nfl
LB/IK
LP FUEL
-0.00
-o.on
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
MASS £11
Nt»
LB/IK
I.B FUEL
B.H5
9.68
10.55
10.47
10.48
4.82
10. 06
3.01
MASS EMI
CO
I.B/HP.
4. )7
3.30
3.25
3.15
3.17
3. OB
3.07
16.28
MASS FMI
nr.
Lfl/HR
1.57
0.26
0.16
0.11
0. 16
0.10
0.16
8.17
MASS EM
HO 2
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
MASS FMI
C02
LB/HR
2246.60
4B49.21
6094.84
6425.31
6686.12
2B49..13
6755.46
I 750.82
MASS EC. I
NO
Lfl/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS tMI
NOX
LR/HR
6.16
14.94
20.47
21.41
22.31
4.37
21.67
1.72
POWER
PERCENT
RATFO
T.O.
5
55
70
83
94
IB
LB/IK IIP-IIU
1 8 . 5 64
1.299
0.90'.
0.416
0.731
1.712
0. 746
171.013
LBMK HP-MR
9515.641
1909.221
1697.255
1667.109
1542.215
1416.234
1641.070
13391.000
THC
LB/IK HP-MS
6.6S.1
0.104
0.044
0.02B
o.nis
0.470
0.036
85.253
NO
LB/IK HP-MR
-0.000
-0.000
-0.000
-0.000
-0.001
-0.000
-0.000
-0.000
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
NO
X
Lfl/lK HP-HR
7.6.974
5.884
5.700
5.555
5.145
5.273
5.252
18.102
IV-28
-------
C»L ID NUMBER: 19 ENGINE TYPE AND MODEL: T56-A15
TEST ORGANIZATION: ALLISON DIVISION
SERIAL NUMBER I BS09
MODE
TAXI-IDLE
TAKEOFF
CLIM60UT
APPROACH
TAXI-IDLE
MODF
TAX-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IOLE
MODE
TAII-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POKER
0.0)0
1.000
0.900
0.300
0.030
FRACTIONAL
POMES
0.0)0
1.000
0.900
0.300
0.0)0
POWER
HP
137.7
4591. 0
4131.9
1377.3
137.7
POKER
HP
137.7
4591.0
4131.9
1377.3
137.7
POWER
HP
137.7
4591.0
4131.9
1377.3
137.7
EMISSION FUEL USAGE TIME IN
RATE RATE NT FACTOR MODE
LB/HR LB/HR MIN.
4.170 463.900 .000 19.00
2.874 2242.194 .000 0.50
2.806 2105.092 .000 2. SO
3.122 1106.494 .000 4.90
4.170 463.900 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.I
EMISSION FUEL USAGE TINE IN
RATE RATE HT FACTOR NODE
LB/HR LB/HR MIN.
6.147 463.900 .000 19.00
0.0 2242.194 .000 0.50
0.001 2105.092 .000 2.50
0.360 1106.484 .000 4.50
6.147 463.900 .000 7.00
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK HP-KR/CVCLEl
LBS POLLUTANT/1000K HP AT T.O. I
EMISSION FUEL USAGE TIME IN
RATE RATE HT FACTOR MODE
LB/HR LB/HR MIN.
1.412 463.900 .000 19.00
23.554 2242.194 .000 0.50
22.167 2105.092 .000 2.50
7.015 1106.484 .000 4.50
1.412 463.900 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CVCLEl
LBS POLLUTANT/IK HP-HR/CYCLE>
LBS POLLUTANT/1000K HP AT T.O.t
CO
MASS
IBS.
1.320
0.024
0.117
0.234
0.486
2.182
5.589
5.643
0.922
' HC
MASS
IBS.
1.946
0.0
0.000
0.027
0.717
2.691
6.892
7.206
0.0
NOX
MASS
LBS.
0.447
0.196
0.924
0.526
0.165
2.258
5.784
6.047
42.754
FUEL
MASS
LBS.
146.90
18.68
87.71
82.99
34.12
390.41
FUEL
MASS
LBS.
146.90
18.68
87. 71
82.99
54.12
390.41
FUEL
MASS
LBS.
146.90
18.68
87.71
82.99
54.12
390.41
LB CO /
IK LB FUEL
8.988
1.282
1.333
2.822
8.988
LB HC /
IK LB FUEL
13.250
0.0
0.001
0.325
13.250
LB NOX/
IK LB FUEL
3.045
10.505
10.530
6.340
3.043
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
LB CO /
HP-HR
0.03027
0.00063
0.00068
0.00227
0.03027
IB HC /
HP-HR
0.04463
0.0
D. 00000
0.00026
0.04463
LB NOX/
HP-HR
0.01026
0.00513
0.00536
0.00309
0.01026
IV-29
-------
DATE: 6/28/71
TEST ORGANIZATION! ALLISON DIVISION
ENCINF SUPPLIFR: ALLISON DIVISION
FNGINE DATA
C»L 10 NUMBER: 20 ENCINF TYPE AND MODEL: T56-A15
RATED HORSEPOHER: 4591.
ENGINE TOTAL TIME: 0. HP5
TIME SINCE HCI SECTION OVERHAUL: 0. MRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. MRS
FIRST STACF NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVFRHAUL: 0. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL: JP-5 FUEL H/C RATIO: \.2
LH/IK
LB FUEL
-0.00
-n.oo
-o.oo
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS FMI
C12
LB/IK
LB FUEL
3129.99
3140.99
3141.51
3129.99
1141.23
1135.41
3141 .45
3115.34
3052.43
MASS EMI
NO
LR/1K
LB FUEL
-0.00
-0.00
-o.nn
-0.00
-n.oo
-o.oo
-n.oo
-o.nn
-n.oo
MASS FMI
NOX
LB/IK
LB FUEL
5.20
8.76
9.21
5.20
12.24
6.56
10.30
4.48
0.77
MASS Ell
cn
LB/HR
5.93
1.24
3.46
6.26
4.2B
4.94
3.95
4.99
16.32
MASS FM
HC
LB/HR
0.3H
o.i/
0.17
0.40
o.ie
0.15
O.IR
0.15
9.4S
MASS EMI
N02
LB/HR
-o.on
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HK
2214.82
4947.06
6188.80
2356.89
6879.29
2809.33
6832.64
2821.81
1709.36
MASS EMI
NU
Lfl/HH
-n.oo
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS EMI
NOX
LB/HR
1.71
13.79
16.15
3.92
26.81
5.87
22.40
4.03
0.43
POWFR
PERCENT
RATED
T.O.
5
93
17
91
If
2
cn
LB/IK HP-HP
27.913
I .245
0.940
24. 152
0.992
6.1 12
n.94n
6.181
171.416
LB/IK HP-MR
10511.812
1893.627
1642.427
9170.758
1594.879
3*77.320
1625.271
3492.766
17955.504
THC
I.B/1K HP-MR
1.803
0.0(,5
n.047
1.573
0.041
0. 185
0.04?
0. 190
99.286
NCI
LB/IK HP-HR
-0.000
-0.000
-n.ono
-n.oon
-o.pno
-o.ooo
-o.ooo
-n.ooo
-n.ono
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
NO
X
LB/IK HP-HR
17.466
5.293
4.933
15.236
6.214
7.270
5.329
4.987
4. 505
IV-30
-------
CAL ID NUMBER) 20 ENGINE TYPE AND MODEL: T56-AI5
TEST ORGANIZATION: ALLISON DIVISION
SERIAL NUMBER! B516
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI- IDLE
TAKEOFF
CLIMB OUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
COMER
0.030
1.000
0.900
0.300
0.030
POWER
HP
137.7
4591.0
4131.9
1377.3
137.7
POWER
HP
137.7
4591.0
4131.9
1377.3
137.7
POWER
HP
137.7
4591.0
4131.9
1377.3
137.7
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR NODE
LB/HR LB/HR MIN.
10.176 612.968 .000 19.00
4.573 2280.831 .000 0.50
3.602 2133.054 .000 2.50
4.281 1138.158 .000 4.50
10.176 612.968 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE)
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/NR MIN.
13.048 612.968 .000 19.00
0.091 2280.831 .000 0.50
0.085 2133.054 .000 2.50
0.052 1138.158 .000 4.50
13.048 612.968 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLEl
LBS POLLUTANT/1000X HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
0.611 612.968 1.000 19.00
28.681 2280.831 1.000 0.50
25.520 2133.054 1.000 2.50
6.487 1138.158 1.000 4.50
0.611 612.968 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
CO
MASS
LBS.
3.222
0.038
0.150
0.321
1.187
4.919
10.720
13.173
0.830
HC
MASS
LBS.
4.132
0.001
0.004
0.004
1.522
5.662
12.340
15.164
0. 166
NOX
MASS
LBS.
0.194
0.239
1.063
0.4B7
0.071
2.054
4.476
5.500
52.061
FUEL
MASS
LBS.
194.11
19.01
88.88
85.36
71.51
458.87
FUEL
MASS
LBS.
194.11
19.01
88.88
85.36
71.51
458.87
FUEL
MASS
LBS.
194.11
19.01
88.88
85.36
71.51
458.87
LB CO /
IK LB FUEL
16.601
2.005
1.669
3.761
16.601
LB HC /
IK LB FUEL
21.287
0.040
0.040
0.046
21.287
LB NOX/
IK LB FUEL
0.997
12.575
11.964
5.700
0.997
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
LB CO /
HP-HR
0.07388
0.00100
0.00087
0.00311
0.07388
LB HC /
HP-HR
0.09474
0.00002
0.00002
0.00004
0.09474
LB NOX/
HP-HR
0.00444
0.00625
0.00618
0.00471
0.00444
IV-31
-------
OtTE: 6/79/71
TEST ORGANIZATION: ALLISON DIVISION
ENGINE SUPPLIER: ALLISON DIVISION
ENGINE DATA *»
CAL 10 NUMBER: 71 ENGINE TYPE AND MUOEL: T56-A15
RATED HORSEPOWER: 4591.
ENGINE TOTAL TIME: 0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
tIMF SINCE:
NI COMPRESSOR OVERHAUL: o. MRS
N2 COMPRESSOR OVFRHAUl: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE C.UIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINF OVERHAUL: 0. HRS
FUEL: JP-S FUEL H/C RATIO: 1.970
OPERATIONAL OAT A «»»«»««.
INLET AIR TEMPFRATUREi DECREES F: START 87.00 FINISH 83.00
ATMOSPHERIC PRESSURE: START 28.70 FINISH 29.00
INLET AIR HUMIDITY, LRS H20/L3 AIR: 0.0140
RELATIVE HUMIDITY: 50.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 154.44, FLOW RA1E, LITERS/MIN:
SAMPLE LINE TRANSPORT TIMF, SEC: 1.00
NUMBER OF TESTS: 11
COMMENTS:
GRFEN RUN
SEOUL NUMBER:
(1MB
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
8.00
-0.00
POWER
PERCENT
RATED
T.O.
5
58
80
86
93
16
92
16
92
2
5
POWER
PERCENT
RATED
T.O.
5
58
80
86
93
16
92
16
92
2
5
POWFR
PERCENT
RATED
T.O.
5
58
80
86
93
16
9?
16
92
2
5
TEST
MODE
?/ n
3/ 2
4/ 3
5/ 4
10/ 5
12/10
6/12
8/ 6
14/ 8
IT/} 4
18/17
F XHAUSI
r.as
TEMP
DEGREES f
-0.00
-o.nn
-0.00
-0.00
-0.00
-o.on
-o.nn
-n.oo
-o.oo
-n.oo
-o.no
MASS EMI
CD
LP/IK
L9 FUEl
.56
.99
.57
.59
. 13
. 94
.66
5.11
1.66
25.60
7.50
co
1. 9 / 1 K
4 .
1 .
0.
0.
1.
5.
0.
5.
0.
150.
23.
POWER ENGINE MFASURED GAS GEN CALC COMPRESSOR ENGINE TURBINE
THRUST, LBS PERCENT SPEED FUEL AIR FLOW E/A DISCHARGE PRESSURE INLET
OR RATED RPM FLOW LB/SEC TEMP RATIO TEMP
SMP T.O. NI N2 LB/HR DFGREFS E EPR DEGRFFS F
215.60 5 13500.00 -0.00 731.00 29.94 0.006800 -0.00 -0.00 1065.00
7671.30 58 13800.00 -0.00 1589.00 29.93 0.014700 -0.00 -0.00 1610.00
3679.50 80 13800.00 -0.00 1980,00 30. no 0.018300 -0.00 -0.00 1850.00
3985.10 86 13800.00 -0.00 2118.00 29.97 0.019600 -0.00 -0.00 1920.00
4769.70 93 13800.00 -0.00 2260.00 29.97 0.020900 -0.00 -0.00 1970.00
765.40 16 13400.00 -0.00 890.00 30.21 O.C08700 -0.00 -0.00 1165.00
4247.80 97 13800.00 -0.00 2241.00 29.97 0.020800 -0.00 -0.00 1970.00
765.40 16 13400.00 -0.00 889.00 30.14 0.005700 -0.00 -0.00 1165.00
4747.80 97 13300. OC -0.00 2258.00 30.04 0.070900 -0.00 -0.00 1970.00
95.20 2 10000.00 -0.00 560.00 20.14 0.007700 -0.00 -0.00 1160.00
735.60 5 13500.00 -0.00 742.00 30.32 0.006800 -0.00 -0.00 1050.00
FXHAUST CO CO THC NO NO NO ALDEHYDES SMUKE PARTICULATES
GAS (DRYI 2 IWETI (DRY) 2 X
PRESSURE PPMV IOKYI PPMV PPMV (DRY! (DRY)
PSI A
-0.00
-n.oo
-0.00
-0.00
-0.00
-C.OO
-0.00
-0.00
-0.00
-o.on
-0.00
MASS EMI
HC
1 B/1K
LB EUFL
0.05
0.10
0.41
0.37
0.25
0.54
0.38
0.54
0. 13
16.54
0.22
IP-Hk
849
17')
947
144
125
747
175
021
892
573
196
PEKCFNT V
59.00 7
34.DO »
34.nO 4
36.00 4
50.00 4
54.00 ?
39.00 4
54.00 2
39.00 4
3b5.nO ?
39.00 1
MASS EMI MASS [Ml
N02 COT.
L9/IK LB/IK
LB FUFL LB FUEL
-'1.00 3141.93
-0.00 3141.13
-n.OO 3140.92
-0.00 3141.01
-0.00 3140.48
-0.00 1135.29
-0.00 3140.87
-0.00 3135.16
-0.00 3141.57
-0.00 3058.93
-0.00 3131.99
CO
7
.55 3.
.43 3.
.32 15.
.53 14.
.70 10.
.18 10.
.70 15.
.15 in.
.70 5.
.70 190.
.55 3.
MASS F»l
NO
LR/1K
LB FUEL
-n.no
-0.00
-0.00
-o.on
-o.on
-n.on
-n.on
-o.oo
-0.01
-o.oo
-o.no
THC
LB/IK HP-HR LJ/1K HP-HR
9748.52'
1868.473
1690.637
1669.385
1662.293
3645.695
1657.020
3641 .440
1669.961
1 7993.715
9863.898
0. 152
0.062
0.273
0. 196
0.135
0.623
0.202
0.630
0.068
07.792
0.707
00 -0.00
oo -o.no
00 -0.00
00 -0.00
00 -0.00
oo -o.on
00 -0.00
00 -C.OO
00 -0.00
00 -0.00
00 -0.00
MASS E»l PASS
NOX CO
PPMV PPMV
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
EMI
LB/IK LB/HK
IB FUEL
1.74 I.
6.51 3.
fl.66 3.
8.41 3.
8.?4
6.01
7.96
5.79
7.83
3.55 1 .
2.96 5.
LB/IK HP-HR
-o.non
-0.000
-0.000
-o.ooo
-o.noo
-0.000
-0.000
-0.000
-0.000
-o.ono
-0.000
14
15
12
36
81
40
72
46
75
33
63
00 40.
00 68.
On 114.
00 116.
00 118.
00 40.
00 114.
00 38.
00 112.
00 30.
00 14.
MASS EMI
HC
LB/HH
0.04
0.16
O.B2
0.78
0.58
0.48
0.86
0.48
0.79
9.76
0.17
NO
2
00 -0
00 -0
oo -o
00 -0
00 -0
00 -0
00 -0
00 -0
00 -0
00 -0
00 -0
MASS EMI
NO 7
LB/HR
-0.00
-0.00
-0.00
-o.on
-0.00
-0.00
-o.no
-0.00
-0.00
-0.00
-0.00
.00 52
.00 54
.00 55
.on 56
.00 56
.00 54
.00 56
.00 54
.00 56
.00 42
.00 52
MASS EMI
C02
LB/HR
2296.75
4991.25
6219.01
6652.66
7097.49
2790.41
7038.68
2787.16
7093.66
1713.00
7323.93
NO
X
.00 -0.00
.on -o.oo
.00 -0.00
.00 -o.oo
.00 -o.oo
.00 -0.00
.00 -o.on
.00 -0.00
.no -o.oo
.00 -0.00
.00 -0.00
MASS F»l MASS
EMI
NO NOX
LB/HR LB/HR
-0.00 1
-0.00 10
-o.on 17
-0.00 17
-0.00 IB
-0.00 5
-0.00 17
-0.00 i
-0.00 17
-0.00 1
-0.00 2
.77
.34
.16
.81
.63
.35
.85
.15
.67
.99
.19
LB/IK HP-HR LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-o.ooo
-O.OOD
-0.000
-0.000
.399
.872
.644
.469
.363
.993
.202
.728
4.160
20.901
9.314
IV-32
-------
CAL 10 NUMBER: 21 ENGINE TYPE AND MODEL: T56-A15
TEST ORGANIZATION: ALLISON DIVISION
SERIAL NUMBER! 8518
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
HOOF
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MOOF
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
I. 000
0.900
0.300
0.030
POWER
HP
137.7
4591.0
4131.9
1377.)
1)7.7
POKER
HP
137.7
4591. 0
4131.9
1377.3
137.7
POWER
HP
137.7
4591.0
4131.9
1)77.3
137.7
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR NODE
LB/HR LB/HR MIN.
7.255 246.359 .000 19.00
3.981 2428.12! .000 0.50
3.320 2193.454 .000 2.50
3.750 1128.447 .000 4.50
7.255 246.359 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CTCLE:
LBS POLLUTANT/100011 HP AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR NODE
LB/HR LB/HR MIN.
4.540 246.359 1.000 19.00
0.756 2428.125 1.000 0.50
0.611 2193.454 1.000 2.50
0.361 1128.447 1. 000 4.50
4.540 246.359 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
0.390 246. )59 .000 19.00
21.488 2428.125 .000 0.50
18.556 2193.454 .000 2.50
4.875 1128.447 .000 4.50
0.390 246.359 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HD/CVCLE:
LBS POLLUTANT/1000K HP AT T.O.:
CO
MASS
LBS.
2.297
0.03)
0.1)8
0.281
0.846
3.596
11.869
9.632
0.72)
HC
MASS
LBS.
1.438
0.006
0.025
0.027
0.530
2.026
6.687
5.426
1.372
NOX
MASS
LBS.
0.124
0.179
0.773
0.366
0.046
1.487
4.907
3.982
39.004
FUEL
MASS
LBS.
78.01
20.23
91.39
84.63
28.74
)0).02
FUEL
MASS
LBS.
78.01
20.23
91.39
84.63
29.74
303.02
FUEL
MASS
IBS.
78.01
20.23
91.39
84.6)
28.74
303.02
LB CO /
IK LB FUEL
29.44B
1.640
1.514
3.32)
29.448
LB HC /
IK LB FUEL
18.429
0.311
0.278
0.320
18.424
LB NOX/
IK LB FUEL
1.585
8.850
8.460
4.120
1.585
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
371.40
ENERGY
HP-HR
43.61
'38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
10J.30
16.07
3TJ.40
LB CO /
HP-HR
0.05267
0.00087
0.00080
0.00272
0.05267
LB HC /
HP-HR
0.03296
0.00016
0.00015
0.00026
0.0)296
LB NOX/
HP-HR
0.00283
0.00468
0.00449
0.00354
0.00283
IV-33
-------
DATE: 6/25/71
TEST ORGANIZATION: ALLISON DIVISION
ENGINE SUPPLIER: ALLISON nlvISION
ENGINE DATA
CAL 10 NUMBER:
22 ENGINE TYPE ANO MUDEL : T56-A15
RATED HORSEPOWER: 4591.
ENGINE TOTAL TIME: 0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: o. MRS
N2 C01PRFSSOP OVERHAUL: 0. HRS
C.OMBUSTUR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVFRHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL: JP-5 FUEL H/C RATIO: 1.970
OPERATIONAL DATA .«««««««..«..«««.««..««...«................
INLET AIR TEMPERATURE, DEGREES F: START 90.00 FINISH
ATMOSPHERIC PRESSURE: START 2H.60 FINISH
INLET AIR HUMIDITY, LflS H20/LB AIR: 0.0155
RFLATIVE HUMlnllY: 49.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGRFES C: 154.44, FLOW RATE, LITFRS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 10
COMMENTS:
GREEN RUN
SERIAL NUMBER:
8512
98.00
29.00
CLOCK
TIME
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWF.P
PERCENT
RATED
T.n.
5
55
76
5
86
17
R6
17
86
2
PO»ER
PERCENT
RATER
T.O.
5
55
76
5
86
17
B6
17
R6
2
POWER
PERCENT
RATED
T.O.
5
55
76
5
R6
17
86
17
86
2
TFST
MODE
2/ 0
I/ 2
4/ 1
in/ 4
IO/IR
12/10
6/12
fl/ 6
14/ R
17/14
EXHAUST
GAS
TEMP
DEGOFFS <=
-0.00
-0.00
-0.00
-0.00
-0.00
-c.on
-0.00
-0.00
-0.00
-o.oo
MASS E-ll
r.o
LK/K
L« FIIFL
9. M
2.21
1. 74
8.49
1.S8
3.79
I.8B
5.49
1.79
27 .94
en
i3/i<
29.
i .
0.
25.
0.
4.
0.
6.
0.
162.
POWER ENGINE MEASURED GAS GEN CALC COMPRESSOR ENGINE TURBINE
THRUST, LBS PERCENT SPEED FUEL AIRFLOW F/A DISCHARGE PRESSURE INLET
OR RATED RPM FLOW LR/SEC TEMP RATIO TEMP
SHP T.O. NI N2 L3/HR DEGREES f EPR DEGREES F
215.60 5 13500.00 -0.00 714.00 29.62 0.006700 -0.00 -0.00 1040.00
2519.90 55 13800.00 -0.00 1510.00 29.35 0.014500 -0.00 -0.00 1610.00
3501.30 76 11BOO.OO -0.00 1900.00 29.11 0.018000 -0.00 -0.00 1850.00
2)5.60 5 11500.00 -0.00 712.00 29.42 0.006700 -0.00 -0.00 10BO.OO
3985.10 86 13800. 00 -0.00 2110.00 29.17 0.020100 -0.00 -0.00 1970.00
807.90 17 13400.00 -0.00 881.00 29.42 0.008300 -0.00 -0.00 1205.00
19B5.10 U6 11800.00 -0.00 2110.00 29.17 0.020100 -0.00 -0.00 1970.00
786.60 17 13400.00 -0.00 672.00 29.42 0.008200 -0.00 -0.00 1205.00
39B5.10 86 11BOO.OO -0.00 2110.00 29.17 0.020100 -0.00 -0.00 1970.00
95.20 2 10000.00 -0.00 554.00 20.09 0.007700 -0.00 -0.00 1200.00
FKHAUST CO CO THC NU NO NP ALDEHYDES SHOKE PARTICULARS
GAS IORY1 2 (HET1 (DRY) 2 X
PWFSSURE PPMV (DRY) PPMV PPKV (DRYI IDRYl
PSI A
-o.no
-o.oc
-O.OT
-0. 00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
MASS F.MI
HC
LH/IK
Lfl FUEL
0.26
0. 12
0.10
0.02
O.OB
0.12
0.09
n. 1 7
0.03
1 4.31
HP-HH
501
351
'(41
644
)9fl
118
995
OBI
J49
585-
PERCENT V
(.6.00
34.00
32.00
66.00
41.00
57.00
19.00
55.00
39.00
380.00
MASS t«l MASS F.MI
NIJ2 C02
L-V1K Lfl/IK
LR FUFL Lfl FUEL
-0.00 3128.53
-0.00 3140.68
-0.00 1141.53
-0.00 1131.13
-0.00 3141. (4
-0.00 1138.24
-0.00 3141.14
-0.00 3135.42
-0.00 3141.48
-0.00 3061.37
CO
2
1.15 1
3.03 J
1.68 3
1.55 0
4.15 1
3.00 3
4. 15 3
2.00 1
4.15 1
2.65 311
.WASS EMI
NT
LB/1K
LB FIIFL
-0.00
-n.OO
-0.00
-0.00
-C.OO
-0.00
-C.OO
-0.00
-0.00
-C.OO
THC
LB/IK HP-MR LB/IK HP-MR
9411 . I R8
1891 .901
1703.794
9462.492
1663.251
3422.191
1661.250
3475.831
1663. 127
17B15. I4B
0.77H
0.070
0.052
0.068
0.044
0.128
0.046
0. 194
0.044
B3.258
PPMV PPMV
.00 -0.00 -0
.00 -O.CO -0
.00 -0.00 -0
.30 -o.on -o
.00 -0.00 -0
.00 -0.00 -0
.00 -0.00 -0
.00 -0.00 -0
.00 -0.00 -0
.00 -0.00 -0
MASS FH1 MASS EMI
NO* en
LB/1K LB/H"
LI FUEL
8.96 6.95
9.86 3.43
12.12 3.30
3. HO 6.04
8.00 3.9»
1.50 3.34
10.29 3.96
6.riR 4.79
6.64 3.FR
2.17 15.48
NO
LB/IK HP-MR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
.00 17.00 -0
.00 91.00 -0
.00 13B.OO -0
.00 IB. 00 -0
.OH 106.00 -0
.00 32.00 -0
.00 110.00 -0
.00 42.00 -0
.00 SB. 00 -0
.00 18.00 -0
MASS FMI MASS EMI
HC NH2
LB/HR LR/HR
0.16 -0.00
0.18 -0.00
0.18 -0.00
0.02 -0.00
0.17 -0.00
0.10 -0.00
O.lfl -0.00
0.15 -0.00
0.17 -0.00
7.93 -0.00
N'l
2
.00 50
.00 54
.00 54
.00 50
.00 57
.00 55
.00 57
.00 55
.00 57
.00 43
MASS FMI
CU2
LB/HR
2231.77
4805.24
5968.90
2229.36
6628.22
2744.79
6623.21
2714.09
6628.52
1696.00
NO
X
.00 -O.CO
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -o.oo
.00 -C.OO
.00 -0.00
.00 -0.00
.00 -o.oo
MASS FHI MASS EMI
NO NOX
LB/HR LB/HR
-0.00 6.40
-0.00 15.09
-0.00 23.40
-0.00 2.71
-0.00 16.88
-0.00 3. OB
-0.00 21.71
-0.00 6.00
-0.00 14.02
-0.00 1.20
LB/IK HP-Hit LH/IK HO-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-o.ooo
27.165
5.940
6.679
11.488
4.237
1.816
5.447
7.631
1.518
12.650
IV-34
-------
CM. 10 NUMBER: 22 ENGINE TYPE AND MODEL: 156-Ais
TEST ORGANISATION: ALLISON DIVISION
SERIAL NUMBER! 8512
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CUMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
POWER
HP
137.7
4591.0
4131.9
1377.3
137.7
POWER
HP
137.7
4591.0
4131.9
1377.3
137.7
POWER
HP
137.7
4591.0
4131.9
1377.3
137.7
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
13.859 524.126 .000 19.00
5.242 2400.930 .000 0.50
4.162 2198.315 .000 2.50
4.465 1166. BIS .000 4. JO
11.859 524.128 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK HP-HR/CVCLE:
LBS POLLUTANT/1000K HP AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
13.812 524.128 .000 19.00
0.071 2400.930 .000 0.50
0.079 2198.515 .000 2.50
0.138 1166.815 .000 4.50
13.812 524. 12B .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
0.414 524.128 .000 19.00
30.582 2400.930 .000 0.50
26.629 2198.515 .000 2.50
6.709 1166.815 .000 4.50
0.414 524.128 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/IOOOK HP AT T.O.:
CO
MASS
LBS.
4.389
0.044
0.173
0.335
1.617
6.558
15.385
17.562
0.951
HC
MASS
LBS.
4.374
0.001
0.003
0.010
1.611
5.999
14.075
16.067
0.130
NOX
MASS
LBS.
0.131
0.255
1.110
0.503
0.048
2.047
4.802
5.482
55.510
FUEL
MASS
LBS.
165.97
20.01
91.60
87.51
61.15
426.25
FUEL
MASS
LBS.
165.97
20.01
91.60
87.51
61.15
426.25
FUEL
MASS
LBS.
165.97
20.01
91.60
87.51
61.15
426.25
LB CO /
IK LB FUEL
26.442
2.1B3
1.893
3.827
26.442
LB HC /
IK LB FUEL
26.352
0.030
0.036
0.118
26.352
LB NOX/
IK LB FUEL
0.790
12.737
12.112
5.750
0.790
ENERGY
HP-HR
43.61
38.26
172.16
103.10
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
41.61
38.26
172.16
103.10
16.07
373.40
LB CO /
MP-HR
0.10063
0.00114
0.00101
0.00324
0.10063
LB HC /
HP-HR
0.10028
0.00002
0.00002
0.00010
0.10028
LB NOX/
HP-HR
0.00301
0.00666
0.00644
0.00487
0.00301
IV-35
-------
DATE: 6/25/71
TFST ORGANIZATION: ALLISON DIVISION
FNGINE SUPPLIFR: ALL I SON DlVISION
ENGINE DATA
CAL in NUMBER:
2)
ENGINE TYPF AND MCIDEL: T56-A15
RATED HORSEPOWER: 4591.
FNGINE TOTAL TIME: 0. HRS
TIME SINCE MOT SFCTION OVERHAUL:
TIME SINCE:
SERIAL NUMBFB:
0. HRS
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL I 0. HRS
COMRUSTOR CAN REPLACEMENT: 0. HRS
FRST STAGE NCI/ZLF GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVFRHAULl 0. HRS
N? TURBINE HVFRHAUL: 0. HRS
FUEL: JP-5 FUEL H/C RATIO: I.970
OPFRATIONAL DATA «««««»«»««««
INLFT SIR TFMPEKATUBE, DEGREES F: START 96.00 FINISH
ATMOSPHERIC PRESSURE: START 28.50 FINISH
INLET AIR HUMIDITY, LBS H20/L" AIR: 0.0161
RFLAMVE HUMIOITY: 44.00 PERCENT
SAMPLE LINE: TEMPERATURE, OFGRFFS C: 154.44, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 10
COMMENTS:
GREEN DUN
97.00
26.80
B513
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
POWER
PERCENT
RATED
T.n.
4
52
73
57
83
16
83
1 8
1
4
POWER
PERCENT
RATED
T.n.
,.
52
73
57
83
18
83
18
1
4
pnwER
PERCENT
RATED
T.O.
4
52
73
57
63
18
B3
18
1
4
TFST POWFR ENGINE MEASUREO GAS GEN CALC COMPRESSOR ENGINE TURBINE
MIJOE THKUST.LBS PERCENT SPEED FUEL AIH FLOW F/A DISCHARGE PRESSURE INLET
IIP RATED RPM FLOW LB/SEC TEMP RATIO TEMP
SHP I.u. N] N2 LB/HR DEGREES f FPR DEGREES F
?/ 0 214.20 4 13500.00 -0.00 706.00 29.39 0.006700 -0.00 -0.00 1070.00
3/ 2 2408.60 5? 13800.00 -0.00 1490.00 79.01 0.014300 -0.00 -0.00 1610.00
4/ 3 3372.00 73 13800.00 -0.00 1662.00 28.87 0.179000 -0.00 -O.OO 1850.00
5/ 4 .J656.60 57 13800.00 -0.00 1977.00 28.67 0.019000 -0.00 -0.00 1970.00
10/ 5 3653.70 H3 11800. OC -0.00 2074.00 26.67 0.020000 -0.00 -0.00 1970.00
17/10 679.20 18 13400.00 -0.00 896.00 79.04 0.008600 -0.00 -0.00 1730.00
0/1? 1653.70 83 13800.00 -0.00 2072.00 26.30 0.020000 -0.00 -0.00 1970.00
8/ !. 829.20 18 13400.00 -0.00 902.00 29.08 0.006600 -0.00 -0.00 1235.00
17/ 1 611.50 1 10000.00 -0.00 564.00 20.08 0.007800 -0.00 -0.00 1210.00
13/17 214.20 4 11500.00 -O.Orl 711.00 29.02 0.006800 -0.00 -0.00 1070.00
FKMAUS! FHHAUST CO CO THC NO NO NO ALOF.HYDES SMOKE PART ICUL ATES
GAS Gas (OPVI 2 (WF7) (DRY| 2 X
(FMO PRESSURE PP"V ICRYl PPMV PPMV (DRY! IDRYI
OFGHFES F
-C.0'1
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI M
CD
LX/IK
IP FUEL 1
(>. 90
2.59
. 73
.69
.81
. 89
. 76
.39
? . 19
1.74
r.u
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
SS FMI
I'C
LI/IK
H FUEL
0.2?
0. 11
0. 09
0.6?
0.27
1 .01
0.51
0.67
14.50
0.22
LB/IK HP-HR
72.799
1.600
0.054
1.257
0.976
5.285
0.944
5.122
234.476
12.430
PERCENT V
55.00
40.00
35.00
36.00
40.00
51 .00
39.00
51 .00
375.00
30.00
1ASS F.MI MASS Ml
ND2 cm
L3/1K LB/IK
1.3 FUEL L6 FUEL
0.0 3 1 3 3 . 1)9
0.0 3140.15
0.0 3141.57
0.0 3140.18
0.0 3140.93
0.0 3114.07
T.O 3140.16
0.0 3I34.')9
0.0 1063.28
0.0 3138.05
CO
2
1.59 3
3.09 3
4.05 3
4.26 22
4.41 10
2.08 13
4.44 19
7.08 12
2.77 350
1.60 3
MASS FMI
Nn
Ln/u
LB FUEL
o.o
o.o
o.o
o.o
0.0
0.0
0.0
0.0
0.0
0.0
TMC
L«/IK HP-HR Lfl/lK MP-HR
10355.859
1942.547
1734.755
2336.872
1690.399
1136. 551
I6«ri.463
3410.279
27207.699
10416.199
0.723
0.071
0.049
0.458
0. 146
1.090
0.275
0.732
128. 776
0.723
.00
.00
.00
.00
.00
.00
.00
.00
.00
.00
MASS [MI
NOX
Lfl/lK
1 B FUEL
4.31
2.23
7.22
10. 17
10.35
4.68
9.09
5.83
2.66
5.74
0
0
0
0
0
0
0
0
0
0
PPMV PPMV
.0 0
.0 0
.0 13
.0 0
.0 0
.n o
.0 0
.0 0
.0 1
.0 o
MASS EMI
en
LP/HR
.88
.35
.22
.34
.76
.38
1.64
4.41
14.89
2.66
NO
LB/IK
0
0
0
0
0
0
0
0
0
0
HP-HR
.0
.0
.0
.0
. 0
.0
.0
.0
.0
.0
.0 21
.0 21
. 0 89
.0 132
.0 139
.0 31
.0 123
.0 37
.0 23
.0 28
MASS E«l
HC
LB/HK
0.15
0.17
0.16
1.22
0.56
0.90
1.06
0.61
8.18
0.15
NC
2
.00 -0.00 5?
.00 -0.00 52
.00 -0.00 56
.00 -0.00 55
.00 -0.00 55
.00 -0.00 56
.00 -0.00 55
.00 -0.00 56
.00 -0.00 44
.00 -0.00 52
MASS FMI MASS FMI
N02 C02
LP./HR LB/HB
0.0 2218.23
0.0 467rt.82
0.0 SH49.S9
0.0 6208.13
0.0 6514.29
0.0 2806.13
0.0 6506.83
0.0 2B27.76
0.0 1727.69
0.0 7231.15
NO
X
.00 -o.oo
.00 -0.00
.00 -0.00
.00 -0.00
.no -o.oo
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
MASS FMI MASS
EMI
NO NQX
LB/HK LB/HR
0.0 3
0.0 3
0.0 13
0.0 70
0.0 21
0.0 4
0.0 16
0.0 5
0.0 1
0.0 4
.00
.32
. 44
.11
.46
.36
.84
.26
.50
.06
LI/IK HP-HR Lfl/lK HP-HR
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
14.299
1.3(10
3.985
7.570
5.570
5.276
4. BIO
6.342
23.617
19.056
IV-36
-------
CtL 10 NUMBERI 23 ENGINE TYPE AND MODEL 1 156-115
TEST ORGANISATION: ALLISON DIVISION
SERIAL NUMBER: esi3
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
POKER
HP
13T.
4591.
4131.
U77.
13T.
7
0
9
3
T
EMISSION FUEL
RATE RATE
LB/HR LB/HR
5.426 628.713
6.136 2740.564
5.139 2468.112
4.7S4 1152.463
S.426 628.715
USAGE
WT FACTOR
.000
.000
.000
.000
.000
TIME IN
MODE
MIN.
19.00
0.50
2. SO
4.50
7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK IB FUEL/CYCLE!
LBS POLLUTANT/IK HP-KR/CYCLE:
LBS POLLUTANT/ 1000K HP AT T.O.:
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.030
1.000
0.900
0.300
0.030
POWER
HP
137.
4S9I.
4131.
1377.
137.
7
0
9
3
7
EMISSION FUEL
RATE RATE
LB/HR LB/HR
7.138 62B.715
1.146 2740.584
1.060 2468.112
0.909 1152.463
7.138 628. TIS
USAGE
MT FACTOR
.000
.000
.000
.000
.000
TINE IN
MODE
MIN.
19.00
O.SO
2. SO
4.50
T.OO
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE 1
LBS POLLUTANT/IK HP-HR/CYCLE:
L8S POLLUTANT/1000K HP AT T.O.:
MODE
FRACTIONAL
POWER
TAXI-IDLE 0.030
TAKEOFF 1.000
CLIMBOUT 0.400
APPROACH 0.300
TAXI-IDLE 0.030
POWER
HP
137.
4591.
4131.
1377.
137.
7
0
9
3
7
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.698 628. 715
30.009 2740.584
25.767 2468.112
6.562 1152.463
1.698 628.715
USAGE
NT FACTOR
.000
.000
.000
.000
.000
TINE IN
MODE
MIN.
19.00
0.50
2.50
4. SO
T.OO
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLEl
LBS POLLUTANT/IK HP-HR/CVCLE:
LBS POLLUTANT/1000K HP AT T.O.:
CO
MASS
IBS.
1.718
O.OSI
0.214
0.357
0.633
2.973
6.116
7.962
1.114
' HC
MASS
LBS.
2.261
0.010
0.044
0.068
0.811
3.215
6.636
8.611
2.081
NOX
MASS
LBS.
0.538
0.250
1.074
0.492
0.198
2. SSI
5.266
6.833
54.471
FUEL
MASS
LBS.
199.09
22.84
102.84
86.43
73.35
484.55
FUEL
MASS
LBS.
199.09
22.84
102.84
86.43
71.35
484. 55
FUEL
MASS
LBS.
199.09
22.84
102.84
86.43
73.35
484.55
LB CO /
IK LB FUEL
8.630
2.239
2.082
4.125
8.630
LB HC /
IK LB FUEL
11.354
0.418
0.430
0.789
11.354
LB NOX/
IK LB FUEL
2.700
10.950
10.440
5.694
2.700
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
101.10
16.07
371.40
LB CO /
HP-HR
0.03939
0.00134
0.00124
0.0034S
0.03939
LB HC /
HP-HR
0.05195
0.00025
0.00026
0.00066
0.05183
LB NOX/
HP-HR
0.0123)
0.00654
0.00624
0.00476
0.01233
IV-37
-------
DUE: 6/24/71
TEST o«GANi2A7in,N: ALLISON DIVISION
ENGINE SUPPLIER: ALLISON DIVISION
ENGINE DAT* *........,......
CAL in NUMBER: 24 ENGINE TVPE AND MODEL: T56-A15
RATED HORSEPOWER: 4591.
ENGINE TOTAL TIME: 0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: o. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
CDMBusTnR CAN REPLACEMENT: o. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. MRS
N2 IURBINE OVERHAUL: 0. HRS
FUEL: JP-5 FUEL H/C RATIO: 1.970
OPERATIONAL DATA »«*«
INLET AIP TEMPERATURE, DEGREES F: START 8ft.00 FINISH 94.00
ATMOSPHERIC PRESSURE: START 28.90 FINISH 29.00
INLET AIR HUMIDITY, L9S H20/LB AIR: 0.0110
RELATIVE HUMIDITY: 48.00 PERCENT
SAMPLE LINF: TEMPERATURE. OEGREES C: 154.44, FLOU RATE, LITERS/nlN:
SAMPLE LINF TRANSPORT TIME, SEC: 1.00
NUMBFR OF TESTS: 11
COMMENTS:
GREEN RUN
SERIAL NUMBER:
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
-0.00
-1.00
-0.00
-o.oo
-0.00
-0.00
-0.00
pnxEo
PERCENT
RATED
T.O.
5
55
77
12
87
1 1
87
18
87
2
s
POWFR
PERCENT
RATED
r.n.
5
55
77
82
87
17
87
18
87
2
5
POWER
PERCENT
RATED
T.O.
5
55
77
B2
87
17
87
IS
17
2
5
TFST
MODE
?/ 0
I/ 2
4/ 3
5/ 4
10/ 5
17/10
6/12
8/ 6
I4/ 8
17/14
IB/ 17
FXHAUSI
GAS
TEMP
OEGOF[S F
-P. on
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS E"l
r.n
i n/u
LB CUFL
7.69
2. 78
1.51
1.25
1.29
1.91
1.27
1.99
1.11
19.72
9.28
POKE" ENGINE
THRUST, LRS
OR
SHP
235.60
7539.90
1547.20
1B09.90
4028.90
607.90
4028.90
829.20
4028.90
95.20
735.60
E XHAIIST
GAS
PPFSSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS FMI
HC
I B/U
LB FUEL
0.25
0.12
0.08
0.08
0.07
0.15
0.07
0.15
0.07
17.74
0.29
Cll
LB/IK
21.
1.
0.
0.
0.
4.
0.
4.
0.
121.
43.
PERCENT SPEFD
RATED
r.n. NI
5 11500.00
55 11800.00
77 I38CO.OO
82 13100.00
87 13800.00
17 134CO.OO
87 13800.00
IB 1.1400.00
87 13800.00
2 10000.00
5 13500.00
CO
IORYI
RPM
N2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
co
2 1
PPMV (OR>1
MEASURED
FUEL
FLOW
LB/HR
726.00
1570.00
1950.00
2065.00
2150.00
892.00
2150. 00
896.00
2150.00
586. CO
1 100.00
THC NH
METI IORY
GAS GEN
AIR ELOU
LB/SEC
CALC COMPRESSOR ENGINC
F/A DISCHARGE PRESSURE
TEMP
RATIO
OFGREES F EPR
1
PPMV PPMV
PERCENT V
54.00
14.00
32.00
10.00
32.00
46. CO
30.00
46.00
79.00
370.00
55.00
MASS EMI MASS EMI
102 C02
LO/1K LB/1B.
LB FUEL Lfl FUFL
-1.00 1111.77
-0.00 1140.62
-0.00 3141.91
-0.00 3142.35
-0.00 3142.31
-0.00 3117.97
-0.00 3147.41
-0.00 3117.81
-0.00 3142.46
-0.00 1078.59
-0.00 3129.14
CO
2
1.40
2.98
4.23
4.79
4.98
2.35
4.93
2.10
4.90
3.00 0.
4.00 0.
3.00 0.
1.00 0.
1.00 0.
3.00 0.
3.00 0.
1.00 0.
3.00 0.
1.18 150.00 0.
1.18
»ASS EMI
Nn
LB/IK
Lfl FUEL
0.0
0.0
o.o
0.0
0.0
o.o
0.0
0.0
0.0
0.0
0.0
IMC
HP-HR LB/IK HP-HR LB/IK HP-HR
691
410
112
679
686
JI6
649
116
632
166
140
9650.520
1941. J22
1727.202
1703.101
1676.874
1444.625
16(6.930
3190.614
1676.958
19950.141
14609.771
0.764
0.071
O.O47
0.041
0.039
0.165
0.019
0.165
0.039
. 78.431
1.370
1.00 0.
MASS FMI
NOX
LB/IK
LB FUEL
5.61
7.49
8.31
7.82
7.06
4.47
7.40
4.85
6. 84
7.02
10.51
Nn
n
0
0
0
0
0
0
0
0
0
0
70.09
29.76
29.59
29.45
79.38
29.65
29.38
29.65
79.38
20.16
79.65
NO
7
IDRYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
0.006700
0.014700
0.018100
0.019500
0.020300
0. 008400
0.020300
O.OPB400
0.070300
O.C08100
0.010300
NO
X
(ORYI
PPMV
24.00
68.00
107.00
1 14.00
107.00
32.00
1 11.00
14.00
102.00
20.00
38.00
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
00 -0.00
00 -0.00
oo -o.oo
00 -0.00
00 -O.OC
00 -0.00
00 -0.00
00 -0.00
00 -0.00
00 -0.00
00 -0.00
TURBINE
INLET
TEMP
DEGREES F
1070.00
1610.00
1850.00
1920.00
1970.00
1200.00
1970.00
1200.00
1970.00
1140.00
1075.00
ALDEHYDES SMOKF P4RTICULATFS
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
MASS EMI MASS EMI MASS F»l
en
LH/HR
5.58
1.58
2.95
2.59
2.76
1.49
2.62
1.58
2.54
1 1.55
10.21
MC 102
LB/HR LB/HH
0.16 -0.
0.19 -0.
0.10 -0.
0. 6 -0.
0. 6 -0.
0. 3 -0.
0. 6 -0.
0. 4 -0.
0. 6 -0.
7.47 -0.
0.32 -0.
NO
2
LB/IK HP-HR LB/IK HP-HR
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0
0
0
0
0
0
0
0
0
0
0
-0.000
-0.000
-0.000
-o.ooo
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
00
00
00
00
00
00
00
00
00
00
00
0 51.00
0 58.00
0 56.00
0 57.00
0 56.00
0 54.00
0 56.00
0 54.00
0 56.00
0 42.00
0 52.00
MASS FMI MASS EMI
CO 2 NO
Lfl/HR LB/t-P
2271.66 0.0
4930.76 0.0
6126.73 0.0
6488.95 0.0
6755.96 0.0
2799.07 0.0
6756.11 0.0
2311.50 0.0
6756.79 0.0
1804.05 0.0
3442.05 0.0
NO
X
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS Ml
NOX
LB/HR
4.07
1 1.76
16.20
16. 14
15.17
3.98
15.90
4.34
14.70
1. 19
11.59
L3/1K HP-HR
17.295
4.611
4.567
4.238
3.766
4.932
1.947
5.240
3.649
12.459
49.184
IV-38
-------
CAL ID NUMBER: 24 ENGINE TYPE »ND MOOELI rs6-»is
TEST ORGANIZATION: ALLISON DIVISION
SERIAL NUMBER I 891T
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAII-IOLE
NODE
TAII-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAII-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIM80UT
APPROACH
TAII-IOLE
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POKER
0.030
1.000
0.900
0.300
0.030
POWER
HP
137.7
4991.0
4131.9
1377.3
137.7
POKER
HP
137.7
4591.0
4131.9
1377.3
137.7
POWER
HP
137.7
4991.0
4131.9
1377.3
137.7
EMISSION FUEL USAGE TINE IN
RATE RATE WT FACTOR NODE
IB/MR LB/HR NIN.
8.492 379.608 .000 19.00
1.631 2394.919 .000 O.JO
2.269 2209.268 .000 2.90
3.876 1194.689 .000 4.90
8.492 379.608 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
4.476 379.608 .000 19.00
0.0 2394.919 .000 0.90
0.032 2209.268 .000 2.90
0.161 1194.689 .000 4.90
4.476 379.608 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE!
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.I
EMISSION FUEL USAGE TINE IN
RATE RATE WT FACTOR NODE
LB/HR LB/HR MIN.
0.777 379.608 .000 19.00
19.712 2394.919 .000 0.90
18.118 2209.268 .000 2.90
6.666 1194.689 .000 4.90
0.777 379.608 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CVCLE:
LBS POLLUTANT/1000K HP AT T.O.:
CO
MASS
LBS.
2.689
0.014
0.099
0.291
0.991
4.079
11.238
10.923
0.296
HC
MASS
LBS.
1.417
0.0
0.001
0.012
0.922
1.993
9.381
9.230
0.0
NOX
MASS
LBS.
0.246
0.164
0.799
0.900
0.091
1.796
4.838
4.703
39.780
FUEL
MASS
LBS.
120.21
19.96
91.89
86.60
44.29
362.94
FUEL
MASS
IBS.
120.21
19.96
91.89
86.60
44.29
362.94
FUEL
MASS
LBS.
120.21
19.96
91.89
86.60
44.29
362.94
LB CO /
IK LB FUEL
22.371
0.681
1.029
3.396
22.371
LB HC /
IK LB FUEL
11.791
0.0
0.019
0.139
11.791
LB NOX/
IK LB FUEL
2.048
8.231
8.216
9.773
2.048
ENERGY
HP- MR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
LB CO /
HP-HR
0.06166
0.00036
0.00099
0.00281
0.06166
LB HC /
HP-HR
0.03290
0.0
0.00001
0.00012
0.03290
LB NOX/
HP-HR
0.00964
0.00429
0.00438
0.00484
0.00964
IV-39
-------
DATE! 6/19/71
TEST ORGANIZATION: ALLISON DIVISION
ENGINE SUPPLIER: ALLISON DIVISION
ENGINE DATA »«*««»«
CAL 10 NUMBER: 25 ENGINE TYPE AND MODEL: T56-A15
RATED HORSEPOWER: 4591.
FNGINE TOTAL TIME: 0. HRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIHF SINCF:
NI COMPRESSOB OVERHAUL: o. HRS
N2 COMPRESSOR OVERHAUL: o. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZlt GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVFRHAUL: o. HRS
FUEL: JP-5 FUEL H/C RATIO: 1.970
OPERATIONAL DATA «««««««»«.«
INLET AIR TFMPFKAIUREi DEGREES F: START 79.00 FINISH 88.00
ATMOSPHERIC PRESSURE: START 29.80 FINISH 29.00
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0094
RELATIVE HUMIDITY: o.oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 154.**, FLDB RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: I.00
NUMBER OF TESTS: 6
COMMFNTS:
FINAL RUN
SERIAL NUMBER:
CLOCK
TIME
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.00
TEST
MODE
I/ 0
?/ I
»/ 2
5/ 1
6/ 5
7/ 6
THRUST
OR
SHP
257.
2671.
3853.
4247.
1157.
7B6.
POWER
,LflS
00
30
70
80
20
70
PERCENT
RATED
T.O.
5
58
H3
92
25
17
Nl
13500.
13800.
11800.
13800.
14300.
13400.
ENGINE
SPEED
RPM
00
00
00
00
00
00
N2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MEASURED
FUEL
FLOW
LB/HR
737.00
1572.00
I960.00
2190.00
1080.00
916.00
GAS GEN
AIR FLOW
LB/SEC
30.60
30.64
30.21
30.07
28.13
30.37
CALC
F/A
0.006600
0.014300
0.018200
0.020200
0.010700
0.008500
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
1075.00
1MO.OO
1850.00
1970.00
1375.00
1220.00
POHEP EXHAUST
PERCENT GAS
RATED TEMP
T.O. DEGRECS r
5
58
83
92
25
17
-o. on
-o.oo
-o. oo
-0.no
-o.oo
-o.on
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
[DRY!
PPMV
55.00
32.00
34.00
15.00
35.00
49.00
CO
2
(CRY)
PERCENT V
1 .35
3.12
3.66
4.19
J.50
2.03
THC
IWETI
PPMV
23.00
11 .00
10.00
10.00
30.00
10.00
NO
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
2
I DRY!
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
X
IDPY)
PPMV
29.00
94.00
176.00
160.00
76.00
42.00
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
56.00
60.00
60.00
58.00
59.00
58.00
PAPTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
POUFR
PERCENT
HATED
T.n.
5
58
83
92
25
17
MUSS FMI
CO
LR/1K
Lf FUFL
8. 1 I
2.05
1. 46
1.6'
2.7<)
4. 82
MASS FMI
HC
LD/1K
L« FUFL
1.17
0.42
0.32
0.28
1.41
0.57
MASS EMI
N02
LH/K
LO FUEL
- 1) . 00
-0.00
-0.00
-O.OII
-n.no
-o.on
MUSS TMI
CU2
LB/1K
LH FUFL
.3126.39
3140. 16
3140.72
3141.17
3136. 7»
1135. 3fi
MASS TMI
NO
LU/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
-O.on
-O.on
MASS FMI
HM
LB/1K
LB FUEL
7.02
9.89
11.30
12.54
9.97
6.78
MASS FM
CO
LH/HH
5.93
3.22
3.68
3.66
3.02
4.41
MASS EMI
HC
LB/HR
1.44
0.65
0.64
0.62
1.52
0.53
MASS EMI
NO 2
LB/HR
-0.00
-O.on
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
Lfl/HH
2288.52
4936.33
6218.62
6879.05
33S7.1B
2872.01
MASS EMI MASS FMI
NO NOX
Lfl/HP LB/HR
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
5.14
15.55
22.38
27.46
10.76
6.71
POWER
PERCENT
RATED
t.O.
5
58
83
92
25
17
0. 454
n.»6l
2.603
5.SOB
LB/IK HP-HR
8904.733
1847.914
1613.675
1619.440
2927.048
3650.703
THC
'K HP-HP
5. 604
0.745
0. 167
0. 147
1.317
0.669
NO
LB/IK HP-HH
-O.OOC
-0.000
-o.ono
-o.non
-o.ooo
-o.oco
LB/IK HP-HR
-0.000
-0.000
-0.000
-o.oon
-0.000
-o.noo
NO
X
Lfl/lK HP-HR
19.997
5.820
5.807
6.465
9.302
7.896
IV-40
-------
CAL ID NUMBER: 29 ENGINE TYPE AND MODEL: T56-M5
TEST ORGANIZATION! ALLISON DIVISION
SERIAL NUMBER! 6»08
HOOE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMROUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.030
I. 000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
POWER
HP
137.7
4591.0
4131.9
1377.3
137.7
POWER
HP
137.7
4991.0
4131.9
13T7.3
137.7
POWER
HP
137.7
4591.0
4131.9
1377.3
137.7
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR NIN.
9.637 64B.213 .000 19.00
4.140 2401.677 .000 0.90
3.829 2167.244 .ODD 2.90
2.946 1141.998 .000 4.50
9.637 6*8.213 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLEl
LBS POLLUTANT/1000K HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR NIN.
1.984 648.213 .000 19.00
2.211 2401.677 .000 0.90
1.972 2167.244 .000 2.90
0.966 1141.898 .000 4.90
1.984 64B.2I3 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
1 LBS POLLUTANT/1000K HP AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
2.308 6*8.213 .000 19.00
61.740 2401.677 .000 0.50
25.617 2167.244 .000 2.90
9.331 1141.898 .000 4.90
2.308 6*8.213 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS PGLLUTANT/1K HP-HR/CYCLE:
LBS POLLUTANT/IOOOK HP AT T.O. :
CO
MASS
LBS.
1.785
0.034
0.199
0.221
0.69B
2.897
5.992
7.693
0.791
HC
MASS
LBS.
0.628
0.018
0.082
0.072
0.231
1.033
2.165
2.769
4.014
NOX
MASS
LBS.
0.731
0.514
1.067
0.700
0.269
3.282
6.883
8.789
112.067
FUEL
MASS
LBS.
209.27
20.01
90.30
85.64
75.62
476.85
FUEL
MASS
LBS.
205.27
20.01
90.30
85.64
75.62
476.85
FUEL
MASS
LBS.
205.27
20.01
90.30
85.64
75.62
476.85
LB CO /
IK LB FUEL
8.696
1.724
1.765
2.980
B.696
LB HC /
IK LB FUEL
3.060
0.921
0.910
0.846
3.060
LB NOX/
IK LB FUEL
3.961
29.707
11.820
8.172
3.961
ENERGY
HP-MR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
LB CO /
HP-HR
0.04093
0.00090
0.00093
0.00214
0.04093
LB HC /
HP-HR
0.01440
0.00048
0.00048
0.00070
0.01440
LB NOX/
HP-HR
0.01676
0.01345
0.00620
0.00678
0.01676
IV-41
-------
SERIAL NUMPER:
OATF: 6/7.W71
TEST ORGANIZATION: ALLISON DIVISION
ENGINE SUPPLIER: ALLISON DIVISION
ENGINE DATA »***»»..................
CAL ID NUMBER: 76 ENGINE TYPE AND MODEL: 156-415
BATED HORSEPOWER: 4591.
ENGINE TOTAL TIME: 0. MRS
TIME SINCE HUT SECTION OVERHAUL: 0. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
NZ TURBINF OVERHAUL: o. HRS
FUEL: jp-5 FUEL H/C RATIO: 1.070
OPERATIONAL OATS »»«»«««««««
INLET AIR TEMPERATURE, OFGREES f: START 82.00 FINISH
ATMOSPHERIC PRESSURE: START 28.70 FINISH
INLET AIR HUMIDITV, LBS H20/LU AID: 0.0092
RELATIVE HUtlllTV: 18.00 PERCENT
SAMPLE LINE: TEMPERATURE, OEGREFS C: 154.44, FLOW RATE, LITERS/MIN: 5.00
SAMPLE LINF THANSPORT TIME. SEC: 1.00
NUMBER OF TFSTS: 10
COMMENTS:
FINAL RUN
69.00
28.90
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PF'CENT
RATED
T.n.
5
55
73
84
R9
18
89
18
2
5
POWER
PERCENI
R ATFO
T.n.
5
55
78
84
89
18
89
18
2
5
POWER
PERCENT
RATED
T.O.
5
55
78
84
89
18
89
Id
2
5
TFSI
MCOE
I/ 0
2/ 1
3/ 7
4/ 3
5/ 4
7/ 5
9/ 7
ll/ 1
14/11
15/ 14
EXHAUST
GAS
TEMP
OEGRFES I-
-0.00
-0 .00
-0.01
-0.11
-0. 00
-1.00
-0.00
-0.00
-n.oo
-0.10
MASS FMI
en
LB/IK
LB F'/Fl
5.53
2.02
. 69
.73
. 78
.04
.87
.14
26.32
7.63
r.r
LR/1K
17.
1 .
0.
0.
0.
5.
0.
5.
162.
21.
POWER ENGINE MEASURED G5S GFN CALC COMPRESSOR ENGINE TURBINF
THRUST, LBS PE'tCFNI SPEED FUEL AlK FLOW F /A DISCHARGE PRESSURE INLET
00, RATFD RPM FLOW LH/SFC TEMP RATIO TEMP
SHP r.O. NI N2 Lfi/HR DEGREES F EPR DEGREES F
235.60 5 13500.00 -1.00 720.00 30.29 0.006600 -0.00 -0.00 1075.00
2539.90 55 13800.00 -0.00 1550.00 30.00 0.014401 -0.00 -0.00 1610.00
3591.00 78 13800.00 -0.00 1950.00 29.36 0.016100 -0.00 -0.00 1850.00
3675.60 B4 13300.00 -0.00 2080.00 29.7? O.CI9400 -0.00 -0.00 1920.00
4116.50 »9 11800.00 -0.00 2170.00 29.65 0.020300 -0.00 -0.00 1970.00
879.10 18 13400.00 -0.00 910.00 79.86 0.008500 -0.00 -0.00 1225.00
4116.50 ft 13800.00 -0.00 217C.OO 79.65 0.020301 -0.00 -0.00 1970.00
879.10 18 11400.00 -0.00 908.00 79.36 0.008400 -0.00 -0.00 1720.00
95.20 7. 10000.00 -0.00 576.00 20. OH 0.000000 -0.00 -0.00 1205. CO
735.60 5 13500. OC -0.00 720.00 79. SO 0.006700 -0.00 -0.00 1090.00
IXHAUST cn r.n THC NG NO NO \LDFHYOES SMOKE PARTICULARS
GAS IDRYl 2 H.FTI (DRY) 7 X
PRESSURE PPMV (DRY) PPMV PPHV IDHY1 (DRYt
PSIA
-0.00
-0.00
-0.10
-0.00
-1.1?
-0.00
-0.00
-".00
-0.01
-0.00
1ASS FMI
HC
LH/IK
L8 fUFL
7.45
0. II
0.08
0.08
0.08
0.16
0.08
1.15
1 6.70
0.71
HP-HH
161
235
915
930
439
528
960
516
? 76
373
PFSCFNT V
60.10 2
34.00 3
36.00 4
37.00 4
40.00 4
54.00 2
42.00 4
54.00 2
390.10 2
67.00 I
MASS FMI MASS TH|
N02 CO?
LI/IK LB/IK
Ltl FUEL LB FUEL
-0.00 1129.03
-1.00 3l4l.0(,
-1.00 3141.65
-0.00 3141.57
-1.01 M41.51
-0.01 3136.16
-1.00 3141.45
-1.00 1136.16
-O.CU 3057.94
-1.00 3131.19
CO
2
. 14 45.
. 16 3.
.27 3.
.27 3.
.49 3.
.14 3.
.61 3.
.14 1.
.83 400.
.75 3.
MASS F«l
NO
LP/1K
L t) FUL'L
-0.00
-1.00
-0.01
-0.00
-1.00
-0.00
-0.00
-1. 00
-0.00
-n.oo
THC
LH/1K HP-HD LB/IK IIP-HK
9562 .414
1916.861
1705.989
1636.053
1656.035
3442 . 1 74
1656.005
3434.609
H501 . 820
9571 .445
7.484
0.064
0. 046
0.045
0.042
0. 180
0.041
0. 179
98.016
0.608
00 -0
00 -0
00 -0
00 -0
00 -0
no -o
00 -0
00 -0
00 -0
00 -0
MASS FMI
NOX
LR/1K
L3 FUEl
4. 89
8.01
9.73
8.31
9.65
7.81
10.69
7. HI
3.61
6.36
.00
.00
.00
.00
.00
.00
.00
.00
.00
.00
"ASS
en
PPHV PPMV
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-a.
EMI
I. H / HI*
4.
3.
1.
3.
3.
4.
3.
4 .
1 5.
5.
0?
14
29
60
HI
58
95
57
45
49
NO
LD/1K
-0
-0
-0
-0
-0
-0
-0
-0
-0
-0
HP-HR
.001
.001
.000
.000
.100
.000
.000
.000
.000
.100
00 32.00 -0
00 32.10 -0
00 120.00 -0
00 108.00 -0
00 I 32.00 -0
00 51.00 -0
01 150.00 -0
00 51.00 -0
00 37.00 -0
00 34.00 -0
MASS E"l "ASS E"I
HC NH2
LR/hw LB/HR
1.76 -0.00
0.16 -0.0"
0.16 -0.00
0.17 -0.00
0.17 -0.00
0.15 -0.00
0.17 -0. 00
0.15 -0.00
9.3) -0.00
0.14 -0. OO
Nil
?
.00 52
.00 56
.01 57
.00 58
.00 55
.00 54
.00 55
.00 54
.00 43
.00 52
MASS FMI
CO?
LB/HR
2252.90
4868.63
6126.21
6534.46
6817.07
2853.91
6816.94
2847.63
1761.37
2255.03
NO
X
.00 -0.00
.00 -0.00
.10 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -C.OO
MASS EMI «ASS
LMI
NO NOX
LB/HR LB/HR
-0.00 3
-0.00 12
-0.00 18
-0.00 17
-C.OO 20
-0.00 7
-0.00 73
-0.00 1
-0.10 2
-0.00 4
.52
.42
.00
.23
.95
.11
. 19
.09
.08
.58
LB/IK HP-HK LB/IK HP-HR
-0.1OO
-0.000
-0.000
-0.00"
-o.oon
-0.000
-0.000
-0.000
-0.000
-?.ooo
14.943
4.310
5.012
4 .458
5.090
8.576
5.631
6.557
71 .871
19.440
IV-42
-------
CAl 10 NUMBER: 26 ENGINE TYPE AND MODEL: T56-A15
TEST ORGANIZATION: ALLISON DIVISION
SERIAL NUMBER: 8907
MODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
0.030
I. 000
0.900
0.300
0.030
POWER
HP
137.
4591.
4131.
1377.
137.
7
0
9
3
7
EMISSION FUEL
RATE RATE
LB/HR LB/HR
8.970 456.065
4.270 2434.323
3.73B 2200.739
4.223 1158.112
8.970 456.065
USAGE TIME IN
WT FACTOR MODE
MIN.
.000
.000
.000
.000
.000
19.00
0.50
2.50
4.50
T.OO
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
IBS POLLUTANT/1000X HP AT T.O.:
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
POWER
HP
137.
4591.
4131.
1377.
137.
7
0
9
3
7
EMISSION FUEL
RATE RATE
LB/HR LB/HR
9.176 456.065
0.0 2434.323
0.030 2200.739
0.124 1158.112
9.176 456.065
USAGE TIME IN
WT FACTOR MODE
MIN.
.000
.000
.000
.000
.000
19.00
0.50
2.50
4.50
7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/ 1000K HP AT T.O.:
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
POWER
HP
137.
4591.
4131.
1377.
137.
7
0
9
3
7
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.636 456.065
23.695 2434.323
21.150 2200.739
6.582 1158.112
1.636 456.065
USAGE TIME IN
HT FACTOR MODE
MIN.
.000
.000
.000
.000
.000
19.00
0.50
2.50
4.50
7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
CO
MASS
LBS.
2.840
0.036
0.156
0.317
1.046
4.395
11.085
11.770
0.775
HC
MASS
LBS.
2.906
0.0
0.001
0.009
1.071
3.987
10.056
10.677
0.0
NOX
MASS
LBS.
0.518
0.197
O.BBI
0.494
0.191
2.281
5.754
6.110
43.010
FUEL
MASS
LBS.
144.42
20.29
91.70
86.86
53.21
396.47
FUEL
MASS
LBS.
144.42
20.29
91.70
86.86
53.21
396.47
FUEL
MASS
LBS.
144.42
20.29
91.70
86.86
53.21
396.47
LB CO /
IK LB FUEL
19.668
1.754
1.699
3.646
19.668
LB HC /
IK LB FUEL
20.120
0.0
0.014
0.107
20.120
LB NOX/
IK LB FUEL
3.588
9.734
9.610
5.683
3.588
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
373.40
LB CO /
HP-MR
0.06513
0.00093
0.00090
0.00307
0.06513
LB HC /
HP-HR
0.06662
0.0
0.00001
0.00009
0.06662
LB NOX/
HP-HR
0.01188
0.00516
0.00512
0.00478
0.01186
IV-43
-------
0»TE: 6/21/71
TEST ORGANIZATION: ALLISON DIVISION
ENGINE SUPPLIER: ALLISUN DIVISION
ENGINE DATA ««««...««.«....«....«.....................
C«L ID NUMBEP: 27 FNGINE TYPE AND MODFL: Ti6-Alb
RATFO HORSEPOWER: 4591.
ENGINE TOTAL TIME: 0. HOS
TINE SINCE HOT SECTION OVFRHAUL: 0. MRS
TIME SINCE:
Nl COMPRESSOR OVFRHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: o. HRS
COMBIISTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZ7LE GUIDE VANF OVERHAUL: 0. HRS
NI TURBINE OVFRHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
fuF.L M/C RATIO:
SERIAL NUMBER:
8510
1.970
B4.00
28.90
FUEL: JP-S
OPERATIONAL DATA ««««««««»»««»«««««»
INLET AIR TEMPERATURE, DEGREES f: START 76.00 FINISH
ATMOSPHERIC PRESSURF: START 28.60 FINISH
INLET AIR HUMIDITY, LBS H20/L1 AIR: 0.011B
RELATIVE HUMIDITY: 60.00 PERCENT
SAMPLE LINE: TEMPERATURF, CSGREES C: 154.44, FLON RATE, LITERS/MIN:
SAMPLF LINE IRANSPRRT TIMF, SET: 1.00
NUMBER OF TESTS: 6
COMMENTS:
FINAL RUN
CLOCK
TIMF
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TEST
MODE
it o
2/ 1
I/ 7
5/ 1
6/ 5
THRUST
OR
SHP
235.
2715.
3809.
4115.
1111.
871 .
POWER
,LBS
60
10
90
40
ao
70
PERCFNT
RATED
T.O.
5
59
82
94
24
ID
Nl
13500.
11800.
13300.
13800.
14300.
11400.
CNGINF
SPEFD
RP»
00
no
OC
00
00
on
N?
-0.00
-o.no
-0.00
-0.00
-0.00
-0.00
MEASURFD
FUEL
FLOM
LB/HR
720.00
1570.00
2000.00
2210.00
1041.00
B99.00
GAS GEN
AIR FLOW
LB/SEC
10.60
10.51
10.32
10.29
28.25
10.25
CALC
F/A
0.006500
0.014100
0.018100
0.020100
0.010200
0.008300
COMPRESSOR
DISCHARGE
TEMP
DFGREES F
-0.00
-0.00
-n.oo
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TF»P
OEGRFFS F
1055.00
1610.00
1B50.00
1970.00
1365.00
1210.00
POWER
PERCENT
RATED
T.O.
5
59
82
94
24
18
EXHAUST
GAS
TEMP
DEGREES F
-o.no
-O.on
-0.00
-0.00
-0.00
-n.oo
FKHAUST
r,«s
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
IORYI
PPMV
49.00
34.00
15.00
39.00
11.00
52.00
CO
2
ICRYI
PERCENT V
1.61
J.52
4.45
4.38
1 1.IH
2.22
THC
(MET)
PPMV
26.00
11.00
2.00
1.00
2.00
I. 00
NO
IORYI
PPMV
-0.00
-0.00
-0.00
-o.no
-0.00
-o.oo
NO
2
(DRY!
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
X
IORYI
PPMV
11.00
74.00
102.00
100.00
B2.00'
11.00
ALDEHYDES SMOKF PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
51.on
57.00
60.00
SB.00
58.00
57.00
-C.OO
-0.00
-0.00
-0.00
-0.00
-0.00
PUHER
PERCENT
RATED
T.O.
5
59
82
94
24
IK
MASS FHI
CO
LB/IH
LB run
5.99
1.91
1.57
1 .7]
2.T7
' .68
MASS EMI
HC
IH/1K
LR FUF.L
I.B5
n.17
0.05
".08
0.07
0.05
"ASS EMI
N02
LI/IK
LB FUI:L
-0.00
-O.OT
-0.00
-11.00
-0.00
-1.00
MASS C«l
C02
LB/1K
LQ FUEL
1110.04
Jl',0.48
3141.91
1141.57
1141 .06
1137.03
»4SS EMI
Ml
LB/1K
LB FUEL
-0.00
-0.00
-0.00
-C.OO
-0.00
-0.00
MASS FMI
NOX
LB/1K
LB FUEL
6.22
6.90
7.51
7.50
B.47
4.58
MASS EMI
CO
LB/HR
4.11
3.01
3.15
J.P3
2.16
4.20
MASS F»l
HC
Lfl/Hk
1.13
0.50
0.11
0.18
0.08
0.0*
MASS Fwl
Nf]2
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
2251.61
49<0.54
6281.81
6942.88
1269. H4
2820.19
MASS FMI
NO
LB/HR
-0.00
-0.00
-0.00
-O.on
-c.oo
-0.00
MASS E.MI
NOX
LB/HR
4.48
10.84
15.06
16.57
8.81
4.12
POUFR
PERCFNT
RATED
T.O.
5
59
82
04
24
18
r.n
Lfl/lK HP-HP
18.101
1.116
0.826
0.884
1.942
LB/IH HP-HR
9565.500
Ifll5."71
1649.117
1601.439
2941.036
3215.279
THC
M HP-HH
5.651
0.714
0.028
0.042
0.070
0.054
NO
LB/IK HP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
Lfl/lK HP-HR
-0.000
-0.000
-0.000
-0.000
-n.ooo
-0.000
NO
X
LO/1K HP-HR
19.018
1.991
1.957
1.822
r.928
4.721
IV-44
-------
CAL 10 NUMBER: 27 ENGINE TYPE AND MODELi T56-«i5
TEST ORGANIZATION: ALLISON DIVISION
SERIAL NUMBERl 8310
MODE
IAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDIE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.010
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1. 000
0.900
0.300
0.030
POWER
HP
117.7
4191.0
4111.9
1377.3
137.7
POWER
HP
137.7
4591.0
4131.9
1177.1
137.7
POWER
HP
137.7
4591.0
4131.9
1377.3
137.7
EMISSION FUEL USAGE TIME IN
RATE RATE NT FACTOR MODE
LB/HR LB/HR HIN.
3.180 197.679 1.000 19.00
3.777 2306.891 1.000 0.50
1.279 2104.478 1.000 2.50
2.179 1119.468 1.000 4.10
1.180 397.679 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/ 1000K HP AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
1.312 397.679 .000 19.00
0.089 2)06.891 .000 0.90
0.096 2104.478 .000 2.90
0.081 1119.468 .000 4.90
1.312 397.679 .000 7.00
TOTAL FOR CYCLE)
LBS POLLUTANT/IK LB FUEL/CYCLE!
LBS POLLUTANT/IK HP-HR/CVCLE:
LBS POLLUTANT/ IOOOK HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR NIN.
0.282 397.679 .000 19.00
17.370 2306.891 .000 0.90
19.906 2104.478 .000 2.90
6.038 1119.466 .000 4.90
0.282 397.679 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK IB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/IOOOK HP AT T.O.:
CO
MASS
IBS.
1.070
0.031
0.137
0.161
0.394
1.796
4.929
4.811
0.686
HC
MASS
IBS.
0.416
0.001
0.004
0.006
0.151
0.979
1.989
1.992
0.161
NOX
MASS
IBS.
0.089
0.149
0.661
0.493
0.031
1.181
1.791
1.701
11.928
FUEL
MASS
LBS.
129.93
19.22
87.69
89.46
46.40
364.70
FUEL
MASS
LBS.
129.93
19.22
87.69
89.46
46.40
364.70
FUEL
MASS
LBS.
129.93
19.22
87.69
89.46
46.40
364.70
LB CO /
IK LB FUEL
8.900
1.637
1.998
1.912
8.900
LB HC /
IK LB FUEL
3.300
0.039
0.046
0.071
J.100
LB NOX/
IK L6 FUEL
0.710
7. 929
7.958
9.299
0.710
ENERGY
HP-HR
43.61
3B.26
172.16
103.10
16.07
171.40
ENERGY
HP-HR
41.61
18.26
172.16
103.10
16.07
373.40
ENERGY
HP-HR
41.61
18.26
172.16
101.10
16.07
173.40
LB CO /
HP-HR
0.02454
0.00082
0.00079
0.00158
0.02454
L8 HC /
HP-HR
0.00993
0.00002
0.00002
0.00006
0.00953
L8 NOX/
HP-HR
0.00205
0.00378
0.001B5
0.00418
0.00205
IV-45
-------
DATE: 6/16/71
TEST ORGANIZATION: ALLISON DIVISION
ENGINE SUPPLIER: ALLISON DIVISION
ENGINE DATA «««««....
CAL 10 NUMBER: 28 ENGINE TYPE AND MOOELi T56-A15
RATED HORSEPOUER: 4,591.
ENGINE TOTAL TIME: 0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAULI 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COHBUSTOR CAN REPLACEMENT: o. HRS
EIRST SIAGE NOiZLF GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAULI 0. HRS
FUEL: JP-S FUEL H/C RATIO: 1.970
OPERATIONAL DATA ««»»««««»«
INLET AIR TEMPERATURE. DEGREES F: START 89.00 FINISH 93.00
ATMOSPHERIC PRESSURE: START 28.80 FINISH 29.00
INLET AIR HUMIDITY, LBS H70/LB AIR: 0.0102
RELATIVE HUMIDIFY: 34.00 PFRCENF
SAMPLE LINE: TEMPERATURE, DEGREES C: 154.44, FLOU RATE, LITFKS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 8
COMMENTS:
FINAL RUN
SERIAL NUMBER:
CLOCK
TIME
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TFST
MODE
I/ 0
?/ I
3/ 7
4/ 1
5/ 4
(./ 5
7/ 6
9/ 7
PDWFR
THKUST.LBS
OR
SHP
757. ro
2496.20
3V5.30
3744.20
39 19.40
975.60
850.50
3919.40
PERCENT
RATED
T.O.
5
54
76
81
85
21
ie
85
EN(
SI
1
Nl
i350o.no
13800.00
I3eno.on
1380(1. 00
iiHoo.no
14300.00
13400.00
13800.00
MEASURED
SPFFO FUEL
RPM FLOU
N2 LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
732.00
1512.00
1925.00
2020.00
2090.00
1040.00
918.00
2100.00
GAS GEN
AIR FLOU
Lfl/SEC
29.90
-0.00
29.90
29.8)
29. 76
27.05
29.65
29.83
CAIC
F/A
0.006600
0.014100
0.017900
O.OlflflOO
0.019500
0.010700
O.OUR600
0.019600
COMPRESSOR
DISCHARGE
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
TURBINE
INLET
TEMP
DEGREES F
1105.00
1610.00
1650.00
1920.00
1970.00
1410.00
1255.00
1970.00
POUER
PERCENT
RATED
T.O.
5
54
76
ai
35
71
18
85
EXHAUST
GAS
TFMP
-o.oo
-o.oo
-o.no
-o.on
-n.oo
-o.oo
-n.oo
-o.oo
EXHAUST
GAS
PRESSURF
PSI A
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CM
IOHYI
PPMV
55.00
12.00
34.on
32.00
35.00
35.00
',9.10
38.00
r.n
2
I DRY)
PFBf.FNT
1.55
3. 26
4. 10
4.65
4.71
2.75
2. 13
4.42
THC
IUETI
PPMV
15.00
9.00
3.00
2.00
4.00
3.00
1.00
4.00
NO
IORYI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NO
2
(DRY)
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
NO
X
I DRY I
PPMV
30.00
108.00
179.00
129.00
153.00
77.00
42.00
153.00
ALDEHYDES SMOKF PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
50.00
52.00
54.00
54.00
54.00
53.00
52.00
54.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER MASS EMI
PERCENT CO
RATED LB/IK
T.n. LB FIIFI.
5
54
76
81
85
.07
.95
.66
. 18
.49
21 7.54
16 4.59
35 1.72
MASS EMI
HC
LB/1K
LB FUEL
1.12
(1.32
0.09
0.05
0.10
0.13
0.05
0. II
MASS EMI
NJ2
LB/IK
LB FUEL
-0.00
-n.on
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MASS E"l
C02
LB/1K
LB FUEL
3130.34
3140.57
3141.68
3142.22
3141.91
3140. IR
3137.16
3141.53
MASS FMI
NO
LB/IK
LB FUFL
-0.00
-n.oo
-0.00
-0.00
-n.oo
-0.00
-0.00
-0.00
MASS FMI
NOX
LB/IK
LB FUEL
6.33
10. ni
10.33
9.11
10.67
9.19
6.47
11.37
MASS EMI
cn
LB/HS
5.17
2.95
3. 19
2.7B
3.11
2.65
4.22
3.61
MASS FMI
HC
LB/MR
O.H2
0.49
0.17
o.in
0.21
0.13
0.05
0.73
MASS EMI
NO 2
LB/HR
-0.00
-0.00
-O.OO
-0.00
-0.00
-n.oo
-0.00
-o.oo
MASS EMI
cr>7
LB/HR
2291.41
4148.54
6047.73
6347.28
6566.59
3265.78
2879.91
6597.70
MASS EMI
Nn
LB/MP
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-o.cc
-0.00
MASS EM
NOX
LB/H«
4.64
16.35
19.89
18.41
27.30
9.56
5.94
73.67
POWER
PERCENT
RATED
T.n.
5
54
76
81
K5
21
18
85
20. 1 16
I.181
0.905
0.742
0.792
2.712
4.958
0.921
LB/IK HP-MR
H915.992
1902.307
1715.57?
1695.731
1675.406
3347.461
3386.136
1683.210
THC
L8/1K HP-HP
3.193
0. 196
0.046
0.028
0.054
0.137
0.059
0.058
NU
LB/IK HP-Hk
-0.000
-0.000
-0.000
-o.ono
-0.000
-O.ODO
-0.000
-o.r.oo
IR/IK MP-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-o.oon
-0.000
ND
X
Lfl/lK HP-HR
18.040
6.548
5.643
4.916
5.689
9.79B
6.980
6.091
IV-46
-------
CAL ID NUMBER: 28 ENGINE TYPE »ND MODEL: 156-115
TEST ORGANIZATION: ALLISON DIVISION
SERIAL NUMBER! 8469
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI- IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
1.000
0.900
0.300
0.030
FRACTIONAL
POWER
0.030
I. 000
0.900
0.300
0.030
POWER
HP
137.7
4591.0
4131.9
1377.3
137.7
POWER
HP
137.7
4591.0
4131.9
1377.3
137.7
POWER
HP
137.7
4591. 0
4131.9
1377.3
137.7
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR NODE
LB/MR LB/HR KIN.
4.215 576.838 .000 19.00
2.583 2387.879 .000 0.90
2.823 2186.542 .000 2.50
2.521 1144.479 .000 4.50
4.215 576.838 .000 7.00
TOTAL FOR CYCLEl
L8S POLIUTANT/IK LB FUEL/CYCLE!
LBS POLLUTANT/IK HP-HR/CYCLEl
LBS POLLUTANT/1000K HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR HIN.
2.087 576.838 .000 19.00
0.310 2387.875 .000 0.50
0.249 2186.542 .000 2.50
0.123 1144.479 .000 4.50
2.087 576.838 .000 T.OO
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
1.975 516.838 .000 19.00
26.544 2387.875 .000 0.50
21.634 2186.542 .000 2.50
8.856 1144.479 .000 4.50
1.975 976.838 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK HP-HB/CYCLEI
LBS POLLUTANT/1000K HP AT T.O.I
CO
MASS
LBS.
1.135
0.022
0.118
0.189
0.492
2.155
4.B22
5.770
0.469
HC
MASS
LBS.
0.661
0.003
0.010
0.009
0.243
0.927
2.074
2.481
0.963
NOX
MASS
LBS.
0.625
0.221
0.985
0.664
0.230
2.726
6.101
7.300
48.182
FUEL
MASS
LBS.
182.67
19.90
91.11
85.84
67.10
446.80
FUEL
MASS
IBS.
182.67
19.90
91.11
85.84
67.10
446.80
FUEL
MASS
LBS.
182.67
19.90
91.11
85.84
67.30
446.80
LB CO /
U LB FUEL
7.307
1.082
1.291
2.203
7.107
LB HC /
IK LB FUEL
3.618
0.130
0.114
0.107
3.618
LB NOX/
IK LB FUEL
3.423
11.116
10.809
7.738
3.421
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
371.40
ENERGY
HP-HR
41.61
18.26
172.16
103.30
16.07
373.40
ENERGY
HP-HR
43.61
38.26
172.16
103.30
16.07
173.40
LB CO /
HP-HR
0.03060
0.00056
0.00068
0.00183
0.03060
LB KC /
HP-HR
0.01515
0.00007
0.00006
0.00009
0.0151!
LB NOX/
HP-HR
0.01434
0.00578
0.00572
0.00643
0.01434
IV-47
-------
OATEI 5/ 6/71
TEST ORGANUATION: AIRESEARCH
ENGINE SUPPLIER: AIRESEARCH
ENGINE DATA
CAL ID NUHBFR: }4 ENGINE TYPE AND MODEL: T76-0-410
RATED HORSEPOWER! 720.
ENGINE TOTAL TIME: 0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: o. HRS
N2 COMPRESSOR OVERHAUL: o. HRS
COHBUSTOK CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: o. HRS
fUEL: JP-5 FUEL H/C KATIO: 1.677
OPERATIONAL DATA ««««4
INLET AIP TEMPERATURE, DEGREES F: START 91.00 FINISH
ATMOSPHERIC PRESSURE: START 2R.61 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0066
RELATIVE HUMIDITY: 42.00 PERCENT
SAMPLE LINE: HMPFHATIIRE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 6
COMMENTS:
SERIAL NUMBER:
59.00
2B.61
CLOCK
TIME
-o.on
-o.oo
-0.00
-0.00
-0.00
TEST
MODE
It 0
2/ I
6/ 2
ll/ 6
16/1 I
-0.00 20/16
THRUST
OR
SHP
2.
142.
262.
431.
571.
666.
POWER
,LBS
10
ao
40
60
20
40
PERCENT
HATED
T.O.
n
11
39
59
T>
92
Nl
27230.
41730.
41 730.
41730.
41730.
41730.
ENGINE
SPEED
RPM
00
00
00
00
00
OC
N2
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
MEASURED GAS GEN
FUEL MR FLOW
FLOW LB/SEC
L8/HB
71.00
192.00
238.00
293.00
347.00
387.00
2.6B
6.50
6.47
6.45
6.)B
6.13
CALC COMPRESSOR ENGINE
F/A DISCHARGE PRESSURE
TFMP RATIO
DEGREES f EPR
0.007700
O.OOB600
0.010700
0.013200
0.015800
O.OI7BOO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWFR
PERCENT
RATED
T.n.
0
19
11
59
79
92
EXHAUST
GAS
TEMP
DEGREES F
621.00
622.00
70fl.00
BI5.00
910.00
1010.00
rXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
CO
IUETI
PPHV
482.20
22). 10
190.20
151 .50
91.10
38.90
cn
2
IWETI
PERCENT V
1.61
1.86
2.29
J.<-5
1.09
3.44
THC
IUETI
PPMV
564.10
91.40
39.90
9.20
2.?0
1.40
NO
IUETI
PPMV
1.90
12.60
27.50
50. 7C
80. SO
98.10
NO
2
IHETI
PPMV
12.10
29.30
29.30
22.10
11.70
8.70
NO
X
IUETI
PPMV
14.00
42.00
56. BO
72.80
92.50
106.80
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWE"
PEHCENT
RATED
1.0.
0
19
19
59
MASS FMI
CO
LB/IK.
L* FUEL
56.66
71.75
16.57
11.45
5.92
2.28
MASS U»l
HC
LB/IK
LP FUEL
17.M6
5.51
1 .99
0.40
O.Ofl
0.05
MASS EMI
N02
LB/IK
LR FUFL
2.14
5. 11
4.19
2.74
1.25
0.84
MASS FMI
C07
LB/IK
LB FUEL
2972.55
1113.11
3114.74
1146.65
1156.20
3167.02
MASS EMI
NO
H/IK
LB FllfL
0.17
2.20
1.91
6.29
e.6i
9.41
MASS FMI
MOX
LB/IK
LB FUEL
2.70
7.35
8.11
9.04
9.BB
10.26
MASS FM
no
Lfl/HR
4.02
4.56
3.94
3.15
2.06
3.88
MASS LMI
HC
LB/HR
2.70
1.07
0.47
0. 12
0.03
0.02
MASS FMI
N02
LB/HR
0.17
0.98
1.00
0.80
0.4}
0.32
MASS EMI
CO 2
LB/HR
211.05
597.72
745.95
921.97
1095.20
1223.70
MASS EMI MASS EMI
NO NOX
L°/HR LB/HR
0.03
0.42
0.94
1.84
2.99
1.65
0.19
1.41
1.91
2.65
3.41
1.97
POWER
PERCENT
RATFD
T.O.
0
19
79
92
cn
LB/IK MP-HR
1915.717
11.919
11.961
7.773
3.598
I . 122
100500.50C
4185.618
2641.461
2136.164
1917.368
1816.290
THC
LB/IK HP-HR
1263.578
7.497
1.678
0.270
0.050
0.027
NO
LB/IK HP-MR
12.399
2.964
3.116
4.272
5.241
5.474
Lft/lK HP-HR
78.960
6. P93
3.513
1.862
0. 759
0.4B5
NO
X
Lfl/lK HP-HR
91.359
9.SSI
6.849
6.135
6.000
5.960
IV-48
-------
CAL to NUMBER: 34 ENGINE TYPE ANO MODEL: T76-G-410
TEST ORGANIZATION: AIRESEARCH
SERIAL NUNBERl GEOOT90
MODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
UXI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.060
1.000
0.900
0.300
0.060
FRACTIONAL
POKER
0.060
1.000
0.900
0.300
0.060
FRACTIONAL
POKER
0.060
1.000
0.900
0.300
0.060
POKER
HP
43.2
720.0
6*8.0
216.0
43.2
POKER
HP
43.2
720.0
648.0
216.0
43.2
POKER
HP
43.2
T20.0
6*8.0
216.0
43.2
EMISSION FUEL USAGE TIME IN
RATE RATE NT FACTOR MODE
LB/HR LB/HR NIN.
6.331 150.239 .000 19.00
0.281 409.937 .000 O.JO
1.169 380.229 .000 2. JO
4.2?* 216. 994 .000 4.SO
6.931 110.239 .000 T.OO
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK HP-MR/CYCLE I
LBS POLLUTANT/1000K HP AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE NT FACTOR MODE
LB/HR LB/HR MIN.
2.563 150.239 .000 19.00
0.0 409.537 .000 0.50
0.009 380.229 .000 2.50
0.737 216.99} .000 4.50
2.563 150.239 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CVCLE:
LBS POLLUTANT/1000K HP AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE MT FACTOR MODE
LB/HR LB/HR MIN.
0.769 150.239 .000 19.00
4.294 409.537 .000 0.50
3.863 380.229 .000 2.50
1.681 216.995 .000 4. SO
0.769 150.239 .000 7.00
TOTAL FOR CYCLE:
IBS POLLUTANT/IK 19 FUEL/CYCLEl
LBS POLLUTANT/IK HP-HR/CVCLEl
LBS POLLUTANT/ 1000K HP AT T.O.I
CO
MASS
LBS.
2.005
0.002
0.049
0.319
0.739
3.113
10.937
45.838
0.326
HC
MASS
LBS.
0.812
0.0
0.000
0.055
0.299
1.166
11.589
17.171
0.0
NOX
MASS
LBS.
0.244
0.036
0.161
0.126
0.090
0.656
6.119
9.659
49.696
FUEL
MASS
LBS.
47.58
3.41
15.84
16.27
17.53
100.63
FUEL
MASS
LBS.
47.58
3.41
15.84
16.27
17.53
100.63
FUEL
MASS
LBS.
47.58
3.41
15.84
16.27
17.33
100.63
LB CO /
IK IB FUEL
42.136
0.687
3.075
19.604
42.136
LB HC /
IK LB FUEL
17.058
0.0
0.025
3.398
17.058
LB NOX/
IK LB FUEL
5.118
10.484
10.160
7.746
5.118
ENERGY
HP-HR
13.68
6.00
27.00
16.20
5.04
67.92
ENERGY
HP-HR
13.68
6.00
27.00
16.20
5.04
67.92
ENERGY
HP-HR
13.68
6.00
27.00
16.20
5.04
67.92
LB CO /
HP-HR
0.14654
0.00039
0.00180
0.01969
0.14654
18 HC /
HP-HR
0.05933
0.0
0.00001
0.00341
0.05932
LB NOX/
HP-HR
0.01780
0.00596
0.00596
0.00778
0.01T80
IV-49
-------
DATE: 5/11/71
TEST ORGANUATION: AIRESEARCH
ENGINE SUPPLIER: AIRESEARCH
ENGINE DATA
CAL 10 NUMBER:
3) ENGINE TYPE AND MODEL: TPE 331-43 A
RATED HORSEPOWER: 575.
ENGINE TOTAL TIME: 0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
SERIAL NUMBER!
P-6I15T
NI COMPRESSOR OVERHAUL: o. MRS
N2 COMPRESSOR OVERHAUL: 0. MRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOJZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINF OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL: JP-S FUEL H/C RATIO: 1.877
OPERATIONAL DATA »»««
INLET AIR TEMPERATURE, DFGRFFS F: START 41.00 FINISH 91.00
ATHOSPHFPIC PRESSURE: START 26.76 FINISH 28.76
INLCT Air. HUMIDITY, LBS H20/LB AIR: 0.0044
RELATIVE HUMIUITV: lb.00 PERCENT
SAMPLE LINE: TEMPFRATURF, DEGRFES C: -0.00, FLOM RATE, LITCRS/MIN:
SAMPLE LINF IRANSPORI TIHF, SEC: -0.00
NUMBER OF TESTS: 6
CriMMFNTS:
-0.00
CLOCK
TIMF
-o.no
-0.00
-0.00
-0.00
-o.oo
-0.00
TFST
MODE
I/ 0
?/ I
hi 2
ll/ 6
lb/ I 1
20/16
HRUST
OR
SHP
2.
6.
139.
266.
393.
<>98.
POWER
.LBS
70
JO
60
60
50
20
PfiRCENT
RATED
T.O.
0
1
24
46
68
86
NI
35535.
41730.
41710.
41 730.
41730.
41730.
ENGINE
SPEED
RPM
00
00
00
00
00
00
N2
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
MEASURED
FUEL
FLOW
IB/HR
101. (JO
150.00
197.00
246.00
293.00
338.00
GAS GEN
AIR FLOW
LB/SEC
CALC
F/A
-0.00 -0.000000
-0.00 -0.000000
-0.000000
-0.000000
-0.000000
-0.00
-0.00
-0.00
-o.oo -o.oooooo
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
0
1
24
46
68
86
EXHAUST
GAS
TFMP
OEC.RFES F
615.00
620.00
745.00
860.00
975.00
1090.UO
CXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.10
-0.00
-0.00
-0.00
-o.no
en co
IWFTI 2
PPMV IWETI
PERCENT V
289.60
125.30
125.40
70.50
27.?0
1 3.60
1.54
I.h2
2.14
2.60
;.93
J.40
THC
IWFTI
PPMV
369.00
24.50
12.00
2.70
2.10
1.60
NO NO
(WETI 2
PPMV IWETI
PPHV
ALDEHYDES SMOKE PARTICULATES
4.60
21.3P
37.80
69.10
97.10
119.10
13.20
19.60
25.50
15.00
8.00
7.30
IWFTI
PPMV
17.80
40.90
63.30
84.90
105.30
126.40
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
3
I
74
46
68
MAIS E»H
CO
Ln/iK
L* FUEL
(6.34
15.44
II. 73
5.45
1.87
0. HI
MASS EMI
HC
L B/IK
III f'JEL
?6.52
1.73
0.64
0.12
O.OH
0.05
MASS Ml
NO 2
L"1/1K
LR FIIFL
2.72
1.97
l.o?
2.01
0.90
0.71
MASS FMI
CO 2
LB/IK
LB FUEL
3035.90
3136.72
1145.53
3156.84
3162.57
3164.31
MASS EMI
NO
LP/1K
LB FUCL
0.95
4.31
5.81
B.77
1C. 98
1 1 .59
MASS EMI
NDX
Lfl/lK
LB FUFL
3.67
6.28
9.73
10.78
11.88
12.30
MASS EMI
CO
LB/HP
3.67
2.32
2.31
1.34
0.55
0.27
MASS FMI
HC
IB/MR
2.66
0.26
0.13
0.03
0.02
0.02
MASS FMI
NO 2
LB/HR
0.27
0.60
0.77
0.49
0.26
0.24
MASS FMI
C02
LB/HR
306.63
470.51
619.67
776.58
926.63
l069.->4
MASS EMI
N(l
LB/HR
0.10
0.65
1.14
2.16
3.22
3.9?
MASS EMI
NOX
LB/HR
0.37
1.24
1.92
2.65
3.48
4.16
POWER
PFRCFNT
RATED
T.O.
0
I
24
46
68
86
CO
LB/ln HP-HP
1359.200
367.642
16.5^5
5.027
1.391
0.547
LB/IK HP-HR
113564.B75
746H3.8I3
4438.891
2912.914
2354.B45
2146.805
THC
LB/IK HP-HR
991.874
41.170
0.907
0. 1 10
0.062
0.037
Nil
LB/1K hP-HR
35.4(,?
102.653
fl. I".7
8.0
-------
CAL 10 NUMBER: 33 ENGINE TYPE AND MODELi TPE 331-43 A
TEST ORGANIIATION: AIRESEARCH
SERIAL NUMBERl P-61157
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI- IDLE
MODE
TAXI-IOLE
TAKEOFF
CLIM80UT
APPROACH
TAXI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.900
0.300
0.060
FRACTIONAL
POWER
0.060
1.000
0.900
0.100
0.060
FRACTIONAL
POKER
0.060
1.000
0.900
0.300
0.060
POWER
HP
34.5
575.0
517.5
172.5
34. 5
POWER
HP
34. 5
575.0
517.5
172.5
3*. 5
POWER
HP
34.5
575.0
517.5
172.5
3*. 5
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR NODE
LB/HR LB/HR NIN.
4.270 151.082 .000 19.00
O.OS1 374.446 .000 0.50
0. 248 349.374 .000 2.50
2.150 210.526 .000 4.50
4.270 151.082 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE'
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
1.506 151.082 .000 19.00
0.043 374.446 .000 0.50
0.040 349.374 .000 2.50
0.106 210.526 .000 4.50
1.506 151.082 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/ IOOOK HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MOOE
LB/HR LB/HR MIN.
0.932 151.082 .000 19.00
4.749 374.446 .000 0.50
4.348 349.374 .000 2.50
2.114 210.526 .000 4.50
0.932 151.082 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLEl
LBS POLLUTANT/ IOOOK HP AT T.O.I
CO
MASS
LBS.
1.352
0.001
0.010
0.161
0.498
2.023
20.443
37.289
0.117
HC
MASS
LBS.
0.477
0.000
0.002
0.008
0.176
0.663
6.699
12.218
0.619
KOI
MASS
LBS.
0.295
0.040
0.181
0.159
0.10*
0.783
7.918
14.442
68.822
FUEL
MASS
LBS.
47.84
1.12
14.56
15.79
17.63
98.94
FUEL
MASS
LBS.
47.84
3.12
14.56
15.79
17.63
98.94
FUEL
MASS
LBS.
47.84
3.12
14.56
15.79
17.63
98.94
LB CO /
IK LB FUEL
28.263
0.216
O.T09
10.213
28.261
LB HC /
IK LB FUEL
9.971
0.114
0.114
0.501
9.971
LB NOX/
IK LB FUEL
6.171
12.682
12.444
10.044
6.171
ENERGY
HP-HB
10.92
4.79
21.56
12.94
4.02
54.24
ENERGY
HP-HR
10.92
4.79
21.56
12.94
4.02
54.24
ENERGY
HP-HR
10.92
4.79
21.56
12.94
4.02
54.24
LB CO /
HP-HR
0.12177
0.00014
0.00048
0.01246
0.12377
LB HC /
HP-HR
0.04367
0.00007
0.00008
0.00061
0.04167
LB NOX/
HP-HR
0.02703
0.00826
0.00840
0.01226
0.02703
IV-51
-------
OATfi: 6/ 1/71
TEST ORGANIZATION: AIRESEARCH
ENGINE SUPPLIER: AIRESEARCH
CAL ID NUMBER: 31 ENGINE TYPE AND MODEL: TPE 111-151 G
SERIAL NUMBER: P-III&S
F.NCINE TOTAL TIMFi
RATEH HORSEPOWER: 590.
0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TINE SINCE:
Nt COMPRESSOR OVFRHAUL: O. HRS
N2 CDMPRFSSOR OVERHAUL: o. HRS
COMRUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIOF VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o, HRS
N2 TURBINE OVFRHAUL: 0. HRS
fUEL: AV KEROS FUEL H/C RATIO: 1.128
OPERATIONAL OAT4 ««»««»«««»«««
INLET AIR TEMPERATURE, DEGREES f: START 12.00 FINISH 12.00
ATMOSPHERIC P3FSSURE: START 28.67 FINISH 28.67
INLEI AIR HUMIDITY, LUS H20/LU AIR: 0.0028
RELATIVE HUMIDITY: 10.00 PERCENT
SAMPLE LINE: TEMPERATURE, OFGRFFS C: -0.00, FLOW KATF, LITERS/HIM:
SAMPLE LINE TRA-ISP'mr TIME, SEC: -0.00
NUMBER OF TESTS: 6
COMMENTS:
CLOCK
TIMF
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
I/ n
?/ I
6/ 2
ll/ 6
16/1 I
70/1 t>
POhER
THRUST, LBS
OR
SHP
I.OU
3.10
171 .40
361.80
476.00
516.60
PERCENT
RATED
f.O.
0
0
?1
61
HO
101
Nl
77150.
41000.
41710.
41710.
417JO.
41 no.
ENGINE
SPEED
RPM
00
00
00
on
00
00
N2
-o.on
-0.00
-0.00
-0.00
-0.00
-0.00
MEASURED
FUEL
FLOW
LB/HR
75.00
117.00
201.00
265.00
307.00
362.00
GAS GEN
AIR FLOW
IB/SEC
2.52
6.06
6.17
6.08
6.04
5.16
0
0
0
0
0
0
CALC
F/A
. oooono
.006800
. ooi8nn
.013000
.015100
.018100
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-o.on
-0.00
-0.00
-O.on
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-n.oo
-0.00
-0.00
-o.no
-0.00
POWER
PERCENT
RATED TEMP
T.O. DEGREES
FXHAUST
GAS
o
0
21
hi
an
101
735.00
S75.no
700.00
qio.no
135.00
1050.00
EXHAUST
GAS
PXFSSURF
PS1 A
-0.00
-0.00
-0.00
-o.on
-o.no
-o.on
CO
(WET)
PPHV
3B7.10
135.(0
H I .10
41.60
16.40
CO
?
I.ETI
PERCENT V
1.74
1.44
2.06
2.51
3.02
3.45
THC
IWET)
PPMV
541.10
138.10
16.80
1 1.20
8.70
5.10
NO
1 WE T I
PPMV
3.10
6.10
11.10
32. 7C
47. BO
62.00
NO
2
1 WFTI
PPMV
7.10
1 3.80
13.10
9. 10
6.30
4.50
I HEIT I
PPMV
11 .00
11.10
32.20
41.10
54.20
66. 50
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-0.00
-0.00
-0.00
PARTICULATFS
-0.00
-0.00
-0.00
-o.oc
-O.'JO
-0.00
OTHER
PERCFNT
RATED
T.O.
M
SO
101
MASS F»|
CO
LP/IK
LH FIIFL
42.46
33. 5R
13. 11
6.32
?. 76
0.15
MAbS FMI
HC
LB/IK
LB FUFL
34.44
10.74
2.04
0.50
1.31
0.20
MASS b^l
NU2
L3/IK
LH FUEL
1.47
3.08
7.08
1.15
0.61
0.43
"ASS EMI
CO?
LB/1K
IB F1IFL
2112.86
3071 .dS
1127.87
1142.77
1148. 8?
3157.03
MASS FMI MASS FMI
NO NOX
LR/1H LB/1K
LB FUEL L9 FUEL
0.56
1.36
3.01
4. 15
5.21
5.1?
.18
.44
. 11
.3?
.11
.15
MASS EMI
CP
I.R/MR
1. IB
4.60
2.64
1.68
O.H5
0.35
MASS EM
HC
LB/HP
2.58
1.47
0.41
0.13
0.10
0.07
MASS EMI
NO 2
LR/HM
n. 11
0.42
0.42
0.31
0.21
0. 16
MASS EMI
CO. 2
LR/HR
224.46
420.84
628.70
812.B3
166.61
1141.03
MASS EM
NO
LB/HP
0.04
0. 11
0.61
1.10
1.60
2.14
MASS FMI
NOX
LB/HR
0.15
0.61
1.01
1.41
I .81
2.30
POWER
PERCENT
KATEO
T.D.
0
0
21
61
80
101
cr
Lfi/lK MP-HR
3114.785
I4nl.8?5
15. 178
4.M3
1 .780
0.571
774464.75C
115756.000
1668.041
2301.111
7030.856
1112.567
THE.
Ln/l« HP-HB
25112.144
474.567
7.3M
0.361
0.213
0. I 11
NU
LR/IK HP-MH
41.K06
60.111
3.55S
3.03H
3.360
3.51't
2
HP-HH
106.531
136.006
7 .41P
O.R4S
0.441
0.261
L9/1K HP-MR
14d.345
116.124
5.114
3.813
1.810
1.854
IV-52
-------
C«L tO NUNBERl 31 ENGINE TYPE AND NOOELl ICE 331-151 G
TEST ORGANIZATION! URESEAOCH
SERIAL NUMBER: P-91165
NODE
TA«I-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
KOOE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.060
I. 000
0.900
0.300
0.060
FRACTIONAL
POKER
0.060
1.000
0.900
0.300
0.060
FRACTIONAL
POKER
0.060
1.000
0.900
0.300
0.060
POKER
HP
35.4
590.0
531.0
1T7.0
35.4
POKER
HP
35.4
590.0
531.0
IT7.0
35.4
POKES
HP
35.4
590.0
531.0
177.0
35.4
EMISSION FUEL USAGE TIME IN
RATE RATE NT FACTOR MODE
LB/HR IB/MR MIN.
3.214 127.414 .000 19.00
0.398 355.748 .000 0.50
0.561 328.656 .000 2.50
2.560 197.618 .000 4.50
3.214 127.414 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLEI
LBS POLLUTANT/ IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR MODE
LB/HR LB/HR MIN.
0.764 127.414 .000 19.00
0.122 355.748 .000 0.50
0.118 328.656 .000 2.50
0.152 197.618 .000 4.50
0.764 127.414 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE!
LBS POLLUTANT/IK HP-HR/CVCLEl
LBS POLLUTANT/ IOOOK HP AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR MODE
LB/HR LB/HR MIN.
0.606 127.414 .000 19.00
2.245 355.748 .000 0.50
2.012 328.656 .000 2.50
1.009 197.618 .000 4.50
0.606 127.414 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK HP-HR/CVCLEl
LBS POLLUTANT/1000K HP AT T.O.I
CO
MASS
LBS.
1.018
0.003
0.024
0.192
0.375
1.612
IB. 598
28.969
0.562
' HC
MASS
LBS.
0.242
0.001
0.005
0.026
0.089
0.364
4.144
6.532
1.730
NOX
MASS
LBS.
0.192
0.019
0.084
0.076
0.071
0.441
5.085
7.920
31.704
FUEL
MASS
LBS.
40.35
2.96
13.69
14.82
14.86
86.69
FUEL
MASS
LBS.
40.35
2.96
13.69
14.82
14.86
86.69
FUEL
MASS
LBS.
40.35
2.96
13.69
14.82
14.86
86.69
LB CO /
IK LB FUEL
25.225
1.118
1.76B
12.956
25.225
LB HC /
IK LB FUEL
5.999
0.344
0.160
I. 781
5.999
LB NOX/
IK LB FUEL
4.757
6.310
6.121
5.101
4.757
ENERGY
HP-HR
11.21
4.92
22.12
11.27
4.13
55.66
ENERGY
HP-HR
11.21
4.92
22.12
I). 27
4.13
55.66
ENERGY
HP-HR
11.21
4.92
22.12
13.27
4.13
55.66
LB CO /
HP-HR
0.09079
0.00067
0.00109
0.01446
0.09079
LB HC /
HP-HR
0.02159
0.00021
0.00022
0.00199
0.02159
LB NOX/
HP-HR
0.01712
0.00360
0.00379
0.0057C
0.01712
IV-53
-------
DATE: 4/10/71
IFST ORGANIZATION: AIRFSEARCH
ENGINE SUPPLIER: AIRFSEARCH
ENGINE DATA
CAL 10 NUMBER: 32
ENGINE TYPE AND MODEL: TPE 331-151 G
RATED HORSEPOWER: 540.
0. MRS
SERIAL NUMBER:
ENGINE TOTAL TIME:
TIHE SINCF HOT SFCTIUN OVERHAUL:
TIME SINCE:
Nl COMPRESSOR OVERHAUL:
N2 COMPRESSOR OVERHAUL:
COMBUSTOR CAN REPLACEMENT:
FIRST STAGE N022LE GUIDE VANE OVERHAUL:
Nl TURBINF OVERHAUL:
N2 TURBINE OVERHAUL:
FUEL H/C RATIO:
0. MRS
0. HRS
o. HRS
0. HRS
0. HRS
0. HRS
0. HRS
FUEL: JP-5 FUEL H/C RATIO: 1.928
OPERATIONAL DATA ««««««»»««««««««.
INLET AIR TEMPFRATUHF, DEGREES F: START 69.00 FINISH 89.00
ATMOSPHFRIC PRESSURE: START 28.75 FINISH 28.75
INLET AIR HUH 1 1)1 IV, LBS H20/LB AIR: 0.0028
RELATIVE HUMIDITY: 11.00 PERCENT
SAMPLE LINE: TEMPERATURE, OEGRFFS C: -0.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPUT TIME, S FC : -0.00
NUMBFR OF TESTS: 6
COMMENTS:
CONCENTRATION RATH REPORTED WET
CLOCK
TIME
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
TEST
MODE
I/ 0
2/ I
hi 2
ll/ 6
16/11
20/16
THRUST
OR
SHP
4.
9.
158.
317.
",76.
596.
POWER
,LBS
10
50
70
30
00
60
PERCENT
RATED
T.O.
0
1
26
53
80
101
Nl
27200.
41730.
41730.
M 730.
41 730.
41 730.
FNRINE
SPEED
RPM
00
no
00
00
00
oo
N2
-0.00
-0.00
-o.no
-o.no
-0.00
-0.00
MEASURED
FUEL
FLOW
LB/HR
77.00
150.00
19B.nO
255.00
317.00
369.00
GAS GEN
AIR FLOW
LB/SEC
7.56
6.21
6.15
6.09
6.00
5.94
CALC
F/A
0.008900
0.007200
0.009500
0.012500
0.015700
0.01R500
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-o.no
-0.00
-0.00
-o.no
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-O.OC
-0.00
-0.00
TURBINF
INLET
TEMP
OEGREtS F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
0
1
26
53
80
101
EXHAUST
GAS
TFMP
DFGRFES F
698.00
59n.OO
700.00
825.00
960.00
1080.10
EXHAUST
GAS
PRFSSURE
PSIA
-0.00
-0.00
-o.on
-o.oo
-0.00
-o.on
cu
(wen
PPMV
ISO. HO
162.00
140.50
103.00
sn.oo
34. 80
CO
2
IWETI
PERCENT V
1.62
1 .44
1.87
2.37
3.14
3.64
THC
(WETI
PPMV
10)7.40
53.60
26.20
6. 10
3.00
1.30
NO
IkEll
PPMV
4.40
14.90
30.90
49.90
3R.30
in. en
NO
2
IUETI
PPMV
12.20
20. BO
21.10
21.00
10.80
7.40
NO
X
IWFT)
PPMV
16.60
35.70
52.00
70.90
99.10
119.20
ALDEHYDES
-0.00
-n.no
-0.00
-0.00
-0.00
-o.no
SMOKE
-0.00
-o.oo
-0.00
-0.00
-0.00
-o.oo
PARTICULATES
-0.00
-0.00
-0.00
-n.oo
-o.co
-0.00
POWFR
PERCENT
0 ATEO
T.O.
0
1
26
53
80
101
MASS E"l
CO
LR/ IK
LB FUEL
41. 39
22.25
14.95
8.68
3.19
1.92
U5. 5 EMI
IIC
I.B/1K
L" FUEL
67.70
4.22
I.SO
0.29
0. 11
0.04
MASS EMI
N112
I.6/ IK
in FUFL
2.28
4.69
3.69
2.91
1.1 1
0.6f
MASS EMI
C02
LB/IK
LB FUEL
2900.17
3107.54
1126.20
3139.61
3I4B.75
3150.94
"ASS EMI
NO
LB/IK
LB FUEL
0.8?
1.36
5.40
6.91
9.26
10.12
MASS EMI
NOX
LQ/1K
1 B FUFL
3.11
8.05
9.n9
9.62
10.39
10.79
MASS EMI
CM
LB/HR
3.34
1.34
2.96
2.21
1.01
0.71
MASS FMI
HC
LB/HR
5.21
0.63
0.32
0.09
0.01
O.C2
MASS [Ml
NO 2
Lfl/HR
n. 18
0.70
0.73
0. 74
0.36
0.25
MASS FMI
C02
LB/HR
223.31
466.13
618.99
H00.60
998.15
1162.70
MASS EMI
NO
LB/HR
C.06
0.50
1.07
1 .76
2.93
3.73
MASS FM
NOX
LR/HB
0.24
1.21
I.BO
2.50
3.29
3.98
POWER
PERCENT
UATFD
T.O.
0
I
26
53
80
101
CM
LP/IK HP-HR
814.844
351. 116
1R.<.51
6.979
2.125
1.186
CO
2
LB/IK HB-HK
54466.680
49066.422
3910.151
25 21.169
20)6.962
1948.172
me
LB/IK HP
1271.lil
66.5T2
1.992
0.2 17
0.073
0.025
NU
I. B/IK HP-HR
15.465
51.075
6.738
5.554
6.1A5
6.258
LH/1K HP-HR
42.880
74.091
4.601
2.337
0.754
0.414
Nil
X
LB/IK HP-HR
58.345
127.166
11.33.1
7.891
6.919
6.672
IV-54
-------
CAL 10 NUMBER: 32 ENGINE TYPE AND MODEL: TPE 331-151 c
TEST ORGANIZATION! AIRESEARCH
SERIAL NUMBER! P91168
NODE
TAXI-IDLE
TAKEOFF
CL1NBOUT
APPROACH
TAXI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH'
TAXI-IOLF
FRACTIONAL
POWER
0.060
1.000
0.900
0.300
0.060
FRACTIONAL
POKER
0.060
1.000
0.900
0.300
0.060
FRACTIONAL
POWER
0.060
1.000
0.900
0.300
0.060
POWER
HP
35. *
590.0
531.0
177.0
35.*
POKER
HP
35.*
590.0
531.0
177.0
35.*
POWER
HP
35.*
590.0
531.0
177.0
35.*
EMISSION FUEL USAGE TIME IN
RATE RATE HT FACTOR MODE
LB/HR IB/MR KIN.
3.116 159.235 .000 19.00
0.700 366.06* .000 0.50
O.B7* 339.250 .000 2.50
3.035 210.1*6 .000 *.50
3.116 159.235 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/ 1000X HP AT F.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE UT FACTOR MODE
LB/HR LB/HR MIN.
0.367 159.235 .000 19.00
0.0 366.06* .000 0.50
0.0 339.250 .000 2. SO
0.262 210.146 .000 *.50
0.367 159.235 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/ 1000K HP AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/KR LB/HR MIN.
1.325 159.235 .000 19.00
3.922 366.06* .000 0.50
3.580 339.250 .000 2.50
1.932 210.1*6 .000 *.SO
1.325 159.235 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000*. HP AT T.O.:
CO
MASS
LBS.
0.987
0.006
0.036
0.228
0.363
1.620
15.890
29.107
0.488
HC
MASS
LBS.
0.116
0.0
0.0
0.020
0.0*3
0.179
1.751
3.208
0.0
NOX
MASS
LBS.
O.*20
0.033
0.1*9
0.1*5
0.155
0.901
8.837
16.188
55.394
FUEL
MASS
LBS.
50. *2
3.05
l*.l*
15.76
18.58
101.95
FUEL
MASS
LBS.
50.42
3.05
14.14
15.76
18.58
101.95
FUEL
MASS
LBS.
50.42
3.05
14.14
15.76
18.58
101.95
LB CO /
IK LB FUEL
19.566
1.911
2.576
14.442
19.566
LB HC /
IK LB FUEL
2.302
0.0
0.0
1.2*9
2.302
LB NOX/
IK LB FUEL
8.322
10.715
10.552
9.193
8.322
ENERGY
HP-HR
11.21
4.92
22.12
13.27
4.13
55.66
ENERGY
HP-HR
11.21
4.92
22.12
13.27
4.13
55.66
ENERGY
HP-HR
11.21
4.92
22.12
13.27
4.13
55.66
LB CO /
HP-HR
0.08801
0.00119
0.00165
0.01715
0.08801
LB HC /
HP-HR
0.01036
0.0
0.0
0.001*6
0.01036
LB NOX/
HP-HR
0.037*3
0.00665
0.0067*
0.01091
0.037*3
IV-55
-------
DATE! 6/18/71
TFST ORGANIZATION: A1RESEARCH
ENGINE SUPPLIER: AIRESEARCH
ENGINE DATA
CAL ID NUMBER:
30 ENGINE TYPE UNO MOREL: TSF 231-1
RATED HORSEPOWER: 474.
ENGINE TOTAL TIME: 0. MRS
TINF SINCE HOT SECTION OVERHAUL: 0. MRS
TIKE SINCE:
SERIAL NUMBER:
2)01-10
NI COMPRESSOR OVERHAUL; o. HRS
N2 COMPRESSOR OVERHAUL: 0. MRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGF NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVFRHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL: JP-5 FUEL M/C RATIO: 1.B77
OPERATIONAL DATA «««««
INLFT AIR TEHPERATUREi DECREES f : START 110. On
ATHOSPHFRIC PRESSURE: START 28.60
INLET AIR HUMIDITY, LBS H?n/LH AIR: 0.0019
RELATIVE HUMIDITY: It. 00 PERCENT
SAKPLF. LINF.: TEMPERATURE, DEGREES C: -0.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TF.STS! 6
COMMENTS:
FINISH 110.00
FINISH 28.60
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
IEST
MODE
I/ 0
?.l \
6/ 2
ll/ 6
16/11
20/16
POWER ENGINF
THRUST, LBS PERCFNT SPFED
OR
SHP
0.0
0.0
71.70
157.80
210.20
257. 90
RATFD
r.o.
0
0
15
33
44
54
RPM
NI
32001.00
37746.00
41936.00
",5065.00
46517.00
47473.00
N2
33(52.00
449B2.00
45004.00
45011.00
44967.00
44946.00
MEASURED
FUFL
FLDH
LB/HR
66.50
9.1.50
125.60
164.40
186.50
203.50
GAS GEN
AIR FLOW
Lfl/SEC
1.61
2.20
2.72
3.13
3.35
3.52
CALC
F/A
0.013000
O.CI2900
0.014100
0.016000
0.017000
0.017700
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
FNGINE
PRESSURE
RATIO
FPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES ^
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATFfl
t.Q.
0
0
I 5
33
44
54
FXHAUSt
GAS
TEMP
DEGBFES E
910.00
935.00
995. no
IC70.00
11 on. on
nao.no
FXHAUST
GAS
PRESSURE
PS1A
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
IWETI
PP"V
345.00
161.00
104.10
75.7C
67.70
61 .40
CO
f
(WET)
PERCENT V
7.46
2.50
2.79
3.05
3.25
3.59
THC
IWETI
PPMV
99.00
21.50
11.80
7.80
8. 10
7.60
NO
IkETI
PPMV
16.80
31 .00
55. 10
03.00
103.00
122. 70
NU
2
IWETI
PPMV
14.40
11.50
10.70
a. no
8.70
12.60
Nil
X
IWCTI
PPMV
31.20
42.50
65.90
91.10
111.70
135.30
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATEO
T.O.
15
J3
44
54
1/vSS EMI
cn
LB/IK
LB FUFL
27.76
12.88
7.49
4.99
3. fl"
3. 44
MASS EMI
HC
Lfl/K
LI FUEL
4.56
0.99
0.49
0.29
0. 29
O.Z4
MASS EMI
N02
LB/IK
LB FUEL
1.90
1.51
1.26
0.95
'1.88
1. 16
MASS EMI
crt2
LB/1K
LB FUFL
3109.60
3142.79
3152.63
3157.09
3I5B.85
3159.66
.MASS FMI
NO
LB/IK
LR FUEL
2.22
4.07
6.51
8.98
10.47
1 1.79
MASS EMI
NQX
Lfl/lK
LB FUFL
4.12
5.59
7.78
9.93
11.35
12.45
MASS Frtl
CO
IB/HP
1.90
1.20
0.94
C.8?
0.72
U.70
MASS EMI
HC
LB/Mk
0.31
0.09
0.06
0.05
0.05
0.05
MASS EMI
Nfl2
LB/HR
0.13
0. 14
0.16
0. 16
0. 16
0.24
MASS FMI
cn2
LB/HO
213.01
293.85
395.97
519.02
589. 12
642. 99
MASS EMI
NO
LB/HR
0. 15
0.38
O.B2
1.48
1.95
2.31
MASS EM
NOX
LH/HR
0.28
0.52
0.98
1.63
2.12
2.53
POWER
PERCENT
RATFO
r.n.
Lfl/H HP-HO
Lfl/lK MP-H'<
THC
LI/IK HP-HR
HCIRSEPOWFP-HR ra THOIJST-HR OASIS NOT C ALCUL A9LF««
HIPStPnwE^-Ha nw THRUST-MR BASIS NOT CALCULABLE***
1> 13.115 5522. r»9B O.rtSI
11 5.196 328'!.13Z 0.307
44 1.441 2B02.687 0.255
54 2.714 2491.176 0.192
NU
LB/IK HP-HR
I 1.402
9.157
9. ZflS
8.901
LR/1K HP-HR
7.214
0.19?
0.784
0.915
NO
X
LB/IK HP-HR
13.637
10.149
10.070
9.B23
IV-56
-------
CAL ID NUMBER: 30 ENGINE TYPE AND MODEL: TSE 231-1
TEST ORGANIZATION; AIRESEARCH
SERIAL NUMBER: 2301-10
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TIKI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IOLF
FRACTIONAL
PONER
0.060
1.000
0.900
0.300
0.060
FRACTIONAL
POWER
0.060
1.000
0.900
0.300
0.060
FRACTIONAL
POWER
0.060
1.000
0.900
0.300
0.060
PONER
HP
28.4
47*. 0
426.6
142.2
28.4
POWER
HP
28. 4
474.0
426.6
142.2
2S.4
POWER
HP
28.4
474.0
426.6
142.2
28.4
EMISSION FUEL USAGE TINE IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
0.486 49.676 .000 19.00
0.287 260.734 .000 0.50
0.400 247.922 .000 2.50
0.853 161.178 .000 4.50
0.486 49.676 .000 7.00
TOTAL FOR CVCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
L8S POLLUTANT/1000K HP AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
0.035 49.676 .000 19.00
0.020 260.734 .000 0.50
0.029 247.922 .000 2.50
0.052 161.178 .000 4.50
0.035 49.676 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
0.148 49.676 .000 19.00
4.51* 260.734 .000 0.50
4.027 247.922 .000 2.50
1.544 161.178 .000 4.50
0.148 49.676 .000 T.OO
TOTAL FOR CYCLE)
LBS POLLUTANT/IK LB FUEL/CYCLE'
LBS POLLUTANT/ IK HP-HR/CYCLE:
LBS POLLUTANT/1000K HP AT T.O.I
CO
MASS
LBS.
0.154
0.002
0.017
0.064
0.057
0.294
6.370
6.569
0.505
HC
MASS
LBS.
0.011
0.000
0.001
0.004
0.004
0.020
0.443
0.457
0.356
NOX
MASS
IBS.
0.047
0.038
0.168
0.116
0.017
0.385
8.357
B.6I9
79.365
FUEL
MASS
LBS.
15.73
2.17
10.33
12.09
5.80
46.12
FUEL
MASS
LBS.
15.73
2.17
10.33
12.09
5.80
46.12
FUEL
MASS
LBS.
15.73
2.17
10.33
12.09
5.80
46.12
LB CO /
IK LB FUEL
9.788
1.102
1.615
5.292
9.788
LB HC /
IK LB FUEL
0.705
0.078
0.116
0.322
0.705
LB NOX/
IK LB FUEL
2.982
17.314
16.242
9.581
2.982
ENERGY
HP-HR
9.01
3.95
17.77
10.66
3.32
44.71
ENERGY
HP-HR
9.01
3.95
17.77
10.66
3.32
44.71
ENERGY
HP-HR
9.01
3.95
17.77
10.66
3.32
44.71
LB CO /
HP-HR
0.01710
0.00061
0.00094
0.00600
0.01710
LB HC /
HP-HR
0.00123
0.00004
0.00007
0.00036
0.00123
LB NOI/
HP-HR
0.00521
0.00952
0.00944
0.01086
0.00521
IV-57
-------
OATf: 7/20/Tl
TEST ORGANIZATION: s H B I TWA
ENGINE SUPPLIER: T H A
ENGINE DATA
CAL ID NUMRFR: 119
FNGINE TYPE AND MODEL1 CJ-B05-3A
SERIAL NUNHFRI GE-I61-J02
RATED THRUST: 11200.
FNGINE TOTAL TIME: 1961B. HAS
TIHE SINCE HOT SECTION OVERHAUL: 0. H8S
TIKE SINCE:
NI COMPRESSOR OVERHAUL: o. HRS
N2 COMPRESSOR OVERHAUL: -o. HRS
coMBimnR CAN REPLACEMENT: o. HRS
FIRST STAGE NOZILE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL H/C RATIO! 2.020
75.00
29.0*
FUEL: JP-4 IF
OPERATIONAL DATA ««««««
INLET AIH TEHPERATUREi OFG1FES F: START 74.00 FINISH
ATHOSPHFRIC PRESSURE: START 79.04 FINISH
INLET AIR HUMIDITY, IBS H20/LR AIR: 0.0111
RELATIVF. HUMIDITY: 56.00 PERCFNI
SAMPLE L1NF.: HMPFRATURE, DEGREFS C: 150.00, FLOW RATF, LITFRS/MIN:
SAMPLE LINF TRANSPORT TIME, SFC: 1.00
NUMBER OF TESTS: 4
COMMENTS:
F/A «ND AIRFLOW CALCULATED FROM FXHAUST COMPOSITION FOR LAST RUN. N02
OETERMINFO RY SUBTRACTION.
POWER
PERCENT
RAIFD
T.O.
85
3
POWFB
PERCENT
RATED
T.n.
6B
76
85
3
POWFR
PERCENT
RATED
T.O.
68
76
85
TEST
MOPE
I/ 0
2/ 1
3/ 2
4/ 3
EXHAUST
GAS
TFMP
IF.GDEES F
957.00
1 074 .00
1 100.00
777.00
MASS F.MI
Cll
I.B/ IK
LB F'ltL
4.52
3.54
3.10
54.22
co
POWER ENGINE MEASURED GAS GEN
THRUST, LBS PERCENT SPEFO FUFL AIH FLOW
OR RATED RP" FLOW IB/SEC
SHP
7720.00
8620.00
9620.00
400.00
EXHAUST
GAS
T.O. Nl N2 LB/HR
6B 7080.00 70BO.OO 6390.00 145.00 0.
76 718C.OO 7180.00 7220.00 152.80 0.
85 7280.00 7780.00 D140. 00 156.50 0.
3 4490.00 4490.00 1090.00 36.00 0.
CO CO THC NO NO
(HEM 2 IWETI IWFTI 2
PRESSURE PPMV IUFT1 PPMV PPMV IWETI
PSIA
15.60
17.70
20. 10
0. 40
"ASS EMI
HC
Lf/IK
LB FUEL
0.09
0.0
0.0
70.21
LH/ IKKTH-HP
3.
2.
2 ,
147.
740
V64
67. )
744
PERCENT V PPMV
57.00 7.51 2.00 53.00 6.00
',8.00 2.70 0.0 62.00 7.00
45.00 2.89 0.0 74.00 9.00
464.00 1.63 102.00 1.00 8.00
MASS EMI MASS EMI MASS [Ml MASS FMI MASS FMI MASS
N12 C02 NO N0< CO HC
LB/1K LB/1K LB/1K LB/IK LW/HR LB/
LI FUEL IB fUFL LR FUEL LB FUEL
0.78 JI25.I19 6.90 7.68 2". 97 0.
0.85 3127.66 7.51 fi.36 25.55 0.
0.91 3I2H..17 8.37 9.2R 25.24 0.
1.54 2992.61 0.19 1.73 59.10 22.
CO 1HC NO
2
CALC
F/A
012200
013100
014500
008400
NO
X
IWFTI
PPMV
59.00
69.00
82.00
9.00
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIO
DEGREES f EPR
-0.00 2.10
-0.00 2.24
-0.00 2.41
-0.00 -0.00
ALDEHYDES SMOKE
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
FMI MASS EMI MASS EMI MASS
Hk
5R
0
0
01
NO
2
Lil/ltUTH-HR Lfl/IK«TH-H« LB/1KHTH-HR LB/1KHTH-HR
2517.365 0.075 5.711
2619.704 0.0 6.289
2647. OH2 0.0 7.086
8154. R55 55.07.1 0.523
C.647
0.710
0. 766
4. 184
NO? CU2 NO
LB/HR LB/HR LB/
4.99 19974.46 44.
6.17 27581.85 54.
7.37 25464.93 6H.
1.67 1261.94 0.
NO
X
LB/IKHTH-HR
6.159
6.999
7.832
4. 707
TURBINE
INLET
TEMP
DEGREES F
-n.oo
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
EMI MASS EMI
NOX
MR LB/HR
09 49.08
21 60.33
16 74.53
21 1.88
IV-58
-------
CAL ID NUMBER: 111 ENGINE TYPE AND MODEL! CJ-805-3*
TEST ORGANIZATION: S M R I TNA
SERIAL NUMBER! 06-161-302
MODE FRACTIONAL
POKER
TAXI-IDLE 0.0*0
TAKEOFF 1.000
CLIMBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.0*0
MODE FRACTIONAL
POHER
TAXI-IDLE 0.0*0
TAKEOFF 1.000
CLINBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.040
MODE FRACTIONAL
POHER
TAXI-101E 0.040
TAKEOFF 1.000
CLINBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.040
POWER
1 TH
448.0
H 200.0
9520.0
4480.0
448.0
PDNER
1 TH
448.0
11200.0
9520.0
4480.0
448.0
POHER
1 TH
448.0
11200.0
9520.0
4480.0
448.0
EMISSION FUEL USAGE TIME IN
RATE RATE NT FACTOR NODE
LB/HR LB/HR MIN.
48.149 880.962 .000 19.00
26.189 9801.957 .000 O.TO
25.857 8323.367 .000 2.20
40.743 3796.427 .000 4.00
48.149 880.962 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE MT FACTOR MODE
LB/HR LB/KR MIN.
17.791 880.962 .000 19.00
0.503 9801.957 .000 0.70
1.243 8323.387 .000 2.20
1.688 3798.427 .000 4.00
17.791 880.962 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE HT FACTOR MODE
LB/HR LB/HR MIN.
1.621 SBC. 962 .000 19.00
104.398 9801.957 .000 0.70
79.004 8321.387 .000 2.20
18.462 3798.427 .000 4.00
1.521 880.962 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LRS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
CO
MASS
LBS.
15.247
0.306
0.948
2.716
5.617
24.835
23.550
25.536
2.728
HC
MASS
LBS.
5.634
0.006
0.046
0.113
2.076
7.873
7.466
8.096
0.524
NOX
MASS
IBS.
0.482
1.218
2.897
1.231
0.177
6.004
5.694
6.174
108.748
FUEL
MASS
LBS.
278.97
114.36
305.19
253.2)
102.78
1054.52
FUEL
MASS
LBS.
278.97
114.36
305.14
253.2)
102.78
1054.52
FUEL
MASS
LBS.
278.97
114.36
305.19
253. 23
102.78
1054.52
LB CO /
IK LB FUEL
54.655
2.672
3.107
10.726
54.655
LB HC /
IK LB FUEL
20.195
0.051
0.149
0.444
20.195
LB NOX/
IK LB FUEL
1.726
10.651
9.492
4.860
1.726
ENERGY
f TH-HR
141.87
130.67
349.07
298.67
52.27
972.53
ENERGY
1 TH-HR
141.87
130.67
349.07
298.67
52.27
972.53
ENERGY
i TH-HR
141.87
130.67
349.07
298.67
12.27
972.53
IB CO /
TH-HR
0.10748
0.00234
0.00272
0.00909
0.10748
LB HC /
TH-HR
0.03971
0.00004
0.00013
0.00038
0.03971
LB NOX/
1 TH-HR
0.00339
0.00932
0.00830
0.00412
0.00339
IV-59
-------
DATE; 7/20/71
TEST ORGANUATION: S H R 1 THA
ENGINE SUPPLIER: THA
ENGINE DATA
CAL ID NUMBER: 120 ENGINE TYPF AND MOOFL: CJ-805-3A
RATED THRUST: 11200.
ENGINE TOTAL TIME: 19618. MRS
TINE SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: o. HRS
NZ COMPRESSOR OVERHAUL: -o. MRS
CONBUSTOR CAN REPLACEMENT: o. HRS
FI»ST STAGE NOiUE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: -0. HRS
SERIAL NUMBER: GF-i6i-302
FUEL H/C RATIO: 2.020
80.00
?9.02
FUEL: jp-4 TF
OPERATIONAL DATA «»«»»«««»
INLET AIR TEMPERATURE, DEGREES F: START 76.00 FINISH
ATMOSPHERIC PRESSURE: START 21.01 FINISH
INLET AIR HUMIDITY, L1S H20/LB AIR: 0.0121
RELATIVE HUMIDITY: si.no PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/MIN:
SAMPLF LINE TRANSPORT TIMF, SEC: 0.60
NUMBER OF TESTS: 4
COMMENTS:
F/A AND AIDFinu CALCULATED FROM EXHAUST COMPOSITION FOR FOURTH RUN. NO2
DETERMINED BY SUBTRACTION.
42.50
ELAPSFD
TIME
0.0
5.00
8.50
11.00
TEST
MODE
I/ 0
2/ 1
V 2
4/ 1
POWER
THRUST, IRS PERCENT
OR RATED
SHP
7720.00
6660.00
9BOO.OO
180.00
T.O.
68
77
87
1
ENGINE
SPEED
RPM
NI
7100.00
7210.00
7650.00
44i)0.00
N2
7100.00
7210.00
7650.00
4490.00
MEASURED
FUEL
FLOW
LB/HR
6390.00
7480.00
8370.00
1080.00
GAS GEN
AIR FLOW
LB/SEC
144.90
153.00
160. 10
38.00
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.012200
0.013600
0.014500
0.007900
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINF
PRESSURE
RATIO
FPR
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEHP
OEGRFFS f
-0.00
-0.00
-0.00
-0.00
POHEP
PERCENT
RATED
T.O.
6B
77
87
3
EXHAUST
GAS
TEPP
DEGREES F
959.00
1045.00
1126.00
734.00
FXHAUST
GAS
PRESSURE
PSI A
15.50
17.70
20.20
0.40
CO
I MET)
PPPV
52.00
43.00
43.00
397.30
CO.
2
IHETI
PERCENT
2.34
2.62
2.91
1.52
THC
IWETI
PPMV
4.00
0.0
0.0
153.00
NO
IHETI
PPHV
52.00
64.00
HI.00
I .00
NO
2
IHET)
PPMV
5.00
7.00
6.00
7.00
NO
X
IHET)
PPMV
57.00
71.00
87.00
8.00
ALDEHYDES SMOKE PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POHER
PERCENT
RATED
T.O.
68
77
87
3
MASS CMI
CO
LB/IK
LB F'lEl
4.42
3.27
2.94
49.63
MASS EMI
HC
LB/IK
Lfl FUEL
0.19
0.0
0.0
25.28
MASS EMI
N02
LR/1K
LB FUEL
0.70
0.87
0.67
1 .44
PASS FMI
C02
LG/IK
LB FUEL
J125.76
112R.lt
3I2B.62
2985.91
MASS EMI
NO
LB/IK
LB FUEL
7.26
7.99
9.10
0.21
LB/IK
Lfl FUEL
7.96
8.86
9.78
1.64
"ASS [Ml
CO
LB/HR
2R.25
24.44
24.63
53.61
MASS EMI
HC
LB/HR
1.24
0.0
0.0
27.30
MASS EMI
NO 2
LH/HR
4.46
(,.54
5.64
1.55
MASS EMI
C02
LR/HR
19973.61
23398.21
26186.54
3224.78
MASS EMI
NO
LR/HR
46.40
59.75
76.20
0.22
MASS EMI
NOX
LB/HR
50.86
66.29
81.84
1.77
POWER
PERCENT
RATED
T.O.
68
77
HI
3.659
2.B22
2.511
141.067
LB/1«TH-H«
2537.255
2701.875
2672.096
14H6.270
THf
L R/1KOIH-HR
0.161
0.0
o.n
71.R38
NO
LR/1K«TM-HK
6.010
6.900
7.775
0.584
LB/ IKJTH-HR
0.578
0.755
0.576
4.0P6
NO
X
LB/!K«TH-HR
6.588
7.654
8.351
4.669
IV-60
-------
CAL ID NUMBER: 120 ENGINE TYPE AND MODEL: CJ-SOS-SA
TEST ORGANIZATION: s K R I TKA
SERIAL NUMBER I CE-161-302
MODE FRACTIONAL
POKER
TAXI-IDLE
TAKEOFF
CLIN80UT
APPROACH
TAXI-IDLE
0.040
1.000
0.850
0.400
0.040
POKER
> TH
448. 0
11200.0
4520.0
4480.0
448.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
46.422 442.364
28.201 10254.402
25.301 8574.402
34.332 3437.208
46.422 442.364
USAGE TIME IN
KT FACTOR NODE
MIN.
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK IB
LBS POLLUTANT/1000K
MODE FRACTIONAL
POKER
TAXI-IDLE
TAKEOFF
CLIM80UT
APPROACH
TAXI-IDLE
0.040
1.000
O.B50
0.400
0.040
POKER
f TH
448.0
11200.0
4520.0
4480.0
448. 0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
23.402 442.364
0.012 10254.402
0.384 8574.402
4.175 3437.208
23.402 442.369
.000 14.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLf.1
LB TH AT T.O.:
USAGE TIME IN
KT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
MODE
TAXI-IOLE
TAKEOFF
CLIMB OUT
APPROACH
TAXI-IOLE
FRACTIONAL
POKER
0.040
1.000
0.850
0.400
0.040
POKER
TH
448.0
11200.0
4520.0
4480.0
448.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.570 442.364
115.527 10254.402
84.564 8574.902
17.023 3437. 20B
1.570 442.364
.000 14.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00 '
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.I
USAGE TIME IN
KT FACTOR MODE
MIN.
TOTAL FOR CYCLE1
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 14.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE i
TH-HR/CYCLEl
LB TH AT T.O.:
CO
MASS
LBS.
14.854
0.324
0.428
2.284
5.474
23.878
22.280
24.553
2.938
' HC
MASS
LSS.
7.411
0.000
0.014
0.278
2.730
10.433
4.735
10.728
0.013
NOX
MASS
LBS.
0.447
1.348
3.101
1.135
0. 183
6.264
5.844
6.441
120.340
FUEL
MASS
LBS.
248.42
114.64
314.60
224.15
104.44
1071.74
FUEL
MASS
LBS.
248.42
114.64
314.60
224.15
109.44
1071.74
FUEL
MASS
LBS.
298.42
114.64
314.60
224.15
104.44
1071.74
LB CO /
IK LB FUEL
44.742
2.750
2.444
4.488
44.742
LB HC /
IK LB FUEL
24.833
0.001
0.045
1.215
24.833
LB NOX/
IK LB FUEL
1.666
11.265
4.856
4.453
1.666
ENERGY
1 TH-HR
141.87
130.67
344.07
248.67
52.27
472.53
ENERGY
< TH-HR
141.87
130.67
344.07
248.67
52.27
472.53
ENERGY
f TH-HR
141.87
130.67
344.07
248.67
52.27
472.53
LB CO /
f TH-HR
0.
0.
0.
0.
0.
10474
00252
00266
00766
10474
LB HC /
TH-HR
0.
0.
0.
0.
0.
05224
00000
00004
00043
05224
LB NOX/
f TH-HR
0.
0.
0.
0.
0.
00350
01031
00888
003BO
00350
IV-61
-------
DATE: 1/26/71
TEST ORGANIZATION: SUB
FNGINE SUPPLIER: TWA
FNGINf DATA
CAL 10 HUNKER: 281 ENGINE TYPE AND HODFL: CJ-815-3A
BATED THRUST: 11200.
ENGINE TOTAL TINE: 0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIKE SINCE:
NI COMPRESSOR OVERHAUL: o. MRS
N2 COMPRESSOR OVERHAUL: 0. HRS
CUHPUST04 CAN REPLACEMENT: 0. HRS
FIRST .STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINF OVERHAUL: o. HRS
FUEL: jp-4 TF FUEL H/C RATIO: 2.020
OPERATIONAL DATA ****%«**««*»
INLET AIR TEMPERATURE, OEGRCES F: START 64.00 FINISH
ATMOSPHERIC PRESSURE: START 29.01 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0099
RELATIVE HUMIOITv: 73.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 150.00. FLOW RATE, LITFRS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER HF TESTS: 4
COMMENTS:
F/A AND AIRFLOW CUCULATED FROM EXHAUST COMPOSITION ON 4TH RUN. N02
DETERMINED BY SUBTRACTION.
SERIAL NUMBER: GE-161-156
6S.OO
29.01
42.50
ELAPSED
TIME
0.0
9.00
16.00
20.00
POWER
PERCENT
RATED
T.H.
74
Bl
90
3
PUMFR
PERCENT
RATED
T .n.
74
Bl
90
3
POWFR
PFRCENT
R ATEn
i.n.
74
HI
90
1
IFST
MODE
I/ 0
2/ 1
3/ ?.
4/ 3
EXHAUST
GAS
TEMP
OEGRFFS f
96b.OO
1011 .00
1 110.10
716.00
MaiS FMI
cn
LB/ 1 K
LB FUFl
4.61
3. J6
3.30
61 .44
r. n
POWER
THRUST, L9S
OR
SHP
8360.00
9100.00
10120.00
400.00
EXHAUST
Gas
PRESSURE
PSIA
17.00
18.70
21.00
0.50
MASS FMI
HC
L B/ 1 K.
LB FUFL
0.0
0.0
0.0
19.96
PERCENT
RATED
ENGINE
SPEED
4PM
T.O. M N2
74 7090
81 7180
90 7170
1 4530
CO
IWET)
PPMV
60.00
51. On
48.00
573.00
MASS FMI MASS
.00 7090.00
.00 7180.00
.00 7370.00
.00 4530.00
CC
2 1
(WETI
PERCENT V
2.5R
2.61
2.90
MEASURED
FUEL
FLOW
LB/HR
6790.00
74BO.OO
8620.00
1060.00
THC NO
GAS GEN
AIR FLOW
LB/SEC
CALC
F/A
COMPRESSOR FNGINE
DISCHARGE PRESSURE
TEMP
DEGREES F
153.60
156.80
161.00
32.40
NO
WET) IWET) 2
PPMV PPM
0.0 51.
0.0 55.
0.0 81.
1.77 325.00 3.
mi vuss FMI
NU2 CO? NO
LI/IK LB/IK LB/IK
LB FUEL LB FUEL LP FUEL
0.25 3125.
0.25 3127.
0.34 11 2 P.
1.41 2981.
cn
?
L1/1K1 TM-MR LB/lKITH-H't
1.
1.
7.
162.
758
172
807
H13
25IH.917
2570.470
2664.419
7902. I '2
97 6.46
IB 6.84
06 9.13
95 0.51
TIIC
LB/IKKTH-HP.
0.0
0.0
0.0
5P.889
MASS FMI
NOK
L B/ IK
LB FUEL
6.71
7.09
9.47
1.94
NO
V IHETI
PPMV
00 2.00
00 2.00
oo i.oo
oo .1 . no
0.012300
0.013200
0.014700
0.009100
NO
X
IWETI
PPMV
53.00
57.00
84. On
11.00
-0.
-0.
-0.
-0.
00
00
00
00
RATIO
EPH
2.20
2.28
2.47
-0.00
ALDEHYDES SMOKF
-0.
-0.
-0.
-0.
MASS F-MI MftSS EMI MASS FMI
CO
L 0/HR
11.47
2B.87
2B.40
65.11
HC
0.0
0.0
0.0
21. 16
NO
?
LB/1KKTH-HH L*/1K»TH-HR
5.
5.
7.
1.
247
620
780
400
0.206
0.204
0.288
1. 734
NO 2
1.72
I.B6
2.92
1.49
00 -0
00 -0
00 -0
00 -0
MASS FMI
CI12
21225.1".
23191.28
26961.91
1160.67
NU
X
.00
.00
.00
.00
MASS
NO
43.
51.
7B.
0.
TURBINF
INLET
TEMP
OT.REES F
-0.110
-0.00
-0.00
-0.00
PARtlCULATES
-0.00
-0.00
-0.00
-0.00
EMI MASS EMI
NOX
86 45.58
14 53.00
73 81.65
56 2.05
LB/ IK1TH-HR
5.452
5.B24
3. 063
5.134
IV-62
-------
CM. ID NUMBER: 28i ENGINE TYPE AND MODEL: CJ-SOS-SA
TEST ORGANIIATION: s W R I TWA
SERIAL NUMBER: GE-161-156
MODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-1016
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
0.0*0
1.000
0.850
0.400
0.0*0
FRACTIONAL
POWER
0.040
1.000
0.850
0.400
0.040
FRACTIONAL
POWER
0.040
1.000
0.850
0.400
0.040
POKER
TH
448.0
11200.0
9520.0
4460.0
448.0
POWER
1 TH
448.0
11200.0
4520.0
4480.0
448.0
POWER
TH
448.0
11200.0
4520.0
4480.0
448.0
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR IB/MR MIN.
82.466 1115.998
24.354 10244.773
29.243 8469.777
48.659 4237.141
82.466 1111.998
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUT ANT/ 1 COOK
EMISSION FUEL
RATE RATE WT
IB/MR LB/HR
21.500 1115.998
0.829 10244.773
0.615 8469.771
0.418 423T.I41
21.500 1115.998
TOTAL FOR CVCLEl
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
2.042 1115.998
150.025 10244.773
73.870 8469.777
17.655 4237.141
2.042 1115.998
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
L8S POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE I
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLEi
TH-HR/CYCLEI
LB TH AT T.Q.t
USAGE TIME IN
FACTOR MODE
MIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.I
CO
MASS
LBS.
26.114
0.284
1.072
3.244
9.621
40.336
33.721
41.475
2.537
HC
MASS
LBS.
6.808
0.010
0.023
0.028
2.508
9.377
7.839
9.641
0.863
HOX
MASS
IBS.
0.647
1.750
2.709
1.177
0.238
6.521
5.452
6.705
156.276
FUEL
MASS
LBS.
353.40
119.52
310.56
282.48
130.20
1196.16
FUEL
MASS
LBS.
353.40
119.52
310.56
2BZ.48
130.20
1196.16
FUEL
MASS
LBS.
353.40
119.52
310.56
282.48
130.20
1196.16
LB CO /
IK LB FUEL
73.894
2.377
3.453
11.484
73.894
LB HC /
IK LB FUEL
19.265
0.081
0.073
0.099
14.265
LB NOX/
IK LB FUEL
1.830
14.644
8.722
4.167
1.830
ENERGY
1 TH-HR
141.87
130.67
349.07
248.67
52.27
472.53
ENERGY
1 TH-HR
141.87
130.67
349.07
298.67
52.27
972.53
ENERGY
TW-HR
141.87
130.67
349.07
298.67
52.27
972.53
LB CO /
1 TH-HR
0.18408
0.00217
0.00307
0.01086
O.IB40B
LB HC /
1 TH-HR
0.04799
0.00007
0.00006
0.00009
0.04799
LB NOX/
TH-HR
0.00456
0.01340
0.00776
0.00394
0.00456
IV-63
-------
OATEI 8/ »/7l
TEST ORGANIZATION: S w R
ENGINE SUPPLIED: TWA
ENGINE DATA
C«l 10 NUMBER: 309
ENGINE TYPE AND HOPEI: CJ-805-3A
SERIAL NUMBFR: GEK.I loe
RATED THRUST: 11200.
ENGINE TOTAL TINE: 72738. HRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TINE SINCE:
NI COMPRESSOR OVERHAUL: o. HRS
NZ COMPRESSOR OVERHAUL: -o. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: -o. HRS
FUEL H/C RATIO: 2.020
75.00
29.00
FUEL: jp-4 TF
OPERATIONAL DATA «».
INLET AIR TEMPERATURE. DEGREES F: START 75.00 FINISH
ATMOSPHERIC PRESSURE: START 29.06 FINISH
INLFT AIR HUMIDITY, LRS HZO/LB AIR: 0.0153
RELATIVE HUMIDITY: 72.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREFS C: 150.00, FLOW RATE, LITERS/MIN: 42.50
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER (IF TFSTS: 4
COMMENTS:
F/A AND AIRFLOW CALCULATED FROM EXHAUST COMPOSITION FOB FOURTH RUN. N02
DETERMINED BY SUBTRACTION. THIS TCST IS THF FIRST OF FOUR RUN ON THIS FNC.INE
THE FUEL USED DURING THIS TEST CONTAINED NO CI-2.
ELAPSED
TIME
0.0
4.00
10.00
15.00
TEST
MODE
I/ 0
2/ 1
3/ 2
4/ 3
POWER
THRUST, LBS PERCENT
OR RATED
SHP
8080.00
3820.00
10000.00
400.00
T.O.
77
78
K9
3
ENGINE
SPEED
RPM
NI
7120.00
7180.00
7.180.00
4510.00
N2
7120.00
7iea.no
7380.00
4510.00
MEASURED
FUEL
FLOW
LB/HR
6670.00
7300.00
S590.00
1090.00
GAS GEN
AIR FLOW
LB/SEC
148.20
152.10
162.50
43.90
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.012500
0.013300
0.014700
0.006900
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURF
PATIO
EPR
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POUFR EXHAUST
PERCENT G»S
RATED TEMP
T.O. DEGREES f
72
78
89
3
968.00
1022.00
I17S.OO
716.00
EXHAUST
GAS
PRESSURE
PSIA
16.50
17.90
20.80
0.50
CO
I WET I
PPMV
5?.00
48.00
46.00
472.00
CO
2
(WET)
PERCENT
2.55
2.70
2.96
1.11
THC
(WET)
PPMV
0.0
0.0
0.0
140.00
NO
(WET)
PPMV
53.00
61.00
75.00
3.00
NO
2
(WET)
PPMV
7.00
5.00
6.00
4.00
ALDEHYDES SMOKE PARTICULARS
1WETI
PPMV
60.00
66.00
81.00
7.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.n.
72
79
89
3
MASS EMI
CO
Lfl/lK
LR FUFU
4.06
3.54
1.09
67. 66
MASS EMI
HC
LB/1K
Lfl FUEL
0.0
0.0
0.0
27.91
MASS EMI
N02
LB/IK
LB FUEL
0.90
0.61
0.66
0.94
MASS EMI
C02
LB/IK
L8 FUEL
3126.87
3127.68
3128. 3H
2950.17
MASS EMI
MO
LB/IK
LE FUFL
6.79
7.39
8.29
0.71
MASS EMI
NOX
LB/IK
LB FUEL
7.69
7.99
8.95
1.65
MASS EMI
CO
Lfl/HK
27.07
25.83
26. 5S
73.75
MASS CM
HC
LB/HF
0.0
0.0
0.0
30.4?
MASS EMI
N02
LB/H»
5.99
4.42
5.69
1.03
MASS EMI
CD 2
LB/HR
20856.19
22832.06
26872.78
3215.90
MASS EMI
NO
LB/HB
45.32
53.93
71.18
0.77
MASS EMI
NOX
LR/HR
51.30
5H.35
76. 86
1.80
POWER
PERCENT
HATFO
T.O.
72
78
89
3
CO
t.B/ IKiTH-HP
1.350
7.929
7.659
184.163
LB/ 1,
-------
CAL ID NUNBERl 309 ENGINE TYPE AND HODELi CJ-805-3A
TEST ORGANIZATION! S H R I TNA
SERIAL NUMBER: GE161 ica
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POKER
0.0*0
1.000
0.850
0.400
0.0*0
POKER
TH
440.0
11200.0
9520.0
4480.0
448.0
EMISSION FUEL
RATE RATE
L8/HR LB/HR
70.769 1085. 125
25.349 9531. 4T7
26.794 7993.285
31.848 3959.430
70.769 1085.125
NT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
NODE
TAXI-IOLE
TAKEOFF
CLIN80UT
APPROACH
TAXI-IOLE
FRACTIONAL
POKER
0.0*0
1.000
0.850
O.*00
0.040
POKER
1 TH
446. 0
11ZOO.O
9520.0
44BO.O
448.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
14.269 1085.12!
0.535 9531.477
0.603 7993.281
1.867 3959.430
34.269 1085.125
HT
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.040
1.000
0.690
0.400
0.040
POWER
1 TH
44B.O
11200.0
9520.0
4480.0
448.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.220 1085.125
100.352 9531.477
70.458 7993.285
18.434 3959.430
1.220 1085.125
KT
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IOOOK
USAGE TINE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLEI
LB TH AT T.O.:
USAGE TIKE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLEl
LB TH AT T.O.I
USAGE TINE IN
FACTOR NODE
MIN.
.000 19.00
.000 O.TO
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLEl
LB TH AT T.O.I
CO
MASS
LBS.
22.410
0.296
0.982
2.123
8.256
34.068
29.924
35.010
2.641
HC
MASS
LBS.
10.852
0.006
0.022
0.124
3.998
15.003
13.178
15.426
0.557
NOX
MASS
LBS.
0.386
1.171
2.583
1.229
0.142
5.512
4.842
5.668
104.533
FUEL
NASS
LBS.
343.62
111.20
293.09
263.96
126.60
1138.47
FUEL
NASS
LBS.
343.62
111.20
293.09
263.96
126.60
1138.47
FUEL
MASS
LBS.
343.62
111.20
293.09
261.96
126.60
1138.47
LB CO /
IK LB FUEL
65.217
2.660
3.352
8.044
65.217
LB HC /
IK LB FUEL
31.581
0.056
0.075
0.471
11.581
LB NOX/
IK LB FUEL
1.125
10.528
8.815
4.656
1.125
ENERGY
f TM-HR
141.87
130.67
349.07
298.67
52.27
972.53
ENERGY
f TH-HR
141.87
130.67
149.07
298.67
52.27
972.53
ENERGY
I TH-HR
141.87
130.67
349.07
298.67
52.27
972.53
LB
I
0
0
0
0
0
LB
0
0
0
0
0
L6
0
0
0
0
0
CO /
TH-HR
.15797
.00226
.00281
.00711
.15797
MC /
TH-HR
.07649
.00005
.00006
.00042
.07649
NOX/
TH-HR
.00272
.00896
.00740
.00411
.00272
IV-65
-------
DATE: 8/ 4/71
{fit ORGANIZATION: S K R I TWA
ENGINE SUPPLIER: TWA
ENGINE DATA
c»i 10 NUMBER: 310
ENGINE TVPE AND MODEL: CJ-805-3A
SERIAL NUNRERI GE-161 108
RATED THRUST: 11200.
ENGINE TOTAL TIME: 2273B. HRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TINE SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZJLF. GUIDE VANE CVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: -o. HRS
FUEL H/C RATIO: 2.020
7T.OO
21.05
FUEL; jp-4 IF
OPERATIONAL DATA «««««
INLET AIR TEMPERATURE, DEGREES F: START 77.00 FINISH
ATMOSPHERIC PRESSURE: START 29.05 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.01SO
RELATIVE HUMIDITY: 69.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.OC, FLOW RATE. LITERS/MIN: 42.
SAMPLE I INF TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 4
COMMENTS:
F/A AND AIRFLOW CALCULATED FROM EXHAUST COMPOSITION FOR FOURTH RUN. NO?
OFtERHINFO dY SUIURACTION. THIS TEST IS THE SECOND OF FOUR TESTS ON THF SAME
ENGINE. THE FUEL USED WAS TO CONTAIN THE NCRMAS CONCENTRATION OF Ct-2, BUT TWA
HAD PROBLEMS WITH THE CI-2 PUMP, SO THE ACTUAL CONCENTRATION IS NOT KNOWN.
ELAPSED
TIME
0.0
5.00
6.00
10. on
TEST
MODE
I/ 0
2/ 1
It 2
4/ 3
PHWFR
THRUST, LRS PERCENT
OR 4ATED
SHP
3160.00
BB20.00
10020.00
400.00
T.O.
72
ra
89
3
ENGINE
SPEED
RPM
Nl
7130.00
7iao.no
7180.00
4520.00
N2
7130.00
7180.00
7380.00
4520.00
MEASURED
FUEL
FLOW
LB/HR
6*60.00
7240.00
8620.00
1090.00
GAS GEN
AIR FLOW
. LB/SEC
147.50
151.80
162.10
44.50
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.012800
0.013300
0.014800
0.006800
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
72
78
B9
1
EXHAUST
CAS
TEMP
UFCRFFS ^
182.00
I 02"). 00
1117.00
716.00
EXHAUST
GAS
PRESSURE
PSIA
16.70
17.90
20.90
0.50
CO
IWETI
PPMV
r>n.oo
67.00
60.00
454.00
CO
2
il.fl)
PERCENT
2.61
2.71
2.97
1.30
THC
IWET)
PPMV
0.0
0.0
0.0
337.00
NO
IWFTI
PPMV
55.00
61 .00
75.00
3.00
NO
2
IUETI
PPMV
3.00
2.00
5.00
5.00
ALDEHYDES SMOKE PARTICULATFS
(WET)
PPMV
58.00
63.00
BO.00
8.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
-0.00
-o.on
-o.oo
-0.00
POWER
PERCENT
RATED
T.O.
72
7B
89
3
MASS EMI
CO
IB/in
L9 FUEL
5.18
4.92
4.02
65. 65
MASS E.MI
HC
IB/U
LB FUFL
0.0
0.0
0.0
27.91
MASS EMI
ND2
L9/1K
LB FUFL
0. 18
0.24
0.55
1.19
MASS EMI
CO 2
LB/IK
LB FUEL
3125.10
1125.51
3126.92
2951.53
MASS EMI
NO
LB/IK
LB FUEL
6.88
7,35
P. 25
0.71
MASS EHI
NOX
LP./1K
LB FUEL
7.26
7.60
8.81
1.90
MASS EM
CO
LB/HR
34.62
15.85
34.66
71.56
"ASS F»I
HC
IB/HP
0.0
0.0
0.0
30.42
MASS EMI
ND2
LB/HR
MASS EMI
CO 2
LB/HR
MASS EMI
NO
LB/HU
MASS EMI
NOX
LR/H
2.51 20675.65
1.76 22785.00
4.74 26954.08
1.29 3219.35
45.99
53.62
71.16
0.7R
48.50
55.37
75.90
2.07
POWER
PERCENT
DATED
T.O.
72
7fl
89
1
4.242
4.065
3.459
17K.D8B
2558.291
2581.3J3
2690.02«
9048.363
THC
LR/IK1TH-HB
0.0
0.0
0.0
76.050
5.636
6.079
7.101
1.942
La/IKHTH-HR
0.307
0.199
0.471
3.236
NO
X
IB/1KOTH-HH
5.943
6.778
7.575
5.178
IV-66
-------
CAL ID NUMBER: 310 ENGINE TYPE AND MODEL: c-i-eos-u
TEST ORGANIZATION: s N R I TKA
SERIAL NUMBER: GE-161 108
MODE
TAXI-IDLE
TAKEOFF
CtlMBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TtKERFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.0*0
1.000
0.650
0.400
0.0*0
FRACTIONAL
POKER
0.040
1.000
0.830
0.400
0.0*0
FRACTIONAL
PC1MER
0.0*0
1.000
0.850
0.400
0.0*0
POKER
f TH
**8.0
11200.0
9520.0
4*80.0
**B.O
POKER
TH
**a.o
11200.0
9520.0
**BO.O
**8.0
POKER
I TH
**8.0
11200.0
9920.0
4*80.0
**B.O
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR MODE
LB/HR LB/HR MIN.
T2.I59 1130.329 1.000 19.00
30.102 9688.805 1.000 O.TO
32.19* 8193.301 1.000 2.20
56.785 3968.873 1.000 *.00
72.159 1130.329 1.000 T.OO
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/ 1000K LB TH AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE HT FACTOR MODE
L6/HR LB/HR MIN.
29.828 1130.329 .000 19.00
0.0 9888. 805 .000 0.70
0.0 8193.301 .000 2.20
6.068 3968. 873 .000 *.00
29.828 1130.329 .000 T.OO
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/ 1000K LB TH AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR MODE
LB/HR LB/HR MIN.
2.204 1130.329 .000 19.00
100.271 9888.80! .000 0.70
68.281 8193.301 .000 2.20
20.651 3968.873 .000 *.00
2.20* 1130.329 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
CO
MASS
LBS.
22. 8SO
0.331
1.180
3.786
B.419
36.386
31.263
37.620
3.196
MC
MASS
LBS.
9.446
0.0
0.0
0.405
3.480
13.330
11.391
13.707
0.0
NOX
MASS
LBS.
0.698
1.170
2.504
1.377
0.237
6.003
5.132
6.175
104.449
FUEL
MASS
IBS.
357.94
115.37
300.42
264.59
131.87
1170.19
FUEL
MASS
LBS.
357.94
113.37
300.42
264.59
131. 87
1170.19
FUEL
MASS
LBS.
357.9*
115.37
300. *2
264.39
131. 87
1170.19
LB CO /
U LB FUEL
63.839
3.044
3.929
14.308
63.839
LB HC /
IK LB FUEL
26.389
0.0
0.0
1.529
26.389
LB NOX/
IK LB FUEL
1.950
10.140
B.334
5.203
1.950
ENERGY
TH-HR
141.87
130.67
349.07
298.67
52.27
972.53
ENERGY
f TH-HR
141.87
130.67
349.07
298.67
32.27
972.53
ENERGY
TH-HR
141.87
130.67
349.07
298.67
32.27
972.53
LB CO /
TH-HR
0.16107
0.00269
0.00338
0.01268
0.16107
LB HC /
t TH-HR
0.06658
0.0
0.0
0.00135
0.06658
LB NOX/
f TH-HR
0.00492
0.00895
0.00717
0.00461
0.00492
IV-67
-------
DATE! 8/ 4/71
TEST ORGANIZATION: S w B I TWA
ENGINE SUPPLIER: Tut
ENGINF 0»I»
C»L to NUMBER: 311
ENGINE TYPE AND MODEL: CJ-BOS-3A
SERIAL NUMBFR: GE-161-108
RATED THRUST: 11200.
ENGINE TOTAL TIME: 22738. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: o. MRS
N2 COMPRESSOR OVERHAUL: -o. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL H/C RATIO: 2.020
FUFL: jp-4 TF
OPERATIONAL DATA «««»««»»«««««
INLET AIR TEMPERATURE. DFGREES F: START 77.00 FINISH 78.00
ATMOSPHERIC PRESSURE: START 29.0* FINISH 29.04
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0134
RELATIVE HUMIDITY: 66.00 PERCENT
SAMPLE LINE: TEMPERATURE, OEGRFES C: 150.00, FLOW RATE, LITERS/HIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 4
COMMENTS:
F/A ANO AIRFLOW CALCULATED FROM EXHAUST COMPOSITION FOR FOURTH HUN. N02
DETERMINED BY SUBTRACTION. THIS IS THE THIRO OF FOUR TESTS ON THIS ENGINE.
THE CI-7 CONCENTRATION IN THE FUEL FOR THIS TEST HAS MINIMUM (0.0125T PY
VOLUME).
FLAPSFD
TIME
0.0
3.00
60.00
10.00
TEST
MODE
I/ 0
21 1
}/ 2
<5
MASS FMI
NOX
LB/IK
LB FUEL
7.79
7.85
9.92
1.52
MASS EMI
CO
LB/HK
29.51
28. SB
30.31
67.11
MASS FMI
HC
LB/HK
0.0
0.0
0.0
28.15
MASS FMI
NO 2
LB/HR
4.33
4.39
5.64
0.94
MASS EMI
CO?
LB/HR
21197.00
23109. 2S
26960.90
3201.21
MASS EMI
NO
Lfl/HP
48.47
53.59
70.46
0.70
MASS F«I
NOX
LB/hR
52. BO
57.98
85. 49
1.64
PERCENT
RATED
T.n.
78
89
1
cn
LB/1K4TH-HH
1.573
1.282
1.031
167.766
LB/IK«TH-HR
2566.722
767.6.052
7696.090
8003.078
THC
L8/1KHTH-HR
0.0
0.0
0.0
JO.380
NO
LB/1KITH-HR
5.868
6.090
7.046
1.755
LB/1KHTH-H8
0.524
0.499
0.564
2.340
NO
X
LB/1KITH-HR
6.392
6.589
8.549
4.095
IV-68
-------
CAL ID NUMBER: 311 ENGINE TYPE AND MODELi CJ-805-3A
TEST ORGANIZATION: s w R I TWA
SERIAL NUMBER! GE-161-IOB
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TIKI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IOLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POM Ed
0.0*0
1.000
0.850
0.400
0.040
FRACTIONAL
POWER
0.040
1.000
0.650
0.400
0.040
FRACTIONAL
PONER
0.040
1.000
0.850
0.400
0.040
POMER
TH
448.0
11200.0
9520.0
4480.0
448.0
POWER
f TH
448.0
11200.0
9520.0
4480.0
448. 0
POWER
I TH
448.0
11200.0
9520.0
4480.0
448.0
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
49.689 779.294 1.000 19.00
31.853 9948. 277 1.000 0.70
32.188 8195.566 1.000 2.20
28.941 1833. 509 1.000 4.00
49.689 779.294 1.000 7.00
TOTAL FOR CYCLE;
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE1
LBS POLLUTANT/ 1000K LB TH AT T.O.l
EMISSION FUEL USAGE TINE IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR NIN.
21.254 779.294 1.000 19.00
1.134 9948.277 1.000 0.70
0.934 8195.566 1.000 2.20
2.698 1833.509 1.000 4.00
21.254 779.294 1.000 7.00
TOTAL FOR CYCLEI
LBS POLLUTANT/IK LB FUEL/CYCLE:
US POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TINE IN
RATE RATE WT FACTOR MODE
LB/HR L8/HR MIN.
0.866 779.294 .000 19.00
104.178 9948.277 .000 0.70
71.064 8195.566 .000 2.20
17.418 3811.509 .000 4.00
0.866 779.294 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
L8S POLLUTANT/IK LB TH-HR/CVCLE:
LBS POLLUTANT/1000X LB TH AT T.O.:
CO
MASS
IBS.
15.735
0.195
1.188
1.931
5.797
25.047
24.603
25.754
3.526
HC
MASS
LBS.
6.730
0.013
0.014
0.1BO
2.480
9.437
9.146
9.704
1.181
NOX
MASS
LBS.
0.274
1.215
2.606
1.161
0.101
5.359
5.307
5.510
10B.519
FUEL
MASS
LBS.
246.78
116.06
300.50
255.57
90.92
1009.83
FUEL
MASS
LBS.
246.78
116.06
300.50
255.57
90.92
1009.83
FUEL
MASS
LBS.
246. 7B
116.06
100.50
255.57
90.92
1009.81
LB CO /
IK LB FUEL
63.761
3.403
3.952
7.563
63.761
LB HC /
IK LB FUEL
27.273
0.114
0.114
0.704
27.271
LB NOX/
IK LB FUEL
l.lll
10.472
8.671
4.5*9
1.111
ENERGY
* TH-HR
141.87
110.67
149.07
298.67
52.27
972.51
ENERGY
1 TH-HR
141.87
130.67
349.07
298.67
52.27
972.53
ENERGY
1 TH-HR
141.87
130.67
1*9.07
298.67
52. 27
972.51
LB CO /
1 TH-HR
0.11091
0.00102
0.00140
0.00647
0.11091
LB HC /
TH-HR
0.04744
0.00010
0.00010
0.00060
0.04744
LB NOX/
1 TH-HR
0.00191
0.00930
0.00746
0.00389
0.00193
IV-69
-------
DATE: 8/ 4/71
TEST ORGANIZATION: S W R
ENGINE SUPPLIER: TWA
ENGINE DATA
CAL ID NUMBER: 312
ENGINE TYPE AND MODEL: CJ-80S-3*
SERIAL NUMBER! GF-161-108
RUED THRUST: 11200.
ENGINE TOTAL TINE: 22T3S. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: o. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL M/C RATIO: 2.020
76.00
29.0*
FUEL: JP-4 TF
OPERATIONAL DATA «»«»»»«
INLET AIR TEMPERATURE, DEGREES F: START 78.00 FINISH
ATMOSPHERIC PRESSURE: START 21.0* FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0154
RELATIVE HUMIDITY: 66.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLCW RATE, LITERS/MIN: 42.50
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUHBE" OF TESTS: 4
COMMENTS:
F/A AND AIRFLOW CALCULATED FROM EXHAUST COMPOSITION FOR FOURTH PUN. N02
OETFBMINEO BY SUBTRACTION. THIS IS THE LAST OF FOUR TESTS ON THIS ENGINE. THE
FUEL USED DURING THIS TtST CONTAINED THE NORMAL CONCFNTS AT ItlN OF CI-2 10.2« BY
VOLUME).
ELAPSED
TIME
0.0
10.00
5.00
9.00
TtST
MDDE
I/ 0
11 1
3/ 2
4/ 1
POWER
THRUST, LBS PERCENT
OR RATED
SHP
aoao.oo
8870.00
10000.00
400.00
T.O.
72
7fl
89
3
ENGINE
SPEED
RPM
NI
7140.00
7210.00
7400.00
4510.00
N2
7140.00
7210.00
7400.00
4510.00
MEASURED
FUEL
FLOW
LB/HR
66bC.OO
7320.00
8590.00
1090.00
GAS GEN
AIR FLOW
LB/SEC
147.80
152.20
162.00
44.50
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.012500
0.013300
0.014700
0.006800
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-o.no
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DFGRFES F
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
72
78
89
3
EXHAUST
GAS
TFMP
DEGREES F
981 .00
1042.00
1114.00
778.00
FXHAUST
GAS
PRESSURE
PSIA
16.40
la.oo
20.80
0.50
co
IWETI
PPMV
65.00
64.00
65.00
492.00
CO
2
IwET)
PERCENT V
2.53
2.70
2.98
I.3K
THC
IWETI
PPMV
0.0
0.0
0.0
372.00
NO
UFT)
PPMV
50.00
57.00
71.00
2.00
NO
2
(WETI
PPMV
4.00
4.00
4.00
6.00
NO
X
(UETI
PPMV
54.00
61.00
75.00
8.00
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.oo
-0.00
POWER
PERCENT
RATED
T.O.
72
78
89
1
MASS EMI
cn
LB/IK
LB FUFL
5. II
4.77
4.14
66.91
MASS F"l
HC
LB/IK
LB FUEL
0.0
0.0
0.0
28.97
MASS EMI
ND2
LB/IK
LB FUFl
0.57
0.48
0.44
1.34
MASS FMI
C02
LB/IK
LB FUEL
3125.21
3125.83
3126.42
2948.63
MASS EMI
wi
LB/IK
LB FUEL
6.46
6.90
7.79
0.45
MASS TMI
NOX
LP/IK
LB FUEL
6.97
7.3d
8.23
1.79
MASS FMI
cn
LB/hk
33.98
34.52
37.28
72.93
MASS [Ml
HC
LB/HR
0.0
0.0
0.0
M.5S
MASS fMI
K02
LB/HR
3.43
3.54
1.77
1.46
MASS FMI
CD2
LB/HR
20782.66
27881.09
76855.95
3714.01
MASS EMI
NO
LB/CR
42.94
50.50
66. 89
C.49
MISS fMI
NOX
LB/HR
46.37
54.04
70.66
1.95
POWER
PERCENT
BATED
T.n.
LB/ IK*IM-HR
4.706
.1*914
3.'71
IR2.120
LBMKKTH-MR
7572.112
2594.728
7685.595
3015.016
THC
LR/1K« TH-HR
n.o
0.0
0.0
78.951
NO
LB/1KHTH-HR
5.314
5.725
6.6S9
1.217
Lfl/IKdIH-HR
0.425
0.40?
0. J/7
3.657
NT
X
LB/IKV TH-HR
5.739
6.127
7.066
4.869
IV-70
-------
CAL ID NUMBER! 112 ENGINE TYPE AND NDDELl CJ-805-3A
TEST ORGANIZATION: s w R i TNA
SERIAL NUMBER! CE-16I-I08
NODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
0.0*0
1.000
O.B50
0.400
0.040
POWER
« TH
448.0
11200.0
9520.0
4480.0
448.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
69.005 465.026
36.430 4838.374
36.574 8220.444
31.411 3738.400
65.005 46S.026
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
L8S POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
NODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
0.040
1.000
0.850
0.400
0.040
POWER
TH
448.0
11200.0
4520.0
4480.0
448.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
30.048 465.026
0.0 4838.374
0.0 8220.444
1.861 1738.400
30.048 965.026
WT
USAGE TIKE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLEl
L8 TH AT T.O.:
USAGE TIME IN
FACTOR NODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
TOTAL FOR CYCLE!
LBS POLLUTANT/ IK LB FUEL/CYCLE!
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1QOOK LB TM AT T.O.I
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.040
1.000
0.890
0.400
0.040
POWER
1 TH
448.0
11200.0
4520.0
4480.0
448.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.257 465.026
93.440 4838.174
66.583 8220.949
16.798 3738.900
1.257 465.026
WT
USAGE TINE IN
FACTOR MODE
MIN.
.000 14.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE 1
LBS POLLUTANT/ 1000K LB TH AT T.O.I
CO
MASS
LBS.
20.585
0.425
1.341
2.044
7.584
32.024
24.557
32.934
1.795
HC
MASS
LBS.
4.531
0.0
0.0
0.124
1.5(1
11.167
12.150
13.539
0.0
NOX
MASS
LBS.
0.398
1.090
2.441
1.120
0.147
5.146
4.745
5.34)
97.314
FUEL
MASS
LBS.
105.59
114.78
301.43
249.26
112.59
1081.65
FUEL
MASS
LBS.
305.54
114.78
301.43
244.26
112.54
1083.65
FUEL
MASS
LBS.
305.54
114.78
101.41
249.26
112.54
1083.65
LB CO /
IK IB FUEL
67.161
3.703
4.444
8.401
67.361
LB HC /
IK LB FUEL
31.184
0.0
0.0
0.498
11.184
LB NOX/
IK LB FUEL
1.303
9.448
8.044
4.443
1.303
ENERGY
1 TH-HR
141.87
130.67
349.07
298.67
52.27
972.53
ENERGY
i TH-HR
141.87
110.67
149.07
298.67
52.27
972.53
ENERGY
1 TH-HR
141.87
I30;67
149.07
298.67
52.27
972.51
IB
f
0
0
0
0
0
LB
0
0
0
0
0
LB
0
0
0
0
0
CO /
TH-HR
.14510
.00325
.00384
.00701
.14510
HC /
TH-HR
.06718
.0
.0
.00042
.06718
NOX/
TH-HR
.00281
.00834
.00699
.00375
.00281
IV-71
-------
DATE: 7/21/71
resr ORGANIZATION: s w R I TWA
ENGINE SUPPLIER: TWA
ENGINE DATA
CAL ID NUMBER: »I9
ENGINE TYPE AND MODEL: CJ-805-3A
SERIAL NUMBER: 161-255
RATED THRUST: 11200.
ENGINE TOTAL TIME: 217*7. MRS
TIMF SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
COMBUSTOK CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: -o. HRS
FUEL H/C RATIO: 2.020
79.00
28.94
FUFL: jp-4 TF
OPERATIONAL DATA »««»«
INLET AIR TEMPERATURE, DEGREES F: START 75.00 FINISH
ATMOSPHERIC PRESSURE: START 23.93 FINISH
INLFT AIP HUMIDITY, LBS H20/LB AIR: 0.0119
RELATIVE HtlMIOITV: 56.01 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 150.OC, FLO RATE. LITERS/MIN:
SAMPLE LINE TRANSPORT IIMF, SEC: 1.00
NUMBEP OF TESTS: 4
COMMENTS!
A/F ANR AIRFLOW CALCULATED FROM FKHAUST COMPOSITION FOR FOURTH RUN. NO?
DETERMINE!! BY SUBTRACTION.
42.50
ELAPSED
TIMF
0.0
5.55
12.00
15.45
TFST
MODE
\i a
zi i
3/ 2
4/ 1
POWER
THRUST, LBS PERCENT
OR RATFD
SHP
0720.00
1560.00
9940.00
400.00
T.O.
73
76
88
3
ENGINE
SPEED
RPM
Nl
7115.00
7165.00
7330.00
4530. CO
N2
7115.00
7165.00
7330.00
4530.00
MEASURED
FUEL
FLOW
LB/HH
6550.00
6410.00
0350.00
1060.00
GAS GEN
AIR FLOW
IH/SEC
147.70
150.80
1M.10
36.40
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.012300
0.012700
0.014400
o.ooaioo
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
2.16
2.24
2.46
-0.00
TUPBINF
INLET
TEMP
DEGREES F
-n.no
-0.00
-0.00
-0.00
POWFR
PERCENT
RATED
T.O.
73
76
EXHAUST FXHAUST
GAS GAS
TEMP PRESSURE
DEGBFFS F PSIA
977.00
1002.00
1121.00
729.00
165.00
1 7.50
20.BO
0.40
CO
IHETI
PP»V
52.00
44.00
38. CO
552.00
CO
2
IhET)
PERCENT
2.54
2.59
2.90
1.56
THC
IWFT)
PPMV
0.0
0.0
0.0
448.00
NO
IWEM
PPMV
54.00
59.00
77.00
2.00
NO
2
IWETI
PPMV
6.00
5.00
6.00
6.00
ALDEHYDES SMOKF PARTICULATFS
(WET)
PPMV
60.00
64.00
61.00
8.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oc
-0.00
POWER
PERCENT
RATED
T.O.
71
76
88
3
MASS EMI
CO
I.B/1K
LR FUEL
4.07
3. 18
7.61
66.15
MASS EMI
HC
LR/1X
LB fUEL
0.0
0.0
0.0
33.49
MUSS EMI
N02
LO/IK
LB FUEL
0.77
0.61
0.68
1. 18
"ASS FMI
C02
LB/U
LB FUFL
3126.84
1127.91
1129.14
2917.4?
MASS EMI
NO
LB/1K
LB FUEL
4.95
7.45
8.69
0.3S
MASS FMI
NOX
LB/1K
LB FUFL
7.7?
8.09
9.36
1.57
MASS FMI
CO
LP/HR
26.69
23.37
21.79
70. 12
MASS EMI
HC
LB/HR
0.0
0.0
0.0
35.50
MASS E.».l
NO 2
IB/HR
5.06
4.36
5.65
1.25
MA5S EMI
C02
LB/HR
20480.79
21613.98
26128.32
3113.66
MASS EMI
NO
LR/HP
45.52
51.47
77.52
0.42
MJSS EM
NOX
18/HR
50.58
55.81
78.18
1.67
POWFR
PERCENT
RATED
T.O.
73
76
cn
LB/1KHIH-HR
3.746
2. MO
2. 192
175.30?
LB/l<«TH-Hi(
2411.5P1
7524.998
262H.604
7784.148
THC
111/ 1KKTH-HH
0.0
0.0
0.0
R8.759
NO
LB/1IUTM-HR
5.538
6.013
7.29h
1.043
LB/1K1TH-HR
0.615
0.510
0.569
3.130
LB/1K1TH-HR
6.151
6.521
1.865
4.173
IV-72
-------
CAL ID NUMBER! 319 ENGINE TYPE AND MODEL: CJ-805-3A
TEST ORGANIZATION! S H R I THA
SERIAL NUMBER: 161-255
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
MODE
TAKI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.0*0
1.000
0.830
0.400
0.040
FRACTIONAL
POWER
0.040
1.000
0.850
0.400
0.040
FRACTIONAL
POKER
0.040
1.000
0.850
0.400
0.040
POKER
f TH
448.0
11200.0
9520.0
4480.0
448.0
POKER
TH
44B.O
11200.0
9520.0
4480.0
448.0
POWER
1 TH
448.0
11200.0
9320.0
44BO.O
448.0
EMISSION FUEL . USAGE TINE IN
RATE RATE HT FACTOR MODE
LB/HR LB/HR MIN.
T4.980 1106.440 1.000 19.00
28.087 10169.684 1.000 0.70
22.659 8346.832 1.000 2.20
69.828 3239.294 1.000 4.00
74.980 1106.440 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE!
LBS POLLUTANT/IK IB TH-HR/CYCLE:
LBS POLIUTANT/1000K LB TH AT T.O.t
EMISSION FUEL USAGE TIME IN
RATE RATE HT FACTOR MODE
LB/HR LB/HR MIN.
40.331 1106.440 .000 19.00
1.433 10169.684 .000 0.70
0.884 8346.832 .000 2.20
0.642 3239.294 .000 4.00
40.331 1106.440 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE 1
LBS POLLUTANT/IK LB TH-HR/CYCLEt
LBS POLLUTANT/1000K LB TH AT T.O.I
EMISSION FUEL USAGE TINE IN
RATE RATE HT FACTOR MODE
LB/HR LB/HR MIN.
1.847 1106.440 .000 19.00
116.866 10169.664 .000 0.70
78.032 8146.832 .000 2.20
16.295 3239.294 .000 4.00
1.847 1106.440 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.I
CO
MASS
LBS.
23.744
0.328
0.831
4.655
8.748
38.305
34.198
39.387
2.926
' HC
MASS
LBS.
12.772
0.017
0.032
0.043
4.705
17.569
15.685
18.065
1.493
NOX
MASS
LBS.
0.585
1.363
2.861
1.086
0.215
6.111
5.456
6.284
121.733
FUEL
MASS
LBS.
350.37
118.65
306.05
213.95
129.08
1120.11
FUEL
MASS
L8S.
350.37
118.65
306.05
215.95
129.08
1120.11
FUEL
MASS
LBS.
350.37
118.65
306.05
215.95
129.08
1120.11
LB CO /
IK LB FUEL
67.767
2.762
2.715
21.557
67.767
LB HC /
IK LB FUEL
36.451
0.141
0.106
0.198
36.451
LB NOX/
IK LB FUEL
1.669
11.492
9.349
5.031
1.669
ENERGY
1 TH-HR
141.87
130.67
349.07
298.67
32.27
972.53
ENERGY
f TH-HR
141.87
1)0.67
349.07
298.67
52.27
972.53
ENERGY
1 TM-HR
141.87
130.67
349.07
298.67
52.27
972.33
LB CO /
1 TH-HR
0.16737
0.00251
0.00238
0.01559
0.16737
LB HC /
1 TH-HR
0.09003
0.00013
0.00009
0.00014
0.09003
LB NOX/
TH-HR
0.00412
0.01043
0.00820
0.00364
0.00412
IV-73
-------
OATE1 7/26/71
TEST ORGANIZATION: S W R I TWA
ENGINE SUPPLIER: T H A
ENGINE OAT*
CAL in NUMBER: 321
ENGINE TYPE AND MODEL: JUC-6
SERIAL NUMBER: 630895
RATEO THRUST: I1QOO.
ENGINE TOTAL TIME: 27290. MRS
TINE SINCE HOT SECTION OVERHAUL: 5672. HRS
TIME SINCE:
Ml COMPRESSOR OVERHAUL: 5672. HRS
N2 COMPRESSOR OVERHAUL: 5672. HRS
COMBUST11R CAN REPLACEMENT: 5672. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 5672. HRS
Nl TURBINE OVERHAUL! 5672. HRS
N2 TURBINE OVERHAUL: 5672. HRS
FUEL H/C RATIO: 2.020
82.00
29.01
FUEL: JP-4 TF
OPERATIONAL DATA «..........
INLET AIR TEMPERATURE, DEGREES F: START 75.00 FINISH
ATMOSPHERIC PRESSURE: START 29.01 FINISH
INLFT AIR HUMIDITY, L9S H20/LB AIR: 0.0093
RELATIVE HUMIDITY: 42.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/HIM
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER CF TESTS: 4
COMMFNTS:
A/F ANO AIRFLOW CALCULATED FROM EXHAUST COMPOSITION FOR FtlURIH RUN. NC12
DETERMINED RV SUBTRACT KIN.
ELAPSED
TIME
TEST
MODE
0.0 I/ 0
12.00 21 I
16.50 3/ 2
19.00 4/ 3
POMFR
THRUST,LBS PERCENT
OR RATEO
SHP T.O.
6600.00
7920.00
9740.00
460.00
61
ENGINf
SPEED
RPM
Nl N2
5730.00 9120.00
5920.00 9270.00
6330.00 9520.00
7320.00 6221.00
MEASURED
FUEL
FLOW
LB/HP
5730.00
6400.00
9120.00
1110.00
GAS GEN
AIR FLOW
LB/SEC
144.00
152.10
167.00
35.00
CALC
F/A
0.01 1100
0.011700
0.013700
o.ocenno
COMPRESSOR FNGINE
DISCHARGE PRESSURE
TEMP KATIO
DEGREES F EPR
-0.00
-0.00
-0.00
. -0.00
1.96
2.11
2.40
1.10
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
61
7 1
KB
4
EXHAUST
GAS
TEMP
DEGREES I
869.00
925.00
ion i.oo
541.00
EXHAUST
GAS
PRESSURE
PS I A
13.40
15.60
20.00
0.70
CO
IWETI
PPMV
38.00
21.00
11.00
714.00
CC
2
(WET)
PERCENT V
2.23
2.34
2.76
1.53
THC
IWFTI
PPMV
0.0
0.0
0.0
2160.00
NO
IWETI
PPMV
46.01
55.01
73.01
2.01
NO
2
IWETI
PPMV
6.00
3.00
0.0
6.00
ALDEHYDES SMOKE PARTICULARS
(WETI
PPMV
52.00
5D.OO
73.00
R.OO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
61
71
88
MASS FMI
Ct)
LB/IK
LB FUEL
3.39
2.38
0.79
78.34
MASS EMI
HC
LB/IK
LB FUEL
0.0
0.0
0.0
135.74
MASS EMI
NH2
LB/IK
LB FUFL
O.RR
0.47
0.0
I.Ofl
MASS EMI
C02
LP/1K
LB FUEL
3127.91
3129.50
3131.99
2637.76
MASS fMl
NO
IB/IK
LB FUEL
6.75
7.69
8.66
0.36
MASS FMI
NOX
LP/1K
LB FUEL
7.62
8. 11
8.66
1.44
MASS FMI
CO
Lfl/HR
19.44
15.25
6.45
86.96
MASS FMI
HC
1 B/HH
0.0
0.0
0.0
150.67
MASS EMI
NO 2
LB/HR
5.04
2.68
0.0
1.20
MASS EMI
C17
Lfl/HR
17922.93
70078.77
25431.77
2927.91
MASS EMI
MO
LB/HR
3B.65
49.21
70.37
0.40
MASS [Ml
NUX
LB/HR
43.69
51.90
70.32
1.60
POWER
PFKCENT
RATEO
t.n.
61
71
CO
LB/IKHIH-HR
2.859
1.926
0.662
189.046
LB/IKHTH-HR
2635.725
2528.885
2611.065
6365.020
THC
I.B/1MTH-HR
0.0
0.0
0.0
327.544
5.604
6.214
7.220
0.670
LB/1KBTH-HR
0.741
0.339
0.0
2.609
N'J
X
LB/IKtlH-HR
6.425
6.553
7.270
3.479
IV-74
-------
CAL 10 NUMBERl 321 ENCINE TYPE «ND MODEL) JT3C-6
TEST ORGANIZATION) S U R I TWA
SERIAL NUMBER! 630895
MODE FRACTIONAL
POWER
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
0.050
1.000
0.650
0.400
0.050
POKER
I TH
550.
11000.
9390.
4400.
550.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
B3.434 1165.353
2.812 93S2.891
9.641 7787.633
32.132 4054.441
83.434 1165.353
USAGE TIME IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
O.OSO
1.000
0.850
0.400
0.050
POWER
TH
550.
11000.
9350.
4400.
550.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
167.968 1165.353
2.647 9352. 891
1.337 7787.633
2.222 4054.447
167. 96B 1165.353
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLE:
IB TH AT T.O.!
USAGE TINE IN
UT FACTOR MODE
NIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.890
0.400
0.050
POWER
TH
550.
11000.
9350.
4400.
550.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.751 1165.353
80.760 9352. 891
67.122 7787.633
23.970 4054.447
1.751 1165.353
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE I
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
MT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
IBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLEi
LB TH AT T.O.I
CO
MASS
LBS.
26.421
0.033
0.354
2.142
9.734
38.683
33.064
38.57*
0.298
HC
MASS
LBS.
53.190
0.031
0.049
0.148
19.596
73.014
62.408
72.808
2.807
NOX
MASS
LBS.
0.555
0.942
2.461
1.598
0.204
5.760
4.923
5.744
85.654
FUEL
MASS
LBS.
369.03
109.12
285.55
270.30
135.96
1169.95
FUEL
MASS
LBS.
369.03
109.12
285.55
270.30
135.96
1169.95
FUEL
MASS
LBS.
369.03
109.12
285.55
270.30
135.96
1169.95
LB CO /
IK LB FUEL
71.595
0.301
1.238
7.925
71.595
LB HC /
IK IB FUEL
144.135
0.283
0.172
0.54B
144.135
LB NOX/
IK LB FUEL
1.503
8.635
8.619
5.912
1.503
ENERGY
TH-HR
174.17
128.33
342.83
293.33
64.17
1002.83
ENERGY
1 TH-MR
174.17
128.33
342.83
293.3)
64.17
1002.83
ENERGY
f TH-HR
174.17
128.33
342.83
293.33
64.17
1002.83
LB CO /
1 TH-HR
0.15170
0.00026
0.00103
0.00730
0.15170
LB HC /
t TH-HR
0.30540
0.00024
0.00014
0.00050
0.10540
LB NOX/
f TH-HR
0.00318
0.00734
0.00718
0.00545
0.00318
IV-75
-------
DATE: 7/13/71
TEST ORGANIZATION! S U 0 I TWA
ENGINE SUPPLIER: T w A
ENGINE DATA
CAL 10 NUMBER: II 1
ENGINE TYPE AND M1IOFL: JI 3C - 7
SERIAL NUMBER! T63U29B
«ATEO THRUST: 12000.
ENGINE TOTAL TIME: 24419. MRS
TIME SINCE HD1 SECTION OVERHAUL: ")HO. MRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 11)0. HRS
NJ CCMPPESSOR OVERHAUL: 9110. HRS
COMBUSTOR CAN REPLACEMENT: 9110. HRS
FIRST STAGE N012LE GUIDE VANE OVERHAUL: inn. HRS
Nl TURBINE OVERHAUL) 9130. HRS
N2 TURBINE OVERHAUL: 9130. HRS
FUEL H/C RATIO: 2.020
S3.00
28.91
fUEL: JP-* TF
OPERATIONAL DATA «»««««»
INLET AIR TEMPERATURE, DEGREES F: STAPT 85.00 FINISH
ATMOSPHERIC PRESSURE: START 28.91 FINISH
INLET AIR HUMIDITY, LBS H20/LR AIR: 0.0191
RELATIVE HUMIDITY: 73.00 PERCENT
SAMPLE LINE: TEMPF.RATURC, DEGREES C: 150.00, FLOW RATE, LITERS/MIN: 4
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 7
COMMENTS:
F/A AND AIRFLOW CALCULATED FROM FXHAUST COMPOSITION FOP FIRST, THIRD AND LAST
RUNS. N02 DETERMINED RY SUBTRACTION
ELAPSED
TIME
1.00
4.45
6.30
15.00
18.00
22.30
77.00
TFST
MODE
4/ 0
5/ i,
</ 5
I/ 4
7/ 1
3/ 7.
4/ t
POWER
THKUST.LRS
UK
SHP
360.00
8220.00
440.00
64UO.OO
7140.00
9500.00
560.00
PERCENT
RATED
T.O.
2
66
3
53
59
71
4
ENGINE
SPEED
RPM
Nl N2
MEASURED
FUEL
FLOW
LB/HR
GAS GEN
AIR FLOW
LB/SEC
CALC
F/A
2
68
3
53
59
71
4
2105.00
6010.00
2260.00
5710.00
583n.OO
63CO.OO
2115.00
5780.00
9340.00
6020.00
9110. OJ
9170.00
9620.00
6420.00
980.00
6860.00
990.00
5400.00
6070.00
8050.00
1210.00
36.30
152.90
37.20
140. 10
145.80
163.30
43.70
0.007500
0.012500
0.007400
0.010700
0.01 1600
0.013700
0.007700
COMPRESSOR
DISCHARGE
TEMP
OFGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
F.PR
1.10
2.20
1.10
1.93
2.04
2.40
1.11
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-o.uo
-0.00
-o.oo
-0.00
-0.00
POWER
PFRCENT
RATED
1.0.
2
68
3
51
59
79
4
FXHAUST FXHAUST
GAS GAS
TEMP PRESSURE
nEGHFFS F PMA
580.00
993.00
555.00
870.00
917.00
1085.00
50?.00
0.40
If..40
C.40
13.60
14.10
10.50
0.60
CO
(WET)
PP^V
785.00
11.00
694.00
45.00
50.00
28. 00
640.00
r.n
2
(WFTI
PERCFNT V
1.76
2.15
1.26
2.10
2.31
2.66
1.37
THC
IUETI
PPMV
1730.00
16.00
1550.00
I r.oo
1 1.00
11.00
1020.00
NO
IWET)
PPMV
2.00
51.00
1 .00
33.00
43.00
71.00
1.00
NO
2
IWETI
PPMV
5.00
4.00
6.00
9. 00
6.00
3.00
6.00
IWFT)
PPMV
7 .00
55.OC
7.00
42.00
49.00
74.00
7.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PART1CULATFS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWEtt
PERCENT
RATED
T.O.
2
68
3
53
59
79
4
MASS FM1
CO
LP/1K
L8 FUFL
101.57
2.79
91.7?
4 . tti
4.30
2. 10
83.09
MASS CMI
Mr
LH/U
LB FUEL
130.7?
0.78
11". 76
0.92
0.54
0.47
75.84
MISS til
102
LB/IK
L9 FUEL
1.08
0.56
1.32
l.-O
0.85
0.37
1.26
MASS EMI
C02
LB/IK
LB FUEL
2611.90
3126.72
?f *°. 58
3124. or
3124.99
1128.65
2794.63
MASS FMI
NO
LB/IK
LP FUEL
0.43
7.09
0.22
5.11
6. 08
P. 71
0.21
"ASS FHI
NOX
LB/IK
LR FUEL
1.52
7.65
1.54
6.51
6. 93
9.10
1.49
MASS E''l
cn
LB/HR
101 .49
19.17
97.30
73.01
?6.I3
16.87
100.54
MASS EMI
HC
LH/HR
128.10
5.32
1 IX. 06
4.98
3.29
1.80
<
-------
CAL ID NUMBER: in ENGINE TYPE AND NODELI JT ic - T
TEST ORGANIZATION! S W R 1 TWA
SERIAL NUMBER: TA11124B
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLF
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.090
FRACTIONAL
PflWER
0.050
1.000
0.850
0.400
0.090
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.090
POKER
f TH
600.0
12000.0
10200.0
4800.0
600.0
POWER
f TH
600.0
12000.0
10200.0
4BOO.O
600.0
POWER
TH
600.0
12000.0
10200.0
4800.0
600.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
84.934 1060.392
17.809 10998.488
18.199 8797.383
20.116 4481.920
84.934 1060.392
TOTAL FOR CYCLE:
IBS POLLUTANT/IK LB
LBS POLLUTANT/IK L6
LBS POLLUTANT/ IOOOK
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
109.896 1060.392
2.9TS 10998.488
0.698 8797.383
3.904 44BI.920
109.896 1060.192
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IOOOK
EMISSION FUEL
RATE RATE HT
LB/HR LB/HR
1.718 1060.392
115.724 10998.488
89.414 8797.181
21.107 4481.920
1.718 1060.192
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IOOOK
USAGE TIME IN
FACTOR MODE
BIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TM-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR NODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
26.896
0.208
0.671
1.341
9.909
39.027
32.401
39.673
1.7)1
HC
MASS
LBS.
14.800
0.0)9
0.026
0.2)4
12.821
47.919
39.781
43.798
2.892
NOX
MASS
LBS.
0.944
1.983
1.279
1.SS4
0.200
7.160
9.949
6. 549
111.994
FUEL
MASS
LBS.
139.78
123.69
322.57
298.77
123.71
1204.47
FUEL
MASS
LBS.
119.78
121.65
122.97
298.77
123.71
1204.47
FUEL
MASS
LBS.
339.78
123.65
322.57
298.77
123.71
1204.47
LB CO /
IK LB FUEL
80.100
1.680
2.086
4.489
80.100
LB HC /
IK LB FUEL
101.641
0.281
0.079
0.782
101.641
IB NOX/
IK LB FUEL
1.620
12.806
10.164
9.201
1.620
ENERGY
TH-HR
190.00
140.00
374.00
320.00
70.00
1094.00
ENERGY
1 TH-HR
190.00
140.00
374.00
320.00
70.00
1094.00
ENERGY
TH-HR
190.00
140.00
374.00
320.00
70.00
1094.00
IB CO /
1 TH-HR
0.14196
0.00148
0.00180
0.00419
0.14196
LB HC /
1 TH-HR
0.18316
0.00029
0.00007
0.00073
0.18316
LB NOX/
TH-HR
0.00286
0.01111
0.00877
0.00486
0.00286
IV-77
-------
DATE: 7/15/11
TEST ORGANIZATION: s w B i TUA
ENGINE SUPPLIER: T M A
ENGINE DATA
CAL ID NUM1FR: 113
ENGINE TYPE AND MODEL: JT 3C - 7
RATED THRUST:
ENGINE TOTAL TIME:
TIKE SINCE HOT SECTION OVERHAUL:
TIME SINCE:
12000.
24*19. MRS
9130. HRS
SEOUL NUMBER: 6311293
Nl COMPRESSOR OVERHAUL! 9130. HRS
N2 COMPRESSOR OVERHAUL: 9130. HRS
COMBUSTOR CAN REPLACEMENT: 9130. HRS
FIRST STAGE NUZZLE GUIDE VANE OVERHAUL: 9130. HRS
Nl TURBINE OVERHAUL: 9130. HAS
HZ TURBINE OVFRHAULI 9130. HRS
FUEL H/C RATIO: 2.020
FUEL: jp-4 TF
OPERATIONAL DATA *«««»*«»»««»«*
INLET AIR TEMPERATUREi DEGREES F: START 86.00 FINISH 86.00
ATMOSPHERIC PRESSURF: START 28.89 FINISH 20.89
INLFT AIR HUMIDITY, LBS H20/LB AIR: 0.0147
RELATIVE HUMIDITY: 51.00 PERCENT
SAMPLE LINE: TEMPERATURE, OEGRFFS C: 150.00, FLOW RATE, LITERS/MINI
SAMPLE LINF TRANSPORT TIME, SFC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
F/A AND AIRFLOW CALCULATED FROM EXHAUST COMPOSITION FOR FOURTH RUN. Nil?
DETERMINED BY SUBTRACT(UN.
ELAPSED
TIME
0.0
7.00
20.00
25.00
30.00
TEST
MODE
I/ 0
i.1 \
3/ 2
4/ 1
5/ 4
POWFR
THRUST, LBS PERCENT
OR RATED
SHP
6*70.00
7360.00
9560.00
.160.00
8400.00
T.O.
54
61
79
2
69
FNGINF
SPEED
RPM
Nl
5710.00
5860.00
6290.00
?300.00
6050.00
N2
9000.00
9240 .00
9610.00
5R70.00
9160.00
MEASURED
FUEL
FLOW
LB/HR
5560.00
6160.00
8100.00
1120.00
7070.00
GAS GEN
AIR FLOW
LB/SFC
139.90
146.50
162.50
37.50
153.50
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.011000
0.011700
0.011800
0.008300
0.012800
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.95
2.06
2.44
1.10
2.25
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-C.OO
-0.00
-0.00
POHEP
PERCENT
RATED
T.O.
54
61
79
2
69
F. XHAUST
GAS
TEMP
UFT.UFFS F
692 .00
710.00
1077.00
537.00
1005.01
FXHAUST
GAS
PRFSSURE
PSIA
12.80
14.60
19.60
0.50
ir.oo
CO
I WET I
PPMV
39.00
8.00
5.00
768.00
21.00
en
7
-------
CAL 10 NUMBER: ID ENGINE TYPE AND MODEL: ji 3C - 7
TEST ORGANISATION: s H R i TMA
SERIAL NUMBER: 5311298
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAKI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.090
1.000
o.89o
0.400
O.OSO
FRACTIONAL
POKER
0.030
1.000
0.850
0.400
0.090
FRACTIONAL
POWER
O.OSO
1.000
o.aso
0.400
O.OSO
POWER
1 TH
600.0
12000.0
10200.0
4800.0
600.0
POWER
TH
600.0
12000.0
10200.0
4800.0
600.0
POWER
1 TH
600.0
12000.0
10200.0
4800.0
600.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
18.307 1247.862
0.0 10*55.68*
0.0 8763.449
22.365 43B8.SS1
18.107 1247.862
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
I2.S02 1247.862
0.0 I04SS.684
1.681 8763.449
6.920 4388.991
12.502 1247.862
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
1.679 1247.862
104.248 10499.684
78.200 8763.449
22.979 4388.991
1.679 1247.862
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-MR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLEI
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TINE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
9.797
0.0
0.0
1.491
2.136
9.424
7.382
8.614
0.0
' HC
MASS
LBS.
1.999
0.0
0.062
0.461
1.499
9.941
4.693
9.430
0.0
NOX
MASS
IBS.
0.932
1.216
2.867
1.909
0.196
6.316
4. 948
9.773
101.392
FUEL
MASS
LBS.
399.16
121.98
321.13
292.97
149.98
1276.62
FUEL
MASS
LBS.
399.16
121.98
321.33
292.97
149.98
1276.62
FUEL
MASS
LBS.
399.16
121.98
321.11
292.97
149.98
1276.62
LB CO /
IK LB FUEL
14.671
0.0
0.0
9.096
14.671
LB HC /
IK LB FUEL
10.019
0.0
0.192
1.977
10.019
LB NOX/
IK LB FUEL
1.349
9.970
8.923
9.149
1.349
ENERGY
I TH-HR
190.00
140.00
374.00
320.00
70.00
1094.00
ENERGY
TH-HR
190.00
140.00
374.00
320.00
70.00
1094.00
ENERGY
f TH-HR
190.00
140.00
374.00
120.00
70.00
1094.00
LB CO /
1 TH-HR
0.03091
0.0
0.0
0.00466
0.03091
LB HC /
t TH-HR
0.02084
0.0
0.00016
0.00144
O.OZ084
LB NOX/
TH-HR
0.00280
0.00869
0.00767
0.00470
0.00280
IV-79
-------
DATE: 7/7ft/71
TEST ORGANIZATION: UNITED/EPA
ENGINE SUPPLIER: UNITFO AIRLINES
FNGINE DATA
CAl ID NUMBER: 158
ENGINE TYPE AND KOOFL: JT 3C - 7
SERIAL NUMBFR:
PATEO THRUST: 12000.
ENGINE TOTAL TIME: 19358. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 12975. MRS
N2 COMPRESSOR OVERHAUL: 97*. MRS
COMBUSTHR CAN REPLACEMENT: 0. MRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: 3366. HRS
N2 TURBINE OVERHAUL: 3867. HRS
FUEL: JET - A FUEL H/C RATIO: 1.920
OPERATIONAL DATA «««««««««««
INLET AIR TEMPERATURE, DEGREES F: START (.6.20 FINISH
ATMOSPHPRIC PRFSSURF: START 29.92 FINISH
INLFT AIR HU-MOITY, LBS H20/LB AIR: 0.0
RFLATIVE HUMIDITY: 65.00 PERCENI
SAMPLE LINE: TEMPERATURE, DEGRFFS C: 160.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 5.00
NUMBFH OF TESTS: 4
COMMFNTS:
REPAIRED ENGINE, NOT CAR80-OLASTFD
EXHAUST GAS TE»PEKATURE IN DEGREES C
EXHAUST CAS PRESSURE IN INCHES HG.
JT3C-7 PROBF USED
62.60
29.98
CLOCK
TIMF
I631.n0
I637.no
1642.00
1721.00
TFST
MODF
I/ 0
21 1
3/ 2
4/ 1
POWER
THRUST, LBS PERCENT
OR RATED
SHP
7677.00
91 13.00
10M8.00
442.00
T.O.
63
75
88
3
ENGINE
SPEED
RPM
Nl
5335.00
6088.00
6387. On
2294. CO
N2
9223.00
9439.00
9698.00
6068.00
MEASURED
FUEL
FLOW
LB/HR
6295.00
7530.00
8951 .00
1701.00
GAS GEN
AIR FLOW
. LR/SEC
-0.00
-0.00
-o.on
-0.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
COMPRESSOR FNGINE
DISCHARGE PRESSURE
TEMP RATIO
DEGREES F EPR
-0.00
-0.00
-0.00
-0.00
2.13
2.17
2.62
-0.00
TURBINF
INLET
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
PERCENT
RATED
T.O.
63
75
88
EXHAUST
GAS
TC-XP
DEGREE1; F
466.00
51 3.00
569.nn
773.00
EXHAUST
GAS
PRESSURE
PS I A
62. 10
68.90
75.BO
31.60
CO
(WET)
PPMV
50.00
50. on
45. nn
810.00
en
?
(uEri
PERCENT V
2.42
2.65
3.00
1.25
THC
IWFTI
PPMV
2.94
2.40
2.40
1560.00
NO
1 WETI
PPMV
58.00
74.00
92.40
9.40
NO
7
IWFTI
PPMV
-0.00
-0.00
-0.00
-0.00
NO
X
IWETI
PPMV
62.40
78.00
98.40
9.BO
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-o.on
-0.00
-0.00
-o.on
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PQWFR
PERCENT
RATED
T.O.
61
75
88
J
MASS EMI
rn
Lfl/lK
L? FUEL
4. 14
3. 7B
3.01
109.41
MASS EMI
HC
1 B/IK
LR FUEL
0.14
0.10
0.09
120.68
MASS [Ml
Nfl2
IB/IK
LO FUEL
-0.00
-n.oo
-0.00
-o.on
MASS FKI
CO 7
LB/IK
LB FUEL
3149.00
3149.66
3150.91
2657.90
MASS FMI
no
I fi/IH
IB FUEL
7.09
9.19
10.15
2.09
MASS MI
NOX
LB/IK
LB FUEL
8.49
9.69
10. en
2.17
MASS EMI
CO
LB/HR
26.07
78.48
76.93
131.40
MASS EMI
HC
LP./HR
O.B8
0.78
0.82
144.94
MASS EMI
NO 2
LB/HR
-0.00
-0.00
-o.no
-o.on
MASS FMI
CD 2
LB/HR
19822.96
23716.96
28203. HO
3186.13
MASS EMI
NO
LB/HR
49.67
69.24
90.81
2.50
MASS FMI
NOX
LB/HR
53.43
77. 9H
96.71
2.61
POWER
PERCENT
RATFD
T.O.
63
75
88
3
rn
IK N T H -H R
3.395
3.125
2.536
797.789
LR/1K« TH-HR
2592.174
2602.541
7656.275
7208.449
0.114
0.086
0.077
377.917
NO
LR/ 1KKTH-HR
6.470
7.597
H.553
5.667
LB/ IK0TH-HR-
-0.000
-0.000
-0.000
-c.oon
NO
V
LB/1K0TH-HR
6.960
B.009
9.108
5.903
IV-80
-------
CAL 10 NUMBER: 199 ENGINE TYPE AND MODEL: JT 3C - 7
TEST ORGANIZATION: UNITED/EPA
SERIAL NUMBER! 632275
NODE FRACTIONAL
POWER
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
0.050
1.000
O.BSO
o.«oo
0.050
POWER
1 TH
600.
12000.
10200.
4800.
600.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
125.910 1917.390
19.916 10326.199
23.257 8612.996
55.184 4190.543
125.910 1317.390
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE FRACTIONAL
POKER
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
T/UI-IOLE
0.050
1.000
0.850
0.400
0.050
POWER
TH
600.
12000.
10200.
4800.
600.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
124.746 1317.390
0.0 10326.199
1.414 8612.996
20.937 4190.543
124.746 1317.390
NT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POKER
0.050
1.000
0.850
0.400
0.050
POWER
* TH
600.
12000.
10200.
4800.
600.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
2.990 1317.390
125.078 10326.199
90.517 8612.996
24.481 4190.543
2.990 1317.390
WT
TOTAL FOR CYCLE:
L8S POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
USAGE TINE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLfi:
LB TH AT T.O.:
CO
MASS
LBS.
39.872
0.232
0.853
3.679
14.690
59.325
46.113
54.228
1.936
' HC
MASS
LBS.
39.503
0.0
O.OS2
1.396
14.554
55.50*
43.143
50.735
0.0
NOX
MASS
LBS.
0.947
1.459
3.319
1.632
0.349
7.706
5.990
7.044
121.603
FUEL
MASS
LBS.
417.17
120.47
315.81
279.37
153.70
1286.52
FUEL
MASS
LBS.
417.17
120.47
315. Bl
279.37
153.70
1286.52
FUEL
MASS
LBS.
417.17
120.47
315.81
279.37
153.70
1286.52
LB CO /
IK LB FUEL
95.575
1.929
2.700
13.169
95.575
LB HC /
IK LB FUEL
94.692
0.0
0.164
4.996
94.692
LB NOX/
IK LB FUEL
2.270
12.113
10.509
5.842
2.270
ENERGY
1 TH-HR
190.00
140.00
374.00
320.00
70.00
1094.00
ENERGY
f TH-HR
190.00
140.00
374.00
320.00
TO. 00
1094.00
ENERGY
TH-HR
190.00
140.00
374.00
320.00
70.00
1094.00
LB CO /
1 TH-HR
0.20985
0.00166
0.00228
0.01150
0.20985
LB HC /
TH-HR
0.20791
0.0
0.00014
0.00436
0.20791
LB NOX/
1 TH-HR
0.00498
0.01042
0.00887
0.00510
0.00498
IV-81
-------
DATE! 7/21/71
TEST ORGANISATION: UNITED/EPA
ENGINE SUPPLIER: UNITED AIRLINES
ENGINF DATA
CAL ID NUMBER: 405
ENGINE TTPE AND MODEL: JT 3C - 7
SERIAL NUMBER I
633959
RATFD ThRUST: 12000.
ENGINE TOTAL TIME: 16966. MRS
TIME SINCE HOT SECTION OVERHAUL: 169IS8. MRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 110*3. MRS
N2 COMPRESSOR OVERHAUL: 17125. HRS
CHMBUSTUR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL; JET - A FUEL H/C RATIO: 1.920
OPERATIONAL DATA ««*»»««««
INLET AIR TEMPERATURE, DEGREES F: START 55.40 FINISH
ATMOSPHERIC PHFSSURF: START 2").87 FINISH
INLET AIR HU"10ITY, LDS H20/LD AIR: 0.0091
RELATIVE HUMIOIIV: 94.00 PERCENT
SAKPLE LINE: TEMPERATURE, DEGREES C: 160.00, FLOH RATE, LITERS/HIM:
SAMPLE LINF IKANSPdRT TIME, SEC: 5.00
NUMBER OF TESTS: 4
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES HG.
REGIILAS PRODUCTION ENGINE
57.02
29.96
:LUC<
TIME
622.00
627.00
630.00
731.00
TEST
MOOF
I/ 0
71 1
3/ 2
4/ 3
POHFR
THRUST.LBS PERCENT
OR RATFC
SUP
7784.00
9120.00
10743.00
436.00
T.O,
64
75
89
3
ENGINE
SPFFO
PPM
Nl
5618.00
6059.00
6384. OC
27.69.00
N2
9259.00
9468.00
9753.00
6050.00
MEASURED
FUEL
FLOW
LB/HR
6307.00
7440.00
9020. OC
1135.00
GAS GEN
AIR FLOW
Lfl/SEC
-0.00
-0.00
-0.00
-0.00
CALC COMPRESSOR
F/A DISCHARGE
TEMP
-0.000000
-0.000000
-0.000000
-0.000000
OEGRFFS F
-0.00
-0.00
-0.00
-0.00
ENGINF
PRESSURE
RATIO
EPR
2.15
2.37
7.64
-0.00
TURBINE
INLET
TEMP
DEGREES 1
-0.00
-O.OC
-0.00
-0.00
POKER EXHAUST
PERCENT f,AS
RATED TEMP
T.O. DEGREES I
64
75
89
1
867.20
948.20
I 06 7 . 00
492.10
F XHAUST
GAS
PRESSURE
PSIA
62.60
68. 70
76. 10
31.60
CO
IWETI
PPMV
60.00
40.00
30.00
flOO.OO
CC
2
IWFT)
PERCENT V
2.25
2.45
2.75
l.in
THC
IHETI
PPMV
1.95
1.26
1.30
1200.00
NO
(MET!
PPMV
54.00
70.00
1C2.00
7.00
NO
2
(HFTI
PPMV
-0.00
-0.00
-0.00
-0.00
NO
X
(hETI
PPMV
64.00
79.00
110.00
9.60
ALOFHrOES
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
PARTICULAUS
-0.00
-0.00
-0.00
-0.00
PUHFR
PERCENT
RATED
T.O.
64
75
89
3
MASS E.'ll
cn
LB/IK
L°. FUEL
J.27
2. 11
114.77
.1ASS EMI
Hf
1 M/l K
LH FUEL
0.06
0.05
9B.60
M4SS EMI
Nil 2
LD/1K
LB FUEL
-0.00
-0.00
-0.00
MASS EMI
cn2
LB/IK
LB FUEL
3150.58
1152.30
2705.05
MASS CM
NO
LB/U
LB FUEL
9.41
12.22
1.65
MASS FM1
NOX
LB/IK
LI FUFL
10.62
13.18
2.26
MASS FMI
CO
LB/HR
24.36
19.74
130.27
MASS EMI
HC
LB/Hk
0.44
0.49
111.91
MASS EMI
NU2
LH/HO
-0.00
-0.00
-0.00
MASS FMI
C02
LB/HR
23440.13
28433.76
3070.23
MASS EMI
NO
LB/HP
70.01
110.25
1.87
MASS bM
NOX
LB/HR
59.02
79.01
118.90
2.57
PFRCENT
RATED
T.O.
64
75
CD
R/ IK"TH-Htf
4. 128
?. 671
1.818
79B.782
LR/1K0TH-HK
>550.(143
2570.?I2
2646.774
7041.809
THC
L3/IKHTH-HR
0.0.11
0.046
0.046
256.679
6.39S
7.677
10.263
4.294
Lfl/IMTH-HR
-0.000
-0.000
-0.000
-0.000
NU
X
LB/l*«TH-HR
7.583
8.664
I 1.068
5.S89
IV-82
-------
C»L to NUMBER: 405 ENGINE TYPE »ND MOOEI: jt jc - 7
TES7 ORGANIZATION: UNITEO/EPA
SERIAL NUMBER I 633559
MODE FRACTIONAL
POKER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
0.050
1.000
0.850
0.400
O.OSO
POWER
TH
600.0
12000.0
10200.0
4800.0
600.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
118.586 1174.937
5.362 10374.938
19.603 8646.199
76.490 3920.626
119.586 1174.937
MT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
NODE FRACTIONAL
PONER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
O.OSO
1.000
0.850
0.400
O.OSO
POKER
1 TH
600.0
12000.0
10200.0
4800.0
600.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
96.838 1174.937
0.0 10374.938
0.0 8646.199
8.134 3920.626
96.838 1174.937
VT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
HOOE
TAXI-IDLE
TAKEOFF
CL1MOOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
O.OSO
1.000
0.650
0.400
0.050
POWER
1 TH
600.0
12000.0
10200.0
4800.0
600.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
2. 806 1174.937
160.598 10374.938
106.754 8646.199
26.170 3920.626
2.806 1174.937
UT
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLEI
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLEi
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
KIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
CO
MASS
LBS.
37.552
0.063
0.719
5.099
13.835
57.268
47.384
52.347
0.521
HC
MASS
LBS.
30.665
0.0
0.0
0.542
11.298
42.505
35.170
38.853
0.0
NOX
MASS
LBS.
0.889
1.874
3.914
1.745
0.327
8.749
7.239
7.997
156.136
FUEL
MASS
L8S.
372.06
121.04
317.03
261.38
137.08
1208.98
FUEL
MASS
LBS.
372.06
121.04
317.03
261.38
137.08
1208.58
FUEL
MASS
LBS.
372.06
121.04
317.03
261.38
137.08
1208.58
LB CO /
IK LB FUEL
100.930
0.517
2.267
19.510
100.930
LB HC /
IK LB FUEL
82.420
0.0
0.0
2.075
82.420
LB NOX/
IK LB FUEL
2.388
15.479
12.347
6.675
2.388
ENERGY
1 TH-HR
190.00
140.00
374.00
320.00
TO. 00
1094.00
ENERGY
1 TH-HR
190.00
140.00
374.00
320.00
70.00
1094.00
ENERGY
TH-HR
190.00
140.00
374.00
320.00
70.00
1094.00
LB
i
0
0
0
0
0
LB
f
CO /
TH-HR
.19764
.00045
.00192
.01594
.19764
HC /
TH-HR
0.16140
0.0
0.0
0.00169
0.16140
LB
0
0
0
0
0
NOX/
TH-HR
.00468
.01338
.01047
.00545
.00468
IV-83
-------
DATE: 7/22/71
TEST ORGANIZATION: UNITFO/EPA
ENGINE SUPPLIER: UNITED AIRLINES
ENGINE OATS
CAL 10 NUMBER:
ENGINE TYPE AND MODFL: JT 3C - 7
SERIAL NUMBER:
633042
RATED THRUST: 12000.
ENGINE TOTAL TIME: 13754. HRS
TIME SINCE HOT SECTION OVERHAUL: 13754. HRS
TIKE SINCE:
Nl COMPRESSOR OVERHAUL 1 -0. HRS
N2 COMPRESSOR OVERHAUL: -o. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOtZlf GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL: JET - A FUEL M/C RATIU: l.<)20
OPERATIONAL DATA »»»«*«*«
INLET AIR TEMPERATURE, DEGREES F: START 57.20 FINISH
ATMOSPHERIC PRESSURE: START 21.11, FINISH
INLET AIR HUMIDITY, LBS H2I1/LB AIR: 0.0096
RELATIVE HUMIDITY: 14.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 160.00, FLOW RATE, LITFPS/MIN:
SAMPLE LINE TRANSPORT T1MF, SEC: 5.00
NUMBER (IF TESTS: 4
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES HG.
F.NGINF CAPBO-BLASTEO PRIOR Tfl EMISSIONS RUN.
HIGH OIL CONSUMPTION.
57.?0
29.98
LOCK
TIMF
449.00
454.00
457.00
51). 00
TEST
MODE
I/ 0
2/ I
3/ 2
4/ 1
POHFR
THRUST, LBS PERCENT
OR RATED
SHP
7H09.00
91 13.00
10861.00
399.00
T.O.
65
75
90
3
FNGINE
SPEFD
RPf
Nl
5838.00
6061.00
6403.00
2251.00
N2
9229.00
9419.00
9709.00
5966.00
MEASURED
FUEL
FLOW
LB/HR
6251.00
7326.00
9974.00
1182.00
GAS GEN
AIR FLOU
LB/SEC
-C.OO
-0.00
-0.00
-0.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
2. 14
2.16
2.65
-0.00
TURBINF
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POHER
PERCENT
RATED
T .0.
65
75
90
3
EXHAUST
GAS
TFNO
DFGRFFS F
H72.60
957.20
1070.60
527.00
EXHAUST
GAS
PRFSSURF
PSIA
62.50
68.60
76.50
11.50
CO
IUETI
PPMV
60. no
45.no
40.00
590.00
CO
2
UEU
PERCENT V
2.15
2.40
2.65
0.90
THC
IWFT)
PPMV
1.60
3.16
3.00
219.00
NO
(UFII
PPMV
36.00
50.00
68.00
8.40
NO
2
UEU
PPMV
-o.no
-0.00
-n.on
-0.00
NO
X
(NET)
PPMV
38.00
52.00
72.00
8.40
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POKER
PERCENT
RATED
65
75
90
3
MASS FMI
CO
LB/IK
LB FUEL
5.59
3. 76
3.03
120. HI
MASS FMI
HC
IB/IK
L8 fUEl
0.19
0.15
n.i)
25.68
MASS EMI
N02
LB/IK
LB FUFL
-0.00
-0.00
-0.00
-n.on
MASS tMI
CO 2
LB/IK
LB FUEl
3146.58
3149.58
3150.78
2895.61
KASS EMI
Nfl
LB/IK
LB FUEL
5.51
6.86
8.45
7.91
MASS EMI
NOX
LB/IK
LB FUEL
5.81
7. 13
8.95
2.83
fASS EMI
CU
LB/HR
34.94
27.53
27.16
142.80
MASS EM
HC
LB/hR
1.70
1.07
1.17
30.36
MASS EMI
N02
LB/HR
-0.00
-0.00
-0.00
-0.00
MASS EMI
C02
LB/HR
19669.28
23073.84
2B275.07
3422.60
MASS EMI
NO
LB/HR
34.43
50.25
75.85
3.34
MASS EMI
NOX
LB/HR
36.34
52.26
HO. 31
3.34
POWER
PERCENT
RATEO
T.n.
65
75
90
3
4.474
1.071
2.501
357.994
LP/1KKTH-HR
2519.796
2531.970
2603.358
8577.953
THC
L «/1K0TH-HH
0. 154
0.118
0. 107
76.084
NO
LB/IKKTH-HR
4.409
5.514
6.98',
6.370
LB/ KOTH-HR
-0.000
-0.000
-0.000
-0.000
NO
X
L9/IK«TH-HR
4.654
5.735
7.394
8.370
IV-84
-------
CAL ID NUMBER: 407 ENGINE TYPE AND NOOEU JT sc - T
TEST ORGANIZATION: UNITEO/EPA
SERIAL NUNBERI 633042
MODE
TAXI-IDLE
TAKEOFF
CLIMB OUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
FRACTIONAL
POKER
0.050
1.000
0.650
0.400
0.050
FRACTIONAL
POKER
0.050
1.000
0.850
0.400
0.050
POKER
1 TH
600.0
12000.0
10200.0
4800.0
600.0
POKER
TH
600.0
12000.0
10200.0
4800.0
600.0
POWER
1 TH
600.0
12000.0
10200.0
4800.0
600.0
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR NODE
LB/HR LB/HR BIN.
129.513 1280.095 .000 19.00
13.406 10009.320 .000 O.TO
23.54T 8430.910 .000 2.20
71.65S 3888.995 .000 4.00
129.513 1280.095 .000 T.OO
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE NT FACTOR MODE
LB/HR LB/HR MIN.
25.973 1280.095 1.000 19.00
0.361 10009.320 1.000 0.70
0.601 8430.910 1.000 2.20
3.230 3888.995 1.000 4.00
25.973 1280.095 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLEl
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR MODE
LB/HR LB/HR MIN.
3.710 1280.095 1.000 19.00
103.358 10009.320 1.000 0.70
70.736 8430.910 1.000 2.20
17.638 3888.995 1.000 4.00
3.710 1280.095 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/tOOOK LB TH AT T.O.:
CO
MASS
LBS.
41.013
0.156
0.863
4.777
15.110
61.919
49.940
56.599
1.303
HC
MASS
LBS.
8.225
0.004
0.022
0.215
3.030
11.497
9.272
10.509
0.351
NO*
MASS
LBS.
1.175
1.206
2.594
1.176
0.433
6.5B3
5.310
6.018
100.487
FUEL
MASS
LBS.
405.36
116.78
309.13
259.27
149.34
1239.88
FUEL
MASS
LBS.
405.36
116.78
309.13
259.27
149.34
1239.88
FUEL
MASS
LBS.
405.36
116.78
309.13
259.27
149.34
1239.88
LB CO /
IK LB FUEL
101.175
1.339
2.793
18.425
101.17$
IB HC /
IK LB FUEL
20.290
0.036
0.071
O.S31
20.290
LB NOX/
IK LB FUEL
2.899
10.326
8.390
4.535
2.899
ENERGY
TH-HR
190.00
140.00
374.00
320.00
70.00
1094.00
ENERGY
t TH-HR
190.00
140.00
374.00
320.00
70.00
1094.00
ENERGY
f TH-HR
190.00
140.00
374.00
320.00
70.00
1094.00
LB CO /
1 TH-HR
0.21586
0.00112
0.00231
0.01493
0.21586
LB HC /
TH-HR
0.04329
0.00003
0.00006
0.00067
0.04129
LB NOX/
TH-HR
0.00618
0.00861
0.00693
0.0036T
0.00618
IV-85
-------
DATE: 7/22/71
TEST ORGANUATION: UNITtO/EPA
ENGINE SUPPLIER: UNITED AIRLINES
ENGINE DATA
CAl ID NUMHFR: 409
ENGINE TYPE AND MODELI JT 3C - 7
SERIAL NUMBER:
6J22B3
RATED THRUST: 12000.
ENGINE TOTAL TIME: 13765. MRS
TIME SINCE HOI SECTION OVERHAUL: 0. HBS
TIME SINCE:
NI COMPRESSOR OVERHAUL: nnoe. HRS
N2 COMPRESSOR OVERHAUL: 15386. HRS
CQMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.920
FUEL: JET - A
OPERATIONAL DATA >«»»«
INLET AIR TEMPERATUREi DEGREES F: START
ATMOSPHERIC PHESSURE: START
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0
RELATIVE HUMIDITY: o.o
SAMPLE LINE: TEMPERATURE, DEGREES C: 160.00
SAMPLE LINE TRANSPORT TIME, SEC: 5.00
NUMBER OF TESTS: 4
COMMENTS:
EXHAUST GAS PRESSUHF IN INCHFS HG.
CARBO-BLASTIKALNUTSI PKIHR TO EMISSICNS PUN.
PROBE SHIFTED 20 DECRIES FROM VERTICAL
73.40
29.98
FINISH
FINISH
68.00
21. 9e
PERCENT
FLOW RATE, LITERS/HIN:
CLOCK
TIME
1404. 00
1407.00
1418.00
1457.00
TEST
MODE
\l 0
11 1
3/ 2
4/ 3
POWER
THRUSI.LBS PERCENT
OR RATED
SHP
7H02.00
9213.00
10743.00
411.00
T.O.
65
76
89
1
ENGINE
SPEED
RPM
Nl
5 B 74. 00
61 1U.OO
6429.00
2238. CO
N2
1361.00
948R.OO
97B3.00
6027.00
MEASURED
FUEL
FLOW
LB/HR
62B9.00
7441 .On
8950.00
1068.00
GAS GEN
AIR FLHW
Lfl/SEC
-0.00
-0.00
-0.00
-0.00
CALC COMPRESSOR
F/A DISCHARGE
TEMP
-0.000000
-0.000000
-0.000000
-0.000000
DEGREES F
-0.00
-0.00
-0.00
-0.00
FNGINE
PRESSURE
RATIO
FPK
2.13
2.37
2.62
-0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-o.oo
-0.00
POWER
PERCENT
RATED
T.O.
65
76
EXHAUST
GAS
TFMP
DEGREES f
F)70. 80
94H.20
1058.00
512.60
EXHAUST
GAS
PRESSURE
PSIA
02.40
68.90
75.80
11.60
co
IHETI
PP1V
bo.nn
40.00
30.00
610.00
CO
2
(MET)
PERCENT V
2.30
2.50
2.80
1.20
THC
IWEII
PPMV
1.38
1.20
1.50
1470.00
NO
IWETI
PPMV
54.00
68.00
94.00
10.00
NU
2
(WET)
PPMV
-0.00
-0.00
-0.00
-0.00
NO
X
(WET!
PPMV
5U.OO
73.00
10.00
10.00
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.oo
-o.oo
-0.00
-o.oo
POWER
PFRCENT
HATED
T.O.
65
76
89
3
MASS CXI
cu
LB/IK
LB FUEL
5.21
3.31
2. 15
87.02
MASS EMI
HC
LB/IK
LB FUEL
0.07
0.06
0.06
120. 10
MASS EMI
ND2
LH/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
MASS b«l
CC12
LB/IK
LB FUEL
1147.49
3150. 7C
3152.34
3661.68
MASS EMI
NO
LB/IK
LB FUEL
7.71
8. 96
1 1.06
2.34
MASS EMI
NOX
LPV1K
LB FUEL
0.30
9.62
1. 18
2.34
MASS EMI
CO
Lfl/HR
32.86
23.87
11.24
92.94
MASS EMI
HC
LB/HR
0.43
0.41
0.55
128.27
MASS EMI
N02
L6/HR
-0.00
-0.00
-0.00
-0.00
MASS EMI
CH2
L8/HR
19794.57
23'.44.34
28211.46
2872. 5B
MASS EMI
NO
LB/HR
48.58
66.66
99.02
2.50
MASS EMI
NOX
LB/HR
52.18
71.57
10.51
2.50
POWER
PFRCENT
RATED
T.Q.
65
76
89
1
Li1 /IKKTH-HM
4.212
2.591
1.791
226.121
2537.115
2544.702
2626.21H
6989.238
THC
IB/IK»TH-HK
0.055
0.045
0.051
312.OR5
NO
LO/1MTH-HR
6.227
/.216
9.217
6.089
LB/IKHTH-HR
-0.000
-0.000
-0.000
-0.000
NO
X
LB/IK«TH-HR
6.688
7.768
0.981
6.080
IV-86
-------
CAL ID NUMBER: »oe ENGINE TYPE «ND MOOELI JT jc - 7
TEST ORGANIZATION! UNITED/EPA
SERIAL NUNBERl 632283
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
I. 000
0.850
0.400
0.050
FRACTIONAL
POKER
0.050
1.000
0.650
0.400
0.050
FRACTIONAL
POWER
0.050
1.000
O.B50
0.400
0.050
POWER
1 TH
600.0
12000.0
10200.0
4800.0
600.0
POWER
1 TH
600.0
12000.0
10200.0
4800.0
600.0
POWER
f TH
600.0
12000.0
10200.0
4BOO.O
600.0
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
87.698 1138.526 .000 19.00
3.953 10165.035 .000 0.70
17.296 8525.746 .000 2.20
65.166 3883.257 .000 4.00
87.698 1138.526 .000 7.00
TOTAL FOR CYCLE:
LaS POLLUTANT/IK IB FUEL/CYClEl
LBS POLLUTANT/IK LB TH-HR/CYCLEJ
LBS POLLUTANT/1000K LB TH AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR IB/MR MIN.
107.406 1138.526 .000 19.00
0.0 10165.035 .000 0.70
0.521 8525.746 .000 2.20
12.884 3883.257 .000 4.00
107.406 11)8.526 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CTCL6:
LBS POLLUTANT/1000K LB TH AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
2.765 1136.526 .000 19.00
123.292 10165.035 .000 0.70
89.981 8525.746 .000 2.20
24.338 3883.257 .000 4.00
2.765 1138.526 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CVCLE:
LBS POLLUTANT/1000X IB TH AT T.O.:
CO
MASS
LBS.
27.771
0.046
0.634
4.344
10.231
43.027
36.358
39.330
0.384
' HC
MASS
LBS.
34.012
0.0
0.019
0.859
12.531
47.420
40.070
43.346
0.0
NOX
MASS
LBS.
0.876
.438
.299
.623
.323
.559
.387
.909
119.867
FUEL
MASS
LBS.
360.53
118.59
312.61
256.68
132.83
1183.45
FUEL
MASS
LBS.
360.53
118.59
312.61
258.68
132.63
1183.45
FUEL
MASS
LBS.
360.53
116.59
312.61
258.86
132.83
1183.45
LB CO /
IK L8 FUEL
77.028
0.389
2.029
16.781
77.026
LB HC /
IK LB FUEL
94.337
0.0
0.061
3.318
94.337
LB NOX/
IK LB FUEL
2.429
12.129
10.554
6.267
2.429
ENERGY
TH-HR
190.00
140.00
374.00
320.00
70.00
1094.00
ENERGY
1 TH-HR
190.00
140.00
374.00
320.00
70.00
1094.00
E MERCY
TH-HR
190.00
140.00
374.00
320.00
70.00
1094.00
LB CO /
1 TH-HR
0.14616
0.00033
0.00170
0.01356
0.14616
LB HC /
1 TH-HR
0.17901
0.0
0.00005
0.00268
0.17901
LB NOX/
TH-HR
0.00461
0.0102T
0.00882
0.00507
0.00461
IV-87
-------
OATfi 6/29/71
rest ORGANIZATION: PRATT t HHITNEY
ENGINE SUPPLIFR: PRATT AND MHITNEY
ENGINE DATA
CAL ID NUMBER: 6Z ENGINE TYPE AND MODEL: JT1D
RATED THRUST: 21000.
ENGINE TOTAL TINE: -0. MRS
TINF SINCE MOT SECTION OVERHAUL: -0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: -o. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
COM8USTOR CAN REPLACEMENT: -0. HRS
FIRST STAGF NOZZLE GUIDF VANF OVERHAUL: -0. HRS
Nl TURBINE OVERHAUL: -0. HRS
N2 TURBINE OVERHAUL! -0. HRS
FUEL: JP-4C FUEL H/C RATIO: 2.000
OPERATIONAL flATA ««»«»««
INLET AIR TEMPERATURE, OCGRFFS F: START 68.00 FINISH 7*.00
ATMOSPHERIC PRESSURE: START 30. i« FINISH 30.10
INLEI AIR HUMIDITY, LBS H20/L8 AIR: 0.0101
RELATIVE HUMIDITY: 60.00 PEPCfNT
SAMPIF LINE: TE«PFRATUPE, DEGREES C: 150.00, FLOH RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 11
COMMENTS:
BURNED fl/M
SERIAL NUMBER:
CLOCK
TIMF
1102.00
11)0.00
1139.00
1148.00
1203.00
12*0.00
1517.00
15*2.00
1553.00
1602.00
1703.00
POUFR
PERCENT
RATED
1.0.
1
8
32
60
94
98
R9
49
10
6
4
PDUFR
PERCENT
RATED
T.O.
3
a
u
64
94
98
99
49
10
6
4
POWER
PERCENT
RATED
T.O.
3
a
32
64
94
98
89
49
10
b
4
TEST
MODE
I/ 0
7/ 1
I/ 2
4/ 1
5/ 4
6/ 5
7/ 6
8/ 7
4/ 8
10/ 9
11/10
EXHHUST
GAS
TEMP
DEGREES r
594.00
592.00
678.00
976.00
1033.00
1070.00
1006.00
778.00
608.01
591.0^
597.'' I
MASS '"-Ml
CO
IB/IK
LB FUEI
104.1'
61.8*
10. l»
1.4(1
0.6H
0.61
0. Id
3.24
46.3!
85.93
108.69
cn
POWER ENGINE MEASURED GAS GEN CALC
THRUST. LBS PERCENT SPEED FUEL AIR FLOW F/A
OP RATED RPM FLOW LI/SEC
SHP r.O. M N2 LB/HO
756.00 3 U25.00 5450.00 1077.00 . 16.08 0.0(18360
1777.00 B 2610.00 6861.00 1523.00 51.70 O.OU8330
6778.00 32 4430.00 P545.00 3577.00 102.70 0.009770
I4628.00 69 5880.00 9575.00 7789.00 161.91 0.013540
I9R55.00 94 659(1. OC 10095.00 11255.00 193.51 0.016420
20712.00 98 6730.00 10210.00 11905.00 19865.00 0.016920
13811.00 89 645C.OC 10008.00 10421.00 185.54 0.015850
10325.00 49 5755. OC 9150.00 5413.00 132.89 0.011440
2790.00 10 2855.00 7235.00 1692.00 59.20 0.008000
1349.00 6 2235.00 6760.00 1763.00 45.17 0.007830
847.00 4 1815.00 5433.00 IC48.00 35.78 O.Offl?IO
EXHAUST CO CO THC NCI NO NO
GAS
-------
CAL 10 NUMBER: 62 ENGINE TYPE AND MOOED JI30
TEST ORGANIZATION: PRATT t UHITNEY
SERIAL NUMBER: x-3is-44
NODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
HII- IDLE
0.050
1.000
0.850
0.400
0.050
POWER
I TH
1050.0
21000.0
1T850.0
8*00.0
1050.0
EMISSION FUEL
RATE RATE
IB/ MR LB/HR
69.480 693. B96
28.6*4 12006.102
15.955 4972.946
36.032 4482.10!
69.488 693.896
USAGE TIME IN
WT FACTOR MODE
NIN.
TOTAL FOR CYCLE:
L8S POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
MODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
0.050
1.000
0.950
0.400
0.050
POWER
* TH
1050.
21000.
17650.
8400.
1050.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
56.082 693.696
12.53* 12006.102
11.410 9972.348
4.679 4482.105
56.062 693.696
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLEl
TH-HR/CYCLE:
LB TH AT T.O.I
USAGE TIME IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.050
1.000
0.650
0.400
0.050
POKER
1 TH
1050.
21000.
1TB50.
8*00.
1050.
0
0
0
0
0
EMISSION FUEL
KATE HATE
LB/HR LB/HR
1.306 693.896
199.107 12006.102
126.417 9972.346
26.752 4462.105
1.306 693.896
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IOOOK
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
22.005
0.334
0.561
2.535
8.107
33.562
30.367
I7.S31
1.591
HC
MASS
LBS.
17.759
0.146
0.418
0.312
6.543
25.179
22.782
13.152
6.964
KOX
MASS
LBS.
0.413
2.323
4.635
1.783
0.152
9.307
6.421
4.862
110.615
FUEL
MASS
LBS.
219.73
140.07
365.65
298.81
60.95
1105.22
FUEL
MASS
LBS.
219.73
140.07
365.65
298. Bl
60.95
1105.22
FUEL
MASS
LBS.
219.73
1*0.07
365.65
298.81
60.95
1105.22
LB CO /
IK LB FUEL
100.142
2.386
1.590
6.485
100.142
LB HC /
IK LB FUEL
80.822
1.044
1.144
1.044
60.822
LB NOX/
IK LB FUEL
1.882
16.564
12.677
5.969
1.882
ENERGY
TH-HR
332.50
245.00
654.50
560.00
122.50
1914.50
ENERGY
TH-HR
332.50
245.00
654.50
560.00
122.50
1914.50
ENERGY
t TH-HR
332.50
245.00
654.50
560.00
122.50
1914.50
LB CO /
1 TH-HR
0.06618
0.00136
0.00069
0.00453
0.06618
LB HC /
1 TH-HR
O.OS34I
0.00060
0.00064
0.00056
0.05341
IB NOX/
f TH-HR
0.00124
0.00948
0.00708
0.00318
0.00124
IV-89
-------
DATE: 6/29/71
TEST ORGANIZATION: PRATI c WHITNEY
ENGINE SUPPLIER: PRATT AND WHITNEY
ENGINE DATA *«««»»««»««»««
CAL ID NUM.9FR: 296 ENGINE TYPE AND MODEL: JT3D
RATED THRUST: 21000.
ENGINE TOTAL TIME: -0. HRS
TIME SINCE HOT SECTION OVERHAUL: -0. HRS
TIME SINCE:
SERIAL NUMBER:
NI COMPRESSOR OVERHAUL: -o. MRS
N2 COMPRESSOR OVERHAUL: -o. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
Nl TURBINE OVERHAUL: -0. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUFL: JP-4C FUEL H/C RATIO: 2.000
OPERATIONAL DATA ««««««««««««««
INLET AIR TEMPERATURE, DEGREES F: START 7*.00 FINISH 73.00
ATMOSPHERIC PRESSURE: START 3C.IO FINISH 30.06
INLET AIR HUMIDITY, IBS H20/LB AIR: 0.0118
RELATIVE HUMIDITY: 62.00 PERCENI
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITFRS/MIN:
SAMPLE LINF TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: <>
COMMENTS:
BURNER B/M
CLOCK
TIME
1713.00
1722.00
1731.00
1753.00
1800.00
1813.00
1830.00
1845.00
1B53.0C
TFSI
MODE
I/
21
V
W
>/
6/
7/
8/
9/
0
1
2
1
4
5
6
I
B
POWER
THRUST, LBS PERCENT
OR RATED
SHP
1890.00
6106.00
11673.00
20079.00
20433.00
1 BITS. 00
10466.00
2355.00
1301.00
T.Q.
B
30
69
95
97
69
49
II
6
ENGINE
SPEED
RPM
Nl
2627.00
4437.00
5925.00
6635.00
6675.00
6440.00
5277.00
2875.00
2210.00
N2
6902.00
8582.00
9627.00
10152.00
10185.00
10017.00
91 72.00
7265.00
6225.00
MEASURED
FUEL
FLOW
LB/HR
1529.00
3540.00
7907.00
11344.00
11540.00
10329.00
5484.00
1706.00
1247.00
GAS GEN
AIR FLOW
LI/SEC
52.55
102.00
159.91
192.46
194.49
185.12
133.22
58.70
45.27
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.008150
0.009730
0.013930
0.016650
0.016760
0.015740
0.011570
O.OOB140
0.007710
DEGRFFS F
292.20
493.70
675.20
7M.50
777.30
753.00
591.50
319.30
244.80
ENGINE
PRESSURE
RATIO
EPR
1.05
1.20
1.58
1.92
1.94
1.83
1.37
1.06
1.04
TURBINE
INLET
TEMP
DEGRFFS F
859.00
1167.00
1583.00
1830.00
1B4I.OO
1760.00
1373.00
R88.00
780.00
POWER EXHAUST
PERCENT GAS
RATED TFMP
T.O. DEGRFES F
30
69
95
97
89
605.10
6">0.80
913.30
1049.20
1058.10
1002.HO
774.10
624.00
585 .30
EXHAUST
GAS
PRESSURE
PSI A
15.51
17.73
23.20
28.01
2B.36
26.70
20. 15
15.70
15.31
cu
(WET)
PPMV
477.00
97.00
17.10
1 1 . 30
11.50
1 1.60
36.60
400. 60
666.40
CO
2
IWFTI
PFRCFNT V
1.57
1.95
2.93
(.49
3.50
3.26
2.32
1.59
1.40
THC
IWET)
PPMV
334.00
29.40
2.60
1.90
1.50
1.40
1.50
1U7.70
649. 80
NO
IWET)
PPMV
11 .00
12.00
0.0
151 .00
156.00
127.30
48.70
9.10
9.20
NO
2
(WET)
PPMV
10.00
13.00
7.90
B.OO
9.00
B.BO
8. 60
11.30
5.00
NO
X
(UFT)
PPMV
21.00
25.00
7.90
159.00
165.00
136.10
57.30
20.40
14.20
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-C.OO
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.co
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
fl
30
69
95
97
89
49
11
MASS E«I
cn
LB/IK
LB EUFL
57.69
9.87
1 .If:
0.65
0. 66
0.71
3.15
'.P. 52
89. IP,
MISS EMI
HC
LB/1K
LB FUFL
23.14
1.71
0. 10
0.06
0.05
0.05
0.07
13.02
48.46
MASS EMI
MU2
LB/1K
LB FUFL
1.99
2.17
o.na
0.75
0.84
0.89
1.21
2.25
1.07
MASS FMI
CC?
LB/IK
Lfl FUEL
2983.62
31 17.54
3135.64
31 36.56
11 36.5H
3136. 49
3132.60
3025.79
2864.36
MASS EMI
NO
IP/IK
LB FUEL
2.19
2.01
0.0
14.19
14.61
12.80
6.87
1.81
1.97
MASS CMI
NOX
LB/IK
Lfl FUEL
4.17
4.1«
0.88
14.94
15.46
13.69
8.09
4.06
3.04
MASS EMI
CO
Lfl/HR
18.21
14.94
9.21
7.13
7.57
7.34
17.25
82.77
11 1.46
MASS FMI
HC
Lfl/HB
35.18
6.07
0.80
0.71
0.57
0.51
0.40
22.21
60.43
MASS EMI
NO 2
LB/HH
3.04
7.69
6.99
8.53
9.73
9.14
6.66
3.84
1.33
MASS EMI
C02
LB/HR
4561.95
11036.01
24793.46
15581.11
36196.13
32396.84
17179.17
5162.00
3571.86
MASS EKI
NO
LR/HK
3.34
7.10
0.0
160.94
168.66
132.25
37.70
1.09
2.45
MASS FM|
NOX
LR/HR
6. 38
14 . 79
6.99
169.46
178.39
141.39
44.36
6.92
3.79
POWER
PERCFNT
RATFP
T.H.
10
69
95
49
11
co
LP/1K0TH-HR
46.671
5.454
0.628
0. 365
0.370
0.119
1 .64H
15.148
85.538
I B/1KKTH-HR
2413.71?
1722.773
1699.734
1772.056
1771.456
1716.1 17
1641.427
2191.931
2741.260
THC
LB/ 1MTH-HR
18.717
0.947
0.055
0.015
0.028
0.027
0. 019
9.412
46.378
NO
LB/IKHTH-HR
1.768
1. 108
0.0
8.015
6.254
7.006
3.602
1.311
1.863
LR/IKHTH-HR
1.607
1.201
0.476
0.425
0.476
0.484
0. 636
1.629
1.023
NO
X
LB/1KHTH-HR
3.375
2.309
0.476
1.440
fl.730
7.490
4.238
2.940
2.907
IV-90
-------
CAL ID NUMBER: 296 ENGINE TYPE AND NQDELl JT30
TEST ORGANIZATION: PRATT t WHITNEY
SERIAL NUMBERl X-31S-44B
MODE FRACTIONAL
POKER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
O.OSO
1.000
0.850
0.400
0.050
POKER
f TH
1050.
21000.
1TB50.
8400.
1050.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
113.292 496.449
14.620 11832.008
9.295 9850.836
28.414 4549.T11
111.292 996.449
USAGE TIKE IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
IBS POLLUTANT/ IK LB
LBS POLLUTANT/IOOOK
HODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.050
1.000
0.850
0.400
0.050
POWER
» TH
1050.
21000.
17850.
8400.
1050.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
105.495 996.449
3.504 11832.008
1.783 9850.836
5.142 4549.711
105.495 996.449
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
MODE
FRACTIONAL
POKER
TAXI-IDLE 0.050
TAKEOFF 1.000
CLINBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.050
POWER
* TH
1050.0
21000.0
17850.0
8400.0
1050.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
2.517 946.449
193.981 11832.008
122.215 4850.836
27.197 4549.711
2.517 996.449
UT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR NODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
35.876
0.171
0.341
1.894
13.217
51.499
41.722
26.899
0.812
HC
MASS
LBS.
33.407
0.041
0.065
0.343
12.308
46.163
37.399
24.112
1.947
NOX
MASS
IBS.
0.797
2.263
4.481
1.813
0.294
9.648
7.816
5.040
107.767
FUEL
MASS
LBS.
315.54
138.04
361.20
303.31
116.25
1234.35
FUEL
MASS
LBS.
315.54
138.04
361.20
303.31
116.25
1234.35
FUEL
MASS
LBS.
315.54
138.04
361.20
303.31
116.25
1234.35
LB CO /
IK LB FUEL
113.696
1.236
0.944
6.245
113.696
LB HC /
IK LB FUEL
105.871
0.296
0.181
1.130
105.871
LB NOX/
IK LB FUEL
2.526
16.395
12.407
5.978
2.526
ENERGY
f TM-HR
332.50
245.00
654.50
560.00
122.50
1914.50
ENERGY
TH-HR
332.50
245.00
654.50
560.00
122.50
1914.50
ENERGY
1 TH-HR
332.50
245.00
654.50
560.00
122.50
1914.50
LB CO /
TH-HR
0.10790
0.00070
0.00052
0.00338
0.10790
LB HC /
1 TH-HR
0.10047
0.00017
0.00010
0.00061
0.10047
LB NOX/
1 TH-HR
0.00240
0.00924
0.00685
0.00324
0.00240
IV-91
-------
DATE: 6/29/71
TEST ORGANISATION: PRATT G WHITNEY
ENGINF SUPPLIER: PRATT ANn WHITNEY
FNC1NF DATA
CAL in NUMBER: ?97 ENGINE TYPE AND MODELS JTIO
RATED THRUST: 21000.
ENGINE TOTAL TIMF: -0. HRS
TIME SINCE HUT SECTION OVERHAUL: -0. HRS
TIKE SINCE:
NI COMPRESSOR OVERHAUL: -o. HRS
N2 COMPRESSOR OVERHAUL: -o. HRS
CONBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANF OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL: JP-5 FUEL H/C RATIO: I.170
OPERATIONAL DATA «««»*»
INLET AIR TEMPFRATURF, DEGREES F: START 71.00 FINISH 68.00
ATMOSPHERIC PRESSURE: START 3C.OB FINISH 30.09
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0130
RELATIVE HUMIDITY: 77.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/HIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 10
COMMENTS:
BURNER ° B/M
SERIAL NUMBER:
CLOCK
TIME
2055.00
2110.00
2122.00
2124.00
2140.00
2149.00
2204.00
2211.00
2228.00
2234.00
POWER
PERCENT
RATED
T.O.
4
9
10
61
93
96
89
49
II
6
POrfFP
PERCENT
HATED
T.O.
4
9
10
69
93
96
89
49
11
6
POWER
PERCENT
RATED
T.O.
4
9
30
69
91
96
89
49
11
6
TEST
"ODE
I/ 0
2/ 1
I/ 2
4/ 3
5/ 4
6C 5
T/ 6
B/ 7
9/ 3
10/ 9
EXHAUST
C.AS
TF.MP
OF.GRCES f
583.00
594 . CO
67H.OO
8H2.00
ioie.no
1056.00
1000. on
767.10
596.00
575.00
MISS EMI
CO
LB/1K
LB FUFL
118.55
71.45
12.45
1.57
O.."i«
0.61
0.80
4.16
54. *6
101 .28
CO
POWER ENGINE
THRUST, LBS PERCENT SPEED
OR RATFD RP*
SHP
857.00
1911.00
64B7.00
14613.00
19723.00
20314.00
18735.00
10480.00
2171.00
1307.00
EXHAUST
GAS
PRESSU"
PSI A
15.10
15.43
17.70
21.15
27.90
ZH.60
26.90
20. 10
15.70
15.30
MASS E*I
HC
LB/1K
Lfl FUEL
115.90
17.59
1.77
0.31
0.17
0.11
0.11
0.25
20.29
77.62
L» /IKK TH-MH
157.
59.
7 .
0.
0.
0.
0.
2.
40.
101.
140
973
016
863
194
361
454
142
779
021
T.O. NI N2
4 1815.00 5445.00
9 2617.00 6860.00
30 4413.00 B557.00
69 5902.00 9580.00
93 6609.00 10108.00
96 6697.00 10179.00
89 6455.00 10000.00
49 5270.00 9138.00
11 2870.00 7240.00
6 2200.00 6182.00
MEASURED
FUFL
FLOW
LB/HR
1136.00
1604.00
3657.00
8C34.00
11472.00
11946.00
10665. 00
5625.00
1769.00
1314.00
cn co TMC NO
(MFTI 2 IW
E PPMV IWETI P
PERCENT V
980.60 1.39 1674
620.90 1.62 570
126. 60 2.02 31
21.00 2.93 8
12.30 3.63 5
11.60 3.71 3
11.40 3.16 3
51.80 2.37 5
4R3.10 1.69 113
861. .70 1.51 1159
MASS EMI MASS EMI MASS EMI
H02 C02 NO
LB/1K LB/U LB/1K
Lfl FUEL LB FUFL LB FUEL
0.28 264C.29 1.55
1.17 2929.14 0.91
1.60 312C.10 3.39
0.66 3141.20 6.13
0.4A 3142.99 12.34
0.59 3143.24 13.29
0.63 3142.98 11.61
1.09 3136. 9"J 5.80
0.91 3002. 9rt 1.95
D.52 2772.45 1.38
co r HC
2
LR/KNTH-HH IH/IKKTH-HH
1499. S44 153.637
245S.575 31.549
1758.936 1.000
1726.983 0.172
IB.! 4. 140 0.099
1848.419 0.064
1789.160 0.060
1681.739 0.112
2240.516 15.140
2787.295 7B.036
FT) IUET
PMV PPM
.00 7.
.10 4.
.50 21.
.00 72.
.40 136.
.50 150.
.10 118.
.10 41.
.10 10.
.80 7.
MASS EMI
N0«
L6/1K
LB FUFL
1.81
2.02
4.99
6.79
12.82
13. ns
12.21
6.89
2.86
1.90
NO
GAS GEN
AIR FLOW
LB/SEC
CALC
F/A
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIO
DEGREES F
36.06
50.95
102.49
161.65
192.75
196.18
187.29
133.90
59.50
45.40
NO
1 2
V (UE1I
PPMV
80 1.40
80 5.90
00 9.90
50 5.9n
30 5.30
00 6.70
70 6.40
90 7.90
5C 4.90
20 7.70
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
MASS EMI MASS
CO
Lfi/HR
134.67
114.61
45.51
12.61
7.78
7.47
B.51
74.55
96.69
133. OH
HC
LB/
111.
60.
6.
2.
1.
1.
1.
1.
35.
101.
008830
OOB820
010010
014000
016810
017190
016070
011800
OOB330
006110
NO
X
IHETI
PPMV
9.20
10.70
10.90
78.40
141.60
156.70
125.10
49.80
15.40
9.90
195.
285.
486.
666.
761.
774.
739.
584.
312.
236.
00
00
00
00
00
00
00
00
00
00
EPR
.02
.05
.20
.58
.92
.96
.84
.37
.06
.04
ALDEHYDES SMOKE
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
FMI MASS EMI
H«
67
29
49
51
96
29
13
IS
90
99
NO
>
LB/IKKTH-HR Lfl / 1KHTH-HR
2.
0.
1.
4.
7.
7.
6.
3.
1.
1 .
053
762
912
467
176
813
60S
112
455
389
0.369
0.936
0.901
0.364
0.279
0.349
0.356
0.587
0.679
0.521
NO 2
LB/HR
n.32
1.79
5.85
5.31
5.50
7.09
6.67
6. 15
1.61
0.68
00 -0
oo -o
00 -0
00 -0
oo -o
00 -0
00 -0
oo -o
00 -0
00 -0
MASS EMI
C07
LB/HR
2999.17
4698.34
1 1410.27
25236.41
36056.39
37549.19
13519.69
17645.58
5112.26
3642.99
NO
X
.00
.00
.00
.00
.on
.00
.00
.00
.00
.00
MASS
NO
LB/
1.
1.
12.
65.
141.
158.
123.
32.
3.
1.
TURBINE
INLET
TEMP
DEGREES F
797.00
898.00
1178.00
1579.00
1630.00
1864.00
1766.00
1380.00
893.00
796.00
PART ICULATES
-0.00
-0.00
-C.OO
-0.00
-0.00
-C.OO
-0.00
-o. on
-0.00
-o.no
EMI MASS EMI
NOX
HR LB/HR
76 7.08
46 3.24
40 18.25
28 70.59
53 147.04
71 165.60
79 130.47
61 36.76
45 5.06
R? 2.50
Lfl/lMTH-HR
2.422
1.698
2. 811
4.631
7.455
8.162
6.964
1.699
2.134
1.910
IV-92
-------
CM. 10 NUMBER) 29T ENGINE TYPE AND MODEL! JI3D
TEST ORGANIZATION: PRATT i WHITNEY
SERIAL NUMBER I X-315-44C
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IOIE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.090
FRACTIONAL
POMER
0.050
1.000
O.B90
0.400
0.030
FRACTIONAL
POMER
0.050
1.000
0.850
0.400
0.050
POMER
1 TH
1050.0
21000.0
17850.0
8400.0
1050.0
POWER
I TH
1050.0
21000.0
17650.0
8400.0
1050.0
POWER
TH
1050.0
21000.0
17850.0
8400.0
1050.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
137.830 1184.024
20.928 12931.859
12.097 10131.215
37.774 4782.535
137.830 1184.024
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
123.160 1184.024
3.008 12531.859
2.431 10131.215
4.155 4782.535
123.160 1184.024
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
2.355 1184.024
189.466 12531.859
114.911 10131.215
26.290 4782.535
2.355 1184.024
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ I OOOK
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE"
TH-HR/CYCLEt
LB TH AT T.O.I
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCL£t
LB TH AT T.O.:
USAGE TIME IN
FACTOR NODE
MIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL/CYCLE!
TH-HR/CVCLEI
IB TH AT T.O.I
CO
MASS
LBS.
43.646
0.244
0.444
2.518
16.080
62.932
46.630
32.871
1.163
' HC
MASS
LBS.
39.001
0.035
0.089
0.277
14.369
53.771
39. 842
28.0B6
1.671
NOX
MASS
L8S.
0.746
2.210
4.213
1.793
0.279
9.147
6.819
4.804
105.259
FUEL
MASS
LBS.
374.94
146.20
371.48
318.84
138.14
1349.59
FUEL
MASS
LBS.
374.94
146.20
371.48
318.84
138.14
1349.59
FUEL
MASS
LBS.
3T4.94
146.20
371.48
318.84
138.14.
1349.59
IB CO /
IK L8 FUEL
116.408
1.6TO
1.194
7.896
116.408
LB HC /
IK LB FUEL
104.018
0.240
0.240
0.869
104.018
18 NOX/
IK LB FUEL
1.9B9
19.119
11.342
9.497
1.989
ENERGY
1 TH-«R
332.50
245.00
614.90
960.00
122.50
1914.90
ENERGY
1 TH-HR
332.90
249.00
694.90
560.00
122.90
1914.90
ENERGY
f TH-HR
331.50
249.00
694.50
560.00
122.90
1914.50
LB CO /
1 TH-HR
0.13127
0.00100
0.00066
0.00490
0.13127
LB HC /
1 TH-HR
0.11730
0.00014
0.00014
0.00049
0.11730
LB NOX/
1 TH-HR
0.00224
0.00902
0.00644
0.00113
0.00224
IV-93
-------
01TE: 6/30/71
TFST ORGANIZATION: PRATT I WHITNEY
ENGINF SUPPLIER: PRATT AND WHITNEY
ENGINF DATA
CAL ID NUMBER: 798 ENGINE TYPE AND HOD El' JT3D
RATED THRUSTI 21000.
ENGINE TOTAL TINE: -0. MRS
TIMF SINCE HOT SECTION OVERHAUL: -0. HRS
TINF SINCE:
HI COMPRESSOR OVERHAUL: -0. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
COHBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGF NOZZLE GUIDE VANE OVERHAUL: -0. HRS
Nl TURBINE OVERHAUL: -0. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL: JP-5 FUEL H/C RATIO: 1.970
OPERATIONAL DATA »«««««««««««
INLET AIR TEMPERATURE. OFGREES f: START 81.00 FINISH 67.00
ATMOSPHERIC PRESSURE: START 10.00 FINISH 29.86
INLET AIR HUMIDITY, UBS H20/LB AIR: 0.0170
RELATIVE HUMIDITY: 73.00 PERCENT
SAMPLE LINE: TEMPERATURE, CEGREES C= 150.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIMF, SEC: 1.00
MJNBFR OF TESTS: 4
COMMENTS:
BURNER " B/M
SERIAL NUMBER:
K-J15-4*0
2.00
CLOCK
TIME
1030.00
1212.00
1)21.00
1533.00
TFST
MOTE
I/
11
M
4/
0
\
2
3
POWER
THRUST, LBS PERCENT
OR RATED
SHP
9188.00
18606.00
16413.00
1748.00
T.O.
43
88
76
R
ENGINE
SPEED
ftPM
Nl
5124.00
6570.00
6289.00
1806.00
N2
9C85.00
10145.00
9955.00
5440.00
MEASURED
FUEL
FLOW
LB/HR
5083.00
11059.00
9444.00
1105.00
GAS GEN
AIR FLOW
LB/SEC
121.91
184.71
171.72
3*.21
CALC COMPRESSOR
F/A DISCHARGE
TFMP
0.011530
0.016910
0.015510
O.OOB800
DEGREES F
57B.50
773.70
737.00
217.70
ENGINE
PRESSURE
RATIO
EPR
1.32
1 .85
1.72
1.02
TURBINE
INLET
TEMP
DEGRFFS F
1)59.00
18*7.00
17)3.00
816.00
POMER
PERCENT
RATED
T.O.
43
an
7(1
8
EXHAUST
GAS
TEMP
DEGRFES F
769.90
1051.30
930. no
676.70
EXHAUST
GAS
PRESSURE
PSIA
19.40
27.07
24.98
15.06
CO
1 WET 1
PPMV
63.50
12.50
14.10
466.60
CO
2
(WFTI
PERCFNT V
;.27
1.55
1.40
1.57
THC
IWETI
PPMV
5.40
1.10
4.60
1650.00
NO
(NET)
PPMV
37.40
134.70
0.0
9.30
NO
2
(WETI
PPMV
6. no
6.00
3.50
2.10
NO
X
IWFTI
PPMV
43.40
140.70
3.50
11.40
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
PARTICIPATES
-0.00
-0.00
-0.00
POWEP
PFRCENT
RATED
T.O.
43
88
78
a
MASS EMI
CO
LB/IK
LB FUEL
5.58
0. 70
0.83
52.41
MASS EMI
HC
LB/IK
LP FUEL
0.27
0.04
0.15
106.15
MASS EMI
N02
L3/1K
LB FUEL
0.67
0.56
0.34
0.39
MASS EMI
C02
Lfl/lK
L9 FUFL
31)5.01
3143.32
1142.80
2770.96
MASS FMI
NO
LB/IK
LB FUFL
5.40
12.47
0.0
1.72
MASS EMI
NOX
LP/1K
LB FUEL
6.27
13.02
0.34
2.10
MASS C»l
CO
LB/HR
28.17
7.79
7.63
57.97
MASS fMI
HC
LB/HR
1.38
0.39
1.46
117.30
MASS [Ml
NO 2
LB/HR
4.40
6.14
3. 19
0.43
MASS EMI
C02
LB/HR
15935.25
34761.98
296X0.56
3061.91
MASS EMI
NO
LB/HR
27.45
117. R9
0.0
1.90
MASS CMI
NO*
LB/HR
31.85
144. C3
3.19
2.32
POWER
PERCENT
RATF.O
T.O.
41
Bfl
78
CO
LB/IKKTH-HR
3.099
0.419
0.477
33.133
LB/ 1MJTH-HR
1714.354
1868.122
lflOH.357
1751.663
THC
LB/1K«TH-H<<
0.150
0.021
O.OD9
67.103
NO
IK«TH-HR
2.9B7
7.411
0.0
I .085
LR/IKKTH-HR
0.479
0.330
0.195
0.245
NO
X
LB/1K«TH-HR
3.466
7.741
0.195
1.330
IV-94
-------
cat ID NUMBER: 298 ENGINE TYPE AND MODEL: JTID
TEST ORGANIZATION: PRATT C WHITNEY
SERIAL NUMBER!
MODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
FRACTIONAL
POWER
0.050
1.000
0. B50
0.400
0.050
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
TH
1050.0
21000.0
1T850.0
8*00.0
1050.0
POWER
1 TH
1050.0
21000.0
1TB50.0
8400.0
1050.0
POWER
1 TH
1050.0
21000.0
17650.0
8400.0
1050.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
46.640 690.214
4.155 12701.266
.11.552 10464.590
15.814 4727. J98
46.640 690.219
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
108.854 690.219
2.794 12701.266
2.102 10464.590
9.807 4727. 398
108.854 690.219
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IOOOK
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
1.112 690.219
201.021 12701.266
128.955 10464.590
27.518 4727.198
1.112 690.219
TOTAL FOR CYCLEl
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
USAGE TIME IN
FACTOR MODE
NIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE!
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.t
CO
MASS
LBS.
14.764
0.048
0.424
2.188
5.441
23.070
20.129
12.050
0.231
HC
MASS
LBS.
34.470
0.011
0.084
0.654
12.700
47.441
41.828
25.041
1.552
NOX
MASS
LBS.
0.152
2.J45
4.728
1.835
0.110
9.190
B. 193
4.405
111.676
FUEL
MASS
LBS.
216.57
146.18
1B3.70
315.16
80.51
1146.14
FUEL
MASS
LBS.
218.57
148.18
181.70
115.16
80.51
1146.14
FUEL
MASS
LBS.
218.57
148.18
181.70
115.16
80.51
1146.14
LB CO /
IK LB FUEL
67.573
0.127
1.104
7.576
67.571
LB HC /
IK LB FUEL
157.709
0.220
0.220
2.074
157.709
LB NOX/
IK LB FUEL
1.611
15.827
12.121
5.821
1.611
ENERGY
TH-HR
332.50
245.00
654.50
560.00
122.50
1914.50
ENERGY
TH-HR
112.50
245.00
654.50
560.00
122.50
1914.50
ENERGY
TH-HR
312.50
245.00
654.50
560.00
122.50
1414.50
LB CO /
TH-HR
0.04442
0.00020
0.00065
0.00426
0.04442
LB HC /
TH-HR
0.10167
0.00013
0.00011
0.00117
0.10367
LB NOX/
TH-HR
0.00106
0.00957
0.00722
0.00328
0.00106
IV-95
-------
DATE: 7/21/71
TEST ORGANIZATION: U.S. BUREAU OF MINES
ENGINE SUPPLIER! AMERICAN AIRLINES
ENGINE DATA
CAL 10 NUNBERl 292
ENGINE TYPE AND MODEL: JTJD-1
SERIAL NUNBERl 642590
RATED THRUST! 17000.
ENGINE TOTAL TIME: 21605. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIMF SINCE:
NI COMPRESSOR OVERHAUL: o. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO: 1.920
FUEL: JET - A
OPERATIONAL DATA »»««««»««»««
INLET AIR TEMPERATURE. DEGREES F: START 85.00 FINISH 85.00
ATMOSPHERIC PRESSURE: START 29.12 FINISH 29.32
INLET AIR HUMIDITY. LBS H20/LB AIR: O.OOBO
RELATIVE HUMIDITY: 21.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 134.00, FLOW RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SEC: 0.99
NUMBER OF TESTS: 5
COMMENTS:
H/C IS CAL-ESTIMATED
USED SPEY PR06E LOCATED ONE PIPE 0/A
DOWNSTREAM DUE TO LOCATION OF A.A.SUPPORT STAND.
SAMPLE LINF TEMP. AVERAGED
9473
CLOCK
TIME
1)0.00
115.00
145.00
150.00
200.00
POWER
PERCENT
RATED
T.O.
49
5
51
68
84
POWER
PERCENT
RATED
T.O.
49
5
51
66
84
POKED
PEOCENT
RATED
T.O.
49
5
51
6B
84
TEST
NflDE
5/ 0
4/ 5
I/ 4
2/ 1
3/ 2
EXHAUST
GAS
TEMP
DEGREES F
740.00
570.00
750.00
825.00
900.00
MASS EMI
CO
LB/1K
L9 FUEL
4.73
87.50
4.29
2. 32
1.43
CO
POWER ENGINE MEASURED
THRUST, LBS PERCENT SPEED FUEL
OR RATED RPM FLOW
SHP T.O. NI N2 LB/HR
8400.00 49 5218.00 8947.00 4500.00
930.00 5 1950.00 5592.00 900.00
8750.00 51 5270.00 89BO.OO 4690.00
11610.00 68 5876.00 9410.00 6390.00
14360.00
FKHAUST
GAS
84 6370.00 9750.00
CO
(WETI
PRESSURE PPMV
PSIA
18.44
14.92
18.68
20. UK
23. 25
MASS EMI
HC
IB/ IK
LB FUEL
0.29
105.16
0.31
0.20
0.12
LB/IKIITH-HR
2.
84.
2.
I .
0.
533
674
298
279
916
55.00
700.00
50.50
29. JO
20.00
MASS EMI *ASS
CO THC
2 IWETI
IWETI PPMV
PERCENT V
2.33 5.80
1.39 1469.00
2.16 6.30
2.52 4.30
2.80 3.00
8170.00
NO
GAS GEN
AIR FLOW
IB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
(WETI
PPMV
36.
0.
37.
60.
86.
EMI MASS tHl MASS tMI
ND2 C02 NO
IB/IK LB/1K LB/1K
LR FUEL LB
3.11 3147
2.05 2729
3.21 3148
1.83 3151
2.35 1153
CO
2
LB/IMTH-HR
1696.254
2641.845
1687.496
1734.657
1794.042
NOX
LR/IK
70
0
70
60
80
MASS
CO
NO
2
IWETI
PPMV
22.00
10.00
23.00
14.00
20.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
NO
X
(WETI
PPMV
58.70
10.00
60.70
74.60
106.80
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIO
DEGREES F EPR
-0.00 1.32
-0.00 1.04
-0.00 1.34
-0.00 1.50
-0.00 1.70
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES SMOKE PARTICULATES
0.92 -0.00
38.40 -0.00
0.65 -0.00
0.32 -0.00
0.31 -0.00
EMI MASS EMI MASS EMI MASS EMI MASS EMI
LB/HR
Hr.
LB/HR
NH2 C02 NO
LB/HR LB/HR LB/HR
-0.00
-0.00
-c.oo
-0.00
-c.oo
MASS
EMI
NOX
IB/hR
FUEL LB FUFL LB FUEL
.68 5.18
.91 0.0
.31 5.26
.70 7.92
.30 10.22
THC
L8/IKITH-HR
0.153
101.770
0.164
0.108
0.070
8.29
2.05
8.47
9.75
12.57
NO
21.
78.
20.
14.
11.
LB/1KITH-HR
2.
0.
2.
4.
5.
777
0
818
361
814
28
75
11
85
71
1.29
94.65
1.44
1.25
1.01
NO
2
LB/IKHTH-HR
1.664
1.987
1.719
1.007
1.340
13.98 14164.54 23.12
1.85 2456.92 C.O
15.04 14765.59 24.66
11.70 20139.36 50.63
19.24 25762.44 83.49
NO
X
LB/1KITH-HR
4.441
1.9H7
4.517
5.368
7.154
37
1
39
62
102
.30
.85
.70
.33
.73
IV-96
-------
C»L 10 NUMBER: 292 ENGINE TYPE AND MODEL: JT30-1
TEST ORGANIZATION: U.S. BUREAU OF MINES
SERIAL NUMBER: 6*2590
MODE
TAXI-IOIE
TAKEOFF
CLTMBOUT
APPROACH
TAXI-IDLF
FRACTIONAL
POWER
O.OSO
1.000
0.850
o.*oo
0.050
POWER
1 TM
850.
17000.
14*50.
6800.
850.
0
0
0
0
0
EMISSION FUEL
RATE RATE
Lfl/NR LB/HR
70.5*6 8*6.397
4.088 9979.613
8.920 8282.012
14.147 3797.192
70.5*6 8*6.397
USAGE TIME IN
NT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
HQOE
TAXI-IOLF
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.050
1.000
0.850
0.400
0.050
POWER
TH
B50.
17000.
14*50.
6800.
850.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR IB/HO
87.958 846. 397
1.100 9979.613
1.5*6 8282.012
1».17I 3797.192
87.958 8*6.397
.000 19.00
.000 0.70
.000 2.20
.000 *.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
L8 TH AT T.O.:
USAGE TIME IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
L9S POLLUTANT/ IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDL*
FRACTIONAL
POWER
0.050
1. 000
0.850
O.»00
0.050
POWER
TH
850.
17000.
14*50.
6800.
850.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.706 8*6.397
1*1.012 9979.613
100.407 8282.012
27.717 3797.192
1.706 8*6.397
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
NT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
L3S POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
.000 19.00
.000 0.70
.000 2.70
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLEI
LB TH AT T.Q.:
CO
MASS
LBS.
22.3*0
0.0*8
0. 327
2.276
8.230
33.221
31.9*3
21.435
0.281
HC
MASS
LBS.
27.853
0.013
0.057
0.958
10.262
39.1*3
37.637
25.256
0.760
NOX
MASS
L8S.
0.5*0
1.6*5
3.682
1.8*8
0.199
7.91*
7.609
5.106
96.773
FUEL
MASS
LBS.
268.03
116.43
303.67
253.15
98.75
10*0.02
FUFL
MASS
LBS.
268.03
116. *3
303.67
253.15
98.75
10*0.02
FUEL
1ASS
LBS.
268.03
116.43
303.67
253.15
98.75
10*0.02
LB CO /
IK LB FUEL
83.3*9
0.410
1.077
8.993
83.3*9
LB HC /
IK IB FUEL
103.921
0.111
0.167
3.785
103.921
LB NOX/
IK LB FUEL
2.016
14.130
12.12*
7.299
2.016
ENERGY
1 TH-MR
269.17
198.33
529.83
451.33
99.17
15*9.83
ENERGY
TH-HR
269.17
198.33
529.83
453.33
99.17
15*9.83
ENERGY
1 TH-HR
269.17
198.33
529.83
*53.33
99.17
15*9.83
LB CO /
1 TH-HR
0.08300
0.0002*
0.00062
0.00502
0.08300
18 HC /
< TH-HR
0.103*6
0.00007
0.00011
0.00211
0.103*8
LB NOX/
< TH-HR
0.00201
0.00829
0.00695
0.00*08
0.00201
IV-97
-------
DATE: 7/19/71
Test ORGANIZATION: s w R I THA
ENGINE SUPPLIER: rut
ENGINE DIM
C»l 10 NUMBER:
ENGINE TYPE AND MODEL: JI3D -38
SERIAL NUMBER: im»230«i
RATED THRUST: isooo.
ENGINE TOTAL TIME: 15372. HRS
TIME SINCF HOT SECTION OVERHAUL: 74. HPS
TIME SINCF:
NI COMPRESSOR OVERHAUL: 15372. HRS
N2 COMPRESSOR OVERHAUL: 15372. HRS
COMBUSTOR CAN REPLACEMENT: 74. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 15372. HRS
NI TURBINE OVERHAUL: 15372. HRS
N2 TURBINF OVERHAUL: 15372. HRS
FUFL: jp-4 TF FUEL H/C RATIO: 2.020
OPERATIONAL DATA ««««.»«»«.........................«.....«...
INLET AIR TFMPERATURE, DEGREES F: START 63.00 FINISH
ATMOSPHERIC PRESSURE: START 28.42 FINISH
INLET AIR HUMIDITY, LBS H21/LB AIR: 0.0107
RELATIVE HUMIDITY: 75.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 150.00, FLOW RATE, LITEHS/MIN:
SAMPLE LINE rp.ANSPPRl TIME, SEC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
F/A AND AIRFLOW CALCULATED FPflM FXHAUST COMPOSITION FOR FOURTH RUN. N02
DETERMINED BY SUBTRACTION.
M..OO
28.95
ELAPSED
TIME
0.0
io.no
25.00
31.00
40.00
TEST
MODE
I/ 0
2/ I
3/ 2
4/ 3
5/ 4
POWFR
THRUST, LBS PERCENT
OK HATED
SHP
1 1060.00
13200.00
15400.00
1(160.00
1S400.00
r.n.
M
73
85
5
15
ENGINE
SPEED
RPM
NI
5785.00
61BO.OO
6510. CO
1710.00
1510. CO
N2
"220.00
7660.00
9B50.00
6220.00
<)fl20.on
MEASURED
FUEL
FLOW
LB/HR
6170.00
7510.00
4190.00
1070.00
9230.00
GAS GEN
MR FLOW
LH/SFC
139.80
154.20
171.50
3B.60
171.50
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.012300
0.013700
0.014900
0.007700
0.015000
DEGREES F
-0.00
-o.no
-0.00
-n.oo
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.50
1.65
1.82
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
PHUER
PERCENT
RATED
T.n.
61
73
85
5
*5
EXHAUST
GAS
TEMP
OEGPFFS F
TM . 00
825.00
914.00
504.00
917.00
EXHAUST
GAS
PRESSURE
PSIA
6.40
P.50
10.SO
0.30
10.60
cn
IriFTI
PPMV .
76.00
20.00
14.00
650.00
1 1 .00
CO
2
IhFU
PFRCENT V
1 .60
2.04
2.51
1.39
7.44
THC
IWETI
PPMV
52.00
65.00
68.00
1060.00
70.00
NO NO
(MET) 2
PPMV (KETI
PPMV
ALDEHYDES SMOKE PARTICULARS
?7.00
44.00
71.00
0.0
70.00
5.00
6.00
4.00
7.00
5.00
(MET!
PPMV
3?.00
50.00
75.00
7.00
75.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
POUFP
PERCENT
R AICIJ
1.0.
61
71
H5
5
85
MAS", EMI
cn
I. B / 1K
L» FUEI
3.22
1.95
1. II
34.01
0. 00
'1SS FMI
Mr.
LB/IK
LB FUEL
1.69
1.62
3. OH
77.51
1.27
MASS 11\
N32
LH/ IK
LB FUEL
1.02
0.96
0.52
1.47
0.67
MASS FMI
CM?
LB/IK
LF1 FUFL
31 18.04
3120.24
3123.04
2788.56
3122.67
IASS fMI
Nil
LP/1K
LR FUEL
5.50
7.04
9.24
0.0
9.37
MASS CM!
NOX
LB/1K
LR FUEL
6.52
7.99
9.76
1.47
10.01
MASS Ell
C"
LB/HR
19.90
14.78
10. 19
39.90
fl.27
MASS EM|
HC
LB/HR
22.79
27.51
78.34
92.94
30. 14
MASS EMI
NO 2
LP/HR
6. 28
7.28
4.76
1.57
6. 17
MASS FMI
CO 2
LB/HR
19238.31
23682.63
26700.71
29B3.7B
28824.11
MASS EMI
NO
LB/HR
33.94
53.40
64.87
0.0
86.45
MASS [Ml
NO*
IB/HR
40.22
60.68
89.65
1.57
92.62
POWER
PERCENT
RATED
T.O.
61
73
B5
5
65
Cil
LO/IK* TH-HB
1 .799
1.119
0.662
S4. *07
0.517
L B/IKKTM-HH
17 19.449
1794.119
1363.682
2814.8119
1R71.696
2.061
2.064
1.B40
J8.246
1 .957
M)
LR/IKHTH-HR
.1.061
4.045
5.51!
0.0
5.613
LH/1KHTH-HR
0.56B
0.552
0.310
1.482
0.401
Nil
X
LB/ IMTH-HR
3.61?
4.597
5.872
1.482
6.014
IV-98
-------
CAL 10 NUMBER: 116 ENGINE TYPE AND MODEL: JT3D -3B
TEST ORGANIZATION: s u R I THA
SERIAL NUMBER! (TUA2304)
MODE
TAXI-IOLE
TAKEOFF
CLINSOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POKER
0.050
1.000
o.eso
0.400
0.050
POWER
f TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION
RATE
LB/HR
292.230
0.0
6.702
17.412
292.230
FUEL
RATE
LB/HR
991.11!
11218.996
9176.982
4395.953
991. US
USAGE
NT FACTOR
1.000
1.000
1.000
1.000
1.000
TIME IN
NODE
MIN.
19.00
0.70
2.20
4.00
7.00
CO
MASS
LBS.
92.539
0.0
0.2*6
1.161
34.093
FUEL
MASS
LBS.
313.85
130.89
336.47
293.06
115.63
L8 CO /
IK LB FUEL
29*. 850
0.0
0.730
3.961
294.850
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
LB CO /
1 TH-HR
0.32470
0.0
0.00044
0.00242
0.32470
TOTAL FDR CYCLE: 128.039
LBS POLLUTANT/IK LB FUEL/CYCLEl 107.604
LBS POLLUTANT/IK LB TH-HR/CVCLE: 78.025
LBS POLLUTANT/1000K LB TH AT T.O.: 0.0
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POKER
f TH
900.
18000.
15300.
7200.
900.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
214.801 991.115
27.784 11218.996
27.207 9176.582
19.179 4395.953
214. B01 491.115
KT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
TH
900.
18000.
15300.
7200.
900.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/KR
1.133 991.115
146.115 11218.996
89.862 9176.582
19.761 4395.953
1.133 991.115
WT
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE!
LB TH AT T.O.I
USAGE TINE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLEl
LB TH AT T.O.I
HC
MASS
LBS.
68.020
0.324
0.998
1.279
25.060
95.681
80.410
58.306
18.008
NOX
MASS
LBS.
0.359
.705
.295
.317
.132
.808
.722
4.149
94.704
FUEL
MASS
LBS.
313.85
130.89
336.47
293.06
115.63
1189.91
FUEL
MASS
LBS.
313.85
130.89
336.47
293.06
115.63
1189.91
LB HC /
IK LB FUEL
216.726
2.477
2.965
4.363
216.726
LB NOX/
IK LB FUEL
1.144
13.024
9.793
4.495
1.144
ENERGY
TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
i TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
LB HC /
1 TH-HR
0.23867
0.00154
0.00178
0.00266
0.23867
LB NOX/
1 TH-HR
0.00126
0.00812
0.00587
0.00274
0.00126
IV-99
-------
DATE: 7/19/71
TEST PRGANUITIUN: s f R i THA
ENGINE SUPPLIED: T U A
ENGINE 0414
f.AL ID NUM5F«: H7 FNGl\e IVPF AN'O MODEL:
P.ATF.n THRUST: 1
ENGINE TOTAL TIMF:
TIME SINCF H'H SFCT1CN OVERHAUL:
TIMF SINCF:
94;,:!. HPS
9463. HPS
SERIAL NU**RFP:
Nl COMPWFSS'IR OVERHAUL: 9463. HPS
N'2 r.CMPF?.SS(IP OVERHAUL: 9463. HPS
C(VM1USM< CAN REPLACEMENT: 9463. HP";
FIRSI srnr.p ri'i/uE GtiinF VANF CVF.WHAUL: 9463. HPS
Nl TURHINE OVERHAUL: 4463. HRS
N2 TURfHNF IVFRHAlll : 9461. HHS
FUEL H/C PAIin: 7.020
FUEL: .l"-4 IF
OPFR ATI ONAL DA TA **«*»# *
INLEI All" rF"PFHMU<-Ei OLGRETS F:
6T 75.00 FINISH 7">.00
AlMOSPHEmC PRtSSURI;: SI4RI 2fl.>)7 FINISH ?H.")6
INLFT M« Himl'irrv, LrtS H2?/L3 A|P.: C.Oini
"FIATIVK MU«iniIY: 4ft. DC PEPT.FNr
SAKPLF LINF: IP'PfOAtllPF, DECSCFS r. : 150. OC, FLO. RATE, LIIEP.S/MIN:
SAMPlF LINE MnNSP!i"T Tl.^f, SEC: I.OC
NUM1F9 Of 1FSIS: h
mMMFNI S:
F/A ANT AIRFLIIJ CALC'JlAtFn FBHM F.oo
7.0.1
3.00
n.oo
0.00
Nfi
IfcFl 1
PPMV
22.""
1. T~
SP.OO
91.00
1 .0"
75.00
Mil
2
ItFTI
PPMV
- . Or)
3.00
3.0"
4.00
(,.00
1.01
ALOFHYOES SMQKfc PARTICULARS
I«FT I
PPMv
4U.IH,
(: 1 . c)G
97.00
7 .00
78. OH
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0. 00
-0.00
-0.00
-o.oc
PHUFK
PERCEMT
PATFO
T .0.
50
62
71
H6
IASS F.«l
rn
LK/1K
LI Fl| = l
3.01
4. 12
1 .2'.
0.77
I'/, . ('
1 .0"!
IASS FM|
HC
1 "/IK
LH FUEL
5.(>3
4 . fl 5
4.21
4.IU
'.9.10
3.6 1
MASS IVI
N 12
LI/IK
Lrt FUF.L
5.10
1 . 5S
0.47
1.51
1 .24
).3f
MASS F*l
012
I.R/IK
11 TLIIL
11 11.00
-1111.
11 19.
1120.
2724.
1121 .
R
4
r
?
7
»»SS
N
L ''
Lll
4
n
0
1 1
r
;
t»l
/ IK
rilFL
.94
. 6S
.09
. In
.21
. 75
MASS [Ml
Miy
LO/1K
L1 FHF|.
5.H',
7. 3l
9.56
I2.27
I .44
I 0 . I 4
H.'.SS FMI
cn
9.64
7.2"
HI MASS EMI
W'2
» LS/h»
2 B . '11
10.77
32.71
)H. 34
97.31
10. Ti
4.M
3.48
1.65
4.73
1.21
3.32
SS FMI
C12
LH/HO
I 5970.:) I
19770.57
24241.39
29179.32
2569.73
26534.21
MASS EMI
NO
LB/HK
25.31
4. 10
7C.66
109.96
0.20
H2. 14
2S.94
46. 45
74.32
114.69
1.42
86.21
PUMEP
PERCENT
RATED
T.D.
50
62
I .591
2. 135
0.724
0 . 4 64
11 .122
0.619
I P / 1 K H T It-He.
1 7', 1 .<-.'; 7
1755.2
-------
CAL ID NUMBER: 117 ENGINE TYPE AND MODEL: JTJD -JB
TEST ORGANIZATION: S W R 1 TWA
SERIAL NUMBER: iTwA3io2>
MODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IOLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IOLE
0.050
1.000
0.850
0.400
0.050
FRACTIONAL
POKER
0.050
1.000
0.850
0.400
0.050
FRACTIONAL
POMER
0.050
1.000
0.850
0.400
0.050
POMER
t TH
900.0
16000.0
15300.0
7200.0
900.0
POKER
1 TH
900.0
18000.0
15300.0
7200.0
900.0
POWER
TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL USAGE TINE IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR NIN.
113.893 878.435
3.828 11033.723
2.428 9180.453
10.974 4160.602
113.893 678.435
TOTAL FOR CVCLE:
LBS POLLUTANT/IK LB
IBS POLLUTANT/ IK LB
LBS POLLUTANT/ 1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
98.843 878.435
36.046 11033.723
34.569 9180.453
24.183 4160.602
98.843 878.435
TOTAL FOR CVCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
1.299 876.435
174.746 11033.723
108.525 9180.453
19.580 4160.602
1.299 878.435
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
36.066
0.045
0.089
0.732
13.287
50.219
44.704
30.603
0.248
HC
MASS
LBS.
31.300
0.421
1.268
1.612
11.532
46.132
41.066
28.112
23.363
NOX
MASS
LBS.
0.411
2.039
3.979
1.305
0.152
7.886
7.020
4.806
113.261
FUEL
MASS
LBS.
278.17
128.73
336.62
277.37
102.48
1123.37
FUEL
MASS
LBS.
278.17
128.73
336.62
277.17
102.48
1123.37
FUEL
MASS
LBS.
278.17
128.73
336.62
277.37
102.48
1123.37
LB CO /
IK LB FUEL
129
0
0
2
129
.654
.347
.264
.638
.654
LB HC /
IK LB FUEL
112
3
3
5
112
.521
.267
.765
.812
.521
LB NOX/
IK LB FUEL
1
15
11
4
1
.476
.837
.821
.706
.478
ENERGY
TH-HR
265.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
LB
0
0
0
0
0
LB
1
0
0
0
0
0
LB
1
0
0
0
0
0
CO /
TH-HR
.12655
.00021
.00016
.00152
.12655
HC /
TH-HR
.10983
.00200
.00226
.00136
.10983
NOX/
TH-HR
.00144
.00971
.00709
.00272
.00144
IV-101
-------
DATE: II 1/71
TEST QRGANIZAT ION: 'JNI ItO/EPA
FNG1NF SUPPLIER: IINITFO AIRLINES
ENGINF DATA »
CAL 10 MIIMBFO: 1?4 ENGINE TYPE ANO MOOH : JT1D -3B
SERIAL NUMBER:
RATFC THRUST: laoon.
ENGINF TOTAL TIMF: 12462. MRS
TIME SINCE HUT SFOini ovf«2. HOS
UHE SINCE:
NI COMPRESSOR OVERHAUL: 12462. HRS
NZ CCMPRF.SSOP OVERHAUL: i<-57<>. HRS
COMBUST!)* CAN REPLACEMENT: 3991. MRS
FIRST STAGE NOZZLE T.IIIOE VANE OVERHAUL: 5993. HRS
Nl IUWVE OVERHAUL: *6fl2. HRS
N2 TURBINE OVERHAUL: 3993. MRS
FUEL: JFI - A
FUEL H/C RATIO: 1.920
1PFR
1NLFI SIP tE'">C»AIUBFi HEGDteS F: START iS.",n FINISH 55.41
ATPOSPHFPIC PRESSURF: START 21.S8 FINISH 2)6
INLFT AIR HUKIOITV, LHS H21/LB AIR: 0.0065
RFLATIVF HIJHiaiTY: 6"».CO PERCENT
S4rPLE LINE: TFMPfdATURF, (IF.f.REES f.: 160.OC. FLOM RiTEi LITtPS/«IN:
SAHPLF LINE TRANSPORT TIME, SEC: 5.CO
NUMBER OF TFSTS: <,
COMMENTS:
FXMAUST GAS PPF.SSU1F IN INCHFS HG.
PRE-°EPAIU RUN
CLOCK
I IMF
120.00
110.00
135.00
145.00
PIWER
PERCENT
RATED
T . 0 ,
51
71
9 1
6
»OWE»
PERCENT
R ATEO
T.U.
51
'3
9 1
6
POWER
PERCENT
RATED
T.O.
51
j-\
1 1
6
TFST
MODE
I/ 0
21 1
I/ 2
4/ 1
FXHAUST
r,AS
TEMP
1LGOEES r
VIH.OO
HOO. 60
012.20
516.00
(ASS rM[
CO
LP./IK
LB PUEL
t. n
4.91
2. II
100.51
en
4.
? .
1.
-0.
POWER
THRUST, LBS
OR
ShP
0100.00
11200.00
16500.00
1125.00
EXHAUST
GAS
PRESSURE
PSI A
40. MO
47.20
54. 30
31 . 10
-------
CAL ID NUMBER; 124 ENGINE TYPE AND MODEL: JTSD -IB
TEST ORGANIZATION: UNITED/EPA
SERIAL NUMBERl 6*57)5
MODE FRACTIONAL
POWER
TAXI-IOLE
TAKEOFF
CLIN80UT
APPROACH
TAX-IDLE
0.050
1.000
O.S50
0.400
0.050
POKER
1 TH
900.0
IBOOO.O
15300.0
7200.0
900.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
161.292 . 714.560
18.161 10271.152
30.252 853 fl. 969
49.445 3992.905
161.292 714.560
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
IBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKF.OFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
1 TH
900.0
IBOOO.O
15300.0
7200.0
900.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
165.350 714.560
0.0 10271. 152
2.242 8538.969
5.495 3992.905
165.350 714.560
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
HODE
TAXI-IDLE
TAKEOFF
CLIMBOUI
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.221 714.560
123.605 10271.152
85.236 8518.969
21.435 J992.905
1.221 714.560
WT
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
CO
MASS
LBS.
51.076
0.212
1.109
3.296
18.817
74.511
73.863
45.406
1.177
HC
MASS
LBS.
52.361
0.0
0.082
0.366
19.291
72.100
71.474
43.937
0.0
NOX
MASS
LBS.
0.387
1.442
3.125
1.429
0.142
6.526
6.469
3.977
80.114
FUEL
MASS
LBS.
226.28
119.83
313.10
266.19
83.37
1006.76
FUEL
MASS
LBS.
226.28
119.83
313.10
266.19
83.37
1008.76
FUEL
HASS
LBS.
226.28
119.83
313.10
266.19
81.37
1008.76
LB CO /
IK LB FUEL
225.
1.
3.
12.
225.
722
768
543
383
722
LB HC /
IK LB FUEL
231.
0.
0.
1.
231.
401
0
263
376
401
LB NOX/
IK LB FUEL
1.
12.
9.
5.
1.
709
034
982
368
709
ENERGY
f TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
LB CO /
I TH-HR
0.17921
0.00101
0.00198
0.00687
0.17921
LB MC /
1 TH-HR
0.18372
0.0
0.00015
0.00076
0.18372
LB NOX/
1 TH-HR
0.00136
0.00687
0.00557
0.00298
0.00136
IV-103
-------
OATF: 7/ I/7I
TEST URGANUATIQN: JNITFn/EPA
INGlNf SUPPLIER: UNIIFO AIRLINES
ENGINE DATA
CAL 10 NUM1E": 125
ENGINE TYPE AND MI10FL: JT31 -3R
SERIAL NUMBER:
RATED THPUST: 11000.
ENGINE TOTAL TIME: 12024. HRS
TI"E SINCE Mill SECTION OVERHAUL: 7510. HRS
TIHE SINCE:
Nl COMPRESSOR OVERHAUL: 15996. HRS
N2 COMPRESSOR OVERHAUL: 13660. HRS
COMRUSTO" CAN REPLACEMENT: 0. HRS
FlrtST STAGE NOZZLE GUIDE VANE DVIRHAUL: 3132. HRS
Nl TU1«!NF OVERHAUL: 7510. HPS
N2 TURBINE OVERHAUL: 0. HRS
FUEL: JFT - A FUEL H/C RATIO: i.92n
DPERATTONAL DATA ****»»*******»»**»**««**»****»*»»
INLFT AIR TEMPERATURE, DEGREES f: STAKT 62.60 FINISH 61.52
ATMOSPHERIC PRESSURf-: START 29.93 FINISH 30.30
INLFT AIR HUMIDITY, LBS H20/LB AIR: 0.0085
RELATIVE HUMIDITY: 69.nO PFRCFNT
SAMPLE LINE: TEMPERATURE, DEGREES C: 160.00, FLOW RATE, LITFRS/«IN:
SAMPLF LINE TRANSPORT TIME, SEC: 5.00
NUMBER OF TESTS: 4
COMMENTS:
EXHAUST GAS PRESVJ1F IN INCHES HG.
CLOCK
TIME
1611.00
1616.00
1622.00
1702.00
POWER
PFRCENT
BATED
T .O.
52
74
91
5
POWER
PFRCFNT
RATFO
T.n.
52
74
S
POWFP
PERCENT
RATED
T.O.
52
74
91
5
TFST
MCDF
I/ 0
2/ 1
M 2
4/ 3
EXHAUST
GAS
TFMP
OFGRFFS r
707. CO
B 1 1 . 40
971 .21
525.20
MASS EMI
ro
LH FUEL
0.68
3.44
102. (5
POWER ENGINE MEASURED GAS GEN CALC COMPRESSOR ENGINE TUROINE
THPUST. I.RS PFRCENT SPEED FUEL AIR FLOW F/A DISCHARGE PRESSURE INLET
OR RATER RPV FLOW LP-/SEC TEMP RATIO TF»P
SHP T.O. M N2 LO/HB DEGREES F FPR DEGREES F
1J69. 01)
1 33P9.00
16492.00
9B5.00
EXHAUST
GAS
PRESSURE
PSIA
40.90
47.70
54.20
30.80
MASS tMI p
HC
LB/I K
LB FUEL
C.27
0.02
0.12
12". 75
52 5230.00 9001.00 5O36.00 -0.00 -0.000000 -0.00 1.3B -0.00
74 5924.00 9464.00 7281.00 -0.00 -0.000000 -0.00 1.61 -0.00
91 6443.00 9B41.00 9425.00 -0.00 -0.000000 -0.00 1.83 -0.00
5 2023.00 5P12.00 1187.00 -0.00 -0.000000 -0.00 0.0 -0.00
CO CO THC NO NO NO ALDEHYDES SMOKF » AR T ICIRATES
(WETI 2 IWETI (MET! 2 X
PP"V IWFTI PPMV PPMV (WET) IWETI
PERCENT V PPMV PPMV
H.50 2.50 5.85 40.00 -0.00 47.00 -0.00 -0.00 -0.00
45.00 2.62 0.45 71.00 -1.00 72.00 -0.00 -0.00 -0.00
30.00 3. .10 0.42 104.00 -0.00 104.00 -0.00 -0.00 -0.00
H40.01 1.18 1145.00 9.50 -0.00 10.50 -0.00 -O.DO -0.00
MSS EMI MASS E*l "ASS hMI MASS EMI MASS EMI MASS E*l MASS EMI MASS EMI MASS F*M MASS fc " I
102 CC:2 NO NUX CO HC N(17 CO? NT" NOX
LH/IK LB/1K LB/1K LB/IK L8/HR LB/HR LB/HR L8/HR LB/HR LB/t-R
LI) FUEL IB FUEL LP FUEL LF1 FUEL
-1.01 3154.06 5.23 6,?0 3.44 1.35 -0.00 158B).')3 26.57 ') 1 . 2 7
-0.00 3150.42 6.93 9.05 75.07 0.14 -O.PO 2293B.2J 64.98 65.90
-1.00 3152.69 11.4} 11.43 18.91 0.15 -C.OO 29714.11 107.69 107.69
-'1.0(1 2641.87 1.90 2.10 121.49 152.82 -0.00 3135.90 2.26 2.49
CD CO THC Nl! NH N!l
2 2 X
m/UKTH-HH LB/K«TH-H9 L B/ 1 KdTH-m I.9/1KHTH-HR LF)/ 1K» TH-HP L1/1KKTH-HR
1.
1 .
171
147
136
1695.371 0.145 2.836 -C.OOO 1.332
1713.215 0.011 4.B5.I -0.000 4.97Z
1801.730 1.009 6.531 -0.000 (-.530
3133.657 155.150 2.291 -C.lon 2.537
IV-104
-------
CAL ID NUMBER I 12$ ENGINE TYPE AND NODE11 JT3D -3B
TEST ORGANUATION: UNITEO/EPA
SERIAL NUNBERI 644691
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.050
1.000
0.850
0.400
0.050
POKER
f TH
900.0
16000.0
15300.0
T200.0
900.0
EMISSION
RATE
LB/KR
129. 77T
T.I 40
21.2T1
3.985
129. TTT
FUEL
RATE UT
LB/HR
663. 3TT
10008.262
8568.125
38T0.219
663. 3TT
TOTAL FOR CYCLE:
IBS POLLUTANT/IK IB
LBS POLLUTANT/IK LB
IBS POLLUTANT/ 1000K
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
1 TH
900.0
18000.0
15300.0
T200.0
900.0
EMISSION
RATE
LB/HR
230.501
0.0
0.0
0.0
230.501
FUEL
RATE UT
LB/HR
663. 3TT
10008.262
8568.125
3BT0.219
663. 3TT
USAGE
FACTOR
.000
.000
.000
.000
.000
TINE IN
NODE
NIN.
19.00
O.TO
2.20
4.00
T.OO
FUEL/CYCLE i
TH-HR/CYCLE:
LB TH AT T.O.I
USAGE
FACTOR
1.000
1.000
1.000
1.000
1.000
TINE IN
NODE
HIN.
19.00
O.TO
2.20
4.00
T.OO
CO
NASS
LBS.
41.096
0.083
0.790
0.266
15.141
ST. 366
58.752
34.958
0.463
HC
NASS
LBS.
72.992
0.0
0.0
0.0
26.892
FUEL
NASS
LBS.
210.07
116.76
314.16
258.01
77.39
976.41
FUEL
NASS
LBS.
210.07
116.76
314.16
258.01
77.39
LB CO /
IK LB FUEL
195.631
0.713
2.483
1.030
195.631
LB HC /
IK LB FUEL
347. 46T
0.0
0.0
0.0
347.467
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
f TH-HR
285.00
210.00
561.00
480.00
105.00
LB CO /
1 TH-HR
0.14420
0.00040
0.00139
0.00055
0.14420
LB HC /
1 TH-HR
0.25611
0.0
0.0
0.0
0.25611
TOTAL FOR CYCLE' 99.884
LBS POLLUTANT/IK LB FUEL/CYCLE: 102.298
LBS POLLUTANT/IK LB TH-HR/CYCLE: 60.868
LBS POLLUTANT/1000K LB TH AT T.O.I 0.0
976.41
1641.00
NODE FRACTIONAL
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
POWER
0.050
1.000
0.850
0.400
0.050
POWER
t TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL
RATE
LB/HR
1.128
124.387
89.156
18.789
1.128
RATE
LB/HR
663.377
10008.262
8568.125
3870.219
663.377
USAGE TINE IN
WT
FACTOR NODE
HIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
TOTAL FOR CYCLE:
LBS
LBS
LBS
POLLUTANT/IK
POLLUTANT/IK
LB
LB
POLLUTANT/1000K
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
NOX
NASS
LBS.
0.357
1.451
3.269
1.253
0.132
6.462
6.618
3.938
80.621
FUEL
NASS
LBS.
210.07
116.76
314.16
258.01
77.39
976.41
LB NOX/
IK LB FUEL
1.700
12.428
10.406
4.855
1.700
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
LB NOX/
TH-HR
0.00125
0.00691
0.00583
0.00261
0.00125
IV-105
-------
OATC: 7/ 6/71
TFST ORGANIZATION: UNITFD/EPA
ENGINE SUPPLIES: UNITED AIRLINES
ENGINE DATA «««««««««««»««.«««««»»
CAL 10 NUMBFH: 128 ENGINE TYPE UNO MOOEL : J110 -3B
SERIAL NUMBFR:
RATED THPUST: 1ROOO.
ENGINE TOTAL TIMF: 8308. MRS
TIME SINCE HOT SECTION OVERHAUL: 810B. MRS
TIKE SINCE:
NI COMPRESSOR OVERHAUL: BSOB. MRS
N2 COMPRESSOR OVERHAUL: 1*3*7. HHS
COHBUSTUR CAN REPLACEMENT: 8308. HRS
FIRST STAGE NOZZLE CUIOE VANE OVERHAUL: B30B. HHS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 8308. HRS
FUFL: JET - A FUEL H/C RATIO: 1.920
OPERATIONAL OATA «»»«»»«»«»»«»«
INLET AIR TEMPERATURE, DEGREES F: START 64.40 FINISH
ATMOSPHERIC PRESSURF: START 2").82 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0085
RELATIVE HUMIDITY: 65.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 160.00, FLOW KATE, LITFRS/H1N:
SAMPLE LINF TRANSPORT TIMF, SEC: 5.00
NUMBER CF TFSTS: 4
COMMENTS:
EXHAUST GAS PRESSURE IN INCHFS Hf,.
66.20
79.B9
CLOCK
TIME
1040.00
1050.00
1055.00
1225.00
POWFK
PERCENT
RATED
T.O.
51
72
90
5
POWFP
PERCFNT
RATED
T.O.
51
72
90
5
POWER
PERCENT
RATED
T.O.
51
72
10
5
TEST
MODF
I/ 0
2/ 1
V 7
4/ 3
EXHAUST
GAS
TEMP
PEGRCFS ^
705.20
8C6.00
111.40
516.00
"ASS EMI
CO
I.R/IK
LR FUFL
10.08
4.41
7.44
66.60
Cf
POWER
THRUST, L9S
OR
SHP
1775.00
1 31 00.00
16350.00
1050.00
FXHAUST
r,AS
PRFSSURF
PSI A
40.80
47.10
51. 70
10.10
MSS EMI
HC
LB/U
L6 FUEL
0.47
0.07
0.05
145.07
PFRCFNT
HATED
ENG INF
SPEED
T.O. NI
51 5113
77 58H
90 (-4C9
5 7010
CO
1 WFT 1
PPMV
.00
.00
.00
.00
RPM
N7
1P62.00
1535.00
9933.00
5716.00
CO
MEASURED
FUFL
FLOW
LR/HR
1436.00
7091.00
9283.00
1192.00
T HC NO
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
NO
2 IHFM IWET) 2
IhET)
PPMV PPMV IKETI
PERCENT V
110.00
55.00
35.00
560.00
MASS EMI MASS
2.18
2. 50
2.BP
9.00 33.
1.50 54.
1.70 BO.
I. 42 2130.00 4.
C"l
N.J2 C02
LB/1K LB/1K
L° FUEL L9 FUFL
-'J.OO 1138.
-1.00 3I48.
-1.00 H5I.
-0.00 2651.
cn
7
LH/lKffTH-HF LR/1K1TH-HR
10.
2.
1 .
75.
255
1R7
IB4
601
3113.240
1704.423
1711.563
3012.187
76
77
91
26
"ASS [Ml
NO
LP./1K
LH FUEL
4.9/
7.11
1.15
0. 74
THf
L <,/ IK KTH-HR
0.4B1
0.037
0.027
Io4.610
MASS EMI
NOX
Lfl/lK
LB FUEL
5.87
7.64
1.61
C.78
PPMV
00 -0.00
00 -0.00
00 -0.00
00 -0.00
CALC
F/A
-0.000000
-o.oooooo
-o.nooooo
-0.000000
NO
X
IWETI
PPMV
39.00
50.00
84.00
4.00
COMPRFSSCR ENGINE
DISCHARGE PRESSURE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
PATIC
EPR
I. 38
1.60
1.83
-0.00
TURBINE
INLET
TEMP
DFGRFFS f
-0.00
-0.00
-0.00
-0.00
ALDEHYDES SMOKE PAOTICULATES
-0.00 -0
-0.00 -0
-0.00 -0
-0.00 -0
"ASS F"I MASS EMI MASS FMI MASS EMI
CO
LB/HR
15.11
31.76
77.63
71. 3R
NO
LH/ 1K«T
5.
3.
>.
0.
HC
L8/HP
4.46
0.49
0.44
17?. 92
ND
7
H-HH L1VIKMH-HR
053
B49
197
8P7
-0.000
-0.000
-0.000
-0.000
N02 CH2
LB/HR L9/HR
-0.00 29617.30
-0.00 22327.14
-0.00 29759.34
-0.00 3162.69
NO
X
LB/1KHTH-HR
5.177
4.134
5.457
0.887
.00
.00
.00
.00
MASS EMI
NO
LE/HR
46.87
50.42
B4.97
0.13
-0.00
-0.00
-0.00
-0.00
MASS EMI
NTt
LB/HR
55.31
54.15
81.21
0.91
IV-106
-------
C»L ID NUMBER: 128 ENGINE TYPE AND MODELS JT30 -IB
TEST ORGANIZATION: UNITED/EPA
SERIAL NUMBER: 669507
MODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIM80UT
APPROACH
TAKI-IOLE
0.050
1.000
0.850
0.400
0.050
POWER
t TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
159.059 1000.640
21.524 9855.155
25.454 8722.555
S3. 969 4295.113
159.059 1000.640
USAGE TINE IN
WT FACTOR MODE
NIN.
TOTAL FOR CYCLE:
IBS POLLUTANT/IK LB
IBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.050
I. 000
0.850
0.400
0.050
POWER
TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL
RATE RATE
IB/HB LB/HR
220.641 1000.640
0.0 9855.355
0.0 8722.555
7.604 4295.113
220.641 1000.640
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-MR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
HOOF
TAXI-IDLE
TAKEOFF
CLIM80UT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.050
0.400
0.050
POWER
1 TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL
RATE RATE
LB/HR L8/HR
0.629 1000.640
104.940 9855.355
76.43B 8722.555
20.175 4295.113
0.629 100C.640
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
50.369
0.251
0.933
3.598
18.557
73.708
63.830
44.917
1.395
HC
MASS
LBS.
69.870
0.0
0.0
0.507
25.741
96.118
83.237
58.573
0.0
KOX
MASS
LBS.
0.199
1.224
2.803
1.345
0.073
5.645
4.888
3.440
68.016
FUEL
MASS
LBS.
316.87
114.98
319.83
286.34
116.74
1154.76
FUEL
MASS
LBS.
316.87
114.98
319.83
286.34
116.74
1154.76
FUEL
MASS
LBS.
316.87
114.98
319.83
286.34
116.74
1154.76
LB CO /
IK LB FUEL
158.958
2.1B4
2.918
12.565
158.958
LB HC /
IK LB FUEL
220.500
0.0
0.0
1.770
220.500
LB NOX/
IK LB FUEL
0.629
10.648
8.763
4.697
0.629
ENERGY
f TM-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
LB
CO /
TH-HR
0.17673
0.00120
0.00166
0.00750
0.17673
IB
0
0
0
0
0
LB
fl
0
0
0
0
0
HC /
TH-HR
.24516
.0
.0
.00106
.24516
NOX/
TH-HR
.00070
.00583
.00500
.00280
.00070
IV-107
-------
DATE: 0/7C/71
TEST ORGANIZATION: UNIIED/FPA
ENGINC SUPPLIER: UNITED AIRLINES
ENGINE DA!4 ««»««» ...............................
CAL ID NUM1FP: 130 ENGINE TYPF AND MODFL: JT30 -3B
SERIAL NUMBER:
RATED THRUST: 18000.
ENGINE TOTAL TIME: 12660. MRS
TIME SINCE HOT SECTION OVERHAUl: -0. MRS
TIMF SINT.F:
NI COMPRESSOR OVERHAUL; -n. HRS
N2 COMPRESSOR OVERHAUL: -o. HRS
COMBUSTOR C»N REPLACEMEMT: -o. HRS
FIRST STAGE NOZZLE GUIDE VANF OVERHAUL: -0. HRS
NI TUIBINE OVERHAUL: -o. HRS
nz TURBINE OVERHAUL: -o. HRS
FUFL: JET - A FUEL H/C RATIO: 1.170
OPERATIONAL DATA «»»«««»»««««.....t».................
INLET AIR TEMPERATURE, DEGREES F: SIART 64.90 FINISH
ATMOSPHERIC PRFSSURF: STAKT 29.92 FINISH
INLET AIR HUMIDITY, LAS H20/LB AIR: 0.0068
RELATIVE HUMIDITY: 60.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 1600.00, FLOW RATE, LITFPS/HIN:
SA-PLE LINF TRANSPORT TIME, SFC: 5.00
NUMBER OF TESTS: <
COMMENTS:
EXHAUST GAS PRESSURE IS IN INCHES HG. WITH r.l-2 FUFL ADDITIVE
59.7C
10.00
CLOCK
TIME
1 702.00
1715.00
1719.00
1847.00
POWER
PERCENT
RATED
T.ll.
49
71
90
POUER
PERCENT
H ATEO
T.O.
49
73
90
6
POWEP
PERCENT
RATED
T.O.
49
73
90
ft
TEST
I/ 0
?/ 1
3/ ?
EXHAUST
GAS
TEMP
DEGREES r
375.00
435.00
490.00
3?.0. 10
MASS CMI
CI1
LP/1K
Lfl FJFL
19. 15
6.54
3. \?
90.31
CM
LH/IK"
10.
3.
1.
1 17.
POWER ENGINE MEASURED GAS GFN
IHRUST.L8S PERCFNT SPEED FUFL AIR FLOW
OR RATm RPM FLOW LI/SEC
SHP T.O. M N2 LI"/H»
898?. 00
13202.00
16361.00
1085.00
F XHAUST
GAS
PRESSURE
PSI A
40.50
47.50
54.10
30.90
M.\SS EMI
HC
LH/l K
L». FJtL
0.64
0.66
0.18
t>9. 74
rn-HP L
666
931
93?
49 5153.00
73 5901. On
90 6422.00
6 2093.00
8820.00
9315.00
9665.00
5803.00
CO CO THC
(HE!! 2 Ik'ETI
PPMV luETI PPHV
PERCENT V
210.00
85.00
50.00
S95.00
MiSS FMI MASS I'M!
NO 2 CO?
Ltt/IK LI/IK
L1! FUEL LB FUtL
-0.00 3124.03
-0.00 3143.10
-0.00 3150.17
-0.00 2R21.K9
2.18 12.30
2.60 15.00
3.02 4.PO
1.77 1200.00
5002.00 -0.00
7387.00 -0.00
9518.00 -0.00
1409.00 -0.00
NO NO
IWETI 2
PPMV (WE II
PPMV
34.00 -0.00
64.00 -0.00
9R.OO -0.00
10.00 -0.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
NO
X
IkETI
PPMV
37.00
66.00
100.00
17.00
COMPRESSOR ENGINF
DISCHARGE PRESSURE
TEMP RATIO
DEGREES F EPR
-0.00 1.36
-0.00 1.61
-0.00 1.83
-0.00 -0.00
ALDEHYDES SMCKE
-0.00 -0.00
-0.00 -0.00
-n.00 -0.00
-0.00 -0.00
PAR
MASS EMI "ASS EMI MASS EMI MASS HMI MASS F.MI MASS FMI MASS EM|
NO NOX CO HC NO? C02 NO
LR/1K LH/1K LR/fR LB/HR LB/HR LB/HR LB/HR
LP "HJEL I.B FUEL
5.09
6.O9
10.69
1.67
CO THf
P./1KSTH-H.1 LC/IK*TH-1'<
1 739. 74M
l'S7.S79
1«32.612
3664.551
0. 35«
0. 3 70
0. 106
90. 560
5.54 95.60
fi.34 48. 79
10.90 31.59
2.00 127.96
3.21
4.88
1.74
98.26
Ml NO
2
L3/IKVTH-HR LB/IKfTH-HR
7.837
4.52'i
6.217
7.164
-0.000
-0.000
-0.000
-0.000
-0.00. 15626.41 25.
-11.00 73207.52 59.
-0.00 29983.15 101.
-0.00 3976.03 2.
NO
X
LR/IKDTH-HR
J.087
4.665
6.344
2.597
48
72
71
35
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
"ASS FMI
NOX
LB/HR
27.73
61.59
103.79
?.fl2
IV-108
-------
CAL 10 NUMBER: 110 ENGINE TYPE AND MODEL: JT30 -38
TEST ORGANIZATION: UNITED/EPA
SERIAL NUMBER: 669210
NODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
0.050
1.000
0.850
0.400
0.050
NODE FRACTIONAL
POKER
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
0.050
1.000
0.850
0.400
0.050
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
I TH
900.0
18000.0
15300.0
7200.0
900.0
POWER
TH
900.0
laooo.o
15300.0
7200.0
900.0
POWER
TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL USAGE TINE IN
RATE RATE WT FACTOR MODE
LB/MR LB/HR M1N.
103.9*6 1131.970 1
17.913 107*1.891 1
33.587 8841.145 1
114.785 4174.469 1
103.946 1131.970 1
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LAS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
87.223 1131.970 1
0.0 10741.891 1
2.260 8841.145 1
6.139 4174.469 1
87.223 1131.970 1
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLEl
TH-HR/CYCLE:
LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
1.915 1131.970
133.762 10741.891
89.157 8841.145
20.411 4174.469
1.915 1131.970
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
32.916
0.209
1.212
7.652
12.127
54.136
44.435
32.990
1.161
HC
MASS
LBS.
27.621
0.0
O.OB3
0.409
10.176
36.289
31.426
23.333
0.0
NOX
MASS
LBS.
0.606
1.561
1.269
1.161
0.221
7.020
5.762
4.278
86.698
FUEL
MASS
LBS.
158.46
125.32
324.18
278.30
112.06
121B.11
FUEL
MASS
LBS.
358.46
125.12
124.18
278.30
132.06
1216.31
FUEL
MASS
LBS.
358.46
125.12
324.18
278.30
132.06
1218.11
LB CO /
IK LB FUEL
91
1
1
27
91
.828
.666
.799
.497
.626
LB HC /
IK LB FUEL
77.054
0.0
0.256
1.471
77.054
LB NOX/
IK LB FUEL
1
12
10
4
1
.692
.452
.084
.890
.692
ENERGY
TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
TH-HR
285.00
210.00
561.00
460.00
105.00
1641.00
LB
0
0
0
0
0
LB
1
CO /
TH-HR
.11550
.00100
.00220
.01594
.11550
HC /
TH-HR
0.09691
0.0
0.00015
0.00085
0.09691
LB
1
0
0
0
0
0
NOX/
TH-HR
.00213
.00743
.OOS81
.00283
.00213
IV-109
-------
BATE: 7/16/71
TF.SF ORGANIZATION: UNI Tf-:)/EPA
ENGINE SUPPLIER: UNITFO AIRLINES
ENGINE DATA .................................................
CAL 10 NUMBFR: m FNGINE TYPE ANO HDOEL: JT30 -IB
SERIAL NUMBER:
HATED THRUST: IBOOO.
FNGIliE TOTAL TIME: 8016. MRS
TIMF SINCE HUT SECTION OVERHAUL: 2112. MRS
TINE SINCE:
Nl COMPRESSOR OVERHAUL: 2992. MRS
N2 COMPRESSOR OVERHAUL: 12527. MRS
cnMBusTnq CAN REPLACEMENT: o. MRS
MUST STAC.F NIU/LE WIDE V4NF OVERHAUL: 0. MRS
NI TURBINE OVERHAUL: 1285. HAS
12 TURBINE OVERHAUL: o. MRS
FIIFL: JET - A FUEL H/C RATIO: 1.970
OPERATIONAL 0«TA ««»««««««««
INLET AIR TEMPERATURE, OFGREES E: START 55.22 FINISH
ATMOSPHFRIC PRESSURE: START 21.7R FINISH
INLET AIR HUMIDITY, LBS H23/LB AIR: O.OI1B2
RELATIVE HUMlnlTY: 66.00 PERCENT
SAHPLE LINE: TEMPERATURE, OE<".REFS C: 160.00, FLOW RATE, LITEPS/N1N:
SAPPLE LINE THANSPORf TI«E, SEC: 5.00
NUMBER OF TFSIS: <,
COMMENTS:
EXHAUST CAS PRESSURE IN INCHFS HG.
PRE-PEPAIR TYPE ENGINE.
5B.28
21.87
CLOCK
TIME
R30.00
642.00
B47.00
946.00
PUWER
PERCENT
RATED
T.O.
4H
72
9 1
5
POWER
PERCENT
RATED
T.O.
4«
72
91
5
POWER
PERCENT
RATEO
T.O.
43
72
11
5
TFST
MfWE
I/ 0
21 I
3/ 2
". / 1
EXHAUST
CAS
TF"P
DEGREES f
663. BO
771.60
1183.40
5 11. BO
MASS E-I
cn
Ln/ IK
LW FUFL
H. P3
4 . 71
2. 1?
115.55
;
L»/1K«
t-
7.
[ .
1 16.
POWER ENGINE MEASURED CAS GEN
TH'JUST.LBS PFRCEMT SPFEO FUEL AIR FLOW
OR RATFO RPM FLU* LB/SEC
SHP
1745.00
13107.00
16511.00
1010.00
EXHAUST
GAS
PRESSURE
PSI A
40. 00
47.10
54.30
30. fin
MASS EMI
MC
LW/IK
LB FUEL
0.56
0.08
0.06
79.92
TH-MO 1
607
511
52S
261
T.O. M
4B 5046.00
72 5819.00
91 6404.00
5 2017.00
C'l CO
1 WET )
PPMV IkET
N2
8846.00
9351 .00
177B .00
5561.00
THC
2 IWETI
1 PPMV
PERCENT V
95.00 2.
60.00 7.
42.00 1.
995.00 1.
"ASS EMI MASS EMI
NC12 CC2
LB/IK LP./K
LP FUEL LB FUEL
-0.00 3140. '.Q
-0.00 3148.14
-0.00 1151.47
-0.00 2765.lt,
CO
2
H/IH.TH-HR LB/1
1 M fl . 2 9 7
1661.451
I 761. 1 A2
1749.141
15 10.50
51 i.sn
10 1.50
51 1200.00
LB/HR
4567.00 -0.00
6923.00 -0.00
1269.00 -0.00
1191. OC -0.00
Nil NO
IWFTI 2
PPMV IWETI
PPMV
32.00 -0.00
68.00 -0.00
91.00 -0.00
1.60 -0.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
NO
X
IWF1 1
PPMV
43.00
62.00
104.00
10.00
COMPRESSOR FNGINE
PISCHARGE PRESSURE
TEMP RATIO
DEGREES " EPR
-0.00 I.J5
-0.00 1.60
-0.00 1.B5
-0.00 -0.00
TUR9IHE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
ALDEHYDES SMOKE PARTICULATCS
-0.00 -O.OC
-0.00 -0.00
-0.00 -0.00
-o.oo -o.oo
MASS Ml MASS FMI MASS FMI MASS EMI MASS FMI MASS FMI MASS EMI
N''
I IV IK
HOX CO
LR/1K LB/HR
HC
LB/HR
NO? CO? NO,
LB/HR LB/HR Lfl/HR
-0.00
-o.on
-0.00
-0.00
M«SS FMI
NDX
LH/HR
IB FUFL LB FUFL
4.09
8.12
10.52
I.M
1HC
* TH-HR
0.212
n.04^
0.011
94. 170
t.57 40.29
8. 13 13.16
11.05 75.11
1.91 137.63
NO
7.55
0.57
0.52
95.06
NO
7
L6/1K1TH-HH LB/1K#TH-HR
2.541
4.7U
5.906
?.I59
-o.oon
-0.000
-o. cpo
-0.000
-0.00 14326.36 22.29
-O.OP 21794.56 61.71
-0.00 29210.94 97.5?
-0.00 3281.63 2. in
NU
X
LB/ 1 K*TM-HR
1.475
4.215
6.205
7.241
21.95
56. 2H
102.45
2.27
IV-110
-------
CAL 10 NUMBER: 133 ENGINE TYPE AND MODEL: JT3D -3B
TEST ORGANIZATION: UNITED/EPA
SERIAL NUMBER: 6*5064
MODE FRACTIONAL
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
POWER
0.050
1.000
O.B50
0.400
0.050
POKER
TM
900.0
laooo.o
15300.0
7200.0
900.0
EMISSION
RATE
LB/HR
293.721
18.876
23.474
42.979
253.721
FUEL USAGE
RATE MT FACTOR
LB/HR
971.948
10223.277
8346.531
3887.598
971.948
.000
.000
.000
.000
.000
TIME IN
NODE
MIN.
19.00
0.70
2.20
4.00
7.00
CO
MASS
LBS.
80.345
0.220
0.661
2.865
29.601
FUEL
MASS
LBS.
307.78
119.27
306.11
259.17
113.39
LB CO /
IK LB FUEL
261.044
1.846
2.812
11.055
26I.O44
ENERGY
1 TH-MR
285.00
210.00
561.00
480.00
105.00
LB CO /
TH-HR
0.28191
0.00105
0.001S3
0.00597
0.2BI9I
TOTAL FOR CYCLE! 113.892
LBS POLLUTANT/IK LB FUEL/CYCLE: 103.001
LBS POLLUTANT/IK LB TH-HR/CYCLE1 69.404
LBS POLLUTANT/1000K LB TH AT T.O.: 1.223
MODE
TAXI-IOLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.050
1.000
O.B50
0.400
0.050
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
TH
900.0
18000.0
15300.0
7200.0
900.0
POWER
1 TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL I
RATE RATE UT
LB/HR LB/HR
45.306 971.948
0.0 10223.277
0.0 8348. 531
3.649 3887.598
95.306 971.948
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS PdLLUTANT/IOOOK
EMISSION FUEL I
RATE RATE HI
LB/HR LB/HR
1.675 971.948
129.334 10223.277
80.936 8348.531
22.503 3887.598
1.675 971.948
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
IBS POLLUTANT/1000K
SAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLF.:
LB TH AT T.O.I
ISAGE TIME IN
FACTOR NODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
HC
MASS
LBS.
30.180
0.0
0.0
0.243
11.119
41.543
37.570
25.315
0.0
NOX
MASS
LBS.
0.530
1.509
2.968
1.500
0.195
6.702
6.062
4.084
83.827
FUEL
MASS
LBS.
307.78
119.27
306.11
259.17
113.39
1105.73
FUEL
MASS
LBS.
307.78
119.27
306.11
259.17
113.39
1105.73
LB HC /
IK LB FUEL
98.057
0.0
0.0
0.934
98.057
IB NOX/
IK LB FUEL
1.723
12.651
9.695
5.788
1.723
ENERGY
I TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
LB HC /
TH-HR
0.10590
0.0
0.0
0.00051
0.10590
LB NOX/
TH-HR
0.00186
0.00714
0.00529
0.00313
0.00186
iv-in
-------
OATF: 7/21/71
TEST ORGANIZATION: IINIrfD/EPA
F.NGINF SUPPLIER: UNITCO AIRLINES
FNG1NF DATA
CAL ID NUMfFU: 116 FNf.INF TYPF AND MODEL: JT3D -3B
RATED Tt-RLSl: 18000.
ENGINE TOTAL TIME: 9064. HRS
TIME SINCE HIT SECTION OVERHAUL: 1137. HRS
TIME SINf.F:
NI CCMPI.ESSOR OVERHAUL; -o. HRS
N2 COMPRESSOR OVERHAUL: -o. HRS
COMBUSTUR CAN REPLACEMENT: -0. HRS
FIRST STAC.F NOZZLE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL: JET - A FUEL H/C RATIO: 1.920
OPERATIONAL DATA ««««««««»««««««»««»
INLET AIR tEMPER.MURE, DFGKFES F: S1ART 62.60 FINISH
ATMOSPHERIC PRESSURE: START 29.92 FINISH
INLFI AIR HUMIDITY, LF>S H20/H) AIR: 11.0103
RELATIVE HUMI1ITY: 72.00 PEB.CF.NT
SAMPIE LINF: TEMPERATURE, CEGRFES C: 160.CO, FLOU HATF, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SFC: 5.00
NUMBER OF TESTS: 4
COMMENTS:
FXHAUST GAS TFMPFKATUP.E IN DEGREES C
FXHAUST GAS PRESS.IBF IN INCHES HG.
SFRIAL NUMBER:
59.00
29.92
CLOCK
T IMF
-0.00
-0.00
-0.00
-0.00
POMER
PERCENT
RATED
T.O.
49
71
90
5
POWER
PERCENT
HATEO
T.O.
49
71
90
5
POUFR
PERCFNT
RATED
T.O.
49
n
90
>
TFST
"Mint;
I/ 0
2/ 1
3/ 2
4/ 1
FXHAUST
GAS
TEMP
PFGRFFS f
175.00
428.10
486.00
270.00
MASS E«l
CO
LB/IK
LB FUFI
9.56
4. 71
1.03
119 .94
CO
POHFR ENGINE
THRUST, LBS
OR
SHP
1963.00
12815.00
16267.00
990.00
[XHAUS1
GAS
PRFSSURF
PS I A
40.40
4 (. . 9 0
53. 9n
31.80
MASS FMI
Mf.
1 B/IK
LP FUEL
0.01
0.05
0.03
125.94
PtRCFNT SI'EEH
RATED
T.O. M
4'l 5116.00
71 5746. OC
90 6361.00
5 2034.00
Cll
( WFM
RPM
N2
fi951 .00
9417.00
9812.00
5849.00
CO
MEASURED GAS GF N
FUEL AIR FLOU
FLOU LB/SFC
Ln/HR
4038.00 -0.00
6963.00 -0.00
9272.00 -0.00
1206.00 -0.00
THC NO NO
2 IWCTI IhET) 2
PPMV l^ET)
Pt-RCENT V
1 10.00
60.00
40.00
910.00
MASS f-'.l MASS F»l
<02 CH2
LI/IK LB/1K
L9 FUEL LH FUEL
-0.00 1140. R5
-1.0" 3148.11
-1.01 3151.05
-0.00 2637.65
rn
2
2.10
2.55
2.65
PP.MV PPMV (WET!
PPMV
0.10 34.00 -0.00
1.20 57.60 -0.00
1.66 88.00 -0.00
1.42 IP60.00 9.40 -0.00
MASS EMI
NT
LB/1K
L8 FUEL
4.85
7.43
10.94
I.Bl
THC
LB/IKKTH-HR L P / IK « TH-H1 LB/IKMH-HR
5.
2.
1 .
111.
160
562
725
.179
1695.154
1 7 10.640
I 796.064
H'12.662
0.001
1.029
1.116
152.415
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
NO
X
(UFTI
PPMV
44.00
63.60
93.00
10.20
COMPRESSOR ENGINF TURBINE
DISCHARGE PRESSURE INLET
TEMP PAIIO TFMP
DEGREES F EPR DEGREES F
-0.00 1.36 -0.00
-0.00 1.59 -0.00
-0.00 1.83 -0.00
-0.00 -0.00 -0.00
ALDEHYDES SMOKE PARTICIPATES
-0.00 -0.00 -0.00
-0.00 -0.00 -0.00
-0.00 -0.00 -0.00
-0.00 -0.00 -0.00
MASS F.M1 M.ASS FMI MASS EMI MASS E"I MASS EMI MASS EMI MASS F " 1
NOX CO
LH/1K LB/HR
Irt FUFL
6.28 46.75
P. 21 12.83
11.56 28.07
1.98 112. HI
NO
Ifl/lKKTH-HR L
2.620
4. C19
6.231
2.20''
HC
Lfl/HR
0.02
0.38
0.27
152.13
NO
2
3/1KHTH-HR
-0.000
-0.000
-0.010
-0.100
N02 CQ2 NO NOX
LB/HR LB/HK LH/HK LB/H*
-0.00 15195.45 23.48 30.3'l
-0.00 21921.85 51.77 57.16
-0.00 29216.57 101.43 107.19
-0.00 3186. 2d 2.20 2.39
NO
X
Lfl/ 1 K1TH-HK
3.3'H
4.460
6.589
2.3<>7
IV-112
-------
CAL ID NUMBER: 136 ENGINE TYPE AND MODEL: JT3D -3B
TEST ORGANIZATION: UNITED/EPA
SERIAL NUMBER:
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
O.B50
0.400
0.050
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
O.OJO
FRACTIONAL
POWER
O.OSO
1.000
0. 850
0.400
0.050
POWER
« TH
900.0
IBOOO.O
15300.0
7200.0
400.0
POWER
t TH
900.0
laooo.o
15300.0
7200.0
900.0
POWER
1 TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
124.306 1133.015
21.156 10517.309
25.372 8653.250
63.594 4028.169
124.306 1133.015
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/iaOOK
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
145.806 1133.015
0.0 10517.309
0.0 8653.250
10.969 4028.169
145.806 1133.015
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOX
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
2.129 1133.015
144.115 10517.309
91.373 8653.250
22.227 4028.169
2.129 1133.015
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLEi
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
39.364
0.247
0.930
4.240
14.502
59.283
49.423
36.126
1.371
HC
MASS
LBS.
46.172
0.0
0.0
0.731
17.011
63.914
53.284
3B.948
0.0
KOI
MASS
LBS.
0.674
1.6B1
3.350
1.482
0.248
7.436
6.199
4.531
93.408
FUEL
MASS
LBS.
358.79
122.70
317.29
268.54
132.18
1199.50
FUEL
MASS
LBS.
358.79
122.70
317.29
26B.54
132.18
1199.50
FUEL
MASS
LBS.
358.79
122.70
317.29
268.54
132.18
1199.50
LB CO /
IK LB FUEL
109.713
2.011
2.932
15.787
109.713
LB HC /
IK LB FUEL
128.689
0.0
0.0
2.723
128.689
LB NOX/
IK LB FUEL
1.BT9
13.703
10.559
5.518
1.879
ENERGY
TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
LB CO /
f TH-HR
0.13812
0.00118
0.00166
O.OOBB3
0.13812
LB HC /
TH-HR
0.16201
0.0
0.0
0.00152
0.16201
LB N0«/
TH-HR
0.00237
0.00801
0.00597
0.00309
0.00237
IV-113
-------
OATE: 7/27/71
TEST ORGANi/.tTiON: s w R i TWA
ENGINE SUPPLIER: r W A
FNGINF DATA
CAL in NUMBER: 282
ENGINE TYPE AND MOOFL: JT3D -3B
SERIAL NUMBER:
RATED THUST: mono.
ENGINE TOTAL MMf: 11564. MBS
TIKE SINCE MOT SECTHIN OVERHAUL: 1564. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 5936. HRS
N2 CCMPHESSCIR OVERHAUL: 5936. HRS
COMBUST CAN REPLACEMENT: 593*. HRS
FIRST STAGF NOZZLE GUIDE VANE OVERHAUL: 5936. HRS
NI TURHINF IIVERHAUL: 5936. HRS
N2 TURBINE OVERHAUL: 59.16. HRS
FUFL M/C RATIII: P.020
75.00
28.98
FUEL: jp-4 TF
OPERATIONAL DATA «»««»««««
INLET AIR TEMPERATURE, OEI'.REFS F: START 75.00 FINISH
ATMOSPHERIC PRFSSIIRF: START 28.98 FINISH
INLtT AIR HUMIDITY, LBS H20/LB AIR: 0.0094
RELATIVE HUMIDIIY: 41.00 PERCENT
SAMPLE LINE: TEMPERATURE, OECREES C: 150.00, FLOW RATE, LITFRS/MlN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TFSTS: 6
COMMENTS:
F/A AND AIRFLOW CALCULATE!' FROM FXHAUST COMPOSITION FUR FIFTH RUN. N02
DETERMINED BY SUBTRACTION.
ELAPSED
TIMF
0.0
4.30
13. DD
2H.OO
.14.00
36.30
TESI
POOF
6/ 0
I/ 6
?./ 1
J/ 2
'./ 3
5/ 4
POWER
THRUST, LHS PEKCFNT
OH RATEH
SHP
9100.00
1 1200.00
11700.00
15420.00
1100.00
14900.00
T.O.
50
62
73
«5
6
82
FNGINF
SPEED
RPM
NI
5440.00
5B60.00
62HC.OC
6680.00
2160.00
656C.CO
N2
0160.00
9460.00
S730.00
100BO.OO
6150.00
9890.00
MEASURED
FUEL
FLOW
LB/HR
5110.00
6320.00
7650.00
9400.00
1110.00
8940.00
GAS GEN
AIR FLOW
L3/SFC
126.00
142.30
157.60
173.90
34.70
170.00
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.011300
0.012300
0.013500
0.015000
0.008000
0.014600
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.37
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TFMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER EXHAUST
PERCENT GAS
RATED TFMP
T.O. PFG»EES r
50
62
7»
R5
739.00
797.00
H62.00
961.00
554.00
94 I.00
EXHAUST
GAS
PRESSURE
PS I A
4.HO
6.50
1.50
10.90
0.30
10.20
C.I
(WED
PP«V
43.00
20.00
9.00
K.OO
649.00
12.00
CO
2
IhFT)
PERCENT V
P. 09
2.27
2.49
2.77
1.44
2.f9
THC
(XET)
PPHV
1.00
12.00
3.00
0.0
1025.00
20.no
NO
(WFTI
PPMV
36.00
47.00
74.00
91.00
2.00
BO. 00
NO
7
(MET)
PPMV
2.00
2.00
1.00
0.0
7.00
1.00
ALDEHYDES SMOKE PARTICULARS
IHFT)
PPMV
38.00
49. OC
75.00
91.00
9.00
81.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-o.oo
-0.00
-0.00
-0.00
POMER MASS fl
PERCENT Cn
RATED Lfl/lK
T.O. Lfl FIIFL
50
62
73
US
4.09
1. 75
0.72
0.5"
80.51
O.H9
ASS EMI
HC
LP/IK
LB FUEL
o.os
0.60
0.14
0.0
72. «1
0.85
MASS FMI
N02
LI/IK
Lfl FUEL
0. 31
0.29
0.13
0.0
1.41
0. 17
MASS EMI
CO?
L W /I K
Lfl FUCL
1126.66
3128.83
3111 .71
3132.34
2806.94
1129.52
MASS EMI
NO
LH/1K
Lfl FUFL
5.63
6.77
9.73
10.76
0.41
9.73
«»SS FMI
NOX
LP/IK
LI FUEL
5.94
7.06
9. 86
10.76
1.83
9.85
"ASS EMI
CO
70.92
I 1.09
5.51
5.41
99.37
7.94
MSSS FMI
HC
L6/HP
0.78
3.HI
I.OS
0.0
90.94
MASS EMI
N02
LB/K5
1.60
1.82
I.01
0.0
1.59
1.09
MASS FMI MASS FMI
C02 NO
LB/HR L8/HP
15977.2)
19774.21
23957.T5
29441.96
3115.70
27977.99
28.77
42.90
74.43
101.12
0.45
86.98
MASS FMI
NIJX
30.37
44.67
75.44
101.12
2.04
d8.07
PUWER
PFKCENT
RATED
T.O.
50
62
73
B5
r.n
LI>/IKJTH-HR
0.190
0.41D
0.351
HI.247
1.533
Lfl/1K
-------
CAL 10 NUMBER: 282 ENGINE TYPE AND MODEL: JT3D -SB
TEST ORGANIZATION! S M R 1 TWA
SERIAL NUMBER: P643B49B
MODE FRACTIONAL
POKER
TAXI-IDLE
TAKEOFF
CLIMB OUT
APPROACH
TAKI-10LE
0.050
I. 000
0.850
0.400
0.050
MODE FRACTIONAL
PONER
TA«I-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
0.050
1.000
0.850
O.»00
0.050
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POKER
1 TH
900.0
18000.0
15300.0
7200.0
900.0
PONER
TH
900.0
18000.0
15300.0
7200.0
900.0
POUER
« TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL USAGE TIME IN
RATE RATE NT FACTOR MODE
LB/HR LB/HR MIN.
80.303 907.073
3.952 11810.000
9.337 9419.023
41.424 4212.953
80.303 907.073
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE NT
LB/HR LB/HR
80.978 907.073
1.771 11810.000
2.459 9414.023
0.285 4212.953
80.978 907.073
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE XT
LB/HR LB/HR
1.445 907.073
151.117 11810.000
100.314 9419.023
19.344 4212.953
1.445 907.073
TOTAL FOR CYCLE:
LBS POLLUTANT/IK 18
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 T.OO
FUEL /CYCLE:
TH-HR/CYCL6:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 O.TO
.000 2.20
.000 4.00
.000 T.OO
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
25.429
0.046
0.342
2.762
9.369
37.948
32.797
23.125
0.256
HC
MASS
LBS.
25.643
0.021
0.090
0.019
9.447
35.220
30.439
21.463
1.148
NOX
MASS
LBS.
0.45B
1.763
3.678
1.290
0.169
7.357
6.358
4.483
97.946
FUEL
MASS
LBS.
287.24
137.78
345.36
280.86
105. «3
1157.08
FUEL
MASS
LBS.
287.24
137.78
345.36
280.86
105.83
1157.08
FUEL
MASS
LBS.
2BT.24
137.78
34S.36
280.86
105.83
1157.08
LB CO /
IK LB FUEL
88
0
0
9
88
.530
.335
.991
.832
.530
LB HC /
IK LB FUEL
89
0
0
0
89
.274
.150
.261
.068
.274
LB NOX/
IK LB FUEL
1
12
10
4
.593
.796
.650
.592
.593
ENERGY
TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
f TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
TH-HR
285.00
210.00
561.00
480.00
105.00
1 64 1 . 00
LB
0
0
0
0
0
LB
0
0
0
0
0
LB
0
0
0
0
0
CO /
TH-HR
.08923
.00022
.00061
.00575
.08923
HC /
TH-HR
.08998
.00010
.00016
.00004
.08998
NOX/
TH-HR
.00161
.00840
.00656
.00269
.00161
IV-115
-------
DATE; 7/10/71
TEST ORGANIZATION: 5 W R 1 TWA
FNGINE SUPPLIER: Tut
ENGINE DATA
CAL 10 NUMBER: 101
ENGINE TYPE AND MODFL: JI3D -3B
RATFD THRUST:
ENGINE TflTIH TIME:
TIME SINCE HUT SECTION OVERHAUL:
TINE SINCE:
IBOOO.
10673. MRS
1939. MRS
SERIAL NUMBER:
NI COMPRESSOR OVERHAUL: 3139. HRS
N2 COMPRESSOR OVERHAUL: 3939. MRS
COMBUSTtlR CAN REPLACEMENT: 1939. HRS
EIRST STAGE NOZZLE GUIDE V4NE OVEPHAUL: 3939. HRS
NI TURBINE OVERHAUL: 3939. HRS
N2 TURBINE OVERHAUL: 3939. MRS
EUEL H/C RATIO: 2.020
FUEL; jp-4 TF
OPERATIONAL DATA ««««««««««
INLE! AIR TEMPERATURE, DF.GRFES F: START 61.00 FINISH 60.00
ATMOSPHERIC PRESSURE: START 29.09 FINISH 29.10
INLET AIP HUMIDITY, LttS H2U/LX AIM: 0.0074
RELATIVE HUMIDITY: 65.oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.OC, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 6
COMMENTS:
E/A AND AIRFLOW CALCULATED FROM FXHAUSI COMPOSITION FRR FIFTH RUN. N02
DETERMINED BV SUBTRACTION.
ELAPSED
TIME
0.0
5.00
13.00
12.00
15.30
40.00
TEST
MUDF
6/ 0
I/ 6
2/ 1
I/ 2
4/ 3
5/ 4
POWEW
THPUST.L9S PERCENT
OR HATED
SHP
9960.00
10860.00
13060.00
15320.00
1040.00
14440.00
r.o.
49
6D
7?
85
5
80
FNG1NF
SPEED
KPM
NI
5130.00
5BOO.OO
61 10.00
6580.00
2050.00
6410.00
N2
9000.00
9270.00
9540.00
9860.00
5950.00
9650.00
MEASURED
FUEL
FLOW
LB/HR
4950.00
607r.no
7390.00
9180.00
960.00
3670.00
GAS GEN
AIR <=LUW
LB/SEC
127.40
143.00
156.50
175.00
30.60
169.20
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.010900
0.011 BOO
0.013000
0.014600
O.C08700
0.014200
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
FNGINE
PRESSURE
RATIO
EPR
1.37
-0.00
-0.00
-0.00
-0.00
-o.oo
TURBINE
INLET
TtNP
DEGREES 1
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
49
60
7?
H5
5
no
EXHAUST
OAS
TEMP
OEGRLES F
70S.00
757.00
mi. oo
901.011
54 1 . nn
864.00
EXHAUST
GAS
PRESSURE
PSIA
4.«0
6.50
K.40
11.10
0.40
in. in
cn
IWETI
PPPV
43.00
IS. 00
9.00
5.00
5B3.no
6.00
cc
2
IHETI
PERCENT V
7. Id
2.34
2.56
2.CS8
1.80
2.10
THC
1UETI
PPHV
4.00
0.0
0.0
0.0
910.00
0.0
NO
IWtTI
PPHV
30.00
41.00
M.OO
H9.00
3.00
76. On
NO
2
I WETI
PPMV
8.00
6.00
4.00
4.00
7.00
5.00
I WET I
PPMV
38.00
49.00
65.00
91.00
10.00
81.00
-0.00
-o.on
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PAOTICULAIFS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POtfEP
PERCENT
RAIEP
T.O.
49
60
7?
35
5
30
MASS FMI
CO
LB/IK
LU FUFL
1 . 'If,
1.5)
0.70
0.15
59.64
0.43
MASS EMI
Hf.
Lfl/IK
LB FUEL
0.21
O.T
0.3
0.0
53.32
0.0
MASS EH
NU2
LI/IK
LB EUH
1.21
0.84
0.51
0.45
1 . 1H
9.5U
"ASS [Ml
CO?
LP/1K
LB FUCL
MASS EMI
NO
LC/IK
LB FUEL
MASS EMI
CO
LB/t-K
MASS CMI
HC
LB/HR
1.21
O.S4
0.51
0.45
1 . 1H
9.5U
3126.44
3130. B3
1132. 15
31 12.70
2H93. 26
3112.57
4.54
6.01
7.74
10. 12
0. 50
8.H9
5.75
6.85
B.25
10.58
1.68
5.47
19.61
9.30
5.14
3.19
57.26
1.70
1.C4
0.0
O.n
o.n
51.18
0.0
MASS FMI
N02
LB/HR
5.99
5.09
3.75
4.18
1.13
5.07
MASS EMI
CO 2
Lfl/HR
15475.88
19004.15
23146.57
2H758.I5
2777.53
27159.36
MASS FMI MASS EMI
ND NOX
LB/HH LR/HR
22.47
36.51
57.21
92.91
0.48
77.07
28.46
41.60
60.96
97.08
1.61
B2.14
POWER
PERCENT
RATED
T.O.
49
60
72
R5
5
80
Cn
LH/IK*IH-HP
2.138
O.R57
n. 193
0.207
55.^53
0. 257
r.n
2
<4TH-HR
1727.21?
1741.922
1772.326
IB'7.164
2610.706
1BBO.R42
THC
LB/1K*IH-HR
0.117
o.o
n.o
o.o
49.216
0.0
NO
L B/ 1 K.«TH-Ma
2.50H
3.162
4.181
6.064
0.465
5.117
LR/1KHTH-HR
0.669
0.469
0.287
C.273
1.086
0.151
NO
I
LB/IK«TH-HR
1.177
1.331
4.66B
6.337
1.551
5.6KB
IV-116
-------
C41 10 NUMBER! 301 ENGINE TYPE AND MODEL: JT3D -SB
TEST ORGANIZATION: S M R I TWA
SERIAL NUMBER:
MODE FRACTIONAL
POKER
TAXI-IDLE 0.050
TAKEOFF 1.000
CLIHBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.050
MODE FRACTIONAL
POWER
TAXI-IOLE 0.050
TAKEOFF l.OOD
CLIHBOUT 0.850
APPROACH 0.400
TAXI-IOLE 0.050
MODE FRACTIONAL
POWER
TAXI-IDLE 0.050
TAKEOFF 1.000
CLIHBOUT 0.830
APPROACH 0.400
TAXI-IDLE 0.050
POWER
f TH
900.0
18000.0
15300.0
7200.0
900.0
POWER
i TH
900.0
18000.0
15300.0
7200.0
900.0
POWER
f TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL USAGE TINE IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
46.291 758.395 .000 19.00
7.433 10680.215 .000 0.70
6.336 9007.215 .000 2.20
31.120 4052.942 .000 4.00
46.291 758.395 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
45.653 758.395 .000 19.00
1.074 10680.215 .000 0.70
1.362 9007.215 .000 2.20
4.011 4052.942 .000 4.00
45.653 758.395 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TINE IN
RATE RATE WT FACTOR NODE
LB/HR LB/HR MIN.
0.912 758.395 .000 19.00
146.354 10680.215 .000 0.70
93.930 9007.215 .000 2.20
I9.26B 4052.942 .000 4.00
0.912 758.395 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
CO
MASS
LBS.
14.659
0.087
0.232
2.075
5.401
22.453
21.309
13.683
0.482
HC
MASS
LBS.
14.457
0.013
0.050
0.267
5.326
20.113
19.088
12.256
0.696
NOX
MASS
LBS.
0.289
1.707
3.444
1.2B5
0.106
6.831
6.483
4. 163
94.859
FUEL
MASS
LBS.
240.16
124.60
330.26
270.20
88.48
1053.70
FUEL
MASS
LBS.
240.16
124.60
330.26
270.20
88.48
1053.70
FUEL
MASS
LBS.
240.16
124.60
330.26
270.20
88.48
1053.70
LB CO /
IK LB FUEL
61.038
0.696
0.703
7.678
61.038
LB HC /
IK LB FUEL
60.197
0.101
0.151
0.990
60.197
LB NOX/
IK LB FUEL
1.202
13.703
10.428
4.754
1.202
ENERGY
TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-MR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
LB CO /
f TH-HR
0.05143
0.00041
0.00041
0.00432
0.05143
LB HC /
t TH-HR
0.05073
0.00006
0.00009
0.00056
0.05073
LB NOX/
TH-HR
0.00101
0.00813
0.00614
0.00268
0.00101
IV-117
-------
DATE: 8/ 2/71
TEST ORGANIZEION: s w R i rut
ENGINE SUPPLIER: TWA
FNGINF DATA
CAL 10 NUMBFR: 10?
ENGINE TY»E AND MODEL: JT3D -IB
SERIAL NUMBER: 641558
RATE1 THRUST: 18000.
ENGINE TOTAL T1NF: 4156. MRS
TIME SINCF HOT SECTION OVERHAUL: 4156. HRS
TIKE SINCF:
NI COMPRESSOR OVERHAUL: MSB. HRS
N2 CCMPRFSSOR OVERHAUL: 4158. HRS
COMOUSTOR CAN RFPLACFMFNT: 4158. HRS
FIRST STAGE NOiZLE GUlnE VANE OVERHAUL: 4158. HRS
Nl TURBINE OVERHAUL: 4158. HRS
N2 TURBINF OVERHAUL: 4158. HRS
FUEL H/r. RATIO: 2.020
FUEL: JP-4 TF
OPERATIONAL OATA ««««««.........«..««.
INLET AIR TEHPFRATURF, DEGREES F: START 72.00 FINISH 72.00
AIMOSPHFPIC PRESSURE: START 28.14 FINISH 28.14
INLFT AIR HUMIDITY, LBS H20/Lrt AIR: 0.0120
RELATIVE HUMI1ITY: 68.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 150.00, FLOW RATE, LITEPS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 6
COMMENTS:
F/A AND AIRFLOW CALCULATED FROM EXHAUST COMPOSITION FOR FIFTH RUN. N02
DETFRMINED BY SUKTRACTION.
ELAPSED TEST POWFR
TINE MODE THRUST.LBS P
OR
SHP
0.0
6/ 0
9040.00
4.15 1/6 IIIBO.OO
4.30 2/ I 13300.00
14.45 3/ 2 15440.00
72.00 4/ 1 960.00
76.00 5/ 4 15000.00
ENGINE
CENT
iTFD
0.
50
62
73
85
5
83
SPEF.P
Nl
5420.00
5840.00
6270.00
6670.00
2030. 30
6550.00
RPM
N2
9130.00
9420.00
96RO.OO
9980.00
5870.00
9900.00
MEASURED
FUEL
FLOW
LB/HR
5030.00
6790.00
7630.00
9360.00
1020.00
8950.00
GAS GEN
AIR FLOW
LB/SFC
126.00
142.30
158.50
173.90
32.00
171.00
CALC
F/A
0.011100
0.017300
0.013400
0.014900
0.008900
0.014500
COMPRESSOR
DISCHARGE
TFMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
FPR
1.37
1.50
1 .66
1.84
-0.00
-0.00
TURBINE
INLFT
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PUWEP
PERCENT
RATED
T.O.
50
62
7J
85
5
83
FXHAUST
GAS
TCHP
OFGREFS f
710.00
790.00
956.00
959.00
516.00
910.00
EXHAUST
CAS
PRISSURF
PSI A
4. 80
6.50
8.60
I I .00
0.30
10.30
CO
!»FT>
PPMV
52.00
26. on
15.00
25.00
045.00
71.00
cn
2
IWET)
PERCENT V
2.71
2.44
2.f5
2.«9
l.tlO
2.81
THC
IUET)
PPMV
17.00
2.00
0.0
0.0
710.00
0.0
NO
(UFTI
PPMV
34.00
45.00
62.00
85.10
4.00
76.00
NO
7
IWFT)
PPMV
3.00
5.00
3.00
2.00
4.00
3.00
ALDEHYDES SMOKE PARTICULATFS
IUET)
PPMV
37.00
50.00
65.00
87.00
8.00
79.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oc
POWER
PERCENT
RATED
T.U.
50
62
73
H5
5
83
MASS FMI
CO
LB/IK
L8 FUFL
4.68
2.12
1.11
1. 72
66. '.5
1.42
MASS FMI
HC.
Lfl/IK
LB FUEL
0.6?
0.09
0.0
0.0
41.90
0.0
MASS EMI
Nf)2
L^/ I*
L» FUEL
0. 44
0.67
'1.37
0.23
0.6,1
0.35
MASS EMI
C02
LI/IK.
LH FUEL
3124.19
3129.65
1 1 .1 1 . 4 7
3110.53
7.913.89
1131.01
MASS FMI
NO
1.9/1K
LB FUEL
5.0?
fc. 03
7.66
9.6.1
0.68
H.H5
MASS EMI
NUX
5.47
6.70
R.03
9.85
1.35
9.70
"ASS EMI
CU
Lli/fR
? 1.53
13.35
8.61
16.11
67.78
12.69
"ASS EMI
HC
LB/HR
3.11
0.51
0.0
0.0
47.73
0.0
MASS EMI
NU2
LB/HR
2.23
4.22
2.83
2.1?
0.69
3.13
MASS FMI
CO 2
LB/HR
15714.70
19685.50
23813.1I
29101.78
2972.17
28022.55
75.27
17.95
58.44
90.09
0.69
79.23
MASS LM1
NOX
LB/HR
27.50
47.17
61.27
97.21
1.38
82.36
PUHER
PERCENT
KATED
T.O.
50
6?
7J
85
5
83
cn
L'J/IKH TH-H*
I. 194
0.647
1.045
70.'. Ort
0.346
LB/1KHTM-H.1
1738.151
1760.77B
1796.47'.
1897.783
3190.007
Iflofl.l 7C
THC
I8/IX1TH-HR
0. 344
0.053
0.0
0.0
44.514
0.0
NO
LB/1KKTH-HH
7.796
3.395
4.394
5.815
0.719
5.282
LP/ IMTH-HR
0.747
0.377
0.213
0.137
0.719
0.209
NO
X
LB/1K«TH-HR
3.042
3.772
4.606
5.
-------
CAL ID NUMBER: 302 ENGINE TYPE AND MODEL: JT3D -3B
TEST ORGANIZATION: s w R i TWA
SERIAL NUMBER: 6*3558
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TIKI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMB OUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
O.B50
0.400
0.050
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
TH
900.0
18000.0
15300.0
7200.0
900.0
POWER
1 TH
900.0
IBOOO.O
15300.0
7200.0
900.0
POWER
TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL USAGE TIME IN
RATE RATE UT FACTOR MODE
LB/HR LB/HR MIN.
52.797 766.013 .000 19.00
17.397 10620.641 .000 0.70
15.036 9179.488 .000 2.20
41.626 4140.949 .000 4.00
52.797 766.013 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
37.698 766.013 .000 19.00
0.859 10620.641 .000 0.70
1.449 9179.488 .000 2.20
4.B60 4140.949 .000 4.00
37.698 T66.013 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE UT FACTOR MODE
LB/HR LB/HR MIN.
0.7SB 766.013 .000 19.00
132.511 10620.641 .000 0.70
87.860 9179.488 .000 2.20
18.624 4140.949 .000 4.00
0.758 766.013 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
CO
MASS
LBS.
16.719
0.203
0.551
2.775
6.160
26.408
24.715
16.093
1.128
HC
MASS
LBS.
11.938
0.010
0.053
0.324
4.398
16.723
15.651
10.191
0.556
NOX
MASS
LBS.
0.240
1.546
3.222
1.242
0.088
6.337
5.931
3.862
85.887
FUEL
MASS
LBS.
242.57
123.91
336.58
276.06
89.37
1068.49
FUEL
MASS
LBS.
242.57
123.91
336.58
276.06
89.37
1068.44
FUEL
MASS
LBS.
242.57
123.91
336.58
276.06
89.57
1068.49
IB CO /
IK LB FUEL
68.924
1.638
1.638
10.052
68.924
LB HC /
IK LB FUEL
49.214
0.081
0.158
1.174
49.214
LB NOX/
IK LB FUEL
0.989
12.477
9.571
4.498
0.9B9
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HH
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
f TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
LB CO /
1 TH-HR
0.05866
0.00097
0.00098
0.00578
0.05866
LB HC /
TH-HR
0.04189
0.00005
0.00009
0.00068
0.04169
LB NOX/
1 IH-HR
0.00084
0.00736
0.00574
0.00259
0.00084
IV-119
-------
DATE: 7/21/71
TEST ORGANIZATION: PKATT t WHITNEY
ENGINE SUPPLIER: PRATT AND WHITNEY
ENGINE DATA
CAl 10 NUMBER: 327 ENGINE TYPE AND MODEL: JT30 -3B
RATEO THRUST: IROOO.
ENGINE TOTAL TIME: -0. MRS
TIKE SINCE HUT SECTION OVERHAUL: -0. MRS
TIKE SINCE:
NI COMPRESSTR OVERHAUL: -o. MRS
N2 COMPRESSOR OVERHAUL: -0. HRS
CCWJSTrm CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIOC VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL: jp-4 F'.IEL n/c RATIO: 2.000
OPERATIONAL DATA ««««««««««««««»«««
INLET AIR TEMPERATURE, DEGREES F: START 78.00 FINISH 62.00
ATMOSPHERIC PRESSURE: START 29.10 FINISH 79.28
INLET MB HUMIDITY, LBS H20/LB AIR: 0.0171
RELATIVE HUMIOITY: -C.OO PERCENT
SAMPLE LINE: IEMPEHATURF, DECREES C: 150.GO, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: t.OO
NUMBER OF TESTS: 6
COMMENTS:
SMOKE DENSITY IS VCN BRAND MEASURE PART ICUl.ATES ABE IN MG/H»»3
SERIAL NUMBER:
CLOCK
TIME
10*2.00
TEST
"OOF
I / 0
1102.00 71 I
1120.00 3/ 7
11)8.00 ',/ 3
I 153.00 s/ 4
1204.00 hi 5
POWER
THSIIST.LBS PERCENT
OR RATED
SHP T.O.
650.00
9675.00
11619.00
1.1758.00
15715.00
17731.00
S3
64
76
87
9H
ENGINE
SPEED
RPM
NI N2
0.0
5220.00
5580.00
5920.00
6260.00
6660.00
5465.00
899S.OO
9230.00
9455.00
9690.00
9980.00
MEASURED
FUEL
FLOW
Lfl/HR
915.00
4765.00
5770.00
6B30.00
B120.00
9700.00
GAS GEN CAIC COMPRESSOR ENGINE
AIR FLOW F/A DISCHARGE PRESSURE
LB/SEC TEMP RATIO
DEGREES F EPR
-0.00 -0.000000
128.12
142.67
158.37
160.59
IBS.46
O.OIOOPO
0.010950
0.011680
0.013660
0.014140
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
1.34
1.43
1.55
1.69
1.83
TURBINE
INLET
TEMP
DEGREES E
-0.00
-0.00
-O.CO
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
53
64
76
87
98
EXHAUST
GAS
TEP P
DEGREES r
-o.no
700.10
750.OP
30O.OO
IOR6.00
95S. 00
EXHAUST
GAS
PRESSURE
PS I «
-0.00
19.53
20.85
2?.41
P4.3-1
26. 37
CO
IUET)
PP»V
9I5.AO
56. 10
36.01
24.40
16.60
12.50
CO
2
(WET)
PERCENT V
1.35
7.05
7.21
2. 39
2. (,3
7.89
THC
IWET 1
PPMV
1154.20
5.00
',.60
3. 10
7.7C
14.60
NO
IwFT)
PPMV
1.70
37.20
0.0
fi3.5O
P3.40
0.0
NO
2
1 1,6 T 1
PPMV
5.00
10.50
10.60
10.60
6. 30
4.70
IWETI
PPMV
6 .70
47.70
10.60
74.10
R9.70
4.70
4B.OO
-0.00
-0.00
-0.00
-0.00
-0.00
14.00
44.00
43.00
44.00
41.00
41 .00
PARTICULATES
-0. 00
-0.00
-r.oo
26.00
76.00
24.00
PIIWFR
PERCENT
RATED
I .1).
76
R7
9B
MASS EMI
rn
LB/IK
L<* FIJH
115.97
5.47
3.25
2.04
1 .26
O.B6
MASS EMI
HC
LB/IK
LB FUEL
9B.7I
1.2H
0.24
0. 15
O.I?
0.5H
MASS E"l
NO?
1. R/IK
LR FUEL
1.04
1 .6H
1.57
I .45
0.79
1.53
MASS FMI
CO?
LB/IK
LB FUEL
26B6.09
1126.39
3131.99
31 14. 14
3135.44
1134.81
MASS fMI
NO
LB/IK
LB FUEL
0.35
5.93
0.0
8.71
10.39
n.o
MASS EMI
NOX
LB/IK
LB EUE1
1.39
7.61
1.57
10.16
11.18
0.53
MASS EMI
CO
LH/hK
IOA. 11
76.06
18.74
11.91
10.71
». 37
MASS El'l
HC
LB/HH
89. R7
1.33
1.37
1.01
0.95
5.60
MASS E«I
N02
LB/HR
C.95
7.98
9.06
9.92
0.38
5. 17
MASS EMI
CD?
Lfl/HK
2457.77
14906. 78
18071.59
2140IS. 16
25459.79
30407.61
MASS EMI
KIT
LB/HK
0.32
23.28
0.0
59. 46
84.40
0.0
MASS FMI
NOX
LB/fK
I.7H
36.26
9.06
69.38
90.78
5.17
POWER
PERCENT
RATED
T.O.
53
64
76
87
9B
C'l
L'J/IK»TH-HP
1.417
1 .01 I
0.651
0.472
LS/U
-------
CAL 10 NUMBER: )2T ENGINE TYPE AND MODEL: JT3D -38
TEST ORGAN)IATION: PRATT t KHITNEY
SERIAL NUMBER: p-66een
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.050
1.000
O.B50
0.400
0.050
POWER
TH
900.
18000.
15300.
7200.
900.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR L8/HR
84.190 789.804
14.863 9872.777
17.244 7893.176
39.779 3703.266
84.190 789.804
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
» TH
900.
18000.
15300.
7200.
900.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
62.389 789.804
3.536 9872.777
3.824 7893.176
6.168 3703.266
62.389 789.804
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
1 TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
0.846 789.804
134.745 9872.777
88.478 7893.176
20.121 3703.266
0.846 789.804
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
USAGE TIME IN
FACTOR NODE
MIN. .
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TM-HR/CYCLE:
LB TH AT T.O.:
USAGE TINE IN
FACTOR MODE
MIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR NODE
HIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
26.660
0.173
0.632
2.652
9.822
39.940
40.192
24.339
0.963
HC
MASS
LBS.
19.757
0.041
0.140
0.411
7.279
27.62B
27.802
16.836
2.292
NOX
MASS
LBS.
0.268
1.572
3.244
1.341
0.099
6.524
6.565
3.976
87.334
FUEL
MASS
LBS.
250.10
115.18
289.42
246.88
92.14
993.73
FUEL
MASS
LBS.
250.10
115.18
289.42
246.88
92.14
993.73
FUEL
MASS
LBS.
250.10
115.18
289.42
246.88
92.14
993.73
LB CO /
IK LB FUEL
106.596
1.905
2.185
10.741
106.596
LB HC /
IK LB FUEL
78.993
0.358
0.484
1.666
78.993
LB NOX/
IK LB FUEL
1.071
13.648
11.209
5.433
1.071
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
TM-MR
285.00
210.00
561.00
480.00
105.00
1641.00
LB CO /
TH-HR
0.09354
0.00083
0.00113
0.00552
0.09354
LB KC /
1 TH-HR
0.06932
0.00020
0.00025
0.00086
0.06932
LB NOX/
TH-HR
0.00094
0.00749
0.00578
0.00279
0.00094
IV-121
-------
DATE: 7/22/71
TEST ORGANIZATION: PK4TT f. WHITNEY
ENGINE SUPPLIER: PRATT AND WHITNFY
ENGINE DATA »««....4...».....»
C4L ID NUM«:t: 128 FNGINE TYPF AND MODEL: JT10 -3P
SERIAL NUMBER:
RATEO Tt-RUST: 18000.
ENGINE TOTAL TIME: -0. MRS
TIME SINCE HOT SECTION OVERHAUL: -0. MRS
TIMF SINCE:
NI COMPRESSOR OVERHAUL: -n. MRS
N2 COMPRFSSOP OVERHAUL: -o. MRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NO/ZLE GUI OF VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. MRS
N? TURBINE OVERHAUL: -0. HRS
FUEL: JP-4 FUF.L H/C RATIO: 2.000
OPERATIONAL DATA »«»«»««««»»*«
INLET AIR TEMPERATURE, DEGREES F: START 82.00 FINISH
ATMOSPHERIC PRESSURE: STARI 30.00 FINISH
INLFT AIR HUH I 01 TV, LBS H20/LB AIR: 0.0106
RELATIVF HUMIDITV: -0.00 PERCENT
SAMPLE LINE: TEMPERATURE, OEGRFES C: 150.00, FLOW RATE, LITERS/MIN:
SAPP1E LINF TRANSPORT TIME, SFC: 1.00
NUMBER OF TESTS: 6
COMFNTS:
SMOKE DENSITY IS VGN HRAND MEASURE PART ICUI. A It S ARF IN HG/M«»3
77.00
29.20
CLOCK
TIME
1640.00
1715.00
1800.00
1814.00
1825.00
1725.00
TEST
MODE
I/ 0
21 1
3/ 2
4/ 1
5/ 4
6/ 5
P1HFR
THOUST.LHS PERCENT
OR RAIFD
SHP
860.00
1 1625.00
11660.00
15677.00
1 7651.00
3400.00
T.O.
ft
64
J5
87
98
49
ENGINE
SPEED
RPM
Nl
1885.00
5600.00
5960.00
6270.00
6690.00
5220.00
N2
5550.00
9210.00
9440.00
9640.no
9940.00
fl980.no
MEASURED
FUEL
FLOW
LB/HR
9.50
5770.00
6910.00
8050.00
9720.00
4715.00
GAS GEN
AIR FLOh
L8/SEC
12.52
143.05
159.98
173.35
IS6.25
127.22
CALC COMPRESSOR
F/A DISCHARGE
TFMP
0.007600
0.010910
0.011720
0.012610
0.014170
0.010030
OfGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
FNGINF
PRESSURE
RATIC
EPR
1.02
1.44
1.56
1.49
1.84
1.34
IURB1NF
INLET
TFMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.'l.
75
87
EXHAUST
r.AI
TEMP
555.00
755.00
805.00
860.00
960.00
705.00
EXHAUST
GAS
PRESSURE
PSI A
15.12
20.89
77. 59
24.30
?6. 50
19.47
CO
IHET)
PP«V
387.10
31.20
20.70
14.°0
10.90
4 9 . > 0
CO
2
IriETI
XERCFNT V
1.1?
2.?3
2. SO
2.75
1. 13
2. OB
THC
IUETI
PPMV
1241.20
4. 10
4.00
'1.50
1.40
6.20
Nil
IIP!)
PPMV
4.80
51.10
67.70
"4.50
1 IR.50
39. 7C
NO
2
(UFTI
PPMV
0.0
6.60
6.20
5.30
4.30
6.50
NO
X
IKFTI
PPMV
4.80
57.70
73.90
89. 80
122. BO
46.20
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
14.00
39.00
43.00
40.00
36.00
17.00
"ARTICULATES
-0.00
-0.00
2ft.CO
22.00
20.00
-n.oo
POWER
PERCENT
RATED
T.O.
64
75
87
9B
49
MASS FMI
CO
LB/1K
LI FUEL
1 15.57
2.79
1.6'J
I.T7
0.70
4.7H
MASS i"\
HC
LB/1K
L(l FUEL
92.61
0.71
C.18
0. 15
0.17
n. 14
MASS EMI
rill?
LI/IK
LD FUEL
0.0
0.97
O.R1
0.61
T.45
1.0?
MASS FMI
C02
Lrt/lK
LO FIIFL
2702.08
3137. 79
31 14.65
1135.66
3116. 11
3129. 1C
MASS EMI
Nil
LB/IK
LP FUEL
1.0?
7.50
h . h7
10.07
1 2 . '. 1
6. ?4
MASS LM1
NUX
Lfl/IK
LB FUFL
1 .03
f .47
9.69
10.70
12.86
7.27
"ASS KMI
cn
LU/HR
1.10
16.10
11.41
8.65
6.76
22.53
MASS F.PI
HC
LB/HR
0.88
1.21
1.26
1.17
1.21
1.60
MASS FMI
NO?
LR/HP
0.0
5.59
5.62
5.09
4.38
4.8?
MASS FMI
CO?
Lfl/HR
25.67
18076.18
21660.41
?5242.04
30484.95
14754.66
MASS E"l
NO
LP/HP
0.01
43.30
61.3?
81.08
170.65
?9. 44
MASS EMI
NO*
LB/HR
0.01
48.89
66.93
86.17
125.03
34.76
POWER
PERCENT
RATFD
T.O.
75
87
98
I .777
1 . 1B5
0.8 36
0.552
0. 383
2.531
L8/IK1TH-H<
29.348
1554.940
1585.6H1
1610.646
I 776.900
1657.828
THC
LB/lKKTIi-HR
1.023
0. 104
0.092
0.075
0.063
0. 180
C.C1 1
1.7? 5
4 . 4 8 'V
b.174
6.035
3.108
LB/ 1MTH-HR
0.0
0.481
0.411
0.325
0.248
0.542
NT
X
LB/1KH1H-HR
0.011
4.206
4.900
5.498
1.083
3.849
IV-122
-------
CAL 10 NUMBER: 32s ENGINE TYPE AND MODEL: JTSD -38
TEST ORGANIZATION: PRATT c WHITNEY
SERIAL NUMBER I
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.650
0.400
0.050
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
TH
900.0
16000.0
15300.0
7200.0
900.0
POWER
1 TH
900.0
leooo.o
15300.0
7200.0
900.0
POWER
TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
22.788 205.820
9.J79 9927.949
12.702 7946.1 BO
31.830 3318.823
22.788 205. 820
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
20.779 205.820
1.468 9927.949
2.655 7946.180
6. 408 3318.823
20.779 205.820
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
0.589 205.820
132.810 9927.949
86.100 7946.180
20.6B5 3318.823
0.589 205.820
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
7.216
0.109
0.466
2.122
2.659
12.572
17.518
7.661
0.608
HC
MASS
LBS.
6.580
0.017
0.097
0.427
2.424
9.546
13.302
5.817
0.952
NOX
MASS
LBS.
0.186
1.549
3.157
1.3T9
0.069
6.341
8.635
3.864
86.080
FUEL
MASS
LBS.
65.18
115.63
291.36
221.25
24.01
717.63
FUEL
MASS
LBS.
65.18
115.83
291.36
221.25
24.01
717.63
FUEL
MASS
LBS.
65.18
115.83
291.36
221.25
24.01
717.63
LB CO /
IK LB FUEL
110.716
0.945
1.599
9.591
110.716
LB HC /
IK LB FUEL
100.959
0.148
0.334
1.931
100.959
LB NOX/
IK LB FUEL
2. 860
13.377
10.835
6.233
2.860
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
4BO.OO
105.00
1641.00
ENERGY
TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
LB CO /
1 TH-HR
0.02532
0.00052
0.00083
0.00442
0.02532
LB HC /
TH-HR
0.02309
0.00006
0.00017
O.OOOB9
0.02309
LB NOX/
TH-HR
0.00065
0.00738
0.00563
0.00267
0.00065
IV-123
-------
DATE: 7/21/71
TEST ORGANIZATION: PRATT C WHITNEY
ENGINE- SUPPLIER: PRATT AND WHITNEY
ENGINE DATA
CAL ID NUMBER: 379 ENGINF TYPE AND MODLL: JTID -IB
RATFO THUUST: isooo.
FNGINF TOTAL TIME: -0. HRS
TINF SINCE HOT SFCTIIIN OVERHAUL: -0. HRS
TIME SINCE:
SERIAL NUMRFR:
NI COMPRESSOR OVERHAUL: -0. MRS
N2 COMPRESSOR OVERHAUL: -o. HRS
CdMBUSTCR CAN REPLACEMENT: -0. HRS
FIRST STAGE HO I Lit GUIDE VANE OVERHAUL: -0 . HRS
Nl TURBINE OVERHAUL: -0. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL: jp-4 FUEL H/C RATIO: 7.000
OPERATIONAL DATA «»«»*«»«««««««««
INLET AIR TEMPERATURE. DEGREES F: START 68.00 FINISH 78.00
ATMOSPHERIC PRESSURE: START 30.00 FINISH 29.20
INLET AIR HUMIDITY, LBS H20/LH AIR: 0.0010
RELATIVE HUMI'lirv: -0.00 PEPCFNT
SAMPLE LINE: TEMPERATURE, DEGREES C: ISO.OC, FLOW RATE, LITERS/MI\:
SAMPLE LINE TRANSPORT TIME, S FC : 1.00
NUMBER OF TESTS: H
COMMENTS:
SMUKE DENSIIY IS VON RRAND MfASURF. PARMCULATFS AWE IN MG/M**1
CLOCK
TIME
975.00
139.00
1070.00
1252.00
1315.00
US').00
1148.00
1405.00
TFST
(ODE
I/ 0
2/ I
3/ 2
4/ I
5/ 4
6/ 5
'/&
8/ 7
PllwER
THRUST, L8S
OR
SHP
850.00
5535.00
880.00
9669.00
1 1717. .00
13774.00
15651.00
I7t>53.00
PERCENT
KATFO
T .0.
4
30
4
51
65
76
86
98
ENGINE
SPEED
Iff
1950.00 5440.00
MEASURED
FUEL
FLOW
LP/HR
inflO.OO
GAS GEN
AIR FLOW
Lb/SEC
CALC
F/A
30
4
51
65
76
86
98
4195.00
IS75.00
5220.00
5610.00
5940.00
(J^O.OO
66 fan.
2655.71
1 104 .40
27C5.JO
)1>H.11
1132. 3H
31 14.53
11 J5.ll
1135.81
MASS E'U
MO
LII/1K.
LH FUIL
C. H f
1.51,
C. 75
6.05
V. 17
11.03
1 (1.40
13.85
MASS h 1 1
NCJX
LB/1K
1 » FUEL
1.51
3.95
.91
.58
.54
.bO
1 . ft 1
1 .01
MASS EMI
C.I)
LR/HU
175.41
49.71
104. 7B
26. 14
18.92
13.30
I i.ns
8. /9
MASS CMI
HC
LB/hP
114. in
6.76
89.78
1.20
0.5H
0.4-',
0.7(.
I.KM
MASS EM
NO?
LB/HR
0. 71
4.50
1 .1 1
7.29
8.01
10.16
9. 70
11 .57
"ASS EMI
CO 2
LR/HP
23ff.45
H925.15
2569. ')tt
14843.91
18277.41
21531.27
25219.39
30793.69
Nn
Lfi/HK
0.94
10.21
0. 72
7 H. 68
41 .8?
55.28
81. 74
MASS EMI
Nil"
Lb/HR
1 .65
I 1.35
1.8
35.9
49. fi
65.4
91.4
147.55
POWER
PERCENT
BATED
T.O.
53
65
76
86
98
r.o
LO / I K » IH-HV
147.562
8. H90
1 ii.n'.s
7. 7?7
1.616
0.969
C.706
0.49H
LB/ IK* TH-HH
3386.408
1617.494
7920. 183
1516.790
1560.571
1572.520
1612.637
1744.390
THC
LfVIK * TM-MB
114.310
1.72?
102.019
0. 124
0.050
0.012
0. C49
0.106
1. 10H
I .848
C.814
7.97J
3.571
4 ,n?8
5.351
7.701
0.838
0.81?
I. ?dft
0.755
0.684
0. 740
0.620
0.655
NO
X
LO/IKflTH-HR
1.946
2.051
2.081
3.724
4.255
4 . 768
5.970
8.159
IV-124
-------
CM 10 NUMBER: 329 ENGINE TYPE AND MODEL: JI3D -38
TEST ORGANIZATION: PRATT t WHITNEY
SERIAL NUMBER: P66sei7
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.050
1.000
o.sso
0.400
0.050
POWER
1 TH
900.
1BOOO.
19300.
7200.
900.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
80.545 874.719
14.233 9995. 387
17.440 7907.129
41.745 3775.425
80.545 8T4.7I9
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
TH
900.
18000.
15300.
7200.
900.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
84.342 874.719
4.178 9995.387
3.305 7907.129
6.730 3775.425
84.342 874.719
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
HOOE
FRACTIONAL
POWER
TAXI-IOLE 0.050
TAKEOFF 1.000
CLIMBOUT 0.8SO
APPROACH 0.400
TAXI-IDLE 0.050
POWER
I TH
900.
IBOOO.
15300.
7200.
900.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.560 874.719
159.271 9995.387
91.570 7907.129
19.308 3775.425
1.560 874.719
WT
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE 2
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIKE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
CO
MASS
LBS.
25.506
0.166
0.639
2.916
9.397
38.624
37.236
23.537
0.923
HC
MASS
LBS.
26.708
0.049
0.121
0.449
9.840
37.167
35.831
22.649
2.708
NOX
MASS
LBS.
0.494
1.858
3.358
1.287
0.182
7.179
6.921
4.375
103.231
FUEL
MASS
LBS.
276.99
116.61
289.93
251.69
102.05
1037.28
FUEL
MASS
LBS.
276.99
116.61
289.93
251.69
102.05
1037.28
FUEL
MASS
LBS.
276.99
116.61
289.93
251.69
102.05
1037.28
LB CO /
IK LB FUEL
92.081
1.424
2.206
11.587
92.081
LB HC /
IK LB FUEL
96.422
0.418
0.418
1.782
96.422
LB NOX/
IX LB FUEL
1.784
15.934
11.581
5.114
1.784
ENERGY
TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
f TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
L8 CO /
1 TH-HR
0.08949
0.00079
0.00114
0.0060B
0.08949
LB HC /
* TH-HR
0.09371
0.00023
0.00022
0.00093
0.09371
LB NOX/
TH-HR
0.00173
0.00885
0.00598
0.00268
0.00173
IV-125
-------
DATE; a/ 5/71
TEST ORGANIZATION: S W R [ TWA
ENGINE SUPPLIER: T n A
FNGINF DATA
CAL ID NUMRER: 331
ENGINE TYPE AND MODEL: JI3D -3B
SERIAL NUMBER: P643434B
RATFO THRUST:
ENGINE TOTAL TIME:
TINE SINCE HPT SECTION OVERHAUL:
TIME SINCE:
laono.
16564. MRS
1654*. MRS
16564. MRS
16564. MRS
7694. MRS
Nl CCMPPFSSOP OVERHAUL:
N? COMPRESSOR OVERHAUL:
COMBUSTIIR CAN REPLACEMENT:
FIRST STAGE NOZZLE GUIDE VANC OVERHAUL: 16564. HRS
NI TURRINF OVERHAUL: 16564. HRS
N2 TURBINC OVERHAUL: 16564. HRS
FUEL: jp-4 TF FUEL H/C RATIO: i.7z?
OPERATIONAL DATA »»«>«««««»
INLET AIR TEMPERATURE, DEGREES F: START 77.00 FINISH 77.00
ATMOSPHERIC PRESSURE: START 29.14 FINISH 29.12
INLET AIR HUMIDITY, LBS H20/LR AIR: 0.0139
RELATIVE HUMIDITY: 63.00 PERCENT
SAMPLE LINE: TFMPERATIIRF, HEGRFES C: 150.OC, FLOW RATE, LITFRS/MIN:
SAMPLE LINE T1ANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 9
COMMENTS:
NO? DETERMINED RV SUBTRACTION.
ELAPSFO
TIMF
0.0
4.00
6.00
10.00
I3.no
16.00
19.00
22.00
24.00
TEST
MODE
6/ 0
I/ 6
2/ 1
I/ 7
4/ 1
5/ 4
7/ 5
V I
=>/ 8
POUFH
THBUST.LRS
on
SHO
8820.00
1 1040.00
13310.00
15410.00
950.00
15410.00
7040.00
5000.00
2950.00
PFRCFNT
RATFI)
T.O.
48
61
73
85
5
85
39
27
16
ENGINE
SPEFD
HPM
Nl N?
MEASURED
FUFL
FLOW
LB/HR
GAS GEN
AIR FLOU
L9/SEC
CALC
F/A
48
61
73
85
5
85
39
27
16
5460.00
5840.00
6250.00
6660.00
7050.00
6640.00
5000.00
4180.00
3490.00
9170.00
9410.00
9680.00
9970.00
5870.00
9910.00
8900.00
8480.00
7fl20.nO
5120.00
6320. nn
7800.00
9490.00
980.00
6540.00
4C5C.OO
7980.00
1990.00
124.40
141.70
158.90
173.20
30.60
173.20
110.00
89.00
63.70
0.01 1400
O.C12400
0.013300
O.CI5200
0.008000
0.015300
0.010700
0.009300
0.008700
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
FPR
1.38
1.50
1.66
1.84
-0.00
-0.00
-0.00
-0.00
-0.00
TUPRINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-o.no
-o.oo
POWER
PFRCENT
RATED
T.O.
48
61
73
85
5
85
39
77
16
EXHAUST
GAS
TFMP
DECREES F
747.nO
806. V,
874.00
957.00
557.00
964.00
667.On
639.nn
594.00
EXHAUST
GAS
PRFSSURF
I'SIA
5.00
(,.50
B.60
10.90
0.30
11.00
2.20
2.70
I. 10
CO
IwFTI
PPMV
43.00
76.00
19.00
34. OC
675.00
7.5.00
65.00
92.00
2'.?. 00
cn
2
(WET)
PFRCENT V
2.14
2.52
7.70
.98
.57
.04
.10
.91
. 79
THC
(VIET)
PPMV
50.00
18.00
26. on
24.00
1060.00
P.7.00
50.00
44.00
I 04.00
NO
(NET)
PPMV
35.00
4K .00
64.00
86.cn
2.00
81 .00
30.00
77.00
14.00
NC
2
IWFTI
PPMV
4.00
7.00
2.00
3.00
7.00
2.00
1.00
1.00
2.00
ALDEHYDES SMOKE PAPTICULATES
i UEM
PPMV
39.00
50.00
66.00
91.00
9.00
33.00
31.on
73.00
16.00
-n.nn
-o.oo
-o.oo
-o.oo
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
-0.00
-0.00
-o.no
-o.oo
-0.00
-c.oo
-o.oc
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PUMFR
PFRCFNT
RATF.D
T .0.
48
61
73
85
5
85
39
27
MASS FMI
CU
3.7*
2.10
1 .43
2.3.'
73.26
1.67
6.27
9.75
27.03
IASS f\
HC
LB/IK
LP FUEL
2.48
1 . 76
1 . 12
0.94
71.16
1 .03
2. 76
2.67
6.65
MAS; FMI
MT2
LI/ lit.
L" FUFL
0.57
0.26
0.75
1.34
1.15
0.2?
0.16
3.17
0. <7
MASS tMI
T.P2
LH/ IK
LU FUEL
3189.04
3193.60
3196.18
3195.49
7891. 39
3196.24
3184.27
3179.08
3141.00
MASS EMI
NO
LIU1K
LR FUF.I.
4.99
6. 36
7.92
9.86
C.39
H. "0
4 . 76
3.H3
2.67
'.ASS FMI
NOX
LG/1K
LR FUFL
5.56
5.62
8.17
10.20
1.73
9. 12
4.91
4.00
2.94
MASS F.M|
CO
I K/HH
19. 10
1 3.25
11.17
77.02
71.79
10.94
25.41
29.04
53.78
MASS EMI
HC
LB/HC
12.72
11.09
6.75
9.90
69.73
6.77
11.19
7.96
13.74
MASS FMI
N07
Lfl/HP
2.92
1.67
1.91
3. 19
1 .32
1.44
C.64
0.52
0.73
MASS F-l
C'J7
LR/HR
16177.87
70183.55
74911. ;(
30325.21
2831.56
20903.4 J
12896.31
9473.64
6250.58
MASS FMI MASS F"l
NO ^OX
LP/HP LH/HR
7.5.53 28.45
4C.19
61.78
93.62
C.lt
51.23
19.26
1.66
3.71
6.81
1.70
9.66
9.90
11.41 II .91
5.11 5.84
POWFR
PERCENT
RATED
T.O.
43
61
73
39
27
16
r.n
LR/ IK, It TH-HP
2.165
1.201
0. 839
1 .429
71.570
0.710
3.609
5.808
1(1.237
10/IS«TH-H»
1651.21.3
1828.220
1873.162
1967.892
1356.4B5
1831 .862
1894.729
2119.P42
THC
L 6/ KH TH-Htt
1.442
I .105
(1.657
0.578
73.405
n. 439
1 . 590
1 .591
4.487
IH/1KKTH-HR
7.P95
3.640
4.647
6.075
0.397
3.778
2.736
2.781
1 .73?
LO/IMTH-HP
0.131
C. 15?
0.145
0.707
I. 390
0.093
0.091
0.104
0.747
NO
X
LR/IK« TH-MH
3.275
3.792
4.757
6.282
I .787
3.872
2.877
2.385
1.990
IV-126
-------
CAL 10 NUMBERl 331 ENGINE TYPE 1ND MODEL: JT3D -38
TEST ORGANIZATION: S W R I TWA
SERIAL NUMBER! P643434B
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAKI-IOLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBOJT
APPROACH
TAXI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.890
0.400
0.050
FRACTIONAL
POWER
O.OSO
1.000
0.850
0.400
O.OSO
FRACTIONAL
POWER
O.OSO
1.000
0.850
0.400
0.050
POWER
TH
900.0
18000.0
15300.0
T200.0
900.0
POWER
1 TH
900.0
18000.0
15300.0
7200.0
900.0
POWER
1 TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
62.882 831.320
19.945 11339.656
13.575 9236.012
25.659 4184.395
62.882 831.320
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LR/HR LB/HR
61.345 831.320
11.310 11339.656
11.176 9236.012
14.401 4184.395
61.345 831.320
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
1.201 831.320
135.739 11339.656
86.023 9236.012
19.821 4184.395
1.201 831.320
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
USAGE TIME IN
FACTOR MODE
HIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TINE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
HIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
19.913
0.233
0.498
1.711
7.336
29.690
26.744
18.093
1.293
HC
MASS
LBS.
19.426
0.132
0.410
0.960
7.157
28.085
25.298
17.114
7.330
NOX
MASS
LBS.
0.380
1.584
3.154
1.321
0.140
6.580
5.927
4.010
87.979
FUEL
MASS
LBS.
263.2S
132.30
338.65
278.96
96.99
1110.15
FUEL
MASS
LBS.
263.25
132.30
338.65
278.96
96.99
1110.15
FUEL
MASS
LBS.
263.25
132.30
338.65
278.96
96.99
1110.15
LB CO /
IK LB FUEL
7S.642
1.759
1.470
6.132
75.642
LB HC /
IK LB FUEL
73.793
0.997
1.210
3.442
73.793
LB NOX/
IK LB FUEL
1.445
11.970
9.314
4.737
1.445
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
LB CO /
1 TH-HR
0.06987
0.00111
O.OOOB9
0.00356
0.06987
LB HC /
1 TH-HR
0.06816
0.00063
0.00073
0.00200
0.06816
LB NOX/
TH-HR
0.00133
0.00754
0.00562
0.00275
0.00133
IV-127
-------
DATE: 8/ 4/71
resr ORGANI/AIION: u.s. HUKEAU OF MINES
ENGINE SUPPLIER: AMERICAN AIRLINES
ENGINE DATA
CAL ID NUMBFB: 337
ENGINE TYPF AND MODEL: JT3D -3B
SERIAL NUMBER: 645)61
RATED IHRUSI: 18000.
ENGINE TOML TIME: 12283. H9 S
II"E SINCF HOT SFCTION OVERHAUL: 1968. HRS
HUE SINCE:
Nl COMPRESSOR OVERHAUL: 1468. HR S
nz COMPRESS OVERHAUL: 1968. MRS
COMBUSTOR CAN REPLACEMENT: I960. HBS
FIRSt STAGE NIHUE GUIDE VANF OVERHAUL: 1968. MRS
NI TURBINE OVERHAUL: 1968. HRS
N2 TURBINE OVFPHAUL: I96B. HRS
FUEL M/C RATIO: 1.920
90.00
79.08
FUEL: JET - A
OPERATIONAL DATA ««»««
INLET AIR TEMPERATURE, DEGREES F: START 85.00 FINISH
ATMOSPHFRIC PRESSURE: START 29.08 FINISH
INLET AIR HUMIDITY, LBS H20/LH AIR: 0.0130
RELATIVE HUMIDITY: 42.00 PERCENT
SAMP1E LINE: TMPFOATU°F, C5GRFES C: 138.00, FLOy RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.99
NUMBER OF TESTS: 6
COMMENTS:
H/C CAL ESTIMATED
SAMPLE LINE TEMP. AVcRAfEO
PRO.I3F CONFIG. ANP LOCATION SAME AS USED FOR SPFY ON 01-02-71
CLOCK TEST POWER
TIMF MOTE THRUST.LBS PERCENT
OR RAItO
SHP T.O.
(.00.00 4/ 0 920.00
60S.00 I/ 4 10851.01
610.00 21 1 13450.00
630.00 5/ 7 10600.00
635.00 "./ 5 790.00
045.00 3/ 4 I'SflOO.OO
ENGINE MEASURED GAS GEN CALC
SPEFO FUEL AIR FLOW F/A
RPM FLOW LU/SEC
Nl N2 LR/HR
5
60
74
5fl
4
87
2020.00
5760.00
6190.00
5710.00
18'iO.OC
370C.OO
5790.00
9360.00
9660.00
9320.00
5460.00
9970.00
1I2C.OO
6020.00
7390.00
5850.00
P90.CO
"270.00
-0.00
157.00
175.00
155.00
-0.00
-0.10
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRFSSURF
PATIO
EPR
1.02
1.47
1.62
1.45
1.02
1 .04
TUR8INE
INLET
TEMP
DFGRFFS F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POHER
PFP.CFNT
60
74
EXHA1ISI
CtS
8 I S . 0"
flS'j.OO
970.00
145.00
3 ? 5 . 00
1030. 01
EXHAUST
GAS
14.63
20.26
22.2 7
20.07
14.63
20.07
855.00
28. (0
21 .30
31.20
765.10
20.00
CO
2
IrfETI
t>ftr.F.m v
1.33
7.35
2.65
2.35
1.29
THC
(UFTI
PPMV
1941.00
6.30
6.30
6.00
1 87b.OO
NO
(UEII
PPMV
0.30
46. PO
42.20
45.10
2.30
NO
2
IUETI
PPMV
6.56
17.00
18.01
23.00
10.10
ALOEHYOES S.MOHF PARTICULATES
-0.no
-C.OO
-0.00
-0.00
-o.on
-0.00
IUET)
PPMV
6.80
63. BO
60.20
68. 10
12.30
125.70
-0.00
0.62
0.51
0.39
40. 70
0.46
-0.00
-0.00
-0.00
-0.00
-0.00
-O.OG
PUUFR
PERCENT
RATFD
T.O.
5
60
7',
58
4
87
MASS FMI
CO
LB/1K
LB FUEL
106.69
2.45
1 .61
2. 66
9B.86
1 .34
MASS FMI
HC
LB/U
LP HJFL
1 18. 72
0.31
0 . 7 1
0.70
138.99
0.32
M4SS FMI
N-17
LVU
LD FUFL
1.34
2. 31
2.74
1.72
7.12
2.70
MASS fMI
C02
LB/1K
LR FUEL
2617.69
1 1 5 1 . 2 C
3152.61
3I5C.9G
7619.75
3157.92
"ASS FMI
NO
IP/IK
LP TUEL
0.06
6. 56
5.26
6.37
0. 49
11.16
MASS FMI
NC'X
LB/IK
LB FIJFL
1 .31
fl.04
7.49
9.55
7.61
13. P6
MASS E-l
CU
LE/HR
1 19.50
14.75
1 1.92
15.58
rt 7 .48
12.44
MASS EMI
HC
LB/HP
155.37
I.H5
2.02
1.72
123.70
2.92
MASS rm
Nl?2
LB/HP
1.61
14.35
16.54
18.80
1.89
25.04
MAIS EMI
CT2
L1/H3
2920.61
18970.20
23297. 76
18432. 77
2331.13
29227. S7
MASS E"I
NO
LB/HR
1.07
39. 49
3ft. 7S
36. 9h
0.43
ini.4l
MASS f'l
NTX
LB/HR
1 .66
53.84
55.31
55. B4
2.32
170. 4S
POWER
PERCFNT
RAT En
T.O.
5
60
74
58
CO
LP / IK KTH-HH
129..186
I .359
O.H86
I .469
111.371
0. 71B
31 74.576
1748.405
1732.175
1738.941
2950.30C
1849.643
THC
LB/lKrfTH-HO
168.R76
n. I 71
0. 150
0. 162
I 51. .5 SO
0. 185
LH/l'iTH-HD
O.C75
3.640
7.EB4
3.489
0.550
6.545
LB/ 1KMH-HR
1.637
1.322
1.230
I . 7Tt*
2.391
1 .5.85
NO
X
LB/IK1TH-HR
I .697
4.962
4 . I I',
5.269
7.941
8.130
IV-128
-------
CAL ID NUMBER: 337 ENGINE TYPE AND MODEL: JI3D -38
TEST ORGANIZATION: U.S. BUREAU OF NINES
SERIAL NUNBERI 645361
MODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
0.050
1.000
0.850
0.400
0.050
NODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
0.050
1.000
0.850
0.400
0.050
MODE FRACTIONAL
POWER
TAX1-10LE
TAKEOFF
CLIMBDUT
APPROACH
TAXI-IDLE
0.050
1.000
0.850
0.400
0.050
POMER
TH
900.0
18000.0
15300.0
7200.0
900.0
POWER
1 TH
900.0
18000.0
15300.0
7200.0
900.0
POWER
1 TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
102.025 927.499
2.558 10945.402
11.408 9018.008
46.814 4275.543
102.025 927.499
TOTAL FOR CYCLE:
L8S POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
129.850 927.499
0.0 10945.402
0.0 9018.008
18.501 4275.543
129.850 927.499
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
2.003 927.499
167.596 10945.402
112.112 9018.008
24.920 4275.543
2.003 927.499
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.I
USAGE TINE IN
FACTOR MODE
MIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TINE IN
FACTOR NODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE;
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
32.308
0.030
0.418
3.121
11.903
47.780
41.718
29.116
0.166
HC
MASS
LBS.
41.119
0.0
0.0
1.233
15.149
57.502
50.206
35.041
0.0
NOX
MASS
LBS.
0.634
1.955
4.111
1.661
0.234
8.596
7.505
5.238
108.627
FUEL
MASS
LBS.
293.71
127.70
330.66
285.04
108.21
1145.31
FUEL
MASS
LBS.
293.71
127.70
330.66
285.04
108.21
1145.31
FUEL
MASS
LBS.
293.71
127.70
330.66
285.04
108.21
1145.31
LB CO /
IK LB FUEL
110.000
0.234
1.265
10.949
110.000
LB HC /
IK LB FUEL
140.000
0.0
0.0
4.327
140.000
LB NOX/
IK LB FUEL
2.160
15.312
12.432
5.829
2.160
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
10%. 00
1641.00
ENERGY
TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
LB CO /
1 TH-HR
0.11336
0.00014
0.00075
0.00650
0.11336
LB HC /
TH-HR
0.14428
0.0
0.0
0.00257
0.14428
LB NOX/
TH-HR
0.00223
0.00931
0.00733
0.00346
0.00223
IV-129
-------
DATE: 8/ii/Ti
TEST ORGANIZATION: S « R
ENGINE SUPPLIER: TWA
ENGINE DATA
CAL ID NUMBER: 140
FNr.lNE TYPE AND HODFL: JT1D -3B
SERIAL NUMBER: IT«A2537(
RATED THRUST: 18000.
ENGINE TOTAL TIME: 17559. HRS
TIKE SINCE MfH SECTION OVERHAUL: 0. HRS
TINE SINCE:
Nl COMPRESSOR OVERHAUL: 17359. HRS
N2 COMPRESSOR OVERHAUL: 17359. HRS
CONBUSTOR CAN REPLACEMENT: 17359. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 17359. MRS
Nl TURBINE OVERHAUL: 17359. HRS
N2 TURBINE OVERHAUL: 17359. HRS
FUFL H/C RATIO: 2.020
S3.00
2B.96
FUEL: jp-4 TF
OPERATIONAL DATA ««..«..........«.«.......................
INLET AIR TEMPERATURE, DEGREES F: START 81.00 FINISH
ATMOSPHERIC PRESSURE: START 28.96 FINISH
INLET AIR HUMIDIFY, LBS H20/LB AIR: 0.0137
RELATIVE HUMIDITY: 49.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIMF, SEC: 1.00
NUMBER OF TESTS: 12
COMMENTS:
NO? DETERMINED BY SUBTRACTION. MAINTENANCE DATA ARE NOT LOGICAL, HUT ARE
LISTED AS GIVEN «Y TWA.
42.50
ELAPSED
TIME
0.0
7.00
16.00
47.00
52.00
57.00
59.30
62.00
64.00
67.00
69.30
74.00
POWER
PERCENT
RATED
1.0.
49
60
72
84
4
6
8
Q
11
13
22
18
POWER
PERCENT
RATED
T.Q.
44
60
72
84
4
6
8
9
11
13
22
38
POWER
PERCENT
RATED
T.O.
49
60
72
84
4
6
8
9
11
1 3
22
18
TEST
MOOf
6/ 0
It (.
2/ 1
J/ >
4/ 1
T/ 4
8/ 7
4/ P
IO/ 4
11/10
12/11
11/12
EXHAUST
GAS
TFMP
DEGREES f
765.00
815.00
883.00
997.00
572.00
574.00
5H3.00
590.00
599.00
617.00
622.00
700.00
MASS EMI
CO
LB/U
L« FUFL
3.4i
? . 19
1 .45
1.6?
77.84
63. 60
57.50
53. 2H
47.41
17.95
16.44
6.20
cn
POWER ENGINE MEASURED GAS GEN CALC
THRUST, LBS PERCFNT SPEED FUEL AIR FLOW F/A
OR RATED RPM FLCW LB/SEC
SHP T.O. Nl N2 LB/HR
8930.00 49 5470.00 9770.00 5100.00 124.00 0.011400
IOB60.00 60 5850.00 9480.00 6310.00 139.20 0.012600
13000.00 72 6230.00 9770.00 7590.00 154.40 0.013700
15280.00 84 6670.00 10040.00 9440.00 171.10 0.015300
880.00 4 1740.00 5790.00 900.00 29.40 O.OOB500
1240.00 6 2330.00 6470.00 1200.00 36.00 0.009300
1500.00 8 2550.00 6770.00 1340.00 47.70 0.009100
1750.00 9 2750.00 7070.00 1470.00 44.50 0.009200
2000.00 11 7920. OC 7000.00 1590. CO 48.30 0.009100
2500.00 13 3220.00 76BO.OO 1840.00 55.90 0.009100
4000.00 22 3980.00 8210.00 2470.00 72.00 0.009500
7000.00 38 5020.00 8920.00 4090.00 108.90 0.010400
EXHAUST CO CO THC NO NO NO
GAS IWETI 2 IWCT) IWETI 2 X
PRESSURE PPMV (WFTI PPMV PPMV
-------
CAL ID NUMBER) 3*0 ENCINE TYPE AND MODEL: JT3D -IB
TEST ORGANIZATION: S U R I TWA
SERIAL NUMBERl ITHA253T)
NODE FRACTIONAL
POWER
TAXI-IOLE
TAKEOFF
CLIHBOUt
APPROACH
TAXI-IOLE
0.050
1.000
0.850
0.400
0.050
HDDE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLlMBflUT
APPROACH
TAXI-IOLE
0.050
1.000
0.890
0.400
0.050
HODE FRACTIONAL
POWER
TAXI-IOLE
TAKERFF
CLIHBOUT
APPROACH
TAXI-IDLE
0.050
1.000
o.eso
0.400
o.oso
POWER
1 TH
900.0
18000.0
15300.0
7200.0
900.0
POWER
1 TH
900.0
18000.0
15300.0
7200.0
900.0
POWER
TH
900.0
18000.0
15300.0
T200.0
900.0
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR NODE
LB/HR LB/HR NIN.
71.805 842.784 1
18.151 11409.559 1
16.321 9444.996 1
32.603 4547.926 1
71.805 842.784 1
TOTAL FOR CYCLE*
LBS PCLLUTANT/1K LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLEI
LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
50.567 842.784
3.828 11404.559
11.212 9444.996
16.660 4547.926
50.567 B42.784
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.l
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
1.259 842.784
146.407 11409.559
95.080 9444.996
24. MB 4547.926
1.259 842.784
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
22.738
0.212
0.598
2.174
8.377
34.099
29.708
20.780
1.176
MC
MASS
LBS.
16.013
0.045
0.411
I. Ill
5. 899
23.479
20.455
14.308
2.4B1
MIX
MASS
LBS.
0.399
1.708
3.486
1.608
0.147
7.348
6.401
4.478
94.894
FUEL
MASS
LBS.
266.88
133.11
346.32
303.19
98.32
1147.83
FUEL
MASS
LBS.
266.88
133.11
346.32
303.19
98.32
1147.83
FUEL
MASS
LBS.
266.88
133.11
346.32
303.14
98.32
1147.83
LB CO /
IK LB FUEL
85.200
1.591
1.728
7.169
85.200
LB HC /
1« LB FUEL
60.000
0.335
1.187
3.663
60.000
LB NOX/
IK LB FUEL
1.493
12.832
10.067
5.303
1.493
ENERGY
< TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
f TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
LB CO /
TH-HR
0.07978
0.00101
0.00107
0.00453
0.07978
LB HC /
TH-HR
0.05619
0.00021
0.00073
0.00231
0.05619
LB NOX/
TH-HR
0.00140
0.00813
0.00621
0.00335
0.00140
IV-131
-------
DATE: 8/19/71
TEST ORGANIZATION: PRATT I WHITNEY
ENGINE SUPPLIED: PRATT AND WHITNEY
ENGINE DATA «
CAL ID NUMBER: 358
ENGINE TVPE AND MOOEL: JT30 -3B
SERIAL NUMBER:
RATED THRUST: 16000.
ENGINE TOTAL TIME: -0. HRS
TIME SINCE HOT SECTION OVERHAUL: -0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: -o. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
N2 TURBINE OVERHAUL: -o. HRS
FUFL: jp-4 FUEL H/C RATIO: 2.000
OPERATIONAL DATA «»»
INLET AIR TEMPERATURE, DEGREES F: START 74.00 FINISH 79.00
ATMOSPHERIC PRESSURE: START 29.75 FINISH 29.15
INLET AIR HUMIDITY, LBS H20/L3 AIR: 0.0133
RFLATIVE HUMIOITY: -0.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITfS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 7
COMMENTS:
CLOCK
T1MF
1208.00
1029.00
1259. OC
1IOH.OO
1320.00
1131.00
1140.00
TEST
MOOE
I/ 0
21 1
3/ 2
4/ 1
5/ 4
6/ 5
7/ IS
POWER
THRUST, LBS PERCENT
OR RATED
SHP
5000.00
840.00
8900.00
IOBOO.OO
12750.00
[if, 00. 00
16400.00
r.o.
27
4
49
59
70
81
91
ENGINE
SPEED
HPM
NI
4IS5.0C
1655.00
5215.00
5600.00
5970.00
6290.00
6690.00
N2
6245.00
54 80. 00
B960.00
9160.00
9420.00
9650.00
9930.00
MEASURED
FUEL
FLOW
L8/HP
2736.00
938.00
4574.00
5606.00
6747.00
7882.00
9397.00
GAS GEN
AIR FLOW
Lfl/SEC
91.41
29.11
127.46
143.97
160.04
173.42
1X5.74
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.006310
0.008950
0.009970
0.010670
0.011710
0.012630
0.014150
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.16
1.02
1.34
1.45
1.57
1.69
1.84
TURBINE
INLET
TEMP
nEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWF.R
PFRCENT
RATED
1.0.
77
4
49
59
70
Bl
91
EXHAUST
GAS
TbMP
DEGREES F
610.00
555.00
700.00
750.00
805.00
865.00
955.10
EXHAUST
GAS
PRESSURE
PSIA
17.00
15.07
19.44
20.91
22.57
24.33
26.38
CO
IWET)
PPMV
155.70
908.60
(.0.10
38.80
20.70
1 7.40
9.10
CO
2
UCTI
PERCENT V
1.80
1.27
2.19
2.21
2.32
2.75
2.85
TMC
(WET)
PPHV
19.70
512.20
1.50
1 .90
0.2C
1.80
3.70
NO
IKED
PPMV
IB. 40
4.60
36.3(1
40.80
60. 10
73.70
112.10
NO
2
(UET)
PPMV
13.40
4.90
3.20
2.90
0.40
1.40
0.60
NO
X
IHFTI
PPMV
31.80
9.50
39.50
43.70
60.50
75. 10
112.70
ALDEHYDES SMOKE PflRTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
POWER
PERCF.NT
RATFn
T.O.
27
70
81
91
MASS EMI
en
L8/IK
LB FUEL
17.11
128.32
5.46
3.50
1 .78
1 .26
0.64
MASS F.MI
HC
LB/1K
LB FUEL
1.21
43.05
0.18
0. 10
0.01
0.16
0.13
MASS EMI
NO?
LB/1K
LI FUEL
2.42
1.14
0.48
0.41
0.06
0.17
0.07
MASS FMI
CU2
LR/IK
LB FUEL
3107.55
2818.04
3178.66
3131. 98
3134.92
1135.33
3116.39
MASS C'll
Nn
LB/1K
LB FUFL
3.32
1.07
5.42
6.04
8. 49
R.78
12.90
MASS EMI
NOX
LP./1K
LB FUEL
5.74
2.70
5.90
6.47
8.55
8.95
12. W
MASS f.»l
CO
LB/HR
46.81
120.36
24.99
19.62
12.01
9.95
5.99
MASS EM
HC
LB/HR
3.31
40. 38
0.83
0.55
0.07
1.24
1.71
MASS EMI
N02
LB/HR
6.62
1.07
7.19
2.41
0.38
1.3?
MASS EMI
C02
LB/HR
6502.25
2643.32
14310.48
17557.66
21151.31
24712.65
9.09
1.00
24.80
31.89
57.28
69.24
0.65 29472.67 121.19
MASS EMI
NOX
L6/MR
15.70
2.07
26.98
36.79
57.66
70.55
121.84
POWER
PERCENT
HATED
T.O.
27
59
70
CO
LB/ IKfTH-HR
9. J61
14J.795
2.HOB
I. 817
0.94?
0.682
0.365
LB/IK«TH-H<
1700.451
3146.814
1607.910
1625.728
1658.927
1692.64?
1797.115
THf.
LB/IK»TH-HR
0.661
48.067
0.094
0.051
0.005
0.085
0.074
Lfl/1KKTH-HR
1.817
1 .192
2.786
3.138
4.491
4.742
7.390
L1/1K«TH-HH
1.323
1.269
0.246
0.223
0.030
0.090
0.040
LB/ 1MTH-HR
3.141
2.461
3.032
3.361
4.522
4.832
7.429
i IV-132
-------
CAL 10 NUMBER: 358 ENGINE TYPE AND MODEL: JT30 -38
TEST ORGANIZATION: PRATT e. WHITNEY
SERIAL NUMBER: P-668820
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
O.B50
0.400
0.050
FRACTIONAL
POMER
0.050
1.000
0.850
0.400
0.050
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POKER
TH
900.0
18000.0
15300.0
7200.0
900.0
POWER
f TH
900.0
1BOOO.O
15300.0
7200.0
900.0
POWER
TH
900.0
18000.0
15300.0
7200.0
900.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
119.588 1040.707
0.0 10583.215
8.851 8846.027
30.697 3699.899
119.588 1040.707
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
40.454 1040.707
0.0 10583.215
0.0 6846.027
1.746 3699.899
40.454 1040.707
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
2.288 1040.707
159.101 10583.215
98.363 8846.027
19.018 3699.899
2.288 1040.707
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
USAGE TINE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN. ,
1.000 19.00
1.000 0.70
1.000 2.20
I. 000 4.00
1.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
37.661
0.0
0.325
2.046
13.992
54. 192
47.311
33.024
0.0
HC
MASS
LBS.
12.810
0.0
0.0
0.116
4.720
17.646
15.405
10.753
0.0
NOX
MASS
LBS.
0.724
1.B56
3.607
1.268
0.267
7.722
6.741
4.706
103.121
FUEL
MASS
LBS.
329.56
123.47
324.35
246.66
121.42
1145.46
FUEL
MASS
LBS.
329.56
123.47
324.35
246.66
121.42
1145.46
FUEL
MASS
LBS.
329.56
123.47
324.35
246.66
121.42
1145.46
LB CO /
IK LB FUEL
114.910
0.0
1.001
8.297
114.910
LB HC /
IK LB FUEL
38.871
0.0
0.0
0.472
38.871
LB NOX/
IK LB FUEL
2.198
IS. 033
11.119
5.140
2.198
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
LB CO /
TH-HR
0. 13288
0.0
0.00058
0.00426
0.13288
LB HC /
t TH-HR
0.04495
0.0
0.0
0.00024
0.04495
LB NOX/
1 TH-HR
0.00254
0.00884
0.00643
0.00264
0.00254
IV-133
-------
DATE: 8/20/71
TEST ORGANIZATION: PRATT C WHITNEY
ENGINE SUPPLIER: PRATT AND WHITNEY
ENGINE DATA .«««««.«««.«..««.««...«.............«.«....«......
CAL II) NUMBER: 359 ENGINE TYPE AND MODEL: JT30 -39
RATED ThRUST: 1ROOO.
ENGINE TOTAL TIME: -0. MRS
TIME SINCE HOT SECTION OVERHAUL: -0. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: -0. HRS
NZ COMPRESSOR OVERHAUL: -o. HRS
COMBUSTOK CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
NZ TURBINE OVERHAUL: -o. HRS
FUfL: JP-4 FUEL H/C RATIO: 2.000
OPERAT10NAL OATA ««»«
INLEt Aid TEMPERATURE, DEGREES F: START 76.00 FINISH 82.00
ATMOSPHERIC PRESSURE: START 29. 55 FINISH 28.95
INLET AIR HUMIDITY, IBS H20/LB AIR: 0.0145
RELATIVE HUMIDITY: -o.oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 7
COMMENTS:
B/N BURNER CONF1GIIRATI ON SMflKE DENSITY IS VCN BRAN MEASURE
SERIAL NUMBER:
CLOCK
TIME
1000.00
1229.00
1100.00
1120.00
1323.00
1133.00
1153.00
TEST
MflOE
I/ .1
2/ I
3/ 2
4/ 3
5/ 4
6/ 5
7/ 6
POWER
THP.UST.LBS PERCENT
UR RATED
SHP
5020.00
840.00
B770.00
10720.00
12600.00
14500.00
17492.00
T.O.
27
4
48
59
69
80
97
ENGINE
SPEED
RPP
Nl
41BO.OO
1860.00
5205. OC
5610.00
5970.00
630C.OC
67)0.00
N2
8225.00
5480.00
8950.00
9180.0(1
9420.00
9655.00
9925.00
MEASURED
FUEL
FLOW
LB/HR
2772.00
951.00
4526.00
5612.00
6703.00
7912.00
9499.00
GAS GEN
MB FLOW
18/SEC
91.78
32.29
125. 4B
147.91
157. BO
171.07
1H3.86
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.008390
0.008190
0.010020
0.010540
0.011BOO
0.012850
0.013450
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.17
1.02
1.33
I.4B
1.56
1.69
1.85
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-O.OC
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
27
4
48
59
69
80
EXHAUST
GAS
TEMP
OF OR FES F
620.00
550.00
705.00
765.00
815.00
K95.00
981.00
FXHAUST
GUS
PRESSURE
PSIA
16.96
15.00
19.25
21.25
22.37
24.18
26. 33
CO
(WET)
PP"V
149.20
908.50
60.40
37.00
21.00
1 7.40
13.60
CO
2
(WET!
PERCENT V
1.59
1.17
1.62
2.20
2. 70
2.93
J.13
THC
IWETI
PPMV
19. 10
244.90
a. 10
2.90
2.10
5.40
5.80
NO
IkETI
PPMV
17.60
S.30
35.00
50.50
59.30
76.90
109.50
N(l
2
IWETI
PPMV
H.50
1.50
0.70
6.40
5.80
5.50
5. 10
NO
X
IWETI
PPMV
26.10
6.80
35.70
56.90
65.10
H2.40
1 14.60
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
27.00
10.00
36.00
37.00
38.00
36.00
36.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
27
4
48
59
69
81
MASS FMI
CO
L«/IK
L8 FUEL
18.54
122. 15
6.60
1.35
1.55
1 .19
0. 82
MASS FMI
HC
LB/IK
LB FUEL
1.36
18.86
0.51
0.15
0.09
0.21
0.20
MASS EM]
N02
LB/1K
LB FUEL
1.74
0.33
0.13
0.95
0.70
0.62
1.50
MASS FMI
C02
LC/IK
IB FUFL
3104.88
2894.09
3125.98
3132.06
3135.06
3115.30
3135.92
MASS EMI
NO
LB/IK
LB FUEL
3.59
1.17
6.28
7.52
7.20
ft. 60
10.78
MASS FMI
NOX
LB/IK
LB FUEL
5.33
1.50
6.41
R.47
7.90
9.22
11.28
MASS EMI
cn
LB/HR
51.40
116.16
29.88
18.81
10.40
<;.3«
7.74
MASS EMI
HC.
LB/Hk
3.77
17.93
2.30
0.84
0.60
1.67
l.«9
MASS EMI
NO 2
LP/HR
4.81
0.32
0.57
5.35
4.72
4.87
4.77
MASS FMI
C02
LB/HR
8606.73
2752.28
14148. IB
175(7.14
21014.31
24806.52
29768.07
MASS EM
NO
LB/HB
9.96
1.11
28.44
42.18
48.25
68.06
102.40
MASS EMI
NUX
LB/HR
14.77
1.41
29.01
47.52
52.97
72.93
107.17
POWER
PERCENT
RATED
T.O.
27
4
48
59
69
80
97
cn
LB/1KHTH-HR
10.739
13R.286
3.407
1.755
0.826
0.647
0.443
1714.4^7
3276.527
1613.248
1639.659
1667.803
1710.795
1702.955
0.751
21.350
0.262
0.079
0.047
0.115
0.108
NCJ
LB/1K1TH-HH
1.984
1.325
1.243
3.935
3.829
4.694
5.854
L9/1KKTH-HR
C.95B
0.175
0.065
0.499
0.375
0.336
0.273
LB/1KKTH-HR
2.942
1.700
1.108
4.433
4.204
5.030
6.127
I
IV-134
-------
CAI 10 NUMBER: 359 ENGINE TYPE AND MODEL: JI30 -39
TEST ORGANIZATION: PRATT t MHITNEV
SERIAL NUMBER: P-668822
MODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
0.050
1.000
0.850
0.400
0.050
POHER
TH
900.
laooo.
15300.
7200.
900.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/KR LB/HR
102.838 985.083
0.0 10226.599
3.849 6602.055
39.066 3803.405
102.838 985.083
USAGE TIME IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOX
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POHER
0.050
1.000
0.850
0.400
O.OSO
POMER
f TH
900.
18000.
15300.
T200.
900.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
16.463 985.083
0.728 10226.559
0.912 8602.095
3.031 3803.405
16.463 985.083
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.090
POWER
1 TH
900.0
18000.0
15300.0
7200. 0
900.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
I.3T4 985.083
120.812 10226.559
82.910 8602.055
21.132 3803.405
I.3T4 9B5.083
WT
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TM-HR/CYCLEl
LBS POLLUTANT/ 1000K LB TH AT T.O.:
CO
MASS
LBS.
32.565
0.0
0.141
2.604
11.998
47.309
42.424
28.829
0.0
HC
MASS
LBS.
5.213
0.008
0.033
0.202
1.921
7.378
6.616
4.496
0.472
NOX
MASS
LBS.
0.435
1.409
3.040
1.409
0.160
6.454
5.787
3.933
78.304
FUEL
MASS
LBS.
311.94
119.31
315.41
253.56
114.93
1115.15
FUEL
MASS
LBS.
311.94
119.31
315.41
253.56
114.93
1115.15
FUEL
MASS
LBS.
311.94
119.31
315.41
253.56
114.93
1115.15
LB CO /
IK LB FUEL
104.395
0.0
0.447
10.271
104.395
LB HC /
IK LB FUEL
16.713
0.071
0.106
0.797
16.713
LB NOX/
IK LB FUEL
1.395
11.814
9.638
5.556
1.395
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
1 TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
ENERGY
TH-HR
285.00
210.00
561.00
480.00
105.00
1641.00
LB CO /
1 TH-HR
0.11426
0.0
0.00025
0.00543
0.11426
LB HC /
1 TH-HR
0.01829
0.00004
0.00006
0.00042
0.01829
LB NOX/
TH-HR
0.00153
0.00671
0.00542
0.00294
0.00153
IV-135
-------
DATE: ?/ t>ni
TEST ORGANIIATION: UNITED/EPA
ENGINE SUPPLIER: UNITED AIRLINES
ENGINE 0«tl »
CAL ID NUM9FR: 129 ENGINE TYPE AND MODEL: JT3D-7
RATED THRUST: 19000.
ENGINE TOTAL TINE: 0. MRS
TINE SINCE HOT SECTION OVERHAUL: 0. HRS
TINE SINCE:
SERIAL NUMBER!
NI CCNPRESSOR OVERHAUL: o. HRS
NZ COMPRESSOR OVERHAUL: o. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOJJLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
NZ TURBINF OVERHAUL: o. HRS
FUEL: JFT - A FUEL H/C RATIO: 1.920
OPERATIONAL DATA »»««««««
INLET AIR TEMPERATUREi DEGREES f: START 59.On FINISH 57.20
ATMOSPHERIC PRESSURE: STOUT 2S.78 FINISH 29.86
INLET AIR HUMIDITY, IBS H20/LB AIR: 0.0069
RELATIVE HUMIDITY: 65.00 PERCENT
SAMPLE LINF: TEMPERATURE. DEGREES C: 160.00. FLOW RATE. LITERS/MIN:
SAKPLE LINE TRANSPORT TIME, SEC: 5.00
NUMBER OF TESTS: 4
COMMENTS:
NEW ENGINE - DATA OUES1IONABLE. SAMPLE LINE BROKEN AFTER TEST.
PROBF LOCATED 15.25 IN. FROM TAILPIPE
1.50
CLICK TEST POWER
TIMF MODE THRUST,LRS PERCENT
OR
SHP
1970.00 I/ 0
1925.00 2/ 1
1910.00 3/ 2
20*0.00 */ 1
9925.00
13150.00
17400.00
1150.00
XENT
.TED
n.
5?
69
91
6
ENGINE
SPEFO
Rf>M
NI N2
5130. OC 8936.00
563*. 00 9300.00
6237.00 9730.00
2026.00 5BC9.00
MEASURED
FUEL
FLOM
LB/HR
5053.00
6821.00
9*37.00
1162.00
GAS GEN
AIR FLOW
LD/SEC
-o.oo
-0.00
-0.00
-0.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINF
PRESSURE
RATIO
EPR
1.39
1.5*
1.82
-0.00
TURBINE
INLET
TEMP
OEGRFES f
-0.00
-O.DO
-0.00
-0.00
POWER
PERCENT
RATED
T.n.
52
69
91
6
FXHAUST
GAS
TEMP
PSGREFS r
710.40
798.flO
910.40
478.40
EXHAUST
GAS
PRESSURE
PS I A
41.00
45.80
51.80
31.00
CO CO
(UFTI 2
PPMV (WSM
PERCENT V
70.00
50.00
35.00
75.00
1 .52
2.62
2.97
0.17
THC.
IHFTI
PPMV
7.80
*.20
3.80
a*.oo
nn NO
(WFT> 2
PPMV (MET!
PPMV
23.00
59.00
92.00
1.00
-0.00
-0.00
-0.00
-0.00
NO
X
IMFTI
PPMV
29.00
63.00
95.00
1.00
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
HATED
T.D.
52
69
91
6
MISS FMI
CO
LP/1K
Lfl FUFI
9.20
1.33
2.36
81.03
MASS EMI
HC
LB/1K
LB FUEL
0.59
0.18
0. 15
51.98
MASS EMI
NU2
LR/IK
LB FUEL
-a. oo
-0.00
-0.00
-0.00
MASS CMI
C02
LB/1K
LB FUEL
S119.H2
31*9. 17
3151.77
2885.97
MASS EMI
NO
I.B/K
LB FUIL
*.97
7.41
IP. 21
1.77
MASS FMI
NDX
LB/1K
LB FUEL
6.26
7.92
10.54
1.77
MASS E.«l
CO
LB/HR
46.50
26.09
22.31
94.16
MASS EMI
HC
LB/HR
2.97
1.26
1.39
60.40
MASS FMI
Nf)2
LB/HR
-0.00
-0.00
-0.00
-0.00
MASS FMI
C02
LB/HR
15865.50
21*81.88
297*3.27
3353.49
MASS E«l
NO
LB/HR
25. 10
50.57
96.32
2.06
MASS EMI
NOX
LB/HS
31.64
54.00
99. *6
2.06
POWER
PERCENT
BATED
T.O.
52
69
cc
LR/1KBTH-HR
4.685
1.984
1.282
11.B79
1598.540
16*3.601
I 709.1H4
2916.081
THC
LH/1KHTH-HR
0.299
0.095
O.ORO
52.521
Nfl
LB/IK BTH-HR
2.529
3.S46
5.535
1.793
LB/1K«TH-HR
-0.000
-0.000
-0.000
-0.000
NO
X
LB/IKKTH-HR
3.188
4.106
5.716
1 .791
IV-136
-------
CM. 10 NUMBER: 129 ENGINE TYPE AND MODEL: JTJD-7
TEST ORGANIZATION: UNITED/EPA
SERIAL NUMBER:
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
* TH
950.0
19000.0
16150.0
7600.0
950.0
EMISSION
RATE
LB/HR
120.410
24.053
18.772
50.786
120.410
FUEL
RATE WT
LB/HR
829.864
10370.813
8655.176
4216.137
829.864
USAGE
FACTOR
.000
.000
.000
.000
.000
TIME IN
MODE
MIN.
19.00
0.70
2.20
4.00
T.OO
TOTAL FOR CYCLE:
LBS POLLUTANT/IK IB FUEL/CYCLE:
LBS POLLUTANT/IK IB TH-HR/CYCLE:
LBS POLLUTANT/ IOOOK LB TH AT T.O.:
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
t TH
950.0
19000.0
16150.0
7600.0
950.0
EMISSION
RATE
LB/HR
92.377
0.0
0.0
3.526
92.377
FUEL
RATE WT
LB/HR
829.664
10370.813
8655.176
4216.137
829.864
USAGE
FACTOR
.000
.000
.000
.000
.000
TIME IN
MODE
MIN.
19.00
0.70
2.20
4.00
7.00
CO
MASS
LBS.
38.130
0.281
0.688
3.386
14.048
56.532
52.392
32.637
1.477
HC
MASS
LBS.
29.253
0.0
0.0
0.235
10.777
FUEL
MASS
LBS.
262.79
120.99
317.36
281.08
96.82
1079.03
FUEL
MASS
LBS.
262.79
120.99
317.36
281.08
96.82
LB CO /
IK LB FUEL
145.096
2.319
2.169
12.046
145.096
LB HC /
IK LB FUEL
111.316
0.0
0.0
0.836
111.116
ENERGY
1 TH-HR
300.83
221.67
592.17
506.67
110.83
1732.17
ENERGY
1 TH-HR
300.83
221.67
592.17
506.67
110.61
IB CO /
1 TH-HR
0.12675
0.00127
0.00116
0.00668
0.12675
LB HC /
TH-HR
0.09724
0.0
0.0
0.00046
0.09724
TOTAL FOR CYCLE: 40.265
LBS POLLUTANT/IK LB FUEL/CYCLE: 37.316
LBS POLLUTANT/IK LB TH-HR/CYCLE! 23.245
LBS POLLUTANT/1000K LB TH AT T.O.: 0.0
1079.03
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
TH
950.0
19000.0
16150.0
7600.0
950.0
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR HIN.
1.106 829.864 1.000 19.00
118.764 10370.813 1.000 0.70
83.489 8655.176 1.000 2.20
21.733 4216.137 1.000 4.00
1.106 829.864 1. 000 T.OO
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK LB TH-HR/CYCLE:
LBS POLLUTANT/ IOOOK LB TH AT T.O.:
KOX
MASS
LBS.
0.350
1.186
3.061
1.449
0.129
6.375
5.908
3.680
72.926
FUEL
MASS
LBS.
262.79
120.99
317.36
281.08
96.82
1079.03
LB NOX/
IK LB FUEL
1.133
11.452
9.646
5.155
1.333
ENERGY
TH-HR
300.81
221.67
592.17
506.67
110.83
1732.17
LB NOX/
f TH-HR
0.00116
0.00625
0.00517
0.00286
0.00116
IV-137
-------
0»IF1 7/19/71
TEST ORGANIZATION: UNITFTI/EPA
ENGINE SUPPLIER: UNITED AIRLINES
ENGINE DATA
CAL 10 NUMBFR:
134
ENGINE TYPE AND MODEL: JT1D-7
SERIAL NUMBER:
RATED THRUST: 19000.
ENGINE TOTAL TIME: 6207. MRS
TIME SINCF MOI SECTION OVERHAUL: 6707. HRS
TIHE SINC.F:
NI COMPRESSOR OVERHAUL: 6207. MRS
NZ COMPRESSOR OVERHAUL: 6207. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: 6207. HRS
N2 TURBINE OVERHAUL: 6207. HRS
fUFL! JET - A FUFL H/C RATIO: 1.920
OPERATIONAL DATA >»»«»«««»»««
INLET AIR TEMPERATURE, DEGREES F: START 72.50 FINISH
ATMOSPHERIC PRFSSURE: START 29.84 FINISH
INLET AIR HUMIDITY, IRS H70/LB AIR: 0.0102
RELATIVE HUMIDITY: 58.00 PERCENT
SAMPLE LINE: TEMPFRATURE, CEGRFES C: 160.00, FLOW RATE, LITERS/KIN:
SAMPLE LINE TRANSPORT TIMF, SEC: 5.00
NUMBER OF TESTS: 4
COMMENTS:
EXHAUST CIS PRESSURE IN INCHES HG
ALL BY-PASS AIR IS DUCTED AND NOT MIXED WITH EXHAUST.
REPAIR ENGINE - METAL IN OIL.
PROBE LOCATED 15.25 IN, FROM TAILPIPE.
6R.OO
29.90
CLOCK
TIME
1230.00
1245.00
1250.00
1422. 00
TEST
MOOF
I/ 0
?l I
M 2
4/ i
POWFR
THRUST, LRS PEKC.FNT
o« RAirn
SHP
10000.00
14076.00
17450.00
1000.00
T.O.
5?
7'.
91
5
ENGINE
SPEED
RPM
NI
5258.00
i9fx4.no
6388.00
1955.00
M2
9150.00
9601.00
9944.00
5824.00
MEASURED
FUEL
FLOW
I B/HR
5440.00
7696.00
9873.00
1143.00
CAS GFN
MR FLOW
LB/SCC
-0.00
-0.00
-0.00
-0.00
CALC
F/A
-0.000000
-o.oooooo
-0.300000
-0.000000
COMPRESSOR ENGINE
DISCHARGE PKESSURF
TEMP RATIO
DECREES F EP«
-0.00
-0.00
-0.00
-0.00
1.36
1.56
1.82
-0.00
TURBINE
INLET
TEMP
DECREES f
-0.00
-0.00
-0.00
-0.00
POWER EXHAUST
PERCENT GAS
RATFD TFBP
T.O. flEGRFES F
52
74
91
5
761.00
865.40
96?.60
546.BO
EXHAUST
GAS
PRESSURE
PSI A
40. 70
47.20
54. 10
30.70
r.o
IWETI
PPMV
80.00
50.00
10.00
881.00
CO
y
(WET)
PFRCENT V
2.35
?.7B
3.15
1.42
THC
(WET)
PPMV
0.84
1.50
1.50
1200.00
NO
IWET)
PPMV
36.00
71.60
105.60
10.00
NO
p
IWET)
PPMV
-0.00
-0.00
-0.00
-0.00
NO
X
1 WF T I
PPMV
42.00
76. OC
106.00
11.00
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
PARTICULATFS
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
57
74
91
5
MASS FM|
cn
Lfl/IK
LB FUFl
6.91
3.61
0.04
IOR.57
MASS EMI
HC
LR/IK
LB FUEL
0,04
0.06
0.05
B4.79
MASS EMI
Nl)2
LB/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
MASS EMI
CTJ2
LB/1K
LB FUEL
1145.07
3150.05
3154.7',
2752.66
MASS EMI
NO
LB/1K
LB FUEL
5.32
0.72
1 1.06
2.03
MASS EMI
NOX
LB/1X
LB FUEL
5.68
9.00
11.10
2.21
MASS EMI
CO
LB/MK
17.07
27.75
6.?1
124.10
MASS EMI
HC
LB/HR
0.22
0.4fl
0.54
96.97
MASS EMI
NO 7
LB/HR
-0.00
-0.00
-0.00
-0.00
MASS EMI
CU2
LB/HR
17 109. IB
24242. 81
31146.73
3146.11
MASS EMI
NO
LB/HR
2B.92
67.10
109.16
2.37
MASS 6M1
NOX
LB/HO
31.97
69. 2fl
109.57
2.55
POWER
PFRCFNT
RATED
T.O.
52
74
91
5
cn
LB/K'TH-MR
1.70/
1.971
0. 161
174 .'104
1710.916
1772.2BO
1784.913
3146.314
THC
L B/IK* TH-HR
0.022
0.014
0.011
96.918
Nfl
I.R/1KHTH-HH
2.B92
4.767
6.255
2.316
I.B/1MIH-HR
-0.000
-0.000
-o.ooo
-0.000
NO
X
Lfl/lKHTH-HR
3.197
4.922
6.279
2.548
-------
CAL ID NUMBER: 134 ENGINE TYPE »ND MODEL: jiio-7
TEST ORGANIZATION: UNITED/EPA
SERIAL NUMBER: 671261
MODE F
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
MODE F
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
WOOF F
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
RACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
RACTIONAL
POHER
0.050
1.000
0.850
0.400
0.050
RACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
f TH
950.
19000.
16150.
7600.
950.
POKER
» TH
950.
19000.
16150.
7600.
950.
POHER
TH
950.
19000.
16150.
7600.
950.
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
EMISSION FUEL
RATE RATE HT
LB/HR LB/HR
114.360 1015.865
5.987 11019.152
20.751 8966.469
45.167 4501.012
114.360 1015.865
TOTAL FOR CYCLE:
LB3 POLLUTANT/IK L8
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
EMISSION FUEL
RATE RATE VI
LB/HR LB/HR
101.818 1015.865
5.468 11015.152
3.687 8966.469
2.189 4501.012
101.818 1015.865
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLIUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
1.789 1015.865
140.431 11015.152
91.866 8966.469
17.936 4501.012
1.789 1015.865
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
USAGE TINE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
16.214
0.070
0.761
1.011
13.342
53.198
44.389
30.827
0.368
HC
MASS
LBS.
12.242
0.064
0.115
0.146
11.879
44.466
17.131
25.671
3.357
KOX
MASS
LBS.
0.566
1.618
3.168
1.196
0.209
6.978
5.827
4.028
86.211
FUEL
MASS
LBS.
121.69
128.51
128.77
100.07
118.52
1197.56
FUEL
MASS
LBS.
121.69
12B.51
128.77
100. OT
118.52
1197.56
FUEL
MASS
LBS.
321.69
128.51
J28.77
300.07
118.52
1197.56
LB CO /
IK LB FUEL
112.574
0.544
2.314
10.035
112.574
LB HC /
IK LB FUEL
100.228
0.496
0.411
0.486
100.228
L8 NOX/
IK LB FUEL
1.761
12.749
10.245
3.985
1.761
ENERGY
1 TH-HR
300.83
221.67
592.17
506.67
110.81
1732.17
ENERGY
TH-HR
300.83
221.67
592.17
506.67
110.83
1712.17
ENERGY
I TH-HR
300.83
221.67
592.17
506.67
110.81
1712.17
LB
1
0
0
0
0
0
IB
1
0
0
0
0
0
LB
1
0
0
0
0
0
CO /
TH-HR
.12038
.00012
.00128
.00594
.12038
HC /
TH-HR
.10718
.00029
.00021
.00029
.10718
NOX/
TH-HR
.00188
.00719
.00569
.00216
.00188
IV-139
-------
DATE: T/16/T1
TEST ORGANIZATION: S W R
ENGINE SUPPLIER: T M A
ENGINE DATA ««««
CAL ID NUMBER:
115
ENGINE TYPE AND MODEL: J14A -II
SERIAL NUMBER:
HATED THKUST: 17500.
ENGINE TOTAL TIKE: 26795. MRS
TIME SINCE HOT SECTION OVERHAUL: 2993. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL:
N? COMPRESSOR OVERHAUL:
COMSUSTOR CAN REPLACEMENT:
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL:
NI TURBINE OVERHAUL:
N2 TURBINE OVERHAUL:
13286. HRS
13286. HRS
2993. HRS
13286. HRS
13236. HRS
13286. HRS
FUEL H/C RATIO: 2.020
69.00
2(1.87
FUEL: JP-4 TF
OPERATIONAL DATA ««««»«««««««««««««»«
INLET AIR TEMPERATURE, DEGREES F: START 89.00 FINISH
ATMOSPHERIC PRESSURE: START 28.87 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0153
RELATIVE HUMIDITY: 50.00 PERCENT
SA'PLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: l.OC
NUMBER OF TESTS: 5
COMMENTS:
F/A AND AIRFLOW CALCULATED FROM FKHAUST COMPOSITION FOH FOURIH KUN. N02
OEIFRMINFD IV SUBTRACTION.
ELAPSED
TIME
0.0
5.00
in.no
13.00
17. nn
TEST
MODE
I/ 0
21 I
3/ 2
1.1 3
I/ 4
POWER
THRUST. LBS PFHCENT
OR RATED
SHP
10020.00
12280.00
13700.00
580.00
12600. On
T.O.
57
70
78
3
71
ENGINE
SPEEfl
RPH
NI
5785.00
6140.00
6450. OC
2115.00
6130.00
N2
8440.00
8730.00
8930.00
5250.00
8750.00
MEASURED
FUEL
FLOW
LB/HP
8580.00
10670.00
12200.00
1360.00
11110.00
GAS GEN
AIR FLOW
LB/SEC
205.20
220.80
231.00
59.00
220.20
CALC
F/A
0.011600
0.013400
0.014700
0.006400
0.014000
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIO
DEGREES F EPP
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
57
70
78
3
71
EXHAUST
GAS
TEMP
DEGREES r
977.00
1107.00
1194.00
623.00
1121.00
EXHAUST
GAS
PRESSURE
PSIA
13. 70
17.20
18.90
0.60
17.90
CO CO
IWETI 2
PPMV IWETI
PFRCENT V
22.00
19.00
17.00
453.00
16.00
2.43
?.76
2.6?
1.25
2.69
THC
IHETI
PPMV
1.00
0.0
0.0
800.00
2.00
NO NO
IWFTI 2
PPMV IWETI
PPMV
ALOFHYDES SMUKF PARTICULATES
54.00
75.00
95.00
3.00
7(,.00
3.00
2.00
2.00
5.00
2.00
IUETI
PPMV
S7.00
77.00
97.00
8.00
78.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PUWER
PERCENT
RATED
T.O.
57
70
78
3
71
1ASS FM1
r.o
I.B/IK
LB FUEL
1.40
1 .37
1.20
65.68
1.10
MASS EMI
«C
LP/1K
LB FUEL
0.05
0.0
0.0
66.41
0.08
MASS EMI
NO?
LB/IK
Lfl FUEL
0.40
0.24
0.?3
1.19
0.24
MASS EMI
CO 2
LB/1K
LB FUEL
3130.78
3131.09
3131.35
2847.78
3131.15
MASS EMI
NO
Lfl/IK
LB FUEL
7.?7
8.89
11.03
0.71
9.?5
MASS EMI
NOX
LB/IK
Lfl FUEL
7.68
9.13
11.26
1.91
9.49
MASS EMI
CO
LB/HR
15. 4«
14.64
14. ',6
89.33
13.17
MASS EMI
HC
LB/HR
0.40
0.0
0.0
10.35
0.94
MASS EMI
NO 2
LB/HR
3.47
2.53
2.83
1.6?
2.70
MASS EMI
C<12
LB/HR
26857.79
33408.68
38202.51
3872.93
34787.03
MASS EMI
NO
LB/HK
62.39
94.91
134.54
0.97
102.75
MASS CMI
NO?
LB/HR
65.86
97.44
137.37
2.59
105.45
POWER
PERCENT
RATFD
T.O.
57
70
78
3
71
CO
LB/IK»TH-HR
I .544
I. 192
1.070
154.017
1.045
L8/IKKTH-HR
2630.4lfl
2720.576
2738.505
6677.555
2760.875
THC
LQ/lKtTH-HR
0.040
0.0
0.0
155.777
0.075
NO
IB/1K1TH-H"
6.2?7
7.779
9.820
1.671)
8.154
LB/1KHTH-HR
0.346
O.?06
O.?07
2.79?
LR/1KITH-HR
6.573
7.935
10 . 02 7
4.468
8.369
IV-140
-------
CAL to NUMBER: us ENGINE TYPE AND MODEL: JT»» -n
TEST ORGANIZATION: S H R I IMA
SERIAL NUNBER: ITUA2233I
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
Ttll-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
O.OSO
1.000
0.850
0.400
O.OSO
FRACTIONAL
POKER
O.OSO
1.000
0.050
0.400
0.050
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
O.OSO
POWER
1 TH
8TS.O
17500.0
14875.0
T 000.0
87). 0
POWER
1 TH
875.0
17500.0
14875.0
7000.0
875.0
POWER
TH
875.0
17SOO.O
14875.0
7000.0
875.0
EMISSION FUEL
RATE RATE NT
LB/HR LB/HR
27.930 1448.223
10.583 15554.047
11.730 13161.851
9.054 S730.9I8
27.930 1448.223
TOTAL FOR CYCLE:
L8S POLLUTANT/IK L8
LBS POLLUTANT/ IK IB
LBS POLLUTANT/ 1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
51.016 1448.223
0.0 15554.047
0.0 13161.859
0.802 S730.918
SI. 016 1446.223
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/ IOOOK
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
3.022 1448.223
289.474 I55S4.047
175.049 13161.859
34.16B 5730.918
3.022 1448.223
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLEl
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
KIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
8.844
0.123
0.430
0.604
3.258
13.260
7.923
8.311
0.706
HC
MASS
IBS.
16.155
0.0
0.0
0.053
S.452
22.160
13.240
13.890
0.0
NOX
MASS
LBS.
0.957
3.377
6.418
2.278
0.353
13.383
7.996
8.389
192.983
FUEL
MASS
LBS.
458.60
181.46
482.60
382.06
168.96
1673.69
FUEL
MASS
LBS.
458.60
181.46
482.60
362.06
168.96
1673.69
FUEL
MASS
L8S.
458.60
181.46
482.60
382.06
I6B.96
1673.69
LB CO /
IK LB FUEL
19.285
0.680
0.891
1.580
19.285
LB HC /
IK LB FUEL
35.226
0.0
0.0
0.140
3S.226
LB NOX/
IK LB FUEL
2.087
18.611
13.300
S.962
2.087
ENERGY
TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
ENERGY
TH-HR
277.08
204.17
545.42
466.67
102.00
1595.42
ENERGY
1 TH-HR
277.08
204.17
54S.42
466.67
102.08
1S95.42
LB CO /
1 TH-HR
0.03192
0.00060
0.00079
0.00129
0.03192
IB MC /
t TH-HR
0.05830
0.0
0.0
0.00011
0.05830
LB NOX/
0 TH-HR
0.00345
0.016S4
0.01177
0.00488
0.0034S
IV-141
-------
DATE: T/19/71
TEST ORGANIZATION: s u R i TUA
ENGINE SUPPLIER: r w «
ENGINE DATA «
CAL ID NUMBER: us
ENGINE TYPF AND MODEL: JT»A -11
SERIAL NUMBER: 611087
RATED THRUST: 17500.
ENGINE TOTAL TIME: 22911. MRS
TIME SINCE HOT SECTION OVERHAUL: 10505. MRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL:
N2 COMPRESSOR OVERHAUL:
COMBUSTOR CAN REPLACEMENT:
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL:
NI TURBINE OVERHAUL:
N2 TURBINE OVERHAUL:
10505. HRS
10505. HRS
10505. HRS
10505. HRS
10505. HRS
10505. HRS
FUEL H/C RATIO: 2.020
73.00
28.98
FUEL: JP-4 TF
OPERATIONAL DATA ««»»««»»««««
INLET AIR TEMPERATURE, OEGRFFS F: START 73.00 FINISH
ATMOSPHERIC PRESSURE: START 28.97 FINISH
INLET AIR HUMIDITY, LUS H20/LB AIR: 0.0093
RELATIVE HUMIDITY: 50.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.OC, FLOW RATE, L1TERS/M1N:
SAMPLE LINE IRANSPORT MME, SEC: 1.00
NUMBER OF TFSTS: 5
COMMENTS:
F/A AND AIKFLQW CALCULATED FROM FXHAUST COMPOSITION FOR FOURTH RUN. N02
DETERMINED BY SUBTRACT ION. ENGINE EQUIPPED 84
1 .507
1 I1.39H
2.089
2595.953
2677.441
2784.1 80
5424.121
26^4.574
THC
LB/1KHTH-HR
0.043
0.0
n.o
122.117
n.n
LB/1KHTH-HR
5.851
7. 191
9.405
0.953
7.9CO
LB/IKIIH-HR
0.622
0.553
0.495
2.859
0.520
NO
X
LB/1KHTH-HR
6.473
7.744
9.900
3.B12
8.419
IV-142
-------
CAL ID NUMBER: lie ENGINE TYPE AND MODEL; JT4A -11
TEST ORGANIZATION: s w R i THA
SERIAL NUMBERl 611087
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POHER
0.050
1.000
O.BSO
0.400
0.050
POHER
1 TH
875.0
17500.0
14875.0
7000.0
675.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
60.002 1431.050
1B.52I 16061.234
19.443 13324.449
IB. 325 6308.166
60.002 1431.050
USAGE TIKE IN
UT FACTOR MODE
NIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
TOTAL FOR CVCLE:
L8S POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TN AT T.O.:
MODE
TAXI-IDLE
TAKEOFF
CL INBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POHER
0.050
1.000
0.850
0.400
0.050
POHER
1 TH
675.0
17500.0
14875.0
7000.0
B75.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
76.B3B 1431.050
0.0 16061.234
0.0 13324.449
1.663 6306.166
76.838 1431.050
USAGE TIME IN
HT FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LRS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POHER
0.050
1.000
O.B50
0.400
0.050
POHER
TH
675.0
17500.0
14875.0
7000.0
B75.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
3.054 1411.050
251.460 16081.234
155.094 13324.449
38.707 6308.168
3.054 1431.050
USAGE TIME IN
HT FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
TOTAL FOR CVCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
CO
MASS
LBS.
19.001
0.216
0.713
1.222
7.000
28.151
16.397
17.645
1.235
HC
MASS
LBS.
24.332
0.0
0.0
0.111
8.964
33.406
19.459
20.940
0.0
NOX
MASS
LBS.
0.967
2.934
5.687
2.580
0.356
12.524
7.295
7.850
167.640
FUEL
MASS
LBS.
453.17
187.61
488.56
420.54
166.96
1716.84
FUEL
MASS
LBS.
453.17
187.61
488.56
420.54
166.96
1716.84
FUEL
MASS
LBS.
453.17
187.61
488.56
420.54
166.96
1716.84
LB CO /
IK LB FUEL
41.929
1.152
1.459
2.905
41.929
LB HC /
IK LB FUEL
53.693
0.0
0.0
0.264
53.693
LB NOX/
IK LB FUEL
2.134
15.637
11.640
6.136
2.134
ENERGY
t TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
ENERGY
TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
ENERGY
i TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
LB CO /
t TH-HR
0.06657
0.00106
0.00131
0.00262
0.06857
LB HC /
f TH-HR
0.08781
0.0
0.0
0.00024
O.OB78I
LB NOX/
TH-HR
0.00349
0.01437
0.01043
0.00553
0.00349
IV-143
-------
0»TE! 7/30/71
TEST ORGANIZATION: s w «
ENGINE SUPPLIER: TWA
ENGINE OATA
CAL ID NUMBER: 299
ENGINE TYPE AND MODEL! JT4A -II
SERUL NUMBER: P610670B
RATED THRUST: 17500.
ENGINE TOTAL TIME: 26595. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 7*94. HRS
N2 COMPRESSOR OVERHAUL: 749*. HRS
COMBUSTOR CAN REPLACEMENT: 7494. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 3033. HRS
NI TURBINE OVERHAUL: 7494. HRS
H2 TURBINE OVERHAUL: o. HRS
FUEL: JP-4 TF FUEL H/C RATIO: 2.020
OPERATIONAL DATA *»««««
INLET MR TEMPERATUREi DEGREES F: START 66.00 FINISH
ATMOSPHERIC PRESSURE: START 29.09 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0080
RELATIVE HUMIDITY: 50.00 PCRCFNT
SAMPLE LINE: TEMPERATURE. TEGREES C: 150.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
N(12 DETERMINED BY SUBTRACTION.
67.00
29.09
ELAPSED
TIME
0.0
12.30
21.10
24.no
11.50
TEST
MOOE
i/ n
11 i
J/ 2
4/ 3
5/ 4
POWFR
THRUST, LBS PE1CENT
OR KATFD
SHP
9720.00
11500.00
14620.00
620.00
14000.00
T.O.
55
65
B.I
3
79
ENGINE
SPECO
RPM
NI
55BD.OO
5B40.00
6450.00
2240.00
6280.00
N2
S170.00
8400.00
8830.00
5210.00
8690.00
MEASURED
FUEL
FLOW
1B/H«
8050.00
9530.00
12920.00
1300.00
12200.00
GAS GEN
AIR FLOW
LB/SEC
205.70
21B.80
240.50
61.30
736.70
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.010900
0.012100
0.014900
0.005900
0.014300
DEGREES F
-0.00
-0.00
-0.00
70.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
2.01
2.22
2. 61
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATtP
T.O.
55
65
HI
3
79
FXHAUST
GAS
TEMP
DEGREES f
BHO.OO
977. On
1184.01
543. 00
1137.00
EXHAUST
GAS
PRESSURE
PS I A
13.60
16.40
21 .20
0.60
20.30
cn
(WET)
PPMV
32.00
29.00
26.00
412.00
21.00
CO
2
(UFII
PERCENT V
2.22
2.46
3.00
1.22
2.88
THC
IWFT)
PPMV
0.0
0.0
0.0
850.00
1.00
NP
1 WET)
PPMV
51.00
64.00
103.00
3.00
90.00
NO
2
(WET)
PPMV
4.00
4.00
3.00
6.00
4. 00
NO
X
IWET)
PPMV
55.00
68.00
106.00
9.00
94.00
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATF.S
-0.00
-0.00
-0.00
-0.00
-0.00
POKER
PERCENT
RATED
T.D.
55
65
83
I
79
MASS EMI
C'J
LBMK
LB FUEL
2.B7
2.35
I. n
61 .01
2.01
M«SS EMI
HC
LB/1K
LB FUEL
0.0
0.0
0.0
72.11
0.04
MASS [Ml
NU 2
IH/IK
LI FUEL
0.59
0.51
0.33
1.46
0.45
MASS EMI
C02
LB/1K
LB FUEL
3128.71
3129.55
1130.51
2839.52
1129.98
MASS EMI
NO
L8/1K
LB FUEL
7.51
n.5i
11.24
0.71
10.21
MASS EMI
MIX
LB/1K
LB FUEL
8.10
9.04
11.56
2.19
10.68
MASS EM
CO
Le/HH
23.11
22.38
22.31
79.34
?4.47
MASS EMI
HC
LB/HB
0.0
0.0
0.0
93.75
0.48
MASS EMI
N02
LB/MR
MASS EMI
C02
LB/HR
4.74 25186.29
5.07 29824.63
4.23 40446.42
1.90 3691.37
5.54 38185.77
MASS EMI
NO
LB/HR
60.49
81.12
145.17
0.95
124.75
M/1SS EMI
NOX
LB/HR
65.23
86.18
149.40
2.85
110.29
POWER
PERCENT
RATED
t.O.
55
65
81
1
79
cn
LF>/ iKff TH-HR
2.177
L.046
127.966
1 .748
2591. H2
2593.446
2766.511
5951.820
27^7.555
THf.
Lfl/lMTH-HR
0.0
0.0
0.0
151.204
0.035
NO
LB/1KHTH-HH
6.223
7.053
9.930
1 .531
<).9I I
L8/1KHTH-HH
0.488
0.441
0.289
3.061
0.396
6.711
7.494
10.219
4.592
9.307
IV-144
-------
CAL ID NUMBER: 289 ENGINE TYPE AND HODEL: JT4A -11
TEST ORGANIZATION: S M R I THA
SERIAL NUMBER! P6106TOB
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
HOOE
TAKI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
FRACTIONAL
POKER
0.050
1.000
0.850
0.400
0.050
FRACTIONAL
POKES
0.050
1.000
0.850
0.400
0.050
POMER
TH
875.0
17500.0
14875.0
7000.0
875.0
POKER
1 TH
675.0
17500.0
14875.0
7000.0
875.0
POWER
TH
875.0
17500.0
14875.0
7000.0
875.0
EMISSION FUEL USAGE TIME IN
RATE RATE HT FACTOR MODE
LB/HR LB/HR MIN.
65.255 1442.430 1.000 19.00
20.322 15612.250 1.000 0.70
21.792 13012.324 1.000 2.20
31.566 6255.691 1.000 4.00
65.255 1442.430 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE)
LBS POLLUTANT/IK LB TH-HR/CVCLE:
LBS POLLUTANT/ 1000K LB TH AT T.O.:
EMISSION FUEL USAGE TINE IN
RATE RATE MT FACTOR MODE
LB/HR LB/HR MIN.
74.538 1442.430 .000 19.00
0.0 15632.250 .000 0.70
0.0 13012.324 .000 2.20
6.106 6255.691 .000 4.00
74.538 1442.430 .000 7.00
TOTAL FOR CYCLE!
LBS POLLUTANT/ IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CVCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE HT FACTOR NODE
LB/HR LB/HR MIN.
3.166 1442.430 .000 19.00
215.725 15632.250 .000 0.70
156.059 13012.324 .000 2.20
37.466 6255.691 .000 4.00
3.186 1442.430 .000 7.00
TOTAL FOR CYCLE:
L8S POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK LB TH-HR/CYCLE:
LBS POLLUTANT/ 1000K LB TH AT T.O.:
CO
MASS
LBS.
20.664
0.237
0.799
2.104
7.613
31.418
18.464
19.693
1.355
HC
MASS
LBS.
23.604
0.0
0.0
0.407
B.696
32.707
19.221
20.500
0.0
NOK
MASS
LBS.
1.009
2.517
5.722
2.498
0.372
12.117
7.121
7.595
143.817
FUEL
MASS
LBS.
456.77
182.38
477.12
417.05
168.28
1701.59
FUEL
MASS
LBS.
456.77
182.38
477.12
417.05
168.28
1701.59
FUEL
MASS
LBS.
456.77
182.38
477.12
417.05
168.28
1701.59
LB CO /
IK LB FUEL
45.240
1.300
1.675
5.046
45.240
LB HC /
IK LB FUEL
51.675
0.0
0.0
0.976
51.675
LB NOX/
IK LB FUEL
2.209
13.800
11.993
5.989
2.209
ENERGY
TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
ENERGY
t TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
ENERGY
I TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
LB CO /
1 TH-HR
0.07458
0.00116
0.00146
0.00451
0.07458
LB HC /
TH-HR
O.OB5I9
0.0
0.0
0.00087
0.08519
LB NO*/
TH-HR
0.00364
0.01233
0.01049
0.00535
0.00364
IV-145
-------
DATE: 8/ 3/71
TEST ORGANIZATION: S W R I TMA
ENGINE SUPPLIER: TWA
ENGINE DATA
CAL ID NUMBER: 106
ENGINF TYPF AND MODEL: JT4A -11
SERIAL NUMBER: 1TWA2220AI
RATED THRUST: 17500.
ENGINE TOTAL TIME: 2732*. MRS
TIME SINCE HOT SECTION OVERHAUL: 32"). MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 7619. MRS
N2 COMPRESSOR OVERHAUL: 7619. MRS
COMBUSTHR CAN REPLACEMENT: 329. MRS
FIRST STAGF NOZZLE GUIDE VANE OVERHAUL: 329. HRS
NI TURBINE OVERHAUL: 7619. HRS
N2 TURBINE OVERHAUL: 7619. HRS
FUEL H/C RATIO: 2.020
75.00
28.95
FUEL: jp-4 TF
OPERATIONAL DATA «»
INLET AIR TEMPERATURE, DEGREES F: START 75.00 FINISH
ATMOSPHERIC PRESSURE: START 28.95 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0116
RELATIVE HUMIOITY: 61.00 PERCENT
SAMPLE LINF: TEMPERATURE, OEGRFFS C: 150.00, FLOW RATE, LITERS/MIN: 42.50
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMflFR OF TFS1S: 5
COMMENTS:
Nfl? DETERMINED BY SUBTRACTION. THIS TEST IS THE FIRST OF 3 SUCCESSIVE TESTS
ON THIS ENGINE. THE FUEL USED Fn« THIS TEST CONTAINED NO CI-2.
ELAPSED
TIME
0.0
R.JO
18.45
23.30
29.00
TEST
MOOE
I/ 0
2/ I
3/ 2
4/ 3
5/ 4
POWER
THRUST, LBS PF.RCFNT
OR RATED
SHP
9580.00
1 1040.00
14360.00
600.00
11760.00
T.O.
54
63
B2
3
7B
ENGINE
SPEED
RPM
NI
5550.00
5800.00
6390.00
2090.00
6250.00
N2
8300.00
B520.00
8980.00
5250.00
B900.00
MEASURFO
FUEL
FLOW
LB/HR
8100.00
9360.00
12840.00
1360.00
12300.00
GAS GEN
AIR FLOW
IB/SEC
199.10
212.50
235.00
56.70
231.50
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.011300
0.012200
0.015200
0. 006700
O.OI4BOO
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
FPR
1.96
2.18
2.61
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREFS F
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.D.
54
63
a?
3
7«
EXHAUST
GAS
TFMP
DEGREES F
909.00
981.00
1116.00
574.00
1157.00
FXHAUST
GAS
PRESSURE
PSIA
13.20
15.90
21.20
0.70
20.40
CIJ
IWETI
PPMV
25.00
22.00
22.00
464.00
22.00
cn
2
IWETI
PERCENI
2.30
2.49
3.08
1.35
2.97
THC
IWETI
PPMV
1.00
0.0
0.0
870.00
2.00
NO
IWETI
PPMV
50.00
62.00
100.00
3.00
93.00
NO
2
IWETI
PPMV
4.00
3.00
2.00
6.00
2.00
ALDEHYDES SMOKE PARTICULATtS
IWFTI
PPHV
54.00
65.00
102.00
9.00
95.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
54
63
82
MASS EMI
CU
LR/IK
LB FUEL
2.17
1.76
1.42
62.38
1.4*
MASS EMI
HC
LB/IK
Lfl FUEL
0.05
0.0
0.0
66.98
O.OB
MASS EMI
N02
LBMK
Lfl FUFL
0.57
1.39
0.21
1.32
0.2?
MASS EMI
C(12
LR/IK
LB FUEL
3120.70
3I>0.47
3131.01
2851.47
3130.71
MASS EMI
NO
LB/1K
LB FUEL
7.11
B.I5
10.63
0.66
10.25
MASS CMI
N(1X
LR/1K
LB FUEL
7.6B
8.54
IC.P4
1.99
10.47
MASS EMI
CO
LB/MR
17.54
16. 4B
18.28
84.83
IB. 15
MASS EMI
HC
Lfl/HS
0.40
0.0
0.0
91. 10
0.95
MASS FM
NO 2
LB/HR
4.61
3.69
2.73
1.80
2.71
MASS EMI
CO 2
LB/HR
25350.60
29301.24
40202.10
3378.00
38507.75
MASS EMI
NU
LB/HP
57.61
76.27
136.45
0.90
126.05
MASS EMI
NOX
LB/hR
62.72
79.96
139.19
2.70
12B.76
POWER
PFRCENT
DATED
T.n.
54
63
B2
3
78
r.n
LB/ llC»TH-Htt
1.431
1 .492
1.271
141.3«5
1.319
LB/IMTH-HR
2646.201
2654.098
2795.696
6463.340
2798.529
THC
LO/1KKTM-HR
0.042
0.0
n.o
151.827
0.069
NO
LB/IMTH-HH
6.014
6.909
9.489
1.502
9.161
LB/1KITH-HR
0.481
0.334
0. 190
3.003
0.197
NU
X
LB/1K«TH-H«
6.495
7.243
9.679
4.505
9.358
IV-146
-------
CM ID NUMBER: 306 ENGINE TYPE AND MODEL: JT*A -n
TEST ORGANIZATION: s w n I TWA
SERIAL NUMBER! ITWA2220AI
NODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIM30UT
APPROACH
TAXI-IOLE
0.050
1.000
0.850
0.400
0.050
POWER
( TH
675. 0
17500.0
14675.0
7000.0
875.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
79.518 1388.586
16.858 15191.160
18.710 13068.754
29.203 6079.773
79.518 1388.586
USAGE TIME IN
WT FACTOR MODE
NIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
195 POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
MODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
0.050
1.000
0.890
0.400
0.090
POWER
TH
875. 0
17500.0
14875.0
7000.0
875.0
EMISSION FUEL
RATE RATE
LB/KR LB/HR
53.413 1388.586
1.723 15191.160
3.492 13068.754
6.420 6079.773
53.413 1388.586
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TINE IN
WT FACTOR MODE
HIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.050
1.000
0.890
0.400
0.050
POWER
TH
875.0
17500.0
14875.0
7000.0
875.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
2.744 1386.596
244.106 15191.160
156.802 13068.754
34.578 6079.773
2.744 1388.586
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
NIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
25.181
0.197
0.686
1.947
9.277
37.288
22.416
23.372
1.124
HC
MASS
LBS.
16.914
0.020
0. 128
0.42 B
6.232
23.722
14.261
14.869
1.148
NOX
MASS
LBS.
0.869
2.848
5.749
2.305
0.320
12.092
7.269
7.579
162.737
FUEL
MASS
LBS.
439.72
177.23
479.19
405.32
162.00
1663.46
FUEL
MASS
LBS.
439.72
177.23
479.19
405.32
162.00
1663.46
FUEL
MASS
LBS.
439.72
177.23
479.19
405.32
162.00
1663.46
LB CO /
IK LB FUEL
57.266
1.110
1.432
4.803
57.266
L8 HC /
IK LB FUEL
38.466
0.113
0.267
1.056
38.466
LB NOX/
IK LB FUEL
1.976
16.069
11.998
5.687
1.976
ENERGY
TH-HR
277.08
204.17
545.42
466. 67
102.08
1595.42
ENERGY
1 TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
ENERGY
TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
LB
0
0
0
0
0
LB
0
0
0
0
0
LB
t
CO /
TH-HR
.09088
.00096
.00126
.00417
.09088
HC /
TH-HR
.06104
.00010
.00023
.00092
.06104
NOX/
TH-HR
0.00314
0.01395
0.01054
0.00494
0.00314
IV-147
-------
OATF.: 8/ 3/71
TEST ORGANIZATION: s w R i rut
ENGINE SUPPLIER: TWA
ENGINE DATA
CAL ID NUMBER: 107
ENGINE TYPE AND MODEL: JT4A -11
SERIAL NUMBER: ITWA2220BI
RATED THRUST: 17500.
ENGINF. TOTAL TIME: 2732*. MRS
TIME SINCE HOT SECTION OVERHAUL: 324. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL:
N2 COMPRESSOR OVERHAUL:
COMBUSTOR CAN REPLACEMENT:
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL:
NI TURBINE OVERHAUL:
N2 TURBINE OVERHAUL:
7619. HRS
7619. HRS
329. HRS
329. HRS
7619. HRS
7619. HRS
FUEL H/C RATIO: 2.020
73.00
28.95
FUEL: JP-4 TF
OPERATIONAL OATA «««««««««««
INLET AIR TEMPERATUREi DEGREES F: START 74.00 FINISH
ATMOSPHERIC PRESSURE: START 28.95 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0117
RELATIVE HUMIimr: 63.00 PERCENT
SAMPLE LINE: TEMPERATURE. OEGRFFS C: 150.00. FLOW RATE, LITERS/MIN: »2.
SAMPLE LINE JRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
NO? DETERMINED RY SUBTRACTION THIS TEST IS THE SECOND OF THREE RUN ON THIS
ENGINE. THE FUEL USED FOR THIS TEST CONTAINED THE NORMAL CONCFNTRAT ION OF CI-2
I0.lt BY VOLUME!.
ELAPSED
TIME
D.O
4.15
10.15
15.00
24.00
TEST
MODE
I/ 0
2/ 1
3/ 2
4/ 3
5/ 4
POWER
THPUST.LBS PERCENT
OR RATED
SHP
941)0.00
11020.00
14460.00
600.00
14060.00
T.O.
54
62
02
3
80
ENGINE
SPEED
RPM
NI
5550.00
5790.00
6410.00
2100.00
6340.00
N2
8290.00
8520.00
8990.00
5220.00
8050.00
MEASURED
FUEL
FLOW
LR/HR
8000.00
9330.00
12950.00
1380.00
12640.00
CAS GEN
AIR FLOW
LR/SEC
199.30
212.40
236.20
57.20
234.20
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.011200
0.012200
0.015200
0.006700
0.015000
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES f
-D.OO
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.n.
54
62
B2
1
80
EXHAUST
GAS
TEMP
DEGREES F
BB9.00
977.00
1191.00
556.00
1179.00
EXHAUST
GAS
PRESSURE
PSIA
13.10
15.90
21.40
0.70
21.00
CO
IwETI
PPMV
19.00
13.00
23.00
491.00
28.00
CO
2
IWET)
PERCENT V
2.?5
P. 41
2.99
1.35
7.96
THC
(WET)
PPMV
1.00
n.o
0.0
929.00
2.00
NO
IWETI
PPMV
46.01
58.01
97.01
3.01
94.01
NO
2
IWETI
PPMV
2.00
4.00
3.00
6.00
2.00
NO
X
IWETI
PPMV
48.00
62.00
100.00
9.00
96.00
ALDEHYDES SMOKE PARTICULATFS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
54
62
»2
3
BO
IASS EMI
Cn
LB/IK
LB FUEL
3.45
2.71
1.53
64.59
I.8B
MASS EMI
HC
LB/IK
LB FUEL
0.05
0.0
0.0
71. 15
0.08
MASS FM|
NO 2
LH/1K
LB FUEL
0.29
0.54
0.31
1 . 32
0.22
MASS EMI
C02
Lfl/lK
LS FUEL
3127.68
112K.96
3130. B3
2036.56
3130.07
MASS EMI
NO
LB/IK
LB FUEL
6.68
7.87
10.62
0.66
10.39
MASS EMI
NOX
IB/IK
LB FUEL
6.98
8.42
10.95
1.98
10.61
MASS EM
CO
LB/HR
27.60
25.44
19.85
89.13
23.82
MASS EMI
HC
LB/HO
MASS EMI
N07
LB/HR
MASS EMI
C02
LB/HR
MASS EMI
NO
LB/HR
MASS EMI
NOX
LB/HR
0.41 2.33 25021.45 53.48 55.80
0.0 5.07 29193.16 73.4'j 7B.51
0.0 4.25 40544.28 137.50 141.76
98.19 1.02 3914.45 0.91 2.73
0.97 2.79 39564.07 131.35 134.14
POWER
PERCENT
RATED
T.O.
54
6?
82
3
no
2.912
2.309
1.373
148.558
I .694
LO/IK«TII-HR
2619.191
2649.107
2B03.892
6524.OB2
2813.945
THC
LB/ IMTH-HR
0.043
0.0
0.0
163.647
0.069
NO
LB/IKfTH-HR
5.641
6.665
9.509
1.516
9.342
LS/1KHTH-HR
0.245
0.460
0.294
1.011
0.199
LB/IKITH-HR
5.886
7.125
9.903
4.547
9.541
IV-148
-------
CAl 10 NUMBER: 307 ENGINE TYPE AND NODEL: JT4A -II
TEST ORGANIZATION: s K R i TKA
SERIAL NUMBER:
-------
DATE: a/ 3/71
TEST ORGANIZATION: s H R i TWA
ENGINE SUPPLIER: TWA
ENGINE DATA «
CAL ID NUMBER: 30"
ENGINE TYPE AND MODEL: JMA -11
SERIAL NUMBER: (TUA2220CI
RATED THRUST: 17500.
ENGINE TOTAL TIKE: 2T324. MRS
TIM SINCE HOT SECTION OVERHAUL: 329. HRS
11 HE SINCE:
NI COMPRESSOR OVERHAUL: 7619. HRS
N2 COMPRESSOR OVERHAUL: 7619. HRS
COMBUSTOH CAN REPLACEMENT: J29. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 329. HRS
Nl TURBINF OVERHAUL: 7619. HRS
N2 TURBINE OVERHAUL: 7619. HRS
FUEL H/C RATIO: 2.07.0
72.00
28.95
FUEL: jp-4 TF
OPERATIONAL DATA «»
INLET AIR TFMPERAIURF, DEGREES F: START 74.00 FINISH
ATMOSPHERIC PRESSURE: START 28.95 FINISH
INLET AIR HUMIDITY, LRS H20/LB AIR: 0.0116
RELATIVE HUMIDITY: 63.00 PERCFNT
SAMPLE LINE: TEMPERATURE. DEGREFS C: 150.00, FLOW RATE, LITERS/MIN: 42.50
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
N02 DETERMINED BY SUBTRACTION. THIS TEST IS THE THIRD OF THREE RUNS ON THIS
FNGINF. THE FUEL USED FOR THIS TEST CONTAINED THE MINIMUM CONCENTRATION OF
CI-2 (0.01251! RY VOLUME).
ELAPSED
TIMF
0.0
-------
CAL ID NUMBER: 308 ENGINE TYPE AND MODEL! JT4A -11
TEST ORGANIZATION) S H 0 I TMA
SERIAL NUMBER: ITVA2220C>
MODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
HOOF
T1XI-IOL6
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.050
1.000
o.BSo
0.400
0.050
FRACTIONAL
POKER
0.050
1.000
0.650
0.400
0.050
FRACTIONAL
PntfF.R
0.050
I. 000
0.850
0.400
0.050
POHER
TH
8T5.0
17500.0
14875.0
7000.0
875.0
POKER
1 TH
875.0
17500.0
14875.0
7000.0
875.0
POWER
1 TH
875.0
17500.0
14875.0
7000.0
875.0
EMISSION FUEL USAGE TINE IN
RATE RATE MT FACTOR MODE
LB/HR LB/HR MIN.
59.241 1303.562 .000 19.00
24.555 15797.063 .000 0.70
19.033 13215.137 .000 2.20
31.630 6032.602 .000 4.00
59.243 1303.562 .000 7.00
TOTAL FOR CYCLEl
LBS POLLUTANT/IK L6 FUEL/CYCLE:
LBS POLLUTANT/IK IB TH-HR/CYCLE:
LBS POLLUTANT/IOQOK LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE NT FACTOR MODE
LB/HR LB/HR MIN.
49.850 1303.562 .000 19.00
1.999 15797.063 .000 0.70
1.133 13215.137 .000 2.20
4.666 6032.602 .000 4.00
49.850 1303.562 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUT ANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K IB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE HT FACTOR MODE
LB/HR LB/HR MIN.
2.296 1303.562 1.000 19.00
230.544 15797.063 1.000 0.70
152.740 13215.137 1.000 2.20
32.502 6032.602 1.000 4.00
2.296 1303.562 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
CO
MASS
LBS.
18.760
0.296
0.696
2.109
6.912
28.765
17.583
18.030
1.637
HC
MASS
LBS.
15.786
0.023
0.042
0.311
5.816
21.977
13.434
13.775
1.332
sox
MASS
LBS.
0.727
2.690
5.600
2.167
0.268
11.452
7.000
7.178
153.696
FUEL
MASS
LBS.
412.79
184.30
484.55
402.17
152.08
1635.90
FUEL
MASS
LBS.
412.79
184.30
484.55
402.17
152.08
1635.90
FUEL
MASS
LBS.
412.79
184.30
484.55
402.17
152.08
1635.90
LB CO /
IK LB FUEL
45.447
1.554
1.440
5.243
45.447
LB HC /
U LB FUEL
38.241
0.127
0.086
0.774
38.241
L8 NOX/
IK LB FUEL
1.761
14.594
11.558
5.388
1.761
ENERGY
TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
ENERGY
1 TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
ENERGY
1 TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
LB CO /
TH-HR
0.06771
0.00140
0.00128
0.00452
0.06771
LB HC /
( TH-HR
0.05697
0.00011
0.00008
0.00067
0.05697
LB NOX/
TH-HR
0.00262
0.01317
0.01027
0.00464
0.00262
IV-151
-------
D»TE! 7/22/71
TEST ORGANIZATION: s w R I TUA
ENGINE SUPPLIER: TWA
ENGINE OAT4 ««
CAL ID NUMBER: 320
ENGINE TYPE AND MODEL: JUA -11
SERIAL NUMBER: P6I1I35B
RATED THRUST: 17500.
ENGINE TOTAL TIME: 27481. HRS
TINE SINCE HOT SECTION OVERHAUL: 284. HRS
TIHF SINCE:
Nl COMPRESSOR OVERHAUL: 6050. HRS
N2 COMPRESSOR OVERHAUL: soso. HRS
COMBUSTOR CAN REPLACEMENT: 284. HRS
FIRST STAGE NOZZLE GUIOE VANE OVERHAUL: 28*. HRS
NI TURBINE OVERHAUL: 8050. HRS
N2 TURBINE OVERHAUL: eoso. HRS
FUEL H/C RATIO: 2.020
78.00
28.91
FUEL: JP-4 TF
OPERATIONAL DATA ..............................................
INLET lift IFMPERATUREi DEGREES F: START 76.00 FINISH
ATMOSPHERIC PRESSURE: SIART ZS.QI FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0146
RELATIVE HUMIDITY: 73.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/HIM:
SAMPLE LINE IRANSPORT TIME, SEC: l.DO
NUMBER OF TESTS: 5
COMMENTS:
F/A ANO AIRFLOW CALCULATED FROM EXHAUST COMPOSITION FOR FOURTH RUN. N02
DETERMINFD BY SUBTRACTION.
ELAPSED
TIME
0.0
6.10
10. SO
16.00
18.00
TEST
MODE
I/ 0
?/ 1
I/ 2
4/ 3
5/ 4
POWER
IHRUST.LBS PERCENT
OR RATED
SHP
10040.00
11760.00
14180.00
520.00
14200.00
T.O.
57
67
81
2
81
ENGINE
SPEED
RPM
Nl
5t.6C.00
5950.00
6430.00
2020. OD
6420. CO
N2
8400.00
8650.00
9030.00
5100.00
9010.00
MEASURED
FUEL
FLOW
LB/HR
8040.00
9480.00
12000.00
1260.00
I2C40.00
GAS GEN
A1K FLOW
LB/SEC
203.00
218.00
235.00
52.00
234.00
CALC COMPRESSOR
f/A DISCHARGE
IEMP
0.011000
0.0)2100
0.014200
0.006800
0.014300
OFGRFFS F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
FPR
2.04
2.25
2.56
-0.00
-0.00
TURBINE
INLET
TEMP
DFGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.n.
5T
67
81
2
81
FKHAUST
GAS
TEMP
DEGREES f
914.00
1037.00
1202.00
547.00
1204.00
EXHAUST
GAS
PRESSURE
PS I A
14.00
16.70
20.50
0.50
20.50
CO CO
IWET1 7
PPMV UETI
PERCENI V
27.00
22.00
17.00
473.00
21.00
2.IB
2.49
2.83
1.26
2.83
THC
IUETI
PPMV
4.00
1.00
0.0
736.00
2.00
NO NO
IWETI 2
PPHV IWETI
PPMV
49.00
61.00
88.00
3.00
86. OC
2.00
3.00
2.00
4.00
4. 00
NO
X
(WETI
PPMV
51.00
64.00
90.00
7.00
90.00
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATEO
T.O.
57
67
81
2
81
MASS Ffl
CO
LB/1K
LI FUEL
2.47
1 . 76
1.20
68.11
1.48
MASS FMI
HC
LB/IK
LB FUEL
0.21
0.05
0.0
60.87
0.08
MASS EMI
NC12
LB/IK
LB FUFL
0.30
0.39
0.23
0.95
0.46
"ASS EMI
CC2
LB/IK
LB FUEL
3128.79
3130.35
31 31.36
?858.92
31 10.70
MASS EMI
NO
LB/IK
LB FUEL
7.35
8.02
10.18
0.71
9.95
MASS FMI
NOX
LB/IK
LB FUEL
7.65
K.41
10.41
1.66
in. 41
MASS FMI
CO
LB/HR
19.83
16.69
14.37
86.06
17. HO
MASS FMI
HC
Lfl/HR
1.68
0.43
0.0
76.70
0.97
MASS EM
NO 2
LB/HR
2.41
3.74
2.78
1.20
5.57
MASS EMI
C02
LB/MR
25155.50
29675.72
37576.32
3602.24
37693.59
MASS EMI
NO
LB/HR
59.11
76.00
122.15
0.90
119.75
MASS EMI
NOX
LB/HR
61.52
79.74
124.93
2.09
125.32
POWER
PERCENT
RATED
T.O.
57
67
81
2
CO
LB/ 1KBTH-HP
I .975
1.419
1.013
165.509
1.254
CO
2505.528
2523.446
2649.952
6927.JH3
2654.478
THC
LO/1K1TH-HR
0.168
0.037
0.0
147.497
0.068
NO
LB/IKITH-HR
5.887
6.463
8.614
1.724
8.433
LB/1KMM-HK
0.240
0.318
0.196
2.299
0.392
NO
X
Lt/IK»TH-Hit
6.128
6.780
B.810
4.021
8.825
IV-152
-------
c»i ID NUMBER: 320 ENGINE TYPE «ND MODEL: JT*» -n
TEST ORGANIZATION: S H B I IMA
SERIAL NUMBER: PMIIJSB
MODE FRACTIONAL
POWER
TAXI-IDLE 0.050
TAKEOFF 1.000
CLINBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.050
NODE FRACTIONAL
POHER
TAXI-IDLE 0.050
TAKEOFF 1.000
CLINBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.050
NODE FRACTIONAL
POHER
TAXI-IDLE 0.050
TAKEOFF 1.000
CLINBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.050
POWER
1 TH
875. 0
17500.0
14875.0
7000.0
875.0
POHER
t TH
875.0
17500.0
14875.0
7000.0
875.0
POHER
t TH
875.0
17500.0
14875.0
7000.0
675.0
EMISSION FUEL USAGE TIME IN
RATE RATE HT FACTOR MODE
LB/HR LB/HR MIN.
75.342 1454.479 .000 19.00
20.761 14829.398 .000 0.70
17.684 12631.184 .000 2.20
32.806 5334.313 .000 4.00
75.342 1454.479 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK IB TH-HR/CYCLE:
LBS POLLUTANT/ 1000K LB TH AT T.O.t
EMISSION FUEL USAGE TINE IN
RATE RATE HT FACTOR MODE
LB/HR LB/HR MIN.
62.941 1454.479 .000 19.00
0.0 UB29.398 .000 0.70
0.0 12631.184 .000 2.20
6.271 5334.313 .000 4.00
62.941 1454.479 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/ 1000K LB TH AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE HT FACTOR MODE
LB/HR LB/HR MIN.
1.T77 1454.479 .000 19.00
209.984 14829.398 .000 0.70
143.585 12631.184 .000 2.20
31.720 5334.313 .000 4.00
1.777 1454.479 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
CO
MASS
LBS.
23.B5B
0.242
0.648
2.187
8.790
35.726
22.025
22.393
1.384
HC
MASS
LBS.
19.931
0.0
0.0
0.418
7.343
27.692
17.072
17.357
0.0
NOX
MASS
195.
0.563
2.450
5.265
2.115
0.207
10.599
6.534
6.643
139.989
FUEL
MASS
LBS.
460.58
173.01
463.14
355.62
169.69
1622.05
FUEL
MASS
LBS.
460.58
173.01
463.14
355.62
169.69
1622.05
FUEL
MASS
Las.
460.58
173.01
463.14
355.62
169.69
1622.05
LB CO /
IK LB FUEL
51.800
1.400
1.400
6.150
51.800
IB HC /
IK LB FUEL
43.274
0.0
0.0
1.176
43.274
LB NOX/
IK LB FUEL
1.221
14.160
11.367
5.946
1.221
ENERGY
f TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
ENERGY
1 TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
ENERGY
t TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
LB CO /
t TH-HR
0.08611
0.00119
0.00119
0.00469
0.08611
LB HC /
TH-HR
0.07193
0.0
0.0
0.00090
0.07193
LB NOX/
f TH-HR
0.00203
0.01200
0.00965
0.00453
0.00203
IV-153
-------
DATE: B/ll/Tl
TEST ORGANIZATION: s w R i TWA
ENGINE SUPPLIER: T H A
ENGINE DATA
CAL ID NUMBER: 339
ENGINE TYPE AND MODEL: JMA -II
SERIAL NUNBFR: ITWA2260I
RATED THRUST: 17500.
ENGINE TOTAL TIHF: 8055. MRS
TINE SINCE HOT SECTION OVERHAUL: 3145. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 6055. HRS
NZ COMPRESSOR OVERHAUL: 8055. HRS
CQKBUSTQR CAN REPLACEMENT: 3145. HRS
FIRST STAGE NOZZLE GUI OF VANE OVERHAUL: 8055. HRS
Nl TURBINE OVERHAUL: 8055. HRS
N2 TURBINE OVERHAUL: 8055. HRS
FUEL: JP-4 TF FUEL H/C RATIO: 2.020
OPERATIONAL DATA «»««
INLET AIR TEMPERATURE, DEGREES F: START 76.00 FINISH
ATMOSPHERIC PRESSURE: START 28.98 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0130
RELATIVE HUMIDITY: 56.00 PFRCFNT
SAMPLE LINE: TFMPFRATURE, DEGREES C: 150.00, FLOM RATE, LITF.RS/NIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 10
COMMENTS:
N02 DETERMINED BY SUBTRACTION.
81.00
28.98
ELAPSED
TIME
0.0
14.00
28.00
35.00
41.00
47.00
57.30
57.00
59.00
65.00
POWER
PERCENT
RATED
T.n.
53
61
81
j
8
9
11
14
19
28
POWER
PERCENT
RATED
T.n.
53
61
61
3
8
9
11
14
19
28
POWER
PERCENT
RATED
r.n.
53
M
61
3
a
9
11
14
19
26
TEST
MODE
I/ 0
71 1
3/ 2
4/ )
7/ 4
8/ 7
9/ 8
IO/ 9
11/10
12/1 1
EXHAUST
r.AS
TFMP
DEGREES F
89H.OO
972.00
1 184.00
540.00
538.00
550.00
561.00
5R3.00
628.00
669 .00
MASS EMI
Cll
LO/IK
LI! FUEL
2.61
?.02
1.33
61 .17
30.45
26.07
70.89
14.94
S.f>4
4.69
CO
POWER ENGINE
THRUST, LBS PERCENT SPEFD
OR RATED RPM
SHP
9360.00
10840.00
14220.00
620.00
1500.00
1750.00
2000.00
7500.00
1500.00
5000.00
EXHAUST
GAS
T.n. NI
53 5660.00
61 5890.00
81 6500. OC
3 2150.00
8 3160.00
9 3370.00
11 3540.00
14 3820.00
19 4310.00
28 4610.00
CO
(MFTI
N2
6267.00
6520.00
6970.00
5240.00
6500.00
6700.00
6950.00
7100.00
7430.00
7730.00
MEASURED
FUEL
FLOW
U8/HH
7R50.00
9110.00
12510.00
1300.00
2000.00
2170.00
2340.00
2660.00
3400.00
4410.00
CO THC Nn
7 IrfEM (WET
GAS GEN
AIR FLOW
IB/SEC
CALC COMPRESSOR ENGINF
F/A DISCHARGE PRESSURE
TEMP RATIO
OFGREES F EPR
204.00
215.00
237.00
58.00
85.10
92.70
98.90
111.80
134.00
157.00
NO
I 2
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
PRFSSURF PPPV (WFT) PPMV PPMV IWETI
PSI A
13.10
15.40
20.60
0. 70
1.80
2.10
2.30
3.00
4.20
6.70
MASS EMI
HC
LB/IK
LB FUFL
0.21
(1.14
O.OS
73.63
70.26
11.74
B.09
5.29
1. F8
n.no
LH/1MTH-HR
2.
1.
1.
126.
40.
17.
24.
15.
8.
4.
185
695
169
56H
596
321
439
901
191
112
PERCENT V
2H.10
24.00
20.00
435. OC
210.00
I7H.OO
145.00
110.00
61.00
II. 00
MASS EMI MASS EMI
N02 CC2
LO/1K L«/1K
LO FUEL LB FUEL
0.31 3128.56
0.55 3129.68
0.22 3110.94
1.62 2834.91
1.43 3029.82
0.72 3060.08
0.47 3076.24
0.45 1095.25
0.70 1114.78
0.21 3123.69
CO
7
2.14 4
7.37 3
3.00 2
1.28 912
1.33 244
1.33 140
1.36 98
1.45 6H
1.40 7.2
1.5' 11
MASS EMI
NO
LB/IK
LB FUFL
6. KB
7.73
10.36
0.61
1.43
2.41
2.84
3.35
4.14
5.62
THC
LB/IK»TH-HR LB/1K«1I!-HR
2623.648
2610.196
2754.439
5944. 168
4039. 75fl
3714.495
3601.543
3293.342
1025.784
2755.096
0.179
0. 171
0.067
154.377
77.015
14.559
9. 460
5.610
1.731
0.704
.00 45.
.00 56.
.no 95.
.00 3.
.00 6.
.00 10.
.00 12.
.00 15.
.00 16.
.00 27.
MASS FM|
NQX
IB/IK
LB FUFL
7.18
fl.28
10.58
7.12
?.86
1.11
3.31
1.79
4.98
5.82
PPMV
00 2.00
00 4.00
00 2.00
00 '.00
00 6.00
00 3.00
00 2.00
00 2.00
00 3.00
00 1.00
MASS bMI MASS
cn
LB/fR
20.45
18.38
16.62
(9.71
60.89
56.56
48.88
19.75
79.37
?0.66
HC
010700
011800
014700
006200
006500
006500
006600
007400
007000
007600
NO
X
IWETI
PPMV
47.00
(.0.00
97.00
10.00
12.00
11.00
14.00
17.00
21.00
78.00
FMI MASS
NO
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
00 1.97
00 2.14
00 2.5B
00 -0.00
00 -0.00
00 -0.00
00 -0.00
00 -0.00
00 -0.00
oo -o.oo
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES SMOKF PARTICULATFS
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
tMI
2
LB/HR Lft/MR
,.
1.
0.
95.
40.
75.
18.
14.
S.
3.
Nn
67 ?.
32 5.
95 ?.
71 2.
52 2.
46 1.
92 1.
07 1.
07 ?..
52 0.
NO
7
LB/1K«TH-MR LB/1K«TM-H9
5.
6.
9 .
1.
1.
2.
3.
3.
4 .
4.
>6 e
497
1 18
456
905
9B1
372
562
06 I
951
0.256
0.464
0. 192
3.398
1.905
0.695
0.554
0.475
0.678
0.183
40
03
73
II
66
57
11
19
37
9?
00 -0.00
00 -0.00
00 -0.00
00 -0.00
oo -o.oo
00 -0.00
00 -0.00
00 -0.00
DO -0.00
00 -0.00
MASS EMI MASS EM
cn2 NO
LB/HR LB/HR
24559.21 53.99
28511.35 70.43
39168.12 129.66
3685.36 0.90
6059.63 2.86
6640.36 5.22
7203.08 6.64
8233.15 8.90
10590.24 14.23
13775.48 2',. 77
Nn
X
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/HH
56.39
75.46
137.39
3.01
5.72
6.79
7.75
10.09
16.61
25.68
L9/1K«TM-HR
6.024
6.961
9.310
.855
.810
.877
.876
.036
.745
5.137
IV-154
-------
CAL ID NUMBER: 339 ENGINE TYPE AND MODEL: JT4A -11
TEST ORGANIZATION: s w a i TWA
SERIAL NUMBER: ITWA2260)
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
TH
875.
17500.
14875.
7000.
875.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
82.774 1473. 194
19.662 15124.785
16.669 12822.031
20.265 6235.242
82.774 1473.194
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
L6S POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
O.B50
0.400
0.050
POWER
t TH
875.
17500.
14875.
7000.
875.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
83.825 1473.194
0.0 15124.785
0.0 12822.031
1.122 62)5.242
83.825 1473.194
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.050
1.000
0.850
0.400
0.050
POWER
TH
875.
17500.
14875.
7000.
875.
0
0
0
0
0
EMISSION FUEL
RATE RATE
L8/HR LB/HR
3.587 1473.194
198.740 15124.785
144.152 12822.031
44.432 6235.242
3.587 1473.194
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
USAGE TINE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLEl
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TM-HR/CYCLE:
LB TH AT T.O.I
USAGE TIME IN
FACTOR MODE
KIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
L8 TH AT T.O.:
CO
MASS
LBS.
26.212
0.229
0.611
1.351
9.657
38.060
22.380
23.856
1.311
HC
MASS
LBS.
26.544
0.0
0.0
0.075
9.T80
36.399
21.403
22.815
0.0
NOX
MASS
LBS.
1.136
2.319
5.286
2.962
0.418
12.121
7.127
7.597
132.493
FUEL
MASS
LBS.
466.51
176.46
470.14
415. 68
171.87
1700.66
FUEL
MASS
LBS.
466.51
176.46
470.14
415.68
171.87
1700.66
FUEL
MASS
L8S.
466.51
176.46
470.14
415.68
171.87
1700.66
LB CO /
IK LB FUEL
56.187
1.300
1.300
3.250
56.187
LB HC /
IK LB FUEL
56.900
0.0
0.0
0.180
56.900
LB NOX/
IK LB FUEL
2.435
13.140
11.242
7.126
2.435
ENERGY
1 TH-HR
277.08
204.17
S45.42
466.67
102.08
1595.42
ENERGY
1 TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
ENERGY
f TH-HR
277.08
204.17
545.42
466.67
102.08
1595.42
LB CO /
1 TH-HR
0.09460
0.00112
0.00112
0.00289
0.09460
LB HC /
TH-HR
0.09580
0.0
0.0
0.00016
0.09580
LB NOX/
TM-HR
0.00410
0.01136
0.00969
0.00635
0.00410
IV-155
-------
DATE) 6/ 2/71
TEST ORGANIZATION: s x R i TWA
ENGINE SUPPLIER: TWA
ENGINE nATA
CAL ID NUMBER: 2<>o
ENGINE TYPE AND MODEL: JTBO-1
SERIAL NUMBER: P649125B
RATED THRUST: 14000.
ENGINE TOTAL TIME: 14289. HRS
TIME SINCE HCU SECTION OVERHAUL! 3433. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 9943. HRS
N2 COMPRESSOR OVERHAUL: 9843. HRS
COMBUSTOR CAN REPLACEMENT: 8843. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 8643. HRS
Nl TURBINE OVERHAUL: 8843. HRS
N2 TURBINE OVERHAUL: 8843. HRS
FUEL: JP-* TF FUEL M/C RATIO: 2.020
OPERATIONAL DATA »«««««4«.«««>«
INLET AIR TEMPERATURE. DEGREES F: START 63.00 FINISH
ATMOSPHERIC PRESSURE: START 28.96 FINISH
INLET AIR HUMIDITY, LflS H20/LB AIR: 0.0127
RELATIVE HUMIDITY: 49.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: ISO.00, FLOW RATE, LITERS/MIN:
SAMPLE LINF TRANSPORT TINE, SEC: 1.00
NUMBER OF TESTS: 5
COMMFNTS:
N02 DETERMINED BY SUBTRACTION.
93.00
28.96
ELAPSED
TIME
0.0
I7.no
30.00
35.00
47.00
TEST
MODE
I/ 0
2/ 1
3/ 2
4/ 3
5/ 4
POWER
THRUST, LBS PERCENT
OK RMFO
SHP
9660.00
1 1490.00
12520.00
800.00
12420.00
T.O.
68
HI
69
5
69
FNGINE
SPEED
RPM
Nl
7310.00
7720.00
7990.00
2590.00
7950.00
N2
UCflO.OO
U400.no
11510. OC
6770.00
11490.00
MEASURED
FUEL
FLOW
LB/HR
5640.00
6790.00
7590.00
880.00
7590.00
GAS GEN
AIR FLOW
L8/SEC
114.60
127.80
133.50
32.20
134.40
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.
0.
0.
0.
0.
013700
014700
015800
007600
015700
DEGREES F
-0.00
-0.00
-0.00
-o.on
-0.00
FNGINE
PRESSURE
RATIO
EPR
1.65
1.79
1.90
-0.00
-0.00
TUR3INE
INLET
TEMP
OEGREFS F
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
68
81
89
5
EXHAUST
GAS
TEMP
DEGREES F
919.00
996.00
1026.00
741.00
1038.00
EXHAUSI
GAS
PRESSURE
PSIA
9. 10
11.20
12.60
0.50
12.50
CO
(WET)
PPMV
16.00
13.00
12.00
394.00
11.00
CC
2
(WET)
PERCENT V
2.90
2.96
3.07
1.59
3.12
THC
IWFT)
PPMV
1.00
0.0
0.0
202.00
1.00
NO
IWETI
PPMV
61.00
94.00
105.00
4.00
104.00
NO
7
(WET)
PPMV
5.00
5.00
S.OO
7.00
5.00
NO
X
IbETI
PPMV
66.00
119.00
110.00
11.00
109.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
68
81
19
5
88
MASS FMI
CO
LB/1K
LB FUEL
1.14
0.88
0. 78
47.M
0.93
MASS EMI
HC
IB/ IK
LB FUEL
C.04
0.0
0.0
13.99
0.04
MASS EMI
N02
LI/IK
LB FUEL
0.51
0.55
0.53
1.39
0.52
ASS EMI
C02
LB/U
LB FUEL
31 31.34
31 11.86
3132.02
3020.04
3131. B4
MASS EH!
NO
LH/IK
1. B FUFL
7.13
9.29
1 1.20
0.79
10.91
MASS EMI
NOX
LB/1K
LB FUEL
7.72
9.94
11.73
2.18
11.44
MASS EM|
CO
LB/HR
6.42
5.94
5.91
41.91
6.30
MASS EMI
HC
LB/HR
0.23
0.0
0.0
12.31
0.2H
MASS EMI
N32
Lfl/HR
3.30
3.75
4.05
1.22
3.98
MASS FMI
C02
LB/HR
17660.76
21234.04
23772.00
2657.63
23770.63
MASS EMI
NO
LB/HR
40.22
62.99
85.00
0.70
82.83
Mass EMI
rtUX
LB/HH
43.52
66.74
19.04
1.92
86. Bl
POWER
OFRCCNT
BATED
T.O.
81
89
5
88
CD
L»/IK«TH-H8
0.665
0.517
0.472
52.192
O.SOH
LB/1K#TH-HH
1828.236
18'i9.<,56
1898.722
3122.042
1913.H99
THC
LH/1MTH-HR
0.074
0.0
0.0
15.314
0.022
NO
LB/1KHTH-HK
5.48 J
6.789
O.B74
6.669
LB/1K«TH-HR
0.341
0.327
0.123
1.529
0.121
LB/1MTH-HB
4.505
5.H14
7.112
2.403
6.990
IV-156
-------
CAL 10 NUMBER: 290 ENGINE TYPE AND MODEL: JT8D-1
TEST ORGANIIATION: S V R 1 TWA
SERIAL NUMBER I P649125B
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWF.R
0.060
1.000
0.850
0.400
0.060
POWER
1 TH
840.
14000.
11900.
5600.
840.
POWER
TH
840.
14000.
11900.
5600.
840.
POWER
TH
840.
14000.
11900.
5600.
840.
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
44.872 892.665
7.696 8832.207
7.503 7263.258
18.495 3536.526
44.872 692.665
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
L8S POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
13.341 892.665
0.768 8832.207
0.632 7263.258
0.858 3536.526
13.341 692.665
TOTAL FOR CYCLE:
L8S POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
1.780 892.665
122.597 8832.207
78.214 7261.258
13.520 3536.526
1.780 892.665
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
L8S POLLUTANT/IK LB
LBS POLLUTANT/1000K
USAGE TIME IN
FACTOR MODE
MIN.
1.000 19.00
1.000 0.70
1.000 2.20
I. 000 4.00
I. 000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-MR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
NIN.
1.000 19.00
1.000 0.70
1.000 2.20
1. 000 4.00
1.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
14.209
0.090
0.275
1.213
5.235
21.042
21.213
15.719
0.641
HC
MASS
LBS.
4.225
0.009
0.021
0.05T
1.556
5.871
5.918
4.391
0.640
NOX
MASS
LBS.
0.564
1.430
2.868
0.901
0.208
5.971
6.019
4.466
102.164
FUEL
MASS
LBS.
282.68
103.04
266.32
235.77
104.14
991.95
FUEL
MASS
LBS.
2B2.68
103.04
266.32
235.77
104.14
991.95
FUEL
MASS
LBS.
282.68
103.04
266.32
235.77
104.14
991.95
LB CO /
IK LB FUEL
50.267
0.871
1.033
5.230
50.267
LB HC /
IK LB FUEL
14.946
0.087
0.087
0.242
14.946
LB NOX/
IK LB FUEL
1.994
11.881
10.768
1.823
1.994
ENERGY
TH-HR
266.00
163.33
436.33
373.31
98.00
1337.00
ENERGY
( TH-HR
266.00
163.33
416.13
173.33
98.00
1137.00
ENERGY
1 TH-HR
266.00
163.33
436.33
171.11
98.00
1117.00
LB
i
0
0
0
0
0
LB
0
0
0
0
0
LB
0
0
0
0
0
CO /
TH-HR
.05142
.00055
.00063
.00330
.05142
HC /
TH-HR
.01568
.00005
.00005
.00015
.01568
NOX/
TH-HR
.00212
.00876
.00657
.00241
.00212
IV-157
-------
DATE: T/15/71
TEST ORGANIZATION: S W R
ENGINE SUPPLIER: TWA
ENGINE OATH
CAL ID NUMBER: 300
ENGINE TYPE AND MODEL: JT8D-1
SERIAL NUMBER: 649L37B
RATED IHRUST: 14000.
ENGINE TOTAL TIME: 8574. MRS
TIME SINCE HOT SECTION OVERHAUL: 2789. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 8574. MRS
N2 COMPRESSOR OVERHAUL: 857*. MRS
COMBUSTdR CAN REPLACEMENT: 2789. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 2789. HRS
Nl TURBINE OVERHAUL: 8574. HRS
N2 TURBINE OVERHAUL: 8574. HRS
FUEL H/C KATIO: 2.020
72.00
7B.B7
FUEL: JP-4 TF
OPERATIONAL DATA ««««.»«««««««««««««« ,......«
INLET AIR TEMPERATUREi DEGREES f : START 72.00 FINISH
ATMOSPHERIC PRESSURE: START 28.87 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0143
RELATIVE HUMILITY: 82.00 PERCENT
SAMPLE LINE: TFMPERATURF, DEGREES C: 150.00, FLOW RATE, LITFRS/MIN:
SAMPLE LINE TRANSPORT TIMF, SEC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
F/A AND AIRFLOW CALCULATED FROM EXHAUST COMPOSITION FOR FOURTH RUN. N02
DETERMINED BY SUBTRACTION.
42.50
ELAPSED
TIME
0.0
4.00
7.30
12.50
14.50
TEST
MODE
I/ 0
2/ 1
3/ 2
4/ 3
5/ 4
POWER
THRUST, LBS PERCENT
OR RATED
SHP
9600.00
11310. TO
13040.00
680.00
M040.no
T.O.
68
80
93
4
93
ENGINE
SPEED
RPN
Nl
72'O.OD
7680.00
Bono.oo
2520.00
H100.00
N2
11140.00
11470.00
11750.00
6620.00
11780.00
MEASURED
FUEL
FLOW
LB/HR
5530.00
6620.00
7760.00
950.00
7810.00
GAS GEN
AIR FLOW
LB/SEC
115.30
127.70
140.10
26.40
140.10
CALC COMPRESSOR
F/A DISCHARGE
TFNP
0.013300
0.014400
0.015400
0.010000
0.015500
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.65
1.80
1.94
-0.00
1.90
TURBINE
INLET
TE»P
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
68
80
93
EXHAUST
GAS
TEMP
OEGRtES F
852.00
915.00
990.00
687.00
990.00
PRESSURE
PS I A
9. 10
11.20
13.30
0.40
U.30
CO
IWFTI
PPMV
37. 00
15.00
6.00
474.00
77.00
CO
2
IWFI)
PERCENT V
2.63
2.72
2.98
1.95
.1.19
THC
(WETI
PPMV
4.00
4.00
5.00
152.00
10.00
NC
(WETI
PPMV
50. PO
63.00
fll.OO
3.00
60.00
NO
2
(WEII
PPMV
6.00
4.00
3.00
8.00
7.00
NO
X
IWET)
PPMV
56.00
67.00
84.00
11.00
H7.00
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
PARMCULATES
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.n.
68
80
93
MASS EMI
cn
LB/IK
LB FUEL
?.4?
1.10
0.40
46.97
1. 37
MASS EMI
HC
LB/1K
LB FUEL
0.17
0.17
0.19
8.63
0.36
MASS FMI
NO?
LB/1K
LB FUF.L
0.75
0.4H
0.33
1.30
0.7?
MASS EMI
C02
LB/1K
L» FUFL
3128.96
3131.06
3132.08
3015. 79
3130. 10
MASS EMI
Ntl
Lfl/1*
LB FUEL
6.22
7.58
fl.90
0.49
B.21
MASS FMI
NOX
LB/1K
LB FUEL
6.96
8.06
9.23
1.79
8.92
MASS EMI
cn
LB/HR
13.40
7.27
3.11
44.67
10.73
MASS EMI
HC
LB/HR
0.96
I. 11
1.49
8.19
2.79
MASS EMI
N02
LB/HR
4.13
3. 19
2.56
1.24
5.61
MASS FMI
CO 2
LB/HR
17303. U
20727.59
24304.96
2884.00
24446.09
MASS EMI
NO
LB/HR
34.39
50. 19
69.06
0.46
64.09
MASS EMI
NOX
LP/HR
38.57
53.37
71.62
1.70
69.70
POWER
PERCENT
"ATED
T.O.
68
no
93
cu
LR/lKiTH-HR
1.396
0.642
0.239
65.613
O.H23
LB/ 1M TH-HR
IK02.410
1829.443
1863.877
4241.168
1874.700
THC
L3/1KHTH-HR
(1.100
0.09B
0.114
12.050
LB/1KHTH-HR
3.582
4.430
5.796
0.68?
4.915
LB/IK HTH-HR
0.430
0.281
0. 196.
1.819
0.430
NO
X
LB/IK«TH-HR
4.012
4.711
5.492
2.SOI
5.345
IV-158
-------
CAL ID NUMBER: 300 ENGINE TYPE AND MODELi JTBD-I
TEST ORGANIZATION: S U R I TWA
SERIAL NUMBER: 649L37B
MODE
TAXI-IDLE
TAKEOFF
CLIHBQUT
APPROACH
TAXI-IDLE
FRACTIONAL
POMER
0.060
1.000
0.850
0.400
0.060
POMER
1 TH
840.0
14000.0
11900.0
5600.0
B40.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
46.934 1049.424
10.863 8464.215
12.603 6975.336
21.337 3388. 150
48.934 1049.424
USAGE TIME IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLEl
L8S POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000*
MODE
TAII-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POMER
TH
640.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
8.073 1049.424
1.490 6*64.215
1.228 6975.336
1.276 3388.150
8.073 1049.424
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POMER
0.060
1.000
0.850
0.400
0.060
POWER
1 TH
840.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.744 1049.424
85.298 8464.215
58.072 6975.336
15.198 3388.150
1.744 1049.424
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIKE IN
FACTOR NODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
15.496
0.127
0.462
1.422
5.709
23.216
22.428
17.364
0.905
HC
MASS
LBS.
2.557
0.017
0.045
0.085
0.942
3.646
3.522
2.727
1.241
NOX
MASS
LBS.
0.552
0.995
2.129
1.013
0.204
4.894
4.727
3.660
71.082
FUEL
MASS
LBS.
332.32
98.75
255.76
225.88
122.43
1035.14
FUEL
MASS
LBS.
332.32
98.75
255.76
225.88
122.43
1035.14
FUEL
MASS
LBS.
332.32
98.75
255.76
225.88
122.43
1039.14
LB CO /
IK LB FUEL
46
1
1
6
46
.629
.283
.807
.297
.629
IB HC /
IK LB FUEL
7
0
0
0
7
.693
.176
.176
.377
.693
LB NDX/
IK LB FUEL
1
10
8
4
1
.662
.078
.325
.485
.662
ENERGY
1 TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
( TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
> TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
LB CO /
TH-HR
0.05825
0.00078
0.00106
0.003BI
0.05825
LB HC /
TH-HR
0.00961
0.00011
0.00010
0.00023
0.00961
LB NOX/
TH-HR
0.00208
0.00609
0.00488
0.00271
0.00208
IV-159
-------
DATE: 8/ 5/71
TEST ORGANIZATION: S W R
FNGINE SUPPLIER: TWA
ENSINE DATA ««»
CAL ID NUMBER: 316
FNGINE TYPE AND MODEL: JTBD-1
SERIAL NUMBER: P6*9I85B
RATED THRUST:
ENGINE TOTAL TIME:
TIME SINCE HOT SECTION OVERHAUL:
TIME SINCE:
1*000.
157*5. MRS
2685. HRS
NI COMPRESSOR OVERHAUL:
NZ COMPRESSOR OVERHAUL:
COMBUSTOR CAN REPLACEMENT:
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL:
NI TURBINE OVERHAUL:
N2 TURBINE OVERHAUL:
119*5. HRS
119*5. HRS
2685. HRS
119*5. HRS
119*5. HRS
119*5. HRS
FUEL H/C RATin: 2.020
70.00
29.11
FUEL: JP-* TF
OPERATIONAL DATA ««»»««««««
INLET AIR TEMPERATURE, DEGREES F : START 71.00 FINISH
ATMOSPHERIC PRESSURE: START 29.10 FINISH
INLET AIR HUMIDITY, LBS H2H/LB AIR: 0.0127
RELATIVE HUMIDITY: 72.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 150.00, FLOU RATE, LITERS/HIN:
SAMPLE LINF TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: fl
COMMENTS:
N02 OETEPMINEn BY SUBTRACTION. THIS TEST IS THE FIRST OF THREF RUN ON THIS
FNGINE. THE FUEL USED CONTAINED NO CI-2.
ELAPSED
TIME
0.0
7.00
11.20
18.10
2*. 45
?7.*5
29. *0
12.30
TEST
MODE
I/ 0
21 1
I/ 2
*./ 3
T/ 4
«l 1
11 B
in/ i
POWER
THRUST, LBS PERCFNT
OR RATED
SHP
9560.00
11500.00
13100.00
1050.00
1520.00
2500.00
5020.00
7120.00
T.O.
68
62
93
7
10
17
35
50
FNGINF
SPEED
kPH
NI
7300.00
7750.00
8140.00
2" 70. 00
1540.00
4340.00
5B'.0.00
MiOO.OO
N2
11000.00
11340.00
11630.00
7350.00
8"30.00
8970.00
9'I9;).00
10530.00
MEASURFD
FUEL
FLOW
LB/HR
5610.00
6810.00
7940.00
1060.00
1*00.00
2010.00
3020.00
*090.00
GAS GFN
AIR FLOW
LB/SEC
115.60
130.00
141.10
37.10
42.40
54.90
80.40
97.80
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.01)500
0.014500
0.015600
0.007900
0.009200
0.010200
0.010400
0.011*00
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.65
1.80
1.95
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINF
INLET
TEMP
DbGRFES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PGWF.R EXHAUST
PEKCFNT GAS
PATEO TFfP
T.O. DECREES F
68
82
91
7
10
17
35
50
865.00
925.00
9fl8.no
649.00
614.1"
7'.?. 00
S04 . ')'t
r*H. in
EXHAUST
GAS
PRESSURE
PSIA
9.4"
11.50
13.50
0.70
1 . in
I. .1 )
4. !0
6. 21)
CO
I WETI
PPMV
29. CO
?o. nn
16.00
3flfl . 00
300. 0')
1 '.7.. 10
so .on
>'l..)0
CO
2
IhETI
PERCENT V
2.75
2.95
3.16
1 .64
1 .*"
2 . 0/1K
Li FUEL
6.90
8.21
9.63
2.91
3.23
3.42
4.29
5.33
OSS F.«[
rr>
LT/HH
11.78
9.20
8.01
48.61
43.50
30.80
15.79
13.63
»:$ FM
fC
LB/MK
O.C
0.0
0.0
6.03
4.32
2.40
0.97
0.20
MASi L"l
Nfl2
1 H/HR
3.3*
3.78
*.9*
1.65
1.67
2.50
0.46
2.10
"A5r, "Ml
CJ2
LD/HR
N.I
LB/I-K
3.34
3.78
4.94
1.65
1.67
2.50
0.46
2.10
1 7558.96
21122.. 91
24865.35
3228.32
4306.33
62*2.86
943*. 92
12792.99
35.38
52.1*
71.57
1.4*
2.86
*.37
12.50
19.52
38.71
55.92
76.50
3.09
4.51
6.87
17.97
21. 81
POKER
PERCENT
RATED
T.O.
68
82
91
7
10
17
35
50
C'J
LB/IK* TH-HR
1.233
0.900
0.612
46.295
28.621
1?.319
3. 1*5
1.91*
LR/IMTH-HR
1836.712
185*.166
1198.118
307*.593
2833.114
2*97.1*3
1879.465
I 796.769
THC
Irt/lK*TH-HR
0.0
0.0
0.0
5.740
2.841
0.968
0. 193
0.028
NO
LB/1MITH-HP
3.701
4.534
5.463
1.372
1 .880
1 .749
? .491
2.741
LB/1IH1H-HR
0.149
0. 379
0.377
1. 568
1. 097
0.999
0.092
0.377
NO
X
Lfl/lK«TH-HR
4.050
*.862
5.4*0
2.9*0
2.977
2.7*8
2.583
3.063
IV-160
-------
CAL ID NUMBER: 316 ENGINE TYPE AND MODELi JISD-I
TEST ORGAN11AT10N: S K R 1 TWA
SERIAL NUMBER: P649iasa
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLIM80UT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIHSOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POKER
0.060
1.000
0.650
0.400
0.060
POKER
TH
840.0
14000.0
11900.0
5600.0
840.0
POHER
1 TH
840.0
14000.0
11900.0
5600.0
840.0
POKER
TH
840.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL
RATE RATE KT
LB/HR LB/HR
91.645 746.851
5.374 8484.348
9.532 7148.559
17.154 3492.050
51.645 746.851
TOTAL FOR CYCLE:
IBS POLLUTANT/IK LB
L8S POLLUTANT/IK L8
IBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE KT
LB/HR L8/HR
5.938 746.851
0.0 8484.348
0.0 7148.559
0.835 3492.050
5.038 7*6.851
TOTAL FOR CYCLE:
L8S POLLUTANT/IK LB
L8S POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE KT
LB/HR LB/HR
1.910 746.851
94.082 8484.348
61.555 7148.559
16.980 3492.050
1.910 746.851
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
USAGE TINE IN
FACTOR NODE
NIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
NIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR NODE
NIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
16.354
0.063
0.350
1.144
6.025
23.935
26.087
17.902
0.44B
HC
NASS
LBS.
1.880
0.0
0.0
0.056
0.693
2.629
2.865
1.966
0.0
NOX
MASS
LBS.
0.605
1.098
2.257
1.132
0.223
5.314
5.792
3.975
78.401
FUEL
MASS
LBS.
236.50
98.98
262.11
232.80
87.13
917.54
FUEL
MASS
LBS.
236.50
98.98
262.11
212. 80
87.13
917.54
FUEL
MASS
LBS.
236.50
98.98
262.11
232.80
87.13
917.54
LB CO /
IK LB FUEL
69.151
0.633
1.333
4.912
69.151
L8 HC /
IK LB FUEL
7.950
0.0
0.0
0.239
7.930
LB NOX/
IK LB FUEL
2.558
11.089
B.611
4.863
2.558
ENERGY
TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
1 TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
1 TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
LB CO /
1 TH-HR
0.06148
0.00038
o.oooao
0.00306
0.0614B
LB HC /
1 TH-HR
0.00707
0.0
0.0
0.00015
0.00707
LB NOX/
1 TH-HR
0.00227
0.00672
0.00517
0.00303
0.00227
IV-161
-------
0»TE! 8/ 5/71
TEST ORGANIZATION: S W R I TWA
ENGINE SUPPLIER; T w A
ENGINE DATA «
CAL 10 NUMBEK: JIT
ENGINE TYPE AND MODEL: JTBD-l
SERIAL NUMBER: P649185B
RATED THRUST:
ENGINE TOTAL TIME:
TIME SINCE HOT SECTION OVERHAUL:
TIME SINCE:
14000.
15745. MRS
2689. MRS
NI COMPRESSOR OVERHAUL:
N2 COMPRESSOR OVERHAUL:
COMBUST1R CAN REPLACEMENT:
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL:
Nl TURBINE OVERHAUL:
NZ TURBINE OVERHAUL:
11945. HRS
11945. HRS
2685. HRS
11945. HRS
11945. HRS
11945. HRS
FUEL H/C RATIO: 2.020
69.00
29.11
FUEL: jp-4 TF
OPERATIONAL DATA »«»
INLET AIR TEMPERATURE, DEGREES f: START 69.00 FINISH
ATMOSPHERIC PRESSURE: START 29.11 FINISH
INLFT AIR HUMIDITY. LBS H20/L8 AIR: 0.0121
RELATIVF HUMIDITY: 49.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 4
COMMENTS:
N02 DETERMINED BY SUBTRACTION. THIS TEST IS THE SECOND OF THREE RUN ON THIS
ENGINE. THE FUEL USED CONTAINED THE NORMAL CONCENTRATION OF CI-2 I0.lt BY
VOLUME).
ELAPSED
TIME
0.0
6.30
9.15
12.00
TEST
MODE
I/ 0
21 1
3/ 2
4/ 1
THRUST
OR
SHP
9540.
11460.
1)060.
1080.
POWER
,L6S PERCENT
RATED
00
00
00
00
r.o.
68
81
93
7
ENGINE
SPEED
RPM
Nl
7250. OC
7140.00
8110.00
3020.00
N2
10940.00
11120.00
11580. 00
7350.00
MEASURED
FUEL
FLOW
LB/HR
5590.00
6780.00
7P40.00
1070.00
GAS GEN
AIR FLOW
LB/SEC
115.20
129.70
140.20
36.60
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.013500
0.014500
0.015500
0.008100
DEGREES F
-0.00
-o.no
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.n.
69
81
91
7
EXHAUSt
GAS
TEMP
DEGREES f
8S2.00
919.00
977.00
649.00
F XHAUST
GAS
PRESSURE
PS I A
9.30
11.50
13.40
0.70
CO CO
(WETI 2
PPMV IWETI
PERCENT V
43.00
37.00
23.00
397.00
2.71
7.91
3.10
1.68
THC
IUETI
PPMV
0.0
0.0
0.0
110.00
NG NO
IWETI 2
PPMV IWETI
PPMV
50.00
67.00
83.00
9.00
3.00
3.00
5.00
5.00
NCI
X
(HETI
PPMV
53.00
70.00
88.00
14.00
ALDEHYDES SMOKE PART ICllL AT ES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-O.OD
POWER
PERCENT
RATED
T.O.
68
81
93
MASS E»I
ca
LB/1K
LR FUEL
3. 16
2.53
1.48
45.74
MASS EMI
HC
LB/IK
LB FUEL
0.0
0.0
0.0
7.26
MASS FMI
nm
L8/1K
LB FUEL
0.36
0.34
0.53
0.95
MASS EMI
C02
LR/IK
LU FUEL
512B.28
3129.26
3130.92
3041.46
MASS EMI
NO
LB/1K.
LB FUEL
6.03
7.53
8.76
1.70
MASS EMI
NOX
IB/ IK
LB FUEL
6.40
7.87
9.29
2.65
PASS EM
co
LS/HR
1 7.66
17.17
11.59
48.94
:
18)3.026
1851.344
1879.510
3013.293
THC
LB/1MTM-HR
0.0
0.0
n.o
7.19?
NO
LB/lKdTH-HR
3.53d
4.456
5.261
1.68H
LB/1KV1H-HK
0.212
0.200
0.317
0.938
NO
X
LB/IKfTH-HR
3.748
4.656
5.57B
2.625
IV-162
-------
CAL 10 NUMBER: 31T ENGINE TYPE AND MODEL: jreo-i
TEST ORGANISATION: s M R I THA
SERIAL NUMBER: P649185B
MODE
TAXI-IDLE
TAKEOFF
CLIMBdUT
APPROACH
TAXI-IOLE
MODF
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POHER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POHER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
POMER
1 TH
840.0
14000.0
11900.0
5600.0
840.0
POWER
TH
840.0
14000.0
11900.0
5600.0
840.0
POKER
1 TH
840.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL USAGE TIME IN
RATE RATE UT FACTOR MODE
LB/HR LB/HR HIN.
52.051 817.867 .000 19.00
8.724 8500.332 .000 0.70
16.712 7100.117 .000 2.20
16.477 3417.406 .000 4.00
52.051 B17.867 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE)
LBS POLLUTANT/IK LB TH-HR/CVCLEl
LBS POLLUTANT/1000K LB TH AT T.Q.:
EMISSION FUEL USAGE TIME IN
RATE RATE MT FACTOR MODE
LB/HR LB/HR MIN.
7.905 817.867 .000 19.00
0.170 8500.332 .000 0.70
0.142 7100.117 .000 2.20
0.243 3417.406 .000 4.00
7.905 817.867 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CVCLE:
LBS POLLUTANT/IOOOK LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE MT FACTOR MODE
LB/HR LB/HR MIN.
2.007 817.867 .000 19.00
90.146 8500.332 .000 0.70
60.243 7100.117 .000 2.20
15.679 3417.406 .000 4.00
2.007 817.867 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/IOOOK LB TH AT T.O.:
CO
MASS
LBS.
16.483
0.102
0.613
1.098
6.073
24.368
25.876
18.226
0.727
MC
MASS
LBS.
2.503
0.002
0.005
0.016
0.922
3.449
3.662
2.579
0.142
NOX
MASS
LBS.
0.695
1.052
2.209
1.045
0.234
5.175
5.496
3.871
75.121
FUEL
MASS
LBS.
258.99
99.17
260.34
227.83
95.42
941.74
FUEL
MASS
LBS.
258.99
99.17
260.34
227.83
95.42
941.74
FUEL
MASS
LBS.
258.99
99.17
260.34
227.83
95.42
941.74
LB CO /
IK LB FUEL
63.642
1.026
2.354
4.822
63.642
LB HC /
IK LB FUEL
9.665
0.020
0.020
0.071
9.665
LB NOX/
IK LB FUEL
2.454
10.605
8.485
4.588
2.454
ENERGY
1 TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
1 TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
1 TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
LB CO /
t TH-HR
0.06197
0.00062
0.00140
0.00294
0.06197
LB HC /
TH-HR
0.00941
0.00001
0.00001
0.00004
0.00941
LB NOX/
TH-HR
0.00239
0.00644
0.00506
0.00280
0.00239
IV-163
-------
DATE: B/ 5/71
TEST ORGANIZATION: s u R I TNA
ENGINE SUPPLIFR: T H A
ENGINE DATA
CAL ID NUMBER: lia ENGINE TYPE AND MODEL: JT8D-I
RATED THRUST: 14000.
FNGINE TOTAL TIME: 15T45. MRS
TIME SINCE HOT SECTION OVERHAUL: 2689. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 11945. MRS
N2 COMPRESSOR OVERHAUL: 11145. MRS
COHBUSTQR CAN REPLACEMENT: 261)5. MRS
FIRST STAGE NOZZLE GUI OF VANF OVERHAUL: 11145. MRS
NI TURBINE OVERHAUL: 11945. MRS
N2 TURBINE OVERHAUL: 11945. HRS
SERIAL NUMBER: P64«ie5B
FUEL H/C RATIO: 2.020
69.00
29.11
FUEL: jp-4 IF
OPERATIONAL DATA »»
INLET AIR TEMPERATURE, Of.GRf.ES F: START 69.00 FINISH
ATMOSPHERIC PRESSURE: START 29.11 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0119
RELATIVE HUMIDITY: 66.00 PERCFNT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOM RATE, LITFRS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 4
COMMENTS:
M02 OETERNINFD BY SUBTRACTION. THIS TEST IS THE LAST OF THREE RUN ON THIS
ENGINE. THE FUEL USED CONTAINED THE MINIMUM CONCENTRATION (IF CI-2 10.0125*
flY VOLUME!.
FLAPSEO
TIMF
TFST
MODE
POMER
THRUST, LBS PERCENT
OR RATFD
SHP
0.0
3. 15
6.00
9.00
I/ 0
11 I
3/ 2
4/ 3
9680
11480
12980
1040
.00
.00
.00
.00
T.O.
69
81
92
7
f NGINf
SPEED
RPM
NI
7300.00
7730.00
8090.00
2990.00
N2
11010.00
1130.00
11570.00
7300.00
MF.ASURFO
FUEL
FLOW
LB/HR
5660.00
6790.00
7070.00
1060.00
CSS GEN
AIR FLOW
IB/SEC
116.70
129.70
140.40
35.70
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.011500
0.014500
0.015600
0. 008200
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TIMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
r.n.
69
ai
92
7
EXHAUST
GAS
TEMP
DEGREES F
556.00
419.00
975.00
65 A. 00
FXHAUST
GAS
PRESSURE
PSI A
9.80
11.50
13.40
0.70
CO CO
(NET) ?
PPMV IHETI
PERCFNT V
42.00
35.00
31.00
398.00
2.76
2.96
3.17
1.70
THC
(MET)
PPMV
0.0
0.0
0.0
80.00
NO NO
I WET I 2
PPMV (WETI
PPMV
54.00
69.00
86.00
7.00
3.00
5.00
4.00
9.00
NO ALDEHYDES
X
(WET)
PPMV
57.00
74.00
90.00
16.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
POMER
PERCENT
RATED
T.n.
69
ai
92
7
M»SS EMI
CO
Lfl/lK
L* FUEL
1.03
2.16
1.95
44. 29
MASS FMI
Hr
L B/ IK
LB FUEL
0.0
0.0
0.0
5.21
MASS FMI
NO?
LB/IK
LI FUCL
0.16
0.55
0.41
1.69
MASS EMI
C02
LP/IK
LH FUEL
3128.48
3129.54
11 JO. 18
104"). 10
MASS FMI
WO
LB/1K
LB FUEL
6.40
7.61
8. 88
1.31
MASS CMI
NOX
LP/IK
LB FUEL
6.75
8. in
9.29
3.00
MASS FM
CO
LB/HR
17.15
15.99
15.33
46.95
MASS CMI
HC
Lfl/HR
0.0
0.0
0.0
5.54
MASS EMI
NO 2
LB/HR
MASS FMI
C02
LB/HR
MASS EMI
NO
LB/MR
MASS EMI
NOX
LB/HR
2.01 17707.19
3.75 21249.57
3.25 24634.52
1.79 3232.25
36.22
51.76
69.87
1.39
3B.21
55.54
73.12
3.18
POUFB
PERCENT
RATF.D
T.n.
69
fll
92
7
CO
LB/ IKMH-HH
1.772
I .393
I. 181
45.146
LB/1KHTH-HR
1829.255
1851.008
1R97.883
3107.938
THC
LB/1MTH-HR
0.0
0.0
0.0
5.311
NO
LB/1K»TH-HR
3.741
4.511
5.381
1 .13B
LB/1K1TH-HR
0.20P
0.327
0.250
1.720
NO
X
LB/1KITH-HR
3.949
4.918
5.611
1.058
IV-164
-------
CAL ID NUMBER: 318 ENGINE TYPE AND MODELI JT8D-1
TEST ORGANIZATION: S N R I THA
SERIAL NUMBERI P649185B
MODE
TAXI-IOLE
TAKEOFF
CLIM80UT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
HOOF
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAKI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
o.»oo
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POMER
TH
840.
14000.
11900.
5600.
840.
POWER
f TH
840.
14000.
11900.
5600.
840.
POWER
f TH
840.
14000.
11900.
5600.
840.
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
EMISSION FUEL
RATE RATE MT
LB/HR LB/MR
37.416 750.110
13.041 8619.195
15.219 7198.500
17.525 3490.320
37.916 750.110
TOTAL FOR CYCLE:
L8S POLLUTANT/IK L8
LBS POLLUTANT/IK LB
IBS POLLUTANT/ 1000K
EMISSION FUEL
RATE RATE «T
LB/HR LB/HR
6.098 750.110
0.181 8619.195
0.059 7198.500
0.437 3490.320
6.098 790.110
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
2.051 750.110
93.047 8619.195
61.150 7198.500
17.143 3490.320
2.051 750.110
TOTAL FOR CYCLE:
LBS POLLUTANT/IK IB
LBS POLLUTANT/ IK LB
LBS POLLUTANI/1000K
JSAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
JSAGE TIME IN
FACTOR MODE
NIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE!
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
NIN.
I .000 19.00
I. 000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL/CYCLE)
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
12.007
0.152
0.558
1.168
4.424
18.309
19.853
13.694
1.087
HC
MASS
LBS.
1.931
0.002
0.002
0.029
0.711
2.676
2.902
2.001
0.151
NOX
MASS
LBS.
0.650
1.086
2.242
1.143
0.239
5.359
5.811
4.009
77.539
FUEL
MASS
LBS.
237.53
100.56
263.94
232.69
87.51
922.24
FUEL
MASS
LBS.
237.53
100.56
263.94
232.69
87.51
922.24
FUEL
MASS
LBS.
237.53
100.56
261.94
232.69
87.51
922.24
LB CO /
IK LB FUEL
50.548
1.513
2.114
5.021
50.548
LB HC /
IK LB FUEL
8.130
0.021
0.008
0.125
8.130
LB NOX/
IK LB FUEL
2.734
10.795
8.495
4.912
2.734
ENERGY
f TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
f TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
LB
1
0
0
0
0
0
LB
1
0
0
0
0
0
LB
<
0
0
0
0
0
CO /
TH-HR
.04514
.00093
.00128
.00313
.04514
HC /
TH-HR
.00726
.00001
.00000
.00008
.00726
NOX/
TH-MR
.00244
.00665
.00514
.00306
.00244
IV-165
-------
DATE: 7/21/71
TEST ORGANIZATION: S w R I TUA
ENGINE SUPPLIER: TUA
FNGINF DATA «
CAL 10 NUMBER: 276
ENGINE TYPE AND MODEL! JTRD-7
SERIAL NUMBER: PA54S64B
RATED THRUST: 14000.
ENGINE TOTAL TINE: 0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: o. MRS
N2 COMPRESSOR OVERHAUL: o. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL: JP-4 TF FUEL H/C RATIO: 2.020
OPERATIONAL DATA «««4««««
INLET AIR TEMPERATURE, DECREES F: START 72.00 FINISH
ATMOSPHERIC PRESSURE: START 28.98 FINISH
INLET AIR HUMIOITV, LBS M20/LB AIR: 0.0121
RELATIVE HUMIDITY: 5n.oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/KIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 4
COMMENTS:
N02 DETERMINED BY SUBTRACTION.
70.00
28.97
FLAPSFO
TIME
0.0
4.30
11.00
20. JO
POWER
PERCENT
PATED
T.O.
68
HI
12
7
POWER
PERCENT
RATED
T .0.
66
HI
92
7
POWER
PERCENT
RATED
T.O.
68
"1
92
7
TfST
MODE
I/ 0
11 1
3/ 2
4/ 3
EXHAUST
r.AS
TEMP
tlEGREFS F
902 . 00
960.00
IC20.00
696.00
M4SS f-M
CD
LB/1K
Li) FUFL
1.5',
1.16
0.83
36.41
PQWFR ENGINE MEASURED GAS GEN CALC
THRUST, LBS PERCENT SPEED FUFL AIR FLOW F/A
OR RATED RPM FLOW LB/SEC
SHP T.O. NI N2 LB/HR
9600.00
1I36C.OO
11000.00
1040.00
EXHAUST
GAS
PRtSSURE
PSIA
9.20
11.20
13.20
0. 70
MtSS FMI
HC
LB/IK
LB FUEL
0.04
0.0
0.0
9.67
68 7210
81 7610
92 8000
7 4140
CO
(WET)
PPMV
21.00
17.00
H.OO
102.00
.00
.00
.00
.00
10910.00
11210.00
11490.00
7280.00
CO THC
2 (WET)
(WET) PPMV
PERCENT V
"ASS EMI MASS EMI
N02 C02
LB/IK LB/IK
LB FUEL LI FUFL
0.72 (130.
0.67 3131.
1.21 1131.
1.78 1049.
CP CO
?
LO/1K»TH-HB LB/1K«TH-H<
0.
0.
0.
35.
889
674
493
7 On
1809.941
1824.826
1859.888
2990.880
71
42
9',
52
2.72 1.00
2.91 0.0
3.12 0.0
1.61 140.00
5550.00 12.
662C.OO l?b.
7720.00 136.
1020.00 36.
50 0.013700
00 0.014700
50 0.015700
50 0.008000
NO NO NO
(WETI 2 X
PPMV (WET) IWETI
PPMV PPMV
D3.00
104.00
121.00
4.00
MASS fM MASS FMI MASS EM
NO NOX CD
LK/IK LB/IK LB/MR
LB FUEL LB FUFL
9 .99
11.62
12.70
0.79
THC
L B/ KUTH-HH
0.024
0.0
0.0
9.480
10.71 8.54
12.29 7.65
12.91 6.41
2.57 37.13
NO
LB/ IK*TH-HP
5.774
6.771
7.540
0.777
6. CO 89.00
6.00 110.00
2.00 121.00
9.00 13.00
COMPRESSOR ENGINE TURBINE
DISCHARGE PRESSURE INLET
TEMP RATIO TFMP
DEGREES F EPR DEGREES F
-0.00
-0.00
-0.00
-0.00
1.64 -0.00
1.79 -0.00
1.94 -0.00
-0.00 -0.00
ALDEHYDES SMOKE PARTICULATES
-0.00 -0
-0.00 -0
-0.00 -0
-0.00 -0
1 MASS EMI MASS EMI MASS EMI
HC N02 C12
LB/HK LB/HK LB/HR
0.23
0.0
0.0
9.86
NO
2
LB/ IKKTH-HR
0.417
0.391
0.125
1.748
4.01 17375.41
4.44 Z0730.02
1.62 24178.54
1.82 3110.51
NO
X
LB/1K«TH-HR
6.191
7.162
7.665
2.525
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
MASS EMI MASS EMI
NO NOX
LB/HK LB/HR
55.43 59.43
76.97 81.36
96.03 99.65
C.8I 2.63
IV-166
-------
CAl 10 NUMBER: 276 ENGINE TYPE AND MODEL: JT80-7
TEST ORGANIZATION: s w R I TWA
SERIAL NUMBER! P654564B
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
TH
840.0
14000.0
11900.0
5600.0
B40.0
POWER
TH
840. 0
14000.0
11900.0
5600.0
640.0
POWER
t TH
8*0.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
31.726 764. 571 1.000 19.00
7.199 8402.617 1.000 0.70
B.193 7077.039 1.000 2.20
16.576 3102.496 1.000 4.00
31.726 764.571 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLEI
LBS POLLUTANT/IK LB TH-HR/CYCLEl
LBS POLLUTANT/ 1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
11.451 764.571 .000 19.00
0.0 B402.61T .000 0.70
0.130 7077.039 .000 2.20
0.418 3102.496 .000 4.00
11.451 764.571 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
1.365 764.571 1.000 19.00
111.885 8402.617 1.000 0.70
88.172 7077.039 1.000 2.20
22.662 3102.496 1.000 4.00
1.365 764.571 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLEI
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/ 1000K LB TH AT T.O.:
CO
MASS
LBS.
10.047
0.084
0.300
1.105
3.701
15.23B
17.012
11.397
0.600
HC
MASS
LBS.
3.626
0.0
0.005
0.028
1.336
4.995
5.576
3.736
0.0
KOX
MASS
LBS.
0.432
1.305
3.233
1.511
0.159
6.640
7.414
4.967
93.237
FUEL
MASS
LBS.
242.11
98.03
259.49
206.83
89.20
89S.67
FUEL
MASS
LBS.
242.11
98.03
259.49
206.83
89.20
895.67
FUEL
MASS
LBS.
242.11
9B.03
259.49
206.83
89.20
695.67
LB CO /
IK LB FUEL
41.495
0.857
1.158
5.343
41.495
LB HC /
IK LB FUEL
14.977
0.0
0.018
0.135
14.977
LB NOX/
IK LB FUEL
1.785
13.315
12.459
7.305
1.785
ENERGY
TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
1 TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
LB CO /
1 TH-HR
0.03777
0.00051
0.00069
0.00296
0.03777
LB HC /
1 TH-HR
0.01363
0.0
0.00001
0.00007
0.0136)
LB NOX/
1 TH-HR
0.00162
0.00799
0.00741
0.00405
0.00162
IV-167
-------
D»TE: 7/28/71
TEST ORGANIZATION: s w R
ENGINF SUPPLIER: T w a
ENGINF DATA «..«....
CAL ID NUMBER:
285
ENGINE TYPE MO MODEL: JT8D-7
SERIAL NUMBER: P654074B
RATED THRUST: 14000.
ENGINE TOTAL TINE: 6438. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 8438. HRS
HZ CCMPRESSOR OVERHAUL: 8438. HRS
COMPUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 8438. HRS
N2 TURBINE OVERHAUL: 8438. HRS
FUEL H/C RATIO: 7.020
76.00
28.95
FUEL: JP-4 TF
OPERATIONAL DATA »««
INLET AIR TEMPERATURE, DEGREES F: START 76.00 FINISH
ATMOSPHERIC PRESSURE: START 28.95 FINISH
INLET AIR HUH 101TT, LBS H20/LB AIR: 0.0090
RELATIVE HUMIDITY: 42.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 150.00, FLOW RATE, LITERS/HIN: 4
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TF.STS: 4
CflMMENTS:
IDLE MODE DATA FOR THF JT80 WERE NORMALLY MEASURED WITH A SINGLE, AXIAL PROBE
TO PRECFOE nlLUIION PROBLEMS I DUE TU EXHAUST PIPE MIXING). FOR THIS TEST A
FULL-SIZE PROBE HAS USED AND A CORRECTION FACTOR HAS APPLIED TO RUN 14
CONCENTRATIONS AS CALCULATED FHOM A CARBON BALANCE. N02 DETERMINED BY
SUBTRACTION.
FLAPSED
TIME
0.0
6.00
12.00
16.00
TEST
MfltlE
I/
2/
3/
4/
0
1
2
3
POWER
THRUST, LBS PERCENT
OR RATED
SHP
9560.00
11460.00
128BO.OO
PBO.OO
T.O.
68
81
91
6
ENGINF
SPEED
RPH
Nl
7210.00
7630.00
7960.00
2670.00
N2
10980.00
11280.00
11580.00
6910.00
MEASURFD
FUEL
FLOW
LB/HR
5620.00
6750.00
7690.00
B80.00
GAS GFN
AIR FLOW
LB/SEC
114.30
128.50
138.50
32. SO
CALC COMPRESSOR
F/A DISCHARGE
TEMP
O.U13700
0.014600
0.015400
0.007500
OFGREFS F
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURF
RATIO
EPR
1.65
1.80
1.94
-0.00
TURBINE
INI.ET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
6H
81
91
6
EXHAUST
GAS
TEMP
nFGRCES F
919.00
979.00
1013.00
702.00
FXHAUST
GAS
PRESSURE
PSIA
9.10
11.40
13.10
0.50
CO
(WETI
PPMV
1 7.00
11.00
8.00
231.00
CO
2
IV.ETI
PERCENT V
2.72
2.95
3.05
1.54
THC
(MET!
PPMV
5.00
1.00
0.0
97.00
NO
IWET)
PPMV
57.00
75.00
. 95.00
5.00
NO
7
(WET)
PPMV
3.00
4.00
5.00
6.00
ALDEHYDES SMOKF PARTICULATES
IWETI
PPHV
60.00
79.00
100.00
11.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
POWER
PERCENT
RATED
T.O.
68
81
91
MASS EMI
cn
L»/IK
LB FUEL
1 .21)
0.74
0.52
29.29
MASS EMI
HC
LB/1K
LB FUFL
0.21
0.04
0.0
7.04
MASS EMI
NO 2
La/in
LB FUEL
0.36
0.44
0.54
1.75
MASS FMI
cn?
LB/1K
LU FIIFL
3130.71
3131.97
3132.42
3067.90
MASS EMI
NO
LR/1K
LB FUEL
6.86
fl.32
10.20
1.04
MASS EMI
NOX
LK/1K
LB FUEL
7.77
8.77
10.74
2.79
MASS EMI
cn
LH/HR
7.00
5.07
4.02
75.77
MASS EMI
HC
Lfl/HR
1.18
0.26
0.0
6. 20
MASS EM
NO 2
Lfl/HR
2.03
3.00
4. 13
1.10
MASS EMI
CO 2
LB/HR
17594.59
21140.78
24088.31
2699.75
MASS EMI
NO
LB/HR
38.54
56.19
78.44
0.97
MASS EMI
NOX
LB/fR
40.57
59.18
82.56
2.02
POWER
PERCENT
RATED
T.n.
6B
81
91
CO
U/IKK TH-HP
0.732
0.438
0.312
29.2H8
LO/IMTH-HR
1840.438
1844.7',5
1870.210
3067.900
THC
LB/1MTH-HR
0.123
0.023
0.0
7 .0'. 4
NO
L3/1KHTH-HR
4.032
4.903
6.090
1.041
LH/IK«TH-HH
0.212
".261
0.321
1.250
NO
X
LB/1MTH-HK
4.244
5.164
6.410
2.291
IV-168
-------
C»L 10 NUMBER: 285 ENGINE TYPE AND NQOELt JT8D-7
TEST ORGANIZATION: s w R I TWA
SERIAL NUMBER: P654074B
MODE FRACTIONAL
POWER
TAXI-IDLE 0.060
TAKEOFF 1.000
CLIHBOUT 0.650
APPROACH 0.400
TAXI-IDLE 0.060
NODE FRACTIONAL
POWER
TAXI-IDLE 0.060
TAKEOFF 1.000
CLIHBOUT 0.850
APPROACH 0.400
TAXI-IOLE 0.060
MODE FRACTIONAL
POWER
TAXI-IOLE 0.060
TAKEOFF 1.000
CLIHBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.060
POWER
TH
840.0
14000.0
11900.0
$600.0
840.0
POWER
1 TH
840.0
14000.0
11900.0
5600.0
840.0
POWER
TH
840.0
14000.0
11900.0
5600. 0
840.0
EMISSION FUEL USAGE TIME IN
RATE RATE UT FACTOR MODE
LB/HR LB/HR MIN.
22.619 741.444 .000 19.00
2.927 8321.195 .000 0.70
4.588 7053.270 .000 2.20
17.378 3690.958 .000 4.00
22.619 741.444 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE XT FACTOR MODE
LB/HR LB/HR MIN.
5.450 741.444 .000 19.00
0.0 8321.195 .000 0.70
0.0 7053.270 .000 2.20
4. IBB 3690.456 .000 4.00
5.450 741.444 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLEl
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/ 1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE UT FACTOR MODE
LB/HR LB/HR MIN.
1.496 741.444 1.000 19.00
114.401 8321.195 1.000 0.70
66.817 7053.270 1.000 2.20
17.484 3690.958 1.000 4.00
1.496 741.444 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/IOOOK LB TH AT T.O.:
CO
MASS
LBS.
7.163
0.034
0.166
1.192
2.639
11.196
12.129
8.374
0.244
HC
MASS
LBS.
1.726
0.0
0.0
0.279
0.636
2.641
2. 861
1.975
0.0
not
MASS
LBS.
0.474
1.335
2.450
1.166
0.175
5.599
6.065
4.187
95.334
FUEL
MASS
LBS.
234.79
97.08
258.62
246.06
86.50
923.06
FUEL
MASS
LBS.
234.79
97.08
258.62
246.06
86.50
923.06
FUEL
MASS
LBS.
234.79
47.08
258.62
246.06
66.50
923.06
LB CO /
IK LB FUEL
30.507
0.352
0.650
4.644
30.507
LB HC /
IK LB FUEL
7.351
0.0
0.0
1.135
7.351
LB NOX/
IK LB FUEL
2.017
13.746
9.473
4.737
2.017
ENERGY
1 TM-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
1 TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
f TH-HR
266.00
163.33
436.33
373.33
48.00
1337.00
LB CO /
t TH-HR
0.02693
0.00021
0.00039
0.00314
0.02693
LB HC /
1 TH-HR
0.00649
0.0
0.0
0.00075
0.00649
LB NOX/
TH-HR
0.00178
0.00817
0.00561
0.00312
0.00178
IV-169
-------
0«TF! 7/12/71
TEST ORGANIZATION: s u R i TWA
ENGINE SUPPLIES: TWA
ENGINE DATA
CAL ID NUNRER: 110
ENGINE TYPE AND MODEL: JT8D-9
SERIAL NUNBFR: P665244B
HATED THRUST: 14500.
ENGINE TOTAL TIME: 614*. HRS
TIME SINCE HOT SECTION OVERHAUL: 614*. HRS
TIME SINCE:
M COMPRESSOR OVERHAUL: 6144. HRS
NZ COMPRESSOR OVERHAUL: 6144. HRS
COMBUSTO* CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 6144. HRS
NI TURBINE OVERHAUL: 6144. HRS
N2 TURR1NF OVERHAUL: 6144. HRS
FUEL: JP-4 TF FUEL H/C RATIO: 2.021
OPERATIONAL DATA .........«..«««.«..«««.«««
INLET AIR TEMPERATURE, DFGXEFS F: START 80.00 FINISH
ATMOSPHERIC PRFSSURF: START 28.HI FINISH
INLET AIR HUMIDITY, L3S H20/LR AIR: 0.0171
RELATIVE HUMIDITY: 72.00 PFRCENT
SAMPLE LINE: TEMPERATURE, 1EGREES C: 150.00, FLOW RATE, L1T6RS/NIN:
SAPPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 4
COMMENTS:
FNGINE FOUIPPFO WITH SMOKELESS BURNEP CANS
ao.no
28.81
42.50
ELAPSED
TIMF
1.00
15.10
26.10
31.00
TFSI
MODE
I/ 0
2/ 1
3/ 2
4/ )
POWFR
THRUST. L9S PERCENT
OR HATED
SHP
9420.00
1 1900.00
13640.00
990.00
T.O.
64
82
94
6
ENGINE
SPEFD
RPM
Nl
7220.00
7740.00
8120.00
4980.00
N2
11100.00
1 1460.00
11630.00
71 10.00
MEASURED
FUFL
FLOW
LB/M"
5400.00
6960.00
8210.00
1230.00
GAS GEN
AIR FLOW
LD/SEC
114.60
132.50
145.70
43.20
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.013100
0.014600
0.015700
0.007900
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINF
PRESSURE
RATIO
EPR
1.65
1.86
2.03
-0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
64
82
94
6
EXHAUST
GAS
TFHP
DEGREES F
921.00
902.00
1065.00
694.00
FKHAUST
GAS
PRESSURE
PSI A
9.00
12.00
14.40
0.60
CO
<»ET>
PPMV
11.00
14.00
12.00
161.00
cn
2
(WET)
PERCENT V
2.32
2.75
3.05
1.67
THC
IWETI
PPMV
3.00
2.10
1.00
50.no
NO
IhETI
PPMV
61.00
94.00
124.00
3. OP
NO
2
IWETI
PPMV
3.00
5.00
8.00
5.00
NO
X
IWETI
PPMV
64.00
99.00
132. OC.
8.00
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
PARTICULl
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RAICD
T.O.
64
R2
94
6
MASS HMI
CO
LB/IK
Ll< F.JFL
0.44
1 .01
0.78
IB. 99
MASS FMI
HC
LB/IK
LB FUFL
0.15
0.08
0.04
3.38
MASS Ftl
Nfl2
LI/IK
LB FUFL
0.42
3.60
O.Hb
0.97
*ASS FMI
C02
LB/lil
LD FUFL
3131.15
3131 .42
3131.91
3094.15
MASS EMI
NO
LB/IK
LB FUEL
B.61
11.10
11.31
n.58
MASS EMI
NOX
LC/1K
Lfl fUEL
9.03
11.78
14.17
1.55
MASS FMI
CO
LB/hR
5. 10
7. OS
6.44
23. 35
MASS FMI
HC
LB/HR
O.BO
0.58
0.31
4.15
MASS FMI
NO?
LB/HR
2.29
4. 14
7.05
1.19
MASS EMI
012
LB/HR
16909.30
21794. 6(1
25712. 9»
3805.80
MASS EMI
NO
LB/HR
46.48
77.88
109.28
0.71
MASS FMI
NOX
LB/HR
4ft. 76
82.02
116.33
1.91
POWER
PERCENT
RATED
T .1.
64
82
94
6
CO
LB/1KKTH-HO
0.542
0.593
0.470
'3.587
CO
2
L H/ 1K&TH-H*
17J5.042
10)1.445
1B7H.229 .
1844.245
THC
LH/ 1KWTH-HR
0.085
0.049
0.022
4. I OS
NO
LB/ IMIH-HR
4.934
6.545
7.98)
0.722
NO
2
L R/ 1K#TM-HR
0.241
0.348
0.515
1.203
NO
X
LB/ 1 K*TH-HR
5.177
6.893
8.498
1 .925
IV-170
-------
CAL 10 NUMBER: no ENGINE TYPE AND MODELi jiso-9
TEST ORGANIZATION: s w R I TWA
SERIAL NUMBER: P665244B
NODE FRACTIONAL
POWER
TAXI-IDLE 0.060
TAKEOFF 1.000
CLIM80UT 0.850
APPROACH 0.400
TAXl-IOLE 0.060
HOOF FRACTIONAL
POWER
TAXI-IDLE 0.060
TAKEOFF t.OOO
CLIHBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.060
MODE FRACTIONAL
POWER
TAXl-IOLE 0.060
TAKEOFF 1.000
CLIMBOUT 0.950
APPROACH 0.400
TAXI-IDLE 0.060
POWER
t TH
870. 0
14500.0
12325.0
5800.0
670.0
POWER
TH
670.0
14500.0
12325.0
5800. 0
670.0
POWER
TH
670.0
14500.0
12325.0
5600.0
870.0
EMISSION FUEL USAGE TIME IN
RATE RATE UT FACTOR MODE
LB/HR LB/HR MIN.
58.225 1015.298 .000 19.00
6.633 9006.500 .000 0.70
7.094 7098.297 .000 2.20
3.360 3654.013 .000 4.00
56.225 1015.298 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CVCLE:
L6S POLLUTANT/1000K LB TH AT T.G.:
EMISSION FUEL USAGE TIME IN
RATE RATE UT FACTOR MODE
LB/HR LB/HR MIN.
29.431 1015. 298 .000 19.00
0.076 9006.500 .000 0.70
0.473 7098.297 .000 2.20
0.657 3854.013 .000 4.00
29.431 1015.296 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
18/HR LB/NR MIN.
1.389 1015.298 .000 19.00
136.096 9006.500 .000 0.70
87.427 7098.297 .000 2.20
22.224 3854.013 .000 4.00
1.389 1015.296 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
CO
MASS
LBS.
18.438
0.077
0.260
0.224
6.793
25.792
24.281
18.626
0.534
HC
MASS
LBS.
9.320
0.001
0.017
0.044
3.434
12.816
12.065
9.255
0.061
NOX
MASS
IBS.
0.440
1.588
3.206
1.482
0. 162
6.877
6.474
4.966
109.503
FUEL
MASS
LBS.
321.51
105.08
260.27
256.93
118.45
1062.24
FUEL
MASS
LBS.
321.51
105.08
260.27
256.93
118.45
1062.24
FUEL
MASS
LBS.
321.51
105.08
260.27
256.93
116.45
1062.24
LB CO /
IK LB FUEL
57.348
0.736
0.999
0.672
57.346
LB HC /
IK LB FUEL
26.968
0.008
0.067
0.171
28.988
LB NOX/
IK LB FUEL
1.366
15.111
12.317
5.767
1.366
ENERGY
TH-HR
275.50
169.17
451.92
366.67
101.50
1384.75
ENERGY
TH-HR
275.50
169.17
451.92
3B6.67
101.50
1384.75
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
1 TH-HR
0.06693
0.00046
0.00058
0.00056
0.06693
LB HC /
t TH-HR
0.03363
0.00001
0.00004
0.00011
0.03163
LB NOX/
TH-HR
0.00160
0.00939
0.00709
0.00363
0.00160
IV-171
-------
D»TE:
TEST ORGANIZATION: s w R i TWA
ENGINE SUPPLIED: TWA
ENGINE DATA
CAL ID NUMBER: n?
ENGINE TYPE AND MODEL : JTBD-9
RATED THRUST: 14500.
ENGINE TOTAL TIMF: 5839. MRS
TIKE SINCE HOT SECTION OVERHAUL: 3143. HRS
TIHE SINCE:
SERIAL MUMPER:
NI COMPRESSOR OVERHAUL: 5B39. HRS
N; COMPRESSOR OVERHAUL: 5339. HRS
CHMRUSTIIR CAN REPLACEMENT: 0. HRS
FIRST STAGF NUZZLE GUIDE VANC OVERHAUL: 33*3. HRS
NI TUKBINE OVERHAUL: 5539. HRS
N2 TURBINE OVERHAUL: 5659. HRS
FUEL H/C RATIO: 2.020
FUEL: jp-4 TF
OPERATIONAL DATA »««««»«««««»»«»«««
INLFT AIR TEMPERATURE, DEGREES F: STAKT 70.00 FINISH 75.00
ATMOSPHERIC PRESSURE: START 26.12 FINISH ?a.9z
INLFT AIR HUMIDITY, LBS H2D/LB AIR: 0.0131
RELATIVE HUMIHITY: 74.00 PERCENT
SAMPLE LINF: TEMPERATURE, DEGREES C: 150.00, Fl.OK RATE, LIIERS/NIN:
SAMPLE LINE 1RANSPORT TIMF, SEC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
F/A AND AIRFLOW CALCULATED FROM EXHAUST COMPOSITION F.'JP FOURTH BUN. N02
DETERMINED »Y SUhTRACTION. CNr.l NF EQUIPPED WITH SMOKELESS BURNER CANS.
ELAPSED
TIME
0.0
11.00
26.00
Jl.30
31.30
TFST
MODE
\l 0
?/ 1
3/ 2
4/ 3
5/ 4
POWFR
THRUST, LSS PERCENT
OR RATED
SHP
<)350.nO
1 1320.00
11740.00
840.00
11320.00
T.O.
64
71
94
5
91
ENGINE
SPEED
RPM
NI
7110.00
7520.00
8090.00
2610.00
7940.00
N?
10830.00
llZ4n.no
1 1630.01
6P.70. 00
11590.00
MEASURED
FUEL
FLOW
1 B/HR
5350.00
652C.OO
9250.00
IC10.00
7800. CO
GAS GEN
AIR FLOW
LB/SEC
115.00
129.30
147.40
35.50
144.50
CALC COMPRESSOR
F/A DISCHARGE
TFMP
0.012900
O.C13400
0.015600
0.007900
0.015000
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.64
1.82
2.04
-0.00
-0.00
TURRINE
INLFT
TEMP
DEGREES F
-0.00
-n.oo
-0.00
-o.on
-0.00
POWER
PERCENT
UATFD
T.O.
64
76
94
5
91
EXHAUST
HAS
Tf MO
nEootFS r
H6 1 .00
97 A. 00
101 7.00
659.00
1 0 1 2 . 00
FXMAUST
GAS
PHCSSURF
PS1 A
9. 10
11.30
14.80
0.50
14.20
CO
I WET)
PPMV
6. no
17. '10
9.00
260.00
12.00
CO
2
IwFTI
PE.1CFNT V
I . 99
2.13
2.38
1.57
2.36
THC
(WtTI
PPMV
i. on
0.0
0.0
30.00
2.00
NO
IUFTI
Pl>»V
63.00
fl5.no
121 .00
3.00
11 1 .00
NO
2
IWETI
PPMV
6.00
6.00
7.00
9.00
6.00
ALDEHYDES SMOKE PARTICULATES
iwm
PPMV
69.00
91.00
128.00
12.00
1 17.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-n.oo
-0.00
POWFR
PERCENT
RATED
T.n.
64
78
94
MASS FMI
CO
LP/IK.
IR FUEL
0. SO
1. 12
0.75
12. 32
1.01
MASS EMI
HC
in/ IK
LP EUEL
0.06
n.o
c.o
5.70
o.in
MASS EMI
^r)2
LI/IK
IB EIIFL
0.49
0.92
0.96
I.P4
0.83
MASS CM!
C02
LP/IK
LI HILL
1112.14
1111.48
3132.06
3066.83
3131.39
MASS t»l
Nn
L'/IK
LR FUFl
10.17
13.06
It. 65
0.61
15.40
'ASS FM|
NflX
LP/IK
l
-------
CAL ID NUNBERI 112 ENGINE TYPE AND MODEL: JTSD-9
TEST ORGANIZATION: s H R I TVA
SERIAL NUMBER: P665H8B
NODE FRACTIONAL
TAXI-IDLE
TAKEOFF
CLIN60UT
APPROACH
TAXI-IDLE
POKER
0.060
1.000
0.650
0.400
0.060
POKER
1 TH
870.0
14500.0
12325.0
5800.0
870. 0
EMISSION FUEL
RATE
LB/HR
33.973
2.290
6.284
2.076
33.973
RATE
LB/HR
1052.942
8850.086
7225.609
3602.475
1052.542
USAGE TIME IN
XT
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
TOTAL FOR CYCLE:
IBS
LBS
IBS
POLLUTANT/IK
POLLUTANT/ IK
LB
LB
POLLUTANT/1000K
FUEL/CYCLE:
TM-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
10.756
0.027
0.304
0.118
3.964
15.190
14.094
10.970
0.184
FUEL
MASS
LBS.
333.30
103.25
264.94
253.50
122.80
1077.79
LB CO /
IK LB FUEL
32.277
0.2S9
1.146
0.546
32.277
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1184.75
LB CO /
TH-HR
0.03905
0.00016
0.00067
0.00036
0.03905
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMHOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
TH
870.0
14500.0
12325.0
5800.0
870. 0
POWER
TH
670.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
7.929 1052.542 1
0.0 8850.086 1
0.0 7225.609 1
0.167 3802.475 1
7.929 1052.542 1
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
2.467 1052.542
188.728 8850.086
107.472 7225.609
27.671 3802.475
2.467 1052.542
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
HC
MASS
LBS.
2.511
0.0
0.0
0.011
0.925
1.447
3.198
2.489
0.0
NOX
MASS
LBS.
0.781
2.202
1.941
1.845
0.268
9.056
8.401
6.540
151.650
FUEL
MASS
LBS.
111.10
101.25
264.94
253.50
122. BO
1077.79
FUEL
MASS
LBS.
113.10
101.25
264.94
253.50
122.80
1077.79
LB HC /
IK LB FUEL
7.533
0.0
0.0
0.044
7.531
LB NOX/
IK LB FUEL
2.344
21.125
14.874
7.277
2.144
ENERGY
f TH-HR
275.50
169.17
451.92
186.67
101.50
1184.75
ENERGY
1 TH-HR
275.50
169.17
451.92
186.67
101.50
1184.75
LB HC /
i TH-HR
0.00911
0.0
0.0
0.00001
0.00911
LB NOX/
1 TH-HR
0.002B4
0.01102
0.00872
0.00477
0.00284
IV-173
-------
DATE: 7/16/71
TEST ORGANIZATION: s w R I TWA
ENGINE SUPPLIER: T u A
ENGINE DAIA
CAL 10 NUMBF": 11",
ENGINE TYPF AND MODEL: JTBD-9
SERIAL NUMBER;
RATED THRUST: 14500.
ENGINE TOTAL TIME: 6144. MRS
TIME SINCE HDT SECTION OVERHAUL: 6144. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 6144. HRS
N2 COMPRESSOR OVERHAUL: 6144. HRS
COM8USTOR CAN REPLACEMENT: o. HRS
FIRST ST4GE NOZZLE GUIOE VANE OVERHAUL: 6144. HRS
NI TURBINE OVERHAUL: 6144. HRS
N2 TURBINE OVERHAUL: 6144. HRS
FUEL H/C RATIO: 2.020
02.00
28.94
FUFL: JP-4 TT
OPERATIONAL DATA ««*«««««««««*»«««««««»*««»«««
INLET AIR TEMI'FRATURF, DEGREES F: START 80.00 FINISH
ATMOSPHERIC PRESSURE: START 28.94 FINISH
INLET Al° HUNIOITY, LBS H20/LB AIR: 0.0133
RELATIVE MUMiniTr: 56.00 PERCENT
SAMPLE LINE: TEMPERATUREi OFGREES C: 150.OC, FLOW RATEi LITFRS/MIN:
SAMPLE LINE TRANSPORT TIME. SFC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
F/A AND AIRFLOW CALCULATED FROM EXHAUST COMPOSITION FOR FOURTH RUN. N02
OETERMINFd HY SUBTRACTION.
ELAPSED
TIME
n.o
i.oo
11.00
19.00
31.00
TFST
"ODE
I/ 0
21 1
3/ 2
4/ 3
5/ 4
POWER
THRUST, LBS PERCENT
OR RATED
SHO
lino. 00
11340.00
13540.00
760.00
136HO.OO
T.n.
66
78
93
5
94
ENGINE
SPEFO
RPM
NI
7200.00
7580.00
81 10.00
2570.00
8120.00
N2
10810.00
1 111,0.00
115)50.00
6630.I10
11580.00
MEASURED
FUFL
FLOW
LB/HR
5680.00
6640.00
8190.00
880.00
8350.00
GAS GEN
AIR FLOW
LB/SEC
116.10
129.00
145.00
28.10
146.00
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.013600
0.014300
0.015700
0.008500
0.015900
OFGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
-o.no
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
66
78
13
5
94
EXHAUST
GAS
TEMP
DEGREES F
9C5. HO
966.nO
1070.00
691.00
1053.00
EXHAUST
GAS
PRESSURE
PSI A
9. 10
11.20
14.20
0.50
14.30
CU
(WFT 1
pp«V
1 1.00
14.00
12.00
333.00
13.00
CO
2
I WET I
PFRCENT V
2.38
2.42
2.63
1.67
2.69
THC
IWETI
PPMV
0.0
0.0
0.0
146.00
0.0
NU
IWETI
PPMV
70.00
89.00
120.00
3.00
122. PO
NO
2
IWETI
PPMV
4.00
4.00
7.00
9.00
5.00
NO
X
IWET)
PPMV
74.00
93.00
127.00
12.00
127.00
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
66
78
93
ISSS F-l
CD
LR/IK
LB FUFL
1.09
1 . 15
0.91
3H..65
0.96
MASS EMI
HC
LB/IK
LE FUEL
0.0
n.o
o.n
9.71
O.n
MASS EMI
N02
L»/ IK
LB FUFL
0.55
0.54
0.87
1.72
0.61
MASS FMI
C02
LB/1K
L3 FUFL
3111.53
3131.43
31)1.81
3045.38
3131 .71
MASS EMI
NO
LP/1K
LB FUEL
9. (.3
12.04
14.94
0.57
14. R5
MASS FMI
NOX
LB/1K
LS FUFL
10.11
12.5"
15.81
2.29
15.46
MASS EMI
CO
I.B/HR
6.18
7.66
7.45
34.0,!
8.04
MASS EMI
HC
LB/HR
0.0
0.0
0.0
8.54
0.0
MASS EMI
N02
LB/HR
3.13
3.59
7.14
1.51
5.08
MASS EMI
C02
LB/HR
17787.08
20792.69
25649.53
2680.37
26149.91
MASS FMI
NO
Lfl/HP
54.69
79.94
122.35
0.50
121.98
MASS FM
NOX
LB/HR
57.82
83.53
129. 4R
2.01
129.06
POWFR
PERCENT
KATFD
T.O.
66
5
94
CO
L R/1K«TH-HR
0.645
0.',75
0.550
'.4. 758
n. 5SS
LB/K»TH-H»
1856.699
1833.571
1894.352
1526.8C6
1911.543
THC
LH/lK»Th-li»
O.n
0.0
0.0
11.2)9
0.0
>.7C9
7 .049
9.036
0.662
9.061
LB/IK«TH-HR
0.326
0. 31 7
0.527
1 .987
0.371
NU
X
LB/IKHTH-HR
6.035
7.366
9.563
2.649
9.434
IV-174
-------
CAL 10 NUMBER: 11* ENGINE TYPE AND MODEL: jieo-9
TEST ORGANIZATION: s w R i THA
SERIAL NUMBER: P665244B
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKF.QFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
TH
870.0
14500.0
12325.0
5800.0
870.0
POWER
1 TH
870.0
14500.0
12325.0
5800.0
870.0
POWER
TH
870.0
14500.0
12325.0
5800. 0
870.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
32.774 922.494
7.734 9035.027
6.439 7522.078
4.421 3780.560
32.774 922.494
TOTAL FDR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
4.289 922.494
0.0 9035.027
0.0 7522.078
0.153 3780.560
4.289 922.494
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE NT
LB/HR LB/HR
2.128 922.494
150.332 9035.027
103.709 7522.078
24.128 J780.560
2.128 922.494
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.I
USAGE TIME IN
FACTOR MODE
MIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
10.379
0.090
0.216
0.295
3.824
14.823
14.350
10.705
0.622
HC
MASS
LBS.
1.358
0.0
0.0
0.010
0.500
1.869
1.809
1.350
0.0
NOX
MASS
LBS.
0.674
1.754
3.803
1.609
0.248
8.087
7.829
5.840
120.956
FUEL
MASS
LBS.
292.12
105.41
275.81
252.04
107.62
1033.00
FUEL
MASS
LBS.
292.12
105.41
275.81
252.04
107.62
1031.00
FUEL
MASS
LBS.
292.12
105.41
275.81
252.04
107.62
1033.00
LB CO /
IK LB FUEL
35.528
0.856
0.856
1.169
35.528
LB HC /
IK LB FUEL
4.649
0.0
0.0
0.041
4.649
LB NOX/
IK LB FUEL
2.306
16.639
13.787
6.382
2.106
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
t TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
t TH-HR
275.50
169.17
451.92
186.67
101.50
1384.75
LB CD /
1 TH-HR
0.03767
0.00053
0.00052
0.00076
0.03767
LB HC /
TH-HR
0.00493
0.0
0.0
0.00003
0.00493
LB NOX/
t TH-HR
0.00245
0.01037
0.00841
0.00416
0.00245
IV-175
-------
CUTE! 7/15/71
TEST ORGANIZATION: s u R i TMA
FNGINE SUPPLIER: TWA
ENGINE DATA
CAL ID NUMBER: 275
ENGINE TYPF AND MODEL: JT80-9
SERIAL NUMBER: P6653368
RATED THRUST: 14500.
ENGINE TOTAL TIME: 3923. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPBESSOR OVERHAUL: 5923. HRS
N2 COMPRESSOR OVERHAUL: 5921. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 5923. HRS
N2 TURBINE OVERHAUL: 5923. HRS
FUEL: JP-4 TF FUEL H/C RATIO: 2.020
OPERATIONAL OATA »«««
INLET AIR TEMPERATURE, DEGREES F: START 82.00 FINISH
ATMOSPHERIC PRESSURF: START 28.88 FINISH
INLET AIR HUMIDITY, IBS H20/LB AIR: 0.0123
RELATIVE HUMIDITY: 53.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITFRS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMHFR OF TESTS: 5
COMMENTS:
NU2 DETERMINED BY SUBTRACTION. ENGINE EQUIPPED WITH SMOKELESS BURNER CANS.
80.00
2B.8B
ELAPSED
TIME
0.0
15.00
37.00
37.00
42.00
TEST
MO.TE
I/ 0
21 1
M 2
4/ 3
5/ 4
POWER
THPUST.L8S PERCENT
OR RATFD
SHP
9500.00
1 1850.00
13500.00
920.00
12750.00
T.O.
65
Bl
93
6
87
tNGINF
SPEED
RPM
M
7330.00
7730.00
BI20.00
2750.00
7900. DO
N2
10930.00
11370.00
11670.00
7020.00
11450. OC
MEASURED
FUEL
FLOH
LB/HR
5600.00
7000.00
B160.00
930.00
7700.00
GAS GEN
AIR FLOW
LB/SEC
114.20
132.10
144.40
32.60
138.70
CALC COMPRESSOR
F/A DISCHARGE
TEMP
O.CI4000
0.014700
0.015700
0.007900
0.015400
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.65
I.fl6
2.01
-0.00
-0.00
TIIRBINF
INLET
TCMP
DEGREES f
-0.00
-o.on
-o.oo
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
65
SI
93
6
ttt
EXHAUST
GAS
TEMP
OFGREFS F
910.00
985.00
1046.00
680.00
1017.00
EXHAUST
GAS
PRESSURE
PSIA
9. 10
12.00
14.20
0.60
13. 10
CO
(MET)
PPMV
11.00
8.00
6.CO
269.00
7.CC
CO
2
IWET)
PFRCFNT V
2.83
2.97
3.15
1.61
1.10
THC
(WET)
PPMV
10.00
10.00
10.00
80.00
14.00
NO
I WET I
PPMV
70.00
100.00
l?5.on
5.00
108.00
NO
2
IWETI
PPMV
5.00
6.00
6.00
7.00
5.00
ALDEHYDES SMOKE PARTICULATES
IWETI
PPMV
75.00
106.00
131.00
12.00
113.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
-0.00
-0.00
POWER
PERCENT
R ATED
T.O.
65
MUSS EMI
CO
LR/IK
LB FUFI.
0. 77
0.54
o. in
12.61
0.4S
MASS EMI
MC
LB/IK
LB FUFL
0.40
0.38
0.16
5.55
0.52
MASS tMI
N02
LB/IK
LB FUFL
0.58
0.66
0.6?
1 .3V
0.53
MASS EMI
CO 2
LB/IK
IB FUFL
3110.0?
3111.34
3131.65
3066.77
1131.12
MASS EMI
NO
LP./IK
LB FUEL
8.10
11.02
12.99
1.00
11.40
MSSS EMI
NOX
LB/IK
LR FUEL
8.67
11.68
13.61
2.39
11.93
MASS EMI
CO
LB/HR
4.34
3.76
3.10
30.11
3.46
MASS EMI
HC
LB/HH
?.?6
2.69
2.96
5.17
3.97
MASS EMI
NO 2
LB/HB
3.24
4.63
5.09
1.30
4.07
M4SS EMI
C02
Lrt/HR
17533.14
7.1919.41
25554.26
2852.09
24109.62
MASS EMI
NO
LB/HP
45.34
77.15
106.01
0.93
87.81
MASS bMI
NOX
LB/HR
48.58
81.78
111.10
2.?2
91.87
POWER
PERCENT
RATFD
T.O.
65
81
93
CO
LR/IKJIH-HR
0.457
0. 117
12. '166
0.272
LB/IK1TM-HR
1145.594
1849.739
1892.VC8
1100. 1(10
1190.950
THC
IB/1K»TM-HR
0.718
0.227
0.710
5.615
0.311
NO
Lfl/lKKTH-HX
4.772
6.511
7.B53
1.006
6.887
LB/1K0TH-HR
0.341
0.391
0.37T
1.409
0.310
NO
X
LH/1KITH-HR
5.113
6.901
8.ZZ9
2.416
7.206
IV-176
-------
CAL ID NUMBER: 27; ENGINE TYPE AND MODEL: jTBD-9
TEST ORGANIZATION: S H R I TWA
SERIAL NUMBER: P665316B
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAKI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
1 TH
870.0
14500.0
12325.0
5800.0
870.0
POWER
TH
870.0
14500.0
12325.0
5800.0
870.0
POWER
f TH
870.0
14500.0
12325.0
5600.0
870.0
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
29. $87 783.840 .000 19.00
2.419 8639.344 .000 0.70
2.917 7472.914 .000 2.20
13.551 5018.750 .000 4.00
29.597 783.840 .000 7.00
TOTAL FOR CYCLE:
L8S POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK L8 TH-HR/CYCLE:
LBS POLLUTANT/IOOOK LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
4.596 783.840 1.000 19.00
3.607 8639.344 1.000 0.70
3.255 7472.914 1.000 2.20
4.001 5018.750 1.000 4.00
4.596 783.840 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/IOOOK LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
1.713 TB3.840 .000 19.00
139.669 8&39.144 .000 0.70
89.342 7472.914 .000 2.20
30.155 5018.750 .000 4.00
1.713 783.840 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK LB TH-HR/CYCLEI
LBS POLLUTANT/IOOOK LB TH AT T.O.:
CO
MASS
LBS.
9.369
0.028
0.107
0.903
3.452
13.860
13.212
10.009
0.195
HC
MASS
LBS.
1.455
0.042
0.119
0.267
0.536
2.420
2.306
1.747
2.902
KOX
MASS
LBS.
0.543
1.629
3.276
2.010
0.200
7.658
7.300
5.530
112.377
FUEL
MASS
LBS.
248.22
100.79
274.01
334.58
91.45
1049.05
FUEL
MASS
LBS.
248.22
100.79
274.01
334.58
91.45
1049.05
FUEL
MASS
LBS.
248.22
100.79
274.01
334.58
91.45
1049.05
LB CO /
IK LB FUEL
37.746
0.280
0.390
2.700
37.746
LB HC /
IK LB FUEL
5.863
0.417
0.436
0.797
5.863
LB NOX/
IK LB FUEL
2.186
16.167
11.956
6.009
2.186
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384. 75
ENERGY
t TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
TH-HR
0.03401
0.00017
0.00024
0.00234
0.03401
LB HC /
TH-HR
0.00528
0.00025
0.00026
0.00069
0.00528
LB NOX/
TH-HR
0.00197
0.00963
0.00725
0.00520
0.00197
IV-177
-------
OAIE: 7/22/71
TFST ORGANIZATION: S W R I THA
ENGINE SUPPLIER: r K 4
ENGINE DATA
CAL ID NIJMUFI' : 777
FNCINF TYPE AN[1 "OOEL: JTRfl-9
SERIAL NUMBFR: P665165B1
RATED TMIUST : 14500.
ENGINE rural. TIMF: BOB2. MRS
IIMF SINCE HOT SECIInN OVEHHAUL: 3147. HRS
TIMF S1NCF:
NI COMPRESSOR OVERHAUL: BOH?. MRS
NZ COMPRESSOR OVERHAUL: 8PB2. HRS
COMBUST" CAN REPLACFMF-JT: 3142. HRS
FIRSl STAGF NOZUE GUI HE VANF OVERHAUL: 3140. MRS
NI TURBINL- OVFHHAUL: HOI?. HHS
N2 TURBINE OVFPHAUL: SOU?. HPS
FUEL H/C RATIO: 2.070
77.00
28.64
FUEL: jp-4 Tt
OPERATIONAL HAT! ».«a«....«..«««...o..................o........
INLET AIR rFMI'tRATUPE, DEGREES F: SIA!U 77.00 FINISH
AT»OSPMFPIC PKESSUPF: STAKT 2S.H4 FINISH
INLET AIB KUMiniTY, LHS HJD/LB AIR: 1.0164
RELATIVE NUHlnllY! 71.00 PERCENT
SAMPLE LINF: TEMPFBATURF, CEGRFFS C: 150.,1C, FLOW RATE, LITERS/NIN:
SAMPIE LINF HANSPOrM TIMF, SEC: 1.00
NUMBER OF TESTS: 5
CO»MENTS:
F/A AND AlKf-LUW CALCUIATFO FHUM FXHAUST COMI'tIS I I I ON FIR FOURTH RUN. N02
DETERMINE'? HV SUhTPACTION. E'IGI NF ECUIPPFD WITH SMOKELESS ?UrtNF« CANS.
FLAPSFO
T IMF
0.0
4.35
7.50
11.10
17.40
POWER
PERCENT
RATED
T.O.
65
71
93
5
19
PflWFQ
PF'CENT
BATEn
T.O.
65
7«
93
5
R9
POUFM
°F PCENT
PATCU
T.O.
65
1ft
9^
5
99
TFSf
I/ 0
2/ 1
I/ 2
'./ 1
5/ 4
EXHAUST
r,As
ir»p
CEGRfFS t
HHS. no
147.00
1037.00
69i;. 0')
1115.00
«,« EM,
CO
LD/ IK
LI FUF.L
1.54
1.05
p. 7*
V. 17
0. 77
Ci;
LO/IK1
0.
Q.
0.
1? .
0.
POHFR
IHRIISI.LIS PFOCENT
HR
SHP
1540.00
1 1340.00
1 15PO.OO
K40.00
12970.00
F XHAUST
r.AS
PRfiSSURt
PSI A
9. 10
11.40
14.30
0.40
11.50
MASS r-H|
HT
LB/IK
LI" FUFL
0.05
0.0
0.0
6.77
n.OH
T1- If L
"4?
57R
',19
175
'.37
g
T
AT FH
.r.
65
7S
9)
5
H9
(Wf
PP
FNC.INF MEASURED CAS GF.N
SPEED FUEL AIR FLOW
NI
7210
7600
B16C
7960
"020
T 1
*V
.00
.00
.00
.00
.01
(V.
KPM
N?
10950.00
11200.00
11570.00
6**40. 00
1 1460.00
CU THC
2 IWETI
ETI PPMV
PERCENT V
MASS
11.
1 '< .
11.
2112.
11.
EMI
00
Tfl
00
or,
00
MASS
C-l
vn?. co?
LB/IK
LH
i
0
o
i
0
h / 1 <
FUFI
.67
.4?
. 44
.50
.46
t.r.
2
« I H-u
LB/IK
L * r
11 10.
31 31.
U32.
3065.
3111.
*
IIFL
fo
59
11
3
11
L '2
1713.177
172
1 71
30'.
0.411
'1. 764
.5.47T
1772.151
2.46 1 .00
2.f5 0.0
2.99 0."
1.71 96.00
2.»4 2.00
FLPW IB/SEC
LB/Hi>
5720.00 I1B.50 0.
6230.00 Ml. 50 0.
7760.00 144. 00 0.
840.00 77.10 0.
7340. oo 143. 5U 0.
NO NO
1 fcFTl 7
PPMV (WF Tl
PPPV
4B.OC 5.00
73.PO 5.00
1C7.CC- 4,00
2.00 9 . 00
93.00 4.00
"ASS EMI MASS EMI -ASS EMI »ASS
M;
LB/IK
LP- FUEL i
7.7?
".C?
11.17
0.37
10.7?
THC
/ IK N H'-HP.
0 . n 2 5
0 . 0
0.0
6.273
0.045
NOX C'! HC
CALC
F/A
012200
013700
015000
C08600
014200
NO
X
(VrFTI
PPMV
63.00
7P.OO
106.0C
11.00
97.00
COMPRESSOR ENGINE
DISCHARGE PRESSURE
IFNP RATIC
DEGREES F FPR
-0.00 1.64
-0.00 1.41
-0.00 7.0?
-0.00 -0.00
-0.01 -O.OC
ALDEHYDES SMUKF
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
FHI MASS F"l MASS EMI MASS
LB/IK LP/H^ LB/Hk
B FUEL
rt.3B H.03 0.
9.64 6.66 0.
11.61 5.69 0.
1.87 27.03 5.
1 1 .IP 5.67 0.
NO
L^/1K«TI Mil I.H/1K
4.272
4 . °^4
6.3H3
0. 375
(. . 01 7
24
0
0
27
5'
NT
2
f TH-HH
0.16',
0. 5.1s
0.750
1.49")
0.761
N02 C02 NH
TI/RHINE
INLET
TtHP
DFGRFFS F
-0.00
-0.00
-0.00
-0.00
-C.OO
PAR 1 ICULATFS
-O.OC
-0.00
-0.00
-c.or
-0.00
CVI MASS FMI
NDX
LB/HR LS/HH LR/HP LH/HR
3.47 16347.23 40.
3.B5 19519. ID 56.
3.40 24305.00 .14.
1.76 7575.00 0.
3.3B 729H7.46 lt>.
NO
X
l-B/1 K»TH-HP
4.586
b.Z94
6.633
1 . H 7 't
6.173
?f, 43.76
IP '»1.03
6H 90.03
31 1 .57
69 82.CU
IV-178
-------
CAL io NUMBER: 277 ENGINE TYPE AND MODEL: JT8D-9
TEST ORGANIZATION: s w R I THA
SERIAL NUMBER! P665165B1
MODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CL1MBOUT
APPROACH
TAXI-IDLE
0.060
1.000
0.850
0.400
0.060
POWER
1 TH
870.0
14900.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
26.890 738.7)9
4.718 8701.129
6.153 7056.152
15.519 345). 174
26.890 7)8.739
USAGE TIKE IN
MT FACTOR NODE
MIN.
TOTAL FOR CYCLEl
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LRS POLLUTANT/IOOOK
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.060
1.000
o.eso
0.400
0.060
POWER
I TH
870.0
1*500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
4.957 7)8.7)9
0.148 6701.129
0.36) 7056.152
0.913 3453.174
4.957 738.739
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
PONER
0.060
1.000
0.850
0.400
0.060
POWER
1 TH
870.0
14500.0
12)25.0
5800.0
870.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.303 738.739
106.342 8701.129
75.212 7056.152
17.951 3453.174
1.303 738.739
MT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IOOOK
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH 'AT T.O.:
CO
MASS
LBS.
8.515
0.055
0.226
1.0)5
3.137
12.967
14.241
9.364
0.380
HC
MASS
LBS.
1.570
0.002
0.013
0.061
0.578
2.224
2.443
1.606
0.119
NOX
MASS
LBS.
0.413
1.241
2.758
1.197
0.152
5.760
6.326
4.160
85.56)
FUEL
MASS
LBS.
233.93
101.51
258. 7)
2)0.21
66.19
910.57
FUEL
MASS
LBS.
233.9)
101.51
258.7)
230.21
66.19
910.57
FUEL
MASS
LBS.
23). 9)
101.51
258.7)
2)0.21
86.19
910.57
LB CO /
IK LB FUEL
36.399
0.542
O.B72
4.494
36.399
LB HC /
IK LB FUEL
6.711
0.017
0.051
0.264
6.711
LB NOX/
IK LB FUEL
1.764
12.222
10.654
5.199
1.764
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1)84.75
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1)84.75
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB
1
0
0
0
0
0
LB
0
0
0
0
0
LB
0
0
0
0
0
CO /
TH-HR
.03091
.00033
.00050
.00268
.0)091
HC /
TH-HR
.00570
.00001
.00003
.00016
.00570
NOX/
TM-HB
.00150
.007)3
.00610
.00310
.00150
IV-179
-------
IliTF: 7/72/71
TCSt ORGAM7AI I0:<: S W K I Ik A
ENGINF SUPPLIER: TW4
FNGINE DATA
CAL in MUM3FP: 27S
TVPF ANII HUOF.L: jtan-9
SERIAL NUWPFR: P665I65H2
RATF.n THRUST: 14500.
ENGINE TOTAL TIME: ROfl?. HPS
ri«E SINCE HOT SFCTMN OVERHAUL: 314?. HO S
TIBF SINCF:
Nl f.OMpOF. SS.1R OVERHAUL:
N2 COMPRESSOR OVERHAUL:
COMBUSTS CAN REPLACEMENT:
FIRST STAGE NUZZLE r.UIOE VANF OVERHAUL:
Nl TURR.INE OVERHAUL:
N? TJRRINE OVERHAUL:
F'lEL M/r RAnn:
enn2. HRS
8082. HRS
314?. HRS
3140. HRS
80S?. HRS
«0fl2. HPS
76.00
7P.78
FUFL: JP-4 TF
OPERATIONAL OATA ***«««««»*«*««*»***
INLFT AIR TEMPERATURE, DTORFFS f : STA»T 77.00 FINISH
ATMOSPHF°IC "RESSIICt: START 28.79 FINISH
INLET AIR HUMOITY, LTS H70/LD AIR: (1.0174
HFLATIVF HUMhMTY: 7Q.OO PERCENT
SAVPLF. LINF: TF'tl'^Tl)PF, TrGPfFS C' ISO.00, FLOW RATE, UITERS/HIN:
SAPPLF LINE [RANSPMRT TIH=, StC: 1.00
NUXREP OF TFSTS: >
COMMENTS:
F/A AND nlRHL'lv. I'.ILCUIATEH F»n'< iXHA'IST CHMPOSITION TDK FnunlH RUV. .\'02
OFTFUXINFO PY Sll". ISACTiriM.
ELAPSFO
TIME
0.0
4.40
10. 15
14.25
lfi.20
I/ 0
T.I I
3/ 2
4/ 3
THRUST,LHS
SHP
1480.00
II"00.00
P60.00
17560.00
RATCC
T.O.
CNf.INt
S!>
4
Nl
7270. OC
7750.00
H220.no
26jn.OO
7870.00
EF fl
pu
N2
infloo.no
1127-1. n:)
11600.00
6860.00
11710.00
WFASUREU
FUEL
FLOW
LS/HR
S200.00
6620.00
7910.00
840.00
7100.00
GAS GEN
Alk FLOW
LR/SEC
iii.ro
17H.20
I4i.no
21.40
m. oo
CALC
F/A
0.012900
O.P14300
O.CI5600
O.OOB200
0.014800
COMPRESSOR
fllSCHARGE
TEMP
OFGRFFS F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINF.
PRFSSURE
RATIO
EPR
1.65
1 . 86
2.04
-0.00
-0.00
TURP1NF
INlET
-o.no
-0.00
-0.00
-0.00
-O.OC
POWER
PFKCENI
"AfFO
t.O.
82
94
F XHAUST
CAS
TE vt>
DECS MS !=
K1 1 . 11
^H. on
in'.o.no
(.71.0(1
FXHAUST
C.AS
PRFSSUKF
PSI A
<,. 10
1?. 10
14.60
n.so
17.90
CO
I.ETI
PP"V
7 '. . DO
1 7. Of!
I4.no
774. CC
I 6.'" 7 I
11.526
11 .'170
0.617
O.n
O.n
o.o
f>. s l s
r .0
5 . "7 7
4.9? j
6.27H
0.577
0. 151
II. 119
0.30H
1.526
0. 3BO
4.277
5.314
6.536
2 .091
5.577
IV-180
-------
CAL ID NUMBER: 273 ENGINE TYPE AND MODEL: jTso-9
TEST ORGANIZATION: s M R i TMA
SERIAL NUMBER: P665165B2
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
KODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
I. 000
O.BSO
0.400
0.060
FRACTIONAL
PONER
0.060
1.000
0.390
0.400
0.060
FRACTIONAL
POWER
0.060
I. 000
0.850
0.400
0.060
POMER
TH
870.0
14500.0
12323.0
5800.0
870.0
POMER
1 TH
870. 0
14500.0
12325.0
5800.0
870.0
POMER
TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL USAGE TIME IN
RATE RATE MT FACTOR MODE
LB/HR LB/HR MIN.
24.526 731.452 .000 14.00
7.431 8354.258 .000 0.70
7.323 6440.484 .000 2.20
15.486 2416.116 .000 4.00
24.526 731. 452 .000 7.00
TOTAL FOR CYCLE:
IBS POLLUTANT/IK LB FUEL/CYCLE:
L8S POLLUTANT/IK L8 TH-HR/CYCLE:
LBS POLLUTANT/tOOOK LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE MT FACTOR MODE
LB/HR LB/HR MIN.
5.173 731.452 1.000 14.00
0.0 8354.298 1.000 0.70
0.115 6940.484 1.000 2.20
0.107 2416.116 1.000 4.00
5.173 731. 452 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCIE:
L8S POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE MT FACTOR MODE
LB/HR LB/HR MIN.
1.346 731.452 1.000 14.00
98.581 8354.258 1.000 0.70
71.154 6440.484 1.000 2.20
14.584 2416.116 1.000 4.00
1.346 731.452 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK LB TH-HR/CVCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
CO
MASS
LBS.
7.767
0.087
0.264
1.032
2.861
12.016
13.888
8.677
0.548
HC
MASS
LBS.
1.638
0.0
0.004
0.007
0.604
2.253
2.604
1.627
0.0
NOX
MASS
LBS.
0.426
1.150
2.604
0.472
0.157
5.314
6.142
3.838
74.318
FUEL
MASS
LBS.
231.63
47.52
256.32
144.41
85.34
861.21
FUEL
MASS
LBS.
231.63
47.52
256.32
144.41
85.34
865.21
FUEL
MASS
LBS.
231.63
47.52
256.32
194.41
85.34
865.21
LB CO /
IK LB FUEL
33.531
0.889
1.048
5.310
33.531
LB HC /
IK LB FUEL
7.073
0.0
0.016
0.037
7.073
LB NOX/
IK LB FUEL
1.840
11.793
10.179
5.001
1.840
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
f TH-HR
275.50
169.17
451.42
386.67
101.50
1384.75
ENERGY
« TM-HR
275.50
164.17
451.42
386.67
101.50
1384.75
LB CO /
1 TH-HR
0.02819
0.00051
0.00059
0.00267
0.02819
LB HC /
I TH-HR
0.00595
0.0
0.00001
0.00002
0.00595
LB NO*/
TM-HR
0.00155
0.00680
0.00577
0.00251
0.00155
IV-181
-------
0«TE: 7/22/71
TEST ORGANIZATION: s w R
ENGINE SUPPLIER: TWA
ENGINE DATA
CAL ID NUMBER: 279
ENS INF TYPF AND MODEL: JT8D-9
SERIAL NUMBER:
RATED THRUST: 14500.
ENGINE TOTAL TIME: 4413. MRS
TIME SINCE HOT SECTION OVERHAUL: 1027. MRS
TINE SINCE:
NI COMPRESSOR OVERHAUL: 4413. HRS
N2 COMPRESSOR OVERHAUL: 4413. HRS
COMRUSTOR CAN REPLACEMENT: 1027. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 1027. HRS
Nl TURBINE OVERHAUL: 4413. HRS
N2 TURBINE OVERHAUL: 4413. HRS
FUEL H/C RATIO: 2.020
EUEL: JP-4 TF
OPERATIONAL DATA «««
INLET AIR TEMPERATURE, DEGREES F: START 71.00 FINISH 71.00
ATMOSPHERIC PRESSURE: START 2S.B2 FINISH 28.83
INLET AIR HUMIDITY, LBS H2U/LB AIR: 0.0141
RELATIVE HUMIDITY: 78.oo PF.RCFNT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.OG, FLO* RATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
F/A AND AIRFLOW CALCULATED FROM EXHAUST COMPOSITION FOR FOURTH RUN. N02
DETERMINED RY SUBTRACT ION. ENGINE EQUIPPED WITH SMOKELFSS BURNER CANS.
ELAPSED
TIMF
0.0
13.55
2B.40
33.40
39.40
TEST
NODE
I/ 0
?/ 1
3/ 2
4/ 3
5/ 4
POWER
THRUST, LBS PERCENT
OR RATED
SHP
9500.00
11900.00
13660.00
1180.00
12660.00
T.O.
65
B2
04
6
B7
ENGINE
SPEFO
DPM
Nl
7170.00
7700.00
H150.00
3100. TO
7tirc.no
N2
10840.00
11260.00
11570.00
7510.00
11370.00
MEASURED
FUEL
FLOW
LB/HR
5180.00
6570.00
7H10.00
1050.00
7100.00
GAS GEN
AIR FLOW
LB/SEC
112.80
128.00
142.30
31.70
135.10
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.012800
0.014200
0.015200
0.009200
0.014600
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPP
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TE*P
DEMFFS 1
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
65
82
94
H
07
EXHAUST
GAS
TFMP
DEGREES f
869. 00
947.00
974.00
673.00
976.00
EXHAUST
GAS
PRESSURE
PSIA
9.70
12.10
14.50
0.90
13.10
CO
(WET 1
PPMV
28.00
16.00
12.no
417.00
16.00
CO
2
(bf II
PERCENT V
2.61
2.87
1.07
1.83
2.97
THC
IWFTI
PPHV
n.o
0.0
0.0
144.00
0.0
NU
1 WET)
PPMV
48.00
6R.on
88.00
3.00
75.00
NO
2
(JET!
PPMV
5.00
4.00
5.00
0.00
4.00
-------
CAl ID NUKBERl 2T9 ENGINE TYPE AND NQDED JT8D-9
TEST ORGANIZATION: S W R I TWA
SERIAL NUM8ERI P665489B
MODE
TAXI-IDie
TAKEOFF
CLINBOUT
APPROACH
TAKI-IOIE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
o.o&o
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
POMER
f TH
670.0
14500.0
12125.0
5800.0
870.0
POMER
t TH
870.0
14500.0
12325.0
5800.0
870.0
POWER
t TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
45.201 748.448
6.531 8296.590
7.897 6848.914
20.753 3470.408
45.201 748. 44B
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
10.131 748.448
0.132 8296.590
0.274 6848.914
0.270 3470.408
10.131 748.448
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000X
EMISSION FUEL
RATE RATE MT
LS/HR LB/HR
1.004 748.448
86.323 8296.590
60.330 6848.914
13.859 3470.408
1.004 748.448
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/ 1000K
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
HIN.
.000 19.00
.000 0.7D
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
L9 TH AT T.O.:
USAGE TINE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
14.314
0.076
0.290
1.384
5.273
21.336
23.612
15.408
0.525
HC
MASS
LBS.
3.208
0.004
0.010
0.018
1.182
4.422
4.894
3.193
0.267
NOX
MASS
LBS.
0.318
1.007
2.212
0.924
0.117
4.578
5.066
3.306
69.456
FUEL
MASS
IBS.
237.01
96.79
251.13
231.36
87.32
903.61
FUEL
MASS
LBS.
237.01
96.79
251.13
231.36
87.32
903.61
FUEL
MASS
LBS.
237.01
96.79
251.13
231.36
87.32
903.61
LB CO /
IK LB FUEL
60.393
0.787
1.153
5.980
60.393
LB HC /
IK LB FUEL
13.536
0.040
0.040
0.078
13.536
LB NOX/
IK LB FUEL
1.341
10.405
8.809
3.993
1.341
ENERGY
i TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-MR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
TH-HR
0.05195
0.00045
0.00064
0.00358
0.05195
LB HC /
TM-HR
0.01164
0.00002
0.00002
0.00005
0.01164
LB NOX/
1 TH-HR
0.00115
0.00595
0.00489
0.00239
0.00115
IV-183
-------
0*TEI 7/21/71
TEST ORGANIZATION! S W R
ENGINE SUPPLIER: T w A
ENGINf DATA
C»L ID NUMBER: 280
ENGINE TYPE AND MODEL! JT8D-9
SERIAL NUMBER: P665170B
RATED THRUST: 14500.
ENGINE TOTAL TIME: 8086. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: aoea. MRS
N2 COMPRESSOR OVERHAUL: 8086. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
XI TURBINE OVERHAUL: 80BB. HRS
N2 TURBINE OVERHAUL: 608B. HRS
FUEL H/C RATIO: 2.020
62.00
76.61
FUEL: jp-4 TF
OPERATIONAL DATA ...4................................
INLET AIR TEMPERATURE, DEGREES F: START 62.00 FINISH
ATMOSPHERIC PKESSURF: START 28.61 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0161
RELATIVE HUMIDITY: 57.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: ISO.(1C, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
F/A AND AIRFLUU CALCULATED FROM EXHAUST COMPOSITION FOR FOURTH RUN. NO?
DETERMINED BY SUBTRACTION. ENGINE EBUIPPFO WITH SMOKELESS RURNER CANS.
42.50
FLAPSEO
TIME
0.0
11. 40
16.25
22.50
27.00
TEST
MODE
I/ 0
2/ 1
3/ 2
4/ 3
5/ 4
IHRUST
OR
SHP
9540.
1 1740.
13760.
670.
11550.
POWFR
IBS PEKCENT
1ATED
00
00
00
00
00
T.n.
65
en
94
4
93
FNGINE
SPEED
RPM
NI
7230.00
7720.00
8230.00
2440.00
8220.00
N2
10970.00
11380.00
11760.00
6490.00
11710.00
MEASURED
FUEL
FLOW
LB/HR
5490.00
6820.00
6300.00
910.00
8250.00
GAS GEN
AIR FLOW
IB/SEC
111.10
126.10
140.40
79.70
138.90
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.013700
0.015000
O.C16400
0.006500
0.0165CO
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.65
1.84
2.03
-0.00
-0.00
TURBINf
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-O.OC
POWER
PERCENT
RATED
T.n.
65
80
44
EXHAUST
GAS
TEMP
OEG°EES F
864.OD
943.00
1019.00
705.00
1005.00
EXHAUST
GAS
PRESSURE
PSIA
9. 10
11.90
14.50
0.40
14.40
cn
IWETI
PPMV
16.00
14. 00
10.00
324.no
9.00
CO
2
IWFt)
PERCENT V
2.76
3.02
3.21
1.69
3.25
THC
IWETI
PPMV
1.00
0.0
0.0
144.00
0.0
NO
IhETI
PPMV
62.00
80.00
1 11.00
3.00
108.00
NO
2
IWFTI
PPMV
3.00
5.00
5.00
9.00
J.OO
ALDEHYDES SMOKE PARTICULARS
IWFTI
PPMV
65.00
85.00
116.00
12.00
111.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATFO
T.O.
65
no
94
4
93
MASS EMI
CO
LO/IK
LB FUEL
1.16
0.92
0.62
17.20
0.55
MASS [Ml
HC
LB/1K
Lfl FUEL
0.04
0.0
0.0
9.47
0.0
MASS FMI
NDZ
LK/IK
LB FUEL
1.J6
0.54
0.51
1.70
0.30
MASS FMI
CIJ2
LB/IK
LB FUEL
3131. 11
3131.79
3132.26
3048.81
3132.37
MASS EMI
NO
LB/1K
LB FUEL
7.35
8.67
11.32
0.57
10.80
MASS EMI
NOX
LB/1K
LB FUEL
7.71
9.21
11.83
2.26
11.18
MASS EMI
CO
LH/XH
6.34
6.30
5.15
33.85
4.55
MASS EMI
HC
LB/HR
0.23
o.c
o.o
8.62
0.0
MASS FMI
N02
Lfl/HH
1.95
3. 70
4.23
1.54
2.49
MASS EMI
CO 2
LB/HR
1 7190.91
21358.80
25957.79
2774.42
25842.08
MASS FMI
NO
LH/CR
40.37
59.15
93.98
0.51
89.77
MASS EMI
NOX
L6/HO
42.32
62. R5
98.21
2.06
92.27
POWER
PERCENT
RATED
T.O.
65
no
94
CO
LB/IK »TH-HR
0.665
0.537
0.375
50.526
0. 336
LB/IKITH-HK
1R01.9S2
1X19.318
lfldl.375
4140.922
1907.165
IHC
LB/1K»TH-HR
0.024
0.0
0.0
12.861
0.0
NO
LB/lKdTH-HR
4.232
5.038
6.830
0.769
6.625
Lfl/IK«TH-HR
0.205
0.315
0.308
2.305
0.184
NO
X
IB/1MTH-HR
4.436
5.353
7.13"
1.074
6.309
IV-184
-------
C»L 10 NUMBER: zso ENGINE TYPE AND MODELI jTso-9
TEST ORGANIZATION! S H R I TWA
SERIAL NUNBERl P665170B
NODE FRACTIONAL
POWER
TAKI-IDLE 0.060
TAKEOFF 1.000
CLIMBOUT 0.850
APPROACH 0.400
TAXI-IOLE 0.060
NODE FRACTIONAL
POWER
TAXI-IOLE 0.060
TAKEGFF I. 000
CLIMBOUT 0.050
APPROACH 0.400
TAXI-IOLE 0.060
MOOE FRACTIONAL
POWER
TAXI-IOLE 0.060
TAKEOFF I. 000
CLIMBOUT 0.950
APPROACH 0.400
TAII-IDLE 0.060
POWER
TH
870.0
14500.0
12325.0
5800.0
870.0
POWER
1 TH
870.0
14500.0
12325.0
5800.0
870.0
POWER
1 TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
28.619 899.137
5.517 8412.793
5.858 7136.168
11.291 3913.170
28.619 899.137
TOTAL FOR CYCLE:
IBS POLLUTANT/ IK LB
LOS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
6.070 899.137
0.881 8912.793
0.289 7136.168
1.041 3933.170
6.070 899.137
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
2.137 899.137
114.861 8912.793
71.512 7136.168
21.008 3933.170
2.137 899.137
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR NODE
NIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL/CYCLE!
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
M1N.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
9.063
0.064
0.215
0.753
3.339
13.433
13.202
9.701
0.444
HC
MASS
LBS.
1.922
0.010
0.011
0.069
0.708
2.721
2.674
1.965
0.708
NOX
MASS
LBS.
0.677
1.340
2.622
1.401
0.249
6.289
6.181
4.542
92.416
FUEL
MASS
LBS.
284.73
103.98
261.66
262.21
104.90
1017.48
FUEL
MASS
LBS.
284.73
103.98
261.66
262.21
104.90
1017.48
FUEL
MASS
LBS.
284.73
103.98
261.66
262.21
104.90
1017.48
LB CO /
IK LB FUEL
31.829
0.619
0.821
2.871
31.829
LB HC /
IK LB FUEL
6.751
0.099
0.041
0.265
6.751
LB NOX/
IK LB FUEL
2.377
12.887
10.021
5.341
2.377
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
t TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
TH-HR
0.03289
0.00038
0.00048
0.00195
0.03289
LB HC /
TH-HR
0.00698
0.00006
0.00002
0.00018
0.00698
LB NOX/
1 TH-HR
0.00246
0.00792
0.00580
0.00362
0.00246
IV-185
-------
0»TEl T/27/71
TEST ORGANIZATION: s w R I TKA
ENGINE SUPPLIER: T M A
ENGINF OATA
C»L ID NUMBFRl 263
ENGINE TYPE AND MODEL: JT8D-4
SERIAL NUMBED! P64B915B
RATED THRUST: 14500.
ENGINE TOTAL TINE: 15252. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIKE SINCE:
Nl COMPRESSOR OVERHAUL: 15252. HRS
N2 COMPRESSOR OVERHAUL: 15252. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL; 0. HRS
Nl TURBINE OVERHAUL: 15252. HRS
N2 TURBINE OVERHAUL: 15252. HRS
FUEL: JP-4 TF FUEL H/C RATIO: 2.020
OPERATIONAL DATA ««»««»«««*
INLET AIR TF.MPERATURE, DEGREES F: START 74.00 FINISH 72.00
ATMnsPHERic PRESSURF: START 26.83 FINISH 28.83
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0107
RELATIVE HUNIDITV: 62.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW HATE, LITFRS/HIN:
SAMPLE LINE TRANSPORT TINE, SFC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
N02 DETERMINED BY SUBTRACTION. ENGINE EQUIPPED KITH SMOKELESS BURNER CANS.
ELAPSFP
r IMF
tEST
Mons
POKER
THRUST, LBS PERCENT
OR RATED
SHP
o.n
7.?0
12.30
14.30
21 .00
I/ 0
2/ 1
3/ 2
4/ 3
5/ 4
9680
11370
12850
1040
17770
.00
.00
.00
.00
.00
T.O.
66
73
88
7
88
FNC.INC
SPEED
BPM
Nl
7280.00
7690.00
8050.00
2930.00
8020.00
N2
10960.00
11270.00
11510.00
7150.00
11420.00
MEASURED
FUEL
FLOK
LS/HR
5600.00
6630.00
7630.00
1010.00
7600.00
GAS GEN
AIR FLOtt
LB/SEC
117.50
129.30
140.70
34.20
140.20
CALC COMPRESSOR
F/A DISCHARGE
TFMP
0.013200
0.014200
0.015100
0.008200
0.015100
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINF
PRESSURF
RATIO
EPR
1.65
1.79
1.92
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-o.oo
POWER
PERCENT
RATEO
T.O.
66
78
88
7
88
EXHAUST
GAS
TEMP
DEGREES F
887.00
937.00
986.00
678.00
984.00
EXHAUST
GAS
PRESSURE
PSIA
9.20
11.20
13.00
0.70
12.90
CO CC
IKETI 2
PPMV turn
PERCENT V
15.00
11.00
10.00
211.00
10.00
2.59
2.78
2.93
1.65
2.95
THC
(WET)
PPMV
1.00
0.0
0.0
42.00
0.0
NO
I WET)
PPMV
63.00
85.00
101.00
12.00
99.00
NO
2
(KETI
PPMV
7.00
2.00
2.00
3.00
3.00
ALDEHYDES SMOKE PARIICULATFS
IHETI
PPMV
65.00
117.00
ICM.OO
15.00
102.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POKER
PERCENT
RATED
T.O.
66
78
88
7
88
MASS FMI
cn
LB/IK
LB FUFL
1.15
0. 79
0.68
25.12
0.68
MASS EMI
MC
LB/1K
LB FUEL
0.04
0.0
0.0
7.86
0.0
MASS EMI
N02
LR/IK
LB FUEL
0.25
0.24
0.22
0.59
0.53
MASS EMI
C02
LB/IK
LB FIIEl
3131.31
3132.00
3132. 17
3085.93
3132.18
MASS EMI
ND
LB/IK
LB FUEL
7.96
10.01
1 1.29
2.35
10.99
MASS EMI
NDX
LB/IK
LB FUEL
8.22
10.25
11.51
2.93
1 1.32
KASS EMI
cn
LB/Hk
6.46
5.23
5.19
25.37
5.14
MAIS FMI
HC
LB/HR
0.25
0.0
0.0
2.89
0.0
MASS EMI
NO 2
L8/HR
1.42
1.56
1.71
0.59
2.53
MASS EMI
CD2
LB/HR
17535.32
20765.17
23898.46
3116.78
23804.55
MASS FMI
NO
LB/HR
44. 59
66.37
86.12
2.37
83.51
MASS EMI
NHX
1. E/MR
46.01
67.93
87.83
2.96
86.04
POKER
PERCFNT
RATEO
T.n.
66
7
88
CO
Lfl/IK(tH-HB
0.668
0.460
0.404
24.391
0.402
LB/1KKTM-HR
1811.500
1826.312
1859.802
2996.9C9
1864.100
THC.
LB/IKITH-HO
0.025
0.0
0.0
7.7H1
0.0
NO
LB/ 1MTH-HP
4 .606
5.R38
6.702
2.279
6.540
L6/1KITH-HR
0. 146
0.137
0. 133
0.570
O.I9«
NO
X
LB/1MTH-HH
4.753
5.975
6.835
2.848
6.738
IV-186
-------
C«L ID NUMBER! 283 ENGINE TYPE AND MODEL: JI8D-9
TEST ORGANIZATION: s H R I TMA
SERIAL NUMBER! 15252.
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.060
1.000
0.650
0.400
0.060
POWER
TH
670.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
25.947 803.260
4.943 8405.980
4.665 7264.555
11.143 3231.326
25.947 803.260
MT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
1 TH
670.0
14500.0
12325.0
5800.0
670.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
2.648 803.260
0.170 6405.980
0.073 7264.555
1.206 3231.328
2.648 603.260
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.060
1. 000
0.850
0.400
0.060
POWER
TH
870.0
14500.0
12325.0
5600.0
870.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.647 803.260
109.397 8405.980
80.286 7264.555
16.341 3231.328
1.847 803.260
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLEI
LB TH AT T.O.:
USAGE TINE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
8.217
0.058
0.171
0.743
3.027
12.215
13.164
8.821
0.396
HC
MASS
LBS.
0.639
0.002
0.003
0.081
0.309
1.233
1.326
0.890
0.137
NOX
MASS
LBS.
0.565
1.276
2.944
1.089
0.215
6.110
6.584
4.412
88.020
FUEL
MASS
LBS.
254.37
98.07
266.37
215.42
93.71
927.94
FUEL
MASS
LBS.
254.37
98.07
266.37
215.42
93.71
«7.94
FUEL
MASS
LBS.
254.37
98.07
266.37
215.42
93.71
427.94
LB CO /
IK LB FUEL
32.303
0.588
0.642
3.448
32.303
LB HC /
IK LB FUEL
3.296
0.020
0.010
0.374
1.296
LB NOX/
IK LB FUEL
2.300
13.014
11.052
5.057
2.300
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB
f
CO /
TH-HR
0.02982
0.00034
0.00038
0.00192
0.02982
LB
0
0
0
0
0
LB
0
0
0
0
0
HC /
TH-HR
.00304
.00001
.00001
.00021
.00304
NOX/
TH-HR
.00212
.00754
.00651
.00282
.00212
IV-187
-------
UAI tl It tot I I
TEST ORGANIZATION: SHU
ENGINE SUPPLIER! IMA
ENGINE D»t»
CAL to NUMBER: 28*
ENGINE TYPE AND MODEL:
SERIAL MUMBER: P6T42S08
RATED THRUST: 1*500.
ENGINE TOTAL THE: 36T3. MRS
TIHE SINCE HOT SECTION OVERHAUL: 0. HRS
TINE SINCE:
Nl COMPRESSOR OVERHAUL: 3673. HRS
N2 COMPRESSOR OVERHAUL: 3673. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: 3673. KRS
N2 TURBINE OVERHAUL: 3673. HRS
FUEL: jp-4 TF FUEL H/C RATIO: 2.020
OPERATIONAL DATA «»«««««*««««««
INLET AIR TEMPERATURE, DEGREES F: START 66.00 FINISH
ATMOSPHERIC PRESSURE: START 28.90 FINISH
INLET AIR HUMIDITY, LBS M20/LB AIR: 0.0130
RELATIVE HUMlniTY: 84.00 PERCFNT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
NO? DETERMINE" BY SUBTRACTION. ENGINE EQUIPPED WITH SMOKELESS BURNER CANS.
67.00
?e.9i
42.50
ELAPSED
TIME
0.0
18.00
51.00
40.00
45.00
TEST
MODE
I/
2/
3/
4/
5/
0
1
2
1
it
POWER
THRUST, LBS PF.RCFNT
OK RATFD
SHP
9520.00
11020.00
13700.00
860.00
12740.00
T.O.
65
75
94
5
87
ENCINE
SPEED
«PM
Nl
7120.00
7520.00
8150.00
2600.00
7870.30
N2
10890.00
11150.00
11580.00
6840.00
11400.00
MEASURED
FUEL
FLOW
LB/HR
5270.00
6150.00
8040.00
850.00
7320.00
GAS GEN
AIR FLO*
LB/SFC
117.00
128.00
148.00
31.20
141.00
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.012500
0.013300
0.015100
0.007600
0.014400
OEGREFS F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.65
1.79
2.0)
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES f
-0.00
-0.00
-0.00
-O.OC
-O.OC
POWER
PERCENT
RATED
T.O.
65
75
94
5
87
EXHAUST
GAS
TEMP
DEGREES F
811.00
880.00
970.00
667.00
945.00
EXHAUST
GAS
PRESSURE
PSIA
9. 10
10.90
14.40
0.60
13.00
CO
(MET)
PPMV
11.00
11.00
8.00
331.00
10.00
CO
2
UET)
PERCENT V
2.48
2.67
2.92
1.57
2.83
THC
IMFTI
PPMV
0.0
0.0
0.0
140.00
1.00
NO
(WFTI
PPMV
58.00
80.00
120.00
3.00
101.00
2
I WET I
PPMV
5.00
6. on
6.00
7.00
4.00
NO
X
IHFTI
PPMV
63.00
86.00
126.00
10.00
105.00
ALDEHYDES SMOKE PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-c.oo
-0.00
POWER
PERCENT
RATED
T.O.
65
75
94
5
87
MASS EMI
cn
LR/1K
LB FUEL
1.04
0.82
0.55
40.82
0.70
MASS FMI
HC
IB/IK
LP FUEL
0.0
0.0
0.0
9.89
0.04
MASS EMI
N02
LBMK
LB FUEL
0.66
0.74
0.67
1.42
0.46
MASS FMI
C02
LB/1K
LB FUFL
1131.60
3131.95
3132.38
1041.98
1132.0?
MASS EMI
Nil
LR/1K
LB FUEL
7.66
9.81
13.46
0.61
11.69
MASS FMI
NOX
LB/1K
IB FUEL
8.32
10.55
14.13
2.03
1?.15
MASS EMI
CO
LB/HH
5.51
5.05
4.39
14.69
5.16
MASS E.«l
HC
IR/HR
3.0
0.0
0.0
8.40
0.30
MASS tMI
ND2
LB/HR
1.48
4.52
5.41
1.21
3.39
MASS EMI
C02
LB/HR
16501.53
19261.50
25184.36
2585.68
22926.41
MASS FMI
NO
LB/MP
40.15
60.33
108.20
0.5?
95.54
MASS EMI
NHX
LR/Hk
43.81
64.86
113.61
1.72
88.92
POWER
PFRCENT
RATED
T.O.
66
75
94
CO
LB/1KKTH-HR
0.578
0.458
0.121
40.343
O.'i05
LB/U»TH-H«
1711.564
1747.867
1838.275
3006.609
1799.562
FHC
LB/1KITH-HR
0.0
0.0
0.0
9.773
0.023
NO
LB/1KHTH-HR
4.238
5.475
7.898
0.601
6.714
Lfl/ 1KKTH-HR
0.365
0.411
0.395
1.401
0.266
NO
X
LB/1KHTH-HR
4.604
5.885
8.292
2.002
6.980
IV-188
-------
C»L ID NUMBER: 28* ENGINE TYPE »ND NOOELI jrao-9
TEST ORGANIZATION! S W R I TMA
SERIAL NUMBER! P674250B
MODE FRACTIONAL
POWER
TAXI-IDLE 0.060
TAKEOFF 1.000
CLIMBOUT 0.8SO
APPROACH 0.400
TAXI-IDLE 0.060
NODE FRACTIONAL
POWER
TAXI-IDLE 0.060
TAKEOFF 1.000
CLIMBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.060
MODE FRACTIONAL
POWER
TAXI-IDLE 0.060
TAKEOFF 1.000
CLIMBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.060
POWER
1 TH
B70.0
14900.0
12325.0
5800.0
BTO.O
POWER
1 TH
BTO.O
14500.0
12325.0
5800.0
870.0
POWER
TH
BTO.O
14500.0
12325.0
5800.0
870.0
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
40.008 886.145 1.000 19.00
6.207 8828.016 1. 000 0.70
4.366 7070.793 1.000 2.20
14.659 3551.601 1.000 4.00
40.008 886.145 1.000 7.00
TOTAL FOR CYCLE 1
LBS POLLUTANT/IK LB FUEL/CYCLE:
IBS POLLUTANT/IK LB TH-HR/CYCLEl
LBS POLLUTANT/1000K LB TH AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
.9.451 8B6.145 1.000 19.00
0.168 8828.016 1.000 0.70
0.267 7070.793 I. 000 2.20
0.429 3551.601 1.000 4.00
9.451 886.145 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLEl
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
1.610 886.145 .000 19.00
133.453 8828.016 .000 0.70
85.160 7070.793 .000 2.20
15.307 3551.601 .000 4.00
1.610 886.145 .000 7.00
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/IOOOK LB TH AT T.O.I
CO
MASS
LBS.
12.669
0.072
0.160
0.977
4.668
18.547
18.867
13.393
0.499
HC
MASS
LBS.
2.993
0.002
0.010
0.029
1.103
4.136
4.207
2.987
0.135
NOX
MASS
LBS.
0.510
1.557
3.123
1.020
0.188
6.398
6.50B
4.620
107.376
FUEL
MASS
LBS.
280.61
102.99
259.26
236.77
103.38
983.02
FUEL
MASS
LBS.
280.61
102.99
259.26
236.77
103.38
983.02
FUEL
MASS
LBS.
280.61
102.99
259.26
236.77
103. 38
983.02
LB CO /
IK LB FUEL
45.148
0.703
0.618
4.128
45.148
LB HC /
IK LB FUEL
10.665
0.019
0.038
0.121
10.665
LB NOX/
IK LB FUEL
1.817
15.117
12.044
4.310
1.817
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
TH-HR
0.04599
0.00043
0.00035
0.00253
0.04599
LB HC /
f TH-HR
0.01086
0.00001
0.00002
0.00007
0.01086
LB NOX/
TH-HR
0.00185
0.00920
0.00691
0.00264
0.00185
IV-189
-------
OATEl 7/28/71
TEST ORGANIZATION! S U R
ENGINE SUPPLIER: I X A
ENGINE DATA
CAL ID NUMBER: 286
ENGINE TYPE «ND MODEL: JT8D-9
SERIAL NUMBER: P6742508
RATED THRUST: 1*500.
ENGINE TOTAL TIME: 3673. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 3673. HRS
N2 COMPRESSOR OVERHAUL: 3673. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 3673. HRS
NZ TURBINE OVERHAUL: 3673. HRS
FUEL H/C RATIO: 2.020
68.00
28.98
FUEL: JP-4 TF
OPERATIONAL DATA «»««»«««««»«»«
INLET AIR TEMPERATURE. DEGREES F: START 67.00 FINISH
ATMOSPHERIC PRESSURE: START 28.98 FINISH
INLET AIR HUMIDITY, LBS H20/L8 AIR: 0.0076
RELATIVE HUMIDITY: 54.00 PERCENT
SAMPLE LINE: TEMPERATURE, OFGRFES C: 150.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME. SFC: I.00
NUMBER OF TESTS: 4
COMMFNTS:
N02 DETERMINED BY SUBTRACTION. ENGINE EQUIPPED KITH SMOKELESS BURNER CANS.
COMMENT LISTED ON CAL ID »285 ALSO APPLY.
42.50
ELAPSED
TIME
0.0
5.00
10.00
15.00
TFST
MODE
I/
21
3/
4/
0
I
2
3
POWER
THRUST, LBS PFRCENT
OR RATED
SHP
10B20.00
11990.00
13850.00
870.00
T.O.
74
82
95
5
ENGINE
SPEFD
RPM
Nl
7360.00
7620.00
BIOO.OO
2650.00
N2
I10RO.OO
11280.00
11600.00
6800.00
MEASURED
FUEL
FLOW
LB/HR
6010.00
6730.00
8050.00
870.00
GAS GEN
AIR FLOW
LB/SEC
126.30
135.00
149.00
37.20
CALC COMPRESSOR
F/A DISCHARGE
IFMP
0.013200
0.013800
0.015000
0.007500
DEGREES F
-0.00
-0.00
-0.00
-0.00
tNGINF
PRESSURE
RATIO
EPR
1.76
1.87
2.04
-0.00
TURBINE
INLET
TFMP
DEGREES F
-0.00
-3.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
74
B2
95
5
FXHAUSI
GAS
TFMP
DEGREES ^
883.00
9IB.OO
981.00
653.00
EXHAUST
GAS
PRESSURE
PS I A
10.70
12.30
14.70
0.60
CO
(WETI
PPMV
12.00
10.00
9.00
272.00
CO
2
IWETI
PERCENT V
2.69
2.63
3.07
1.56
THC
(WETI
PPMV
1.00
1.00
0.0
138.00
NO
I WET)
PPMV
74.00
93.00
135.00
5.00
Nfl
2
IWETI
PPMV
5.00
5.00
6. on
6.00
ALDEHYDES SMUKC PARTICULATFS
(WET)
PPMV
79.00
98.00
141.00
11.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
74
12
95
5
MASS EMI
cn
LB/1K
L8 FUEL
O.H9
0. 70
0.5B
33.88
MASS EMI
HC
LB/1K
LB FUEL
0.04
0.04
0.0
9.S4
MASS EMI
N02
LB/1K
LB FUFL
0.61
0.58
0.64
1.23
MASS EMI
C02
L8/1K
IB FUEL
3111.73
3132.02
3132.32
3053.00
MASS EMI
NO
LB/IK
LB FUEL
9.01
10.76
14.40
1.02
MASS E»l
NC1X
LP/1K
LB FUEL
9.61
11.34
15.04
2.25
MASS FMI
CO
LS/HR
5.34
4.74
4.70
2S.47
MASS EMI
HC
LB/HR
0.26
0.27
0.0
a. 56
MASS FMI
NO 2
LB/HP
3.66
3.89
5.15
1.07
MASS FMI
C02
LB/HR
18821 .6fl
21078.52
25215.20
2656.11
MASS ffl
NO
LB/HP
54.13
72.41
115.92
0.89
MASS FMI
NOX
LP/HR
57.79
76.31
121.07
1.96
POWER
PERCENT
RATED
T.O.
74
82
95
5
CO
LB/1KKTH-HR
0.494
0.395
0.340
33.879
LB/IK«TH-HR
1739.527
1758.008
IB20.592
3053.OC4
THC
L1/1KHTH-HR
0.024
0.023
0.0
9. 844
NO
LB/1K«TH-H«
5.003
6.039
B.369
1.023
LB/IMTH-HB
0.338
0. (25
0.37?
1.228
NO
X
LR/1KUTH-HR
5.341
6.364
8.741
2.250
IV-190
-------
CAL 10 NUMBER: 286 ENGINE TYPE »NO MODEL: jrto-9
TEST ORGANIZATION! S M R I TNA
SERIAL NUMBER: P6742508
MODE FRACTIONAL
POKER
TAKI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
0.060
1.000
0.850
0.400
0.060
POWER
t TH
870.0
1*500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
33.198 829.335
3.499 8596.344
4.600 7090.523
16.010 3627.520
33.198 829.335
USAGE TIME IN
MT FACTOR MODE
NIN.
TOTAL FOR CYCLEl
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IOOOK
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAKI-IDLE
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
POMER
TH
870.0
1*500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
9.701 829.335
0.665 8596.344
0.723 7090.523
1.184 3627.520
9.701 829.135
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.I
USAGE TIME IN
UT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
L8S POLLUTANT/IOOOK
MODE
TAKI-IOLE
' TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POMER
0.060
t.OOO
0.650
0.400
0.060
POMER
f TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.924 829.335
139.373 8596.344
87.191 7090.523
13.813 3627.520
1.924 829.335
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLEI
L8 TH AT T.O.:
USAGE TINE IN
UT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.Q.:
CO
MASS
LBS.
10.513
0.041
0.169
1.067
3.873
15.663
16.290
11.311
0.282
HC
MASS
L8S.
3.072
0.008
0.027
0.079
1.132
4.317
4.490
3.117
0.535
NOX
MASS
LBS.
0.609
1.626
3.197
0.921
0.224
6.578
6.841
4.750
112.139
FUEL
MASS
LBS.
262.62
100.29
259.99
241.83
96.76
961.49
FUEL
MASS
LBS.
262.62
100.29
259.99
241.83
96.76
961.49
FUEL
MASS
LBS.
262.62
100.29
259.99
241.83
96.76
961.49
LB CO /
IK LB FUEL
40.030
0.407
0.649
4.413
40.030
18 HC /
IK L8 FUEL
11.697
0.077
0.102
0.326
11.697
LB NOX/
IK LB FUEL
2.320
16.213
12.297
3.808
2.320
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
I TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB
t
CO /
TH-HR
0.03816
0.00024
0.00037
0.00276
0.03816
LB
1
0
0
0
0
0
LB
HC /
TH-HR
.01115
.00005
.00006
.00020
.01115
NOX/
TH-HR
0.00221
0.00961
0.00707
0.00238
0.00221
IV-191
-------
OATE1 T/29/TI
TEST ORGANIZATION: s w R
ENGINE SUPPLIER: T H A
ENGINE DATA
CAL ID NUMBER: 287
ENGINE TYPE AND MODEL: JT8D-9
SERIAL NUMBER: P654589B
RATED THRUST: 14500.
ENGINE TOTAL TIME: 4226. MRS
TIME SINCE HOT SECTION OVERHAUL: 2*2. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 4226. HRS
NZ COMPRESSOR OVERHAUL: 4226. HRS
COMBUSTOR CAN REPLACEMENT: 242. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 242. HRS
Nl TURBINE OVERHAUL: 4226. HRS
N2 TURBINE OVERHAUL: 1226. HRS
FUEL: JP-4 TF FUEL H/C RATIO: 2.020
OPERATIONAL DATA ««»».
INLET AIR TEMPERATUREt DEGREES F: START 58.00 FINISH 58.00
ATMOSPHERIC PRESSURE: START 24.01 FINISH 29.00
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0110
RELATIVE HUMIDITY: 97.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: ISO.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
ENGINE EQUIPPED WITH SMUKFLESS BURNER CANS. NC2 DETERMINED BY SUBTRACTION.
ELAPSED
TIME
0.0
IS. 00
28.00
31.00
)7.00
TFSI
MODE
If 0
21 1
3/ 2
4/ 3
5/ <<
POWER
THRUST, LBS PERCENT
OR RATED
SHP
9500.
11400.
13200.
1020.
13260.
00
00
00
00
00
T.O.
65
78
91
7
91
ENGINE
SPEED
aPM
Nl
7220.00
7550.00
aooo.oo
2850.00
7960.00
N2
10700.00
11170.00
11480.00
7110.00
11450.00
MEASURED
FUEL
FLOW
LB/HR
5400.00
6500.00
7810.00
980.00
78*0.00
GAS GEN
AIR FLOW
LB/SEC
118.00
132.20
145.70
34.50
146.20
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.012700
0.013700
0.014900
0.007900
0.014900
OFGOEES F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.64
-0.00
-0.00
-0.00
-0.00
TURBINF
INLET
TEMP
0CGRFES F
-0.00
-0.00
-0.00
-0.00
-0.00
POWEP
PERCENT
RATED
T.O.
65
78
91
7
91
EXHAUST
GAS
TEMP
DEGREES F
346.00
907.00
977.00
656.00
977.00
EXHAUST
GAS
PRESSURE
PS I A
9.10
1 1.50
13.60
0.60
13.50
CO
(MET)
PPMV
16.00
11.00
9.00
354.00
8.00
CO
2
IWET)
PERCENT V
2.58
?.ao
3.00
1.64
7.99
THC
IWETI
PPMV
0.0
0.0
0.0
142.00
0.0
NO
IWETI
PPMV
69.00
89.00
121.00
3.00
1 16.00
NO
2
IWFT)
PPMV
6.00
5.00
5.00
9.00
4.00
NO
X
IWFTI
PPMV
75.00
94.00
126.00
12.00
120.00
ALDEHYDES SMCKF PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
HATED
T.O.
65
71
91
7
91
MASS EMI
CO
LB/IK
LB FUEL
1 .24
0.78
0.60
MASS EMI MASS EMI MASS FMI
HC NO 2 CO2
LB/1K LB/IK LB/1K
LB FUEL LB FUEL L8 FUEL
0.1
0.0
0.0
9.60
0."
0.76 3131.30
0.58 3132.01
0.55 3IJ2.30
1.74 3041.26
1.44 3132.40
MASS FMI
NO
IB/IK
IB FUFL
8.75
10.41
13.21
0.58
17.70
MASS EMI
NOX
LB/IK
LB FUEL
9.52
10.99
13.75
2.33
13.14
MASS EMI MASS FMI MASS EMI MASS EMI
CO HC NO? C12
LB/HR UB/HR LB/HR LB/HR
MASS EMI MASS FM|
Nl) NOX
LH/HP LB/HR
6.67 0.0 4.11 16909.02 41.27 51.39
5.09 0.0 3.80 20358.06 67.65 71.45
4.67 0.0 4.26 24443.27 10J.15 107.41
4C.95 9.41 1.71 2980.44 0.57 2.28
4.18 0.0 3.43 24558.04 99.60 103.04
POWER
PERCENT
RATED
i.n.
65
78
91
7
91
CO
LB/1KHTH-MR
0.703
0.447
0.354
40.142
0.315
LB/1MTH-HR
1719.896
1785.795
1853.27R
7921.999
1857.039
LB/1KHTH-HK
0.0
0.0
0.0
9.222
0.0
NU
LB/1KITM-HH
4.976
5.934
7.614
0.559
7.511
L3/1KHTH-HR
0.431
0.333
0.323
1.676
0.259
NO
X
LB/1K«TH-HR
5.409
6.267
S.137
2.235
7.770
IV-192
-------
C»L 10 NUMBER! 287 ENGINE TYPE AND MOOEll JT8D-9
TEST ORGANIZATION: S W R I TWA
SERIAL NUMBER) P654589B
MODE FRACTIONAL
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
POWER
0.060
1.000
o.aso
0.400
0.060
POUER
f TH
870.0
1*500.0
12325.0
5800.0
870.0
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN. .
68.738 789.361 1.000 19.00
5.330 8708. Til 1.000 0.70
4.811 7234.828 1.000 2.20
16.201 3590.599 1.000 4.00
68.738 789.361 1.000 7.00
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLEx
LBS POLLUTANT/ 1000K LB TH AT T.O.:
CO
MASS
L8S.
21.767
0.062
0.176
1.080
8.019
31.105
32.801
22.463
0.429
FUEL
MASS
LBS.
249.96
101.60
265.28
239.37
92.09
948.31
LB CO /
IK LB FUEL
87.081
0.612
0.665
4.512
87.081
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
TH-HR
0.07901
0.00037
0.00039
0.00279
0.07901
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POUER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POMER
0.060
1.000
0.850
0.400
0.060
POWER
f TH
870.0
14500.0
12325.0
5800.0
870. 0
POWER
TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL I
RATE RATE WT
LB/HR LB/HR
11.397 789.361
0.172 8708.711
0.221 7234.828
0.208 3590.599
11.397 789.361
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
1.393 789.361
130.491 8708.711
90.110 7234.828
18.647 3590.599
1.393 789.361
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
SAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
JSAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
HC
MASS
LBS.
3.609
0.002
O.OOB
0.014
1.330
4.963
5.233
3.584
0.138
NOX
MASS
LBS.
0.441
1.522
3.304
1.243
0.162
6.67)
7.037
4.819
104.993
FUEL
MASS
LBS.
249.96
101.60
265.28
239.37
92.09
948.31
FUEL
MASS
LBS.
249.96
101.60
265.28
239.37
92.09
948.31
LB HC /
IK LB FUEL
14.438
0.020
0.031
0.058
14.438
LB NOX/
IK LB FUEL
1.764
14.984
12.435
5.193
1.764
ENERGY
t TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
f TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB HC /
1 TH-HR
0.01310
0.00001
0.00002
0.00004
0.01310
LB NOX/
1 IH-HR
0.00160
0.00900
0.00731
0.00321
0.00160
IV-193
-------
OATCI 7/29/71
TEST ORGANIZATION: S W R I TWA
ENGINE SUPPLIERl I H A
FNCINF DATA
CAL ID NUMBER: 286
ENGINF TYPE AND MODEL: JT8D-9
SERIAL NUMBERI P674266B
RATED THRUST: 14500.
ENGINE TOTAL TIME: 4078. MRS
TINE SINCE HOT SECTION OVERHAUL: 29*5. HRS
TINE SINCE:
NI COMPRESSOR OVERHAUL: »078. HRS
N2 COMPRESSOR OVERHAUL: «OTB. HRS
CONBUSTOR CAN REPLACEMENT: 2945. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 29*5. HRS
NI TURBINE OVERHAUL: 4078. HRS
N2 TURBINE OVERHAUL: 4078. HRS
FUEL: JP-4 TF FUEL H/C RATIO: 2.020
OPERATIONAL DATA «»«»«««« ..,.,....»».
INLET AIR TEMPERATURF> DEGREES F: START 61.00 FINISH
ATMOSPHERIC PRESSURE: START 29.02 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0107
RELATIVE HUMIDITY: 86.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIMF, SEC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
ENGINE EQUIPPED WITH SMOKELESS BURNER CANS. NC2 DETERMINED BY SUBTRACT ION.
63.00
29.02
42.50
ELAPSED
TIME
0.0
10.00
20.no
25.00
31 .00
TEST
MODE
I/
11
3/
4/
5/
0
1
2
3
4
THRUST
OR
SHP
9700.
izoon.
13840.
HBO.
1)360.
POUFR
.LBS PERCENT
BATED
00
00
00
00
00
T.O.
66
8?
95
6
92
f. r»r. i Hf.
SPEED
BPM
Ml
71)0.00
7640.00
8090.00
2520.00
7960.00
N2
10710.00
1 1 irtO.OO
11420.00
6950.00
11260.00
MEASURED
FUEL
FLOW
CAS GEN
AIR FLOU
LB/SEC
CALC
F/A
LB/HR
5470.
6840.
813C.
910.
7770.
00
00
00
00
00
119.00
135. BO
149.30
32.40
146.50
0.012800
0.014000
0.015100
0.007800
0.014700
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIO
DEGREES F SPB
-0.00
-0.00
-0.00
-0.00
-0.00
1.65
1.86
2.02
-0.00
-0.00
TURBINE
INLFI
TEMP
nr.GREES F
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
66
82
95
FXHAUST
GAS
TEMP
DEGREES F
838.00
R9e.OO
961.00
682.00
941.00
EXHAUST
GAS
PRESSURE
PS I A
9.20
12.00
14.50
0.60
13.70
CO CO
IMF.TI 2
PPMV IhFTI
PERCENT V
12.00
9.00
6.00
285.00
6.00
2.59
2.61
2.97
1.62
2.94
THC
(WET)
PPMV
0.0
0.0
0.0
120.00
0.0
NO
(HEM
PPMV
65.00
90.00
117.00
6.00
107.00
NO
2
IWETI
PPMV
3.00
4. CO
5.00
7.00
7.00
NO
X
IWEU
PPMV
68.00
94.00
122.00
13.00
I 14.00
ALDEHYDES SMOKE PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.no
-0.00
-0. 00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
66
62
95
6
92
MA
-------
CAI ID NUMBER: 2ee ENGINE TYPE AND MODEL: jiso-9
TEST ORGANIZATION: s w R i TWA
SERIAL NUMBER: P6T4266B
MODE FRACTIONAL
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
POKE"
0.060
1.000
0.850
0.400
0.060
POKER
f TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE
LB/MR
33.905
2.840
3.938
9.291
33.905
RATE
LB/HR
817.096
8499.000
7098.379
2975.971
817.096
USAGE TINE IN
HT
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
TOTAL FOR CVCLEl
LBS
LBS
L8S
POLLUTANT/IK
POLLUTANT/IK
LB
LB
POLLUTANT/1000X
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
10.736
0.033
0.144
0.619
3.956
15.489
16.985
11.185
0.229
FUEL
MASS
LBS.
258.75
99.15
260.27
198.40
95.33
911.90
LB CO /
IK LB FUEL
41.494
0.334
0.555
3.122
41.494
ENERGY
TH-HR
275.50
169.17
451.92
3B6.67
101.50
1384.75
LB CO /
TH-HR
0.03897
0.00020
0.00032
0.00160
0.03897
MODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIM80UT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
TH
870.0
14500.0
12325.0
5800.0
870.0
POWER
TH
B70.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
7.559 817.096
0.170 8499.000
0.142 7098.379
0.227 2975.971
7.559 817.096
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE HT
LB/HR LB/HR
1.888 817.096
125.981 8499.000
80.093 7098.379
17.350 2975.971
1.888 817.096
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
L8 TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
HC
MASS
LBS.
2.394
0.002
0.005
0.015
0.882
3.298
3.616
2.382
0.137
KOX
MASS
LBS.
0.59B
1.4TO
2.937
1.157
0.220
6.381
6.998
4.608
101.364
FUEL
MASS
LBS.
258.75
99.15
260.27
198.40
95.33
911.90
FUEL
MASS
LBS.
258.75
99.15
260.27
198.40
95.33
911.90
LB HC /
IK LB FUEL
9.251
0.020
0.020
0.076
9.251
LB NOX/
IK LB FUEL
2.310
14.823
11.283
5.830
2.310
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB HC /
1 TH-HR
0.00869
0.00001
0.00001
0.00004
0.00869
LB NOX/
1 TH-HR
0.00217
0.00869
0.00650
0.00299
0.00217
IV-195
-------
OATEl 8/ 3/71
TEST ORGANIZATION: s w R i IMS
ENGINE SUPPLIED: T « A
ENGINE DAT*
CAL ID NUMBER: 303
ENGINE TYPE AND MODEL: JT6D-9
SERIAL NUMBER: P674379B
RATED THRUST: 14500.
ENGINE TOTAL TIME: 3686. MRS
TIME SINCE HOT SECTION OVERHAUL: 460. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 3686. HRS
N2 COMPRESSOR OVERHAUL: 3686. HRS
COMBUSTOR CAN REPLACEMENT: 460. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 3686. HRS
NI TURBINE OVERHAUL: 36B6. HRS
N2 TURBINE OVERHAUL: 3686. HRS
FUEL H/C RATIO: 2.020
78.00
28.67
FUEL: JP-4 TF
OPERATIONAL DATA *»«««««*»«*
INLET AIR TEMPERATURE, DEGREES F: START 78.00 FINISH
ATMOSPHERIC PRESSURE: START 28.97 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0129
RELATIVE HUMIDITY: 60.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOM RATE, L1TERS/MIN: 42
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 4
COMMENTS:
N02 DETERMINED BV SUBTRACTION. ENGINE EOUIPPFO KITH SMOKELESS BURNER CANS.
THIS TEST AND TEST CAL NO. 304 WERE RUN ON THE SAME JT8D-9 ENGINE. TEST 303
WAS RUN WITH NG SMOKE ELIMINATOR (ETHYL CJ-21 IN THE FUEL AND TEST 304 HAS RUN
KITH FUEL CONTAINING THE NORMAL CONCENTRATION OF CI-2 10.H BY VOLUME!
ELAPSED
TIME
0.0
5.00
10.00
19.00
TEST
MODF
11
21
3/
4/
0
I
2
3
POWER
THKUST.LRS PERCENT
OR RATED
SHP
9640.00
11820.00
13780.00
900.00
T.O.
66
81
95
6
ENGINE
SPEED
RPM
Nl
7250.00
7730.00
8260.00
2710.00
N2
IOB80.00
11210.00
11570.00
6960.00
MEASURED
FUEL
FLOW
LB/HR
5540.00
6840.00
8220.00
880.00
GAS GEN
AIR FLOW
LB/SEC
116.50
132.20
147.40
32.30
CALC COMPRESSOR
E/A DISCHARGE
TEMP
0.013200
0.014400
0.015500
0.007600
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POHER
PERCENT
RATFO
T.O.
66
81
95
6
EXHAUST
GAS
TEMP
DEGREES F
830.00
945.00
1018.00
680.00
FXHAUST
GAS
PRESSURF
PSIA
9.00
11 .90
14.50
0.60
en
IWETI
PPMV
11.00
12.00
11.00
318.00
CO
7
IWETI
PERCENT V
2.69
2.93
3. 14
1.60
THC
IWETI
PPMV
0.0
0.0
0.0
167.00
NO
IWETI
PPMV
62.00
86.00
119.00
5.00
NO
2
IWETI
PPMV
5.00
4.00
6.00
7.00
ALDEHYDES SMOKE PARTICULATES
I WET)
PPMV
67.00
90.00
125.00
12.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
66
81
95
MASS EMI MASS FMI
CO HC
IB/IK Lfl/lK
LB FUEL LB FUEL
0.82
0.82
0.70
38.47
0.0
0.0
0.0
1 1.57
MASS EMI
^02
LB/IK
LB FUEL
0.61
0.45
0.63
1.19
MASS EMI
C02
LB/IK
LB FUEL
3131.96
1111.96
3132.14
3041.06
MASS EMI
NO
LB/IK
LB FUEL
7.55
9.61
12.41
C.99
MASS EMI
NOX
LB/IK
LB FUEL
8.15
10.06
13.03
2.18
MASS EMI
CO
LB/HH
4.52
5.53
5.74
13.85
MASS EMI
HC
LB/HR
0.0
0.0
0.0
10. 18
MASS EMI
NO 2
LB/HR
3.17
3.06
5. 14
1.22
MASS EMI
CO 2
LB/HR
17351.05
21472.59
25746.21
2676.11
MASS EMI
NO
LB/HB
41.81
65.73
102.00
0.37
1ASS EMI
NUX
LD/HR
45.18
68. 79
107. 15
2. 10
POWFR
PERCENT
HATED
T.O.
66
61
95
6
co
LB/1KHTH-HR
0.468
0.472
0.417
37.613
LB/IK«TH-H'»
1799.902
1312.402
1368.375
2973.481
THC
LB/1KHTH-HR
0.0
0.0
0.0
I 1.31 3
NO
LO/1KITH-HR
4.337
5.561
7.402
0.971
LB/1KHTH-HR
0.350
C.?59
0.373
1.160
NO
X
LB/IK»TH-HR
4.687
5.S20
7.775
2.131
IV-196
-------
C»L 10 NUMBER: 303 ENGINE TYPE *ND MODEL: J180-9
TEST ORGANIZATION: S W R I TWA
SERIAL NUMBER' P6743T9B
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.950
0.400
0.060
POKER
TH
870.
14500.
12325.
5600.
870.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
33.265 746.939
6.794 8704.867
5.361 7259.121
10.568 3423.015
33.265 746.939
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000X
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
1 TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
10.019 746.939
0.0 8704.867
0.218 7259.121
0.609 3423.015
10.019 746.939
WT
TOTAL FOR CYCLE:
IBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
TH
870.
14500.
12325.
5800.
870.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.192 746.939
126.443 8704.867
79.471 7259.121
18.366 3423.015
1.192 746.939
WT
USAGE TIME IN
FACTOR MODE
MIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL/CYCLE!
TH-HR/CVCLEl
LB TH AT T.O.:
USAGE TINE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
CO
MASS
LBS.
10.534
0.079
0.197
0.705
3.881
15.395
16.741
11.118
0.547
HC
MASS
LBS.
3.173
0.0
0.008
0.041
1.169
4.390
4.774
3.170
0.0
NOX
MASS
LBS.
0.377
1.475
2.914
1.224
0.139
6.130
6.666
4.427
101.735
FUEL
MASS
LBS.
236.53
101.56
266.17
228.20
87.14
919.60
FUEL
MASS
LBS.
236.53
101.56
266.17
228.20
87.14
919.60
FUEL
MASS
LBS.
236.53
101.56
266.17
228.20
87.14
919.60
LB CO /
IK LB FUEL
44.535
0.780
0.739
3.087
44.535
LB HC /
IK LB FUEL
13.414
0.0
0.030
0.178
13.414
LB NOX/
IK LB FUEL
1.596
14.526
10.948
5.365
1.596
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
TH-HR
0.03824
0.00047
0.00043
0.00162
0.03824
LB HC /
f TH-HR
0.01152
0.0
0.00002
0.00011
0.01152
LB NOX/
TH-HR
0.00137
0.00872
0.00645
0.00317
0.00137
IV-197
-------
OATE1 «/ 3/71
TEST ORGANIZATION! S W R I TUA
ENGINE SUPPLIER! IMA
ENGINE Dirt
CAL ID NUMBER: 30*
ENGINE TYPE «ND MODEL! JT8D-9
SERIAL NUMBER! P674J79B
RATED THRUSH 14500.
ENGINE TOTAL TINE: 3686. MRS
TINE SINCE HOI SECTION OVERHAUL: 460. HRS
TINE SINCE!
Nl COMPRESSOR OVERHAUL: 3686. HRS
N2 COMPRESSOR OVERHAUL! 3686. HRS
COMSUSTOR CAN REPLACEMENT: 460. HRS
flRST STAGE NOZZLE GUIDE VANE OVERHAUL: 1686. HRS
Nl TURBINE OVERHAUL: 3686. HRS
N2 TURBINE OVERHAUL: 3686. HRS
FUEL H/C RATIO: 2.070
FUEL: JP-4 TF
OPERATIONAL DATA ««««»«t««««*»>*
INLET AIR TEMPERATURE, DEGREES F: START 80.00 FINISH 80.00
ATNOSPHFRIC PRESSURE: START 20.97 FINISH 20.97
INLET AIR HUMIDITY, LBS HZO/LB AIR: 0.0129
RELATIVE HUMIDITr: 54.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.OC, FLOW RATE, LITtRS/MIN:
SAMPLE LINE TRANSPORT MMF, SFC: 1.00
NUMBER OF TESTS: 4
COMMENTS I
N02 DETERMINED BY SUBTRACTION. ENGINE EQUIPPED WITH SMOKELESS BURNER CANS.
FUEL CONTAINS THF 'NORMAL' CONCENTRATION OF CI-2 SMOKE SUPPRESSANT 10.II BY
VOLUMEI. THIS IS THF SAME ENGINE 1E5TEO DURING TEST CAL NO. 303.
ELAPSED
TIME
0.0
3.30
8.00
13.00
TFST
MODE
I/
2/
3/
4/
0
1
2
3
POWER
THRUST, LBS PERCENT
OR RATED
SHP
9700.
11900.
11740.
900.
00
00
00
00
T.O.
66
82
94
6
ENGINE
SPEED
RPM
Nl
7250.00
7790.00
8260.00
2720.00
N2
10890
11260
11590
6950
.00
.00
.00
.00
MEASURED
FUEL
FLOW
LB/HR
5480.00
6910.00
5300.00
890.00
GAS GEN
AIR FLOW
LB/SEC
116.70
132.90
146.60
32.30
CALC
F/A
0.013000
0.014400
0.015700
0.007600
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIO
DEGREES F EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TUKBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
66
B2
94
EXHAUST
OAS
TEMP
DEGREES F
878.00
950.00
I 03 I.00
685.00
EXHAUST
GAS
PRESSURE
PSIA
9.00
1 1.90
14.30
0.60
CO
I WET I
PPMV
26.00
19.00
15.00
345.00
CO
2
IWETI
PERCENT
2.66
2.98
3.20
1.59
THC
IMETI
PPMV
0.0
0.0
0.0
194.00
NO
IWFTI
PPMV
61.00
89.00
119.00
5.00
NO
2
IUFTI
PPMV
5.00
2.00
4.00
7.00
NO
X
(WET)
PPMV
(.6.00
91.00
123.00
129.00
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POKER
PERCENT
RATED
T.O.
66
B2
94
6
MASS EMI
CO
LB/1K
LB FUEL
1.95
1.27
0.93
41 .R5
MASS FMI
HC
LH/1K
LB FUEL
0.0
0.0
0.0
13. 4H
MASS EMI
N02
LR/IK
LR FUFL
0.62
0.22
0.41
1.39
MASS EMI
C02
LA/IK
LB FUEL
3 1 30 . 1 8
3131.24
3131.77
3030.51
MASS EMI
NO
LB/IK
LB FUEL
7.50
9.78
12. 18
1.00
MASS FMI
NOX
LB/IK
LB FUEL
8.12
10.00
12.58
25.70
MASS EMI
CO
LB/HR
10.67
8.78
4.95
37.25
MASS FMI
HC
LB/HR
0.0
0.0
0.0
12.00
MASS EMI
NO 2
LB/HP
3.37
1.52
2.17
1.24
MASS EMI
C02
LB/HR
17153.39
21636.89
16598.39
2697.15
MASS EMI
NU
LB/HR
41.12
67.55
64.53
0.89
MASS EMI
unx
LB/HR
«4.49
69.07
66.70
22.88
POWER
PERCENT
KATFD
T.O.
66
82
94
CO
LH/IK«TH-IIR
1.100
0.738
0.160
41.385
LB/ IMTM-HR
176(1.391
1818.726
120H.034
2996.838
THC
LB/1K«TH-HR
0.0
0.0
0.0
11.328
NO
LB/1K0TM-HR
4.239
5.677
4.696
0.985
LB/1KKTM-HR
0.347
0. 128
0.158
1.379
LB/ IKKTH-HR
4.587
5.804
4.854
25.418
IV-198
-------
CAL 10 NUNBERl 304 ENGINE TYPE AND MODEL1 JT80-9
TEST ORGANIZATION: s w R i TWA
SERIAL NUMBER: P674379S
MODE
TAX-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POVER
0.060
1.000
0.850
0.400
0.060
POKER
f TH
870.
14500.
12325.
5800.
870.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/KR LB/HR
32.009 761.719
9.190 8561.344
10.375 7169.719
15.135 3286.938
32.009 781.719
KT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POILUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
CLIKBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POVER
0.060
1.000
0.850
0.400
0.060
PONER
1 TH
870.
14500.
12325.
5 BOO.
870.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
11.374 781.719
0.0 8561.344
0.0 7169.719
1.014 3286.938
11.374 781.719
KT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
IBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POKER
1 TH
870.
14500.
12325.
5800.
870.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
3.594 781.719
234.290 8561.344
151.259 7169.719
35.232 3286.938
3.594 781.719
WT
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
USAGE TIME IN
FACTOR MODE
NIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE"
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLEl
TH-HR/CYCLEi
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CVCLEl
TH-HR/CYCLE!
LB TH AT T.O.I
CO
MASS
LBS.
10.136
0.107
0.380
1.009
3.734
15.367
16.692
11.098
0.739
HC
MASS
LBS.
3.602
0.0
0.0
0.068
1.327
4.996
5.427
3.608
0.0
NOX
MASS
LBS.
1.138
2.733
5.546
2.349
0.419
12.186
13.236
8.800
188.509
FUEL
MASS
LBS.
247.54
99.88
262.89
219.13
91.20
920.65
FUEL
MASS
LBS.
247.54
99.88
262.89
219.13
91.20
920.65
FUEL
MASS
LBS.
247.54
99.88
262.89
219.13
91.20
920.65
LB CO /
IK LB FUEL
40.947
1.073
1.447
4.605
40.947
LB HC /
IK LB FUEL
14.550
0.0
0.0
0.309
14.550
LB NOX/
IK LB FUEL
4.598
27.366
21.097
10.719
4.598
ENERGY
f TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
f TH-HR
0.03679
0.00063
0.00084
0.00261
0.03679
LB HC /
t TH-HR
0.01307
0.0
0.0
0.00017
0.01307
LB NOX/
1 TH-HR
0.00413
0.01616
0.01227
0.00607
0.00413
IV-199
-------
0»TEl 7/U/T1
TEST ORGANIZATION: s w R
ENGINE SUPPLIER: T H A
ENGINE DATA
CAL 10 NUMBER: 305
ENGINE TYPE AND MODEL: JT8D-9
SERIAL NUMBER! P674299B
RATED THRUST: 14500.
ENGINE TOTAL TIME: 3674. HRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 367*. HRS
N2 COMPRESSOR OVERHAUL: 3674. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: 3674. HRS
N2 TURBINE OVERHAUL: 3674. HRS
FUEL: JP-4 TF FUEL H/C RATIO: 2.020
OPERATIONAL DATA »«»««
INLET AIR TEMPERATUREi DEGREES F: START 79.00 FINISH
ATMOSPHERIC PRESSURE: START 28.92 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0152
RELATIVE HUMIDITY: 68.00 PERCFNT
SAPPLF LINE: TEMPERATURF, DEGREES C: ISO.00. FLOW RATE, LITERS/HIM:
SAMPLE IINE TRANSPORT TIME. SEC: 1.00
NUMBER OF TESTS: *
COMMENTS:
N02 OETERM1NFD BY SUBTRACTION. ENGINE EQUIPPED WITH SMOKELESS RURNFR CANS.
79.00
28.92
ELAPSED
TIME
0.0
5.00
11.10
16.30
TFST
MODE
I/
21
3/
4/
0
1
2
3
POWER
THRUST, LBS PERCENT
OR RATED
SHP
9450.00
11120.00
13400.00
1020.00
T.n.
65
78
92
7
ENGINF
SPEED
RPM
NI
7160.00
7550.00
8060.00
2850.00
N2
10830.00
11160.00
11480.00
7120.00
MEASURED
FUEL
FLOW
LB/HR
5470.00
6520.00
7850.00
1190.00
GAS GEN
AIR FLOW
LB/SEC
115.10
128.50
144. 10
34.10
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.013200
0.014100
0.015300
0.009700
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.65
1.81
2.02
-0.00
TURPINE
INLET
TEMP
DEGRFES F
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
65
78
92
7
FXHAUST
GAS
TEMP
DEGREES F
895.00
941.00
loni.oo
681.00
EXHAUST
CAS
PRtSSURE
PS1A
9. 10
11.30
14.10
0.60
en
IHETI
PPMV
26.00
20.00
1 7.00
305.00
cn
2
(MET)
PERCENT V
2.65
2.80
3.05
I.85
THC
IWETI
PPMV
1.00
0.0
0.0
94.00
NO
(WEI)
PPMV
63.00
85.00
120.00
2.00
NO
2
IWET)
PPMV
6.00
4.00
n.oo
8.00
ALDEHYDES SMOXE PARTICULARS
IMETI
PPMV
69.00
89.00
128.00
10.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
65
ra
92
7
MASS EMI
cn
LR/1K
l« FUEL
1.95
1.42
1.11
32.18
MASS EMI
HC
LR/IK
LB FUFL
0.04
0.0
0.0
5.68
MASS FMI
Ntl2
LB/IK
LH FUFL
0.74
0.47
0.86
1.39
MASS EMI
C02
LB/IK
LR FUEL
3130.05
31 31.00
1131.50
3067. C9
MASS EMI
NO
LB/IK
Lfl FUFL
7.78
9.94
12.88
0.15
MASS EMI
NOX
LP./U
LB FUEL
8.52
10.40
13.74
I.T.I
MASS EMI
CO
LB/HR
10.69
9.28
8.72
38.30
MASS FMI
HC
LB/HH
0.24
0.0
0.0
6.76
MASS EM
N02
LB/HR
4.05
3.05
6.74
1.65
MASS FMI
CU2
LB/HR
17121.39
20414.14
24582.25
3649.84
MASS EMI
NO
LB/HR
42.55
64.7H
101.11
0.41
MASS FMI
NOX
Lfl/HR
46.60
67.83
107.65
2.06
POWER
PFRCENT
RATED
i.n.
65
78
92
7
CO
LB/IKHTH-HR
1.131
0.420
0.651
17.546
Lfl/lK«TH-MR
1811.797
1803.369
1814.496
3578.274
THC
LB/1K«!H-HR
0.025
0.0
0.0
6.627
NO
L9/1KMH-HR
4.503
5.723
7.545
0.404
LO/1K«TH-HR
0.429
0.269
0.503
1.618
NO
X
LB/1K«TM-HR
4.932
5.992
8.048
2.322
IV-200
-------
CAL ID NUMBER: 109 ENGINE TYPE AND MODEL: JTBD-9
TEST ORGANIZATION: s H R I TWA
SERUl NUMBER: P674299B
MODE FRACTIONAL
TAXI-IDLE
TAKEOFF
CUMBOUT
APPROACH
TAXI-IDLE
POKER
0.060
1.000
0.950
0.400
0.060
POWER
TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE HATE
LB/HR LB/MR
51.007 1082.791
8.538 8519.730
9.27* 7168.73*
15.276 3521.186
51.007 1082.743
TOTAL FOR CYCLE:
IBS POLLUTANT/IK
LBS POLLUTANT/IK
USAGE TIME IN
WT
LB
LB
IBS POLLUTANT/1000K
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE"
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
16.152
0.100
0.340
1.018
5.951
23.561
22.085
17.015
0.687
FUEL
MASS
LBS.
142.88
99.86
262.85
234.89
126.11
1066.82
LB CO /
IK LB
47.
0.
1.
4.
47.
FUEL
107
997
294
336
107
ENERGY
1 TM-H»
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
TH-HR
0.05861
0.00059
0.00075
0.00261
0.05863
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TtXI-IOLE
FRACTIONAL
POHER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
POHER
f TH
870.0
14500.0
12325.0
5800.0
870.0
POWER
f TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE UT
LB/HR LB/HR
7.703 1082.793
0.309 8559.730
0.359 7168.734
1.227 3523.386
7.703 1082.791
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
1.816 1082.793
117.944 8559.710
85.091 7168.714
17.923 1521.186
1.816 1082.79}
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
HC
MASS
LBS.
2.439
0.004
0.013
0.082
0.899
3.417
3.221
2.482
0.249
NOX
MASS
IBS.
0.575
1.609
1.120
1.195
0.212
6.711
6.291
4.847
110.989
FUEL
MASS
LBS.
142.88
99.86
262.85
234.89
126.11
1066.82
FUEL
MASS
LBS.
142.88
99.86
262.85
214.89
126.11
1066.82
LB HC /
IK LB FUEL
7.114
0.036
0.050
0.348
7.114
LB NOX/
IK LB FUEL
1.677
16.115
11.870
5.087
1.677
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
186.67
101.50
1384.75
LB HC /
1 TH-HR
0.00885
0.00002
0.00003
0.00021
0.00885
LB NOX/
TH-HR
0.00209
0.00951
0.00690
0.00309
0.00209
IV-201
-------
OATEl 8/ 6/71
TEST ORGANIZATION: s w R i rut
ENGINE SUPPLIER: rut
ENGINE OATi
C»l ID NUMBER: 330
ENGINE TYPE AND MODEL: JT80-9
SERIAL NUMBER: P665*OBB
RATED THRUST: 14500.
ENGINE TOTAL TIME: 6025. HRS
TINE SINCE HOT SECTION OVERHAUL: 2937. HRS
TINE SINCE:
NI COMPRESSOR OVERHAUL: 6029. HRS
N2 COMPRESSOR OVERHAUL: 6025. HRS
COMBUSTOR CAN REPLACEMENT: 2937. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 2937. HRS
NI TURBINE OVERHAUL: 6025. HRS
N2 TURBINE OVERHAUL: 6025. HRS
FUEL: JP-4 TF FUEL H/C RATIO: 1.722
OPERATIONAL DATA *»*«»»*«»«««««»«««*«»
INLET AIR TEMPERATURE, DEGREES F: START 65.00 FINISH 65.00
ATMOSPHERIC PRESSURE: START 24.12 FINISH 29.12
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.0113
RELATIVE HUMIDITY: 83.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.OC, FLOW RATE, LITFRS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 8
COMMENTS:
NO 2 DETERMINED BY SUBTRACTION. ENGINE EOUIPPED WITH SMOKELESS BURNER CANS.
ELAPSED
TIME
0.0
6.00
9.00
12.00
14.30
16.00
19.30
22.00
TEST
MODE
4/ 0
7/ 4
B/ 7
II fl
10/ 9
1/10
21 1
3/ 2
POWER
THRUST, IBS
OR
SHP
aon. oo
1850.00
2960.00
4090.00
5180.00
9640.00
11380.00
13910.00
PERCENT
RATED
T.O.
6
12
20
2B
35
66
78
95
ENGINE
SPEED
RPM
NI N2
MEASURED
FUEL
FLOW
LR/HR
GAS GEN
AIR FLOW
LB/SEC
CALC
F/A
6
12
20
2B
35
66
78
95
27.30.00
3800.00
466C.OO
5)10.00
5780.00
7580.00
7710.00
8190.00
6840.00
8230.00
8920.00
9450.00
9760.00
106BO.OO
10740.00
11400.00
930. CO
1570.00
IP40.00
2420.00
2950.00
5540.00
6510.00
(1370.00
32.90
47.50
59.60
71.70
B2.30
11B.ZO
131.20
150.20
0.007900
0.009200
0.006600
0.009400
0.010000
0.013000
0.013800
0.015500
COMPRESSOR
DISCHARGE
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
IURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
6
12
20
28
35
66
78
95
EXHAUST
GAS
TEMP
DEGREES F
666.00
698.00
610.00
648.00
685.00
B51.00
900. 00
993.00
EXHAUST
CAS
PRESSURE
PSIA
0.60
1.30
?. 30
3.30
4.30
9.40
11.30
14.70
cn
1 WETI
PPMV
362.00
169.00
B8.00
55.00
29.00
IB. 00
1 1 .00
6.00
CO
2
IHETI
PERCENT V
1.65
1.91
1.80
1.94
2.07
2.65
2. BO
3. 14
THC
IWETI
PPMV
140."0
22.00
13.00
4.00
2.00
0.0
0.0
0.0
NO
IWFTI
PPMV
11.00
17.00
IB. 00
22.00
29.00
62.00
76.00
111.00
NO
2
IMETI
PPMV
2.00
5.00
3.00
7.00
(,.00
5.00
5.00
8.00
NO
X
IWETI
PPMV
13.00
22.00
21.00
29.00
35.00
67.00
61.00
119.00
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-0.00
-0.00
-0.00
-O.DO
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.co
-0.00
-c.co
POKER
PERCENT
RATED
T.O.
6
12
20
28
35
66
7fl
95
MASS EMI
CO
LB/1K
Lii FUEL
43.39
17.85
4.91
5.76
2.B5
1 .38
0.89
0.39
MASS EMI
HC
IB/ IK
LB FUEL
9.61
1.33
0.84
n.24
0.11
0.0
0.0
0.0
MASS EMI
M02
LB/IK
LB FUEL
0.39
0.87
0.55
1.20
0.97
0.61
0.60
O.flS
MASS FMI
C02
LB/IK
LB FUCI.
3107.18
3170.01
3183.115
3192.00
3196.43
3199.54
3200.45
3201. 10
MASS EMI
NO
LB/IK
I.B FUEL
2.17
2.95
3.3)
3.78
4.68
7.83
9.08
11.83
MASS EMI
NOX
LB/IK
LB FUEL
2.56
3.82
3.88
4.99
5.65
B.46
9.68
I?.6B
MASS EMI
CO
LB/HR
40.15
2B.03
18.23
13.94
8.41
7. 66
5.21
3.26
ASS FMI
HC
LB/HR
B.94
2.09
1.54
0.5H
0.33
0.0
0.0
0.0
MASS FMI
N02
LB/HR
0.37
1.36
1.02
2.41
2.B6
3.50
3.89
7. 14
MASS EMI
CU2
LB/HR
2B89.68
4976.92
585B.27
7724.64
9430.93
17725.44
20834.94
26793.20
MASS EMI
NO
LB/HR
2.01
4.63
6.12
9.16
13.81
43. )5
59.12
49.01
MASS EMI
NI1X
LB/HR
2.38
5.99
7.14
12.07
16.67
46. 85
63.01
106. 15
POWER
PERCENT
RATED
T.O.
6
12
20
26
35
66
78
95
cn
LB/1KHTH-HR
45.851
15.150
6. 15B
3.4C8
1.623
0. 795
0.459
0.234
LR/1K» TH-HR
32B3.722
2640.227
1979.147
IRB8.666
1B20.643
1838.719
1B30.B3H
1926.183
IHC
LB/IKMIH-HR
10.156
1.129
0.521
0. 142
0.064
0.0
0.0
0.0
NO
LB/1KITH-HR
2.2P9
2.503
2 .069
2.239
2.666
4 .497
5.195
7.11B
L*V 1KKTH-HR
0.416
0.736
0.345
0.712
0.552
0.363
0.342
0.513
NO
X
LB/IK«TH-HR
2.705
3.239
2.414
2.951
3.2IB
4.860
5.537
7.6M
IV-202
-------
C»L ID NUMBER! 130 ENGINE TYPE AND MODEL: JT8D-9
TEST ORGANIZATION: S M R I TWA
SERIAL NUNBERl P6654088
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TA«I-IOLE
FRACTIONAL
POWER
0.060
1.000
0.810
0.400
0.060
POWER
1 TH
8TO.
14500.
12321.
5800.
870.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
34.122 710.021
5.126 8727.305
6.353 7091. 416
9.212 3378.473
34.122 790.021
MT
TOTAL FOR CTCLEl
L8S POLLUTANT/IK LB
IBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
NODE
TAII-IOLE
TAKEOFF
CLINBOUT
APPROACH
TAII-IDLE
FRACTIONAL
POWER
0.060
1.000
0.650
0.400
0.060
POWER
TH
B70.
14500.
12321.
5800.
8TO.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
6.663 790.021
0.166 8727.305
0.218 7091.418
0.289 3378.473
6.683 790.021
wr
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TM-HR/CYCLE:
LB TH AT T.O.I
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
TOTAL FOR CYCLE I
LBS POLLUTANT/IK LB FUEL/CYCLE!
LBS POLLUTANT/IK 18 TM-HR/CYCLE1
LBS POLLUTANT/IOOOK LB TH AT T.O.I
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.8*0
0.400
0.060
POWER
1 TH
870.
14500.
12325.
5800.
870.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
2.093 790.021
117.144 8727.305
77.195 7091.418
19.496 3376.473
2.093 790.021
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
USAGE TIME IN
FACTOR MODE
HIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.t
CO
MASS
LBS.
10.805
0.060
0.233
0.614
3.981
15.693
16.685
11.333
0.412
HC
MASS
LBS.
2.116
0.002
0.008
0.019
0.780
2.925
3.147
2.112
0.134
NO I
MASS
LBS.
0.663
1.36T
2.830
1.300
0.244
6.404
6.690
4.625
94.253
FUEL
MASS
LBS.
250.17
101.82
260.02
225.23
92.17
929.41
FUEL
MASS
LBS.
250.17
101.82
260.02
225.23
92.17
929.41
FUEL
MASS
LBS.
250.17
101.62
260.02
225.23
92.17
929.41
LB CO /
IK LB FUEL
43.191
0.567
0.896
2.727
43.191
LB HC /
IK LB FUEL
8.459
0.019
0.031
0.086
6.459
LB NOX/
IK LB FUEL
2.649
13.423
10.866
5.771
2.649
ENERGY
f TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
i TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
TH-HR
0.03922
0.00035
0.00052
0.00159
0.03922
LB HC /
TH-KR
0.00768
0.00001
0.00002
0.00005
0.00768
LB NOX/
TH-HR
0.00241
0.00808
0.00626
0.00336
0.00241
IV-203
-------
D«TE: 8/ 9/71
TEST ORGANIZATION: S W R I TMA
ENGINE SUPPLIER: TWA
ENGINE DATA
CAL 10 NUMBER: 332 ENGINE TYPE AND MODEL: JT80-9
RATED THRUST: 1*500.
ENGINE TOTAL TIMF: 0. MRS
TIPE SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: o. MRS
N2 COMPRESSOR OVERHAUL: o. MRS
COMRUST1R CAN REPLACEMENT: 0. HRS
FIRST STAGE N022LE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE HVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUFL: jp-4 Tr FUEL H/C RATIO: 1.722
OPERATIONAL DATA «»»«««»«»»«««««««««««
INLET AIR TEMPERATURE. DEGREES F: START 87.00 FINISH
ATMOSPHERIC PRESSURE: START 21.05 FINISH
INLET AIR HUMIDITY, IBS H20/LB AIR: 0.0121
RELATIVE HUMIDITY: 41.00 PERCENT
SAMPLE LINE: TEMPERATURE, OFGRFFS C: 150.00, FLOW RATE. LIICRS/MIN: 4
SAMPLE LINE TRANSPORT TIMF, SEC: 1.00
NUMBER OF IESTS: 10
COMMFNTS:
N02 DETERMINER RY SUBTRACTION. ENGINF EQUIPPED WITH SMOKELESS BURNER CANS.
THIS ENGINE HAS NEW, AND WAS USED AS A CALIBRATION ENGINE TO CHECK TWA'S TEST
CELLS AGAINST PKATT L WHITNEY'S.
SERIAL NUMBER: P66570*B
87.00
29.05
FLAPSEO
TIMF
0.0
6.00
B.OO
12.00
17.00
23.00
25.00
29.00
34.00
39.00
POWFR
PERCENT
RATED
T.Q.
65
79
17.
6
8
10
12
70
J4
48
POWER
PERCENT
RATED
T.O.
65
79
97
6
8
10
12
20
34
41
POWER
PFRCENT
RATED
T.O.
65
79
92
6
8
10
12
20
34
48
TEST POWFR ENGINE MEASURED GAS GEN
XflDE THKUST.LBS PERCENT SPEED FUEL AIR FLOW
OR RATED RPM FLOW LB/SF.C
SHP
I/ 0 9500.00
11 1 11500.00
3/ 2 13450.00
4/ 3 flRO.OO
11 4 1260.00
8/ 1 1500.00
9/ a 1760.00
IO/ 9 3000.00
11/10 5020.00
12/11 7000.00
EXHAUST EXHAUST
GAS GAS
TEMP PRf.SSUR
DEGBEFS r PSIA
876.00 9.00
960.00 11.30
1074.00 14.10
717.00 0.60
759.00 0.80
770.00 1.10
777.00 1.10
667.00 2.30
718.00 4.10
770.00 6.20
MASS EMI MASS EMI
cn HC
LB/1K LB/1K
LO FUEL LH FUEL
1.14 0.04
0. 79 0.0
0.52 0.0
37.33 7.79
23.93 5.16
19.71 3.53
16.42 2.67
9.07 1.67
7.95 0.55
7.17 0.70
r.n
LB/IKITH-HR
0.652
0.453
0.309
39.448
23.935
18.394
14. 365
5.306
2.113
1.739
I.n. Nl N2 L8/HR
65 7330. OC 10980.00 5410. CO 114.90
79 7660.00 11300.00 6620.00 129.00
97 8170.00 11650.00 8020.00 143.80
6 2770.00 6900.00 930.00 32.20
H 3280.00 7650.00 1260.00 36.90
10 3530.00 7990.00 1400.00 39.70
12 37BO.OO 8280.00 1540.00 43.50
70 47HO.OO 9130.00 1920.00 58.70
34 5820.00 9950. OC 2940.00 79.00
48 6550.00 10480.00 3990.00 96.10
CO CO THC NO NO
IWETI 7 IWETI IWFTI 2
E PPMV IWEM PPMV . PPMV IWETI
PERCENT V PPMV
15.00 2.67 1.00 66. CO 5.00
11.00 2.15 0.0 85.00 5.00
8.00 .14 0.0 116.00 5.00
310.00 .65 113.00 11.00 1.00
234.00 .96 88.00 13. Oil 2.00
192.00 .96 60.00 16. CO 1.00
162.00 .99 46.00 18.00 2.00
86.00 .92 31.00 19.011 2.00
41.00 .11 10.00 28.00 4.00
25.00 2.34 4.00 43.00 5.00
CALC
F/A
0.013100
0.014200
0.015500
0.008000
0.009500
0.009800
0.009800
0.009300
0.010300
0.011500
NO
X
IWETI
PPMV
71.00
90.00
121.00
12.00
15.00
17.00
20.00
21.00
32.00
48.00
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TFMP RATIO
OEGREFS f EPR
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
TURBINE
INLET
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
ALDEHYDES SMOKE P ART ICULATES
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
HISS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS E«l
NO? cn? NO NOX cn
LB/1K LB/IK LB/1K LB/1K LH/HR
LB FUCL LO FUEL LB FUEL Lfl FUEL
0.63 3199.80 8.27 8.90 6.19
0.59 1200. 4H 9.98 10.57 5.20
0.53 320C.90 12.36 12. H9 4.16
0.20 3121.69 2.18 2.37 34.71
0.34 3149.96 2.18 2.52 30.16
0.17 3161.07 ?.70 2.87 27.59
0.33 3168.59 3.00 3.33 25.28
0.35 31B2.32 3.29 3.64 17.42
0.63 3193.99 4.43 5.06 11.61
0.71 3197.75 6.14 6.86 8.68
CO THC NO
2
HC
LB/HR
0.24
0.0
0.0
7.25
6.50
4.94
4.1 1
3.60
1.62
0.80
NO
2
LB/1KHTH-HR LB/1MIH-HH LB/1KHTH-HR LB/IKHIH-HR
1822.199 0.025 4.709
1842.3(1 0.0 5.744
1903.638 0.0 7.371
3299.053 8.236 2.299
3149.962 5.155 2.184
2950.333 3.292 2.518
2772.520 2.336 2.672
2036.684 1.199 2.107
1870.584 0.323 2.595
1822.717 0.114 3.501
0.357
0.33B
0.318
0.709
0.336
0.157
0.291
0.222
0.371
0.407
NO? C02 Nt)
LB/HR Li/HR LR/HR
3.39 17310.81 44.73
3.B9 21187.15 66.06
4.27 25671. IB 99.14
0.18 2903.17 2.07
0.42 3968.95 2.75
0.24 4425.50 3.7B
0.51 4879.61 4.61
0.67 6110.05 6.37
1.86 9390.33 13.03
2.85 12759.02 24.51
NU
X
LB/lPt«TH-MR
5.066
6.082
f.689
2.508
2.520
2.675
2.913
2.329
2.966
3.909
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/HR
4B.I?
69.94
103.41
2.21
3. 18
4.01
5.13
6.99
14.89
27.36
IV-204
-------
CM. to NUMBER: 332 ENGINE TYPE »NO NODEL: jTBD-9
TEST ORGANIZATION: $ H R I TWA
SERIAL NUNBERl P665704B
NODE
TAXI-IOLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POKER
t TH
870.
14500.
12325.
5800.
870.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
41.007 1011.247
5.372 8804.355
5.957 7284.480
11.322 3487.744
41.007 1011.297
MT
TOTAL FOR CTCLEI
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
NODE
TAXI-IOLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
POKER
TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
8.470 1011.297
0.0 8804.355
0.148 7284.480
1.597 3487.744
8.470 1011.297
NT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS PQLLUTANT/IOOOK
MODE
TAXI-IOLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
POKER
TH
870.
14500.
12)25.
5800.
870.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
2.299 1011.297
123.869 8804.355
83.491 7284.480
20.300 3487.744
2.299 1011.297
KT
TOTAL FOR CYCLEl
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
USAGE TINE IN
FACTOR NODE
NIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLEl
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR NODE
NIN.
1. 000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.Q.l
USAGE TINE IN
FACTOR MODE
HIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CVCLE:
LB TH AT T.O.:
CO
NASS
LBS.
12.985
0.063
0.218
0.755
4.784
18.805
18.072
13.580
0.432
HC
MASS
LBS.
2.682
0.0
0.005
0.106
0.488
3.782
3.635
2.7)1
0.0
NOK
NASS
LBS.
0.728
1.445
3.061
1.353
0.268
6.856
6.589
4.951
99.665
FUEL
NASS
LBS.
320.24
102.72
267.10
232.52
117.48
1040.56
FUEL
NASS
LBS.
320.24
102.72
267.10
232.52
117.98
1040.36
FUEL
NASS
LBS.
320.24
102.72
267.10
232.52
117.48
1040.56
LB CO /
IK LB FUEL
40.549
0.610
0.818
3.246
40.544
LB HC /
IK IB FUEL
8.376
0.0
0.020
0.458
8.376
IB NOI/
IK LB FUEL
2.273
14.069
11.461
5.821
2.273
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
TH-HR
0.04713
0.00037
0.00048
0.00195
0.0471)
IB HC /
1 TM-HR
0.00974
0.0
0.00001
0.00028
0.00974
LB NOX/
1 TH-HR
0.00264
0.00854
0.00677
0.00350
0.00264
IV-205
-------
0«TEl T/12/T1
TEST ORGANIZATION: U.S. BUREAU OF MINES
ENGINE SUPPLIER: AMFRICAN AIRLINES
ENGINE DATA
CAL 10 NUMBER: 89
FNGINE TYPE AND MOREL: JTBD-1
SERIAL NUMBER! 653301
RATED THRUST: 1*000.
ENGINE TOTAL TIME: 11982. HRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL:
N2 COMPRESSOR OVERHAUL:
COMBUSTOR CAN REPLACEMENT:
FIRST STAGE NOZZLE GUIDE VANF OVERHAUL:
NI TURBINE OVERHAUL:
N2 TURBINE OVERHAUL:
FUEL H/C RATIO! 1.920
0. HRS
0. HRS
0. HRS
0. HRS
0. HRS
0. HRS
FUEL! JET - A
OPERATIONAL DATA «»«««««««««»»
INLET AIR TEMPERATURE, DEGREES F: START 95.00 FINISH 96.00
ATMOSPHERIC PRESSURE: START 14.35 FINISH 14.35
INLET AIR HUMIOITY, LBS H2D/LB AIR: 0.0150
RELATIVE HUMIOITY: 42.00 PERCENT
SAMPLE LINE: TFMPERATURE, DEGREES C: 122.00, FLOW RATF, LITERS/MIN:
SAMPLE LINE TRANSPORT TIMF, SEC: -0.00
NUMBER OF TESTS: 6
COMMENTS:
H/C IS CAL-ESTIMATED
TEMP. SAMPLE LINE AVERAGED
A NON-SMOKELESS HOI SECTION
INSTALLED DURING THIS SHOP VISIT
TOP ARM OF PROBE FAILFD DURING LAST RUN
WITHOUT RETROFIT
16.00
LOCK
TIME
TEST
MODE
POWFR
THRUST, LBS PERCENT
UR RATED
SHP
145.00
400.00
405.00
415.00
420.00
425.00
I/ 0
I/ 1
5/ I
4/ 5
3/ 4
2/ 3
790
870
8760
10340
11330
12150
.00
.00
.00
.00
.00
.00
T.O.
5
6
62
71
80
BIS
FNGINE
SPEED
RPM
NI
2745.00
2834.00
7200.00
7596.00
7805.00
8005.00
N?
6935.00
7052.00
11079.00
11310.00
11510.00
11654.00
MEASURED
FUEL
FLOW
LB/HR
1135.00
1065.00
5290.00
6260.00
6P60.00
7440.00
GAS T.EN
AIR FLOW
LB/SEC
-0.00
-o.on
-0.00
-0.00
-o.oo
-0.00
CAU COMPRESSOR FNGINE
F/A DISCHARGE PRESSURE
TFMP RATIO
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
DEGREES F FPR
-0.00
-0.00
-0.00
0.00
-0.00
-o.oo
.04
.04
.5B
.72
.81
.87
TURBINE
INLET
TFMP
DEGREES F
14.33
14.33
14.20
14.18
14.17
14.16
POWER
PERCENT
RATED
T.O.
5
6
62
73
80
EXHAUST
GAS
TEMP
DEGREES F
730.00
700.00
B70.00
915.00
970.00
1000.00
F XHAUSI
GAS
PRFSSURE
PS I A
14.90
14.90
77.55
24.35
25.65
26.55
CO CO
(WFTI 2
PPMV (WET)
PERCENT V
105.00
109.00
25.50
27.70
26.20
27.20
0.49
0.49
1.77
2.07
2.12
2.22
THC
IMtT)
PPMV
45.40
47.50
3.50
3.00
2.60
3.00
NO NO
IWETI 2
PPMV IWFTI
PPMV
6.50
4.90
43.50
32.90
37.80
41.00
3.00
3.00
10.00
15.00
17.00
27.00
NO
X
IriFT)
PPMV
9.50
7.90
53.50
47.90
54.80
68.00
ALOEHVOES SMOKE PARTICULATES
-0.00
3.30
0.25
0.26
0.12
0.07
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-O.DO
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
5
6
62
71
80
86
MASS FMI
cn
LB/IK
LR FUEL
41.76
43.30
2.B9
2.64
2.48
2.46
M4SS EMI
HC
LB/IK
LB FUEL
10.14
10.81
0.23
0. 17
0.14
0.16
MASS EMI
N02
LB/IK
LR FUEL
1.96
1.96
1.B6
2.39
2.6
-------
CM. 10 NUMBER: 69 ENGINE TYPE »ND MOOED
TEST ORGANIZATION! U.S. BUREAU OF MINES
SERIAL NUNBERl 653301
NODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAX-IDLE
0.060
1.000
0.850
0.400
0.060
POKER
TH
840.
14000.
11900.
5600.
840.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
42.445 1111.696
13.636 8566.836
14.401 T253.754
22.901 3601.282
42.445 1111.696
USAGE TIME IN
KT FACTOR NODE
MIN.
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POKER
i TH
840.
14000.
11900.
5600.
840.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
11.848 1111.696
0.441 8566.836
0.604 T253.754
2.085 3601.282
11.848 1111.696
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLEl
L8 TH AT T.O.I
USAGE TIME IN
NT FACTOR MODE
MIN.
TOTAL FOR CYCLEl
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK IB
LBS POLLUTANT/ IOOOK
MODE
TAXI- IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
POKER
TH
840.
14000.
11900.
S600.
840.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
5.527 1111.696
124.353 8566.836
68.880 7253.754
24.304 3601.282
5.527 1111.696
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CVCLEt
TH-HR/CYCLEl
LB TH AT T.O.I
USAGE TIME IN
MT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IOOOK
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLEl
TH-HR/CYCLEl
LB TH AT T.O.:
CO
MASS
LBS.
13.441
0.159
0.528
1.527
4.952
20.607
18.945
15.413
1.136
HC
MASS
LBS.
3.752
0.005
0.022
0.139
1.382
5.301
4.873
3.965
0.368
NOX
MASS
LBS.
1.790
1.451
2.526
1.620
0.645
7.992
7.347
5.977
103.627
FUEL
MASS
LBS.
352.04
99.95
265.97
240.09
129.70
1087.74
FUEL
MASS
LBS.
352.04
99.95
265.97
240.09
129.70
1087.74
FUEL
MASS
LBS.
352.04
99.95
265.97
240.09
129.70
1087.74
LB CO /
IK LB FUEL
38.180
1.592
1.985
6.359
36.180
LB HC /
IK LB FUEL
10.658
0.052
0.083
0.579
10.658
LB NOX/
IK LB FUEL
4.972
14.516
9.496
6.749
4.972
ENERGY
t TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
1 TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
LB CO /
f TH-HR
0.05053
0.00097
0.00121
0.00409
0.05053
L8 HC /
TH-HR
0.01411
0.00003
0.00005
0.00037
0.01411
LB NOX/
1 TH-HR
0.00658
0.00889
0.00579
0.00434
0.00658
IV-207
-------
OATEl 7/26/71
TEST ORGANIZATION! U.S. BUREAU OF MINES
ENGINE SUPPLIER) AMERICAN AIRLINES
ENGINE DATA
CAL ID NUMBER: 344
ENGINE TYPE AND MDDELt JT8D-1
SERIAL NUMBER! 65330*
RATED THRUST! 14000.
ENGINE TOTAL TIME: 13257. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCF.:
NI COMPRESSOR OVERHAUL: 6390. HRS
Hi COMPRESSOR OVERHAUL: 6390. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: o. HRS
FUEL: JET - A FUEL H/C RATIO: 1.970
OPERATIONAL DATA ..............................................
INLET AIR TEMPERATURE, DEGREES F: START SI.00 FINISH
ATMOSPHERIC PRESSURE: START 29.31 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.009*
RELATIVE HUMIDITY: 6i.oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 131.00, FLOW RATE, LITFRS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.99
NUMBER OF TESTS: 5
COMMENTS:
H/C CAL ESTIMATED
SAMPLE LINE TFMP. AVERAGED
WITHOUT RETROFIT
-0.00
29.31
16.00
LOCK
TIME
MO. 00
415.00
".20.00
425.00
430.00
TEST
MODE
2/
I/
3/
4/
5/
0
2
I
1
4
POWER
THRUST, IBS PERCENT
OR RATED
SHP
9150.00
990.00
10800.00
11960.00
12570.00
T.O.
65
7
77
65
89
ENGINE
SPEED
RPM
Nl
7190.00
2120.00
7580.00
7860.00
6010.00
N2
10680.00
7170.00
11200.00
11400.00
11520.00
MEASURED
FUFL
FLOW
LB/HR
5460.00
1075.00
6360.00
7120.00
7610.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
CALC COMPRESSOR
F/A DISCHARGE
TEMP
-0.010000
-0.000000
-0.000000
-0.000000
-0.000000
DEGREES F
-0.00
-0.00
-0.00
-0.00
-o.no
ENGINE
PRESSURE
RATIO
EPR
1.60
1.04
1.64
1.85
1.92
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
r.o.
65
7
77
85
EXHAUSI
GAS
TFMP
DEGREES F
875.00
655.00
940.00
970.00
995.00
EXHAUST
GAS
PRESSURE
PS1A
22.71
14.97
24.24
26.36
27.20
CO
IWETI
PPCV
19.50
107.00
16.00
15.50
15.00
CO
2
IWETI
PFRCFNT
1.98
0.65
2.26
2.46
2.59
THC
(WETI
PPMV
2.20
5i.no
1.90
1.90
1.90
NO NO
IkET) 2
PPMV (WETI
PPMV
ALDEHYDES SMOKE PARTICIPATES
60.80
2.40
95.00
105.40
lift.50
6. CO
2.00
9.50
9.50
10.00
(WET)
PPMV
66.80
4.40
93.50
114.90
128.50
0.33
4.10
0.35
0.32
0.41
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
65
7
77
85
89
MASS EMI
CO
Lfl/lK
LB FUEL
1.98
32. ?B
1 .42
1 .26
1.16
MASS EM
HC
LH/IK
LH FUEL
0. 13
8.95
0.10
0.09
0.08
MASS FMI
ND2
L9/1K
Lfl FUEL
I. 00
0.99
1.24
1.27
1.27
MASS EMI
CD2
LB/IK
LB FUFL
3152.44
1080.63
3153.39
3153.66
3153.83
MASS EMI
NO
LB/IK
LB FUEL
10.12
1.19
12.40
14.11
15. C8
MASS EMI
NOX
L8/1K
IB FUEL
11.12
2.18
13.64
15.40
16.36
I-ASS EMI
CO
LH/HR
10.79
54.70
9.04
9.00
8.85
MASS EM!
HC
LB/HR
0.70
9.62
0.61
0.63
0.64
MASS EMI
NO 2
LB/HR
MASS EMI
C02
LB/HR
MASS EMI
NO
LB/HR
MASS EMI
NOX
LB/HR
5.45
1.07
7.89
9.06
9.69
17212.30
3311.67
20055.56
22454.04
24000.65
55.25
1.28
78.85
100.57
114.80
60.71
2.34
86.74
109.64
124.48
POWER
PERCENT
RATED
T.O.
65
7
77
65
89
CO
LH/IKITH-HR
1.179
35.146
O.r)37
0. (53
0.704
1831.126
3345.124
IB55.997
1877.426
1909.360
IHC
LB/IK«TH-HR
0.076
9.717
0.057
0.053
0.051
NO
LO/1 KITH-HP
6.C39
1.291
7.301
8.400
9.13?
IB/1K«TH-MR
0.596
1.076
0.730
0.75B
0.771
LB/IKfTH-HR
6.635
2.367
8.031
9.167
9.903
IV-208
-------
C»L ID NUMBERl 344 ENGINE TYPE AND NODELI JT60-I
TEST ORGANIZATION! U.S. BUREAU OF DINES
SERIAL NUMBERl 65330*
MODE
TAXI-IOLE
TAKEOFF
CL1MBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.060
1.000
O.B30
0.400
0.060
POKER
TH
840.
14000.
11900.
9600.
840.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR L8/HR
31.112 951.672
6.531 8423.043
7.572 T216.984
22.534 3874.643
31.312 951. 672
USAGE TINE IN
HT FACTOR MODE
MIN.
TOTAL FOR CYCLE I
IBS POLLUTANT/ IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
BODE
TAXI-IDLE
TAKEOFF
CLIH80UI
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POKER
TH
840.
14000.
11900.
S600.
840.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
B.741 951.672
0.138 B421.043
0.299 7216.984
2.229 3874.643
8.741 951.672
HT
TOTAL FOR CYCLEl
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
MODE
TAXI-IDLE
TAKEOFF
CLIKBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
POKER
* TH
840.
14000.
11900.
5600.
840.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.837 951.672
156.399 8423.043
110.335 7216.984
30.704 3874.643
1.837 951.672
HT
TOTAL FOR CYCLEl
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE'
TH-HR/CYCLE:
LB TH AT T.O.t
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE I
TH-HR/CYCLE:
LB TH AT T.O.I
USAGE TIME IN
FACTOR MODE
NIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCIE:
LB TH AT T.O.I
CO
MASS
LBS.
9.916
0.076
0.278
1.502
3.653
15.425
14.924
11.537
0.544
HC
MASS
LBS.
2.768
0.002
0.011
0.149
1.020
3.949
3.821
2.954
0.115
NOX
MASS
LBS.
0.582
1.825
4.046
2.047
0.214
8.713
8.430
6.517
130.332
FUEL
MASS
LBS.
301.36
98.27
264.62
258.31
111.03
1033.59
FUEL
MASS
LBS.
301.36
98.27
264.62
258.31
111.03
1013.59
FUEL
MASS
LBS.
301.36
98.27
264.62
258.11
111.03
1033.59
LB CO /
IK LB FUEL
32.901
0.775
1.049
5.816
12.901
LB HC /
IK LB FUEL
9.185
0.016
0.041
0.975
9.185
LB NOX/
IK LB FUEL
1.930
18.568
19.288
7.924
1.910
ENERGY
TH-HR
266.00
161.33
416.13
371.11
98.00
1117.00
ENERGY
f TH-HR
266.00
161.33
436.11
171.11
98.00
1137.00
ENERGY
1 TH-HR
266.00
163.13
436.33
173.33
98.00
1337.00
LB CO /
f TH-HR
0.01728
0.00047
0.00064
0.00402
0.01728
LB HC /
TH-HR
0.01041
0.00001
0.00003
0.00040
0.01041
LB NOX/
f TH-HR
0.00219
0.01117
0.00927
0.00548
0.00219
IV-209
-------
OATE1 T/19/71
TEST ORGANIZATION: U.S. BUREAU OF MINES
ENGINE SUPPLIER: ANFRICAN AIRLINES
ENGINE nATA
CAL 10 NUMBER: 295
ENGINE TYPE AND MODEL: JTBD-.l
SERIAL NUMBER: 6*9131
RATED THRUST: 14000.
ENGINE TOTAL TIME: 144*3. MRS
TIME SINCE HOT SECTIQN OVERHAUL: 3948. MRS
TIKE SINCE:
NI COMPRESSOR OVERHAUL: 5M?. MRS
N2 COMPRESSOR OVERHAUL: 5712. HRS
COMBUSTOR CAN REPLACEMENT: 3148. HRS
FIRST STAGE NOZiLE GUIDE VANE OVERHAUL: 3948. HRS
NI TURBINE OVERHAUL: 3948. HRS
N2 TURBIMF OVERHAUL: 3948. HRS
FUEL: JET - A FUEL H/C RATIO: 1.920
OPERATIONAL DATA «««««««««««»«»«
INLET AIR TF.MPERATURF, UEGREES f : SIARt Td.OO FINISH
ATMOSPHERIC PRESSURE: START 29.35 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR; o.oioo
RELATIVE HUMiniTY: 51.00 PEP.CFNT
SAMPLE LINE: TEMPERATURE, DEGREES C: 101.00, FLOW DATE, LITERS/MINI
SAMPLE LINE TRANSPORT TIME, SEC: 0.99
NUMBER OF TESTS: 6
COMMENTS:
H/C IS CAL TEMP. AVERAGHl
3-ARM PROBE USED
WITHOUT RETROFIT
78.00
29.35
16.00
LOCK
TIME
215.00
220. flO
225.00
730.00
215.00
235.00
TfST
MonE
4/ 0
I/ 4
2/ 1
V 2
5/ 3
4/ 5
POWER
THRUST, LBS PFPf.tNT
OR RATEO
SHP
1000.00
10060.00
12050.00
12790.00
9410.00
1030.00
r.u.
7
78
86
91
67
7
ENMNE
SPEEO
"*PM
Ml
23*5.00
7539.00
7786.00
7970. OC
7205.00
2120.00
N2
7089.00
11248.00
11449.00
1 1580.00
11040.00
7198.00
MEASURER
FUFL
FLOW
L8/HR
990.00
6260. 00
6950.00
7410.00
5310.00
980.00
GAS GEN
AIR FLOW
L9/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CALC COMPRESSOR ENGINE
F/A DISCHARGE PRESSURE
TEMP RATIO
-0.
-0.
-0.
-0.
-1.
-0.
000000
000000
000000
000000
000000
000000
DEGREES F EPR
-n.oo 1.04
-o.oo
-0.00
-0.00
-0.00
-0.00
.79
.86
.93
.63
.04
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER EXHAUST
PERCENT GAS
RATED TEMP
T.O. OEGRfES t
7
78
86
91
67
7
690.00
940.00
975.00
1005.10
875.00
700.00
EXHAUST
GAS
PRESSURE
PSI A
14.99
25.10
26.35
27.15
21. 17
14.99
cu
I JEM
PPMV
183.00
29.20
26.80
27.20
32.10
153.00
CO
f
C»f Tl
PFRCFNt V
0. 71
2.02
2.16
2.26
1.70
0.60
THC
IWFTI
PPMV
67.50
3.20
2.60
2.20
2.2P
64.80
NO
IWETI
PPMV
1 .60
58.90
72.70
81.90
42.90
1.90
N'J
2
(WET)
PPMV
5.50
15.00
15.00
24.00
IB. 00
6.00
NO
X
l.tTI
PPMV
7.10
71.90
87.70
105.90
60.90
9.90
ALDFHYOES
5.28
0.25
0.24
0.14
0.1 r
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-O.OC
-0.10
-0.00
POWER
PERCENT
RATED
T.O.
7
78
86
91
67
7
MASS EMI
C'l
1 B/1K
L8 FUFl
49.87
2.90
2.49
2.41
3. HI
49.42
MASS EMI
HC
LB/1K
LB FUFL
13.66
0.18
0. 14
0.11
0.15
1 1.99
MASS FMI
Ntl?
LB/1K
LO FUEL
2.46
2.45
2.29
1.50
3.49
1.18
MASS FMI
C02
LI/IK
LH FUFl.
3040.07
3150.64
3151.60
3151. /9
1149. 5C
3041.14
V.ASS F.MI
NO
L8/U
LB FUEL
0.7J
9.60
11.09
11.94
8.31
2.07
MASS FMI
NCX
LP/IK
LB FUEL
3.18
12. 05
13.38
15.44
1 1.79
5.25
MASS F-l
CO
LP/HR
49.37
18.15
1 7.10
1 7.09
2C.22
48. 44
MASS FMI
HC
LB/HR
13. 52
1.14
C.96
0.83
0.79
1 1.75
MASS EMI
NCI?
1. 8/HR
2.44
15.31
15.90
25.93
18.51
3.12
MASS EMI
C02
L8/HR
3009.66
19724.21
21903.62
23154.75
16723.84
2984.44
MASS EMI
ND
LO/HR
0.71
60.12
77.07
88.48
44.12
2.03
MASS [M
NOX
LB/HR
3.15
75.44
92.97
114.41
62.63
5.15
POWER
PFRCFNT
OAT60
T.O.
7
78
86
91
67
7
49. 3 71
1.656
1.415
1.199
2. 149
47.025
3009.665
I 799.656
1BI7.728
1826.016
1777.241
2817.51 I
13.520
0. 104
0.080
0.065
0.084
U.4T7
8/ IK HTH-Hlt
0.70T
5.4P6
6.396
6.918
4.689
1.969
LIW IK-TH-HR
2.437
1.397
1.320
2.027
1 .967
3.029
NO
X
LB/IK1 TH-HR
3.146
6.881
7.715
8.945
6.656
4.998
IV-210
-------
C»L ID NUNBERl 293 ENGINE TYPE »NO NODELI JT80-1
TEST ORGANIZATION: U.S. BUREAU OF NINES
SERIAL NUNBERl 6*9131
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLINSOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
TH
8*0.0
1*000.0
11900.0
5600.0
8*0.0
POKER
TH
8*0.0
14000.0
11900.0
S600.0
840.0
POWER
TH
840.0
14000.0
11900.0
5600.0
840. 0
EMISSION FUEL USAGE TINE IN
RATE RATE WT FACTOR NODE
LB/HR LB/HR NIN. .
41.611 836.814 .000 19.00
15.490 82T8.098 .000 O.TO
18.171 6954.324 .000 2.20
34.553 3309.290 .000 4.00
41.611 836.814 .000 7.00
TOTAL FOR CYCLE)
LBS POLLUTANT/IK IB FUEL/CVCLEl
LBS POLLUTANT/IK LB TH-HR/CYCLEl
LBS POLLUTANT /1000K LB TH AT T.O.I
EMISSION FUEL USAGE TINE IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR H1N.
11.577 836.814 1.000 19.00
0.234 8278.098 1.000 0.70
0.381 6954.324 1.000 2.20
2.879 3309.290 1.000 4.00
11.577 836.814 1.000 7.00
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB FUEL/CYCLEl
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.I
ENISSION FUEL USAGE TINE IN
RATE RATE NT FACTOR NODE
LB/HR LB/HR NIN.
2.576 836.814 .000 19.00
155.711 6278.098 .000 0.70
93.248 6954.324 .000 2.20
26.997 3309.290 .000 4.00
2.576 836.814 .000 7.00
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB FUEL/CVCLEi
LBS POLLUTANT/IK LB TH-HR/CYCLEt
LBS POLLUTANT/1000K LB TH AT T.O.I
CO
NASS
LBS.
13.177
0.181
0.666
2.304
4.855
21.182
22.659
15.843
1.291
HC
NASS
LBS.
3.666
0.003
0.014
0.192
1.351
5.225
5.590
3.908
0.195
NOX
NASS
LBS.
0.816
1.817
3.419
1.800
0.301
8.152
8.721
6.097
129.776
FUEL
NASS
LBS.
264.99
96. 5 8
254.99
220.62
97.63
934.81
FUEL
MASS
IBS.
264.99
96.58
254.99
220.62
97.61
934.81
FUEL
NASS
LBS.
264.99
96.58
234.99
220.62
97.63
934.81
LB CO /
IK LB FUEL
49.725
1.871
2.613
10.441
49.723
LB HC /
IK LB FUEL
13.835
0.028
0.055
0.870
13.835
LB NOX/
IK LB FUEL
3.079
18.812
13.409
8.158
3.079
ENERGY
TH-MR
266.00
163.31
436.3]
373.33
98.00
1317.00
ENERGY
TH-HR
266.00
161.33
436.33
371.11
98.00
1117.00
ENERGY
1 TH-HR
266.00
161.33
436.33
371.33
98.00
1337.00
LB CO /
TH-HR
0.04954
0.00111
0.00153
0.00617
0.04954
LB HC /
TH-HR
0.01378
0.00002
0.00003
0.00051
0.01178
LB NOX/
1 TH-HR
0.00107
0.01112
0.00784
0.00482
0.00107
IV-211
-------
OUf.1 6/29/71
TEST ORGANIZATION: UN ITto/EPA
ENGINE SUPPLIED: UNITED AIRLINES
ENGINE DATA
CAL ID NUMBER: 122
ENCINF TYPE AND MODEL: JTBD-7
SERIAL NUMRERl
RATED THRUST: 1*000.
ENGINE TOTAL TIME: 9768. MRS
TINE SINCE HOT SECTION OVERHAUL: 0. HRS
TINE SINCE:
NI COMPRESSOR OVERHAUL: 11173. HRS
N2 COMPRESSOR OVERHAUL: 1157*. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANF OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINF OVERHAUL: o. MRS
fUEL: JET - « FUEL H/C RATIO: 1.920
OPERATIONAL DATA ««««««»»» .«.......»...,.....(........
INLET AIR TEMPERATURE. DEGREES f : START 56.30 FINISH
ATMOSPHERIC PRESSURE: START it.95 FINISH
INLFT AIR HUMIDITY, LRS H20/LB AIR: 0.0066
RELATIVE HUMIDITY: 69.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 160.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SFC: 5.00
NUMBER OF TESTS: 4
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES HG
55.40
30.00
CLOCK
TIME
TEST
MOOF
POWER
THRUST, LBS PERCENT
UK RATED
SMP
2355.00
5.00
10.00
235.00
I/
21
M
4/
0
1
2
3
1 1050
12100
13700
1100
.00
.00
.00
.00
T.O.
78
86
97
7
ENGINE
SPEED
RPM
NI
7300.00
7617.00
8010.00
2960.00
N2
10927
11121
11387
11300
.00
.00
.00
.00
MEASURFO
FUEL
FLHW
GAS GEN
AIR FLOW
LB/SEC
LB/HR
6291
6S66
8083
593
.00
.00
.00
.00
-0.00
-0.00
-0.00
-0.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
COMPRESSOR
DISCHARGE
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
ENGINF
PRESSURE
RATIO
EPR
1.75
l.B*
1.98
-0.00
TURBINE
INLFT
TFMP
DEGREES F
-0.00
-0.00
-o.oo
-0.00
POWER
PERCENT
RATED
T.O.
78
86
97
7
EXHAUST
GAS
TEMP
OFGRFES F
178.00
914.00
978.80
665.60
EXHAUST
GAS
PRESSURE
PSIA
52.50
55. 10
59.30
31.80
cn
IWETI
PPMV
95.00
95.00
95.00
131.00
CO
2
IUETI
PFRCFNT V
1.70
2.50
2.78
0.47
THC
(WET)
PPMV
5.40
4.50
4.20
16.50
NO
I MET I
PPMV
53.80
120.00
152.50
1.25
NO
2
IUETI
PPMV
-0.00
-0.00
-0.00
-0.00
ALDEHYDES SMOKE PARTICULATES
(MET)
PPMV
55.00
121.00
155.00
4.50
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
PtlWfO
PFRCENT
RATED
T.O.
78
86
97
MASS EMI
r.o
LB/1K
LB FI1FI
11.16
7.60
6.R4
55.09
MASS EMI
HC
LR/U
LB FUEL
0.36
0.21
0.17
3.91
MASS FM1
"02
LB/IK
LB FUEL
-0.00
-o.on
-0.00
-0.00
MASS EMI
C02
LB/IK
LB FUEL
3137.36
3143.38
3144.67
3058. 6C
MASS EMI
NO
LB/IK
LB FUFL
10.38
15.77
18.03
0.85
MASS ENI
N'OX
LB/IK
LB FUEL
10. M
15.90
18.3)
3.06
MASS EMI
CU
LR/HB
70.20
52.96
55. ?B
32.67
MASS EMI
HC
LB/HR
2.29
1.44
1.40
2.37
MASS EMI
N02
LB/HR
MASS EMI
C02
LB/HR
MASS EMI
ND
LB/MP
MASS EMI
NOX
Lfl/HB
-0.00
-0.00
-0.00
-0.00
19737.14
21896.78
25418.35
1813.75
65.30
109.88
145.77
0.50
66.75
110.79
148.15
1.82
POME"
PERCENT
RATED
T.O.
78
86
97
«..353
4.377
4.035
29.696
LO/1KHTH-HR
1716.166
1809.651
1*55.354
1648.864
IHC
LB/IKHTH-MP
0.207
0. 11"
0.102
2.110
no
LB/1MTH-HR
5.909
9.OBI
10.640
0.45R
LB/IKHTH-HR
-0.000
-0.000
-C.OOO
-o.ooo
NO
X
LB/IMTH-HR
6.041
9.156
10.814
1.650
IV-212
-------
CAL ID NUMBERi 122 ENGINE TYPE AND MODEL) JT80-7
TEST ORGANIZATION: UNITED/EPA
SERUL NUMBER! 69*623
NODE FRACTIONAL
POKER
TAKI-IOLE 0.060
TAKEOFF 1.000
CLINaOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.060
MODE FRACTIONAL
POKER
TAXI-IDLE 0.060
TAKEOFF 1.000
CLIHBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.060
NODE FRACTIONAL
POKER
TAXI-IDLE 0.060
TAKEOFF 1.000
CLIHBOUT 0.950
APPROACH 0.400
TAXI-IDLE 0.060
POKER
1 TH
B40.0
14000.0
11100.0
5600.0
B40.0
POKER
TH
B40.0
14000.0
11900.0
9600.0
840.0
POKER
TH
840.0
14000.0
11900.0
9600.0
840.0
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR NODE
LB/HR LB/HR MIN.
28.028 473.920 .000 19.00
91.908 81)7.016 .000 0.70
90.916 6893. 90B .000 2.20
49.644 3308.871 .000 4.00
28.028 471.420 .000 7.00
TOTAL FOR CTCLEl
LBS POLLUTANT/IK LB FUEL/CYCLE!
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR MODE
LB/HR LB/HR MIN.
2.264 473.920 1.000 19.00
0.888 6137.016 1.000 0.70
1.288 689). SOB 1.000 2.20
1.994 3308.871 1.000 4.00
2.264 473.920 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLEJ
LBS PnilUTANT/lOOOK LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR MODE
LB/HR LB/HR MIN.
1.164 473.920 .000 19.00
193.196 8137.016 .000 0.70
107.178 6893.908 .000 2.20
28.418 330B.871 .000 4.00
1.164 473.920 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000X LB TH AT T.O.:
CO
MASS
LBS.
8.876
0.606
1.892
3.310
3.270
17.913
23.198
13.398
4.326
HC
MASS
LBS.
0.717
0.010
0.047
0.106
0.264
1.149
1.483
0.896
0.740
NOX
MASS
LBS.
0.369
1.787
3.930
1.899
0.136
8.116
10.910
6.070
127.630
FUEL
MASS
LBS.
190.07
94.93
291.30
220.99
99.29
772.18
FUEL
MASS
LBS.
190.07
94.93
251.30
220.99
95.29
772.18
FUEL
MASS
LBS.
150.07
94.93
291.30
220.59
55.29
772.18
LB CO /
IK LB FUEL
99.142
6.379
7.371
15.003
99.142
LB HC /
IK LB FUEL
4.778
0.109
0.188
0.482
4.778
LB NOX/
IK LB FUEL
2.497
18.622
19.638
8.589
2.457
ENERGY
TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
LB CO /
TH-HR
0.03337
0.00371
0.00425
0.00886
0.03337
LB KC /
TH-HR
0.00270
0.00006
0.00011
0.00028
0.00270
LB NOX/
* TH-HR
0.00139
0.01094
0.00901
0.00507
0.00139
IV-213
-------
OATEI T/ 2/71
TEST ORGANIZATION! UNITED/EPA
ENGINE SUPPLIER! UNITED AIRLINES
ENGINE 0>T*
C»L ID NUMBER: 127
ENGINE TYPE AND MODEL: JTBD-7
SERIAL NUHBEIU
RATFD THRUST! 14000.
ENGINE TOTAL TIME: 3779. MRS
TINE SINCE HOT SECTION OVERHAUL: 3355. HRS
TINE SINCE:
NI COMPRESSOR OVERHAUL: 1077. MRS
N2 COMPRESSOR OVERHAUL: 2832. MRS
CONBUSTOK CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 3355. HRS
NI TURBINF OVERHAUL: 3224. HRS
N2 TURRINE OVERHAUL I 0. HRS
FUEL: JET - A FUEL H/C RATIO: 1.920
OPERATIONAL OAIA «*««««4...««.4««««««.«.«..««.
INLET AIR TEMPERATURE, DEGREES F: START 54.86 FINISH
ATMOSPHERIC PRESSURE: START 2<>.<»i FINISH
INLET AIR HUMIOITr, LRS H20/LB AIR: 0.0060
RELATIVE HUMIDITY: 65.no PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 160.00, FLOW RATE, LITFRS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 5.00
NUMBFR OF TESTS: 4
COMMFNTS:
EXHAUST GAS PRESSURE IN INCHES HG.
54.14
29.97
LOCK
TIME
TEST
MODE
POWER
THBUST.LBS PFRCFNT
OR RATED
SHP
28.00
32.00
36.00
150.00
I/
7/
3/
4/
0
1
2
1
10074
I217B
134J9
935
.00
.00
.00
.00
r.o.
78
66
95
6
ENGINE
SPEED
RPM
NI
7356.00
7633.00
7940.00
2831.00
N2
10875
11076
11269
6939
.00
.00
.00
.no
MEASURED
FUEL
FLOW
GAS GFN
MK FLOW
LB/SEC
LB/HR
6293
7059
7934
1073
.00
.00
.00
.00
-O.on
-0.00
-0.00
-0.00
C«LC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.75
1.85
1.96
-0.00
TURRINF
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POWFR
PERCENT
RATED
T.O.
78
EXHAUST
GAS
TEMP
DEGREES r
8K7.00
9?4.80
96H.OO
649.40
fXHAUST
GAS
PRESSURE
PSIA
57.20
55.30
56.50
31.40
CM
(MET)
PPHV
75.00
20.00
20.10
90.00
CO
2
(MET)
PERCENT
2.14
2.75
2.45
0.48
THC
(WET)
PPMV
1.20
0.75
0.30
47.00
NO
IWET)
PPMV
8.60
103.00
125.00
4.00
NO
2
(WETI
PPMV
-0.00
-0.00
-0.00
-0.00
NO
X
(MET)
PPMV
91.00
108.00
131.00
4.00
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
78
86
95
6
U»SS EMI NSSS EMI
CO Mr.
LR/1K IR/IK
L3 FUFL LB FUEL
7.34
i.Tn
1.64
36.65
0.06
0.04
0.01
9.80
M451 EMI
N02
FUEL
MASS FMI
C02
LB/IK
LH FUFL
-0.00 3152.03
-0.00 3152.9R
-0.00 3153.2fl
-0.00 3071.42
LB/IK
LR PUFL
1.32
15.09
16.82
2.68
MASS EM|
NOX
LB/IK
LB FUEL
14.01
15.P2
17.63
2.68
MASS EMI
CO
LB/HR
14.75
12.59
13.00
39.33
MASS EMI
HC
LB/HR
MASS EMI
102
LR/HP.
MASS FMI
CO?
LB/HR
MASS EMI
NO
LB/HR
MASS EMI
NOX
LB/HR
0.41 -0.00 19835.73 8.33 88.13
0.27 -0.00 72256.89 106.51 111.68
0.11 -0.00 25018.09 133.44 139.84
10.51 -0.00 3295.64 2.87 2.67
POWER
PERCENT
RATED
T.O.
78
86
95
cn
Lft/ IKiTH-HO
1.344
1.034
0.967
42.062
L8/1K«TH-H«
1807.52C
1827.631
1661.604
1574.74*,
TMC
LB/1KITH-HP
0.037
0.07?
O.OOB
11.747
NO
L3/ I K«TIHH
0.759
B.746
LR/lKtTH-HR
-0.000
-C..OOO
-0.000
-0.000
LB/IK«TH-HR
8.035
9.171
10.406
3.071
IV-214
-------
CAL 10 NUMBER! 127 ENGINE TYPE AND MODEL: JT80-T
TEST ORGANIZATION! UNITEO/EPA
SERIAL NUMBER! 656065
MODE
TAXI-IDLE
TAKEOFf
CLIMBOUT
APPROACH
TAKI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POKER
0.060
1.000
O.B50
0.400
0.060
POWER
TH
B40.0
14000.0
11900.0
5600.0
840.0
POWER
f TH
840.0
14000.0
11900.0
5600.0
840.0
POWER
t TH
840.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
36.131 972.871
9.301 8285.004
11.730 6939.211
26.452 3372.059
36.131 972.871
TOTAL FOR CYCLE!
IBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
L8S POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
8.820 972.871
0.0 8285.004
0.219 6939.211
1.667 3372.059
8.820 972. 871
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POILUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
2.406 972.871
154.669 8285.004
106.596 6939.211
28.600 1372.059
2.406 972.871
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
L8S POLLUTANT/ IK LB
LBS POLLUTANT/ 1000K
USAGE TINE IN
FACTOR MODE
MIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL/CYCLE:
TH-HR/CYCLEI
LB TH AT T.O.I
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE!
TH-HR/CYCLE;
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
11.441
0.109
0.430
1.763
4.215
17.959
18.004
13.432
0.775
HC
MASS
LBS.
2.793
0.0
0.008
0.111
1.029
3.941
1.951
2.948
0.0
KOX
MASS
LBS.
0.762
1.B04
3.909
1.907
0.281
B.662
8.684
6.479
128.891
FUEL
MASS
LBS.
308.08
96.66
254.44
224.80
113.50
997.48
FUEL
MASS
LBS.
308.08
96.66
254.44
224.80
113.50
997.48
FUEL
MASS
LBS.
308.08
96.66
254.44
224.80
113.50
997.48
LB CO /
IK LB FUEL
37.138
1.123
1.690
7.845
37.138
LB HC /
IK LB FUEL
9.066
0.0
0.032
0.494
9.066
LB NOX/
IK LB FUEL
2.473
18.669
15.361
8.481
2.473
ENERGY
TH-HR
266.00
161.31
416.33
373.33
98.00
1317.00
ENERGY
1 TH-HR
266.00
161.31
436.33
371.31
98.00
1117.00
ENERGY
TH-HR
266.00
161.11
436.33
373.33
98.00
1337.00
LB CO /
1 TH-HR
0.04301
0.00066
0.00099
0.00472
0.04301
LB HC /
f TH-HR
0.01050
0.0
0.00002
0.00010
0.01050
L8 NOX/
1 TH-HR
0.00286
0.01105
0.00896
0.00511
0.00286
IV-215
-------
0»TE: 7/26/71
TEST ORGANIZATION: U.S. BUREAU OF MINES
ENGINE SUPPLIER: AMERICAN AIRLINES
ENGINE DATA
CAL ID NUMBER: 145
ENGINE TYPE AND MODEL: JT8D-7
SERIAL NUMBER: 654*62
RATED THRUST: 14000.
ENGINE TOTAL TIME: 9611). MRS
TIME SINCE HOT SECTION OVERHAUL: 4917. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 9646. HRS
N2 COMPRESSOR OVERHAUL: 9698. HRS
COMBUSTOR CAN REPLACEMENT: 3718. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 4917. HRS
Nl TURBINE OVERHAUL: 9696. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL: jp-4 FUEL H/C RATIO: o.o
OPERATIONAL DATA «««
INLET AIR TEMPERATURE, DEGREES F: START 71.00 FINISH
ATMOSPHERIC PRESSURE: START 29.29 FINISH
INLET AIR HUMIDITY, L8S HZO/LB AIR: 0.0144
RELATIVE HUMIDITY: 79.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 136.OC, FLOW RATE, LITERS/UN:
SAMPLE LINE TRANSPORT TIMF, SEC: 0.99
NUMBER OF TESTS: 6
COMMENTS:
H/C CAL ESTIMATED
SAMPLE LINE TEMP. AVERAGED
ENGINE DID NOT LITE OFF ON FIRST TWO ATTEMPTS
THUS A LARGE AMOUNT OF RAM FUELSOAKEO PROBF BEFORE FIRST IDLE MODE
PROBE LOCATED 10" FROM TAILPIPE
FIRST IDLE MODE UNTRIMMFO
WITHOUT RETROFIT
71.00
29.29
16.00
CLOCK
TIME
940.00
955.00
1010.00
1015.00
1020.00
1030.00
TEST
MODE
I/ 0
5/ 1
I/ 5
4/ 1
3/ 4
^l 3
POWFR
THRUST, IBS PEKCFNT
OP RATED
SHP
740.00
9750.00
1000.00
11940.00
12060.00
12960.00
T.O.
5
69
7
7B
86
92
ENGINE
SPEED
RPM
Nl
2580.00
7275.00
2900.00
7530.00
77RO.OO
7990.00
N2
6650.00
11060.00
7150.00
11250.00
11480.00
llf>20.00
MEASURED
FUEL
FLOW
LD/HR
960.00
5740.00
1110.00
6520.00
7230.00
7860.00
GAS GEN
AIR FLOW
LB/SEC
CALC
F/A
COMPRESSOR
DISCHARGE
TFMP
DEGRFFS F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
0.0
0.0
0.0
0.0
0.0
0.0
-0
-0
-0
-0
-0
-0
.00
.00
.00
.00
.00
.00
ENGINE
PRESSURE
RAIIU
EPR
I.C4
1.67
1.04
1.76
1.86
1.94
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
POWER EXHAUST
PERCENT GAS
OATtO TEMP
T.O. DEGREES F
5
61
7
78
86
92
730.00
910.00
710.00
960.00
1000.00
1015.00
EXHAUST
GAS
PRESSURE
PSIA
14. HI
23.49
14.81
24.92
26. 27
27.17
en
(WFT 1
ppyy
5(.10
29.00
31.00
11.20
14.20
16.20
CD
2
IUETI
PERCENT V
D.51
2.02
0.53
2.11
2.54
2.72
THC
IWETI
PPMV
127.40
1.70
67.01
1.50
1.51
1.50
NO
IWETI
PPMV
2.90
47.20
3.90
56.20
67.10
78.50
NU
2
IWETI
PPMV
2.00
24.00
7.00
40.00
51.00
60.00
NO
X
(WET)
PPMV
4.90
71.20
10.90
96.20
116.10
136.50
ALDEHYDES
-0.00
0.34
4.25
0.41
0.56
0.61
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
5
69
7
78
86
92
MASS EMI
CO
LB/IK
LB FUEL
66.12
3.14
55.57
1.15
3. 14
3.10
MASS EMI
HC
LR/IK
LB FUEL
31 .61
0. 11
16.28
0.09
O.OR
0.07
»ms EMI
N02
LH/IK
Lfl FUEL
1.42
4.54
4.«a
6.62
7.6H
8. 44
MASS CMI
CP2
L8/1K
LB FUEL
3471.47
3658. «9
3512.48
3658.95
3659.30
1659.38
MASS EMI
NO
LR/1K
LB FUEL
2. CO
H.94
2.72
9.11
10. 11
11.04
"ASS EMI
NOX
LB/1K
LR FUFL
3.49
13. 4H
7.59
15.93
17.79
19.48
MASS EMI
CO
LB/HR
63.67
19. 19
61 .68
21.82
22.67
24.16
MASS EMI
HC
LB/HR
30.36
0.64
18.07
0.56
0.57
0.56
MASS [Ml
NO 2
LD/HR
1.37
26.09
b.41
43.19
55.51
66.13
MASS EMI
C02
LB/HR
3J34.51
21002.00
1921.05
23656.34
26456.75
28762.69
MASS EKI
NO
Lfl/HR
1.98
51.10
3.02
60.68
73.06
86.78
MASS E"l
NOX
LB/HR
3.35
77.39
8.43
103.86
12ft. 60
153.11
POWER CO
PERCENT
RATED LB/IK»TH-HI>
T.O.
5 86.037
69
7 6
78
66
92
.168
.682
.995
.880
.180
LB/ IMTH-MR
2154.052
3921.048
2190.651
2193.760
P219.143
41.011
0.066
I R.068
0.052
0.0',7
0.045
LB/IKHTH-HR
2.071
5.262
3.016
5.546
6.055
6.696
LB/IKHTH-HR
1.847
2.675
5.414
3.947
4.605
5. 118
NO
X
LB/IKfTH-HR
4.526
7.93J
6.430
9.494
10.66]
11.814
IV-216
-------
CAL ID NUMBER: 3*5 ENGINE TYPE AND MODELi JTBD-T
TEST ORGANIZATION! U.S. BUREAU OF MINES
SERIAL NUNBERl 694462
MODE
TAXI-IDLE
TAKEOFF
ClIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POMER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POMER
0.060
1.000
0.890
0.400
0.060
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
POMER
TH
840.0
14000.0
11900.0
1600.0
840.0
POMER
f TM
840.0
14000.0
11900.0
5600.0
840.0
POWER
f TH
840.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL USAGE TIME IN
RATE RATE XT FACTOR MODE
LB/HR LB/HR MIN.
63.311 10T2.08T 1.000 19.00
24.687 8639.38} 1.000 O.TO
21.938 7313.923 1.000 2.20
40.093 3367. 071 1.000 4.00
63.311 IOT2.087 I. 000 7.00
TOTAL FOR CYCLE I
L9S POLLUTANT/IK LB FUEL/CYCLE!
LBS POLLUTANT/ IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000X LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE NT FACTOR MODE
LB/HR LB/HR MIN.
23.697 1072.087 .000 19.00
0.0 8639.383 .000 0.70
0.0 7313.523 .000 2.20
6.350 3367.071 .000 4.00
23.697 1072.087 .000 7.00
TOTAL FOR CYCLEl
LBS POLLUTANT/IK LB FUEL/CYCLE!
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/IOOOK LB TH AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR MODE
LB/HR LB/HR MIN.
4.032 1072.087 .000 19.00
188.663 8639.383 .000 0.70
128.360 7313.923 .000 2.20
32.695 3367.071 .000 4.00
4.032 1072.087 .000 7.00
TOTAL FOR CYCLEl
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/IOOOK LB TH AT T.O.:
CO
MASS
LBS.
20.048
0.288
0.804
2.673
7.386
31.200
29.490
23.336
2.057
HC
MASS
LBS.
7.304
0.0
0.0
0.423
2.765
10.692
10.106
7.997
0.0
NOX
MASS
LBS.
1.277
2.201
4.707
2.180
0.470
10.834
10.241
8.104
197.219
FUEL
MASS
LBS.
339.49
100.79
268.16
224.47
129.08
1098.00
FUEL
MASS
LBS.
339.49
100.79
268.16
224.47
129.08
1098.00
FUEL
MASS
LBS.
339.49
100.79
268.16
224.47
129.08
1098.00
LB CO /
IK LB FUEL
99.094
2.898
3.000
11.907
54.054
LB HC /
IK LB FUEL
22.104
0.0
0.0
1.886
22.104
LB NOX/
IK LB FUEL
3.761
21.838
17.591
9.710
1.761
ENERGY
TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
t TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
f TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
LB CO /
f TH-HR
0.07937
0.00176
0.00184
0.00716
0.07537
LB HC /
i TH-HR
0.02821
0.0
0.0
0.00113
0.02821
LB NOX/
TH-HR
0.00480
0.01348
0.01079
0.00584
0.00480
IV-217
-------
0»TE> 7/29/71
TEST ORGANIZATION: U.S. 9UREAU OF MINFS
ENGINE SUPPLIER: AMERICAN AIRLINES
FNCINE DATA
CAL 10 NUMBER: 146
ENGINE TYI>E AND MODEL: JT80-7
SERIAL NUMBER:
RATED ThBUST: 14000.
ENGINE TOTAL TIME: i804. MRS
TIME SINCE HOT SECTION OVERHAUL: 2161. HRS
TINF SINCE:
NI COMPRESSOR OVERHAUL: 5604. HRS
N2 COMPRESSOR OVFRHAUL: 5R04. HRS
COMBUSTOR CAN REPLACEMENT: 2161. HRS
FIRST STAGE NOZZLE GUID<= VANF OVERHAUL: 2161. HRS
NI TURBINE OVERHAUL: 5804. HPS
N2 TURBINE OVFRHAUL: 580. HRS
FUEL: JET - A FUEL H/C RATIO: 1.120
OPERATIONAL DATA «*««»»«««»
INLET AIR TEMPERATURF, DEGREES F: START 67.00 FINISH
ATMOSPHERIC PRESSURE: START 29.30 FINISH
INLET AIR HUMIOITV, LBS H20/LB AIR: 0.0110
RELATIVE HUMIDITY: 78.00 PERCENT
SAMPLE LINE: TEMPERATURE, CEGRFES C: 137.CO, FLOW RATE, LITFRS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.19
NUMBER OF TESTS: 4
COMMENTS:
H/C CAL ESTIMATED
SAMPLE LINE TEMP. AVERAGED
PROBE LOCATED 10" FROM T4ILP1PF
WITHOUT RETROFIT
68.00
21.30
CLOCK
TIME
820.00
871.00
815.00
845.00
TEST
MOOE
4/ 0
3/ 4
2/ 3
I/ 2
POWER
THRUST, L8S PERCENT
OR RATED
SHP
10780.00
12060.00
111 50.00
1050.00
T.O.
76
86
91
7
tNGINE
SPEED
RPM
Ml
7410.00
7300.00
8070.00
2950.00
M2
11130.00
11360.00
11540.00
7240.00
MEASURED
FUEL
FLOW
Lfl/HP
62BO.OO
7110.00
7110.00
1040.00
GAS GEN
A IP FLOW
LH/SEC
-0.00
-0.00
-0.00
-0.00
CALC COMPRESSOR
F/A DISCHARGE
TCMP
-0.000000
-0.000000
-0.000000
-0.000000
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
PATIC
EPR
1.75
1.87
1.97
1.04
T UR P. 1 N E
INLET
TEMP
OFGREES F
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
T.O.
76
86
91
7
EXHAUST
GAS
DEGREES f
865.00
910.00
950.00
620.00
EXHAUST
GAS
PSIA
25.01
76.54
27.13
14.18
CO
(»ET)
20.70
16.00
14.00
10'. 00
CC
2
PERCENT V
2.02
7 . L 9
2.44
0.51
THC
IWETI
10.80
6.50
3.10
41.70
NO
(WCI 1
58.00
77.90
90. 60
0. 70
NO
2
PPMV
6.50
a. oo
9.00
5.00
NO
X
OPMV
64.50
80.10
99.60
5.70
SLDFHYOES
-0.10
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
PARTICULI
-0.00
-0.00
-O.CO
-0.00
POWFR MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS twl MASS LXI MASS EMI MASS EMI MASS EMI
PERCENT CO HC N02 C02 N'l MOX r.P HC N02 C02 NO NUX
RATED 1.B/1K LB/IK IV1K LH./1K LB/IK I.P/IK LR/H" LB/HP LB/HR LVHR LB/HK LB/HR
T.O. LB FUEL Lfl FUEL LO FUFL LB FUFL L13 FUEL LB FUEL
76
86
93
7
2.01
1.47
1.15
40. SB
0.61
0.14
0.18
10.BP
l.Oh 3151.05
1.20 3157.65
1.22 1153.58
1.14 1061.81
1.46
10.17
17.2'.
0.44
10.52
17. 17
13.46
3.5*
12.51
1C.42
9.11
42.57
3.86
2.43
1.4S
11.11
6.66 11788.61
3.56 72415.35
1.62 24144.(8
1.26 3184.28
51.40
71.00
16.83
0.46
66.06
86.56
106.45
3.72
POWER
PERCENT
RATED
T.O.
76
86
93
7
CP
LB/IK KTH-HR
1 . 168
C.164
0.693
40.415
cr
2
LB/1KHTH-HR
1815. 67R
1658.653
1 "16.14 1
3032.651
THC
LB/1KKTH-HP.
0. 358
r.2"l
0. 1 1 1
10.777
NO
I B/ 1K*TH-HH
5.510
6.4(,B
7.363
0.4TJ
NO
2
LR/ IK* IH-HR
0.6IR
0.710
0.731
3.108
NO
X
LP/1KHTH-HR
6.128
f.l 7fl
8.015
1.543
IV-218
-------
CAL ID NUMBER: 346 ENGINE TYPE »NO MODELl JT8D-T
TEST ORGANISATION! U.S. BUREAU OF HIKES
SERIAL NUMBER: 654992
MODE
TA«I-IOLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POM Eft
0.060
I. 000
0.850
0.400
0.060
FRACTIONAL
POKER
0.060
l.OOD
0.850
0.400
0.060
FRACTIONAL
POUER
0.060
1.000
0.850
0.400
0.060
POKER
i TH
840.0
14000.0
11900.0
1600.0
840.0
POKER
1 TH
B40.0
14000.0
11900.0
5600.0
840.0
POWER
f TH
B40.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL USAGE TINE IN
RATE RATE WT FACTOR NODE
LB/HR LB/HR MIN.
94.100 822. T01 .000 19.00
8.258 8522.590 .000 O.TO
11.486 7158.480 .000 2.20
30.095 3379.01! .000 4.00
34.100 822.701 .000 T.OO
TOTAL FOR CYCLE I
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TINE IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
10.188 822.701 1.000 19.00
0.508 8522.190 1.000 0.70
1.000 7118.480 1.000 2.20
6.594 3379.051 1.000 4.00
10.388 822.701 1.000 7.00
TOTAL FOR CYCLE:
L8S POLLUTANT/IK LB FUEL/CYCLE:
LAS POLLUTANT/ U LB TH-HR/CYCLEl
LBS POLLUTANT/ 1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE HT FACTOR MODE
LB/HR LB/HR MIN.
2.816 822.701 I. 000 19.00
125.935 8522.590 I.DOO 0.70
86.411 7158.480 1.000 2.20
24.617 3379.055 1.000 4.00
2.816 822.701 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
CO
MASS
LBS.
10.798
0.096
0.421
2.006
3.978
17.300
18.333
12.940
0.688
HC
MASS
LBS.
3.290
0.006
0.110
0.440
1.212
5.017
1.319
3.782
0.423
NOX
MASS
LBS.
0.892
1.469
3.169
1.641
0.329
7.499
7.947
1.609
104.946
FUEL
MASS
LBS.
260.12
99.43
262.48
221.27
91.98
943.68
FUEL
MASS
LBS.
260.52
99.43
262.48
221.27
95.98
943.68
FUEL
MASS
LBS.
260.12
99.43
262.48
225.27
95.98
943.68
LB CO /
IK LB FUEL
41.448
0.969
1.60!
8.906
41.448
LB HC /
IK LB FUEL
12.627
0.060
0.419
1.912
12.627
LB NOX/
IK LB FUEL
3.423
14.777
12.072
7.281
3.423
ENERGY
f TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
f TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
TH-HR
266.00
163.33
436.33
371.33
98.00
1337.00
LB CO /
1 TH-HR
0.04059
0.00059
0.00097
0.00137
0.04019
LB HC /
t TH-HR
0.01237
0.00004
0.00025
0.00118
0.01237
LB NOX/
TH-HR
0.00335
0.00900
0.00726
0.00440
0.00331
IV-219
-------
DATE! 6/23/71
TEST ORGANIZATION: PRATT C MHITNFY
ENGINE SUPPLIER: PRATT AND WHITNEY
ENGINF DATA
CAL 10 NUMBER: 63 ENGINE TYPE AND MODEL: JT80
RATED THRUST: 15500.
ENGINE TOTAL TIME: -0. MRS
TIME SINCE HOT SECTION OVERHAUL: -0. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: -o. HRS
N2 COMPRESSOR OVERHAUL: -o. HRS
COHBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
N2 TURBINF OVERHAUL: -0. HRS
FUEL: JP-*C FUEL H/C RATIO: 2.000
OPERATIONAL OAT A ««
INLET AIR TEMPERATURE, DEGREES F: START 79.99 FINISH 78.25
ATMOSPHERIC PRESSURE: START 29.BB FINISH 29.86
INLET AIP HUMIDIFY, LBS H20/LB AIR: 0.1400
RELATIVE HUMIDITY: 81.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/M1N:
SAMPLE LINE TRANSPORT TIMF, SEC: 1.00
NUMBER OF TESTS: 10
COMMENTS:
BURNER 409-H
SERIAL NUMBER:
CLOCK
TIME
1010.00
1023.00
1032.00
1043.00
1102.00
1111. on
1120.00
1130.00
1138.00
1150.00
POWER
PERCENT
RATED
T.O.
5
11
38
64
84
100
77
44
32
a
POWER
PERCENT
RATFO
T.O.
5
11
3B
64
34
100
77
44
32
a
POWER
PERCENT
RATED
T.O.
5
11
38
64
84
100
77
44
32
8
TEST
M01E
I/ 0
2/ 1
3/ ?
4/ 3
5/ 4
6/ 5
11 6
8/ 7
9/ 3
EXHAUST
r.AS
TEMP
OFGRFES F
780.00
774.40
763.10
390.60
989.40
1086. 00
965.10
803.30
735.00
764.40
MASS EMI
CO
LR/IK
LR FUFL
40.32
1 7.40
5.30
1.77
3. 79
2.70
4.59
7. 75
1 7.39
29.34
r.o
L B/ IK *
48.
14.
1.
1.
2.
1 .
7.
4.
10.
26.
POWER ENGINE MEASURED GAS GFN CALC COMPRESSOR ENGINF TURBINE
THRUST, LBS PERCENT SPEED FUEL SIR FLOW F/A DISCHARGE PRESSURE INLFT
OR RATED RPM FLOW LB/SFC TEMP RATIO TEMP
SHP T.O. NI N2 LB/HR DEGREES f EPR DEGREES F
792.00 5 2675.00 6515.00 950.10 30.10 0.008700 248.00 1.04 1001.00
1857.00 11 3810.00 H160.00 1519.00 43.49 0.009710 359.50 1.10 1128.00
6015.00 38 6040.00 9935.00 3452.50 87.45 0.010970 578.20 1.35 1340.00
9982.00 64 7145.00 10770.00 5644.00 116.95 0.013410 696.50 1.64 1405.00
13033.00 84 7800.00 11160.00 7563.00 138.30 0.015200 772.30 1.90 1770.00
15581.00 100 8435.00 11590.00 9374.50 155.78 0.016310 843.80 2.12 1927.00
12055.00 77 7580.00 11055.00 6825.50 129.13 0.014690 749.30 1.80 1720.00
6973.00 44 6365.00 10185.00 3981.50 103.30 0.010710 615.80 1.42 1360.00
4981.00 32 5620.00 9655.00 2927.00 77.40 0.010510 539.20 1.28 1275.00
1283.00 8 3175.00 7400.00 1155.00 35.14 0.009140 309.70 1.06 1038.00
FXHAUST CO CO THC NO NO NO ALDEHYDES S.MOKE PARTICULATES
GAS IriETI 2 (Ul-ri (WET) 2 X
PRESSURE PPMV (WET) PPMV PPHV (WET) (WET)
PSI A
15.20
15.98
19. 59
73.71
27. 4J
30.55
25.97
21.56
18.66
15.49
MASS EMI
HC
1 H/K
LB FUEL
8.65
2.05
0.44
0.19
0.22
0. 18
0.24
0.48
0.83
4.15
959
236
043
002
198
677
598
421
513
',17
PFRCENT V
229.20
114.50
42.60
18.30
43.90
35.80
49.30
59.60
116. ro
142.20
-MASS EMI MASS FMI
NU2 C07
LH/1K L»/1K
LI FUFL LB FUEL
0.99 3049.89
1.25 3104.77
1.12 3128.21
0.92 3133.88
1.13 3131.20
1.30 3133.00
1.27 3129.88
1.60 3174.75
2.06 3107.35
2.41 3080.26
CO
1.09 84.
1.30 21.
1.60 6.
2.06 7.
2.31 4.
2 . 64 4 .
2.14 4.
1.53 6.
1.79 9.
0.95 35.
MASS FMI
NO
LB/1K
LB FUEL
7.69
3.84
8.03
13.37
19.80
25.97
18.73
10.48
7. 50
1.46
'HC
2
LB/1K
3.22')
1.145
4.610
7.814
11 .4B8
15.623
10.319
5.985
4.410
3.112
40 12.60 -0
00 20.40 -0
50 44. BO -0
80 92.70 -0
30 148.00 -0
51 719.80 -0
30 177.50 -0
5C 56.60 -0
20 38.00 -0
10 17.30 -0
«USS E"l MASS tMI
HC NO 2
LB/HR LB/hR
8.22 0.94
3.12 1.90
1.53 3.88
2.22 5.21
1.64 3.90
1.70 12.21
1.64 8.66
1.91 6.17
2.44 6.04
4.79 7.78
NO
'
1. 193
1.121
0.645
0.522
0.6B3
0.784
0.719
1.914
1.213
2. 167
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.no -o.oo
.00 -0.00
.00 -0.00
.00 -0.00
MASS EMI MASS EMI
C,12 NO
LB/HR LR/HR
2397.39 2.56
4716.13 5.84
10800.13 27.71
17687.61 73.00
23681.24 149.72
29370.79 243.47
21362.96 124.40
12439.20 41.73
9095.20 21.96
3557.70 3.99
NO
X
4.421
4.166
5.256
8.336
12.170
16.407
11 .038
6.899
5.62J
5.279
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS IMt
N0»
LB/HR
3.50
7.74
31.61
83.21
158.61
255.63
133.06
48. 11
28.01
6.77
IV-220
-------
CAL 10 NUMBER 1 63 ENGINE TYPE AND MODEL: JI8D
TEST ORGANIZATION! PRATT I MH1TNEY
SERIAL NUMBERI
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IOLE
TAKEOFF
CLIMB OUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POXER
0.060
1.000
0.650
0.400
0.060
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
POKER
f TH
910.0
15500.0
13175.0
6200.0
910.0
POKER
1 TH
910.0
15500.0
13175.0
6200.0
910.0
POKER
1 TH
910.0
15500.0
13175.0
6200.0
910.0
EMISSION FUEL USAGE TIME IN
RATE RATE NT FACTOR NODE
LB/HR LB/HR MIN.
38.597 966. US .000 19.00
20.127 9485.969 .000 O.TO
20.115 7814.688 .000 2.20
32.719 16T2.174 .000 4.00
18.597 966.115 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE!
LBS POLLUTANT/1000K LB TH AT T.O.I
EMISSION FUEL USAGE TIKE IN
RATE RATE KT FACTOR MODE
LB/HR LB/HR MIN.
6.769 966.115 .000 19.00
2.017 9485.969 .000 0.70
1.920 7814.688 .000 2.20
2.510 1672.174 .000 4.00
6.769 966.115 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TINE IN
RATE RATE UT FACTOR MODE
LB/HR LB/HR MIN.
1.995 966.115 .000 19.00
261.961 9485.969 .000 0.70
161.697 7814.688 .000 2.20
17.145 1672.174 .000 4.00
1.995 966.115 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
. LBS POLLUTANT/ IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
CO
MASS
LBS.
12.222
0.235
0.746
2.181
4.503
19.887
18.750
11.435
1.515
HC
MASS
LBS.
2.144
0.024
0.070
0.169
0.790
3.196
3.013
2.159
1.519
NOX
MASS
LBS.
1.265
3.056
5.929
2.490
0.466
13.206
12.450
8.921
197.175
FUEL
MASS
LBS.
105.94
110.67
286.54
244.81
112.71
1060.67
FUEL
MASS
LBS.
305.94
110.67
286.54
244.81
112.71
1060.67
FUEL
MASS
LBS.
105.94
110.67
286.54
244.81
112.71
1060.67
LB CO /
IK LB FUEL
39.951
2.122
2.602
8.910
19.951
IB HC /
IK LB FUEL
7.007
0.213
0.246
0.689
7.007
LB NOX/
IK LB FUEL
4.135
27.616
20.691
10.170
4.135
ENERGY
TH-HR
294.50
180.81
483.08
413.33
108.50
1480.25
ENERGY
TH-HR
294. SO
180.83
483.08
411.33
108.50
1480.25
ENERGY
TH-HR
294.50
180. S3
483.08
413.33
108.50
1480.25
LB CO /
f TH-HR
0.04150
0.00130
0.00154
0.00528
0.04150
LB HC /
1 TH-HR
0.00728
0.00013
0.00015
0.00041
0.00728
LB NOX/
TH-HR
0.00410
0.01690
0.01227
0.00602
0.00410
IV-221
-------
DATE: 6/21/71
TEST ORGANIZATION: PRATT c WHITNEY
ENGINE SUPPLIED: PRATT ANr) WHITNEY
ENGINE DATA ...«...................,..,,.,...,,,.
CAL ID NUMBFR: 150 ENGINE TYPE AND MODEL: JTRO
SERIAL NUMBER:
RATED THRUST: 15500.
ENGINE TOTAL TIME: -0. HRS
TIME SINCE HOT SECTION OVERHAUL: -0. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: -0. HRS
NZ COMPRESSOR OVERHAUL: -o. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FUST STAGE NQ22LE GUIDE VANE OVERHAUL: -0. HRS
Nl TURBINE OVERHAUL: -0. HRS
N2 TURBINE OVERHAUL: -n. HRS
FUEL: JP-4C FUEL H/C RATIO: 2.000
OPERATIONAL DATA «««««»»«
INLET AIR TEMPERATUREf DEGREES f: START 83.29 FINISH
ATMOSPHERIC PRESSURE: START 24.82 FINISH
INLET AIP HUMInlTY, LBS H20/LH AIR: 0.0108
RELATIVE HUMIDITY: 42.OP PEPCFNT
SAMPLE LINF: TEMPERATUKF, DEGREES C: 15.00, FLOW RATE, LITFRS/MIN:
SAMPLE LINE TRANSPORT TIMF, SEC: 1.00
NUMBER OF TESTS: 10
COMMENTS:
BURNFR « 409-H
83.21
29.80
CLOCK
TIME
] 3*1. CIO
1353.00
1400.00
1451.00
150B.OO
1513.00
1523.00
1530.00
1554.00
1611.00
POWER
PERCENT
RATF.O
T.O.
5
11
39
64
84
100
7T
45
31
R
POWER
PERCENT
RATED
T.O.
5
' 11
19
6*
14
100
77
45
11
B
POWER
PFRCENT
RATFD
T.O.
<;
II
19
64
84
100
77
45
31
a
TEST POWER
MOOE THRUST, LBS PERCENT
OH RATED
SHP
I/ 0 790.00
?/ 1 178?. 00
3/ 2 6063.00
4/ 1 9963.00
5/ 4 13048.00
6/ 5 15592.00
7/ 6 12072.00
S/ 7 6976.00
9/ H ',911.00
10/ 9 1353.00
EXHAUST TXHAUST
GAS GAS
T.O.
5
11
39
64
84
100
77
45
31
8
ENGINF
SPEFO
RPM
Nl
2655.00
3765.00
5595.00
7190.00
7845.00
8515.00
7625.00
6404. OC
5652.00
3269.00
C'J
IWF
Tl
N2
6685.00
8110.00
10005.00
10800.00
11255.00
1 1685.00
1 1120.00
10240.00
9716.00
7547.00
MFASURFD
FUEL
FLOW
LB/Hk
966.00
148(1.00
3502.50
5622.50
7556.00
9593. CO
6932.50
3985.00
2916.50
1 188.00
CO THf. NO
2 Iw
ET) IWE1
GAS GEN
AIR FLOW
L8/5EC
CALC
F/A
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIO
DEGREES F
29.70
41.10
B7.20
114.50
115.20
153.70
129.00
93.90
77.50
36. 10
NO
1 2
TEMP PRESSURE PPMV (WFT1 PPMV PPMV (hETl
OET.RFES F PS I A
780.00 15.20
774.40 15.98
763.10 11.59
890.60 23.73
999.40 27.41
1 Of 6. 00 30.55
965.10 ?5.97
803.80 20.56
715.00 18.66
764 .40 11.67
MASS F1I MASS EMI
CO HC
LB/IK LP/ln
LB FUFL L? FUEL
17.74 7.01
16.15 1.58
8.29 0.54
1.44 0.42
0.80 0.30
0.56 0 . 2 .1
0.9] 0.28
1.78 0.41
6.70 0.71
??.80 7.05
cn
Lfl/iKd TH-HP.
-.6 . 1 52
13.651
4.7D9
O.HI?
0.461
0.144
0.534
1.875
3.964
20.021
PERCENT V
211.
105.
f>H.
16.
10.
8.
1 1.
27.
',9.
132.
MASS FMI
N'12
LO/1K
L8 FUU
1.32
1.80
.61
.07
.16
.40
.11
.69
7.26
2.31
CO
2
10
no
40
10
60
60
70
50
20
00
"ASS tMI
CO?
LB/IK
in FUFL
3C59.22
1107.72
1123.21
3134.13
1115.67
JI36.22
3115.51
1111.24
3125.77
3094 . 1 0
1.09 68
1.28 17
1.64 7
2.26 8
2.66 7
3.07 6
2 . T. 1 6
1 .67 7
1.46 9
1.14 23
.MASS tMI
NO
LR/IH
LB FUFL
2.05
1.78
8.76
13. OR
20.12
25.80
18.66
10.55
7.61
4.11
THC
LR/K#TH-M1 LQ/lKKTH-t-n
1 740.765
2594.996
U04.242
1768.821
1815.843
1929.565
1800.'i06
1788. 7C3
1S4B.4 77
2716.771
8. 569
1.123
0.311
0.217
0. 1 74
0.144
0.162
0.281
0.420
2.502
.50 7.
.90 14.
.80 44.
.30 96.
.00 163.
.10 241.
.20 142.
.20 53.
.10 34.
.80 14.
MASS tMI
rax
Lh/lK
L3 FUEl
3. 37
5.58
10. J9
15. C5
21 .28
27.20
19.97
12.23
9.89
6.44
Ml)
PPMV
00 4.50
90 7.10
00 8.20
40 7.40
30 9.40
60 11.10
90 10.00
80 *.60
10 10. ID
50 8.20
O.OC9040
0.009530
0.01 1 170
0.013651
0. 015536
0.017350
0.014940
0.01 1790
0.010460
0.009150
NO
X
IfcFT I
PPMV
11.50
22.00
52.20
103.80
172.70
754. 70
152.90
62.40
44.20
22.70
244
366
593
720
712
870
768
630
554
521
.80
.00
.00
.70
.00
.20
.80
.80
.00
.50
EPP
1.04
1.10
1.35
1.64
1.90
2.12
1 .60
1.42
1.28
1.06
ALOFHYOES SMOKE
-0
-0
-0
-0
-0
-0
-0
-0
-0
-0
MASS F"l MASS EMI MASS [Ml
CO
LP/HR
16.46
24.11
29.04
H .09
*. .01
5. 16
0.45
13.08
11.55
77. C9
LR/IK»TH-H<< CS
7.
3.
5.
7.
11.
15.
10.
6.
4.
1.
51 1
15*
060
887
654
875
717
024
511
612
HC
LB/HR
6.7;
2.36
1.90
2.36
2.27
2.25
1.96
1.96
2.07
1.38
NO
2
/IK* IH-HR
1 . M 4
1.505
0.941
0.605
0.671
O.A61
0.750
0.963
1.337
2.043
NH?
Lrt/HR
1.28
i.. 68
S.77
6.01
6.75
11.42
9.05
6.72
6.59
2.76
.00 -0.
.00 -0.
.00 -0.
.00 -0.
.00 -0.
.00 -0.
.00 -0.
.00 -0.
.00 -0.
.00 -0.
MASS FMI
C02
LB/MR
2955.20
4624.28
10919.12
17622.78
23693. 12
30085.78
21716.91
12477.99
91 14.114
1675.79
NO
X
00
00
00
00
00
00
00
00
00
00
MASS
ra
TURBINE
INLET
TEMP
DEGREES F
IOCI.OO
1 128.00
1340.00
1405.00
1770.00
1922.00
1720.00
1360.00
1275.00
1038.00
PART 1CULATFS
-0.00
-0.00
-0.00
-0.00
-0.00
-C.CO
-0.00
-0.00
-0.00
-0.00
F«l MISS EMI
NOX
LB/hP IB/HR
1.
5.
10.
78.
152.
247.
129.
47.
22.
4.
9fl 3.26
63 8.31
6H 16.40
SB 84.61
0* 160. HI
52 260.94
37 136.42
0? 48.74
26 28.85
!> 7.65
ia/IK«TM-HK
',.126
4.663
6.003
1.493
12.325
16.735
11.467
6.987
5.850
5.655
IV-222
-------
CAL ID NUMBER: 150 ENGINE TYPE >ND MODEL: JT8D
TEST ORGANIZATION: PRATT ( MHITNEY
SERIAL NUMBERl X-370-47B
NDOE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IOLE
HODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
O.BSO
0.400
0.060
POWER
TH
930.0
15500.0
13175.0
6200.0
930.0
POWER
1 TH
930.0
15500.0
13175.0
6200.0
930.0
POWER
1 TH
930.0
15500.0
13175.0
6200.0
930.0
EMISSION FUEL I
RATE RATE WT
LB/HR LB/HR
39.756 962.141
5. 581 9178.480
6.952 7656.805
18.183 3631.703
39.756 962.141
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
L8S POLLUTANT/ 1000K
EMISSION FUEL I
RATE RATE NT
LB/HR LB/HR
5.179 962.141
2.326 9178.480
2.053 7656.805
2.171 3631.703
5.179 962.141
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK L8
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
EMISSION FUEL I
RATE RATE WT
LB/HR LB/HR
4.214 962.141
252. 277 9178.480
166.615 7656.805
37.315 3631.703
4.214 962.141
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
SAGE TIME IN
FACTOR NODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TM-HR/CYCLE:
LB TH AT T.O.:
JSACE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.I
JSAGE TIME IN
FACTOR MODE
HIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CVCLE:
LB TH AT T.O.:
CO
MASS
IBS.
12.589
0.065
0.255
1.212
4.638
18.760
17.920
12.673
0.420
HC
MASS
LBS.
1.640
0.027
0.075
0.145
0.604
2.491
2.380
1.683
1.751
MOX
MASS
LBS.
1.335
2.943
6.109
2.488
0.492
13.366
12.768
9.030
189.886
FUEL
MASS
LBS.
304.68
107.08
280.75
242.11
112.29
1046.87
FUEL
MASS
LBS.
304.68
107.08
280.75
242.11
112.25
1046.87
FUEL
MASS
LBS.
304.68
107.08
280.75
242.11
112.25
1046.87
LB CO /
IK LB FUEL
41.320
0.608
0.908
5.007
41.320
LB HC /
IK LB FUEL
5.383
0.253
0.268
0.598
5.381
LB NOX/
IK LB FUEL
4.380
27.486
21.760
10.275
4.380
ENERGY
TH-HR
294.50
180.83
483.08
413.33
108.50
1480.25
ENERGY
TH-HR
294.50
180.83
483.08
413.33
108.50
1480.25
ENERGY
1 TH-HR
294.50
180.83
483.08
413.33
108.50
1480.25
LB CO /
TH-HR
0.04275
0.00036
0.00053
0.00293
0.04275
LB HC /
TH-HR
0.00557
0.00015
0.00016
0.00035
0.00557
LB NOX/
TH-HR
0.00453
0.01628
0.01265
0.00602
0.00453
IV-223
-------
D»TSI 6/23/71
TEST ORGANIZATION: PRATT c WHITNEY
ENGINE SUPPLIER: PRATT AND WHITNEY
ENGINE OAT A ««««..«».»««..«<......................................
CAL ID NUMBER: 151 ENGINE TYPE AND MODEL: JTSD
RATED THRUST: 15500.
ENGINE TOTAL TIME: -0. MRS
TINE SINCF HHT SECTION OVERHAUL: -0. MRS
TIMF SINCE:
NI COMPRESSOR OVERHAUL: -o. HRS
H2 COMPRESSOR OVERHAUL: -o. HRS
COMBUSTUR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
Nl TURBINE OVERHAUL: -0. HRS
N2 TURBINF OVERHAUL: -o. HRS
FUEL: JP-S FUEL H/C RATIO: 1.970
OPERATIONAL DATA ««>««»«>«««««««..««
INLEI AIR TEMPERATURE, DEGREES F : START 81. 41 FINISH 77.48
ATMOSPHERIC PRESSURE: START 29.81 FINISH 79.84
INLFT AIH HUMIDITY, LHS H2D/LB AIR: 0.0153
RELATIVE HUMIDITY: 65.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 15C.OO, FLPW RATE, LITERS/MIN:
SAMPLE LINF TRANSPORT TIME, SFC: 1.DC
NUMBER OF TESTS: 10
COMMENTS:
BURNER o 40*) H
SERIAL NUMBER:
CLOCK
TIME
1802.00
1821.00
1833.00
1852.00
1910.00
1916.00
1930.00
1933.00
1950.00
2008.00
POWE°
PERCENT
T.Q.
5
11
38
64
83
100
77
44
32
7
POWER
PERCENT
RATED
T.n.
^
11
38
64
83
ion
77
44
32
7
PIWER
PERCFNT
RATED
T.n.
5
11
38
64
83
100
77
44
37
7
TESI
M01E
I/ 0
2/ 1
3/ 2
4/ 3
5/ 4
6/ 5
7/ 6
8/ 7
9/ B
in/ 9
EXHAUST
GAS
T C MP
OEGRFES f
7P9.4C
785.00
710.60
910.60
1002.50
1 100.00
9/5.60
808. 7n
741.90
760.60
MASS EMI
cn
LB/IK
LB FUFl.
',6.20
17.52
5. 39
1.61
0.83
0.57
1.00
4.00
7.97
28.43
r. n
POWER
THRUST, LBS
OR
SHP
791.00
1825.00
5991.00
9990.00
13001.00
15579.00
12023.00
6932. On
4963.00
11 74.00
E XhAUST
GAS
PSI A
15.21
16.00
19.55
23.59
27.25
30.61
26.03
20.53
18.67
15.40
1ASS EMI
HC
LU/1K.
LB FUEL
5.5H
1.96
0.56
0.25
0. 16
0.13
n.15
0.35
0.66
4.80
PERCFNT
RATED
T.C. N
5 2636
II 2815
38 6045
64 7177
83 7807
100 *472
77 7581
44 6355
32 5637
7 3067
cn
IHETI
7»5.00
125.60
46. 90
1 >( . 60
12.20
9.50
14.10
37. 70
62.40
17«. no
MASS FMI MASS
ENGINE
SPEEO
RPM
1 N2
.00 6679.00
.00 B194.00
.00 9973.00
.00 10777.nO
.00 11203.00
.00 11627.00
.00 11056.00
.00 10187.00
.00 9677.00
.00 7257.00
MEASURED
FUEL
FLOW
LB/HR
97C.OO
1539.00
34P5.50
5779.00
7656.50
9650.50
6986.00
4012.50
2981.00
1136.00
GAS GEN
AIR FLOW
LB/SEC
CALC
F/A
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP
DEGREES F
29.70
43. IB
86. IB
115.54
136.7?
154.92
129.26
94.31
78.00
34.07
CO THC NO X'l
2 IWFT) lt.FT
PFRCFNT V
1.20 60
1.42 24
1.7 a
2.4 5
2.9 4
3.3 3
2.7 3
l.HB 5
1 . S6 9
1.73 52
F"l MASS EMI
N02 C02 VI
L11/1K LP/IK IP/K
LB TUEI. LB F
2. OH 3056.
1.60 3111.
I.3S 3134.
0.98 3141.
1.02 1142.
.15 3143.
.O-i 3142.
.34 3137.
.85 3130.
.57 1086.
CO
T
LB/IK1TH-HR Lfl/lKHTH-HR
56.
14.
3.
0.
0.
0.
0.
2.
4 .
27.
658
771
128
929
490
350
583
3IB
786
509
3748.325
2621.983
1B73.645
1B17.185
1850. B3B
1947.1 18
1B25.9H?
1815.975
I8BO.I 37
2986.773
IHL LB FUEL
62 1.6?
61 2.84
55 6.74
37 11.35
79 1 6. M
27 22.04
54 14.20
7.H 9.47
?C 5.B7
6* 2.36
THC
L B/ 1KBTH-HR
6.H43
1.657
0.375
0.144
0.042
O.OB?
O.OB6
0.701
0.395
4.647
.10 6.
.60 12.
.50 15.
.30 84.
.00 144.
.90 225.
.60 120.
.70 54.
.no 28.
.50 9.
MASS IMI
NOX
IB/IK
LB FUEL
3.70
4.44
8. 14
12.33
17.20
23.25
15.26
10.76
7.72
3.94
NL
LB/1KHT
1.
2.
3.
6.
9.
13.
H.
5.
3.
2.
1 7
PPMV
10 7.80
40 7.00
80 7.40
30 7.30
30 9.10
90 II. <>0
60 9. 00
00 /.70
OO B.BO
on 6. on
0.009080
0.009910
0.011240
0.013970
0.015640
O.OI731B
0.015025
0.011B2d
0.010620
O.C09270
NO
X
PPMV
13.90
19.40
43.20
91.60
153.41
737. 7T
129.60
61.70
36.80
15.00
261.
369.
588.
70S.
778.
856.
755.
618.
543.
795.
30
30
30
70
30
70
80
00
30
70
RATIO
EPR
.04
.in
.35
.63
.89
.13
.80
.47
.29
.06
TURBINE
INLET
TEMP
D6GRFFS F
991.90
1133.20
1349.50
161 1.40
177', .50
1941.90
1719.20
1410.90
1270.10
101 1.60
ALOFHYDES SMOKE PAOT 1 CULATl S
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
"ASS PMI MASS EMI MASS FMI
CP
LB/HR
44. B2
26.96
18.74
9.23
d.38
5.46
7.01
16.07
73.76
37.30
H-Hfl L
9«?
395
92?
563
529
685
251
453
528
285
HC
LB/HR
5.41
.02
.95
.44
.20
.28
.03
.3"
.96
5.46
NO
?
I/ IK B 'H-HP
2.547
1.352
O.B11
0.568
0.601
0.715
0.616
0.778
1. 109
1 .623
N02
LC/HU
2.01
2.47
4.86
5.68
7.81
11.14
7.40
5.39
5.50
1.79
00 -0
00 -0
no -n
00 -o
no -o
00 -0
00 -0
00 -0
OC -0
00 -0
MASS FMI
CO 2
LB/HR
2964.93
4781). 77
10925.46
18153.68
24062. 74
30334.14
21953.79
12588.34
9331.12
3506.47
NT
X
.00
.00
.00
.no
.00
.OP
.00
.00
.00
.00
MASS EM
NO
LP/HR
1.58
4. 37
23. 50
65. 57
123. B9
213.2(1
99.21
3 /. 80
17.51
7.68
-0.00
-n.oo
-0.00
-0.00
-c.oo
-0.00
-0.00
-o.no
-n.oo
-0.00
MASS EMI
MIX
LH/t-P
3.59
6.B4
28.36
71.24
131.70
224.34
106.61
43.19
23.01
4.47
LB/1KI TH-MH
4 .539
3. 748
4.733
7.132
10.130
14.400
8.867
6.230
'..637
3. 808
IV-224
-------
CAL 10 NUMBER: 151 ENGINE TYPE »ND MODEL: JT80
TEST ORGANIZATION: PRATT c MHITNEY
SERI»L NUMBER! X-3TO-47C
NODE
TAXI-IDLE
TAKEOFF
CLIH80UT
APPROACH
TAXI-IDLE
FRACTIONAL
POHER
0.060
1.000
0.850
0.400
0.060
POHER
TH
930.0
15500.0
13175.0
6200.0
9)0.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
60.595 1050.830
8.049 961 B. 285
10.278 7902.832
21.374 3810.882
60.595 1050.830
UT
TOTAL FOR CTCLEI
IBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
IBS POLLUTANT/1000K
MODE
FRACTIONAL
POHER
TAII-IOL6 0.060
TAKEOFF 1.000
CLIMBOUT 0.830
APPROACH 0.400
TAXI-IDLE 0.060
POKER
1 TH
930.0
15500.0
131T5.0
6200.0
930.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
5.869 1050.830
1.500 9618.285
1.233 7902.832
2.256 3810.882
5.869 1050.830
MT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
PONER
1 TH
930.
15500.
13175.
6200.
930.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
3.287 1050.830
224.084 9618.285
137.551 7902.832
32.194 3810.882
3.287 1050.830
MT
USAGE TINE IN
FACTOR NODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-MR/CYCLEI
LB TH AT T.O.:
USAGE TIME IN
FACTOR NODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.t
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.I
CO
MASS
LBS.
19.188
0.094
0.377
1.425
7.069
28.153
25.331
19.019
0.606
HC
MASS
LBS.
1.858
0.018
0.045
0.150
0.685
2.756
2.480
1.862
1.129
NOX
MASS
LBS.
1.041
2.614
5.044
2.146
0.383
11.228
10.103
7.586
168.665
FUEL
MASS
IBS.
332.76
112.21
289.77
254.06
122.60
1111.40
FUEL
MASS
LBS.
332.76
112.21
289.77
254.06
122.60
1111.40
FUEL
MASS
LBS.
332.76
112.21
289.77
254.06
122.60
1111.40
LB CO /
IK LB FUEL
57.664
0.837
1.301
5.609
57.664
LB HC /
IK LB FUEL
5.585
0.156
0.156
0.592
5.585
LB NOX/
IK LB FUEL
3.128
23.298
17.405
8.448
3.128
ENERGY
TH-HR
294.50
180.83
483.08
413.33
108.50
1480.25
ENERGY
TH-HR
294.50
180.83
483.08
413.33
108.50
1480.25
ENERGY
TH-HR
294.50
180.83
483.08
413.33
108.50
1480.25
LB CO /
TH-HR
0.06516
0.00052
0.00078
0.00345
0.06516
LB HC /
1 TH-HR
0.00631
0.00010
0.00009
0.00036
0.00631
LB NOX/
TH-HR
0.00353
0.01446
0.01044
0.00519
0.00353
IV-225
-------
DATE: 6/24/71
TEST ORGANIZATION: PRATT c WHITNEY
FNGINE SUPPLIER: PRATT AND WHITNEY
ENGINE DATA ««»>*
CAL in NUMBER: 152 ENGINE TYPE AND MODEL: JTBO
RATEO THRUST: 15500.
ENGINE TOTAL TIME: -0. MRS
TIHE SINCE Hi)T SECTION OVERHAUL: -0. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: -o. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
CQMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIOE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
N2 TURBINF OVERHAUL: -o. HRS
FUEL: JP-S FUEL H/C RATIO: 1.970
OPERATIONAL OAT A «««««o»«««»««>««»»»»«
INLET AIR TEMPERATURE, DEGREES F: START 75.45 FINISH 86.66
ATMOSPHERIC PRFSSUBF: START 29.86 FINISH 29.81
INLET AIK HUMIDITY, LBS H20/LB AIR: 0.0152
RELATIVE HUMIDITY: 75.10 PERCFNT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE. LITFRS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER CE TESTS: 4
COMMENTS:
BURNER = 409 H
SERIAL NUHBFR:
CLOCK
TIME
952.00
1125.00
1320.00
1431.00
TEST
MODE
I/ 0
2/ 1
I/ 2
4/ 1
THPUST
OR
SHP
4992 .
14510.
I26H6.
1174.
POWER
,LBS PERCENT
RATED
or
00
00
00
T.C.
32
91
fll
8
FNC. INF
SPEED
RPM
NI
564C.OO
f200.nc
7785. 00
3105.00
N2
9670.00
11465.10
11225.00
7595.00
"EASURED
FUEL
FLOW
IH/HR
2981.50
8792.00
7462.50
1 390. 00
GAS GEN
AIR FLOW
LH/SEC
78.60
147.51
1 19.37
15.98
C«UC COMPRESSOR
ftk niSCHARGF
TEMP
O.OIOS40
0.016560
0.014670
0.010730
DFGREES F
517.00
825.HO
619.50
37B.BO
ENGINE
PRESSURE
RATIO
FPR
1.29
2.01
I.8H
1 .08
TURBINE
INLET
TEMP
OFGCFES F
1259.80
1871.60
1590.70
1074.50
POUFR
PERCENT
RATED
T.n.
12
91
11
R
FXHAUST
GAS
TEP"
DFGREES f
717.80
1058.00
1013. 10
785.90
EXHAUST
CAS
PRESSURE
PS I A
ie. n
29.22
27.116
15. XI
CO
(WET)
PPMV
59.90
in. 30
1 1.20
151.40
CO
2
IWETI
PERCENT V
1.55
2.74
2.flfl
0.59
THC
IWETI
PPMV
9.40
5. HO
5.90
35.70
NO
(WETI
PPKV
25.6C
1 78.90
147.10
7.9C
NO
2
IWtTI
PPMV
6. 10
9.50
7.50
10.60
NO
X
IWFTI
PPMV
31.70
1 PS. 40
154.60
18.50
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
PAOTICIM ATFS
-0.00
-0.00
-0.00
-0.00
P3WEP
PERCENT
RATED
T.O.
12
91
91
n
MASS FMI
cn
LD/1K
LS FUEL
1. 17
0.75
0.92
49.73
MASS EMI
HC
IB/lH
L* FUEL
0.10
0.24
0.21
6.72
MASS FMI
N')2
Lii/lK
LB EUFL
1.56
1.14
0.86
5.72
MASS CKI
C02
LB/U
LB FIIFL
31L1.40
1142.56
H',2.44
1047. «7
»ASS CMI
NO
LB/IK
LP FUEL
2.37
71 .45
U. . 7 8
4.?7
MASS (-Ml
NOX
Lfl/lK
Lfl FUEL
2.91
22.59
1 7.61
9.99
MASS E."l
CO
LB/HK
10.05
6. SI
6.^4
59.19
MASS EMI
HC
LB/HH
0.90
2. 13
1.75
9.34
MASS 1 M 1
N02
LR/HR
1.68
10.01
6. 38
7.96
MASS FMI
CH2
L3/HK
9357.13
27630.41
23450.45
4236.54
MASS EMI
NO
LB/HH
7.05
1 88.59
125.21
5.91
M.\SS FMI
NOX
IP/HB
0.73
198.61
131.60
13. B9
POWER
PERCENT
HATED
T.O.
12
91
81
a
LP/1KKTH-HP
2.011
o.w>
0.519
50. 157
1374.051
1904.232
1848.510
308J.360
THC
LR/1KSTH-HR
0.181
0. 147
0. I1H
6.801
NO
LQ/IK KTH-Hft
1.411
12.99H
9. ! 7 0
4.316
0.337
0.690
0.501
5.791
1 .749
13.68S
10. 174
10.107
IV-226
-------
CM. 10 NUMBER: 152 ENGINE TYPE AND MODEL: jiso
TEST ORGANIZATION: PRATT C WHITNEY
SERIAL NUMBER: X-370-470
MODE
TAXI-IOLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IOLE
HODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
HOOF
TAXI-IOLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IOIE
FRACTIONAL
POKER
0.060
1.000
O.BSO
O.*00
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
1 TH
930.0
15500.0
13175.0
6200.0
930.0
POWER
TH
930.0
15500.0
1 3 1 75 . 0
6200.0
930.0
POWER
* TH
930.0
15500.0
13175.0
6200.0
930.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
102.156 1098.22*
7.318 9*70.8**
7.*67 7812.359
11.633 3713.650
102.156 1098.22*
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
17.517 1098.22*
2.39* 9* 70. B**
2.057 7812.359
1.399 3713.650
17.517 1096.22*
TOTAL FOR CYCLE1
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
0.689 1098.22*
239.5*5 9*70.8**
150.127 7812.359
19.373 3713.650
0.689 1098.22*
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
USAGE TIME IN
FACTOR MODE
HIN.
.000 19.00
.000 0.70
.000 2.20
.000 *.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 *.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLF.:
LB TH AT T.O.:
USAGE TIME IN
FACTOR NODE
MIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 +.00
1.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
32.3*9
0.085
0.27*
0.776
11.918
+5. +02
+0.52J
30.672
0.551
HC
MASS
LBS.
5.5*7
0.028
0.075
0.093
2.0**
7.787
6.950
5.261
1.802
NOX
MASS
L6S.
0.218
2.795
5.505
1.292
0.080
9.889
8.826
6.681
180.303
FUEL
MASS
LBS.
3*7.77
1 10. +9
286. +5
2*7.58
128.13
1120. +2
FUEL
MASS
LBS.
3*7.77
110. *9
286. +5
2*7.58
128.13
1120.42
FUEL
MASS
LBS.
3*7.77
H0.*9
286.45
2*7.58
128.13
1120.42
LB CO /
IK LB FUEL
93.019
0.773
0.956
3.132
93.019
LB HC /
IK LB FUEL
15.950
0.253
0.263
0.377
15.950
LB NOX/
IK LB FUEL
0.627
25.293
19.217
5.217
0.627
ENERGY
TH-HR
29*. 50
180.83
483.08
413.33
108.50
1*80.25
ENERGY
f TH-HR
29*. 50
180.83
483.08
413.33
108.50
1*80.25
ENERGY
1 TH-HR
29*. SO
180. 83
483.08
413.33
108.50
1*80.25
LB CO /
1 TH-HR
0.10985
0.000*7
0.00057
0.00188
0.10985
LB HC /
1 TH-HR
o.oiee*
0.00015
0.00016
0.00023
o.oiaa*
LB NOX/
TH-HR
0.0007*
0.015*5
0.01139
0.00312
0.0007*
IV-227
-------
0«TEI 7/U/71
TEST ORGANIZATION: U.S. BUREAU OF MINES
ENGINE SUPPLIER! AMERICAN AIRLINES
ENGINE DATA
CAL in NUMBER!
ENGINE TYPE AND MODEL: JI80-1
SERIAL NUMBER: 65*458
RATED THRUST: 14000.
ENGINE TOTAL TIME: 8340. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIKE SINCF:
NI COMPRESSOR OVERHAUL: o. HRS
NZ COMPRESSOR OVERHAUL: o. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NUZZLE GUIDE VANF OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N? TURBINE OVERHAUL: o. HRS
FUEL: JFT - A FUEL H/C RATIO: 1.920
OPERATIONAL DATA «»««««««««««««««««««««««««»«»
INLET AIR TEMPERATURE, DEGREES F: START 98.00 FINISH
ATMOSPHERIC. PRESSURE: START 14.35 FINISH
INLET AIR HIIMIDITV, LBS H20/LO AIR: 0.0130
RELATIVE HUMiniTV: 30.00 PFRCFNT
SAMPLE LINE: TEMPFR ATURE, OEGREFS C: 134.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 7
COMMENTS:
H/C IS CAL-ESTI.MATtn
TEMP. SAMPLELINC AVERACFD
TOP ARM OF PROBE FAILED OURINC, 2ND LAST HUN
WITH RETROFIT
99.00
14.35
CLOCK
TIME
1100.00
105.00
110.00
115.00
1.20
125.00
no. on
tFST
MODE
I/ 0
6/ 1
I/ 6
4/ 1
.1/4
?/ t
I/ 2
POWFR
THRUST, LBS "ERCFNT
OR KATFO
SHP
170.00
1580.00
990.00
101 10.00
11130.00
12020.00
1BO.OO
T.O.
6
61
7
72
79
B5
6
FNGI.ME
SPFFO
RPM
NI
294B.OO
7177.00
2965.00
7514.00
7773.00
7984.00
?97?.00
N2
7775.30
1 1055.00
7317.00
11340.00
I 1548.00
1I6HT.OO
7327.00
MFASURFD
FUFL
FLOW
LB/HR
1133.00
5190.00
1C24.00
6150.00
.5770.00
7410.00
IC30.00
CAS GEN
MR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CALC COMPRESSOR
F/A niSCHARGE
TFMP
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
DEGREES F
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
ENGINF
PRESSURE
RATIO
EPK
1.01
2.12
1.01
2.36
2.54
2.69
1.01
TURBINE
INLET
TEMP
DEGREES F
98.00
98.00
99.00
99.00
99.00
99.00
99.00
POWER EXHAUST
PFRCENT f.AS
RAIED TEMP
T.O. OEGRFFS r
6
61
7
72
79
85
6
715.00
900.no
715.00
940.00
990.00
1020.00
M5.00
PXHAUST
CAS
PRESSURE
PS I A
15.60
JO. 70
15.60
14.40
37.10
19.70
15.60
Cfl
(WET)
PPMV
87.00
19.50
St. 00
14.20
13.20
1 9. 50
91 .00
CO
2
IWFTI
PERCENT V
0.71
1.9B
0.69
1.98
2.07
2.19
1.00
IHf.
(UFT )
PPMV
24.20
7.70
23.30
1.70
I.K>
1.30
15.00
N<1
I WFTI
PPMV
4.10
1 11 .00
4.60
90.00
IOB.OO
13C.O?
B.50
NC
2
IWETI
PPMV
3.00
8.50
1.00
9.00
10.00
11.00
5.00
NO
X
IhETI
PPMV
7.10
1 19.50
7.60
99.00
I1R.OO
141.00
13.50
AlCCHYDES SMOKE PARTICULATFS
2.71
U.26
-0.00
0.23
0.27
0.36
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
1.0.
6
61
7
72
79
85
6
MASS FHI MASS EMI
CO "C
Ln/lK LO/IK
LB FUH. Lfl FUFL
24.23
1.98
21. 79
1.14
1.76
1. It
IB.05
3.86
0.13
3.HI
0. 10
0.09
0.07
3.91
ASS EMI
N02
LB/IK
LB FUEL
.37
.41
.41
.50
.59
.66
.61
MASS EMI
TU2
LII/1K
LB IUIL
1107.27
3157.44
1108.01
3152.77
3152. H7
3157.90
3116.67
MASS F.MI
MO
LP/1K
LB ruFL
1.81
16.48
?. 17
14.98
17.20
19.57
7.77
IASS tMI
NlIX
LB/1K
LB FUTL
3.25
19. B9
3.51
16. 4B
18.79
71.22
4.40
PASS F»I
r.n
LB/HH
>7.46
10.26
74.37
11.14
11.94
13.24
13.59
MASS EPI
HC
LB/MR
4.17
0.66
3.92
0.61
0.60
0.51
4.10
MASS EMI
NO?
LB/HR
1.56
7.34
1.45
9.21
10. 78
12.27
1.6R
MASS FMI
CO?
LB/HR
3520.48
16161. 14
3183.60
191B9.74
21344.95
23362.95
3210.12
MASS EKI
NO
2. 13
95.B9
2.22
92.13
116.42
l',4.9fl
2.B5
MASS EMI
NOX
LB/hR
3. 6S
103.23
3.66
101.35
127.70
157.25
4.51
POWER
PERCENT
RATED
T.O.
6
61
7
72
79
B5
6
cn
Lfl/ IKfcTH-MR
2B.304
1.195
24.611
1.127
1.073
I. 101
18.971
LB/lK«Th-H1
3629.363
1906.893
3214.744
1917.828
1917.116
1941.673
1275.MO
THC
LB/1KHTH-HH
4.509
0.077
3.557
0.060
0.054
0.047
4. 179
NO
LS/lKITtl-IIR
2.191
11.175
7..740
9.113
10 .460
17.06?
2.911
L3/1KKTH-HB
1.603
0.656
1.461
0.911
0.969
1.021
1.712
nil
x
LB/1KMH-HR
3.794
12.031
3.702
10.024
I 1.429
13.082
4.623
IV-228
-------
CAL ID NUMBER: <>o ENGINE TYPE AND MODEL: jieo-i
TESI ORGANIZATION: u.s. BUREAU OF MINES
SERIAL NUMBER: 654458
NODE FRACTIONAL
POKER
TAXI-IDLE 0.060
TAKEOFF 1.000
CUMBOUT 0.850
APPROACH 0.400
TAXI-IOLE 0.060
MODE FRACTIONAL
POWER
TAXI-IOLE 0.060
TAKEOFF 1.000
CLIMBOUT 0.850
APPROACH 0.400
TAXI-IOLE 0.060
MODE FRACTIONAL
POWER
TAXI-IDLE 0.060
TAKEOFF 1.000
CLIMBOUT O.B50
APPROACH 0.400
TAXI-IDLE 0.060
POWER
TH
840.0
14000.0
11900.0
5600.0
840. 0
POWER
1 TH
840.0
14000.0
11900.0
5600.0
840.0
POWER
1 TH
840.0
14000.0
11100.0
5600.0
840.0
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR NODE
LB/HR LB/HR MIN.
19.193 89 1.559 .000 19.00
10.484 8910.309 .000 O.TO
10.594 T423.398 .000 2.20
14.186 3520.968 .000 4.00
19.393 891.559 .000 7.00
TOTAL FOR CrCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/IOOOK LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
3.824 891.559 .000 19.00
0.326 8910.309 .000 O.TO
0.423 7423.398 .000 2.20
0.837 3520.968 .000 4.00
3.824 891.559 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/ 1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
3.096 891.559 .000 19.00
231.395 8910.309 .000 0.70
151.836 7423.398 .000 2.20
40.701 3520.968 .000 4.00
3.096 891.559 .000 7.00
TOTAL FDR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/IOOOK LB TH AT T.O.:
CO
MASS
LBS.
6.141
0.122
0.388
0.946
2.262
9.860
9.887
7.375
0.874
MC
MASS
LBS.
1.211
0.004
0.015
0.056
0.446
1.732
1.737
1.295
0.271
NOX
MASS
LBS.
0.980
2.700
5.567
2.713
0.361
12.322
12.356
9.216
192.829
FUEL
MASS
LBS.
282.33
103.95
272.19
234.73
104.02
997.22
FUEL
MASS
LBS.
282.33
103.95
272.19
234.73
104.02
997.22
FUEL
MASS
LBS.
282.33
103.95
272.19
234.73
104.02
997.22
LB CO /
IK LB FUEL
21.751
1.177
1.427
4.029
21.751
LB HC /
IK LB FUEL
4.289
0.037
0.057
0.238
4.289
LB NOX/
IK LB FUEL
3.472
25.969
20.454
11.560
3.472
ENERGY
1 TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
t TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
LB CO /
1 TH-HR
0.02309
0.00075
0.00089
0.00253
0.02309
LB HC /
TH-HR
0.00455
0.00002
0.00004
0.00015
0.00455
LB NOX/
f TH-HR
0.00369
0.01653
0.01276
0.00727
0.00369
IV-229
-------
DATE: T/U/TI
TEST ORGANIZATION! UNITED/EPA
ENGINE SUPPLIER: UNITED AIRLINES
ENGINE DATA «...«........
CAL ID NUMRFR: 1)? ENGINE TYPE AND MODEL: JT8D-1
SERIAL NUMBER:
RATED THRUST: 14000.
ENGINE TOTAL TIME: 13276. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 11535. HRS
N2 COMPRESSOR OVERHAUL: 13426. HRS
COMBIISTHR CAN REPLACEMENT: 0. HRS
FIPS1 STAGE NOZ/LE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: o. HRS
FUEL: JET - A FUEL H/C RATIO: 1.920
OPERATIONAL DATA *«»«»«»««»»««««»*««»»«»«»««««««
INLET AIR TEMPERATURE, DEGREES F: START 53.06 FINISH
ATMOSPHERIC PRESSURE: START 29.75 FINISH
INLET AIR HUMIDITV, LFIS H20/LH AIR: 0.0048
RELATIVE HUMIDITY: 54.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 160.00, FLO* RATE, LITEKS/MIN:
SAMPLE LINE IRANSPPPT TIMF, SEC: 5.00
NUMBER OF TESTS: 4
COMMENTS:
FXHAUSI GAS PRESSURE IS IN INCHES HC..
NEW SMOKELESS XURNERS
51.ISO
29.75
CLOCK
TIME
550.00
554.00
557.00
1447.00
IFST
MODE
I/ 0
2/ 1
I/ 7
4/ 1
POWER
THRUST, L^S PERCENT
OR RATEO
SHP
10755.00
12060.00
11413.00
861.00
T.O.
76
66
9*>
6
FNG1NF
SPEED
RPM
M
7369. OC
7674.00
7714.30
5798.00
N2
10948.00
1 1 162.00
11270.00
6976.00
MEASURED
FUEL
FLOW
1. B/HR
6167.00
6946.00
7893.00
1C86.CO
GAS GEN
A IP FLOW
LO/SFC
-0.00
-0.00
-0.00
-0.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIO
DFGHEFS F FPR
-0.00
-0.00
-0.00
-0.00
1.71
1.84
1.96
-0.00
TURRINE
II1LET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATEO
T.I).
76
86
15
6
EXHAUSI
GAS
TEMP
tlEGRFES F
865.40
906.80
959.00
6R7.20
EXHAUST
GAS
PRESSURE
PS I A
51.50
54.80
58.10
II .10
CO
IUEU
PP1V
10.00
10.50
10.50
20.00
r.o
2
IWFTI
PERCENT V
2.55
2.70
2.85
2.25
THC
IWET)
PPMV
2.10
2.10
2.25
15.60
NO
UETI
PPMV
104.00
I 12 .OP
167.00
2.50
NO
2
IWET)
PPMV
-0.00
-0.00
-0.00
-0.00
NO
X
IWETI
PPMV
126.00
146.00
172.00
1.00
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
PARTICU1ATES
-C.OP
-0.00
-0.00
-0.00
POWER
PERCENT
RATEO
T.O.
76
86
95
6
MASS EMI
cn
LR/1K
LS EIJFI
0.79
0. 78
0. 74
1 .73
MASS EMI
HC
LO/IK
LR FUEL
0.09
0.09
0.09
0.80
MASS EMI
NO?
LH/1K
L" FUFl
-0.00
-0.00
-0.00
-5.00
MAS? EMI
Ct'2
LP/1K
IB FtlFL
11 54. 1'l
1154.4?
1154.48
1I5C.90
MASS EMI
tin
LH/1K
LF\ FUEL
13.45
16.12
18.74
0.37
MASS I.M1
NOX
LB/IK
Lfl FUEL
ld.29
17. HI
19.00
0.44
MASS EMI
CO
l.fl/HR
4.86
5.42
5.84
1.94
"ASS FK,I
HC
LR/Hk
0.58
0.62
0.72
0. 86
MASS FMI
NO 2
LP/HR
-0.00
-0.00
-0.00
-0.00
MASS EMI
CC2
LB/HR
19453.14
21910.57
24898.29
3421.88
MASS EMI
NO
L1VHR
82.94
111.98
147. 95
0.40
MASS F»I
NOX
IB/MR
100.49
123.86
157.09
0.48
PHWEP
PERCENT
RATEn
T.O.
76
86
95
6
rn
LB/IK|(TH-HI>
0.451
O.V50
0.'.35
7.248
1108.753
1816.797
1853.517
1974.309
IHf
LR/1KMH-HP
^.054
0.052
0.051
1.004
NU
LK/1KHTH-HH
7.712
9.2P5
11.01',
0.462
LH/IKHTH-HR
-O.ono
-n.ooo
-0.000
-0.000
N.I
X
LR/IKHTH-IIO
9.343
10.770
11.694
0.554
IV-230
-------
CAL ID NUMBER: 132 ENGINE TYPE AND MODEL: JTSO-I
TEST ORGANIZATION: UNITEO/EPA
SERIAL NUMBER! 6*93*0
NODE
TAXI-IDLE
TAKEOFF
CLIHBQUT
APPROACH
TAXI-tOLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAm-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POMER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.630
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
i TH
8*0.0
14000.0
11900.0
5600. 0
8*0.0
POKER
TH
8*0.0
1*000.0
11900.0
5600.0
8*0.0
POWER
TH
8*0.0
1*000.0
11900.0
5600.0
8*0.0
EMISSION FUEL USAGE TINE IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR HIN.
2.2*7 1089.509 .000 19.00
5.693 8210.797 .000 0.70
5.352 7026.5*7 .000 2.20
3.07* 3449.023 .000 *.00
2.2*7 1089.509 .000 7.00
TOTAL FOR CYCLE:
L8S POLLUTANT/IK L8 FUEL/CYCLE:
L8S POLLUTANT/IK 18 TH-HR/CYCLE:
LBS POLLUTANT/ 1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
0.869 1089.509 1.000 19.00
0.565 8210.797 1.000 0.70
0.476 7026.547 1.000 2.20
0.492 3449.023 1.000 4.00
0.969 1089.509 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POILUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR NODE
LB/HR LB/HR MIN.
0.438 1089.509 .000 19.00
167.922 8210.797 .000 0.70
123.556 7026.547 .000 2.20
31.4*6 34*9.023 .000 *.00
0.*3B 1089.509 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
CO
NASS
LBS.
0.711
0.066
0.196
0.205
0.262
!.**!
1.365
1.078
0.*74
HC
NASS
LBS.
0.275
0.007
0.018
0.033
0. 101
0.*34
0.411
0.324
0.471
NOX
NASS
LBS.
0. 139
1.959
4.530
2.096
0.051
8.776
8.314
6.564
139.935
FUEL
NASS
LBS.
345.01
95.79
257.64
229.93
127.11
1055.49
FUEL
NASS
LBS.
3*5.01
95.79
257.6*
229.93
127.11
1055.49
FUEL
NASS
LBS.
3*5.01
95.79
257.6*
229.93
127.11
1055. *9
LB CO /
IK LB FUEL
2.062
0.693
0.762
0.891
2.062
LB HC /
IK LB FUEL
0.798
0.069
0.068
0.1*3
0.798
LB NOX/
IK LB FUEL
O.*02
20.451
17.58*
9.117
O.*02
ENERGY
TH-HR
266.00
163.33
*36.33
373.33
98.00
1337.00
ENERGY
TH-HR
266.00
163.31
*36.33
373.33
98.00
1337.00
ENERGY
1 TH-HR
266.00
163.33
*36.33
373.33
98.00
1337.00
LB CO /
f TH-HR
0.00267
0.000*1
0.000*5
0.00055
0.00267
LB HC /
TM-HR
0.00104
0.0000*
0.0000*
0.00009
0.00104
18 NOX/
1 TH-HR
0.00052
0.01199
0.01038
0.00562
0.00052
IV-231
-------
0»T6l 7/20/71
TEST ORGANIZATION: u.s. BUREAU OF HI NFS
ENGINE SUPPLIER! AMERICAN AIRLINES
ENGINE DATA
CAL ID NUMBER: 291
ENGINF TYPF AND MODEL! JT8D-I
SERIAL NUMBER: 6*8920
RATED TCRUST: 14000.
ENGINE TOTAL TINE: 15449. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIMF SINCE:
NI coMpRtssoR OVERHAUL: o. MRS
N2 COMPRESSOR OVERHAUL: o. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.920
79.00
29.50
FUEL: JET - A
OPERATIONAL DATA »««««««««««««««
INLET AIR TEMPERATURE. DEGREES F: START 78.00 FINISH
ATMOSPHERIC PRESSURE: START 29.50 FINISH
INLET AIR HUMIDITY, LOS H20/LB AIR: O.OOBO
RELATIVE HUMIDITV: 34.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 135.00, FLOM RATE, LITERS/MIN:
SAMPLE LINF TRANSPORT TIMF, SEC: 0.90
NUMBER OF TESTS: 5
COMMENTS:
H/C IS CAL-ESTIMATFn
PROBE POSITIONED 18" FROM TAILPIPE EXIT PLANt
(UNBALANCED PROBE CONFIGURATION REQUIRES MOUNTING NEAR STAND!
SAMPLE LINE TEMP. AVERAGED
WITH RETROFIT
CLOCK
TIMF
1110.00
IU5.00
1145.00
1150.00
1205.00
TEST
MORE
I/ 0
2/ 1
3/ 2
4/ 3
5/ 4
POKER
THRUST, LBS PERCENT
OR RATFO
SHP
10900.00
11980.00
12760.00
1040.00
9610.00
T.n.
77
85
91
7
68 '
F KG 1 NF
SPFFO
RPM
NI
7600.00
7850.00
R035.00
2980.nO
7280.00
N2
11200.00
11410.00
1 1560.00
7310.00
1 1000.00
MEASURED
FUFL
FLOW
I.B/HP
6410.00
7090.00
7630.00
1068.00
5590.00
CIS GEN
AIK FLOU
L8/SFC
-o.no
-o.oo
-0.00
-0.00
-0.00
CAI.C COMPRESSOR
F/A DISCHARGE
TEMP
-o.oounoo
-0.000000
-0.000000
-0.000000
-0.000000
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRFSSURE
RATIO
EPR
1.74
1.83
1.90
1.06
1.63
TURBINE
INLEI
TEMP
DFGRFFS F
-0.00
-0.00
-0.00
-0.00
-0.00
POWFR
PFRCFNT
RATCU
T.O.
77
85
91
7
E»HAUST
GAS
TFMP
DECAFFS F
920.00
955.On
990.00
670.00
B75.00
FXHAUST
GAS
PRFSSURF
PS I A
75.0.5
26. 35
27.35
15.05
23.43
CH
(HFTI
PPMV
16.50
1 7.50
17.50
101 .CO
20.50
cn
2
tUF.T)
PERCENT V
2.26
2.44
2.59
0.69
7.03
THC
(WETI
PPMV
4 .3^
1.70
1.30
47. 5D
i.7n
ND
(UFII
PPMV
101. HO
124.10
144.90
5.10
79. |0
MO
?
(WETI
PPMV
8.50
9. on
10.00
0.80
1.80
NU
X
IKFTI
PPMV
110.10
133.10
154.90
5."0
60.90
ALDEHYDES SMOKE PART1CUIATES
0.35
0.45
0.41
4.15
0.37
-0.00
-n.oo
-0.00
-o.oo
-0.00
-0.00
-0.00
-n.on
-o.oo
-o.oo
POWER
PERCENT
RATED
T.D.
77
«>
91
7
68
MASS FMI
r.r>
I.B/IK
LO FUFL
1.47
1.44
1. 36
28. 71
2.03
MASS E.'ll
HC
1 fl/IK
LB FUEL
0.72
0.08
0.06
7. 75
0.10
MASS F'M
102
LI/IK
L« FUEL
1.24
1.77
1.27
0.37
J.29
ASS IMI
CC7
LR/IK
LB FUEL
3152.99
3153.41
3153.60
3C89.40
3 152. '.4
MASS FMI
NO
IB/IK
Lfl FUtL
14.85
16.77
18.44
7.39
12.84
MASS EMI
NDX
LB/1K
IB FUEL
16.09
17.98
19.72
2.76
13.13
MASS FMI
CU
LB/MR
9.39
10.21
10.35
30.74
11.33
MASS E»l
HC
LI/ MR
1.40
0.57
0.44
8.28
0.54
NO 2
LB/HR
7.95
1.62
9.71
0.40
1.63
MASS EMI
C12
LR/HR
20210.64
72357.66
24061.96
3299.48
17622.15
MASS FMI
ND
LB/MP
95.17
118.87
140. 73
2.55
71. 7R
MASS CMI
NDX
LR/HR
103.12
127.50
150.44
2.95
73.42
POKER
PERCENT
RATED
T.O.
77
85
91
cn
LR/ IKKTH-HP
O.B62
O.P52
o.eii
29.556
1. 179
CO
?
Lfl/IK* TH-HR
1BS4.1HI
1866.749
1815.733
31(2.576
1833.730
me
LR/lKHTH-l'R
0. 129
0.047
0.035
7.961
0.056
LR/1KDTH-HU
8.731
V.923
11.029
7.451
7.470
LB/IMTII-MR
0. 729
0.720
0.761
0.3B5
0. I 70
NO
K
LB/IK«TH-MR
9.460
13.642
11.790
2.836
7.640
IV-232
-------
CAL 10 NUMBER: 291 ENGINE TYPE AND MODEL: JTBO-I
TEST ORGANIZATION: u.s. BUREAU OF MINES
SERIAL NUMBER: 64B920
MODE FRACTIONAL
POWER
TAXI-IDLE 0.060
TAKEOFF 1.000
CLIMBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.060
HODE FRACTIONAL
POWER
TAXI-IOLE 0.060
TAKEOFF 1.000
CLIMBOUT 0.650
APPROACH 0.400
TAXI-IOLE 0.040
MODE FRACTIONAL
POWER
TAXI-IOLE 0.060
TAKEOFF 1.000
CLIMBOUT 0.850
APPROACH 0.400
TAXI-IOLE 0.060
POWER
TH
840.0
14000.0
11900.0
5600.0
840.0
POWER
I TH
840.0
14000.0
11900.0
5600.0
840.0
POWER
1 TH
840.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL USAGE TIME IN
RATE RATE NT FACTOR MODE
LB/HR LB/HR MIN.
24.991 834.939 .000 19.00
9.075 8369.012 .000 0.70
9.353 7057.273 .000 2.20
17.363 3354.049 .000 4.00
24.991 834.939 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE NT FACTOR MODE
LB/HR LB/HR MIN.
7.643 834.939 .000 19.00
0.0 8369.012 .000 0.70
0.642 7057.273 .000 2.20
2.619 3354.049 .000 4.00
7.643 834.939 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CVCLE:
L8S POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE XT FACTOR MODE
LB/HR LB/HR MIN.
1.995 834.939 1.000 19.00
188.105 8369.012 1.000 0.70
127.245 7057.273 1.000 2.20
29.583 3354.049 1.000 4.00
1.995 834.939 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
L8S POLLUTANT/IOOOK LB TH AT T.O.:
CO
MASS
LBS.
7.914
0.106
0.343
1.158
2.916
12.436
13.204
9.301
0.756
HC
MASS
LBS.
2.420
0.0
0.024
0.175
0.892
3.510
3.727
2.625
0.0
KOX
MASS
LBS.
0.632
2.195
4.666
1.972
0.233
9.697
10.296
7.253
156.754
FUEL
MASS
LBS.
264.40
97.64
258.77
223.60
97.41
941.81
FUEL
MASS
LBS.
264.40
97.64
258.77
223.60
97.41
941.81
FUEL
MASS
LBS.
264.40
97.64
258.77
223.60
97.41
941.81
LB CO /
IK LB FUEL
29.931
1.084
1.329
5.177
29.931
LB HC /
IK LB FUEL
9.154
0.0
0.091
0.781
9.154
LB NOX/
IK LB FUEL
2.389
22.476
18.030
8.820
2.389
ENERGY
TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
1 TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
1 TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
LB CO /
f TH-HR
0.02975
0.00065
0.00079
0.00310
0.02975
LB HC /
1 TH-HR
0.00910
0.0
0.00005
0.00047
0.00910
LB NOX/
I TH-HR
0.00238
0.01344
0.01069
0.00528
0.00238
IV-233
-------
DATE! T/21/T1
TEST ORGANIZATION: U.S. BUREAU OF MINES
FNGINE SUPPL1FR1 AMERICAN AIRLINES
ENGINE DATA
CAL ID NUNBFR: 293
ENGINE TYPE AND MODEL: JT8D-I
SERIAL NUMBER: 448822
RATED THRUST: 14000.
ENGINE TOTAL TIME: 14661. HRS
TIME SINCE HPT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL:
N2 COMPRESSOR OVERHAUL:
COMBUSTOR CAN REPLACEMENT:
FIRST STAGE NOZ7LE GUIDE VANE OVERHAUL:
NI TURBINE OVERHAUL:
N2 TURBINE OVFRHAUL:
FUEL H/C RATIO: 1.970
0. MRS
0. HRS
0. HPS
0. HRS
0. HRS
0. HRS
90.00
29.30
FUFL: JET - A
OPERATIONAL DATA ««««««««««««»«»«»«
INLET AIR TfMPERATUKF, DEGREES F: STAB! 39.00 FINISH
ATMOSPHERIC PKESSURF: START 29.30 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0090
RELATIVE HUMIDITY: 27.oo PERCENT
SAMPLE LINE: TEMPERATURE, CEGRFES C: 132.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIMF, SFC: 0.99
NUMBER OF TESTS: 5
COMMENTS:
H/C IS CAL-ESTIMATEO
PROBF LOCATED 18" FROM TAILPIPE EXIT PLANE
(CONFIG. SAME AS USED ON 7-16-71 TEST!
Nlll COUNTER NOT OPERATING
SAMPLE LINE TEMP.AVERAGED
WITH RETROFIT
LOCK
TIME
120.00
J45.00
350.00
355.00
400.00
TEST
WOE
4/ 0
I/ 4
11 1
3/ 2
4/ 1
POWER
THRUST, LBS
OR
SHP
970.00
10080.00
11640.00
12450.00
950.00
PERCENT
*AIFO
T.O.
6
71
83
88
6
ENGINE
SPEEO
R
NI
0.00
o.oo
0.00
0.00
0.00
PM
N2
7225.00
11165.00
11410.00
11535.00
7238.00
MEASURED
FUEL
FLOW
LB/HR
1060.00
5910.00
7050.00
7770.00
1012.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
FNGINF
PRESSURE
RATIO
EPR
1.04
1.69
1.83
1.90
1.04
TURBINE
INLET
TFMP
DEGKEFS F
-0.00
-0.00
-0.00
-0.00
-0.00
POWER EXHAUST
PERCENT GAS
RATCO TEMP
T.O. PEGREES F
71
83
68
6
730.00
9'. 0.00
995.00
1050.00
730.00
EXH4UST
c.»s
PRESSURE
PSI»
14. 99
73.95
25. BB
26.K5
14.99
CO
I UE T )
ppwy
I8H.OO
I 4.00
1 3.50
14.00
111.00
CO
2
IUFTI
PERCFNT V
0.93
2.24
2.49
2.57
0.77
IMC
(«FI 1
PPMV
-0.00
1.70
2.60
7.80
46.40
NO
(WFTI
PPMV
2.20
90.50
172.60
136.70
4.30
Nil
2
(WFTI
PPMV
5.00
10.50
17.00
13.00
4.50
NP
X
(WET)
PPMV
7.20
101.00
134.60
149.70
s.eo
ALDEHYDES
4.51
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
OAUTICUL4IES
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
&
71
83
8B
6
MASS C"I
C;J
LB/IK
LB FUFL
39.10
1.25
1.09
1 . 09
2B.37
MASS EMI MASS f-MI
HC NH2
LP/IK LB/IK
LR FUFL La PUCL
-0.00
0.09
0.12
0.13
6. 79
.f4
.55
.50
.67
.89
MASS EMI
C02
LR/IK
LB FUEL
3093.36
H53.MS
3153.85
3153.33
3097.67
MASS EMI
Kf>
LB/IK
Lfl FUEL
0.76
13.37
16.21
17.54
i .ai
MASS EMI
NO It
LB/IK
LB FUEL
2.50
14.H7
17.82
19.20
3.69
MASS EMI
cn
LB/HB
42. 19
7.44
7.6'
7.95
28.71
MASS EMI
HC
LB/HR
-o.ro
0.52
O.P5
0.91
6.P7
MASS EMI
NO 2
LB/HR
1. 84
9.16
1 1.20
12.12
1.91
MASS EMI
C02
LB/HH
3278.96
18701.30
22234.63
22928.32
3129.78
MASS EMI
NO
LG/MB
^.81
78.99
114. 45
127.49
1.B3
MASS fl
NOX
LB/HR
2.65
BB. 15
175.65
139.62
3.74
POWER
PERCENT
RATED
T.O.
6
71
83
BR
43.491
n.73B
0.659
0.638
30.226
LB/1K4TM-H1
3330.367
1855.2B8
1910.192
1941.632
3294.503
THC
L fl/1K«Th-HR
-0.000
0.051
0.073
0.073
7.236
I/!K*TH-Hfl
D.B36
7.836
9.B32
10.240
1.921
LB/1KKTH-HR
1.900
0.909
0.962
0.974
2.013
LB/1««TH-HS
2.716
D.745
10.795
11.214
3.936
IV-234
-------
CM. ID NUMBER: 293 ENGINE TYPE AND MODEL: JTSD-I
TEST ORGANIZATION: u.s. BUREAU OF NINES
SERIAL NUMBER* 6*8822
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
BODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POKER
f TH
6*0.0
1*000.0
11900.0
5600.0
8*0.0
POKER
TH
8*0.0
1*000.0
11900.0
5600.0
8*0.0
POWER
1 TH
8*0.0
1*000.0
11900.0
5600. 0
8*0.0
EMISSION FUEL I
RATE RATE HT
LB/HR L8/HR
35.980 971.287
3.*10 8319.1*8
6.0*7 701*. 898
17.430 3354.598
19.880 971.287
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000X
EMISSION FUEL 1
RATE RATE KT
LB/HR LB/HR
6.613 971.287
0.2*5 8319.1*8
0.581 701*. 898
1.796 335*. 598
6.613 971.287
TOTAL FOR CYCLE:
LBS POLLUTANT/IK L8
LSS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE KT
LB/HR LB/HR
2.8*6 971.287
187.627 8319.148
128.154 7014.898
34.273 3354.598
2.846 971.287
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
ISAGE TIME IN
FACTOR MODE
HIM.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.I
JSACE TIME IN
FACTOR MODE
M1N.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
18 TH AT T.O.:
JSAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 *.00
.000 7.00
FUEL/CYCLE:
TH-MR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
11.362
0.0*0
0.222
1.162
4.186
16.971
16.992
12.69*
0.28*
HC
MASS
LBS.
2.09*
0.003
0.021
0.120
0.772
3.010
3.013
2.251
0.20*
NOX
MASS
LBS.
0.901
2.189
4.699
2.285
0.332
10.406
10.418
7.783
156.355
FUEL
MASS
LBS.
307.57
97.06
257.21
223.64
113.32
998.80
FUEL
MASS
LBS.
307.57
97.06
257.21
223.6*
113.32
998.80
FUEL
MASS
LBS.
307.57
97.06
257.21
223.64
113.32
998.80
LB CO /
IK LB FUEL
36.941
0.410
0.862
5.196
36.941
LB HC /
IK LB FUEL
6.809
0.029
0.081
0.535
6.809
LB NOX/
IK LB FUEL
2.930
22.554
18.269
10.217
2.930
ENERGY
ff TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
1 TH-HR
266.00
163.13
436.33
373.33
98.00
1337.00
ENERGY
TH-HR
266.00
163.33
4)6.33
373.33
98.00
1337.00
LB CO /
TH-HR
0.04271
0.00024
0.00051
0.00311
0.04271
LB HC /
1 TH-HR
0.00787
0.00002
0.00005
0.00032
0.00787
LB NOX/
1 TH-HR
0.00339
0.01340
0.01077
0.00612
0.00339
IV-235
-------
DATE: 7/15/71
TEST nBGANUATION: UNITED/EPA
ENGINE SUPPLIER: UNITED AIRLINES
FNCINE DATA
CAL ID NUMBER: 404
FNCINE TYPE AND MODEL: JTSD-1
SERIAL NUMBER:
653428
RATFH THRUST: 14000.
ENGINE TOTAL TIME: 12137. MRS
TIME SINCE HOT SECTION OVERHAUL: 8824. MRS
TIMF SINCE:
NI COMPRESSOR OVERHAUL: 14420. MRS
N2 COMPRESSOR OVERHAUL: 15057. MRS
COMBUSTOR CAN REPLACEMENT: 0. MRS
FIRST STAGE NCUZLE GUIDE VANE OVERHAUL: 0. MRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVFRHAUL: 0. HRS
FUEL: JET - n FUEL H/C RATIO: 1.120
OPERATIONAL DATA «»»«
INLET AIR TEMPERATURE, OEGRFFS F: START 65.50 FINISH
ATMOSPHERIC PRESSURE: START 21.77 FINISH
INLET AIR HUMIDITY, LBS H2D/L9 AIR: 0.0074
RELATIVE HUMIDITY: 55.00 PERr.FNT
SAMPLE LINE: TEMPERATURE, DEGREES C: 160.00, FLOW KATE, LITFRS/MIN:
SAMPLE LINC TRANSPORT TIME, SEC: 5.00
NUMBER OF TESTS: 4
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES HG.
EXHAUST GAS TEMPERATURE IN DEGREES C
NEW SMOKELESS BUHNERS
66.20
21.82
CLOCK
TIMf
1446.00
1453.00
1457.00
1716.00
TCST
NOOF
I/ 0
2/ 1
V 2
4/ 1
POWER
THRUST, LBS PEKCFNT
OR RATFO
SHP
10842.00
12241.00
1 1414.00
1015.00
T.O.
77
87
15
7
ENGINE
SPFFD
RPM
Nl
7436.00
7760.no
B040.00
2172. OC
12
10186.00
112ll.no
11317.00
7220.00
MEASURED
FUEL
FLOW
LB/HR
6321.00
7216.00
9054.00
1162.00
GAS GEN
AIR FLOW
IB/SEC
-0.00
-0.00
-O.OC
-0.00
CALC CflMPRESSOR
F/A DISCHARGE
TEMP
-0.000000
-0.000000
-0.000000
-0.000000
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
FPR
1.73
1.B5
1.15
-0.00
TURBINE
INLET
IFMP
OEGRFFS F
-0.00
-0.00
-0.00
-0.00
POWER EXHAUST
PERCENT r.«S
RATED TEMP
T.n. DEGREES r
77
87
15
7
so6.no
528.00
15R.OO
FXHAUST
GAS
PRESSURE
PSIA
5i. 70
55.20
5S.20
31.40
CO
IWETI
PPNV
2D.OO
10.00
30.00
51.00
cc
2
I.ET)
PCRCFNT V
7.45
7.60
2.75
0.55
THC
IWFTI
PPMV
1 .50
1.50
1 ,KO
11.40
NU
IWFTI
PPMV
11 .00
120.00
142.00
3.60
NO
2
IWFTI
PPMV
-0.00
-0.00
-0.00
-0.00
ALDEHYDES SMOKE PASTICULOTFS
I WET I
PPMV
18.00
125.00
141.00
4.00
-0.00
-o.no
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-o.co
-O.on
-o.no
-0.00
POWFR
PERCENT
RATED
T.n.
77
S7
15
7
MASS EMI
tn
LH/IK
Li) FUFl
?.21
2.31
?. 11
1H.06
ms FMI
HC
LB/1K
LP FUFL
0.07
0.07
O.OB
?.36
MASS EMI
N02
LH/1K
L9 FUEL
-0.00
-l.on
-1.00
-0.00
MASS CMI
cn?
LB/IIC
Lfl FUFL
1152.09
3157. H7
3152.75
3121.05
MASS EMI
NO
IP./K
LB FUEL
12.74
15.21
17.0?
7.14
MASS EMI
NOX
LB/IK
Lfl FUEL
13.18
15.84
17.62
2.37
ASS EMI
CD
LP/HH
14.51
16. 7r,
17.61
70. IB
MASS E»I
HC
I.B/HR
0.45
0.48
0.61
2.74
MASS E«l
Nfl2
LB/HR
-0.00
-0.00
-O.on
-0.00
MASS FMI
C02
LO/HR
11141. 60
72808.31
25388.11
3626.65
MASS [Ml
NO
LB/MR
77.46
110.05
117.95
2.48
MASS FMI
NU*
LB/HR
83.42
114.61
141.87
7.76
POWER
PFRCENT
RATED
T.O.
77
fl7
15
7
CD
LB/IK*TH-HR
l.ITi
I .16U
1.114
20.274
LR/ 1K«TH-HR
1110.021
1161.278
1812.661
1504.014
THC
Lrt/IK#TH-HR
0.041
0.031
0.045
2.647
7. 145
8.110
10.217
2.31H
NO
2
IfTH-HR
-0.000
-0.000
-0.000
-0.000
L1/1MTH-MR
7.614
1.165
10.576
2.664
IV-236
-------
CAL 10 NUMBER: 404 ENGINE TYPE AND MODEL: JI80-1
TEST ORGANIZATION: UNITED/EPA
SERIAL NUMBER!
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
TH
840.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
17.109 924.629
16.324 8492.324
15.427 7125.680
16.054 3302.655
17.309 924.629
NT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK L8
L8S POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POKER
TH
840.
14000.
11900.
5600.
840.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
2.950 924.629
0.394 8492.324
0.507 7125.680
0.842 3302.655
2.950 924.629
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
I. 000
0.650
0.400
0.060
POWER
TH
840.
14000.
11900.
5600.
840.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.815 924.629
160.015 8492.324
107.678 7125.680
25.792 3302.655
1.815 924.629
NT
TOIAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
USAGE TIME IN
FACTOR NODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
5.481
0.190
0.566
.070
.019
.327
.506
.976
.360
HC
MASS
LBS.
0.934
0.005
0.019
0.056
0.344
1.358
1.384
1.015
0.328
NOX
MASS
LBS.
0.575
1.867
3.948
1.719
0.212
8.321
8.481
6.224
133.346
FUEL
MASS
LBS.
292.80
99.08
261.27
220.18
107.87
981.20
FUEL
MASS
LBS.
292.80
49.08
261.27
220.18
107.87
981.20
FUEL
MASS
LBS.
292.80
99.08
261.27
220.18
107.87
981.20
LB CO /
IK LB FUEL
18.720
1.922
2.165
4.B6I
18.720
LB HC /
IK LB FUEL
3.190
0.046
0.071
0.255
3.190
LB NOX/
IK LB FUEL
1.963
18.842
15.111
7.809
1.963
ENERGY
TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
1 TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
L8 CO /
i TH-HR
0.02061
0.00117
0.00130
0.00287
0.02061
LB HC /
f TH-KR
0.00351
0.00003
0.00004
0.00015
0.00351
LB NOX/
f TH-HR
0.00216
0.01143
0.00905
0.00461
0.00216
IV-237
-------
DATE: 6/29/71
TEST ORGANIZATION: UNITF.O/EPA
ENGINE SUPPLIER: UNITED AIRLINES
ENCINE DATA
CAL ID NUMBCP: 123
ENGINE TYPE AND MODEL: JTSD-T
SERIAL NUMBER:
RATED THRUST: HOOD.
ENGINE TOTAL TIMF: 14869. MRS
TIME SINCE HOT SECTION OVERHAUL: 4064. MRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 12192. HAS
N2 COMPRESSOR OVERHAUL: 10281. HRS
CQMBUSTOH CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: o. HRS
FUEL: JET - 4 FUEL H/C RATIO: 1.920
OPERATIONAL DATA »«««
INLET AIR TEMPERATUREi DEGREES F: START 59.90 FINISH
ATMOSPHERIC PRESSURE: START 29.94 FINISH
INLET AIR HUMIDITY, LRS H20/LB AIR: 0.0076
RELATIVE HUMIDITY: 69.oo PERCENT
SAMPLE LINF: TEMPERATURE. DEGREES C: 160.00, FLOW RATE, LIFERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 5.00
NUMBER OF TESTS: 4
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES Hf,
SMOKELESS BURNERS
63.50
30.00
CLOCK
TIME
815.00
B40.00
845.00
1005.00
TEST
MODE
I/ 0
2/ 1
3/ 2
4/ 3
POKER
THRUST, LBS PERCENT
OR HATED
SHP
11050.00
12250.00
11550.00
1050.00
T.O.
7R
87
96
7
ENGINE
SPEED
0PM
Nl
7395.00
7670.00
7996.00
2942.00
N2
11099.00
11303.00
11521 .00
722H.OO
MFASURED
FUEL
FLOW
IB/HR
6321.00
7086.00
BC13.00
Il33.no
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
COMPRFSSOR
DISCHARGE
TFMP
DFGPF.ES F
-0.00
-0.00
-0.00
-0.00
ENGINF
PRESSURE
RATIO
EPR
1.75
1.85
1.96
-0.00
TURBINE
INLET
TFMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POWFR
PFRCENT
RATED
T.O.
7B
87
96
7
EKHAUSI
GAS
TEMP
DEGREES F
869.00
906.BO
95I.BO
676.40
FXHAUST
GAS
PRFSSURF
PS I A
52.40
55.30
SB.BO
31.50
CO
IWFTI
PPMV
30.00
20.00
15.00
60.00
CO
2
IWETI
PFRCENT V
2.76
2.60
2.71
0.33
THC
IWETI
PPMV
0.60
0.45
0.60
16.50
NO
IWETI
PPMV
95.00
102.50
150.00
2.50
NO
2
HEM
PPMV
-0.00
-0.00
-0.00
-0.00
NO
X
IhFT)
PPMV
100.00
105.00
154.7C
3.20
ALDEHYDES SMOKE "ARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
78
87
96
7
MASS EMI
cn
LB/IK
LH FUFL
2.66
1.54
1.11
15.69
MASS EMI
HC
IB/ IK
LR FUEL
0.03
0.02
0.03
5.62
MASS EMI
NU2
ID/IK
Lfl FUEL
-0.00
-0.00
-0.00
-0.00
MASS CMI
CO?
LO/1K .
LB FUFL
US1.G?
31*3.41
3154.07
3084.39
MASS EMI
NO
LR/1K
LB FUEL
13. fl5
13.00
18.25
2.44
MASS EMI
NOX
LB/IK
LB FUEL
14.58
13.31
18. 62
3.11
MASS EMI
CO
LB/HO
IS. 83
10.94
1.90
4C.44
MASS EMI
HC
LB/hR
0.10
0.14
0.20
6.37
MASS EMI
N02
LB/HP
-0.00
-0.00
-0.00
-C.OO
MASS EMI
C02
LB/HR
19421.40
22345.05
25273.59
3494.61
MASS EMI
so
LO/HB
87.54
92.09
146.24
2.77
MASS EMI
NOX
LB/HR
92.15
94.34
150. B2
3.54
POWFR
PERCENT
RATFD
T.O.
78
87
96
7
CO
Lfl/lK» TH-HH
1.523
0.993
0.657
18.513
LB/IK«TH-HR
1102.842
1824.096
1865.210
3328.201
1HC
LB/1KI1H-HH
0.017
0.012
0.015
6.066
NO
L1/1KHTH-HS
7.922
7.518
10.793
2.616
LB/1KITH-HR
-0.000
-0.000
-r.OOO
-0.000
NO
X
L9/1K«TH-HR
B.319
7.701
11.131
3.J74
IV-238
-------
C»L 10 NUMBER: 12) ENGINE TYPE AND NOOELl JT80-7
TEST ORGANIZATION: UNITEO/EPA
SERIAL NUMBER: 649)61
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAII-IOLE
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
POWER
TH
840.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
32.538 890.156
4.281 8358.797
12.632 6931.7)8
)1.202 M94.577
32.538 890.156
WT
TOTAL FOR CTCLEl
1.8 S POLLUTANT/IK L8
L6S POLLUTANT/IK IB
IBS POLLUTANT/IOOOK
NODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
1 TH
840.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
5.982 890.156
0.0 8)58.797
0.0 69)1.738
0.712 3394.577
5.982 890.156
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK IB
L8S POLLUTANT/IK LB
LBS POLLUTANT/1000X
MODE
FRACTIONAL
POWER
TAXI-IDLE 0.060
TAKEOFF 1.000
CLIHBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.060
POWER
1 TH
840.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
2.211 890.156
163.301 8358.797
110.775 69)1.7)8
30.360 ))94. 577
2.211 890.156
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLEl
L8 TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLEI
L8 TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.I
CO
MASS
LBS.
10.304
0.050
0.463
2.080
3.796
16.613
17.321
12.485
0.357
HC
MASS
LBS.
1.894
0.0
0.0
0.047
0.698
2.640
2.739
1.974
0.0
NOK
MASS
LBS.
0.700
1.905
4.062
2.024
0.258
8.949
9.286
6.693
136.084
FUEL
MASS
LBS.
281.88
97.52
254.16
226.31
103.85
963.72
FUEL
MASS
LBS.
281.68
97.52
254.16
226.31
10). 85
96). 72
FUEL
MASS
LBS.
281.68
97.52
254.16
226.)!
103.85
963.72
LB CO /
IK LB FUEL
36.553
0.512
1.822
9.192
36.55)
LB HC /
IK LB FUEL
6.720
0.0
0.0
0.210
6.720
LB NOX/
IK LB FUEL
2.484
19.5)6
15.981
8.944
2.484
ENERGY
TH-HR
266.00
16).))
4)6.33
373.))
98.00
1337.00
ENERGY
1 TH-HR
266.00
163.))
436.33
37).))
98.00
1337.00
ENERGY
TH-HR
266.00
16).))
4)6.))
373.33
98.00
1337.00
LB
0
0
0
0
0
LB
t
0
0
0
0
0
LB
1
CO /
TH-HR
.0)874
.000)1
.00106
.00557
.0)874
HC /
TH-HR
.00712
.0
.0
.0001)
.00712
NOI/
TH-HR
0.00263
0.01166
0.00931
0.00542
0.00263
IV-239
-------
0»TE: 7/30/71
TEST ORGANIZATION: U.S. BUREAU OF MINES
ENGINE SUPPLIER: AMERICAN AIRLINFS
ENGINE DATA
CAI 10 NUMBER: 3*7
ENGINE TYPE AND MODEL: JT8D-7
SERIAL NUMBER:
RATED THRUST: 14000.
ENGINE TOTAL TIME: 9583. MRS
TIME SINCF HOT SECTION OVERHAUL: 0. H»S
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 0. MRS
N2 COMPRESSOR OVERHAUL: 0. HRS
CflMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NUllLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: 7003. HRS
N2 TURBINE OVERHAUL: o. HRS
FUEL: JET - A FUEL H/C RATIO: 1.920
OPERATIONAL DATA »«««««»»««««««
INLFT AIR TEMPERATURE, DEGREES F: START 7*.00 FINISH 75.00
ATMOSPHERIC PRFSSURF: START 29.45 FINISH 29.45
INLET AIR HIM 101 TV, LflS H20/LB AIR: 0.0100
RELATIVE HUMIDITY: 54.00 PERCENT
SAMPLE LINE: TEWEKATURC, DFGHFES C: 137.00, FLO* RATE, L1TFRS/MIN:
SAMPLE LIN* TRANSPORT TIME, SEC: 0.99
NUMBER OF TESIS: 5
COMMENTS:
H/C CAL ESTIMATRl
SAMPLE LINC TEMP. AVFRAC.EO
PROBE LOCATED Id" FROM TAILPIPF J1TH RETROFIT
CLOCK
TIMF
1200.00
1205.00
1210.00
1215.00
1220.00
TFSr
HOOF
POWER
THRUST,LP.S PF.RCFNT
OR RATtn
SHP T.C.
icon.oo
10860.00
17000.00
11300.00
70
7
77
85
FNC1NF
SPEHO
PPM
Nl N2
73BO.OO 11110.00
2890.00 7140.00
7570.OH 11270.00
7840.00 11500.00
8150.00 11730.00
MEASURED
FUFL
FLOW
LR/HR
5740.00
1045.00
6380.00
7120.00
8060.00
GAS GEN
AIM FLOW
LB/SEC
CALC
F/A
-0.00 -0.000000
-0.00 -0.000000
-0.00 -0.000000
-0.00 -0.000000
-0.00 -0.000000
COMPRESSOR
DISCHARGE
TEMP
OEGRF.ES F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRFSSURE
RATIO
EPR
1.66
1.05
1.75
1.85
1.46
IURBINE
INLFT
TEMP
OFGRFFS F
-0.00
-0.00
-0.00
-0.00
-0.00
POWER EXHAUST
PERCENT f.AS
RATED TFKP
T.O. r>EG»CES f
70
7
77
95
890.00
685. 00
930.00
970.On
1C7?.00
EXHAUST
GAS
PRFSSURE
PSI A
21.85
15. 12
?5.02
26.41
27.97
CO
1 WETI
PP*V
1 3.00
76.20
13.80
1 <.30
1 1.30
CO
2
IMFT)
PFRCENT V
I .ti
0.53
7.15
2.34
2.59
THC
(MET)
PPMV
2.60
14.60
9.90
4.60
6.90
Nn
IhFT)
PPMV
75.20
3.f.0
93. ',0
I 1 4 . (.0
142.90
MO
2
IWFT)
PPMV
6, 50
3. on
5.5n
6. 00
a. on
NO
<
(UED
PPMV
81.70
6.60
98 .90
170.60
150.90
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-o.no
-0.00
PART1CULATES
-n.no
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
1.0.
70
7
77
85
94
MASS FM|
CO
LP/IK
LB CUEI
1.35
28. ?t
I .29
1. 1H
1.07
USS E*I
HC
LB/1K
LB fUFL
0. 15
7.)6
0.53
0.42
0.11
MASS E"l
N02
L'J/ IK
Lfl FUCL
1.11
1.P3
J.84
0.85
1.02
MASS IMI
C02
LO/1K
IB FUFL
3153.34
1091.26
1152.41
3152. H7
3153.37
MASS FMI
Nil
Lb/I K
LB FUFL
12.84
2.20
14.32
16.14
18. 11
PASS TMI
NOX
LB/IK
LB FUFl
13.95
4.02
15.16
16.99
19.21
MASS FMI
CD
Lfl/l-K
7. 7(.
29.56
8.22
fl.43
8.62
"ASS EMI
HC
LB/HP
7.69
3.36
3.01
2.47
MASS FMI
N02
LH/HR
6.37
1.91
5.38
6.02
8.21
MASS EMI
C02
LB/HK
18100.18
3230.37
20112.39
22448.44
25416.15
MASS FMI
NU
LB/HR
73.73
2.29
91.34
114.93
146.60
MASS EMI
NOX
LB/HR
80.10
4.21
96.72
120.95
I54.BO
POWER
PERCENT
RATED
T.O.
70
7
77
85
C.ll
LB/ IK HH-HR
0. 7 TJ
29.559
n. 757
0.707
0 .648
cc
7
HHTH-HR
1H76.456
1230.167
1851.97C
1870.7C1
1910.989
THC
LB/1KBTH-HU
0. Oin
7.617
n.il I
0.251
0.116
NO
1 !V IKfT M-HR
/ .440
?. .294
H.41 1
9.578
11.022
LB/1K4TH-HR
C.643
1.912
0.495
0.501
0.617
NO
K
LB/1MTH-HR
B.OB3
4.205
8.906
10.079
I 1.6.19
IV-240
-------
CAL ID NUMBER: 347 ENGINE TYPE AND MODEL: JT80-7
TEST ORGANIZATION: u.s. BUREAU OF NINES
SERIAL NUMBER) 65*133
MODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
0.060
1.000
0.850
0.400
0.060
POMER
1 TH
840.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
26.479 908.471
6.853 8547.906
7.130 7185.T19
17.079 3287.870
26.479 908.471
WT
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
POWER
1 TH
840.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
6.951 908.471
1.882 8547.906
2.650 7185.719
3.421 3267.870
6.951 908.471
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IOOOK
MODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
1 TH
840.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL
RATE RATE
L8/HR LB/HR
3.260 908.471
178.049 6547.906
122.605 7185.719
32.072 3287.870
3.260 908.471
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IDOOK
USAGE TINE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.I
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.D.:
CO
MASS
LBS.
8.385
0.080
0.261
1.139
3.089
12.954
13.272
9.689
0.571
HC
MASS
LBS.
2.201
0.022
0.097
0.228
0.811
3.359
3.442
2.512
1.568
NOX
MASS
IBS.
1.032
2.077
4.496
2.138
0.360
10.123
10.372
7.572
148.374
FUEL
MASS
LBS.
287.66
99.73
263.48
219.19
105.99
976.06
FUEL
MASS
LBS.
287.66
99.73
263.48
219.19
105.99
976.06
FUEL
MASS
LBS.
287.68
99.73
263.48
219.19
105.99
976.06
LB CO /
IK LB FUEL
29
0
0
5
29
.146
.802
.992
.194
.146
LB HC /
IK LB FUEL
7
0
0
1
7
.651
.220
.369
.041
.651
LB NOX/
IK LB FUEL
3
20
17
9
3
.588
.830
.062
.755
.588
ENERGY
1 TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
f TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
1 TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
LB CO /
1 TH-HR
0.03152
0.00049
0.00060
0.00305
0.03152
LB HC /
TH-HR
0.00827
0.00013
0.00022
0.00061
0.00627
LB NOX/
1 TH-HR
0.00388
0.01272
0.01030
0.00573
0.00388
IV-241
-------
DATE: e/ z/7i
TEST ORGANIZATION: U.S. BURFAU Of MINES
ENGINE SUPPLIER: AMERICAN AIRLINES
ENCINF DATA
CAL in NUMBFR: 348
ENGIN? TVPE AND MODEL: JT8D-7
SERIAL NUMBER: 654374
RATED THRUST: 14000.
ENCINF TOTAL TIMF: 10486. MRS
TIME SINCF HOT SECTION OVERHAUL: 0. MRS
TIME SINCF:
NI COMPRESSOR OVERHAUL:
N2 COMPRESSOR OVERHAUL:
COMBUSTOR CAN REPLACEMENT:
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL:
NI TURBINE OVFRHAUL:
N2 TURBINE OVERHAUL:
FUEL H/C RATIO: 1.920
0. HRS
0. HRS
0. HRS
0. HRS
0. HRS
0. KRS
-0.00
-0.00
FUEL: JET - A
OPERATIONAL DATA .».«.»««««««»«»«««
INLET AIR TEMPERATURE. DEGREES F: START 80.00 FINISH
ATMOSPHERIC PRESSURE: START 29.30 FINISH
INLET MR HUMIDITY, LBS H20/LB AIR: 0.0120
RELATIVE HUMIDITY: 53.00 PERCENT
SAMPLE LINE: TEMPERATURE, OEGRFES C: 135.CC, FLOW HATF, LITEKS/MIN:
SAMPLE LINE TRANSPORT MMF, SEC: 0.99
NUMBER OF TESTS: 6
COMMENTS:
H/C CAL FSTIMATF.r) SA1PLF LINE TEMP. AVFRAGEO WITH RETROFIT
LOCK
TIME
135.00
150.00
155.00
205.00
215.00
270.00
TEST
MOOR
4/ 0
5/ 4
4/ 5
I/ 4
21 1
3/ J
POUER
THRUST, LUS PERCENT
OR RATED
SHP
990.
9600.
970.
10H50.
1 1750.
;.'I70.
00
00
00
00
00
0"
T.O.
1
68
6
77
83
fti
ENGINE
SPEFD
RPM
NI
0.0
7300.00
2890.00
7560.00
7BOO.OO
7Hnn.cc
N2
7230
10830
7115
1 1025
11210
11275
.00
.00
.00
.00
.00
.00
MEASURED
FUEL
FLOW
GAS GFN
AIR FLOW
LB/SEC
CALC
F/A
LB/HR
1065
5670
1070
6460
7090
7110
.00
.00
.00
.00
.00
.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.000000
-o.oooooo
-0.000000
-0.000000
-o.onoooo
-0.000000
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIO
OFGRELS F FPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
1.04
1.65
1.04
I .74
1.84
1.87
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
68
6
77
8)
86
EXHAUST
GAS
TEMP
DEGREES F
700.00
895.00
695.00
945.00
970.00
9RO.OO
FXHAUST
GAS
PRESSURF
PS1 A
14.97
23.44
14.97
24.711
?>>. 16
26.53
C'J
(WFTI
PP«W
13.50
19.50
96.00
19.50
19.00
19.00
CO
2
IWFTI
PERCENT V
0.77
2.22
0.75
2.52
2.7?
2. HO
THr.
IWET)
PPMV
36.70
2.60
41.50
5.40
2.20
1.70
no
IWETI
PPM V
4.00
64.10
4.10
86.40
103.90
109.60
NO
2
1
t
ETI
PMV
.50
.00
.00
18.00
19.50
19.50
NO
X
UETI
PPMV
8.50
79.10
9.10
104.40
12.1.40
129.10
ALOEHVOES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
7
68
6
77
83
86
MASS EMI
r.o
LK/K
L8 FUEL
27.72
1. 76
75.93
1.55
1.40
1.36
MASS EMI
HC
1 B/IK
LK FUEL
5.40
0.13
6.4?
0.25
0.09
C.07
MUSS EMI
NI12
LI/IK
LB FUFL
1.90
7.23
7.72
2.35
2.36
7.30
MUSS FMI
CO?
LB/IK
L8 FUEL
3105.19
3152.75
3097.54
3152.77
3153.43
3153.56
r-ASS EMI
NO
LR/IK
LP FUFI-
1 .61
9.52
1.8?
11.30
12.59
17.90
MASS FMI
NO*
LP/1K
LH FUEL
3.58
11.74
4.04
1?.65
14.96
15.20
MASS EM
CO
LB/HR
24.19
9.99
77.74
10.03
9.94
9.96
MASS Efl
HC
LR/HR
MASS EMI
.NO 2
L1/HR
MASS EMI
C02
LB/HR
MASS EMI
NO
LB/HR
MASS EMI
NflX
IR/HR
5.75
0.76
6.87
l.SO
0.66
O.bl
7.02
12.63
2.37
15.21
15.76
16.78
3307.24
17876.10
3314.37
20366.91
22357.62
23052.50
1 .80
53.96
1.95
73.00
89.28
94.33
3.8?
66.59
4.32
88.21
106.04
111.11
POWER
PFRCFNT
RATFD
T.O.
7
68
6
77
R3
86
r.c
LB/IKK TH-HP
24.'.37
1. "41
10.157
0.974
0.«46
O.H2I
LB/IKKTH-H1
3140.651
1862.094
3602.578
1177.135
1902.794
1902.021
THC
L B/IK0TH-HR
5.B04
0.079
7.465
0. 147
0.056
0.042
NO
LB/1KJIH-HR
1.614
5.621
7.115
6.7?»
7.593
7.761
LB/1KKTH-HR
2.041
1.315
2.580
1.402
1.426
1.385
Nl]
X
LB/IKJTH-HR
3.8,55
6.916
4.695
8.130
9.024
9.168
IV-242
-------
CAL ID NUMBER: 348 ENGINE TYPE AND MODEL: JTBD-7
TEST ORGANIZATION! U.S. BUREAU OF MINES
SERIAL NUNBER: 65*37*
MODE
TAX-IDLE
TAKEOFF
CLIMB OUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IOLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
POWER
TH
840.0
14000.0
11900.0
5600.0
840.0
POWER
* TH
840.0
14000.0
11900.0
5600.0
840.0
POWER
t TH
840.0
14000.0
11900.0
5600.0
840.0
EMISSION FUEL USAGE TIME IN
RATE RATE UT FACTOR MODE
LB/HR LB/HR MIN.
23.727 966.152 .000 19.00
8.454 8664.551 .000 0.70
8.558 7293.980 .000 2.20
16.453 3208.673 .000 4.00
23.727 966.152 .000 7.00
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/ IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
6.138 966.152 .000 19.00
0.0 8664.551 .000 0.70
0.387 7293.960 .000 2.20
1.911 3208.673 .000 4.00
6.138 966.152 .000 7.00
TOTAL FOR CYCLE!
LBS POLLUTANT/ IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/ 1000K LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
3.590 966.152 .000 19.00
166.816 8664.551 .000 0.70
111.933 7293.980 .000 2.20
27.879 3208.673 .000 4.00
3.590 966.152 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-KR/CVCLE:
LBS POLLUTANT/1000K LB TH AT t.O.s
CO
MASS
LBS.
7.514
0.099
0.314
1.097
2.768
11.791
11.778
8.819
0.705
HC
MASS
LBS.
1.944
D.O
0.014
0.127
0.716
2.801
2.798
2.095
0.0
NOX
MASS
LBS.
1.137
1.946
4.104
1.659
0.419
9.465
9.454
7.079
139.013
FUEL
MASS
LBS.
305.95
101.09
267.45
213.91
112.72
1001.11
FUEL
MASS
LBS.
305.95
101.09
267.45
213.91
112.72
1001.11
FUEL
MASS
LBS.
305.95
101.09
267.45
213.91
112.72
1001.11
LB CO /
IK LB FUEL
24.558
0.976
1.173
5.128
24.558
LB HC /
IK LB FUEL
6.353
0.0
0.053
0.596
6.353
LB NOX/
IK LB FUEL
3.716
19.253
15.346
6.689
3.716
ENERGY
TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
1 TH-MR
266.00
163.33
436.33
373.33
98.00
1337.00
ENERGY
1 TH-HR
266.00
163.33
436.33
373.33
98.00
1337.00
LB CO /
TH-HR
0.02825
0.00060
0.00072
0.00294
0.02825
LB HC /
t TH-HR
0.00731
0.0
0.00003
0.00034
0.00731
LB NOX/
t TH-HR
0.00427
0.01192
0.00941
0.00496
0.00427
IV-243
-------
OATfl 7/2J/T1
TEST ORGANIZATION: UNITED/EPA
ENGINE SUPPLIER: UNITFO AIRLINES
ENGINE DATA
CAL 10 NUMBER: 409
ENC.INE TYPE AND MODEL: JTBO-7
SERIAL NUMBER:
RATED THRUST: 14000.
ENGINE TOTAL TIMF: 15408. MRS
TIME SINCE HOT SECTION OVERHAUL: 1540R. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 13921. MRS
N2 COMPRESSOR OVERHAUL: 10937. MRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUlDF VANE OVERHAUL: 0. HRS
Nt TURBINE OVERHAUL: o. HRS
N2 TURRINF OVERHAUL: 0. HRS
FUEL: JET - A FUEL H/C PATIU: 1.920
OPFRATIONAL DATA .««*»«»«»««»«.»
INLF1 Alt TFMPERATIIRE. OE-GRFFS F: START 60.80 FINISH
ATMOSPHERIC PRESSURE: START 29.90 FINISH
INLET MR HUMIDITY, LBS H20/LB AIR: 0.0087
RELATIVE HUMI1ITY: 76.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 160.00, FLOW RATE, LITFRS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 5.00
NUMBFR OF TESTS: 4
COMMENTS:
EXHAUST GAS PRFSSURE IN INCHES HG.
SMOKELESS RENUILT FNGINF.
EPR OUT OF LIMITS IHIGHI.
58.28
30.02
CLOCK
MME
1001.00
I006.oo
1010.00
1 100.00
POWER
PFRC6NT
RATED
T.H.
75
85
97
7
POWER
PERCENT
RATED
T.O.
75
85
97
7
POWFR
PERCENT
RATED
T.O.
75
85
97
7
TFST
MUHE
I/ 0
21 1
3/ 2
V 3
EXHAUST
GAS
TEMP
DEG1FFS F
970. BO
9 1 4 . 00
9*9. 80
728.60
M4SS F.HI
CO
IB/IK
LI FUFL
3.92
3.61
3.22
3ft. 4H
PIJWER FNC.1NE
THRUST. LSS PERCFM SPFED
DR KATFO RPM
SHP T.H. Ml N2
10624.00
12004. CO
13585.00
1010.00
75 7293
«5 76C4
97 79R3
7 2952
EXHAUST CO
GAS IWETI
PRESSURE PPMV
PSU
51.80
55.30
59.30
31.70
USS FMI
HC
LI/IK
Lfl FUFL
0. 06
0.04
0.04
10.22
CO
Lf» / IK1 TH-HP
2.
2.
1.
4K
267
104
419
377
45.00
45.00
45.HO
140.00
.00
.00
.00
.00
10751.00
10980.00
11237.00
7143.00
MEASUBI'O GAS GEN
FUEL SIR FLOW
FLOW L8/StC
LB/HR
6142.00 -0.00
6998.00 -0.00
8089.00 -0.00
1201.00 -0.00
CC THC NO NO
2 IWETI IWFTI 2
(WET) PPMV PPMV MET)
PfRCFNI V PPMV
2.
2.
2.
0.
M5SS E»l MASS EMI
N12 C02
Lf/lK L»/|l<
L" CUFL 1 K FUFL
-n.OI) 3149.
-1.03 3150.
-0.01 315".
-0.00 3070.
cn
2
L?./IK» TH-H^l
\ H^O. S4 1
IB36.42K
1876.054
3651. \1?
56
11
72
53
30 1.20 74.00 -0.00
50 O.H4 95.00 -0.00
Hn 0.00 118.00 -0.00
75 61.50 7.60 -0.00
MASS FHI
NO
LI1/1K
Lf FUEL
10.59
12.51
13. 88
3.25
THC
LR/1 KK TH-HB
0.035
0.022
0.022
12.155
CALC COMPRESSOR ENGINE
F/A DISCHARGE PRESSURE
TEMP RATIO
DEGREES F EPR
-0.000000
-O.COOOOO
-0.000000
-0.000000
NO
X
(WETI
PPMV
H4.00
103.00
128.00
8.00
-0.00 1.73
-0.00 1.84
-0.00 1.98
-0.00 -0.00
TURBINF
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
ALDEHYDES SMOKE PARTICULATES
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
M4SS EMI VAiS Ml MASS FMI MASS EMI MASS EMI MASS E.»
NOX CO HC W12 C'JZ NO
LP/1K LP/^-F: LB/HP LVHR LR/HH LB/HR
Lrt FUFL
1 2 . OP 74.09
13.57 25.25
15.06 26.07
3.42 43.81
O.I/ -0
0.21 -I)
0.30 -0
12. 2R -0
NO ND
2
Ln/IKBTH-HH LH/1KKTH-HR
6. 124
7.29b
8.265
3.H6H
-0.000
-0.000
-0.000
-0.000
.00 19344.61 65.06
.00 22044.48 87.57
.00 25486.20 112.28
.00 3687.70 ).91
NO
X
Lfl/lK«TH-HR
5.952
7.410
(f.966
4.071
-0.00
-0.00
-0.00
-0.00
I Mass EMI
NOX
LB/HR
M.R(>
94.95
121.80
4.11
IV-244
-------
CAL 10 NUMBER: 409 ENGINE TYPE AND MODEL: JI8D-7
TEST ORGANIZATION: UNITED/EPA
SERIAL NUMBER! 648770
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POMER
0.060
1.000
0.850
0.400
0.060
POWER
f TH
840.
14000.
11900.
5600.
840.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
31.699 915.873
23.861 8263.066
23.952 6997. 859
28.818 3337.709
33.699 915.873
USAGE TIME IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
IBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IOLE
TAKEOFF
CLIM80UT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
f TH
840.
14000.
11900.
5600.
840.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR L8/HR
10.976 915.873
0.0 8263.066
0.122 6997.859
1.750 3337.709
10.976 915.873
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR /CYCLE:
LB TH AT T.O.:
USAGE TIME IN
WT FACTOR NODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
HOOE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
* TH
840.
14000.
11900.
5600.
840.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
2.421 915.871
130.025 8261.066
94.019 6997.859
26.164 3117.709
2.421 915.873
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
WT FACTOR MOOE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LHS POLLUTANT/IK LB
LBS POLLUTANT/1000X
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
10.671
0.278
0.878
1.921
3.932
17.681
18.183
13.224
1.988
HC
MASS
LBS.
3.476
0.0
0.004
0.117
1.280
4.877
5.016
3.648
0.0
NOK
MASS
LBS.
0.767
1.517
3.447
1.744
0.282
7.758
7.978
5.802
108.354
FUEL
MASS
LBS.
290.03
96.40
256.59
222.51
106.85
972.38
FUEL
MASS
LBS.
290.01
96.40
256.59
222.51
106.85
972.38
FUEL
MASS
LBS.
290.03
96.40
256.59
222.51
106.85
972.38
LB CO /
IK LB FUEL
36.795
2.888
3.423
8.634
36.795
LB HC /
IK LB FUEL
11.984
0.0
0.018
0.524
11.984
LB N0>/
IK LB FUEL
2.643
15.736
13.435
7.839
2.643
ENERGY
f TH-HR
266.00
163.33
436.33
371.11
98.00
1117.00
ENERGY
1 TH-HR
266.00
163.33
436.33
173.11
98.00
1117.00
ENERGY
1 TH-HR
266.00
161.31
436.33
373.33
98.00
1337.00
LB CO /
TH-HR
0.04012
0.00170
0.00201
0.00515
0.04012
LB HC /
I TH-HR
0.01107
0.0
0.00001
0.00031
0.01307
LB NOX/
TH-HR
0.00288
0.00929
0.00790
0.00467
0.00288
IV-245
-------
OATEl 6/23/71
TEST ORGANIZATION: U.S. BUREAU OF MINES
ENGINE SUPPLIER: AMERICAN AIRLINES
ENGINE DATA
CAL 10 NUMBER: 87
ENGINE ITPE AND MODEL: JT-80-9S
SERIAL NUMBER: 665397
RATED THRUST: 1*500.
ENGINE TOTAL TIME: 5469. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: n. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Ml TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: n. HRS
FUEL: JET - A FUEL H/C RATIO: 1.970
OPERATIONAL DATA ««««««««
INLET AIR TEXPERATURF, OCGRFES F: START 85.00 FINISH
ATMOSPHERIC PRESSURE: START 14.35 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0130
RELATIVE HUMIOITr: 52.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOW RATF, LITERS/KIN:
SAMPLE LINE TRANSPORT TIME, SFC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
H/C IS CAL-ESTIMATFO
SMOKELESS ENGINE
86.00
14.33
CLOCK
TIMF
1 135.00
1150.00
1215.00
1225.00
1235.00
TEST
MODE
I/ 0
21 1
3/ 2
4/ 3
5/ 4
THRUST
OR
SHP
680.
10230.
LOflOO.
1 184(1.
13610.
POWFR
.LBS PE»CENT
RATED
00
00
00
00
00
T.n.
6
70
74
91
93
FNGINE
SPFED
RPM
Nl
2770.00
7360.00
7490.00
7720.00
8180.00
N2
7C60.00
1 1040.00
11160.00
11310.00
11620.00
MEASURED
FUEL
FLOW
LB/HP
1000.00
5820.00
6700.00
6880.00
8190.00
GAS GFN
AIR FLOW
LB/SFC
-0.00
-0.00
-0.00
-0.00
-0.00
CAIC COMPRESSOR
F/A DISCHARGE
TFMP
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRFSSURE
RATIO
FPR
1.02
2.09
2.14
2.2B
2.55
TURBINE
INLET
TIMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
6
70
74
81
93
FXHAUST
GAS
TFMP
DEGREES F
76S.no
950.30
965.00
1000.00
1060.00
EXHAUST
f.AS
PRFSSURF
PS I A
10.30
24. 50
24.70
75.90
28.30
CO
IWFTI
PPMV
n7. nn
-0.00
11.00
18.10
16.00
CO
2
IUETI
PERCFST V
1.07
-O.CO
2.41
2.67
2.01
THC
(HFT)
PPMV
108.00
-0.00
13.00
14.70
17.30
NO
IKFTI
PPMV
1 7.40
-0.00
")/. 60
121 .00
170.00
NO
2
(WET)
PPMV
6.00
-0.00
6.00
8.00
12.00
NO
X
IttETI
PPMV
23.40
-0.00
103.60
129.00
182.00
ALOEHVOES
4.19
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-o.oo
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
POWEP
PERCENT
RATED
T.O.
6
70
74
81
91
MASS EMI
cn
LP/IK
LD FUEL
76.34
0.20
1 .50
1.15
1.10
MASS EMI
HC
LP/IK
LP FUFL
1 1.89
0.12
0.62
0.63
0.68
MASS EMI
N.12
LJ/1K
LO FUEL
1 .90
0.31
T . fl?
0.09
1.35
MASS FMI
cn?
LB/IK
LB FUFL
3081.87
3155.76
3151.H4
1152.03
3152.31
MASS EMI
Nil
LB/IK
LP FUEL
5.50
0.33
13.14
14.93
19.12
MASS EMI
NMX
LH/IK
LD FUFL
7.39
0.66
14.16
15. 02
20.47
MASS FMI
CO
LO/HR
26.1',
1.17
9.29
9. 10
1.97
MASS EMI
HC
LB/HR
11. H9
0.67
3.84
4.35
5.56
MASS FM
Nil 2
LB/HP
1.90
1.97
5.00
6.79
1 1.05
MASS EMI
CD2
LB/HR
MASS EMI MASS FMI
NO NOX
LB/HR LB/HR
3081.87 5.50
18363.61 1.92
19541.38 92.73
21645.95 102.74
75817.18 156.59
7.39
3.84
87.82
109.53
167.65
POWER
PERCENT
HATED
T.O.
6
70
74
81
93
P/ 1K«IH-HP
29.937
0.114
0.860
0. 756
0.659
CO
2
<1 TH-M-*
(502.121
1795.074
1809.387
1H31.5B4
1896.942
IHC
LH/1MTH-HB
13.516
0.065
0.156
0.36U
0.40H
NU
I B/1KHTH-IIR
6.245
O.I8S
7.660
B.677
I 1.506
LB/IKKTH-HR
2.154
0. lap
0.471
0.574
0.812
LB/1MTH-HR
8.399
0.375
8.131
9.7.51
12.Hfl
IV-246
-------
CAL ID NUMBER: 87 ENGINE TYPE »ND MODEL: jT-eo-9S
TEST ORGANIZATION: U.S. BUREAU OF MINES
SERIAL NUNBERl 665347
NODE FRACTIONAL
POKER
TAKI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUI
APPROACH
TAXI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
O.B50
0.400
0.060
FRACTIONAL
POKER
0.060
1.000
0.850
0.400
0.060
POKER
1 TH
870.
14500.
12325.
5800.
B70.
POWER
1 TH
EMISSION FUEL USAGE TIME IN
RATE RATE KT FACTOR NODE
LB/HR LB/HR MIN.
0
0
0
0
0
24.495 975.771 1.000 19.00
6.635 8812.832 1.000 0.70
8.388 7305.855 1.000 2.20
18.596 3429.552 1.000 4.00
24.495 975.771 1.000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE NT FACTOR MODE
LB/HR LB/HR MIN.
870.0
14500.0
12325.0
5800.0
870.0
POKER
II TH
9. 883 975.771 1
4.717 B8I2.832 1
4.513 7305.855 1
3.514 3429.552 1
9.863 975.771 1
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLIUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE MT FACTOR MODE
LB/HR LB/HR MIN.
870.0
14500.0
12325.0
5800.0
870.0
6.869 975.771 1
207.454 8612.832 1
125.870 7305.855 1
34.704 3429.552 I
6.869 975.771 1
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
7.757
0.077
0.308
1.240
2.858
12.239
11.974
8.838
0.534
HC
MASS
LBS.
3.130
0.055
0.165
0.234
1.153
4. 736
4.635
3.421
3.795
NOX
MASS
LBS.
2.175
2.420
4.615
2.314
0.801
12.326
12.058
8.901
166.917
FUEL
MASS
LBS.
308.99
102.82
267.86
228.64
113.84
1022.17
FUEL
MASS
LBS.
308.99
102.82
267.68
226.64
113.84
1022.17
FUEL
MASS
LBS.
308.99
102.62
267.68
228.64
113.84
1022.17
LB CO /
IX LB FUEL
25.103
0.753
1.146
5.422
25.103
LB HC /
IK LB FUEL
10.129
0.535
0.616
1.025
10.129
LB NOX/
IK L6 FUEL
7.039
23.540
17.229
10.119
7.039
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
TH-HR
275.50
169.17
451.92
366.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB
0
0
0
0
0
LB
0
0
0
0
0
LB
1
0
0
0
0
0
CO /
TM-HR
.02615
.00046
.00068
.00321
.02615
HC /
TH-HR
.01196
.00033
.00037
.00061
.01136
NOX/
TM-HR
.00790
.01431
.01021
.00598
.00790
IV-247
-------
DATE: 7/22/71
TEST ORGANIZATION: U.S. BUREAU OF MINES
ENGINE SUPPLIER: AMERICAN AIRLINES
ENGINE DATA
CAL ID NUMBER: 29*
ENGINE TTPF AND MODEL: JT-80-9
SERIAL NUMBER: 6*511*
RATFD THRUST: nsoo.
ENGINE TOTAL TIME: 3385. HRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: o. HRS
NZ COMPRESSOR OVERHAUL: o. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
NZ TURBINF OVERHAUL: o. HRS
FUEL: JET - A FUEL H/C RATIO: 1.920
OPERATIONAL DATA ««*»»»»«
INLET AIR TEMPERATURE, OFGREES F: START 93.00 FINISH
ATMOSPHERIC PRESSURE: START 29.20 FINISH
INLET AIR HUMIDITY, LAS H7.0/LB AIR: 0.0168
RELATIVE HUMIHITV: 6!>.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 130.00, FLOW RATF, LirE«S/»IN:
SAHPLE LINE TRANSPORT TIME, SFC: 0.99
NUMBER OF TESTS: 6
COMMENTS:
H/C 1S-CAL ESTIMATED
ENGINE RETURNED rn TF.ST AFTER REPAIR
SAMPLE LINE TEMP. AVERAGED
WITH RETROFIT
62.00
29. 20
16.00
LOCK
TIMF
220.00
240.00
250.00
255.00
300.00
305.00
TEST
MtltlE
4/ 0
5/ 4
FUEL
8.09
0.1 1
H.20
O.OK
0.08
0.05
MASS E"l
N02
L13/U
LP EUFL
1.65
1.75
2.02
2.00
1.61
1.04
MASS EMI
C02
IH/IK
L8 FUEL
3C81.92
3153.19
3087.09
3153.34
3153. S6
3153. SB
MASS t.Ml
NO
IB/IK
L» FUFL
1.20
12.53
1.3J
15.13
15.71
19.06
MASS FKI
NOK
LP./1K
LB FUEL
7.85
14.27
3.39
17.12
1 7.5B
20.99
MASS EMI
CO
LP/HB
3 7 . 79
9.52
32.12
9.51
9.60
9.79
MASS EMI
HC
LB/BR
9.2B
0.67
8.94
0.54
0.57
0.46
MASS EMI
N02
IB/HP
1.90
10.86
7.20
12. K7
13.38
16. on
MASS EMI
CU7
LB/MR
3534.96
19612.85
3364.92
20307.48
27484.84
26145.70
MASS EMI
NO
LB/HO
1.37
77.93
1.50
97.42
1 1 1.99
157.97
MASS EMI
MIX
IB/HP
3.77
86.79
3.69
110. 2B
125.36
174.04
POWER
PERCENT
RATED
T.O.
6
72
7
74
81
92
CO
LR/ IMIH-HR
39.774
0.902
30.022
O.B75
0.807
0.728
CO
2
<«TH-I«
3721.014
1859.038
3144.786
166S.214
1891.072
1945.164
THC
LR/1««TH-HR
9.T73
0.063
8.354
0.050
0.048
0.034
NI;
LB/1KPITH-HH
1.446
7.387
1.397
6.962
9.419
11.753
LO/1KHTH-HR
1.995
1.029
2.055
1. 164
1.125
1. 196
NO
X
Lfl/IK»TH-HH
3.441
8.416
3.452
10.146
10.544
12.950
IV-248
-------
CAL ID NUMBER! 294 ENGINE TYPE «ND MODEL I JT-80-9
TEST ORGANIZATION: u.s. BUREAU OF NINES
SERIAL NUMBER: 665314
MODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXt-IOLE
NODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IOLE
NODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
o.eso
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.650
0.400
0.060
POWER
TH
8TO.O
1*500.0
12325.0
5800.0
870.0
POWER
II TH
870.0
1*500.0
12325.0
5800.0
870.0
POWER
TH
870. 0
1*500.0
12125.0
5800.0
870.0
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR IB/MR NIN.
31.159 977.719 .000 19.00
9.12* 91*1.723 .000 0.70
9.803 7595.383 .000 2.20
21.67* 3624.235 .000 *.00
31.159 977.719 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CVCLE:
LBS POLLUTANT/IOOOK LS TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
8.38* 9T7.7I9 .000 19.00
0.0 91*3.723 .000 0.70
0.456 7595.183 .000 2.20
2.690 3624.235 .000 4.00
8.18* 977.719 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB FUEL/CYCLE:
LBS POLLUTANT/IK IB TH-HR/CVCLE:
LBS POLLUTANT/IOOOK LB TH AT T.O.:
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
2.888 977.719 .000 19.00
222.620 91*3.723 .000 0.70
1*0.2*8 7595.383 .000 2.20
3*. 118 362*. 235 .000 4.00
2.888 977.719 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/IOOOK LB TH AT T.O.:
CO
MASS
LBS.
9.867
0.106
0.359
1.445
3.635
15.413
14.673
11.131
0.73*
HC
MASS
IBS.
2.655
0.0
0.017
0.179
0.978
3.B29
3.6*5
2.765
0.0
NOX
MASS
LBS.
0.91*
2.597
5.1*2
2.275
0.337
11.265
10.72*
8.135
179.119
FUEL
MASS
LBS.
309.61
106.68
278.50
2*1.62
11*. 07
1050.47
FUEL
MASS
LBS.
309.61
106.68
278.50
2*1.62
11*. 07
1050.47
FUEL
MASS
LBS.
309.61
106.68
278.50
241.62
114.07
1050.47
LB CO /
IK LB FUEL
31.869
0.998
1.291
5.980
31.869
LB HC /
IK LB FUEL
8.575
0.0
0.060
0.7*2
8.575
L6 NOX/
IK LB FUEL
2.951
2*. 1*7
18.465
9.414
2.953
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
f TH-HR
275.50
169.17
451.92
186.67
101.50
1384.75
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
1 TH-HR
0.03581
0.00061
0.00080
0.0017*
0.01581
LB HC /
TH-HR
0.0096*
0.0
0.0000*
0.000*6
0.0096*
LB NO*/
1 TH-HR
0.00312
0.01515
0.01118
0.00588
0.00332
IV-249
-------
0«T6« 7/2T/71
TEST ORGANIZATION: u.s. BUREAU OF MINES
ENGINE SUPPLIER: AMERICAN AIRLINES
ENGINE DATA
CAL 10 NUMBER: }49
ENGINE IYPF AND MODEL: JT-80-9
SERIAL NUMBER:
RATED THRUST: 1450C.
ENGINE TOTAL TIME: 5500. MBS
TIME SINCE MOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: o. MRS
N2 COMPRESSOR OVERHAUL: 0. MRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST ST«GE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: 6681. HRS
N2 TURBINE OVERHAUL: 7641. HRS
FUEL: JET - A FUEL H/C RATIO: 1.920
OPERATIONAL DATA «««««««««»
INLET AIR TEMPERATURE, DEGREES F: START 71.00 FINISH
ATMOSPHERIC PRESSURE: START 29.30 FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: O.OI5J
RELATIVE HUMIDITY: 67.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 135.CC, FLOW RITE, LITERS/KIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.99
NUMBER OF TFSTS: 5
COMMENTS:
H/C CAL ESTIMATED SAMPLE LINE TEMP AVERAGED bITH RETROFIT
Bl.OO
29.10
CLOCK
TIME
1200.00
1210.00
1220.00
1230.00
1235.00
TEST
MODE
5/ 0
4/ 5
I/ 4
2/ 1
I/ 2
POWER
THRUST, LBS PERCENT
(1R HATED
SHP
10900.no
990.00
10900.00
12000.00
11720.00
T.O.
75
&
75
87
94
ENGINE
SPEED
RPM
NI
7440.00
2890.00
7500.00
7730.00
8150.00
N2
11145.00
7180.00
11160.0(1
11350.00
11670.00
MEASURED
FUEL
FLOW
Lfl/HR
4710.00
970.00
6770.00
6880.00
8110.00
GAS GEN
AIR FLOW
LH/SFC
-0.00
-0.00
-0.00
-0.00
-0.00
CALC COMPRESSOR
F/A DISCHARGE
TEMP
-0.000000
-O.OOOOPO
-0.000000
-o.oooooo
-o.nooooo
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.75
1.05
1.76
1.85
2.02
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
POHFP. EXHAUST
PERCENT GAS
RATED TEM»
T.O. DFGRtES F
75
6
75
82
94
930.00
690.00
935.00
970.00
1035.00
FXMAUST
GAS
PRESSURE
PS I A
24.78
15.07
24.94
76.17
28.53
CO
(Wf-TI
PPMV
19.20
107.00
19.60
19.40
19.20
CO
2
UETI
PERCENT V
2.33
0.77
2.39
2.57
2.88
THC
(UETI
PPMV
1.50
51.80
2.60
2.20
2.20
NO
(HETI
PPMV
as. oo
1 .91
H5.60
103.40
149.30
NO
2
IWFTI
PPMV
17.00
6.00
18.00
20.00
21.00
NO
X
(HETI
PPMV
100.00
7.90
103.60
123.40
170.10
ALDCHYOES SMOKE PASTICULATES
0.19
4.34
0.17
0.19
0.27
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.H.
75
6
75
82
94
MASS FMI
cn
LB/IK
LB FUEL
1.65
27.35
1.65
1 .51
1 .14
MISS EMI
HC
LH/1K
Lfl FUEL
0.07
7.58
0.13
n. 10
C.09
Mass EMI
N12
LR/1K
L8 FUEL
2.40
2.57
2.4H
2.57
2.40
MASS EMI
CP2
LB/1K
LB FUFL
1153.09
3092.12
3152.96
3153.24
3153.55
MASS FMI
NO
LS/IK
IP FUEL
11.74
0.80
11. HI
13.26
17.09
MASS FMI
NOX
LB/1K
LB FUEL
14. 15
3.32
14.79
15.63
19.49
MASS EMI
cn
ie/HR
11.27
26.53
10.24
1C. 42
10.85
MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI
HC N02 C02 NO NOX
LB/HR LB/HR L6/HR L6/HP LB/HR
0.46
7.35
0.78
0.68
0.71
14.93
2.44
15.44
17.65
19.50
19580.67
2999.35
19611.41
21694.28
25575.25
72.92
0. 77
73.43
91.25
138.60
87.85
3.22
88.87
108.90
158.10
POKER
PERCENT
RATED
T.O.
75
6
75
82
CO
LB/1KITII-IIK
0.94?
76.795
0.939
O.R69
O.'9l
LB/1 rt*TH-HR
1796.3T2
3029.651
1799.212
1807.857
1864.CB5
THC
LB/1K«TH-HR
0.042
7.429
0.071
0.056
0.052
LB/IK«TH-HR
6.690
0.782
6.737
7.604
10.102
LB/IKKTH-HR
I .370
2.468
1.417
1.471
1.421
NO
X
LR/IKKTH-HR
d.060
3.249
8.153
9.075
11.521
IV-250
-------
CAL 10 NUNBERl 3*9 ENGINE TYPE AND NOOELl JT-8D-9
TEST ORGANIZATIONl U.S. BUREAU OF NINES
SERIAL NUNBERl 665401
MODE FRACTIONAL
POKER
TAXI-IDLE
TAKEOFF
CL 1X9 OUT
APPROACH
TAXI-IDLE
0.060
1.000
O.B50
0.400
0.060
POWER
TH
870.
14500.
12323.
5800.
870.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
25.624 926.992
9.533 8704.117
9.460 7330.152
13.590 3208.258
25.624 926.992
USAGE TIME IN
WT FACTOR NODE
NIN.
TOTAL FOR CYCLE:
L8S POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MORE FRACTIONAL
POWER
TAXI-IOLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
0.060
1.000
0.850
0.400
0.060
POWER
1 TH
870.
14500.
12325.
5800.
B70.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
7.310 926.992
0.339 8704.117
0.459 7330.152
2.109 320B.25B
7.310 926.992
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE I
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TINE IN
WT FACTOR MODE
NIN.
TOTAL FOR CTCLEi
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
1 TH
870.
14500.
12325.
5800.
870.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
2.786 926.992
183.927 8704.117
122.037 7330.152
31.081 3208. 258
2.786 926.992
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLEI
LB TH AT T.O.:
USAGE TINE IN
WT FACTOR NODE
NIN.
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
8.114
0.111
0.347
0.906
2.989
12.468
12.646
9.004
0.767
HC
NASS
LBS.
2.315
0.004
0.017
0.141
0.853
3.329
3.377
2.404
0.273
NOX
MASS
LBS.
0.882
2.146
4.475
2.072
0.325
9.900
10.042
7.149
147.987
FUEL
NASS
LBS.
293.55
101.55
268.77
213.88
108.15
985.90
FUEL
NASS
LBS.
293.55
101.55
268.77
213.88
108.15
985.90
FUEL
MASS
LBS.
293.55
101.55
268.77
213.88
108.15
985.90
LB CO /
IK LB FUEL
27.642
1.095
1.291
4.236
27.642
LB HC /
IK LB FUEL
7.B86
0.039
0.063
0.657
7.886
LB NOX/
IK LB FUEL
3.006
21.131
16.649
9.688
3.006
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
t TH-MR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
f TH-HR
0.02945
0.00066
0.00077
0.00234
0.02945
LB HC /
i TH-HR
0.00840
0.00002
0.00004
0.00036
0.00840
LB NOX/
1 TH-HR
0.00320
0.01268
0.00990
0.00536
0.00320
IV-251
-------
DATE: 7/26/71
TEST ORGANIZATION: U.S. BUREAU OF MINES
ENGINE SUPPLIER: AMERICAN AIRLINES
ENGINE OtTA
CAL ID NUMBER: 150
ENGINE TYPE AND MODEL: JT-BD-9
SERIAL NUMBFR: 665166
RATED THRUST: 1*400.
FNGINE TOTAL TIMF: 7161. HRS
7IHE SINCE HOT SECTION OVERHAUL: 1986. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 2853. HRS
N2 COMPRESSOR OVERHAUL: 3R94. HRS
COMBUSTOR CAN REPLACEMENT: 1986. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 19B6. HRS
Nl TURBINE OVERHAUL: 5001. HRS
N2 TURBINF OVERHAUL: 5372. HRS
FUEL I-/C RATIO: 1.920
72.00
29.30
FUEL: JET - A
OPERATIONAL DATA «««««»«««««««««««»
INLET «1R TEMPERATURE, DEGREES F: START 72.00 FINISH
ATMOSPHFBIC PRFSSURl: START 29.JO FINISH
INLFT AIR HUMIDITY, LBS H73/LB AIR: 0.0130
RELATIVE HUMIDIT»: 76.00 PERCFNT
SAMPLE LINE: TEMPEKATURE, DEGREES C: 139.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT T1MF, SEC: C.99
NUMBER OF TESTS: 6
COMMENTS:
H/C CAL ESTIMATED SAMPLE LINE TEMP. AVERAGED WITH RETROFIT FIRST IDLE NOTE
UNTRIMMED
,LOf.K
TIMF
125.00
1)5.00
HO. 00
150.00
155.00
200.00
TFST
"HOE
4/ 0
5/ 4
4/ 5
\l 4
71 1
3/ 2
POWER
THRUST, LBS PERCENT
0" RATFO
SHP
960.00
10400.00
1020.00
10900.00
12000.00
13700.00
T.O.
6
71
7
75
82
Q4
ENGINE
SPEFD
RPM
Nl
2360.00
7360.00
2900.00
7430. OC
7670. OC
8110.00
N2
6950.00
11000.00
7060.00
10900.00
11130.00
1U10.00
MEASURED
FUEL
FLOW
1 B/HR
1110.00
6100.00
1040.00
6330.00
696C.OO
8210.00
GAS GFN
MR FLOW
LB/SEC
-0.00
-0.00
-0.00
288.00
300.00
314.00
CALC COMPRESSOR
F/A DISCHARGE
TEMP
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
OEGRFES f
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSUOF
RATIO
EPR
1.04
1.72
1.04
1. 76
1.85
2.03
TURBINE
INLET
TEMP
DEGREES 1
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
71
7
75
H2
EXHAUST EXHAUST
GAS GAS
TEMP PRESSURE
DFGRFES F PSIA
725.00
935.00
725.00
915.00
960.110
1020.00
14.99
24.40
14.99
25.04
2'. .35
2U.IO
cn
I WETI
PPfV
151.00
23.00
158.00
22.50
70.50
19.50
cn
2
1 WET 1
PERCENT V
0.77
2.42
0.82
2.44
7.62
2.93
THC
IUEM
PPMV
95 .00
3.90
90.70
2.40
2.20
7.20
NO NO
(WFTl 2
PPMV 1
3.10
82.10 1
7.30
41.30 1
69.30 1
en
PMV
.C3
.00
.50
.00
.00
70.00 21.00
I WFT)
PPMV
7. 10
98.10
14.80
62.30
88.30
91.00
-0.00
0.25
7.14
0.23
0.24
0.36
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-C.OO
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
6
71
7
75
82
94
MASS EMI
cn
LB/IK
LB FUFL
3 .17
.91
3 .56
. RS
.57
. 34
MASS EMI
HC
LB/K
LB FUEL
13.75
C.19
12. J5
O.I 1
0. in
0.09
MASS F»l
NO 2
L1/K
LB FUEL
1 .66
2.13
7.93
2.57
2.39
2.36
MASS EMI
CD7
LB/IK
LB FUEL
3058.18
3152.39
3062.99
3152.67
1153.16
11 51.55
MASS EMI
NH
LR/1K
LB FUFL
1.29
11.18
7.85
5.85
8.72
7.88
MASS EMI
NOX
LB/1K
Lfl EUFL
2.95
13.36
5.78
8.47
11.11
10.74
MUSS CMI
cn
LB/H«.
42. J7
11. M
39.06
11.71
10.93
10.97
MASS FMI
HC
LB/HK
15.27
1.13
12.84
0.72
0.67
0.71
MASS FHI
HO?
Lfl/h-R
1.84
13.29
3.05
16.25
16.64
19.40
MASS EMI
Cfl2
LB/HR
3394.58
19229.55
3185.51
19956.41
21945. ?7
25890.67
MASS E"I
NO
LB/hR
1.43
68.20
7.96
37.02
60.68
64.66
MASS EMI
NUX
LB/HR
1.2?
81.49
6.01
53.27
77.32
B4.06
POWER
PERCENT
RATED
T.O.
71
7
75
82
94
CO
Lfl/lKJIH-HR
44.133
I . 1 Ifl
38.299
1.175
0.911
O.HOO
LB/1MTH-HR
J516.025
1848.996
3123.049
1830.863
187B.831
1889.830
THC
L P/IK* TH-HM
15.°f>2
0. 109
12.597
0.066
0.056
0.052
NO
l.B/ 1MTH-MR
1 .488
2.906
3.3V7
5.057
4.770
7
1KK1 H-HR
1.970
1.278
2.986
1.490
1.186
1.416
NO
X
L8/1K«TH-HR
3.409
7.816
5.89J
4.887
6.443
6.136
IV-252
-------
CAL 10 NUMBER! 350 ENGINE TYPE AND MODEL: JT-8D-9
TEST ORGANIZATION: U.S. BUREAU OF MINES
SERIAL NUMBER! 669166
MODE
TAXI-IOLE
TAKEOFF
ClIMKOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.8SO
0.400
0.060
POWER
f TH
870.0
14500.0
12325.0
5800.0
870.0
POWER
1 TH
670.0
14500.0
12325.0
5800.0
870.0
POWER
1 TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL I
RATE RATE WT
LB/HR LB/HR
33.870 924.888
7.052 8801.363
9.806 7399.922
19.023 3254.844
33.870 924.888
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL I
RATE RATE WT
LB/HR LB/HR
12.377 424.886
0.187 8801.363
0.964 7399.922
3.592 3254.844
12.377 924.868
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
2.642 924.888
123.275 BB01.363
85.889 7399.922
22.374 3254.844
2.642 924.888
TOTAL FOR CYCLEl
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
SAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
ISAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
JSAGE TIME IN
FACTOR MODE
HIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLEI
LB TH AT T.O.:
CO
MASS
LBS.
10.726
0.082
0.360
1.268
3.952
16.387
16.523
11.834
0.567
HC
MASS
LBS.
3.919
0.002
0.035
0.239
1.444
5.640
5.687
4.073
0.151
NOX
MASS
LBS.
0.836
1.436
3.149
1.492
0.308
7.224
7.284
5.217
99.187
FUEL
MASS
LBS.
292.88
102.66
271.33
216.99
107.90
991.79
FUEL
MASS
LBS.
292.ee
102.68
271.33
216.99
107.90
991.79
FUEL
MASS
LBS.
292.68
102.68
271.33
216.99
107.90
991.79
LB CO /
IK LB FUEL
36.621
0.801
1.325
5.845
36.621
LB HC /
IK LB FUEL
13.382
0.021
0.130
1.103
13.382
LB NOX/
IK LB FUEL
2.856
14.006
11.607
6.874
2.856
ENERGY
» TH-HR
275.50
169.17
451.92
366.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
t TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
fl TH-HR
0.03893
0.00049
0.00080
0.00328
0.03893
LB HC /
TH-HR
0.01423
0.00001
0.00008
0.00062
0.01423
L6 NOX/
1 TH-HR
0.00304
0.00850
0.00697
0.00366
0.00304
IV-253
-------
OATE1 7/28/71
TCST ORGANIZATION: U.S. BUREAU OF NINES
ENGINE SUPPLIED: AMERICAN AIRLINES
ENGINE DATA
CAl in NUMBER: 151
ENGINE TVPE >NO MODEL: JT-BO-9
SERIAL NUMBERi
RATED THRUST: 1*300.
ENGINE TOTAL TIME: 6077. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 6077. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINF OVERHAUL: 6077. HRS
N2 TURBINF OVERHAUL: o. HRS
FUEL H/C RATIO: 1.970
FINISH -o.oo
FINISH 21.29
FUEL: JET - A
OPERATIONAL DATA «««
INLET AIR TEMPERATURE* DEGREES F: START HI.00
ATMOSPHERIC PRESSURE: START 20.29
INLFT AIR Hill 101 IV, L8S H2D/LR AIR: 0.0180
RFLATIVE HUMIDITY: 76.oo PERCENT
SAMPLE LINF: TEMPERATURE, OEGRFFS C: 14).OC, FLOW RATF, LITERS/MIN: 16.
SAMPLE LINE TRANSPORT TIMEi SCC: 0.99
NUMBER OF TESTS: 5
COMMENTS:
H/C CAL ESTIMATED SAMPIF LINE TEMP. AVERAGED USF" 0-ARHEO PKfldE APPROX. 6 INCHES
FROM TAILPIPE. *ITH RETROFIT
LOCK
TIME
610. OR
620.00
625.00
610.00
630.00
TFST
HOOF
5/ 0
'./ 5
I/ 4
11 1
I/ 2
POUFM
THOUST.LBS PERCENT
OR "ATEO
SHP
10750.00
10PO.OO
10900.00
12000.00
I 1580.00
r.O.
74
6
75
82
91
ENGINE
SPEFD
RPH
NI
7450. OC
2900.00
7480.00
7730.00
BI30.00
N2
11040.00
7200.00
1 1040.00
11260.00
11510.00
MEASURED
FUEL
FLCH
Lfl/HR
6220.00
1020.00
6340.00
6970.00
8110.00
GAS GEN
AIR FLOW
LR/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
CALC COMPRESSOR
F/A DISCHARGE
TEMP
-0.
-0.
-0.
-0.
-0.
000000
000000
000000
000000
000000
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIC
EPR
1.74
1.03
1.76
1.87
2.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATFO
T.O.
74
6
75
82
93
FXHAUST
GAS
TFMP
OEGRFFS <=
'150.00
700.00
155.00
910.00
I 100.00
F XHAUST
GAS
PPESSURF
PS I A
24.68
14.87
24.90
26.43
78.38
CO
(WET)
PPMV
19.00
105.00
17.50
16.50
16.00
CO
2
IUETI
PERCFNT V
2.24
0.85
2.26
2.34
2.57
THC
IWFTI
PPMV
2.40
J3.70
2.60
2.40
2.40
NO
(HCTI
PPMV
84.20
1.30
87.80
108.60
142.4(1
NO
2
( WETI
PPKV
7.bO
4.50
3.50
9.50
10.00
NO
X
(NET)
PPMV
91.70
7.80
96.30
118.10
152.40
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
POWFR
PERCENT
RATED
T .n.
7'.
t,
75
8?
91
MASS FMI
CO
Lfl/K
LB FUEL
. 70
7 .41
.55
.47
.25
MASS EMI
HC
LB/IK
LB FUEL
0.12
4.49
0. 13
0.12
0.11
MASS EMI
NI12
LB/IK
L9 FUEL
.10
.72
.24
. ?4
.2"
MASS FMI
C02
Lfl/IK
LB FUFL
1152.88
1105.22
JI53.0B
3153.14
1153.6]
Lfl/IK
LB FUEL
12.39
1.76
12.81
15.10
MASS EMI
NTX
LO/1K
LB FURL
11.49
2.98
14.05
16.64
19.55
cn
LR/MP
10.59
24.90
9.85
9.86
1C. 13
MASS L»l
HC
LP/CR
MASS FNI
NO 2
LB/HR
MASS EMI
C02
LR/HR
MASS EM
NO
LB/HR
0.77
4.58
0.84
0.62
6.86
1.75
7.86
9.31
10.40
19610.89
3167.3J
19990.55
21978.79
255T5.96
77.06
1.29
81. 19
106.64
148.15
MASS FMI
NOX
LB/HR
81.91
3.04
89.05
115.96
15B.55
POWER
PERCENT
RATFO
T.O.
74
6
75
82
C"
LB/IKHTII-HR
0.985
24.901
0.904
0.822
0. 746
1824.269
1167.172
1813.996
1PM .566
1881.355
THC
LB/1KHTH-H1
0.071
4.577
O.OJ7
O.OM)
O.PH4
LB/IK»TH-H°
7. 169
1 .285
7.44 fl
8.896
10.909
L1/1K»TH-HR
0.639
1.753
0.721
0.777
0. 766
NO
X
LB/IK«TH-HR
7.807
1.038
8.170
9.664
11.675
IV-254
-------
CAL 10 NUMBER: 351 ENGINE TYPE AND NODELI jT-eo-9
TEST ORGANIZATION! U.S. BUREAU OF MINES
SERIAL NUMBER! 665399
MODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CL IM80UT
APPROACH
TAXI-IDLE
0.060
I. 000
0.650
0.400
0.060
POWER
1 TH
870.0
14500.0
12325.0
5800.0
670.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
22.924 926.453
9.152 8717.707
9.858 7391.855
17.288 3506.767
22.924 926.453
USAGE TIME IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IOLE
TAKEOFF
CLIH80UT
APPROACH
TAXI-IDLE
FRACTIONAL
POMER
0.060
1.000
0.850
0.400
0.060
POWER
1 TH
670.0
14500.0
12325.0
5600.0
870.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
4.090 926.453
0.566 6717.707
0.761 7391.855
1.454 3508.787
4.090 928.453
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE!
TH-HR/CYCLE!
LB TH AT T.O.I
USAGE TIME IN
WT FACTOR MODE
HIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POMER
0.060
1.000
0.850
0.400
0.060
POWER
f TH
B70.0
14500.0
12325.0
5800.0
670.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
2.611 928.453
191.204 B717.707
125.976 7391.855
25.844 3508.767
2.611 928.453
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CVCLEI
LB TH AT T.O.:
USAGE TIME IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IOOOK
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLE:
LB TH AT T.O.I
CO
MASS
LSS.
7.259
0.107
0.361
1.153
2.674
11.554
11.452
8.344
0.736
HC
MASS
LBS.
1.295
0.007
0.026
0.097
0.477
1.904
1.887
1.375
0.456
MOX
MASS
LBS.
0.827
2.231
4.619
1.723
0.305
9.704
9. 618
7.006
153.842
FUEL
MASS
LBS.
294.01
101.71
271.03
233.92
108.32
1008.94
FUEL
MASS
LBS.
294.01
101.71
271.03
233.92
108.32
1006.99
FUEL
MASS
LBS.
294.01
101.71
271.03
233.92
108.32
1008.99
LB CO /
IK LB FUEL
24.691
1.050
1.334
4.927
24.691
LB HC /
IK LB FUEL
4.405
0.065
0.103
0.414
4.405
LB NOX/
IK LB FUEL
2.812
21.933
17.043
7.366
2.812
ENERGY
f TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
366.67
101.50
1364.75
ENERGY
t TH-HR
275.50
169.17
4SI.92
366.67
101.50
1384.75
LB
1
0
0
0
0
0
LB
1
CO /
TH-HR
.02635
.00063
.00080
.00296
.02635
HC /
TH-HR
0.00470
0.00004
0.00006
0.00025
0.00470
LB
1
0
0
0
0
0
NOX/
TH-HR
.00300
.01319
.01022
.00446
.00300
IV-255
-------
DATE: 7/20/71
IFSI ORGANISATION: PRATT C WHITNEY
ENCINE SUPPLIER: PBATT AND WHITNEY
ENGINE OAT A «.»»«««.«». »
CAl ID NUMBER: 352 ENGINE TYPE AND MODEL: JT-BO-9
RATER THRUST: 14500.
ENGINE TOTAL TIME: -0. HRS
TIME SINCE HOT SECTION OVERHAUL: -0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: -o. HRS
N2 COMPRESSOR OVERHAUL: -n. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL: jp-4 FUEL H/C RATIO: 2.000
OPERATIONAL OATA «»»««»
INLET AIR TEMPERATURE, DEGREES F: START 72.OC FINISH 77.00
ATMOSPHERIC PRESSURE: START 29.79 FINISH 29.79
INLET AIR HUMIDITY, LRS H20/LB AIR: -0.0000
RELATIVE HUMIDITY: -0.00 PERCENT
SAMPLE LINE: TEMPEHATURF, CEGREFS C: 150.OC, FLOW RATE, LITFRS/HIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER CF IESTS: 6
COMMENTS:
FXHAUST C»S PRESSURE IN INCHES HG
SPOKF DENSITY IS VON BRAND MEASURE PARTICULATFS ARE IN MG/M«»1
SERIAL NUMBER:
CLOCK
TIME
1141.00
1241.00
125R.OO
1111.00
1320.00
1150.00
TEST
MCltlE
I/ 0
4/ I
5/ 4
6/ 5
7/ 6
9/ 7
POhfiR
THkUST.LBS PERCENT
OR RATED
SHP
5000.00
9'. 50. 00
10770.00
1 1650.00
13600.00
780.00
T.O.
34
65
74
81
93
5
ENGINE
SPEFO
RPH
NI
5710. OC
7090.00
7395.00
7655.00
8125.00
7530.00
N2
9790.00
10810.00
1 1030.00
11205.00
11525.00
6530.03
MEASURED
FUEL
FLOW
LB/HR
2841.00
5250.00
6035.00
6675.00
3000.00
908.00
GAS GEN
AIR FLOW
IH/SEC
H2.80
120.70
178.90
116.10
149.90
28.80
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.009500
0.012100
0.013000
0.013600
O.OI4BOO
0.008BOO
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.30
1.61
1.74
1.B4
2.02
1.04
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
UATEO
T.H.
14
65
74
81
91
5
EXHAUST
CAS
TEMP
DEGREES F
695.00
835.00
835.On
915.00
985.00
710.00
CXHAUST
GAS
PRTSSURE
PS I A
3fl. 32
47. 98
51.16
53.97
58.84
30.S9
CO
IHETI
PPMV
47.10
17.50
14.60
12.60
10.60
197.20
CO
2
I HEM
PE8CENI
1.42
2.10
2.73
2.46
7.6H
1.00
THC
.FT)
PPMV
.80
.60
.50
.30
.00
.50
nn
IhtTI
PPMV
29. sn
78.60
98.20
120.50
168. 3C-
5.10
NO
2
I WET)
PPMV
9.90
10.80
9.80
9.10
10.80
6.70
NO
X
IWETI
PPMV
19.70
89.40
10H. 00
129.60
179. 10
11.60
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.no
SMOKE
16.00
24.00
25.00
76.00
27.00
2.00
PARTICIPATES
-0.00
-0.00
13.00
13.00
14.00
-0.00
POWER
PERCENT
HATED
T.'J.
14
81
91
5
MASS EMI
f.O
LB/K
LB FUEL
f>.bO
1 .66
1.11
1.02
0. 79
ie.ifl
"ASS FMI
HC
IB/IK
Lf ruFL
n. 39
C.20
0.03
0.06
0.09
7. 19
MASS FMI
N02
Lfl/lK
L3 FUFL
2.28
1.69
1.44
1.71
1.32
7.14
MASS EM|
CD2
LB/1K
LB FUEL
3176.32
3134.60
3135.6?
3135.97
3136.27
3057.73
fASS FMI
Nn
LH/1K
LR FUEL
6.86
17.26
14.43
16.06
70.59
1 .63
MASS F«l
nor
LP/IK
LB FUEL
9.14
13.95
is. H8
17.27
21.91
3.77
MASS EMI
CU
LP/l-1
16.76
8.73
7.B9
6.82
6.3?
34. R5
MASS EMI
HC
LB/HP
1.10
1.01
0.15
0.40
0.6B
6.53
MASS EMI
NO?
I B/HR
6.48
B.85
P. 69
8.09
10.57
1.94
MASS EMI
C02
LB/HR
8K88.I2
16456.63
IB92t.4B
20912.61
25090.16
2776.47
MASS EM
NO
LB/HR
19.50
64.39
87.11
107.19
164.72
1.48
MASS tMI
NDX
LB/HR
25.9B
73.?4
95.Bl
115.29
175.29
3.4?
POWER
PERCENT
RATED
T.O.
14
65
74
81
93
5
3.753
0.924
0.732
0.576
0.464
44 . /i 7'.
LB/IKUFH-HK
1 M7.625
17-.1.442
1757.055
17M.465
1344.865
1559.508
THC
Lft/1K0TH-MR
O.?19
0. 109
0.014
0.034
O.OSO
«. 369
NO
LB/1K1TH-HR
3.9fO
6.K14
B.CF9
9.C46
17.111
I .898
LB/IK»TH-HR
1.296
0.936
0.607
0.683
0.777
7.493
NO
X
LB/1KHTH-HR
5.195
7.750
8 .896
9.729
12.889
4.391
IV-256
-------
CU ID NUMBERl 352 ENGINE TYPE AND NOOELI JT-BD-9
TEST ORGAN!ZATIONI PRATT £ WHITNEY
SERIAL NUMBER) P-665T09
MODE
TAXI-IOLE
TAKEOFF
CLIMB OUT
APPROACH
TAXI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POKER
0.060
1.000
0.890
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
1 IH
870.0
14500.0
12325.0
5800.0
870.0
POMER
f TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
31.939 980.839
2.953 8565.398
5.316 7193.688
15.963 3251.086
31.939 980.839
TOTAL FOR CYCLE t
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
5.938 9B0.839
0.463 8565.398
0.624 7193.688
1.095 3251.086
5.838 980.839
TOTAL FOR CVCLEl
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IOOOK
USAGE TINE IN
FACTOR NODE
M1N.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE i
TH-HR/CVCLEI
LB TH AT T.O.:
USAGE TINE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLEI
LB TH AT T.O.I
CO
MASS
LBS.
10.114
0.034
0.195
1.064
3.726
15.134
15.051
10.929
0.238
HC
MASS
LBS.
1.849
0.005
0.023
0.073
0.681
2.631
2.617
1.900
0.373
FUEL
MASS
LBS.
310.60
99.93
263.77
216.74
114.43
1005.47
FUEL
MASS
LBS.
310.60
99.93
263.77
216.74
114.43
100S.47
LB CO /
IK LB FUEL
32.563
0.345
0.739
4.910
32.563
LB HC /
IK LB FUEL
5.952
0.054
0.087
0.337
5.952
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
TH-HR
0.03671
0.00020
0.00043
0.00275
0.03671
LB HC /
I TH-HR
0.00671
0.00003
0.00005
0.00019
0.00671
MODE FRACTIONAL
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
POWER
0.060
1.000
0.850
0.400
0.060
POWER
TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE
LB/HR
3.861
213.495
133. 188
32.191
3.861
RATE
LB/HR
980.839
8565.398
7193.686
3251.086
980.839
USAGE TIME IN
NT
FACTOR NODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
TOTAL FOR CYCLEl
LBS
LBS
LBS
POLLUTANT/IK
POLLUTANT/ IK
LB
LB
POLLUTANT/1000K
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
NOX
MASS
LBS.
1.223
2.491
4.884
2.146
0.450
11.193
11.133
8.083
171.778
FUEL
MASS
LBS.
310.60
99.93
263.77
216.74
114.43
1005.47
LB NOX/
IK LB FUEL
3.936
24.925
18.515
9.902
3.936
ENERGY
< TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB NOX/
t TH-HR
0.00444
0.01472
0.01081
0.00555
0.00444
IV-257
-------
OATEI T/2I/T1
TEST ORGANIZATION: PRATT t WHITNEY
ENGINE SUPPLIFR: PRATT AND WHITNEY
ENGINE DATA «
CAL ID NUMBER: 153 ENGINE TYPE AND MODEL: JT-BO-9
SFRIAL NUMBER:
RATED THRUST: 145CO.
ENGINE TOTAL TIME: -0. MRS
TIME SINCE HOT SECTION OVFRHAUl: -0. MRS
TINE SINCE:
NI COMPRESSOR OVERHAUL: -o. MRS
N2 COMPRESSOR OVERHAUL: -0. MRS
COMBUSTDR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
NZ TURBINF OVERHAUL: -o. HRS
FUEL H/C RATIO: 2.000
77.00
30.06
FUEL: jp-4
OPERATIONAL DATA ««««««««»««»»«««»»»«»»«
INLET AIR TEMPERATURE, DEGREES F: START 72.00 FINISH
ATMOSPHERIC PRESSURE: START 30.08 FINISH
INLET AIR HUMIDITY, LBS H20/LR AIR: -0.0000
RELATIVE HUMIOI1Y: -0.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.OC, FLOW RATE, LITERS/PIN:
SAMPLE LINE TRANSPORT TIMF, SEC: 1.00
NUMBER OF TESTS: 6
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES HG
SMOKE DENSITY IS VON RRANO MEASURE PARUCULATES ARE IN NG/M..3
2.00
CLOCK
TIMF
1658.00
1739.00
1751.00
1406.00
181 1.00
1831.00
TFST
MODS
21 0
3/ 2
4/ 1
5/ 4
6/ 5
7/ 6
POWFR
THRUST, LBS PF.KCENT
OR RATED
SHP
5000.00
1450.00
10770.00
11050.00
11600.00
7X0.00
T.O.
14
65
74
Bl
93
S
ENGINE
SPEED
RPM
NI
5770.00
7205.00
7515.00
7780.00
B250.00
7600.00
N2
9790.00
10810.00
linio.no
1120S.OO
1152S.OO
6530.00
MEASURED
FUEL
FLOH
LB/HR
2843.00
5250.00
6035.00
11205.00
8000.00
408.00
GAS GFN
AIR FLOW
LI/SEC
82.10
121.40
131.90
140.00
15J.OO
21. 40
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.009500
0.012100
o.ci3ono
0.013600
0.014300
n.nOHBOO
DEGREES F
-0.00
-0.00
-0.00
-o.on
-0.00
-o.oo
ENGINE
PRESSURE
RATIO
EPR
1.29
1.64
1.75
1.B5
2.04
1.04
TURBINF
INLET
TEMP
OFGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POKER EXHAUST
PERCENT GAS
RATFD TEMP
T.O. DEGREES F
34
65
74
81
93
5
700.00
855.00
900.00
915.00
995.00
675.00
F XHAUST
C,AS
PRESSURE
PSIA
38.61
48.61
51.87
54.83
59.80
31.27
cn
(WETI
PPMV
1 1.00
1 6. 60
14.10
12. K)
11. on
220.30
cc
2
IWFTI
PERCENT V
2.59
7.. 01
2.32
2.47
2.7?
0.67
ThC
IWETI
PPMV
i.eo
1.50
1.30
1.20
4.60
86.90
NG
(MET)
PPMV
1 6 7 . 00
87.20
1C5.00
121. 70
162.30
2.40
NO
2
IWETI
PPMV
8.60
7.30
7.70
8.90
9.70
5.40
NO
X
1 WET)
PPMV
175.60
94.50
112. BO
132.60
172.00
7.60
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
16.00
24.00
25.00
21.00
11.00
1.00
"ARTICULATES
-0.00
-0.00
12.00
14.00
16.00
-0.00
PDWFR
UFRCENT
RATED
T.O.
34
65
74
81
93
5
MASS F"l
CO
LP/IK
LB FUEL
0.15
1.65
1.21
1.03
O.HI
4B.fl4
M4SS FMI MISS Ifl
HC. NQ2
Lfl/lK LB/1K
LR C'JFL L8 FUEL
0.08
0.20
0.06
0.05
C.19
11.03
.01
. 19
.09
.18
.17
.97
"ASS EMI
C02
LR/IK
LB FUEL
3116.19
3114.61
1135.66
3115.98
3115.95
303C.71
PASS EMI
NO
IB/IK
LB FUFL
21. 14
14.22
1'.84
16.42
19.56
0.87
MASS CMI
NUX
LP/IK
LB FUEL
22.21
15.41
15.94
17.60
20.71
2.77
MASS HM1
cn
LB/HR
2.41
8. 65
7.12
1 1.50
6.46
44.35
MASS FPI
HC
LB/HR
0.23
1.04
0.39
0.62
1.55
10.0?
MASS FMI
NT.2
LB/HR
3.09
6.25
6.57
11.24
9. 15
1.79
MASS EMI
CO 2
Lfl/HR
6916.20
16456. 7C
18923.73
151)8.66
25087.57
2751.90
MASS f.»
NO
LB/HR
60. 10
74.64
89.53
183.97
156.49
0.79
M4SS EMI
NOX
Lfl/HR
63.20
80.88
96. 19
197.20
165.B4
2.51
POWER
PERCENT
RATED
T.O.
34
65
74
81
91
5
cn
LP/1KKTH-HR
0.4 H2
0.915
0.680
0.970
0.475
56.858
L1/1OTH-HU
17H1.?4C
1741.449
1757.078
2965.288
1844.675
3528.077
THC
Ltl/lK*TH-HK
0.045
0. 1 1 1
0.016
0.053
0. 114
12.845
17.02C
7.898
8.313
15.575
11.507
I .017
0.619
0.661
0.610
1.117
0.6RH
2.789
LB/1KKTH-HR
12.639
8.559
8.-til
16.642
12.194
3.222
IV-258
-------
C»L 10 NUMBER! 353 ENGINE TYPE »ND HDOEL1 JT-8D-9
TEST ORGANIZATION: PRATT C WHITNEY
SERIAL NUMBER I P-6T4550
MODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TA«I-IOLE
0.060
1.000
0.850
0.400
0.060
POWER
TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL USAGE TIME IN
RATE RATE NT FACTOR MODE
LB/HR LB/HR MIN.
40.473 929.537
4.577 8597.602
6.178 7138.484
26.024 3288.813
40.473 929.537
TOTAL FOR CVCLEl
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000X
.000
.000
.000
.000
.000
19.00
0.70
2.20
4.00
7.00
FUEL/CYCLE I
TH-HR/CYClEl
LB TH AT T.O.:
12
0
0
1
4
19
19
14
0
CO
MASS
LBS.
.816
.053
.227
.735
.722
.553
.869
.120
.368
FUEL
MASS
LBS.
294.35
100.31
261.74
219.25
108.45
984.10
LB CO / ENERGY
IK LB FUEL « TH-HR
43.541
0.532
0.865
7.913
43.541
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
TH-HR
0.04652
0.00032
0.00050
0.00449
0.04652
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.650
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
TH
870.0
14500.0
12325.0
5800.0
870.0
POWER
f TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR NODE
LB/HR LB/HR MIN.
8.500 929.537 .000 19.00
0.220 8597.602 .000 0.70
0.420 7138.484 .000 2.20
1.643 3288.813 .000 4.00
B.500 929.537 .000 7.00
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB FUEL/CYCLE!
LBS POLLUTANT/ IK LB TH-HR/CYCLE:
LBS POLLUTANT/ 1000K LB TH AT T.O.I
EMISSION FUEL USAGE TINE IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR NIN.
2.796 929.537 .000 19.00
197.465 8597.602 .000 0.70
131.913 7138.484 .000 2.20
34.64B 3288.813 .000 4.00
2.796 929.537 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK IB FUEL/CYCLE!
LBS POLLUTANT/ IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
HC
MASS
LBS.
2.692
0.003
0.015
0.110
0.992
3.811
3.872
2.752
0.177
NOX
MASS
LBS.
0.885
2.304
4.837
2.310
0.326
10.662
10.834
7.700
158.880
FUEL
MASS
LBS.
244.35
100.31
261.74
219.25
108.45
984.10
FUEL
MASS
LBS.
294.35
100.31
261.74
219.25
108.45
984.10
LB HC /
IK LB FUEL
9.144
0.026
0.059
0.500
9.144
LB NOX/
IK LB FUEL
3.008
22.967
18.479
10.535
3.008
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB HC /
1 TH-HR
0.00977
0.00002
0.00003
0.00028
0.00477
LB NQI/
TH-HR
0.00321
0.01362
0.01070
0.00597
0.00321
IV-259
-------
DATE: 8/30/71
TEST ORGANIZATION: PRATT L WHITNEY
ENGINE SUPPLIFR: PRATT AND WHITNEY
ENGINE OATS
C»L ID NUMBER: 357
ENGINE TYPF AND MODEL: JT-8D-9
SERIAL NUMBER:
RATED THRUST: 14500.
ENGINE TOTAL TIMF: -0. HRS
TIME SINCE HnT SECTION OVERHAUL: -0. HRS
TIMF SINCE:
NI COMPRESSOR OVERHAUL: -o. HRS
N2 COMPRESSOR OVERHAUL: -o. HPS
CDMBUSTDR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
Nl TURBINE OVERHAUL: -0. HRS
N2 TURPINF OVERHAUL: -0. HRS
FUEL: JP-4 FUEL H/C RATIO: 7.000
OPERATIONAL DATA «««»«»««*»»««««
INLET AIR TFMPERATUPE, DFGRFES F: START 87.00 FINISH
ATMOSPHERIC "RESSURF: START 29.80 FINISH
INLET AIH HUMIDITY, LBS H20/LB AIR: -0.0000
RELATIVE HUMIOITY: -0.00 PERCENT
SAMPLE LINE: TEMPERATURE, OFGRFES C: 150.00, rLOH PATE, LITFPS/M1N:
SAMPLE LINF TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 6
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES HG
SMOKE DENSITY IS VON BRAND MEASURE
87.OC
79.76
CLOCK
TIME
1359.00
1438.00
1714.00
1531.00
1541.00
1301.00
TFST
MOOE
I/ 0
M 1
4/ 3
5/ 4
6/ 5
7/ 4
7.518
8.819
10.161
LB/IK#TH-HR
1.074
I.62R
0.754
0.725
0.824
0.816
NO
X
LB/IKKTH-HR
4.985
1 .689
r.4ia
8.243
9.643
10.977
IV-260
-------
CAL 10 NUMBER 1 357 ENGINE TYPE AND MODEL: JT-6D-9
TEST ORGANIZATION: PRATT t WHITNEY
SERIAL NUMBER:
MODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
0.060
1.000
0.850
0.400
0.060
POWER
TH
670.0
14500.0
12325.0
5600.0
670.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
29.299 908. 1B9
3.432 8798.668
5.425 7390.512
13.595 3364.328
29.299 908. 169
USAGE TIME IN
WT FACTOR MODE
M1N.
TOTAL FOR CYCLE:
L8S POLLUTANT/IK LB
LSS POLLUTANT/IK LB
LBS POLLUTANT/1000K
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.650
0.400
0.060
POWER
TH
670.0
1*500.0
12325.0
5800.0
670.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
2.812 908.169
0. 735 6798.668
0.926 7390.512
1.169 3364. 328
2.612 906.189
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLIUTANT/IOOOK
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
1 TH
670.0
14500.0
12325.0
5600.0
870.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.875 908.169
177.574 8798.668
125.448 7390.512
31.436 3364.328
1.875 908.189
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE;
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TM-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
9.276
0.040
0.199
0.906
3.418
13.842
13.961
9.996
0.276
HC
MASS
LBS.
0.891
0.009
0.034
0.078
0.328
1.339
1.351
0.967
0.591
NOX
MASS
LBS.
0.594
2.072
4.600
2.096
0.219
9.580
9.662
6.916
142.876
FUEL
MASS
LBS.
287.59
102.65
270.99
224.29
105.96
991.47
FUEL
MASS
LBS.
287.59
102.65
270.99
224.29
105.96
991.47
FUEL
MASS
LBS.
287.59
102.65
270.99
224.29
105.96
991.47
IB CO /
IK LB FUEL
32
0
0
4
32
.261
.390
.734
.041
.261
LB HC /
IK LB FUEL
3
0
0
0
1
.097
.084
.123
.348
.097
LB NOX/
IK LB FUEL
2
20
16
9
2
.064
.162
.974
.344
.064
ENERGY
> TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1364.75
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1364.75
LB CO /
f TH-HR
0.03368
0.00024
0.00044
0.00234
0.03366
LB HC /
TH-HR
0.00323
0.00005
0.00006
0.00020
0.00323
LB NOX/
1 TH-HR
0.00215
0.01225
0.01018
0.00542
0.00215
IV-261
-------
0*TEl 7/ 9/71
TEST ORGANIZATION: PRATT C WHITNEY
ENGINE SUPPLIER: PRATT AND XMITNFY
ENGINE 01T«
C»L ID NUMBER: 39?
ENGINE TYPE AND MODEL: JT-80-9
SERIAL NUMBER:
RATED THRUST: 14500.
ENGINE TOTAL TIME: -0. MRS
TIME SINCE HOT SECTION C1VERHAUL: -0. MRS
TIPE SINCE:
NI COMPRESSOR OVERHAUL: -o. MRS
NZ COMPRESSOR OVERHAUL: -o. MRS
COMBUSTOR CAN REPLACEMENT: -0. MRS
FIRST STAGF NOZZLE GUIDE VANF OVERHAUL: -0. MRS
NI TURBINE OVERHAUL: -o. HRS
NZ TURBINE OVERHAUL: -o. HRS
FUEL H/C PATIO: 2.000
96.00
29.96
FUEL; JP-4C
OPERATIONAL DATA «««««
INLFf AIR TEMPERATURE, DEGREES F: START 96.00 FINISH
ATMOSPHERIC PRESSURE: START 29.96 FINISH
INLFT AIR HUMIDITY, LRS H20/LB AIR: 0.0099
RELATIVE HUMIDITY: -0.00 PERCEN1
SAMPLE LINE: TEMPERATURE, CECREES C: 150.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 8
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES HG
SMOKF DENSITY IS VON BRAND MEASURE PARTICULARS ARE IN MO/M»»3
2.00
CLOCK
TIME
1190.00
1321.00
1311.00
1145.00
1190.00
1410.00
1441.00
1507.00
TFSf
MODE
I/ 0
II 1
3/ 2
4/ 1
5/ 4
6/ 5
7/ 6
9V 7
POWER
THRUST, LBS
OR
SHP
1100.00
680.00
1600.00
5000.00
9050.00
10350.00
11550.00
13100.00
PERCENT
RATED
T.O.
7
4
11
34
62
71
79
90
ENGINE
SPEED
R
Ml
3040.nc
7439.00
3590.00
5775.00
7100.00
7410.00
7715.00
PI 15.00
PM
N2
7325.00
6420.00
BC60.00
9030.00
10900.00
11125.00
11340.00
Ili90.00
MEASURED
FUEL
FLOW
LR/MR
1127.00
990.00
1427.00
2894.00
5090.00
5B65.00
6677.00
7815.00
GAS GEN
MR FLOW
LB/SEC
33.50
27.60
39. 70
71.50
115.90
123.70
1313.00
141.70
CALC
fit.
O.OD9JOO
0.009200
0.009900
0.011200
0.017200
0.013200
0.014100
0.015100
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-o.oo
FNGINE
PRESSURE
RATIO
EPR
1.05
1.03
1.08
1.10
1.60
1.71
1.83
1.9B
TUR8INC
INLFT
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.ll.
7
4
II
14
62
71
7O
90
EXHAUST
GAS
TFMP
DEGREES f
710.00
730.00
745.00
715.00
B50.00
895.00
940.00
1000.00
F XMAUST
GAS
PRESSURE
PSIA
1145.00
30.76
32.15
18. 51
47.36
50.5?
53.90
58.08
r.o
IWETI
PPMV
156.40
277.30
I 10.90
47.10
17.90
14.10
12.10
10.50
CO
2
1 HE 1 )
PERCENT V
1.14
1. 14
1.75
1.51
2.09
2.23
2. )l
2.48
TMC
IWFTI
PPMV
35.40
115.60
19. 10
5.30
0.10
0.20
4.30
2.7C
NO
1 WE T I
PPMV
10.70
8.50
11.60
32.60
80.00
99.40
116.90
1?9. in
NC
2
( WE T 1
PPMV
3.00
5.10
3.40
5.60
5.20
5.90
7.90
7.50
NO
X
(WFTI
PPMV
13.70
13.60
17.00
38.20
85.20
105.10
174.80
166.60
ALDEHYDES
-0.00
30.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
1.00
1.00
7.00
12.00
24.00
26.00
27.00
30.00
PARTICULATFS
-0.00
-n.oo
-0.00
-0.00
-0.00
13.00
14.00
16.00
POWER
PERCENT
RATED
T.O.
II
14
62
71
79
IASS EMI
r.O
L8/1K
LB FUEL
26.94
46.96
17.52
6.15
1.71
1.26
1.11
0.85
MASS E'4I
HC.
L8/IK
LH tUEL
3.49
1 1.21
1. 73
0.39
0.02
0.01
0.21
0. 12
MASS EMI
NT?
LB/1K
LB FUFL
0.85
1.42
0.89
1.20
O.B2
0.87
1.12
0.99
MASS EMI
C02
LB/1K
IB FU E L
3095.83
101:1.21
3105.47
3127.00
3115.02
1115. 73
3115.41
1116.07
MASS EMI
NH
LR/IK
LB FUEL
3.03
2.36
3.51
6.97
12.54
14.61
16.59
71.03
MASS EMI
NOX
LP/1K
LB FUEL
3.88
3.78
4.4?
8.16
13.36
15.4"
17.71
22.0,.
MASS EM|
CO
LR/HK
10.21
41.79
25.00
17.74
8.70
7.40
7.44
6.60
MASS EMI
HC
L9/HR
3.97
9.98
2.47
1.14
0.08
0.06
1.42
0.97
MASS FMI
NII2
L6/HR
0.95
1.26
1.26
3.45
4. 15
5.09
7.48
7.75
MASS EMI
CO 2
LB/HR
1462.30
2699.56
4431.51
9013.25
15957.22
18391.08
20935.13
245GB. 42
MASS EMI
NO
LB/HR
3.4C
2.10
5.04
20.09
63.85
85.70
110.75
164.37
MASS EMI
NOX
LB/t-K
4.35
1.37
6.10
23.54
68.00
90.79
118.24
172.12
POWER
PERCENT
RATED
T.n.
II
14
62
71
79
90
en
LP/IKfcTH-HR
27.4BJ
61.460
15.625
3.549
0.961
0. 715
0.644
0.504
LB/IK« TH-HR
3147.548
1969.V37
2769.693
1801.651
1761.229
1776.916
1812. 565
1870.872
TMC
LB/lMTH-Ha
i.563
14.674
1.543
0.778
0.009
0.006
0. 123
0.074
NO
L8/1MTH-HR
3.CB8
3.094
3.150
4.019
7.056
8.280
9.589
17.547
NO
?
LH/IKITH-HR
0.866
1.B57
0.789
0.690
0.459
0.491
0. 648
0.591
NO
X
Lfl/lKITH-HR
3.954
4.951
1.938
4.7C8
7.514
8.771
10.237
13.139
IV-262
-------
CAL 10 NUMBER! 392 ENGINE TYPE AND MODEL 1 JT-80-9
TEST ORGANIZATION: PRATT t UHITNEV
SERIAL NUNBERl P674552
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE
IB/MR LB/HR
32.660 991.122
2.205 6698.324
4.731 7333.910
16.311 3293.130
32.660 991.122
USACE TIME IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAX-IDLE
TAKEOFF
CLIH80UT
APPROACH
TAXI-IDLE
FRACTIONAL
POMER
0.060
1.000
0.850
0.400
0.060
POWER
TH
870.0
14500.0
12325.0
5800.0
BTO.O
EMISSION FUEL
RATE RATE
LB/HR LB/HR
7.153 991.122
0.506 8698.324
0.527 7333.910
1.102 3293.130
7.153 991.122
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
NODE
FRACTIONAL
POWER
TAXI-IOLE 0.060
TAKEOFF 1.000
CLINBOUT 0.850
APPROACH 0.400
TAXI-IOLE 0.060
POWER
TH
670.0
14500.0
12325.0
5600.0
670.0
EMISSION FUEL
RATE RATE
LB/HR L8/HR
3.626 991.122
229.109 8698.324
146.356 7333.910
29.997 3293.130
3.626 991.122
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE l
TH-HR/CYCLEl
LB TH AT T.O.:
USACE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR NODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
10.342
0.026
0.173
1.087
3.810
15.439
15.145
11.149
0.177
HC
MASS
LBS.
2.265
0.006
0.019
0.073
0.835
3.199
3.138
2.310
0.409
NOX
MASS
Las.
1.148
2.673
5.366
2.000
0.423
11.611
11.389
8.385
184.340
FUEL
MASS
LBS.
313.86
101.48
268.91
219.54
115.63
1019.42
FUEL
MASS
L8S.
313.86
101.46
268.91
219.54
115.63
1019.42
FUEL
MASS
LBS.
313.86
101.48
268.91
219.54
115.63
1019.42
LB CO /
IK LB FUEL
32.952
0.253
0.645
4.953
32.952
LB HC /
IK LB FUEL
7.217
0.058
0.072
0.335
7. 217
LB NOX/
IK LB FUEL
3.659
26.339
19.956
9.109
3.659
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB
0
0
0
0
0
LB
0
0
0
0
0
LB
0
0
0
0
0
CO /
TH-HH
.03754
.00015
.00038
.00281
.03754
HC /
TH-HR
.00822
.00004
.00004
.00019
.00822
NOX/
TH-HR
.00417
.01580
.01187
.00517
.00417
IV-263
-------
0»TE: 7/14/71
TEST ORGANIZATION: PRATT i WHITNEY
ENGINF SUPPLIER: PRATT AND WHITNEY
ENGINE DATA
CAL ID NUHBFR: 394 ENGINE TYPE AND MODEL: jr-ao-9
RATED THRUST: 14500.
ENGINE TOTAL TIME: -0. HAS
TIME SINCE HOT SECTION OVERHAUL: -0. MRS
TIME SINCE:
MI COMPRESSOR OVERHAUL: -o. MRS
N2 COMPRESSOR OVERHAUL: -0. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
NJ TURtiNE OVERHAUL: -o. HRS
FUFL: jp-4C FUEL H/C RATIO: 2.000
OPERATIONAL DATA «»«»»«»«»»««
INLF.T AIR TEMPERATURF, DEGREES F: START 78.00 FINISH 80.00
ATMOSPHERIC PRESSURE: START 29.59 FINISH 79.58
INLET AIR HUMIDITY, LEtS H20/LB AIR: 0.0109
RELATIVE HUMIDITY: -o.oo PFRCENT
SAMPLE LINE: TEMPERATURE, OEGRFES C: 150.00, FLO* RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TFSTS: 8
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES HG
SMOKE DENSITY IS VON BRAND MEASURE PARTICULATFS ARE IN MG/M««3
SERIAL NUMBER: P-665705
CLOCK
TIME
TEST
MODE
POWER
THPUST.LBS PERCENT
OR RATED
SHP
1119.00
1124.00
1138.00
1142.00
1252.00
1303.00
1921.00
1 J39.00
I/ 0
7.1 1
3/ 2
>,/ 3
5/ 4
hi 5
7/ 6
B/ 7
690
1250
1740
5000
9470
10700
11720
13660
.00
.00
.00
.00
.00
.00
.00
.00
T.O.
4
a
11
34
65
73
BO
94
ENGINF
SPEFO
RPM
NI
24io.no
3190.00
3695.00
5750.00
7165.00
7440.00
76H5.00
82CO.OO
12
6360.00
7515.00
8130.00
9630.00
10860.00
11060.00
11230.00
11560.00
MEASURED
FUEL
FLOW
LB/HR
B79.00
1IB9.00
1487.00
2861.00
5340.00
6040.00
6700.00
3120.00
GAS GEN
AIR FLOW
LB/SEC
27.50
36.20
42.10
85.20
121 .00
17B.OO
135.30
149. .30
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.008900
O.OU9100
0. 009BOO
0.009300
0.012300
0.013100
0.013800
0.015100
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPK
1.03
1.06
1.09
1.30
1 .66
1.76
1.85
2.04
TURBINE
INLFT
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
POWER FXHAUST
PERCENT CAS
BATED TEMP
T.O. DEGREES I
II
34
65
73
80
94
720.00
705.00
715.00
695.00
855.00
900.00
935.00
1005.00
EXHAUST
GAS
PRESSURE
PSIA
30.58
31.38
32. 18
3B.26
48. 19
M.17
53.66
59.23
co
(MET 1
PPMV
215. 3P
119.50
100.60
43.30
1 7.30
14.30
12.70
10.30
CO
2
l.tTI
PtRCFNT V
C.93
0.98
1.13
1.42
?.10
2.23
2.34
2.64
THC
1WFT)
PPMV
81.30
30.70
16.10
4. 10
1.50
1.10
1.7C
1. 80
NO
IWETI
PPMV
5.60
6.9C
10.90
29.30
7R.30
96.60
11B.30
170.20
NO
2
IWETI
PPMV
1.00
2.20
2.00-
4.60
4.60
5.80
3.90
7.30
NO
X
IHETI
PPMV
6.60
9.10
12.90
33.90
82.90
102.40
122.20
177.50
ALDEHYDES SMOKF PARTICULATES
5.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
2.00
6.00
5.00
13.00
-0.00
24.00
24.00
24.00
-0.00
-0.00
-0.00
-0.00
-o.on
-o.oo
12.00
12.00
PUWER
PERCENT
RATFO
T.O.
II
34
65
73
MASS FMI
Cn
LR/IK
LB FUFL
44. dO
73.99
1 7. SO
6. 14
1.64
1.28
1.01
0.76
MASS EMI
HC
IB/ IK
LB FUEL
1.69
3.5t
1.61
n.33
0.08
0.06
0.08
0.06
MASS F»l
NO 2
L9/ 1 K
L3 FUEL
1.34
0.73
0.57
1.06
0.72
0.65
0.55
0.91
MASS FMI
CD?
Lfl/K
LO FUEL
3040.77
3090.38
3105.67
3127.20
3134.94
3135.56
3135.31
3136. 31
MSS FMI
NO
IP/IK
LK FUFL
1.91
2.27
3. 13
6.75
12.22
14.70
16.57
71.14
MASS HMI
NOX
L6/1K
LR FUFL
7.76
3.00
3.71
7.60
12.94
15.05
17.12
22.04
MASS E"l
CO
LB/HR
35.38
78.52
26.17
1 7.56
B./s
7.73
7.26
6.32
MASS FMI
HC
LH/HF
8.5?
4.20
2.40
0.94
0.44
0.34
0.56
0.63
MASS FMI
N02
L9/HH
0.30
0.86
0.85
3.03
3.33
5.15
3.66
7.36
MASS EMI
CO 2
LU/HR
2672.63
3674.46
4618.13
8946.91
16740.57
18936.91
21009.96
25466.61
MASS EMI
NO
Lfl/HR
1.68
2.7C
4.66
19.30
65.25
85.76
111.04
171.64
MASS FMI
NOX
LB/HR
1.93
3.57
5.51
27.33
69.09
90.91
114.70
179.00
POWER
PbRCFNT
RATED
T.O.
B
II
34
65
73
60
94
CO
1K«TH-HR
57.075
22.613
15.031
3.513
0.977
0.722
0.619
0.4U3
L8/ IK«TH-HR
3871.612
29 39.569
2654.100
1789.383
1767.747
1769.991
1792.659
1864.135
THC
LH/IK*IH-HR
12.343
3.357
1.378
0. 198
0.046
0.032
0.047
0.046
NO
LB/IKCTH-MH
2.43P
2. 164
2.676
3.860
6.690
K.015
9.474
12.565
LB/1K«TH-HR
0.435
n.r,90
0.491
0.606
0.405
0.481
0.312
0.539
LB/1K»TH-HR
2.874
2.954
3.167
4.466
7.295
8.497
9.767
13.104
IV-264
-------
CAL ID NUMBER: 394 ENGINE TYPE AND MODELi jT-go-9
TEST ORGANIZATION! PRATT C WHITNEY
SERIAL NUMBER: p-6657os
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
I. 000
0.850
0.400
0.060
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
FRACTIONAL
POHEK
0.060
1.000
0.850
0.400
0.060
POWER
f TH
870.0
14500.0
12325.0
5800.0
870.0
POWER
1 TH
870.0
14500.0
12325.0
5800.0
870.0
POWER
TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
32.759 992.664
3.174 8600.570
5.686 7253.199
16.478 3211.089
32.759 992.669
TOTAL FOR CYCLE!
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
6.495 992.664
0.332 8600.570
0.350 7253.199
1.017 3211.089
6.495 992.669
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE NT
LB/HR LB/HR
2.237 992.669
211.123 8600.570
136.287 7253.199
27.182 3211.089
2.237 992.669
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
USAGE TIME IN
FACTOR MODE
NIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
NIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
NIN.
1.000 19.00
1.000 0.70
1.000 2.20
1.000 4.00
1.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
tO. 374
0.037
0.208
1.099
3.822
15.540
15.378
11.222
0.255
HC
MASS
LBS.
2.057
0.004
0.013
0.068
0.758
2. 899
2.869
2.094
0.267
NOX
MASS
LBS.
0.708
2.463
4.997
1.812
0.261
10.242
10.135
7.396
164.869
FUEL
MASS
LBS.
314.34
100.34
265.95
214.07
115. Bl
1010.52
FUEL
MASS
LBS.
314.34
100.34
265.95
214.07
115.81
1010.52
FUEL
MASS
LBS.
314.34
100.34
265.45
214.07
115.81
1010.52
LB CO /
IK LB FUEL
33.001
0.369
0.7B4
5.132
33.001
LB HC /
IK LB FUEL
6.543
0.0)9
0.048
0.317
6.543
LB NOX/
IK LB FUEL
2.253
24.548
18.790
8.465
2.253
ENERGY
f TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
LB CO /
TH-HR
0.03765
0.00022
0.00046
0.00284
0.03765
LB HC /
1 TH-HR
0.00747
0.00002
0.00003
0.00018
0.00747
LB NOX/
1 TH-HR
0.00257
0.01456
0.01106
0.00469
0.00257
IV-265
-------
I)»TF: 7/15/71
TEST ORGANIZATION: PRATT f, UHITNEY
ENGINE SUPPLIER: PRATT AND HHITNEV
ENGINE DATA
C»L 10 NUMBER: VIS ENGINE TYPE AND MDOEL: JT-8D-9
RATED IMRUST: 14500.
ENGINE TOTAL TIHE: -0. HPS
TIME SINCE HOT SECTION OVERHAUL: -0. MRS
TIHE SINCF:
NI COIPRESSOR OVERHAUL: -o. MRS
N2 COMPRESSOR OVERHAUL: -o. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGF NUZZLE GUIDE VANE OVERHAUL! -0. HRS
Nl TURBINE OVERHAUL: -0. H8S
N2 TURBINE OVERHAUL: -0. HPS
SERIAL NUMBER:
FUEL H/C RATIO: 2.000
75.00
29.76
FUEL: -IP-*
OPERATIONAL 0AM +»******«*««»«**»******»*
INLET AIR TEMPERAIUKE, DEGREES F: START 70.00 FINISH
ATMOSPHERIC PRESSURE: START 29.76 FINISH
INLFT AIR HUMIDITY, L8S H20/LB AIR: 0.01CJ
RELATIVE HUMIDITY: -0.00 PERCENT
SAMPLF LINE: TEMPERATURE, DEGRFFS C: 150.CC, FLOU RATE, LITFRS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: B
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES HG
SMOKE DENSITY IS VON BRAND MEASUXF PARTICULATES AltE IN MG/M««3
CLOCK
TIME
TEST
MODF
POKER
THPUST.LRS PF.KCFNT
OR HATFO
SHP
921.00
933.00
943.00
950.00
1 101.00
111). 00
1129.00
1 140.00
I/ 0
11 1
I/ 2
<,/ 3
7/ 4
8/ 7
9/ B
hi 1
720
l?20
1720
5000
10800
11850
13600
9540
.00
.00
.00
.00
.00
.00
.00
.00
T.n.
4
M
1 1
34
74
Bl
93
65
ENG INF
SPEf:D
8PM
Ml
2425.00
3150. OC
36RO.OO
5735.00
7450.00
7680.00
ai60.no
7150.00
N?
6340.00
7405.00
8060.00
9770.00
11035.00
11 175.00
11500.00
IOH40.00
MEASUSEO
FUFL
FLU*
L3/HR
872.00
11J9.00
14R1 .00
2869.00
6065.01
6780.00
8010.00
5275.00
GAS GEN
AIR FLC1W
Lfl/SEC
28.00
36.30
42.50
86.60
129.90
137.40
150.90
122.00
CALC COMPRESSOR
F/A DISCHARGE
TFMP
0.009600
0.009020
0.009680
0.009190
0.012970
0.013600
0.014700
0.012000
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINF.
PRESSURE
RATIO
EPR
1.03
1.06
1.09
1.30
1 .75
1.85
2.02
1.64
TURBINE
INLFT
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.n.
fl
11
34
74
01
93
65
F XHAUST
GAS
TFMP
DFGREFS F
700.00
705.00
720.00
690.00
890.00
920.00
990.00
840.00
FKHAUST
CAS
PRESSUar.
PSIA
30.75
11.55
12.J5
31.31
51.25
54.13
58.90
'8. 16
CO
I.ETI
PP*V
216.70
118.10
93.40
46.80
14.50
17.50
10. tO
1 7.00
CO
2
IxFTI
PFRCENT V
0.'17
0.99
1.07
1.40
2.26
8. 30
a. 10
8.70
THC
IMFT)
PPMV
75.30
14.20
3.70
6.50
2.00
5.80
6.7C
>.90
Nn
IhETI
PPMV
3.20
5.HO
fl.70
21". 80
99.70
120.PO
165.30
B5.90
NO
2
IMF. Tl
PPMV
3.80
4.50
3.00
7.20
7.80
8. 30
9.10
8.20
KU
X
IMETI
PPMV
7.00
10.30
11. 10
36.00
101.50
1 211. 30
173.40
94.10
ALDEHYDES SMOKC PART1CULATCS
5.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
1.00
2.00
1.00
12.00
24.00
27.00
29.00
-0.00
-o.oo
-0.00
-0.00
-0.00
12.00
14.00
14.00
-c.oo
PUWER
PERCENT
UATED
T.O.
B
II
34
74
81
93
65
ASS EMI
cn
LI/IK
LD FIJCL
43.31
23.55
17.2"
6.29
I . ?8
0. 30
0.77
0.41
MASS EMI
HC
LB/1K
LB FUEL
H.*,2
1.62
0.39
0.50
0.10
0.08
0.09
0.05
MASS FMI
N02
LB/1K
LB FUU
1 .25
1 .47
0.91
1.59
1.13
0.33
n.33
0. 31
MASS E"l
CO 2
LH/ 1 K
LB FUEL
3046.05
3096.31
3109.53
3126.49
3135.46
3137.05
3137.06
3136.94
MASS tMI
NO
LB/1K
LB FUEL
1.05
1.90
2.64
6.36
14.46
4.74
6.69
3.44
MASS EMI
NUX
LP/1K
LB FUFL
7.30
3.37
3.55
7.95
15.59
5.07
7.02
3.76
MASS EM
en
LB/t-K
37.77
27.76
25.58
1 8.05
7.77
2.04
2.13
2.18
MASS EMI
HC
LB/HR
7.52
1.91
0.56
1.44
0.61
0.54
0.29
MASS EMI
N02
LB/HR
MASS EMI
C02
LB/HR
MASS t
MO
MASS EMI
NdX
LC/KR
1.09
1.73
1. 35
4.56
6.86
2.27
7.63
1.73
2656.15
3650.55
4605.21
8969.89
19016.54
21269.20
25127.88
16547.38
0.92
2.24
3.91
u.25
87.70
J2.I5
53.61
18.12
2.00
3.97
5.76
77. PI
^4.56
34.37
56.23
19.85
POWER
PERCENT
RATEP
T.O.
I I
34
74
81
93
65
r.o
Lfl/KTH-HR
52.453
22 . 7 5 7
14.875
3.610
0.719
0.172
0.157
0.??9
LB/ 1KKTH-HR
3689.103
2992.253
2677.449
1793.971!
1 760.740
1794.870
1847.638
1734.526
THC
Lfl/IKIrTM-HR
10.439
1.564
0.337
0.787
0.057
0.046
0.056
0.030
LH/ltc* IH-MH
1.272
1 .833
7.276
3.649
8.120
2.71 )
3.942
1 .900
LR/IK> TH-HR
1.511
1.422
0.785
0.912
0.635
0.188
0. 193
0. 181
NO
X
LH/IKiTH-HR
2.783
3.254
3.061
4.562
8.756
2.900
4.135
2.081
IV-266
-------
CAL 10 NUNBERI 395 ENGINE TYPE AND NODEII JT-8D-9
TEST ORGANIIATIONi P««TT t KHITNEY
SERIAL NUNBERl P-665706
MODE FRACTIONAL
POKER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
0.060
1.000
O.B50
0.400
0.060
POKER
i TH
870.0
1*500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
11.002 949.518
0.564 8544.902
1.913 7198.484
14.942 1322.161
31.002 949.318
USAGE TIME IN
KT FACTOR KOOE
MIN. .
TOTAL FOR CrCLEl
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IOOOK
NODE FRACTIONAL
POKER
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
0.060
1.000
O.B50
0.400
0.060
POKER
TH
870.0
14500.0
12325.0
3800.0
870.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
5.558 949.518
0.102 8544.902
0.482 7198.484
1.256 3322.161
5.558 949.518
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLCl
IB TH AT T.O.:
USAGE TIME IN
KT FACTOR MODE
MIN.
TOTAL FOR CYCLEi
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
MODE FRACTIONAL
POKER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
0.060
1.000
0.850
0.400
0.060
POKER
1 TH
870.0
14500.0
12325.0
5800.0
870.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
2.328 949.518
182.490 8544.902
129.129 7198.484
28.989 3322.161
2.328 949.518
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLEI
TH-HR/CYCLE:
LB TH AT T.O.I
USAGE TIME IN
KT FACTOR MODE
MIN.
TOTAL FOR CYCLE!
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK IB
LBS POLLUTANT/IOOOK
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYClEl
TH-HR/CYCLEI
LB TH AT T.O.:
CO
MASS
LBS.
9.817
0.007
0.070
0.996
3.617
14.507
14.557
10.476
0.045
HC
MASS
LBS.
1.760
0.004
0.018
0.084
0.648
2.514
2.S22
1.815
0.241
NOX
MASS
LBS.
0.737
2.129
4.742
1.933
0.272
9.812
9.846
7.086
146.831
FUEL
MASS
LBS.
300.68
99.69
263.94
221.48
110.78
996.57
FUEL
MASS
LBS.
300.68
99.69
263.94
221.48
110.78
996.37
FUEL
MASS
LBS.
300.68
99.69
263.94
221.48
110.78
996.57
IB CO /
IK LB FUEL
12.651
0.066
0.266
4.498
12.651
LB HC /
IK LB FUEL
5.854
0.035
0.067
0.378
5.854
LB NOX/
IK LB FUEL
2.451
21.357
17.966
8.726
2.451
ENERGY
1 TH-HR
275.50
169.17
451.92
386.67
101.50
1384.75
ENERGY
1 TH-HR
273.50
169.17
451.92
386.67
101.30
1384.75
ENERGY
1 TH-HR
275.50
169.17
451.92
186.67
101.50
1384.75
LB
*
CO /
TH-HR
. 0.03563
0.00004
0.00016
0.00258
0.03363
LB
0
0
0
0
0
LB
t
0
0
0
0
0
HC /
TH-HR
.00639
.00002
.00004
.00022
.00639
NOX/
TH-HR
.00268
.01259
.01049
.00300
.00268
IV-267
-------
0»TEl T/16/71
TEST ORGANIZATION! PR1TT ( WHITNEY
ENGINE SUPPLIER I PRATT AND WHITNEY
ENGINE DATA
CAL 10 NUMBER: 396 ENGINE TrPE AND HODEl: JT-80-9
RATEO THRUST: 14500.
ENGINE TOTAL TIME: -0. MRS
TIME SINCE HOI SECTION OVERHAUL: -0. HRS
TIME SINCEl
SERIAL NUMBER:
Nl COMPRESSOR OVERHAUL: -0. MRS
HZ COMPRESSOR OVERHAUL! -0. HRS
COMBUSTOK CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIHE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
N2 TURBINE OVERHAUL: -o. HRS
FUEL H/C RATIO: 2.000
FINISH
FINISH
84.00
29.87
FUEL! JP-4
OPERATIONAL DATA «««
INLET AIR TEMPERATUREt DEGREES F: START 80.00
ATMOSPHERIC PRFSSURF: START 29.86
INLET AIR HUH[01 TV, LBS H20/L9 AIR: 0.0099
RELATIVE HUMinlTv: -0.00 PERCENT
SAMPLE LINE! TEMPERATURE! DEGRFES C: 150.OC, FLOW RATE, LITERS/MIX:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 6
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES HG
SMOKE DENSITY IS VHN BRANO MEASURE PARTICULARS APE IN NG/N«»3
CLOCK
TINE
1126.00
3142.00
1218.00
1212.00
1241.00
1301.00
TEST
Nans
I/
2/
3/
4/
5/
6/
0
I
2
I
4
5
THRUST
OR
SHP
5100.
740.
9500.
10750.
11950.
13650.
POWER
.LBS PERCENT
RATED
00
00
00
00
00
no
T.O.
35
5
65
74
82
94
ENGINF
SPEED
RPM
Nl
57B5.00
2615.00
71AC.OO
7440.00
7725.00
0160.00
N2
9900
6675
10935
11140
I1J40
11635
.00
.00
.00
.00
.00
.00
MEASURED
FUEL
FLOW
L8/HR
2911.00
899.00
5340.00
6106.00
6875.00
9130.00
GAS GEN
AIR FLOW
LB/SFC
66.20
29.40
119.90
127.90
135.70
148.30
CALC
F/A
O.C09400
0.00«500
0.012400
0.013300
0.014100
0.015200
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIO
DEGREES F EPR
-0.00
-o.no
-0.00
-0.00
-0.00
-0.00
1.30
1.04
1.63
1.75
1.85
2.02
TURBINE
INLET
TFMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
-0.10
POWER
PERCENT
RATED
T.O.
35
5
65
74
82
94
EXHAUST EXHAUST
GAS GAS
TEMP PRESSURE
DEGREES F PSIA
705.00
685.00
860.00
900.00
940.00
995.00
3B.61
30.95
4S.I 7
51.36
54.44
59.12
CO CO
(WETI 2
PPMV IUET)
PERCENT v
44.80
227.70
17.40
n.so
12.00
10. (0
1.46
0.95
2.11
2.?7
2.45
2.74
THC
IWCTI
PPHV
6.00
102.10
3.30
4.60
3.20
1.90
NO NO
IWET1 2
PPMV IWETI
PPMV
ALDEHYDES SNOKF PARTICULATES
30.90
7.20
S5.30
105.90
131.60
174.50
6.10
4.70
7.80
a. no
9.70
10.40
I WET I
PPMV
37.00
11.40
93. (0
114.70
141.50
IB4.90
-0.00
7.00
-0.00
-0.00
-0.00
-0.00
15.00
1.00
19.00
21.00
23.00
25.00
-0.00
-0.00
-0.00
10.00
12.00
12.00
POWER
PERCENT
RATED
T.O.
35
5
65
74
82
94
MASS EMI NASS ENI
CO HC
LB/1K LB/1K
LB FUEL LB FUEL
6.11
46.26
1.65
1.21
0.98
0.75
NASS FNI NASS EMI NASS EMI
NO 2 C02 NO
LH/IK LB/1K LB/1K
LR FUFL LB FUEL LB FUEL
0.47
ii.an
0.18
0.23
0.15
O.OB
3126.87
3032.47
3134.67
3135.20
3135.80
.24 3136.35
6.92
2.40
13.25
15,29
17.64
20.88
HASS Etl
N0>
LB/1K
LB FUFL
8.2R
3.97
14.46
16.56
IP. 93
22.13
NASS FHI
CO
LB/HR
17.78
41.59
8.79
7.41
6.72
6.10
NASS EM
HC
LB/HR
1.36
10.6K
0.95
1.41
1.03
0.64
NASS tHI
NO 2
LB/HR
3.98
1.41
6.47
7. 74
H.92
MASS EMI
C02
LB/HR
9102.30
2726.19
16739.13
19143.54
21558.62
10.12 25498.49
MASS EMI
NO
LB/HR
20.14
2.16
70.74
93.36
121.24
169.76
MASS EMI
HOt
LB/HR
24. II
3.57
77.21
101.12
130.16
179.88
POWER
PERCENT
RATED
T.O.
35
5
45
74
82
94
CO
L8/1K«TH-HO
3.4B6
56.199
0.925
0.689
0.562
0.447
1794.766
3684.041
1762.014
1710.795
1S04.068
1868.021
THC
1.B/1K«TH-HR
0.267
14.432
0.100
0. 132
0.086
0.047
NO
Lfl/lKKTM-HR
3.949
2.919
7.447
8.6B5
10.146
12.437
LB/lKtTH-HR
0.780
1.905
0.6X1
0.722
0.747
0.741
NO
X
LB/1K«TH-HR
4.728
4.824
8.128
9.407
10.892
13.178
IV-268
-------
CAL ID NUNBERI 996 ENGINE TYPE AND NODEL I JT-BD-9
TEST ORGANIZATION! PRATT ( KHITNEY
SERIAL NUNBERI P-66S708
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.060
1.000
0.830
0.400
0.060
POKER
1 TH
STO.O
14900.0
12321.0
9800.0
B70.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
40.029 96T.9T4
9.033 8T07.441
9.883 T332.4T7
17.3TT 3342.371
40.029 967.9T4
USAGE TIME IN
KT FACTOR MODE
MIN.
TOTAL FOR CYCLEl
LBS POLLUTANT/ IK LB
IBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
NODE
TAXI-IDLE
TAKEOFF
CLIN90UT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.060
1.000
0.950
0.400
0.060
POWER
1 TH
870. 0
14900.0
12329.0
9800.0
670.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
9.190 967.974
0.209 8TOT.441
0. 370 7332.477
1.249 3342.371
9.190 967.974
KI
TOTAL FOR CYCLEl
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.060
1.000
0.8 90
0.400
0.060
POKER
1 TH
870.0
14900.0
12329.0
9800.0
870.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
3.993 967.974
208.963 B707.441
149.999 7332.477
30.369 3342.371
3.933 967.974
KT
TOTAL FOR CYCLEl
IBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE I
TH-HR/ CYCLEl
LB TH AT T.O.I
USAGE TIME IN
FACTOR NODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CVCLEi
TH-HR/CYCLEi
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLEI
18 TH AT T.O.:
CO
MASS
LBS.
12.676
0.099
0.216
1.198
4.670
18.779
18.943
13.361
0.409
HC
MASS
LBS.
2.89B
0.002
0.014
0.083
1.068
4.064
4.013
2.933
0.168
NOX
MASS
LBS.
1.292
2.433
9.338
2.024
0.461
11.909
11.369
8.311
167.809
FUEL
MASS
LBS.
306.92
101.99
268.86
222.82
112.93
1012.72
FUEL
MASS
LBS.
306.32
101.99
268.86
222.82
112.93
1012.72
FUEL
NASS
LBS.
306.92
101.99
268.86
222.82
112.93
1012.72
LB CO /
IK LB FUEL
41.393
0.978
0.802
9.199
41.393
LB HC /
IK LB FUEL
9.433
0.024
0.090
0.374
9.493
LB NOX/
IK LB FUEL
4.084
23.932
19.896
9.089
4.0B4
ENERGY
I TH-HR
279.90
169.17
491.92
386.67
101.90
1384.79
ENERGY
1 TH-HR
275.90
169.17
451.92
386.67
101.90
1384.79
ENERGY
f TH-HR
279.50
169.17
431.92
386.67
101.50
13B4.73
LB
f
0
0
0
0
0
LB
t
0
0
0
0
0
LB
CO /
TH-HR
.04601
.00033
.00048
.00300
.04*01
HC /
TH-HR
.01092
.00001
.00003
.00022
.01052
NOX/
TH-KR
0.00454
0.01438
0.01181
0.00324
0.004S4
IV-269
-------
D«TE: T/12/T1
TEST ORGANIZATION: PRATT c WHITNEY
ENGINE SUPPLIER! PRATT AND WHITNEY
ENGINE DATA «««««»»»«»«»««««««««««»«
CAL ID NUMBERl 313 ENGINE TYPE AND MODEL: JT8D-U
RATED THRUST: 15000.
ENGINE TOTAL TIME: -0. MRS
TINE SINCE HOT SECTION OVERHAUL: -0. HRS
TIME SINCEl
NI COMPRESSOR OVERHAUL: -o. HRS
N2 COMPRESSOR OVERHAUL: -o. HRS
COHRUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANF OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -0. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUFL: JP-4 FUEL H/C RATIO: 2.000
OPERATIONAL DATA «««««*««»»*«*«»
INLET AIR TEMPERATURE, DEGREES F: START -0.00
ATMOSPHERIC PRESSURE: START -0.00
INLFT AIR HUMIDITY, LBS H20/LB AIR: -0.0000
RELATIVE HUMIDITY: -0.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIMF, SFC: 1.00
NUMBER OF TESTS: 9
COMMENTS:
EXHAUSI GAS PRESSURE IN INCHES HG
SMOKE DENSITY IS VON BRAND MEASURE PARTICULATES ARE IN MG/M»»3
SERIAL NUMBER:
FINISH -0.00
FINISH -0.00
CLOCK
TIME
1033.00
1040.00
1058.00
1121.00
1222.00
1239.00
125*. 00
1310.00
13)1.00
TEST
MODE
I/ 0
7.1 \
I/ 2
4/ 3
5/ 4
6/ 5
7/ 6
B/ 7
9/ 8
POWER
THRUST.LBS PERCENT
OR RATFD
SHP
1350.00
1870.00
650.00
5070.00
9550.00
10920.00
12000.00
13360.00
14330.00
r.a.
e
12
5
33
A3
72
79
89
95
FNC1NE
SPEED
RPM
NI
3250.00
3760.00
2605.00
S675.00
71 10.00
7180.00
7625.00
7950.00
8270.00
N2
7545.00
8160.00
6640.00
9740.00
10770.00
10990.00
11155.00
11370.00
11545.00
MEASURED
FUEL
FLOW
LB/HR
1293.00
1596.00
945.00
2930.00
5465.00
6275.00
6950.00
7930.00
8640.00
GAS GEN
MR FLOW
LB/SEC
CALC COMPRFSSOR ENGINE
F/A DISCHARGE PRESSURE
TEMP RATIO
DEGREES F EPR
37.70
43.70
30.20
71.00
122.00
129.60
136.00
146.60
1537.00
0.009500
0.010100
O.C08700
0.011200
0.012400
0.013500
0.014200
0.015000
0.015600
-0
-0
-0
-0
-0
-0
-0
-0
-0
.00 1.07
.00
.00
.00
.00
.00
.00
.10
.04
.29
.64
.75
.86
.00 1.98
.00 2.07
TURBINE
INLET
TEMP
OEGRFES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
POWER EXHAUST
PFRCENT GAS
RATED TFMP
T.O. OEGRFFS F
12
5
33
63
72
79
715.00
735.00
675.00
710.00
860.00
905.On
940.00
985.00
1025.00
EXHAUST
GAS
PRESSURE
PSIA
32.09
37.68
31.29
36.65
48. 70
51. 89
54.68
58.45
60.94
CO
( WFTI
PPMV
136.80
110.30
214.40
46.30
15.60
13.70
12.00
10.50
9.90
CO
2
IkFTI
PERCENT
1.14
1.23
1.09
I.S3
2.25
2.41
7.51
2.61
2.79
THC
(WEI!
PPMV
11.60
12.40
74.60
4.90
1.20
0.7C
0.50
1.40
1.70
NO
(WETI
PPMV
17.60
15.50
5.10
13.40
95.80
1 18. 80
142.40
175.10
198.30
NO
7
(WETI
PPMV
5.10
6.40
5.80
7.50
7.60
8.50
10.00
11.90
15.60
ALDEHYDES SMOKE PARTICULARS
IWETI
PPMV
17.70
21.90
10.90
40.90
103.40
127.10
157.40
187.00
213.90
-o.no
-o.oo
6.00
-o.oo
-0.00
-o.oo
-o.oo
-o.oo
-o.oo
2.00
3.00
1.00
15.00
25.00
77.00
28.00
29.00
11.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
14.00
14.00
16.00
PIJWFR
PERCENT
RATED
T.n.
6
12
5
11
63
72
79
89
95
MASS EMI
r.o
LB/IK
LB FUEL
23.62
17.73
16.27
6.07
1.18
1.11
P. 95
0.7H
0.71
MASS EMI M4SS EMI
HC NU2
LB/IK LB/IK
LB FUFL LS FUF.L
3.12
1.14
7.63
0.37
0.06
0.03
0.02
0.06
0.07
. 45
.69
.70
.60
.1 1
.16
.30
.46
.81
MASS EMI
C02
LB/IK
LB FUEL
3092.07
3106.76
3056.70
3127.28
1135.40
1115.87
3136.20
1116.35
3116.44
MASS EMI
NO
LB/IK
LR FUEL
1.57
4.09
1.50
7.14
13.96
16.16
18.45
21.42
21.10
MASS EMI
NOX
LB/IK
Lfl FUEL
5.02
5.78
3.20
P.74
15.06
17.32
19.75
22.88
25.14
MASS FMI
CO
LB/HR
30.53
28.30
36.16
17.65
7.56
7.12
6.56
6.20
6.12
MASS EMI MASS EMI MASS EMI
HC N02 C02
LB/HR LB/HR LB/HR
4.04
1.67
7.21
1.07
0.33
0.71
0.16
0.47
0.60
MASS EMI
NO
LB/HR
MASS EMI
NUX
LB/HR
1.87
2.70
1.61
4.70
6.05
7.26
9.01
11.54
15.84
3998.05
4958.38
2888.56
9162.93
17134.98
19677.59
21796.56
24871.26
27098.63
4.62
6.53
1.41
20.91
76.27
101.40
126.25
169. BP.
201.35
6.49
9.23
3.02
25.61
82.32
106.66
137.26
181.42
217.19
POWER
PERCENT
RATED
T.n.
12
5
33
63
72
79
89
95
CO
LR/1K1TH-HR
22.618
15.133
42.543
1.481
P.792
0.652
0.548
0.464
0.427
LB/IK«TH-HR
2961.518
2651.543
3196.113
1807.285
1794.239
1801.978
1816.380
1661.621
1691.056
THC
LB/1KHTH-HR
2.992
0.974
8.478
0.21 I
0.035
0.019
0.013
0.035
0.047
NO
IB/IKJTH-HH
3.472
3.493
1.662
4.124
7.986
9.286
10.668
17.715
14.051
LR/1KJTH-HR
1.385
1.442
1.890
0.926
0.634
0.664
0.751
0.864
1.105
NO
X
LB/IK«TH-HR
4.807
4.915
3.553
5.051
6.620
9.950
11.438
13.579
15.156
IV-270
-------
C»L 10 NUNBERI 193 ENGINE TTPE «ND MODELl JT80-11
TEST ORGANKATIONI PRATT t WHITNEY
SERIAL NUMBER! P6T6215
NODE
TAXI-IDLE
TAKEOFF
CL IN BOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.060
I. 000
0.850
0.400
0.060
POWER
f TH
900.0
15000.0
12750.0
6000.0
400.0
EMISSION FUEL
RATE RATE
LB/KR LB/HR
34.864 1019.094
I.79B 9015.714
4.675 7648.812
16.156 1488.132
14. 864 1019.014
USAGE TINE IN
WI FACTOR MODE
MIN.
TOTAL FOR CYCLE"
LBS POLLUTANT/ IK L6
LBS POtlUTANT/lK LB
LBS POLLUTANT/1000K
NODE
TAXI-IOLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.060
1.000
0.850
0.400
0.060
POWER
1 TH
400.0
15000.0
12750.0
6000.0
900.0
EMISSION FUEL
RATE RATE
L8/HR LB/HR
7.001 1014.014
0.0 9035.714
0.045 7646.812
0.945 3488.112
7.001 1019.014
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE i
TH-HR/CYCLEl
LB TH AT I.O.:
USAGE TIME IN
WT FACTOR MODE
MIN.
TOTAL FOR CTCLEl
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POILUTANT/IOOOK
MODE
FRACTIONAL
POWER
TAXI-IDLE 0.060
TAKEOFF 1.000
CLINBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.060
POWER
TH
900.0
15000.0
12750.0
6000.0
900.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
1.421 1014.014
241.876 9015.714
164.505 7648.812
14.660 1488.112
1.421 1019.014
.000 14.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLEi
TH-HR/CYCLEl
LB TH AT T.O.I
USAGE TIME IN
NT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK IB
LBS POLLUTANT/ 1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CVCLEI
LB TH AT T.O.I
CO
MASS
LBS.
11.040
0.021
0.171
1.090
4.068
16.391
15.461
11.442
0.140
HC
MASS
LBS.
2.218
0.0
0.002
0.063
O.aiT
1.099
2.924
2.164
0.0
NOX
MASS
LBS.
1.084
2.822
6.012
2.311
0.199
12.648
11.912
8.829
188.126
FUEL
MASS
LBS.
122.69
105.42
280.46
212.54
118.89
1060.00
FUEL
MASS
LBS.
122.69
105.42
2B0.46
212.54
ua.89
1060.00
FUEL
MASS
LBS.
322.69
105.42
280.46
212.54
118.89
1060.00
LB CO /
IK LB FUEL
14.211
0.199
0.611
4.689
14.211
LB HC /
IK LB FUEL
6.872
0.0
0.006
0.271
6.872
LB NOX/
IK LB FUEL
1.359
26.769
21.S07
9.937
3.359
ENERGY
1 TH-HR
285.00
175.00
467.50
400.00
105.00
1432.50
ENERGY
f TH-HR
285.00
175.00
467.50
400.00
105.00
1412.50
ENERGY
« TH-HR
285.00
175.00
467.50
400.00
105.00
1412.50
LB
1
CO /
TH-HR
0.01874
0.00012
0.00017
0.00271
0.01874
LB
1
0
0
0
0
0
LB
1
0
0
0
0
0
HC /
TH-HR
.00778
.0
.00000
.00016
.00778
NOX/
TH-HR
.00180
.01611
.01290
.00578
.00180
IV-271
-------
DATEI 7/ 7/71
TEST ORGANIZATION! PRATT t WHITNEY
ENGINE SUPPLIER! PRATT AND UHITNEV
ENGINE DATA
CAL ID NUMBER: 61 ENGINE TYPE AND MODEL: JT90
RATED THRUST: 43500.
FNGINE TOTAL TIME! -0. MRS
TIME SINCE HOT SECTION OVERHAUL: -0. MRS
TIME SINCE!
NI COMPRESSOR OVERHAUL: -o. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
CriMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
NT. TURBINE OVERHAUL: -o. HRS
FUEL: jp-4C FUEL H/C RATIO: 2.000
OPERATIONAL DATA «»«
INLET AIR TEMPERATURE. OEGRFES F: START 81.60 FINISH 76.30
ATMOSPHERIC PRESSURE: START 21.91 FINISH 30.00
INLET AIR HUMIDITY, LBS H20/L1 AIR: 0.0100
RELATIVE HUMIDITY: 42.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: ISO.00, FLOU RATE, LITFRS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 10
COMMENTS:
D-7 SHORT CONE
SERIAL NUMBER!
X-495-14A
CLOCK
TINE
2121.00
2138.00
21*8.00
2201.00
2213.00
2222.00
2232.00
22*3.00
2250.00
2303.00
POWER
PERCENT
HATED
T.O.
6
9
23
71
8*
9*
75
47
17
7
POWER
PERCENT
RATED
T.O.
6
9
23
71
04
94
75
47
17
7
POWER
PERCENT
RATE5
T.n.
6
9
23
71
B4
94
75
47
17
7
TFSr
MODE
I/ 0
11 1
3/ 2
4/
5/
6/
7/
a/
9/ 8
10/ 9
EXHAUST
CAS
TEMP
OEGRFFS F
670.50
675.90
76S.OO
953.80
1010.10
1524. 10
1436. 10
1397.00
1166.10
1116. ro
MASS EMI
CO
LB/1K
LB FUFL
50.40
41 .90
7.47
0.72
0.60
0.60
0.66
1.18
15.84
51.32
CO
POHFR ENGINE MEASURED GAS GFN CALC COMPRESSOR ENGINE TURBINE
THPUST.LBS PERCENT SPEED FUEL AIR FLOW F/ A DISCHARGE PRESSURE INLET
OR RATED RPM FLOU LB/SEC TFMP RATIO TEMP
SHP T.O. NI N2 LB/HR DEGREES F EPR DEGREES F
2948.00 6 1022.50 4956.00 1732.00 45.64 0.010500 837.30 .02 1122.20
402B.OO 9 1185.60 5330.00 2071.00 53.39 0.010800 885.40 .02 1180.90
10167.00 23 1860.60 6386.00 4246.00 86.51 0.013600 1061.20 .07 1518.00
31708.00 71 2989.60 7252.00 11879.00 165.40 0.019960 1321.60 .28 2111.90
36753.00 84 3172.00 7394.00 14183.00 181.71 0.071690 1370.30 .36 2251.50
40WO.OO 94 3302.nO 7556.00 16052.00 192.71 0.023100 1407.40 .42 2364.50
13044.00 75 3045.60 7288.00 12588.00 175.00 O.OZOOOO 1333.00 .31 2155.00
20780.00 47 2543.00 7168.00 8470.00 129.50 0.018200 1232.00 1.16 1954.20
7538.00 17 1610.50 6048.00 3250.00 75.10 0.012000 995.40 1.05 1363.40
3413.00 7 110?. «0 5151.00 1682.00 52.20 0.010000 857.60 1.02 1135.10
C XHAUST CO CO IHC NO NO NO ALDEHYDES SMflKE PART I f.UL A TES
GAS IMFT) 2 (WET) UETI 2 X
PRESSURE PPMV (UETI PPMV PP»V (WFTI IWFTI
PSIA
It. 94
15.03
15.64
18. 66
19.70
20.57
U.9B
16.96
15.36
14.98
MASS FMI
HC
LB/1K
LB FUFL
16. 71
4.57
0.75
0.21
0.18
0.23
0.21
0.26
2.05
12.93
LB/1K1TH-HR
14.
21.
3.
0.
0.
0.
0.
0.
6.
28.
427
542
121
275
233
236
252
477
S30
577
PERCENT V
488.
361.
84.
12.
11.
1 1.
11.
17.
150.
423.
MASS EMI
NQ2
LD/1K
LB FUFL
0.89
.54
.31
.27
.52
.84
.41
.16
2.14
2.25
cn
2
00
50
20
20
00
60
20
70
6(1
20
MASS EMI
C02
LB/IK
LB FUFL
2999.83
3059.37
3123.95
3136.07
3116.30
3136.18
3116.12
31J5.18
3107.22
3020. B6
1.59 743
1.68 68
2.24 1
3.37
3.64
3.84
1.18
3.00
1.88 3
1.57 18
MASS FMI
NO
LR/1K
LB CUFL
1.61
2.2H
6.08
21.99
28.73
34.50
74.41
15.42
4.63
1.39
THC
LB/IK«TH-HR LB/1KHTH-HR
1762.449
1572.976
1304.642
1193.695
17.10.299
1228.750
1194.695
1270.369
1339.673
1665.763
9.818
2.351
0.312
0.081
0.070
0.089
0.001
0.105
O.H86
7.128
.00 9.
.90 12.
.70 41.
.30 226.
.60 319.
.60 404.
.30 251.
.1)0 141.
.10 76.
.30 6.
MASS Ml
NOX
Lfl/lK
L3 FUEL
2.77
3.83
7.39
73.20
30.26
36.35
25.82
16.57
6.77
3.64
NO
PPHV PPMV
30 4.
00 8.
70 9.
00 12.
00 16.
10 21.
70 14.
10 10.
60 12.
90 11.
MISS E.MI
cn
18/HR
101.49
86.77
11.71
8.58
6.56
9.68
8.33
9.91
51.49
97.53
LB/IKHTH-HH
1.
1.
2.
e.
11.
13.
9.
6.
1.
0.
078
175
539
369
088
518
300
246
996
765
50 11.
10 20.
00 50.
50 738.
90 335.
60 425.
50 266.
60 151.
40 39.
20 13.
MASS EMI
HC
LB/HR
28.94
9.47
3.17
2.54
2. 56
3.63
2.66
2.18
6.6B
24.31
NO
2
80 -0.00 -0.
10 -0.00 -0.
70 -0.00 -0.
50 -0.00 -0.
90 -0.00 -0.
70 -0.00 -0.
20 -0.00 -0.
70 -0.00 -0.
20 -0.00 -0.
10 -0.00 -0.
MASS EMI MASS EMI
N02 C02
LR/HR LB/HR
1.54 5195. 70
3.19 6335.95
5.57 13264.29
14.45 17252.62
21.59 44482.09
29.60 50141.66
17.70 39477.48
9.75 26198.25
6.96 10098.46
4.24 5685.25
NO
X
00
00
00
00
00
00
00
00
00
00
MASS EMI
NO
LB/Hk
3. 18
4.73
25. Rl
261.17
407.53
553.82
307.32
129.80
15.05
2.61
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/HR
4. 71
7.92
31.19
275.61
429.12
583.42
325.03
139.55
22.01
6.85
LR/IKITH-HR LB/IKfTH-HR
0.521
0.793
O.S4B
0.463
0.587
0.723
0.536
0.469
0.924
1.242
1.599
1.967
3.087
6.831
11.676
14.240
9.636
6.715
2.920
2.008
IV-272
-------
CM. 10 NUMBER! 61 ENGINE TYPE AND NODELI JT40
TEST ORGANIZATION! PRATT I VHITNEY
SERIAL NUMBER! X-445-14A
NODE FRACTIONAL
POKER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
O.OTO
1.000
0.850
0.100
O.OTO
POKER
< TH
30*5.0
43100.0
36975.0
13050.0
30*5.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
112.53* 1889.137
18.885 17066. *61
IB. 179 1*937. 789
26.695 5*58.695
112.53* 1889.137
USAGE TIME IN
NT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
NODE
TAXI-IDLE
TAKEOFF
CLIKBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
O.OTO
1.000
0.850
0.300
O.OTO
POKER
1 TH
30*9.0
*3500.0
36175.0
13090.0
30*9.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
85.205 1889.137
6.622 17066. *6l
5.6*1 1*937.785
9.5*2 5*58.695
85.205 1889.137
.000 19.00
.000 O.TO
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLE!
LB TH AT T.O.I
USAGE TIME IN
KT FACTOR MODE
MIN.
TOTAL FOR CYCLE)
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
O.OTO
1.000
0.850
0.300
O.OTO
POKER
f TH
30*9.0
43500.0
36979.0
13090.0
30*9.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
5.822 1889.137
681.509 17066.461
***.902 1*537. TB5
90.315 9*98.649
5.822 U89.137
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLE!
LB TH AT T.O.!
USAGE TIME IN
KT FACTOR MODE
MIN.
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IOOOK
.000 19.00
.000 O.TO
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLEI
LB TH AT T.O.I
CO
MASS
LBS.
35.636
0.220
0.667
1.780
13.129
51.431
26.861
12.690
0.906
HC
MASS
LBS.
26.982
0.077
0.207
0.369
9.9*1
37.976
19.629
9.272
1.776
NOX
MASS
LBS.
1.8**
7.991
16.313
3.39*
0.679
30.1*1
15.7*2
7.437
182.780
FUEL
MASS
LBS.
598.23
199.11
533.05
363.91
220.40
191*. 70
FUEL
MASS
LBS.
598.23
199.11
533.05
363.91
220.40
1914.70
FUEL
MASS
LBS.
59B.23
199.11
533.05
363.91
220.40
1414.70
LB CO /
IK LB FUEL
59.569
1.107
1.250
4.890
59.569
LB HC /
IK LB FUEL
45.103
0.388
0.388
1.015
45.103
LB NOX/
IK LB FUEL
3.082
39.933
30.603
9.217
3.082
ENERGY
1 TH-H»
96*. 25
507.50
1355.79
870.00
355.25
4052.75
ENERGY
f TH-HR
964.25
507.50
1355.75
870.00
399.29
4052.75
ENERGY
i TH-HR
964.25
507.50
1355.75
870.00
355.25
4052.75
LB
*
0
0
0
0
0
LB
1
CO /
TH-HR
.03696
.00043
.00044
.00205
.03646
HC /
TH-HR
0.02798
0.00015
0.00019
0.00042
0.02798
LB
0
0
0
0
0
NOX/
TH-HR
.00141
.01567
.01203
.00386
.00141
IV-273
-------
OATf.1 7/ «/7l
TEST ORGANIZATION! PRATT I WHITNEY
ENGINE SUPPLIER: PRATT AND WHITNEY
ENGINE DATA «.,,.....
CAL ID NUMBER: 1*7 ENGINE TYPE AND MODEL: JI90
SERIAL NUHRER:
X-495-14S
RATED THRUST: 41500.
ENGINE TOTAL TIME: -0. HRS
TIME SINCE HOT SECTION OVERHAUL: -0. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: -0. HPS
N2 COMPRESSOR OVERHAUL: -0. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOULE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
N2 TURBINE OVERHAULl -0. HRS
FUEL: jp-4C FUEL H/C RATIO: 2.000
OPERATIONAL DATA »««»»«»
INLET AIR TEMPERATURE. DEGREES F: START 85.20 FINISH
ATMOSPHERIC PRESSURE: START 30.07 FINISH
INLET AID HUMIDITY, LRS H20/LB AIR: 0.1100
RELATIVE HUMIDITY: 47.50 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: ISO.00, FLOW RATE, LITERS/MIN:
SAMPLE LINF TRANSPORT TIMF., SEC: 1.00
NUMBER OF TESTS: 10
COMMENTS:
D-7 SHORT CDNE
84.60
30.07
2.00
CLOCK
TIME
1050.00
1059.00
1112.00
1133.00
1140.00
1151.00
1703.00
1212.00
1225.00
1218.00
POWER
PERCENT
RATED
T.O.
6
a
25
70
85
79
78
49
16
7
POWER
PERCENT
RATF.O
T.O.
6
8
25
70
85
79
78
49
16
7
POWER
PERCENT
RATED
T.O.
6
8
25
70
85
79
78
49
16
7
TEST
MODE
I/ 0
3/ 2
4/ 3
>/ 4
6/ 5
7/ 6
8/ 7
9/ 8
IO/ 9
EXHAUST
T.AS
TEMP
OEGRFES f
1130.20
1138.50
1269.70
1444.00
1570. 10
1497.20
1492.40
I1A6.60
1200.40
1145.10
MASS EMI
CO
LB/IK
LB FUFL
124.83
85.88
4.57
0.57
0.48
0.49
0.51
1.07
11.30
42.86
CO
POWER ENGINE MEASURED GAS GEN CALC COMPRESSOR ENGINE TURBINE
THRUST, LBS PERCENT SPEED FUEL AIR FLOW F/A DISCHARGE PRESSURE INLET
OR RATEO RPM FLOW LB/SEC TEMP RATIO TEMP
SHP T.O. Nl N2 LB/HR DEGREES F EPR DEGREES f
2747.00 6 1023.40 4977.00 1749.00 45.58 0.011630 839.00 .02 11308.00
3764.00 8 1191.40 5370.00 2102.00 53.56 0.011900 BB8.IO .02 1191.00
11040.00 25 1977.00 6622.00 4846.00 91.30 0.016090 1101.20 .08 1619.20
30841.00 70 3032.80 7420.00 12463.00 166.53 0.022690 1352.20 .29 2136.80
37004.00 85 3242.40 7580.00 15218.00 184.58 0.025000 1405.80 .38 2347.80
34530.00 79 3172.00 7503.80 14128.00 177.94 0.024070 1384.60 .35 2282.50
33946.00 78 3144.10 74B4.70 13834.00 174.73 0.024000 1377.70 .33 2203.20
21482.00 49 2652.90 7108.60 8618.00 135.01 0.019350 1255.90 .18 1937.30
7306.00 16 1642.20 6I7R.60 3397.00 74.73 0.015780 1019.40 .05 1418.00
3323.00 7 1130.80 5272.10 1960.00 50.47 0.011770 876.20 .02 1172.70
FXHAUST CO CO THC NC NO NO ALDEHYDES SMOKE PARTICULATES
GAS IWETI 2 IWFTI IWETI 2 X
PRESSURE PPMV (WET! PPMV PPMV I WE T 1 IWETI
PSIA
14.94
15.03
15.78
18.82
20.08
19.54
19.14
17.17
15.36
14.99
M4SS EMI
HC
LB/IK
LR FUEL
15.58
8.34
0.36
0.06
0. 13
0.29
0.29
0.22
1.21
9.38
LR/ 1K1TH-HP
79.
47.
2.
0.
0.
0.
0.
0.
5.
25.
622
961
008
231
199
201
209
429
255
282
PERCENT V
1069.00 1.
751.70 1.
55.90 2.
10.60 3.
9.70 4.
9.50 3.
9.7C 3.
15.90 2.
116.HO 2.
369.40 1.
MASS EMI MASS FMI
Nil? C02
LB/IK LB/IK
LB FUFL LB FUEL
1.57 2898.87
7.01 7979.92
1.17 3129.57
1.53 3136.67
1.96 3136.63
1.81 3136.18
l.7i 3116.14
1.18 3135.46
2.16 3116.66
2.53 3044.67
CO
2
58 233
66 127
43 7
70 2
01 4
86 9
78 9
97 5
05 21
67 141
MASS EMI
NO
LB/IK
LB FUFL
1 .44
2.03
7.39
24.69
33.62
79.76
77.94
15.06
4.53
1.32
TMC
LB/lMtTH-HR LB/IK0TH-HR
1849.057
1664.130
1373.770
1267.543
1289.950
1783.174
1278.072
1257.864
1449.122
1795.834
9.939
4.659
0.159
0.026
0.053
0.118
0.118
0.088
0.564
5.531
.00 7.
.50 10.
.70 54.
.10 278.
.50 411.
.70 344.
.60 322.
.70 136.
.90 28.
.10 6.
MASS EMI
NOX
LR/1K
LB FUFL
3.01
4.03
8.56
26.27
35.58
31.07
79.69
16.25
6.69
3.85
NO
50
80
90
60
10
50
10
50
50
90
MASS
CO
PPMV PPMV
8.
10.
a.
17.
24.
21.
20.
1 0.
13.
13.
EMI
LB/HR
218.
180.
22.
7.
7.
6.
7.
9.
38.
84.
32
52
16
13
35
94
09
21
39
01
LB/IKHTH-HR
0.
1 .
3.
9.
13.
11.
11.
6.
2.
0.
918
132
244
978
875
972
385
044
106
776
20 15.70
70 21.50
70 63.60
30 295.90
00 435.10
30 365.80
20 342.30
70 147.20
60 42.10
30 20.20
MASS EMI MASS FM
HC Nfl2
L8/H» LB/HR
27.25 2.75
17.54 4.22
1.75 5.68
0.61 19.11
1.95 29.87
4. 06 25.56
4.02 24.74
1.89 10.18
4.12 7.34
18.38 4.97
NO
2
LR/ 1K4TH-HR
1.003
1.121
0.514
0.620
0.807
0.740
0.714
0.474
1.005
1.495
-0.00 -0.
-0.00 -0.
-0.00 -0.
-0.00 -0.
-0.00 -0.
-0.00 -0.
-o.oo -o.
-0.00 -0.
-0.00 -0.
-0.00 -0.
1 MASS EMI
C02
LB/HR
5070.11
6263.79
15165.88
39092.29
47733.28
44308.00
43385.41
27021.43
10587.28
5967.55
NO
X
LB/ 1K*TH-HH
1.921
2.253
3.759
10.597
14.632
12.712
12.099
6.517
3.111
2.7T1
00
00
00
00
00
00
00
00
00
00
MASS EMI
NO
LB/HR
2.52
4.26
35.82
307.72
511.57
413.40
386. 46
129.83
15.39
2.58
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NUX
Lfl/HR
5.27
8.48
41.50
326.83
541.44
438.96
410.71
140.00
22.73
7.55
IV-274
-------
CM. ID NUMBER: 147 ENGINE TYPE AND NOOElt JT9D
TEST ORGANIZATION: PRATT I WHITNEY
SERIAL NUNBEUI X-49S-14B
NODE
TAXI-IOLE
TAKEOFF
CLINBOUT
*PPRO»CH
TAXI-IOLE
HODE
TAXI-IOLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.070
1.000
0.950
0.300
0.070
FRACTIONAL
POWER
0.070
1.000
0.850
0.300
0.070
FRACTIONAL
POWER
0.070
1.000
0.850
0.300
0.070
POWER
TH
3045.0
43500.0
36975.0
13050.0
30*5.0
POWER
TH
3045.0
43500.0
36975.0
13050.0
3045.0
POWER
1 TH
3045.0
43500.0
36975.0
13050.0
3045.0
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR KIN.
129.265 1144.465 .000 19.00
4.727 18016.625 .000 0.70
11.819 15128.035 .000 2.20
22.675 5462.012 .000 4.00
129.265 1844.465 .000 7.00
TOTAL FOR CYCLEl
IBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.:
EMISSION FUEL USAGE TINE IN
RATE RATE HT FACTOR MODE
LB/HR LB/HR MIN.
23.592 1844.465 .000 19.00
2.786 18016.625 .000 0.70
3.114 15128.035 .000 2.20
1.353 5462.012 .000 4.00
23.592 1844.465 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000X LB TH AT T.O.:
EMISSION FUEL USAGE TINE IN
RATE RATE MT FACTOR MODE
LB/HR LB/HR MIN.
6.737 1844.465 .000 19.00
904.633 18016.625 .000 0.70
538.073 15128. 035 .000 2.20
54.637 5462.012 .000 4.00
6.737 1844.465 .000 7.00
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK LB TH-HR/CYCLEl
LBS POLLUTANT/ 1000K LB TH AT T.O.:
CO
MASS
LBS.
40.934
0.055
0.433
1.512
15.081
58.015
30.086
14.315
0.12T
HC
MASS
LBS.
7.471
0.033
0.114
0.090
2.752
10.460
5.425
2.581
0.747
NO I
MASS
LBS.
2.134
10.554
19.729
3.642
0.786
36.845
19.108
9.091
242.622
FUEL
MASS
LBS.
584.08
210.19
554.69
364.13
215.19
1928.29
FUEL
MASS
LBS.
584.08
210.19
554.69
164.13
215.19
1928.29
FUEL
MASS
LBS.
584.08
210.19
554.69
364.13
215.19
1928.29
LB CO /
IK LB FUEL
70.083
0.262
0.781
4.151
70.083
LB HC /
IK LB FUEL
12.791
0.155
0.206
0.248
12.791
LB NOK/
IK LB FUEL
3.653
50.211
35.568
10.003
3.653
ENERGY
1 TH-MR
964.25
507.50
1355.75
870.00
355.25
4052.75
ENERGY
t TH-HR
964.25
507.50
1355.75
870.00
355.25
4052.75
ENERGY
1 TH-HR
964.25
507.50
1355.75
870.00
355.25
4052.75
LB CO /
f TH-HR
0.04245
0.0001 I
0.00032
0.00174
0.04245
LB HC /
1 TH-HR
0.00775
0.00006
o.ooooa
0.00010
O.OOTT5
L8 NOX/
TH-HR
0.00221
0.02080
0.01455
0.00419
0.00221
IV-275
-------
OATEI n em
TEST ORGANIZATION: PRATT C WHITNEY
ENGINF SUPPLIER: PRATT AND WHITNEY
ENGINE DATA
CAL 10 NUMBER: 148 ENGINE TYPE AND MODEL: JT90
RATED THRUST: 41500.
ENGINE TOTAL TIME: -0. MRS
TIME SINCF Hor SECTION OVERHAUL: -0. HPS
TIME SINCE:
NI COMPRESSOR OVERHAUL: -o. MRS
N2 COMPRESSOR OVERHAUL: -o. MRS
COMRUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZ2LF GUIDE VANE OVERHAUL: -0. HRS
Nl TURBINE OVERHAUL: -0. HRS
N2 TURBINF OVERHAUL: -0. HRS
FUEL! JP-5 FUEL H/C RATIO: 1.970
OPERATIONAL DATA »» .
INLET AIP TEMPERATURE! DEGREES F: START 89.40 FINISH H8.30
ATMOSPHERIC PRESSURE: START 30.03 FINISH 30.02
INLET AIR HUMlnlTY, LBS H20/LB AIR: 0.0083
RELATIVE HUMIDITY: 21.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITEPS/NIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TFSTS: 7
COMMENTS:
0-7 SHORT CONE
SERIAL NUMBER:
X-495-14C
CLOCK
TIME
1711.00
1723.00
1730.00
1752.00
1759.00
1328.00
1830.00
TEST
MOOE
I/ 0
2/ 1
3/ 2
4/ 3
5/ 4
6/ 5
7/ 6
POWER
THRUST, LBS PERCENT
OR RATED
SHP
2482.00
3493.00
10968.00
312BO.OO
16151.00
33051.00
21006.00
r.n.
5
8
75
71
83
75
48
ENGINE
SPEFD
RP«
Nl
996.00
1 166.00
1984.00
3061.00
3231.00
3130.00
2640.00
N2
4896.00
5310.00
6642.00
7381.00
7564.00
7433.00
7050.00
MEASURED
FUEL
FLOW
Lfl/HR
1700.00
2063.00
4930.00
12778.00
15004.00
13610.00
8540.00
GAS GEN
AIR FLOW
L6/SEC
44.24
51.75
90.15
167.13
181.26
172.24
133.73
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.010680
0.011070
0.015190
0.021240
0.022990
0.021950
0.017740
DEGREES F
379.00
433.40
657.10
903.10
953.70
921.40
794.80
ENGINF
PRESSURE
RATIO
EPR
1.01
1.02
1.08
1.30
1.37
1.32
1.17
TURBINE
INLET
TEMP
DEGREES F
1120.80
1195.10
1644.40
2198.60
2339.00
2254.00
1910.10
POWER
PERCENT
RATED
T.n.
25
71
81
75
48
EKHAUS!
GAS
TFMP
DEGREES r
678.30
692.90
814.50
1015.30
1082.00
1019.10
899.30
EXHAUST
GAS
PRESSURE
PSIA
14.90
14.99
15. 75
18.92
19.89
19.21
17.09
r.o
1 WE T 1
PPHV
468. 10
340.50
71.00
9.90
9.80
10.00
22.40
CO
2
IWETI
PERCENT V
1.80
1.81
2.49
3.5«
4.00
1.75
2.87
THC
IWET)
PPMV
240.60
132. SO
9.50
2.20
0.90
2.10
2.50
NU
IWETI
PPMV
9.60
13. 80
62.41}
314.10
4A5. 40
367. 6C
141.00
NO
2
(WET)
PPMV
11.10
15.30
13.00
17.50
25.20
20.30
1 1.90
ALDEHYDES SMOKE PARIICULATES
IWETI
PPMV
20.70
79.10
75.40
331.60
490.60
1ST.90
154.90
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
POWER
PERCENT
RATED
T.O.
25
71
81
75
48
MASS FMI
CO
Lfl/ lH
LB FUEL
50.07
36.30
5.85
0.55
0. 49
0.53
1.56
MASS EMI
HC
LB FUEL
14.74
8.11
0.44
0.07
0.01
0.07
0.10
MASS EMI
NO?
L I/ IK
Lfl FUEL
1.95
2.68
1.71
1.61
2.07
1.78
1.36
MASS EMI
CI12
L O/ 1 K
L3 FUFL
1025.41
3065.25
1134.14
1143.46
1141.68
3143.49
3141.60
MASS EMI
NO
L B/ IK
Lfl FUEL
1.69
2.42
8.71
26.63
38.24
32.21
16.16
MASS [Nl
NOX
L B/ IK
L9 FUEL
1.64
5.10
9.92
10.44
40.31
13.99
17.71
MASS EMI
CO
85.13
74. 8R
28.81
7.07
7.15
7.26
11.13
MASS EMI
HC
25.06
16.71
2.15
0.90
0.39
0.91,
0.65
MASS EMI
NO 2
1.12
5.53
6.43
20.53
31.06
24.21
11.61
MASS EMI
CO 2
5143.19
6321.60
15451.30
40167.16
47167.82
47782.94
26810.95
MASS EMI
NO
2.67
4.99
40.46
368.42
573.71
416.41
119.76
MASS EMI
NOX
6.18
10.51
48.91
388.94
604.78
462.64
151.39
PUWER
PERCENT
RATED
T.O.
25
71
83
75
48
CO
LH/1KITH-HK
34.297
21.438
2.629
0.226
0.203
0.220
O.n34
L R/1KKTH-H1
2072.197
1810.165
1406.762
1214.117
1304.745
1294.452
1277.300
inr
LB/lKfTH-HR
10.096
4.789
0. 196
0.029
0.011
0.029
0.041
NO
LB/1KHTH-HR
1.155
1.427
3.691
11.778
15.B70
13.265
6.653
LH/1KI1H-HR
1.336
1.5B2
0.769
0.656
0.659
0.713
0.554
NO
X
Ln/l»»TH-HR
2.491
3.009
4.460
12.434
16.729
11.998
7.207
IV-276
-------
t«L ID NUMBERI 1*8 ENGINE TYPE AND MODEL: JT9D
TEST ORGANIZATION! PRATT ( HMITNEY
SERIAL NUMBER: X-495-14C
NODE FRACTIONAL
POMER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAII-IDLE
O.OTO
1.000
0.850
0.300
O.OTO
POKER
I TH
3045.
43500.
36975.
13090.
30*5.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
84.971 1899.832
7.947 17927.234
8. Oil 19234.750
26.390 9647.430
64.971 1199.892
USACE TIME IN
NT FACTOR MODE
NIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK IB
IBS POLLUTANT/ 1000K
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
O.OTO
1.000
0.650
O.JOO
O.OTO
POWER
TH
30*5.
*3500.
16975.
13050.
30*3.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
20.312 1899.832
3.657 17927.234
3.108 15234.750
2.509 5647.430
20.312 1899.832
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TM-HR/CYCLE:
LB TH AT T.O.:
USACE TIME IN
«T FACTOR NODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
O.OTO
1.000
0.850
0.300
0.070
POWER
TH
30*5.
43500.
36979.
13090.
30*9.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
T.631 1899.832
958. TIB 17927.234
616.146 15234.750
62.475 5647.410
7.631 1899.832
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCIE:
LB TH AT T.O.:
USAGE TIME IN
NT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/ IOOOK
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CVU.E:
LB TH AT T.O.:
CO
MASS
LBS.
26.907
0.093
0.294
1.759
9.913
36.967
19.605
9.615
0.213
HC
MASS
LBS.
6.432
0.043
0.114
0.167
2.370
9.126
4.638
2.252
0.981
NOI
MASS
LBS.
2.417
II. 185
22.592
4.165
0.890
41.249
20.965
10.178
257.127
FUEL
MASS
IBS.
601.61
209.19
958.61
376.50
221.65
1967.51
FUEL
MASS
LBS.
601.61
209.15
558.61
376.50
221.65
1967.51
FUEL
MASS
LBS.
601.61
209.15
598.61
376.50
221.65
1967.51
LB CO /
IK LB FUEL
44.726
0.443
0.526
4.673
44.726
LB HC /
IK LB FUEL
10.691
0.204
0.204
0.444
10.691
LB NOX/
IK LB FUEL
4.017
53.478
40.443
11.063
4.017
ENERGY
1 TH-HR
964.25
507.50
1355.75
870.00
355.25
4052.75
ENERGY
1 TH-HR
964.25
507.50
1395.75
870.00
355.25
4052.75
ENERGY
1 TH-HR
964.25
507.50
1335.75
670.00
355.23
4052.73
LB CO /
f TH-HR
0.02791
0.00016
0.00022
0.00202
0.02791
LB HC /
t TH-HR
0.00667
0.00006
0.00008
0.00019
0.00667
LB NOX/
1 TH-HR
0.00251
0.02204
0.01666
0.00479
0.00251
IV-277
-------
CUTE I 7/ 8/71
TEST ORGAN! IATION: PRATT t WHITNEY
ENGINE SUPPLIER: PRATT AND WHITNEY
ENGINE DATA
CAL to NUMBER: 149
ENGINE TYPE AND MODEL: JTID
SERIAL NUMBER!
X-495-140
RATED THRUST: 43500.
ENGINE TOTAL TIME: -0. MRS
TIKE SINCE HOT SECTION OVERHAUL: -0. MRS
TIME SINCEl
HI COMPRESSOR OVERHAUL: -o. MRS
N2 COMPRESSOR OVERHAUL: -o. MRS
CONBUSTOR CAN REPLACEMENT: -0. MRS
FIRST STAGE N022LE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. MRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL: JP-5 FUEL H/C RATIO: 1.970
OPERATIONAL DATA »t......«»..««»«....
INLET AIR TEMPERATURE. DEGREES f: START 88.00 FINISH 70.20
ATMOSPHERIC PRESSURE: START 30.02 FINISH 30.02
INLET AIR HUMIDITY, LBS H20/L3 AIR: 0.0104
RELATIVE HUMIDITY: 29.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: ISO.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIMF, SEC: 1.00
NUMBER OF TESTS: 6
COMMENTS:
0-7 SHORT CONE
CLOCK
TIMF
18*0.00
IBS). 00
2)03.00
11.00
113.00
43). 00
TEST
MODE
I/ 0
2/ I
)/ 2
4/ )
5/ 4
(,/ 5
POWER
THRUST. LRS PERCENT
UR RATED
SHP
7297.00
2951.00
10967.00
30560.00
33733.00
2909.00
T.O.
16
6
25
70
77
6
ENGINF
SPEED
RPM
Nl
1668.00
1082.00
-0.00
2999.00
3100.00
10*6.00
N2
6185.00
5119.00
6538.00
7230.00
7306.00
4974.00
MEASURED
FUfL
FLOW
L9/HR
3504.00
1871.00
4925.00
12255.00
13540.00
1B27.00
GAS GEN
AIR FLOW
LB/SEC
75. 6B
48.23
-0.00
167.98
177. B3
47.97
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.012860
0.010780
0.015180
0.020270
0.021150
0.010580
DEGREES f
568.50
404.60
-0.00
852.20
877.40
369.30
FNGINE
PRESSURE
RATIO
EPR
1.05
1.02
-0.00
1.29
1.33
1.02
TURBINE
INLET
TEMP
OF.GRFES F
1427.10
1150.50
-0.00
2046.00
2124.10
1103.30
POWER
PERCENT
RATED
T.O.
16
6
75
70
77
EXHAUST
GAS
TFMO
DEGREES r
748.00
677.00
-0.00
958.00
983.10
640.70
EXHAUST
r,«s
PRESSURE
PSIA
15.32
14.93
-0.00
18. 78
19.38
14.96
CO
IWFTI
PPMV
136.00
812.30
69.30
11.10
10. 70
CO
2
IWETI
PERCENT V
2.12
1.80
2.53
3.60
3. SO
THC
IWFTI
PPMV
26.00
173.90
5.40
4.00
2.50
NO
IWETI
PPMV
41.10
17.10
50.90
224.40
268.70
NO
2
IWETI
PPMV
15.90
13.50
B.30
13.80
0.40
IWETI
PPMV
57.00
30.60
59.20
238.20
269.10
7.50
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATF.S
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
16
6
25
70
77
6
MASS EMI MASS EMI MASS EMI MASS FMI MASS EMI
CO HC N02 C02 NO
LR/1K LB/IK LH/IK LB/1K LB/1K
LB FUEI LR FUEL UB FUEL LB FUEL LR FUEL
12.74
87.64
5.47
0.62
0.56
64.98
1.40
10.49
0.24
0.13
0.08
2?. 72
2.45
2.33
1.08
1.26
0.03
3120.68
2978.05
3135.27
3143.21
3143.43
0.10 2980.10
6.32
2.96
6.59
20.48
23.24
1.35
MASS EMI
NDX
LB/1K
Lii FUEL
8.77
5.29
7.67
21.74
23.27
1.44
MASS EMI
CO
LB/HR
44.65
163.97
?6.92
7.56
7.63
lid. 72
MASS EMI
HC
LB/HP
4.89
19.62
1.20
1.56
1.02
41.51
MASS EMI
NO 2
LB/Hk
8.57
4.37
5.30
15.44
0.47
0.1B
MASS EMI
C02
LB/HR
10934.85
5571.93
15441.19
38520.00
42562.07
5444.64
MASS CHI
NO
LB/HR
22.16
5.53
32.48
251.01
314.62
2.46
MASS EMI
NOX
LB/HH
30.74
9.90
37.77
266.44
315.09
2.64
POWER
PERCENT
RATED
T.O.
16
6
25
70
77
6
cn
LB/ U0TH-HP
6. 1 16
55.566
2.456
0.247
0.226
40.810
LR/IKSTH-HH
1498.540
inns. 151
1408.610
1260.471
1261.734
1871.655
THC
Lfl/ IKMH-MH
0.670
6. 649
0.110
0.051
0.030
14.26H
NO
LB/1KKTH-HR
3.037
1.875
2.963
8.214
9.327
0.845
LB/lK»Th-HR
1.175
1.480
0.483
0.505
0.014
0.060
NO
X
LB/1K«TH-HR
4.212
3.356
3.446
8.719
9.341
0.906
IV-278
-------
C»L 10 NUMBERl 149 ENGINE TYPE AND NOOELl JT9D
TEST ORGANIZATION! PRATT ( HHITNEY
SERIAL NUMBERI I-49S-I4D
MODE FRACTIONAL
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
COKE*
O.OTO
I. 000
0.650
0.900
O.OTO
POKER
TH
30*5.0
43900.0
36973.0
1303O.O
3041.0
EMISSION
RATE
LB/HR
160.184
10.779
13.259
29.600
160.584
FUEL USAGE
RATE WT FACTOR
LB/HR
1971.791
17325.500
14807.000
1789.273
1971.791
.000
.000
.000
.000
.000
TIME IN
MODE
MIN.
19.00
0.70
2.20
4.00
7.00
CO
MASS
LBS.
90.852
0.126
0.416
1.973
18.735
FUEL
MASS
LBS.
624.40
202.13
542.92
383.95
230.04
LB CO /
IK LB FUEL
81.441
0.622
0.695
3.113
61.441
ENERGY
1 TH-MR
964.25
907.50
1355.75
670.00
355.25
L8 CO /
TH-HR
. 0.05274
0.00025
0.00036
0.00227
0.05274
TOTAL FOR CVCLEl 72.172
LBS POLLUTANT/IK LB FUEL/CYCLE! 36.350
LBS POLLUTANT/IK LB TH-HR/CYCLEl 17.608
LBS POLLUTANT/1000K LB TH AT T.O.I 0.289
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
NODE
TAXI-IDLE
TAKEOFF
CLIM60UT
APPROACH
TAXI-IOLE
FRACTIONAL
POKER
O.OTO
1.000
0.850
0.300
0.070
FRACTIONAL
POMES
O.OTO
1.000
0.850
0.300
0.070
POKER
1 TH
3045.0
43300.0
36973.0
13050.0
3045.0
POWER
1 TH
3045.0
43300.0
36975.0
13050.0
3045.0
EMISSION FUEL I
RATE RATE WT
LB/HR LB/HR
19.546 1971.791
3.436 17323.300
2.009 14807.000
1.485 3789.273
19.548 1971.791
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
EMISSION FUEL 1
RATE RATE WT
LB/HR LB/HR
3.297 1971.791
575.361 17325.500
403.764 14607.000
49.631 5769.273
3.297 1971.791
TOTAL FOR CYCLE:
LBS POLLUTANT/IK L8
LBS POLLUTANT/IK LB
LRS POLLUTANT/1000X
ISAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 T.OO
FUEL /CYCLE I
TH-HR/CVCLEl
LB TH AT T.O.I
JSAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE)
TH-HR/CYCLE1
LB TH AT T.O.l
HC
MASS
LBS.
6.190
0.040
0.074
0.099
2.281
8.661
4.374
2.143
0.922
NOX
MASS
LBS.
1.044
6.713
14.805
3.310
0.365
26.257
13.223
6.479
154.317
FUEL
MASS
LBS.
624.40
202.13
542.92
38S.95
230.04
1985.45
FUEL
MASS
LBS.
624.40
202.13
542.92
365.95
230.04
1985.45
LB HC /
IK LB FUEL
9.914
0.198
0.136
0.256
9.914
LB NOX/
IK LB FUEL
1.672
33.210
27.270
8.576
1.672
ENERGY
1 TH-HR
964.25
507.50
1359.75
870.00
395.23
4052.75
ENERGY
TH-HR
964.25
507.50
1335.79
870.00
355.25
4052.75
LB HC /
1 TH-HR
0.00642
0.00008
0.00005
0.00011
0.00642
LB NOX/
f TH-HR
0.00108
0.01323
0.01092
0.00380
0.00108
IV-279
-------
DATEI 7/28/M
TEST OSGANI1ATIONI PRAM t HITNEV
ENGINE SUPPLIER! PRATT AND VMItNEf
ENGINE DATA
CAL 10 NUNBER: 121 ENGINF TYPE AND liOOELI JT90-7
RATCO THR.USTI 49900.
FNGINf torn TINE: -0. HOS
(IDE SINCE HOT SECTION OVERHAUL! -0. MUS
TIPIE SINCEI
Nl COMPRESSOR OVERHAUL! -0. HIS
N2 COMPRESSOR OVERHAUL: -o. HAS
crmnusroR ON REPLACEMENT: -o. HIS
FIRST STAGE NDULE GUInE VANF OVERHAUL! -0. HRS
Nl TURBINE OVERHAUL! -0. MIS
N2 TURBINE nvERHAULI -0. HIS
FUEL: JP-4 FUFl H/C RATIO! 2.000
SERIAL NUMBER!
INLET AIR TEMPERATURE, DEGREES F: START 72.80 FINISH 77.00
ATMOSPHERIC PRESSURE: START 28.60 FINISH 26.60
INLET AIR HUNIOITY, LBS H20/LB AIR: 0.0091
RELATIVE HUMIDITY: -0.00 PEDCFNT
SAMPLE LINE: TENPERATURE, OEGREFS C> 190.00, FLOy RATE, IITFRS/NIN: 2.00
SANPLE LINE TRANSPORT TINE, SEC: 1.00
HUNKER OF TESTS! 19
COMMENTS:
BURNER CONFIGURATION - 10
CLOCK
TIMF
1011.00
1041.00
1091.00
1104.00
1112.00
1119.00
1126.00
1111.00
1140.00
1147.00
1194.00
1201.00
1208.00
1219.00
1222.00
POKE!
PERCENT
RATED
T.O.
7
a
9
100
96
91
B9
69
62
60
76
71
70
66
64
POKER
PERCENT
RATED
T.O.
7
6
9
too
96
91
89
69
62
60
76
71
70
66
64
POKER
PERCENT
RA1ED
T.O.
1
6
9
100
96
91
89
69
82
80
16
11
70
66
64
TFST
NODE
I/ 0
2/ 1
I/ 2
4/ 1
9/ 4
6/ 9
7/ 6
8/ 7
9/ a
IO/ 9
11/10
12/11
11/12
14/11
19/14
EXHAUST
GAS
TENP
DEGREES F
641.00
648.00
694.00
1092.00
1021.00
1014.00
999 . 00
982.00
961.00
991.00
916.00
921.00
910.00
694.00
880.00
MASS ENI
CO
LB/IK
LA FUEL
92.11
41.87
19.66
0.41
0.29
0.17
0.21
0.18
0.16
1.40
1.41
1.81
1.80
1.97
2.19
POKFR ENGINE
THRUST, LBS
OR
SHP
1171.00
1994.00
4168.00
49999.00
41794.00
42910.00
40B4I.OO
29997.00
17742.00
16491.00
14612.00
11916.00
120C8.0D
10449.00
29146.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS ENI
X
LB/IK
LS FUEL
11.92
8.11
9.61
0.19
0.10
0.16
0.16
0.14
0.14
0.0
0.02
0.06
0.10
0.99
0.60
CO
LB/IKi
26.
20.
16.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
TH-HR I
661
909
409
194
091
061
080
176
124
481
489
619
614
667
719
PFKCFNT SI
RATED
T.O. Nl
7 1016.00
B 1099.00
9 1196.00
100 1114.00
96 1270.00
91 1219.00
89 1182.00
69 1141.00
82 1092.00
80 1047.00
76 2991.00
71 2999.00
70 2899.00
66 2840.00
64 2788.00
EFO
P"
N2
4991.00
9187.00
9117.00
7414.00
7401.00
1182.00
7149.00
7129.00
7789.00
7791.00
7216.00
7180.00
7149.00
7102.00
7096.00
MEASURED CAS GEN
FUFL AIR FLO»
FLOy LB/SEC
Lfl/HR
1719.00 -0.00
1864.00 -0.00
2010.00 -0.00
16911.00 -0.00
19604.00 -0.00
19061.00 -0.00
14196.00 -0.00
11846.00 -0.00
11112.00 -0.00
12988.00 -0.00
11910.00 -0.00
11497.00 -0.00
10696.00 -0.00
10291.00 -0.00
9189.00 -0.00
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
cn co THC NH NO
IKETI
PPMV IK
2 III
II P
PERCENT V
494.10
377.90
108.80
.90
.10
.10
.00
.90
6.10
21.20
22.60
27.90
27.10
29.20
11.90
NASS EMI NASS FNI
NQ2 CO2
LB/IK LB/IK
LB FUEL L8 FUEL
0.0 1022.84
0.0 1046.41
0.68 1066.26
.81 1116.94
.91 llir.07
.AO 1116.98
.77 1116.96
.94 1116.77
.90 1116.19
.19 1119.99
.87 1119.48
.02 1114.74
.88 1114.61
.74 1111.92
.87 1112.10
CO
7
B/1KITH-HR LB
1940.946
1491.991
1410.984
1111.012
1117.194
1112.881
1107.. 670
1467.416
1091.418
1062.771
1076.297
1072.921
1067.079
1098.649
1091.990
.67 180
.67 122
.69 89
.90 9
.17 2
.98 9
.90 4
.49 4
.41 4
.11 0
.20 0
.06. 1
.02 2
.99 29
.87 20
NASS FNI
NO
LB/IK
LB FUEL
1.01
1.07
2.90
19.21
39.94
29.74
29.47
77.64
79.29
21.99
72.67
21.49
20.02
49.99
41.98
THC
MKITH-HR
6.076
1.891
2.991
0.069
0.019
0.061
0.099
0.069
0.090
0.0
0.006
0.020
D.019
0.116
0.270
ETI IKFTI 2
PNV PPMV IKETI
PPMV
.70 19.90 0.0
.80 16.10 0.0
.20 19.30 3.60
.90 376.00 19.30
.90 369.10 19.80
.60 324.70 19.60
.80 114.90 18.90
.20 290.80 16.20
.10 262.60 19.60
.0 242.20 17.90
.90 221.10 27.90
.60 201.60 19.00
.70 184.90 26.90
.10 414.00 24.10
.20 168.00 29.20
NASS EMI NASS ENI MASS
NO I CO
LB/IK Llt/HR
LB FUEL
1.01 89. 1
1.01 82. 6
9.9B 11. 7
37.01 1. 9
37. 6 1. 6
11. 4 2. 1
11. 4 1.28
79. a 9.21
26. 9 4.69
21. 4 11.61
29. 9 16.19
21. 7 20.77
27. 0 19.65
48. 9 20.10
44. 4 21.42
NO
LB/lKtTM-HR LE
1.931
1.461
1.115
12.702
17.. 809
10.992
10.356
12.931
6.786
6.281
1.796
7.347
6.815
15.911
14.101
HC
LA/
20.
19.
11.
1.
1.
2.
2.
1.
1.
0.
0.
0.
I.
10.
7.
/IK
CALC
F/A
010000
010000
010000
021000
022000
022000
021000
021000
020000
020000
019000
019000
oiaoon
018000
018000
NO
X
IKETI
PPNV
19.90
16.10
29.40
195.10
189.10
144.10
111.40
107.00
278.20
7.60.10
248.80
220.60
211.00
418.70
192.20
COMPRESSOR ENGINF
OISCHAPGE PR
TE"P
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
FSSURF
RATIO
EPR
1.02
1.02
.02
.46
.42
.40
.18
.16
.14
.37
.30
1.28
1.76
1.29
1.21
ALDEHYOFS SNOKE
-0.00 -0
-0.00 -0
-0.00 -0
-0.00 -0
-0.00 -0
-0.00 -0
-0.00 -0
-0.00 -0
-0.00 -0
-0.00 -0
-0.00 -0
-0.00 -0
-0.00 -0
-0.00 -0
-0.00 -0
ENI NASS ENI NASS FNI
HR
9
a
1
Q
4
o
b
91
«9
0
21
68
11
23
87
NO
2
tTH-HR
0.0
o.n
0.114
0.652
0.687
0.611
0.622
0.120
0.522
1.296
0.969
0.692
0.919
0.977
0.966
N02 C02
IB/ MB LB/HR
0.0 5196.26
0.0 5r19.41
1.17 6161.18
29.96 51975.66
10.07 48950.89
27.08 47108.82
.42 45014.14
.12 41411.74
.70 41192.10
.25 19470.25
.55 17)41.58
.21 16024.46
.13 14154.91
.21 12710.59
.14 10660.14
NO
K
LA/IKf TH-HR
1.511
1.461
2.566
1 1.194
11.491
11.169
10. 981
11.691
9.108
9.9T9
8. T64
8.014
7.794
16.496
19.028
.00
.00
.00
.00
.00
.00
.00
.00
.00
.00
.00
.00
.00
.00
.00
NASS
NO
IB/
5.
9.
9.
961.
960.
448.
423.
182.
111.
101.
269.
246.
218.
477.
410.
TURBINF
INLEI
IFNP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARIICULATFS
ENI
HR
17
ra
81
12
ra
96
01
70
67
92
98
50
11
B9
98
-0.00 .
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
NASS FNI
NOI
Ifl/HR
9.17
9.TB
11.21
611.68
90.89
T5.64
48.46
04.0)
51.17
49. 17
101.51
269.71
249.47
501.07
4)8.01
TV
IV-280
-------
CAL ID NUMBER: 323 ENGINE TYPE AND MODELi JT40-T
TEST ORGANIZATION: PRATT I WHITNEY
SERIAL NUMBER1 P-6B5603
MODE FRACTIONAL
POKER
TAXI-IDLE
TAKEOFF
CL 1* BOUT
APPROACH
TAXI-IDLE
0.070
1.000
0.830
0.300
0.070
POWER
TH
3185.
45500.
3)671.
13650.
3185.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
TT.165 1*03.093
3.611 16342.0*7
15.273 137)6.523
32.866 4643.3B7
77.165 1403.093
WT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
CL IN BOUT
APPROACH
TAII-IOLE
FRACTIONAL
POKER
0.070
1.000
0.850
0.100
0.0 TO
POWER
1 TH
3185.
45500.
38675.
13650.
3165.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
16.747 1403.093
3.992 16342.047
3.085 13736.523
2.704 46*3.367
16.747 1403.093
KT
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK L6
LBS POLLUTANT/10001
NODE
TAXI-IOLE
TAKEOFF
CLIH80UT
APPROACH
TAII-IOLE
FRACTIONAL
POWER
O.OTO
1.000
0.850
0.300
0.070
POKER
TH
3185.
45500.
38675.
13650.
3183.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
4.532 1403.093
603.415 16342.047
402.453 13736.523
44.881 4643.387
4.532 1403.093
KT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK IB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
USAGE TIME IN
FACTOR MODE
KIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CVCLEI
TH-HR/CVCLE:
IB TH AT T.O.I
USAGE TIME IN
FACTOR MODE
NIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
24.436
0.042
0.560
2.191
9.003
36.231
22.477
8.547
0.093
HC
MASS
LBS.
3.303
0.047
0.113
O.IBI
1.954
7.597
4.713
1.792
1.024
NOX
MASS
LBS.
1.435
7.040
14.757
2.492
0.529
26.752
16.597
6.311
154.722
FUEL
MASS
LBS.
444.31
190.66
503.67
309.36
163.69
1611.89
FUEL
MASS
LBS.
444.31
140.66
503.67
304.36
163.69
1611.89
FUEL
MASS
LBS.
444.31
190.66
503.67
309.56
163.69
1611.89
LB CO /
IK LB FUEL
54.996
0.221
1.112
7.078
54.996
LB HC /
IK LB FUEL
11.936
0.244
0.225
0.583
11.436
LB NOX/
IK LB FUEL
3.230
36.924
24.298
4.666
3.230
ENERGY
1 TH-HR
1008.38
530.83
1418.08
910.00
371.58
4239.08
ENERGY
TH-HR
1008.58
330.83
1418.08
410.00
371.58
4239.08
ENERGY
1 TH-HR
1008.58
530.83
1418.08
910.00
371.38
4239.08
LB CO /
f TH-HR
.0.02423
0.00008
0.00039
0.00241
0.02423
LB HC /
f TH-HR
0.00526
0.00009
0.00008
0.00020
0.00526
LB N0>/
TH-MR
0.00142
0.01326
0.01041
0.00324
0.00142
IV-281
-------
DATE: 7/28/71
TEST DRGANIJATIONI PRATT C. WHITNEY
ENGINE SUPPLIER: PRATT AND MHITNEY
ENGINE DATA
CAL 10 NUMBED: 12* ENGINE TYPE «NO MODEL: JT90-7
RATED THRUST: 45500.
ENGINE TOTAL TIME: -0. MRS
TINE SINCE HOT SECTION OVERHAUL: -0. HRS
TINE SINCF:
NI COMPRESSOR OVERHAUL: -o. HRS
N2 COMPRESSOR OVERHAUL: -o. HRS
COKBUSTOR CAN REPLACEMENT: -0. MRS
FIRST STAGE NOJZLF GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
N? TURBINE OVERHAUL: -o. HRS
FUEL: JP-4 FUEL H/C RATIO: 2.000
OPERATIONAL DATA «»«»»«»«
INLET AIR TEMPERATURE, DEGREES f- START 90.00 FINISH 79.90
ATMOSPHERIC PRESSURE: START jq.es FINISH 29.95
INLET AIR HUMIDITY, 18S H20/L8 AIR: 0.008?
RELATIVE HUMIDITY: -0.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 160.00, FLO* RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: i.00
NUMBER OF TESTS: 6
COMMENTS:
8UPNFR CONFIGURATION - 10
SERIAL NUMBER:
P-665602
CLOCK
TIME
1609.00
1616.00
1621.00
1630.00
1637.00
1638.00
1648.00
1653.00
TEST
MODE
I/ 0
2/ 1
I/ 2
4/ 1
5/ 4
6/ 5
7/ 6
B/ I
POMER
THRUST, LBS
OR
SHP
45787.00
42070.00
39345.00
15544.00
10448.00
3207.00
3570.00
4009.00
PERCENT
RATED
T.O.
100
92
86
78
66
7
7
8
ENGINE
SPEED
RPM
NI N2
MEASURED
FUFL
FLOW
LB/HR
100
92
86
78
66
7
7
8
3341.00
3233.00
3152. OC
1036.00
2853.00
1000.00
1056.00
1117.00
7478.00
7411.00
7349.00
7260.00
7125.00
5017.00
5161.00
5281.00
16549.00
14921.00
13827.00
12307.00
10147.00
1595.00
1797.00
1926. CO
GAS GEN
AIR FlOu
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CALC
F/A
0.023000
0.022000
0.021000
0.020000
0.018000
0.010000
0.010000
0.010000
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIO
OEGRFFS F EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
1.45
1.40
1.16
1.31
1.25
1.02
1.02
1.02
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PUHER
PERCENT
RATFD
1.0.
100
92
B6
78
66
7
7
EXHAUST
GAS
TEMP
DEGRtES f
10X0.00
1038.00
1009.00
970.00
916. 00
730.00
679.00
682.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
co
(WET)
PPMV
7.30
6.50
6.10
5.70
6.40
410.60
351.20
314.60
CO
2
(UFTI
PERCENT V
3.92
3.72
3.57
3.35
3.10
1.60
1.63
1.67
THC
(UETI
PPMV
NO NO
I HE II ?
PPMV IWETI
PPMV
3.92
3.72
3.57
3.35
3.10
1.60
1.63
1.67
8.80
18. 10
13.30
9.50
7.40
152.60
114.70
92.80
442.70
177.90
319.90
256.10
0.0
10.40
11.50
12.60
26.40
23.80
19.70
16.70
11.80
15.00
16.30
17.10
NO
X
I MET I
PPMV
469.10
401.70
139.60
272.80
13. 60
45.40
27.80
29.70
ALDEHYDES SMOKF PAHTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
POMER
PERCENT
RATED
T.O.
100
92
86
78
66
7
7
8
MASS EMI
CO
LB/ 1«
LB FUEL
0.17
0.15
0.14
0.14
0.41
49. 51
41.83
16.72
MASS FM1
HC
LU/IK
LB FUEL
0.26
0.56
0.43
0.12
0.27
10.54
7.82
6.20
MASS EMI
NU2
LB/1K
LB FUFL
2.21
2. 10
1.B1
1.61
1.46
2.97
1.19
I.2H
MASS FMI
C07
LO/U
LB FUEL
1136.46
3115.67
3136.04
3116. 12
3136.15
3011.05
1050.55
1063.02
MASS EMI
ND
LB/1K
L» FUEL
37.03
11. 10
29. IB
25.06
n.o
2.0<,
?.25
2.42
MASS EMI
NIIX
LB/1K
LB FUEL
19.24
35.40
11.19
26.70
1.46
8.99
5.44
5.69
MASS EMI
cn
LB/hR
6.15
5.20
4.72
4.18
4.26
78.96
75.17
7C.71
MASS E"l
HC
LB/HR
4.25
a. 10
5.B9
3.99
2.82
16.81
14.06
11.95
MASS EMI
N02
Lfl/HR
36.54
31.29
25.01
20.12
15.10
4.74
5.73
6.31
MASS EMI
C02
LB/HR
51905.22
46787.35
43362.03
38598.70
32451.80
4834.52
5481.34
5899.38
MASS EMI
NO
L8/HP
612. BO
496.87
406.20
308.47
0.0
3.29
4.04
4.65
MASS EMI
NOX
LB/HR
649.34
528.16
431.21
328.59
15.10
14.34
9.77
10.97
POWER
PERCENT
RATED
T.D.
100
92
86
78
66
CO
LB/IKIFH-HR
0.134
0.124
0. 120
O.IIB
0. 140
24.622
21.057
17.641
LB/1KKTH-HK
1133.624
1112.111
1112.09H
1035.942
1065.811
1507.491
1515.511
1471.S14
THC
LB/1KHTH-MR
0.091
0.197
0.150
0. 112
0.093
5.241
3.919
2.9B1
NO
LO/1K«TH-'W
11.184
11.811
10.124
8.679
0.0
1.024
1.133
1 .161
L3/1KKTH-HR
0.798
0. 744
0.636
0.566
0.496
1.477
1.605
1.575
NO
X
LB/IKITH-HR
14.182
12.554
10.960
9.245
0.496
4.472
2.738
2.736
llV-282
-------
CAL ID NUMBERl 32* ENGINE TYPE AND NOOELt JI90-7
TEST ORGANIZATION! PRATT 4 WHITNEY
SERIAL NUMBER: P-68S602
NODE FRACTIONAL
TAXI-IDLE
TAKEOFF
CLIMBDUT
APPROACH
TAXI-IDLE
POWER
0.0 TO
I. 000
0.850
0.300
O.OTO
POKER
f TH
3185.0
45500.0
38673.0
136SO.O
3185.0
EMISSION
RATE
LB/HR
83.413
8.07*
6.6B6
21.469
83.413
FUEL USAGE
RATE HT FACTOR
LB/HR
1633.514
16*76.223
13645. 39B
4951.391
1633.519
.000
.000
.000
.000
.000
TIME IN
MODE
MIN.
19.00
0.70
2.20
4.00
7.00
CO
MASS
LBS.
26.414
0.094
0.245
1.431
9.732
FUEL
MASS
LBS.
517.28
192.25
500.33
330.09
190.58
LB CO /
IK LB FUEL
51.064
0.490
0.490
4.336
51.064
ENERGY
1 TM-MR
1008.58
S30.83
1418.08
910.00
371.56
LB CO /
1 TH-HR
0.02619
0.00018
0.00017
0.00157
0.02619
TOTAL FOR CYCLE: 37.916
LBS POLLUTANT/IK LB FUEL/CYCLE! 21.910
LBS POLLUTANT/IK LB TH-HR/CYCLE: 8.944
IBS POLLUTANT/1000K LB TH AT T.O.I 0.207
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.070
1.000
0.850
0.300
0.070
FRACTIONAL
POMER
0.070
1.000
0.850
0.300
0.070
POMER
1 TH
3163.0
45500.0
36675.0
13650.0
3165.0
POWER
1 TH
3185.0
45500.0
38675.0
13650.0
3185.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
17.412 1633.519
4.900 16478.223
4.781 13645.396
3.104 4951.391
17.412 1633.519
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE HT
LB/HR LB/HR
8.688 1633.519
654.127 16478.223
414.190 13645.398
37.925 4951.391
8.686 1633.519
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
USAGE TIME IN
FACTOR MODE
HIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.I
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-MR/CYCLE:
LB TH AT T.O.:
HC
MASS
LBS.
5.514
0.057
0.175
0.207
2.031
7.984
4.614
1.664
1.256
NOX
MASS
LBS.
2.751
7.631
15.187
3.862
1.014
30.445
17.593
7.182
167.725
FUEL
MASS
LBS.
517.28
192.25
500.33
330.09
190.56
1730.53
FUEL
MASS
L8S.
517.28
192.25
500.33
330.09
190.58
1730.53
LB HC /
IK LB FUEL
10.659
0.297
0.350
0.627
10.659
LB NOX/
IK LB FUEL
5.319
39.696
30.354
11.699
5.319
ENERGY
f TH-HR
1008.58
530.83
1418.08
910.00
371.58
4239.08
ENERGY
1 TH-HR
IOOB.58
330.83
1418.08
910.00
371.58
4239.08
LB HC /
1 TH-HR
0.00547
0.00011
0.00012
0.00023
0.00547
LB NOX/
1 TH-HR
0.00273
O.OI43B
0.01071
0.00424
0.00273
IV-283
-------
OATtl 7/29/71
TEST ORGANIZATION: PRATT £ WHITNEY
ENGINE SUPPLIES: PRATT AND WHITNEY
ENGINE DMA
CtL 10 NUMBED: 325 ENGINE TYPE AND MODELi JT9D-7
RATED IHRUST: 45500.
FNGIhE TnTAL TIHF: -0. HRS
TIME SINCE HOT SECTION OVERHAUL: -0. HRS
TIME S1NCEI
Nl COMPRESSOR OVERHAUL: -0. HRS
N2 COMPRESSOR OVERHAUL: -n. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAULl -0. HRS
NI TURBINE OVERHAUL: -o. HRS
N2 TURBINE OVERHAUL: 0. HRS
SERIAL NUMBER!
FUEL! JP-» FUEL H/C RATIO: 2.000
OPERATIONAL DATA «»««
INLET AIR TFMPERATURE, DEGREES F: STAUT 79.70 FINISH 75.60
ATMOSPHERIC PRESSURE: START 21.95 FINISH 29.85
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0154
RELATIVE HUMIDITY: -0.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, PLOW RATEi LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: a
COMMENTS:
BURNER CONFIGURATION - 10
2.00
CLOCK TEST POWER
TIMF MODE THRUST,LBS PERCFNT
OR RATED
SHP r.O.
1101.00 I/ 0 2626.00
1129.00 21 I 3205.00
1138.00 I/ 2 1595.00
1152.00 4/ 1 43656.00
1413.00 5/ 4 32549.00
1947.00 6/ 5 30066.00
2007.00 7/ 6 36393.00
2020.00 8/ 7 39943.00
ENGINF
SPEED
RPM
Nl N2
MEASURED
FUEL
FLOW
LB/HR
5
7
7
95
71
66
79
87
918.00
1015.00
1071.00
5290.00
2939.00
2828.00
3053.00
3165.00
4860.00
5093.00
5218.00
7558.00
7325.00
7189.00
7395.00
7490. On
1555.00
1707.00
1811.00
15364.00
I099R.OO
9912.00
12323.00
11712.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-o.no
-0.00
-0.00
-0.00
CALC
F/A
0.010000
0.009000
0.009000
0.021000
0.017000
0.016000
0.018000
0.019000
COMPRESSOR
DISCHARGE
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
.01
.02
.02
.43
.28
.24
.32
.37
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.10
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
5
7
7
95
71
66
79
87
EXHAUST
GAS
TEMP
DEGREES F
677.00
671,00
668.00
1052.00
932.00
8B7.00
956.00
IC03.00
EXHAUST
GAS
PRESSURE
PS I A
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO
(MET)
PPHV
572.70
473.70
429.90
12.00
10.10
21 .20
16.10
12.20
CO
2
(WEU
PERCENT V
1.74
1.73
I.7S
3.97
3.40
2.80
3.32
1.51
THC
(WET)
PPMV
NO NO
(WED 2
PPMV IUEII
PPMV
ALDEHYDES SMOKE PARTICUIATES
1.74
1.73
1.7S
3.97
3.40
2.80
3.32
1.51
401 .90
2ao.io
226.50
5.20
4. 10
2.10
0.80
1.20
9.60
9.10
B.UO
265.60
209.10
167.30
204.90
219.20
7.20
10.60
12.90
17.30
16.70
6.20
14.60
15.40
IkFTI
PPMV
16.80
19.70
21.70
282.90
225.80
273.50
219.50
214.60
-0.00
-o.no
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
-o.oo
-0.00
-o.oo
-o.oo
-0.00
-0.00
-0.00
-n.oo
-o.oo
-0.00
-o.on
-n.oo
-o.oo
-o.oo
-o.oo
POWER
PFRCENI
RATED
T.O.
5
7
7
95
71
66
79
87
MASS EMI
CO
LB/IK
LB FUFL
62.24
52.40
47.28
0.60
1.06
1.51
0.97
0.69
MASS EMI
HC
LR/1K
LB FUEL
75.02
17.74
14.27
0.15
0.14
0.09
0.03
0.04
1ASS EH I
N02
UI/1K
LB FUFL
1.29
1.91
2.33
1.43
1.61
n.73
1.44
1.44
MASS CMI
co?
LB/1K
LB FUEL
2971.12
3006.71
3024.31
3136.39
3135.70
3135. 14
3136.15
3136.55
MASS EMI
NO
LB/1K
LB FUFL
1.71
1.65
1 .59
21.94
20.16
19.58
20.23
20. 48
MASS FMI
NOX
LP/1K
LB FUEL
3.00
3.58
3.92
23.16
21.77
32.01
21.68
21.92
MASS EMI
CO
LB/HR
96.79
99.44
85.61
9.27
1 1.68
14.97
11.93
9.51
MASS FMI
MC
LB/HR
39.90
30.29
25.84
2.30
1.52
0.85
0.14
0.54
MASS EMI
NO?
Le/Ht
2.00
3.29
4.22
21.95
17.71
7.19
17.77
19.71
MASS EMI
CO 2
LB/HR
4620.19
5132.49
5477.0?
48167.41
14486.40
31075.46
3B646.75
41009.33
MASS EMI
NO
LB/MR
2.46
2.12
2.88
317.02
221.72
194.11
249.14
280.78
MASS E.MI
NOX
LB/hR
4.66
6.11
7.10
158.97
219.43
117.32
267.11
300.51
POWER
PERCENT
RATED
T.O.
5
7
7
95
71
66
79
87
CO
LB/U«TH-MR
16.957
27.907
23.920
0.21?
0. 159
0.498
0.328
0. 238
Lf/lKITH-HR
1759.480
1601.40?
1523.509
1101.799
1057.B98
1031.575
1061.928
1076.743
THC
LR/1K*TH-HR
14.814
9.451
7. IBB
0.051
n.n47
0.02B
0.009
0.013
NO
LR/1K4TH-HR
I.015
0.981
0.801
7.720
6.601
6.456
6.851
7.030
LB/1KHTH-HR
0.761
1.026
1.174
0.503
0.54}
0.239
0.488
(1.494
LB/ I MTH-HR
1.776
1.906
I .975
8.223
7.145
10.554
7.340
7.521
IV-284
-------
CAL 10 NUMBER: 325 ENGINE TYPE AND MODEL: JMD-T
TEST ORGANIIATION: PRATT C NHITNEV
SERIAL NUMBER! P-663071
MODE FRACTIONAL
POMER
TAXI-IDLE
TAKEOFF
CLIHBOUr
APPROACH
TAXI-IDLE
0.070
I. 000
0.850
0.300
O.OTO
POMER
TH
3183.
43500.
386T5.
13630.
3185.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
i)8. 475 1824.762
12.982 16079.000
13.323 13221.047
36.413 4969.230
98.475 1824.762
USAGE TIME IN
MT FACTOR MODE
NIN.
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POMER
O.OTO
1.000
0.890
0.300
O.OTO
POMER
1 TH
3183.
43300.
386T3.
13630.
31B3.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
31.437 1824.762
0.0 16079.000
0.404 13221.047
3. 70B 4969.230
31.437 1824.762
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
MT FACTOR MODE
MIN.
TOTAL FOR CYCLEI
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
ClIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
O.OTO
1.000
0.850
0.300
O.OTO
POWER
t TH
3IB3.
43500.
38675.
13650.
3185.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
9.403 1824.762
578.342 16079.000
402.483 13221.047
61.486 4969.230
9.403 1824.762
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
HT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IOOOK
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
L«S.
31.184
0.151
0.489
2.428
11.489
45.740
25.491
10.790
0.333
HC
MASS
LBS.
9.955
0.0
0.015
0.247
3.668
13.883
7.738
3.275
0.0
NO*
MASS
LBS.
2.978
6.750
14.758
4.099
1.097
29.681
16.541
7.002
148.344
FUEL
MASS
LBS.
577.84
187.59
484.77
331.28
212.89
1794.37
FUEL
MASS
LBS.
577.84
187.59
484.77
331.28
212.89
1794.37
FUEL
MASS
LBS.
577.84
187.59
484.77
331.28
212.89
1794.37
LB CO /
IK LB FUEL
53.966
0.807
1.008
7.328
53.966
LB HC /
IK LB FUEL
17.228
0.0
0.031
0.746
17.228
LB NOX/
IK IB FUEL
5.153
35.981
30.443
12.373
5.153
ENERGY
t TH-HR
1008.58
530.83
1418.08
910.00
371.38
4239.08
ENERGY
TH-HR
1008.58
530.83
1418.08
910.00
371.58
4239.08
ENERGY
TH-HR
1008.58
530.83
1418.08
910.00
371.58
4239.08
LB CO /
1 TH-HR
0.03092
0.00029
0.00034
0.00267
0.03092
LB HC /
TH-HR
0.00987
0.0
0.00001
0.00027
0.00987
LB NOX/
TH-HR
0.00295
0.01272
0.01041
0.00450
0.00295
IV-285
-------
DATE: 8/ 5/71
TEST ORGANIZATION: PRATT t HHITNEY
ENGINE SUPPLIER: PRATT AND WHITNEY
ENGINE DATA
CAL ID NUMBER: 326 ENGINE TYPE AND MODEL: JT90-7
RATED THRUST: 45500.
ENGINE TOTAL TIME: -0. MRS
TIME SINCE HOT SECTION OVERHAUL: -0. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: -o. MRS
NZ COMPRESSOR OVERHAUL: -o. HRS
COHBUSTOR CAN REPLACEMENT: -o. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
Nl TURBINE OVERHAUL: -0. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL: JP-4 FUEL H/C RATIO: 2.000
OPERATIONAL DATA «««»««»«»»»«»««««««
INLFT AIR TEMPERATURE, DEGREES F: START 76.00 FINISH 74.90
ATMOSPHERIC PRESSURE: START 24.85 FINISH 21.82
INLET AIR HUMIDITY, IBS H20/LB AIR: 0.0074
RELATIVE HUMIDITY: -0.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
BUHNER CONFIGURATION - R/M
SERIAL NUMBER 1
CLOCK
TIME
1611.00
1624.00
1617.00
1835.00
1842.00
TESI
M10E
I/ 0
2/ 1
I/ 2
4/ 3
5/ 4
POWER
THRUST,LRS PERCENT
01 RATED
SHP T.O.
4559.00
14868.00
41250.00
4562.00
2905.00
10
76
90
10
ENGINE
SPEED
RPM
Nl N2
MEASURED
FUEL
FLOW
I 8/HR
1276.00 5549.00 2271.00
3131.00 7316.00 13605.00
3271.00 7620.00 16411.00
1276.OC 5544.00 2273.00
1023.00 5036.00 1720.00
GAS GEN
AIR FLOW
LB/SfC
-0.00
-0.00
-0.00
-0.00
-0.00
CALC
F/A
0.010000
0.020000
0.022000
0.010000
0.010000
COMPRESSOR
DISCHARGE
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.03
1.36
1.46
1.03
1.02
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-o.no
POWER
PERCENT
RATED
T.O.
10
76
90
10
6
EXHAUS1
GAS
TEMP
DEGREES f
670.00
9110.00
1054.00
670.no
659.00
EXHAUST
GAS
PRESSURE
PSI A
-0.00
-0.00
-0.00
-0.00
-0.00
CO
IWETI
BPXV
75*. 20
3.40
1.10
271.00
425.70
CO
2
(WET)
PERCENI V
1.71
1.39
3.57
1.65
1.38
THC
IWET)
PPMV
47.60
1. 10
0.40
56.00
141.90
NO
(WFTI
PPMV
4 .90
2/2.30
421.10
16.10
0.30
NO
2
(WETI
PPMV
16.20
17.50
25. )0
14.90
4.80
NO
X
IWET)
PPMV
21.10
289.80
446.40
31.00
5.10
ALDEHYDES
-0.00
-0.00
-0.00
-0.00
-0.00
SMOKE
-0.00
-0.00
-0.00
-o.on
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
10
76
90
10
6
MASS EMI
CO
LB/1K
LB FUEL
29.40
0.20
0.17
32. 16
59. I 7
*ASS EMI
HC
LR/1K
LB FUEL
3.13
0.04
0.01
3.11
1 1. 10
MASS FMI
N02
LI/IK
LB FUEL
3.05
1.69
2.32
2.90
1 .11)
MASS EMI
C02
LB/IK
LB FUEL
3082.97
3117.33
1137.44
3076.77
3013.79
MASS EMI
NO
LB/1K
LB FUEL
0.92
26.34
38.69
3.14
0.07
MASS EMI
NC1X
LB/1K
LB FUEL
3.98
28.0'.
41.01
6.04
1.16
MASS EMI
CO
LB/HR
66.76
2.72
2.fl5
71. 10
101.77
MASS EMI
HC
LB/HP
7.10
0.50
0.21
8.65
19.43
MASS [Ml
NO 2
LB/HR
6.93
23.03
18. 15
6.60
1.88
MASS EMI
C02
LB/HR
7001.41
42683.35
514R8.4A
6993.49
5183.71
MASS EMI
NO
Lfl/HR
2.10
358.42
634.91
7.13
0. 12
MASS EMI
NOX
LB/HR
9.03
381.45
673.05
13.74
2.00
POWER
PERCENT
RATED
T.O.
10
76
90
10
6
CD
LB/1KKTH-HR
14.644
0.078
0.069
16.025
35.033
1515.737
1224.141
124R.206
1512.988
1734.410
THC
LB/ IMTH-HR
1.558
0.014
0.005
1 .696
6.638
NO
L9/1KHTH-HK
0.4bC
10.779
15.392
LB/1KKTH-HR
1.571
0.661
0.925
1.447
0.649
LB/IKHTH-HR
1.981
10.940
16.116
3.011
0.689
IV-286
-------
C»L ID NUNBERI 326 ENGINE TYPE AND NODEL! JT9D-T
TEST ORGANIIATIONl PRATT ( MHITNEY
SERIU NUNBERI P683614
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.070
1.000
O.BSO
0.300
0.070
POKER
f TH
3185.0
45500.0
38675.0
13650.0
3113.0
EMISSION FUEL
RATE RATE
L6/HR LB/HR
90.684 16*3.798
6.516 16075.172
9.465 15166.035
38.765 3470.563
90.684 1643.748
USAGE TINE IN
NT FACTOR NODE
NIN. .
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS PQUUTANT/IK IB
LSS POLLUTANT/1000K
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POKER
0.070
1.000
0.850
0.300
0.070
POKER
1 TH
3185.0
45500.0
38675.0
13650.0
3189.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
14.615 1643.748
0.212 18075.172
0.879 15166.035
2.122 5470.563
14.615 1643.798
.000 14.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLEl
LB TH AT T.O.I
USAGE TINE IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLE!
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
KOOE
FRACTIONAL
POKER
TAXI-IDLE 0.070
TAKEOFF 1.000
CLINBOUT 0.850
APPROACH 0.300
TAXI-IDLE 0.070
POWER
TH
3185.0
45500.0
38675.0
13690.0
3185.0
EMISSION FUEL
RATE RATE
LB/HR L8/HR
3.624 1643.798
882.182 18075.172
526.113 13166.035
52.943 5470.363
3.624 1643.798
.000 14.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL /CYC LEI
TH-HR/CYCLEl
LB TH AT T.O.I
USAGE TINE IN
UT FACTOR NODE
MIN.
TOTAL FOR CYCLE!
LBS POLLUTANT/IK IB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
.000 14.00
.000 O.TO
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLEI
TM-HR /CYCLE!
LB TH AT T.O.I
CO
NASS
LBS.
28.717
0.076
0.347
2.384
10.580
42.304
22.942
9.979
0.167
HC
NASS
LBS.
4.628
0.002
0.032
0.141
1.705
6.509
3.530
1.536
0.034
NOX
NASS
LBS.
1.148
10.292
14.241
3.530
0.423
34.683
18.809
8.182
226.200
FUEL
NASS
LBS.
520.54
210.88
556.09
364.70
191.78
1843.98
FUEL
NASS
LBS.
520.54
210.88
536.09
364.70
191.78
1843.98
FUEL
MASS
LBS.
520.54
210.88
556.09
364.70
191.78
1843.48
LB CO /
IK LB FUEL
55.167
0.361
0.624
7.086
55.167
LB HC /
IK LB FUEL
8.841
0.012
0.058
0.388
8.891
LB NOX/
IK LB FUEL
2.205
48.806
34.640
4.678
2.205
ENERGY
TH-HR
1008.38
530.83
1418.08
410.00
371.58
4234.08
ENERGY
1 TH-HR
1008.58
530.83
1418.08
910.00
371.38
4234.08
ENERGY
f TH-HR
1008.58
330.83
1418.08
410.00
371.58
4234.08
LB
1
0
0
0
0
0
LB
1
0
0
0
0
0
LB
f
CO /
TH-HR
.028*7
.00014
.00024
.00284
.02(47
HC /
TH-HR
.00454
.00000
.00002
.00016
.00439
NOX/
TH-HR
0.00114
0.01434
0.01160
0.00388
0.00114
IV-287
-------
DATE: B/ i/71
TEST ORGANIZATION: PRATT C WHITNEY
ENGINE SUPPLIER: PRATT UNO WHITNEY
ENGINE DATA
C»L ID NUNBFR: 355 ENGINE TVPE AND MODEL: JT9D-7
RATED THRUST: 45500.
ENGINE TOTAL TIME: -0. MRS
TIME SINCE HOT SECTION OVERHAUL: -0. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: -o. HRS
HZ COMPRESSOR OVERHAUL: -o. MRS
COMBUSTOR CAN REPLACEMENT: -o. MRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
Nl TURBINE OVERHAUL: -0. HRS
NZ TURBINE OVERHAUL: -o. HRS
FUEL: jp-4 FUEL H/C RATIO: 2.000
OPERATIONAL DATA «««««..»««.««.«....»...«.«..............».........
INLET AIR TEMPERATUREi DEGREES F: START 76.30 FINISH 74.90
ATMOSPHERIC PRESSURE: START 29.87 FINISH 29.67
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0074
RFLAT1VE HUMIDITY: -0.00 PERCENT
SAMPLE LINE: TEMPERATURE, CEGREES C: 150.00, FL04 RATE, LITFRS/M1N:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES HG
SERIAL NUMBER:
CLOCK
TIME
1612.00
1624.00
1632.00
1030.00
1043.00
TEST
MODE
I/ 0
2/ 1
3/ 2
4/ 3
5/ 4
PDWFR
IHRUST.LBS PERCENT
OR RATFO
SHP
5325.00
39014.00
45B34.00
5330.00
3397.00
T.O.
11
85
100
11
7
ENGINE
SPEED
RPM
Nl
1276.00
3131.00
3271.00
1276.00
1023.00
N2
5453.00
7220.00
7405.00
5457.00
4958.00
MEASURED
FUFL
FLOW
LB/HR
2724.00
13464.00
16752.00
2230.00
1685.00
GAS GEN
AIR FLOW
LB/SEC
CALC COMPRESSOR ENGINE
F/A DISCHARGE PRESSURE
TEMP RATIO
DEGREES F EPR
-0.00
-0.00
-0.00
-0.00
-0.00
0.008600
0.017000
o.oieooo
O.OOB600
O.OOR600
-0
-0
-0
-0
-0
.00
.00
.00
.00
.00
.03
.36
.46
.03
.02
TURBINE
INLET
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
11
85
100
11
7
EXHAUST
GAS
TEMP
DEGREES F
670.00
9HO.OO
1054.00
670.00
659.00
EXHAUST
GAS
PRESSURE
PS I A
-0.00
-n.io
-0.00
-0.00
-0.00
co
IWETI
PPMV
256.00
3.40
1.10
271.00
475.70
CO
2
IHET)
PERCENT V
1.71
3.39
3.57
1.65
1.38
THC
IWETI
PPMV
47.60
1.10
0.40
56.00
141.90
NO
1 WET)
PPMV
7.90
272.30
421.10
16.10
0.3C
NO
2
1 WET)
PPMV
16.20
17.50
25.30
14.90
7.80
ALDEHYDES SMOKE PARTICULATES
IWETI
PPMV
71.10
289.80
446.40
31.00
5.10
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.f).
11
85
100
II
MASS EMI
cn
LR/1K
LR FUEL
29.38
0.20
0.17
32. 16
59. 17
MASS EMI
HC
IB/IK
LB FUEL
1.13
0.04
0.01
3. PI
1 1.30
MASS Ell
NT?
Lfl/lK
LB FUFL
3.05
1 .69
2.32
7.90
1.7S
MASS EMI
C02
LR/1K
Lfl FUEL
3083.01
3137.33
3137.44
3076.77
3013. 79
"ASS EMI
NO
I.I/ IK
L3 FUEL
1.49
26.34
3H.69
3.14
0.07
MASS EMI
NQX
Lfl/lK
LB FUEL
3.98
28.04
41.01
6.04
1.16
MASS FM
CO
LB/HR
65.33
2.70
2.82
71.72
99.70
MASS EMI
HC
LB/HR
MASS EMI
NU2
LB/HR
MASS EMI
CI12
LB/HR
MASS EMI
NO
Lfl/HR
MASS EMI
NQX
LR/HR
6.96
0.50
0.21
8.49
19.03
6.79
22.80
37.78
6.48
3.00
6856.61
42240.99
50989.62
6961.19
5078.23
3.31
354.70
628.75
7.00
0.12
8.84
377.50
666.53
13.48
1.96
POWER
PERCENT
RATED
T.O.
11
85
100
11
7
CU
LD/IKWTH-HP
12.269
0.069
0.061
13.456
29.350
CO
7
IK* TH-HR
1237.676
1082.714
1117.485
1287.277
1494.917
THC
L P/l K« TH-HR
1.106
0.013
0.005
1 .593
5.603
NO
LB/ 1 K«TH-Hft
0.627
9.092
11.718
1.313
0.034
LR/1KHTH-HR
1.275
0.584
1.824
1.215
0.8H3
NO
X
LB/1K»TH-HR
1.661
9.676
14.542
2.528
0.578
IV-288
-------
CM. 10 NUMBER I 355 ENGINE TYPE AND MODEL: JT90-7
TEST ORGANIZATION! PRATT I MHITNEY
SERIAL NUMBER: P689614
MODE FRACTIONAL
POMER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
0.070
1.000
0.890
O.JOO
0.070
POMER
TH
3169.
45500.
38675.
13690.
1189.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
79.733 1930.134
1.096 16160.711
9.690 13379.939
98.261 4443.086
79.733 1930.134
USAGE TIME IN
NT FACTOR MODE
MIN.
TOTAL FOR CrCLE:
LBS POLLUTANT/ IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.070
1.000
0.350
0.300
0.070
POMER
1 TH
3189.
49900.
38679.
13690.
3189.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
16.990 1930.134
0.970 16160.711
0.801 13379.935
4.438 4443.086
16.990 1910.134
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLEl
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TIME IN
MT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POMER
0.070
1.000
0.850
0.300
O.OTO
POMER
TH
3189.
49900.
38679.
13690.
3189.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
4.811 1910.114
641.069 16160.711
379.29] 13179.939
92.991 4443.086
4.811 1930.134
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE TINE IN
MT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LSS POLLUTANT/1000K
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE I
LB TH AT T.O.:
CO
MASS
LBS.
29.249
0.013
0.394
3.884
9.102
38.802
23.689
9.191
0.028
HC
MASS
LBS.
9.368
0.011
0.029
0.296
1.978
7.682
4.689
1.812
0.249
NOX
MASS
LBS.
1.921
7.479
13.907
3.906
0.961
26.977
16.467
6.164
164.376
FUEL
MASS
LBS.
484.94
188.94
490.44
296.21
178.92
1638.24
FUEL
MASS
LBS.
484.94
188.94
490.44
296.21
178.92
1638.24
FUEL
MASS
LBS.
484.94
188.94
490.44
296.21
178.92
1618.24
LB CO /
IK 18 FUEL
92.109
0.068
0.721
11.113
92.109
LB HC /
IK LB FUEL
11.078
0.060
0.060
0.999
11.078
LB NOX/
IK LB FUEL
1.144
39.668
28.197
11.837
3.144
ENERGY
TH-HR
1008.98
910.81
1418.08
910.00
371.98
4239.08
ENERGY
1 TH-HR
1008.58
910.83
1418.08
910.00
371.98
4239.08
ENERGY
f TH-HR
1008.98
930.83
1418.08
910.00
371.98
4239.08
LB CO /
TH-HR
0.02903
0.00002
0.00029
0.00427
0.02903
LB HC /
» TH-HR
0.00532
0.00002
0.00002
0.00033
0.00932
LB NOX/
TH-KR
0.00151
0.01409
0.00981
0.00389
0.00191
IV-289
-------
DATEI 6/10/71
TEST ORGANIZATION: A1RESEARCH
ENGINE SUPPLIER: AIRESEARCH
ENGINE DATA «............».«.«..............».».«».4«......»«
C»L ID NUMBED: 29 ENGINE TYPE AND MODEL: TFE 731-2
SERIAL NUMBER:
RATED THRUST: 2800.
ENGINE TOTAL TIME: 0. MRS
TINE SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: o. MRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL! 0. HRS
N2 TURBINE OVERHAUL: o. HRS
FUEL! AV KEROS FUEL H/C RATIO: 1.929
OPERATIONAL DATA ««»»««««««..
INLET AIR TEMPERATUREt DEGREES F: START 91.00 FINISH 91.00
ATMOSPHERIC PRESSURE: START 26.55 FINISH 29.55
INLET AIR HUMIDITY, L8S H20/L9 >IR: 0.0036
RFLATIVF HUMIDITY: 10.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: -0.00, FLOH RATE, LITERS/MIX: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 6
COMMENTS:
ICK
ME
0.00
0.00
0.00
0.00
o.oo
0.00
TEST
MOOE
I/ 0
2/ 1
6/ 2
11/6
If./ 11
20/16
POWER ENGINE
THHUST.LBS PERCENT SPEED
OR RATED RPM
SHP
193.00
406.00
1045.00
1637.00
2222.00
2605.00
T.O.
6
14
37
59
79
91
Nl
5760.00
8470.00
13040.00
15710.00
17650.00
19560.00
N2
16800.00
21070.00
25370.00
27020.00
27960.00
28430.00
MEASURED
FUEL
FLOW
LB/HR
177.00
785.00
597.00
858.00
1150.00
1330.00
GAS GEN
AIR FLOW
LB/SEC
4.87
7.58
14.21
19. OB
23.79
26.60
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.010900
0.011300
0.012400
0.013500
0.014500
0.015000
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POUEP.
PERCENT
RATED
T.n.
&
14
37
58
79
93
FXHAUST
GAS
TEMP
DEGRFES F
954.00
945.00
1171.00
1329.00
I 461 .00
1517.00
FXHAUST
GAS
PRESSURE
PS I A
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CO CO
1UET) 2
PPMV I»ETI
PEKCENT V
463.40
763.60
149.30
65.50
37.70
24.70
2.20
2 .60
2.96
THC
(MET!
PPMV
253.80
84.70
29.90
3.90
1.20
0.80
NO NO
(NET) 2
PPKV IWETI
PPMV
ALDEHYDES SHHKE PARTICULATES
6.2P
14.50
34.50
58.00
94.60
110.30
7.70
6.50
9.00
6.80
5.80
6.20
IHET)
PPHV
13.90
21.10
42.60
64.80
90.40
116. Stl
-0.00
-0.00
-0.00
-o.oo
-o.oo
-o.oo
-o.oo
-0.00
-0.00
-o.oo
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-o.uo
-0.00
POKER
PERCENT
RATED
T.O.
6
14
37
59
79
93
MASS FMI
CO
IB/IK
L8 FUEL
44.26
23.68
11.45
4. 59
2.58
1.64
MASS EMI
HC
LR/IK
L8 FUEL
13.89
4.36
1.27
0. 16
0.05
0.03
MASS FMI
N02
L9/IK
LB FUEL
1.21
0.96
1.01
1.78
0.65
0.67
MASS EMI
C02
LR/IK
L9 FUEL
3046.44
3104.91
3132.59
3146.43
3149.90
3151.41
MASS EMI
NO
LB/1K
LB FUEL
0.97
2.14
4.35
6.67
9.51
11.99
MASS EMI
NOX
LB/1K
Lfl FUEL
2.19
1.11
5.37
7.45
10. 16
12.67
MASS EMI
CO
LB/HR
7.83
6.75
6.72
3.93
2.97
2.17
MASS EM
HC
LB/HR
2.46
1.24
0.75
0.13
0.05
0.04
MASS EMI
ND2
LB/HR
MASS EMI
Cfl2
LB/HR
MASS EMI
NO
IB/MR
MASS FMI
NOX
LB/HR
0.21
0.27
0.59
0.67
0.75
0.90
539.22
994.90
1939.93
2699.64
3622.16
4191.38
0.17
0.61
7.55
5.77
10.93
15.95
0.39
0.99
3.15
6.39
11.69
16.85
POUeR
PERCENT
RATED
T.O.
6
14
37
56
79
93
CO
LB/IKHTH-MR
40.591
16.621
6.431
2.404
1.335
0.935
Lfl/lK«TH-HK
7793.881
2179.554
1759.650
1649.137
1610.227
1608.975
THC
LB/1K«TH-H«
12.732
3.059
0.713
0.097
0.024
0.015
NO
L FW 1KBTH-HR
O.H92
1.502
2.441
3.496
4.921
6.123
H/IKHTH-HR
1. 108
0.673
0.566
0.410
0.337
0.344
NO
X
LB/1K«TH-H«
2.000
2.185
3.014
3.906
5.258
6.467
IV-290
-------
CAL ID NUMBERI 29 ENGINE TYPE AND NODEll Iff 731-2
TEST ORGANIZATION! AIRESEARCH
SERIAL NUMBERI 7305-2
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
MODE
TAXI-IDLE
TAKEOFF
CLIMB OUT
APPROACH
TAXI-IOLE
FRACTIONAL
POKER
0.060
1.000
0.900
0.300
0.060
FRACTIONAL
POKER
0.060
1.000
0.900
0.300
0.060
FRACTIONAL
POWER
0.060
1.000
0.900
0.300
0.060
POHER
f TH
168.0
2600.0
2520.0
8*0.0
168.0
POKER
1 TH
168.0
2800.0
2520.0
840.0
168.0
POWER
t TH
168.0
2800.0
2520.0
8*0.0
168.0
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/NR L8/HR MIN.
.ITT 169.623 .000 19.00
.617 1387.052 .000 0.50
.26* 1282.9*7 .000 2.50
.90* 477.032 .000 4.50
.177 169.623 .000 7.00
TOTAL FOR CVClEl
LBS POLLUTANT/IK LB FUEL/CTCLEI
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE NT FACTOR MODE
LB/HR LB/HR MIN.
2.600 169.623 1.000 19.00
0.059 1387.052 1.000 0.50
0.087 1282.9*7 1.000 2.50
0.9*7 477.032 1.000 4.50
2.600 169.623 1.000 7.00
TOTAL FOR CYCLEl
LBS POLLUTANT/IK LB FUEL/CVCLEi
LBS POLLUTANT/IK LB TH-HR/CYCLE:
LBS POLLUTANT/1000K LB TH AT T.O.I
EMISSION FUEL USAGE TIME IN
RATE RATE WT FACTOR MODE
LB/HR LB/HR MIN.
0.320 169.623 .000 19.00
19.572 1387.052 .000 0.50
15.576 1282.9*7 .000 2.50
2.219 477.032 .000 4.50
0.320 169.623 .000 7.00
TOTAL FOR CVCLEl
LBS POLLUTANT/IK LB FUEL/CYCLEI
LBS POLLUTANT/IK LB TH-HR/CYCLE1
LBS POLLUTANT/1000K LB TH AT T.O.I
CO
MASS
LBS.
2.589
0.013
0.09*
0.518
0.95*
4.169
23.918
15.783
0.491
HC
MASS
LBS.
O.B23
0.000
0.00*
0.071
0.303
1.202
6.695
4.550
0.177
NOX
MASS
LBS.
0.101
0.163
0.6*9
0.166
0.037
1.117
6.410
4.230
58.250
FUEL
MASS
LBS.
53.71
11.16
S3. *6
35.76
19.79
17*. 30
FUEL
MASS
LBS.
53.71
11.56
53.46
35.76
19.79
17*. 30
FUEL
MASS
LBS.
53.71
11.56
53.46
35.78
19.79
17*. 30
LB CO /
IK LB FUEL
48.205
1.165
1.765
14.473
48.205
LB KC /
IK LB FUEL
15.328
0.0*3
0.066
1.986
15.328
LB NOX/
IK LB FUEL
1.686
14.111
12.1*1
4.652
1.886
ENERGY
1 TM-HR
53.20
23.33
105.00
63.00
19.60
26*. 13
ENERGY
1 TH-HR
53.20
23.33
105.00
63.00
19.60
26*. 13
ENERGY
1 TH-HR
53.20
23.33
105.00
63.00
19.60
26*. 13
LB CO /
f TH-HR
0.0*867
0.00058
0.00090
0.00822
0.0*867
LB HC /
1 TH-HR
0.01548
0.00002
0.00003
0.00113
0.015*8
LB NOX/
1 TH-HR
0.00190
0.00699
0.00618
0.0026*
0.00190
IV-291
-------
DATE! S/ 3/71
TEST ORGANIZATION: u.s. BUREAU OF NINES
ENGINE SUPPLIER: AMERICAN AIRLINES
ENGINE DATA
CAL 10 NUMBER' 334 ENGINE TVPE AND MODEL: SPEr 511-14
RATED THRUST: 11400.
ENGINE TOTAL TIME: 7500. MRS
TIME SINCF HOT SECTION OVERHAUL: 0. HRS
TIME SINCEl
Nl COMPRESSOR OVERHAUL: 7500. HRS
NZ COMPRESSOR OVERHAUL: 7500. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL! 0. HRS
Nl TURBINE OVERHAUL! 7500. HRS
Hi TURBINE OVERHAUL! 7500. HRS
FUEL: JET - A FUEL H/C RATIO: 1.920
OPERATIONAL DATA «»»««*»««»»»
INLFT AIR TEMPERATURE, DEGREES F: START 73.00 FINISH 73.00
ATMOSPHERIC PRESSURE: START 29.06 FINISH 29.06
INLET AIU HUMIDITY, LBS H20/LB AIR: 0.0130
RELATIVE HUMIDITY: 7i.no PERCENT
SAMPLE LINE: TEMPERATURE, OEGRFES C: 139.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.99
NUMBER OF TESTS: 6
COMMENTS:
H/C CAL ESTIMATED
SAMPLE LINE TEMP AVERAGED
PROBE CONFIG. AND LOCATION SAME AS USED FOR SPC» ON 08-02-71
SERIAL NUMBER:
CLOCK
TIME
1000.00
1005.00
1010.00
1015.00
1015.00
1025.00
TEST
MODE
2/ 0
3/ 2
4/ 3
5/ 4
6/ 5
I/ 6
POWFR
THRUST, LBS PERCENT
OR RATED
SHP
11000.00
10500.00
99HO.OO
1300.00
7480.00
610.00
T.O.
96
92
87
Bl
65
5
ENGINE
SPEED
RPM
Nl
5420.00
8260.00
81 10.00
7940.00
7390.00
2670.00
N2
12360.00
12210.00
12070.00
11900.00
11630.00
7512.00
MEASURED
FUEL
FLOW
Lfl/HR
7280.00
6A60.00
6480.00
6030.00
4710.00
900.00
GAS GEN
AIR FLOW
L8/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CALC COMPRESSOR
F/A DISCHARGE
TEMP
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
2.50
2.44
2.34
2.24
1.98
1.05
TURBINE
INLET
TEMP
OFGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATEO
T.O.
96
92
87
81
65
5
EXHAUST
GAS
TFMP
flEGREES f
1160.00
112.50
1100.00
1065.00
975.00
830.00
EXHAUST
GAS
PRESSURE
PSIA
35.40
34.41
33.18
31.86
2R.10
15.10
CO
IWET1
PPMV
30.70
30. 7C
36.20
37.70
45.00
r.a
2
(UFTI
PERCENT V
2.94
2. tO
2.69
2.53
2.19
THC
(WFT)
PPMV
4.00
3.40
3.10
3.10
3.40
NO
IhFTI
PPMV
154. 7C
141.20
124.70
llfl.60
72.00
NO
2
(WET)
PPMV
IB. 00
14.00
28.00
26.00
55.00
NO
X
(UETI
PPMV
172.7C
155.20
152.70
144.60
127.00
6.40
ALDEHYDES SMOKF PARTICULATFS
0.54
0.50
0.53
0.48
0.48
36.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
POWER
PERCENT
RATEO
T.O.
96
92
87
81
65
5
MASS FMI
cn
LO/1K
Lfl FUEL
2.09
2.20
?. 70
2.99
4.12
55.30
MASS E.MI
HC
LD/1K
LB FUEL
0. 16
0.14
0. 13
0.14
0.16
47.78
MASS EMI
NO?
LB/IK
LB FUFL
2.02
1 .65
1.43
3. 38
H.27
O.B7
MASS EMI
C02
LB/IK
LR FUEL
3152.17
3152.05
3151.28
3150. HI
314B.93
2951.62
MASS EMI
NO
LB/IK
LB FUEL
17.34
16.62
15.27
15.44
10. R2
0.06
MASS EMI
NQX
LB/IK
LB FUEL
19.36
18.26
18.70
18.83
19.09
C.9?
MASS FM
CO
Lfl/HR
1 5.25
15.09
1 7.49
1 8.02
19.40
49.77
MASS EMI
HC
LB/HR
1.14
0.96
0.86
0.85
0.84
38.51
MASS EMI
Nfl2
LR/HR
14.69
11.30
22.22
20.41
38.94
0.78
MASS EMI
Cd2
LB/HR
22947.79
21623.05
20420.32
18999.37
14831.45
2656.46
MASS E»I
NO
LB/HR
126.23
113.99
98.96
93.11
50.97
0.05
MASS FMI
NOX
Lfl/HR
14C.92
125.29
121.18
113.52
89.91
0.83
POWER
PERCENT
RATED
T.O.
96
92
B7
81
65
5
CO
LB/1KKTH-HR
1.386
1.437
1.752
1.937
2.593
81.595
LB/1K«TH-H«
2086.162
2059.339
2046.125
2042.943
1982.815
4354.848
THC
LB/1KHTH-HK
0.103
0.091
0.086
0.091
0. 112
63.124
NO
LB/1KHTH-HR
11.476
10.856
9.916
10.012
6.815
0.085
LB/ IKMH-HR
1.335
1.076
2.226
2.195
5.206
1.276
LB/1KKTH-HR
12.811
11.933
12.142
12.206
12.021
1.162
IV-292
-------
CAL 10 NUMBERl 11* ENGINE TYPE AND MODEL: SPEY 511-14
TEST ORGANIZATION: u.s. BUREAU OF NINES
SERIAL NUMBER! TOT2
MODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
ClINBOUT
APPROACH
TAXI-IDLE
0.040
1.000
0.850
0.400
0.0*0
POWER
f TH
456.
11400.
9690.
4560.
496.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
16.765 599.451
13.37* 7753.320
16.024 6148.152
29.600 3167.199
16.765 599.491
USAGE TIME IN
VT FACTOR MODE
NIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POWER
0.040
1.000
0.850
0.400
0.040
POWER
1 TH
4S6.
11400.
9690.
4560.
456.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
79.847 599.451
0.0 7751.120
0.190 6148.152
0.950 1167.199
79.847 599. 451
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.t
USAGE TIME IN
WT FACTOR NODE
NIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POWER
0.040
1.000
0.850
0.400
0.040
POWER
' 1 TH
456.0
11400.0
9690.0
4560.0
456.0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
0.619 599.451
157.299 7751.120
121.688 6148.152
16.918 1167.199
0.619 599.451
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CVCLE:
LB TH AT T.O.:
USAGE TIME IN
WT FACTOR MODE
MIN.
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000X
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
11.642
0.156
0.58B
1.971
4.289
18.646
21.481
18.819
1.169
HC
MASS
LBS.
29.285
0.0
0.007
0.061
9.116
14.671
41.658
15.025
0.0
ND«
MASS
LBS.
0.202
1.815
4.469
2.461
0.075
9.041
11.187
9.115
160.979
FUEL
MASS
LBS.
189.61
90.46
212.77
211.15
69.94
794.14
FUEL
MASS
LBS.
189.81
90.46
212.77
211.15
69.94
794.14
FUEL
MASS
LBS.
189.81
90.46
212.77
211.15
69.94
794.14
LB CO /
IK LB FUEL
61.111
1.725
2.524
9.146
61.111
LB HC /
IK L6 FUEL
111.201
0.0
0.010
0.100
111.201
LB NOX/
IK LB FUEL
1.067
20.268
19.200
11.656
1.067
ENERGY
TH-HR
144.40
111.00
159.10
104.00
51.20
9B9.90
ENERGY
1 TH-HR
144.40
111.00
155.10
104.00
51.20
989.90
ENERGY
f TH-HR
144.40
111.00
159.10
104.00
51.20
989.90
LB CO /
1 TH-HR
0.08062
0.00117
0.00169
0.00649
0.08062
LB HC /
1 TH-HR
0.17910
0.0
0.00002
0.00021
0.17910
LB NOX/
TH-HR
0.00140
0.01380
0.01298
0.00810
0.00140
IV-293
-------
DATE: fl/ J/TI
TEST ORGANIZATION: U.S. BUREAU OF MINES
ENGINE SUPPLIED: AMERICAN AIRLINES
ENGINE DATA
CAL 10 NUMBER: 335
ENGINE TYPE AND MODEL: SPEY
SERIAL NUMBERi
RATED THRUST: 11400.
ENGINE TOTAL TIHF: 7861. Has
TINE SINCE HOT SECTION OVERHAUL: 652. HRS
TIME SINCEl
Nl COMPRESSOR OVERHAUL: T861. HRS
N2 COMPRESSOR OVERHAUL: 7861. HRS
CONBUSTOR CAN REPLACEMENT: -0. HAS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 652. HRS
NI TURBINF OVERHAUL: 7861. HRS
N2 TURBINE nvERHAUL: 7841. HRS
FUEL: JET - A FUEL H/C RATIO: 1.470
OPERATIONAL DATA ««»
INLET AIR TEMPERATURE, DEGREES F: START 79.00 FINISH
ATMOSPHERIC PRESSURE: START 29.OS FINISH
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0130
RELATIVE HUMIDITY: 60.oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 139.00, FLOW RATE, LITERS/MlN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: 0.19
NUMBER OF TESTS: 6
COMMENTS:
H/C CAL ESTIMATED
SAMPLE LINE TEMP. AVERAGED
PROBE CONFIG. AND LOCATION SAME AS ON 08-02-71
79.00
29.08
LOCK
TIME
155.00
200.00
210.00
215.00
220.00
225.00
TFST
MODE
21 0
3/ Z
4/ 1
5/ -
6/ ")
I/ 6
POWER
THRUST, LHS PERCENT
OR RATED
SHP
11090.00
loeoo.oo
10170.00
'/MO.OO
7500.00
630.00
T.O.
97
94
as
83
65
5
ENGINE
SPEED
RPM
Nl
8500.00
R390.00
8200.00
8030.00
7420.00
2700.00
N2
12400.00
12360.00
12200.00
12040.00
11630.00
75HO.OO
MEASURED
FUEL
FLOW
LB/HR
7370.00
7140.00
6570.00
6120.00
472C.OO
930.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
CALC COMPRESSOR
F/A DISCHARGE
TEMP
-0.
-0.
-0.
-0.
-0.
-0.
000000
000000
000000
000000
000000
000000
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
2.51
2.47
2.36
2.28
1.99
1.59
TURBINF
INLET
TEMP
UEGRFFS F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
t.O.
97
94
88
83
65
5
E XHAUST
GAS
TEMP
DEGREES F
1165.00
1140.00
1 100.00
1075.00
970.00
520.00
FXHAUST
GAS
PRFSSURF
PSIA
35.58
34.98
33.52
32.33
28.13
22.72
CO
IWETI
34.20
33.20
34.20
35.30
42.50
CO
2
IW Tl
PERCENT V
2.93
3.02
2.67
2.57
2.17
THC
IWETI
PPMV
2.50
1.30
2.00
2.00
2.00
NO
IWET)
PPMV
154.30
143.90
131.70
172.0C
88.50
NO
2
IWET)
PPMV
8.50
11.50
13.00
18.50
16.50
NO
X
I WET)
PPMV
162.80
155.40
144.70
140.50
105.00
9.70
ALDEHYDES SMOKt PARTICULATES
0.62
0.37
0.40
0.29
0.34
38.00
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-0.00
-o.oo
-0.00
-0.00
-0.00
-o.oo
POWER
PERCENT
RATED
T.n.
97
94
8fl
83
65
5
MASS EMI MASS EMI MASS EMI
CO HC N02
LB/1K LB/IK LB/1K
LB FUEL LB FUFL LB FUEL
2.34
2.21
2.57
7.75
3.93
106.37
0.10
0.05
0.09
0.09
0.11
75.59
0.96
1.25
1.60
2.37
7.50
0.77
MUSS EMI
C02
Lfl/lK
LB FUEL
3151.94
3152.29
3151.67
3151.32
3149.43
7781.38
MASS EMI
NO
LH/IK
LB FUEL
17.35
15.70
16.75
15.64
13.43
1.71
MASS EMI
NOX
LB/IK
LB FUEL
18.31
16.96
17.86
18.01
15.93
2.47
MASS EMI
CO
Lfl/HR
1 7.26
15.75
16.88
16. 86
IB. 53
18.92
KASS EMI
HC
LB/HR
0.72
0.35
0.57
0.55
0.50
70.30
MASS EMI
NO 2
L H/HR
7.04
8.96
10.54
14.51
11.82
0.71
MASS FMI
C<12
LB/HR
23229.79
22507.33
20706.13
19286.05
14865.32
2586.69
MASS EMI
NO
LB/MR
127.89
112.11
106.77
95. 71
63.38
1.59
MASS EMI
NOX
LB/hR
134.93
121.07
117.31
110.22
75.19
2.30
POWER
PERCENT
RATED
T.O.
97
83
65
5
CO
LB/IKNTH-HR
1.S56
1 .45S
1.668
1.773
2.471
157.018
LB/1K4TH-HR
2094.661
2084.012
2046.060
2027.976
1982.042
4105.848
TMf.
LB/IMTH-HR
0.065
0.013
0.056
0.058
0.067
111.590
NO
LB/1KKTH-HR
11.532
10.381
10.551
10.064
8.450
2.523
LB/IKHTH-HR
0.635
0.830
1.041
1. 526
1.576
1. 130
Nil
X
Lb/lKHUH-HR
12.167
11.211
11.592
11.590
10.026
3.652
IV-294
-------
CAL 10 NUMBER: 339 ENGINE TYPE AND MODEL: SPET 511-14
TEST ORGANIZATION: U.S. BUREAU OF MINES
SERIAL NUMBER: 7065
NODE FRACTIONAL
POWER
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
0.040
1.000
0.650
0.400
0.040
POWER
f TH
456.0
11400.0
9690.0
4960.0
496.0
EMISSION FUEL
RATE RATE WT
LB/HR LB/HR
79.001
11.490
12.968
91.393
75.001
686.454
7669.500
6402.168
3069.966
686.454
TOTAL FOR CTCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
mot
FRACTIONAL
POKER
TAXI-IDLE 0.040
TAKEOFF 1.000
CLIMBOUT 0.850
APPROACH 0.400
TAXI-IDLE 0.040
POWER
f TH
496.0
11400.0
9690.0
4960.0
496.0
EMISSION FUEL
RATE RATE MT
LB/HR LB/HR
52.981 686.454
0.0 7669.500
0.0 6402.168
10.579 3069.966
52.981 686.454
USAGE
FACTOR
I. 000
1.000
1.000
1.000
1.000
TIME IN
NODE
M1N.
19.00
0.70
2.20
4.00
7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.:
USAGE
FACTOR
1.000
1.000
1.000
1.000
1.000
TIME IN
MODE
NIN.
19.00
0.70
2.20
4.00
7.00
CO
MASS
LBS.
23.750
0.134
0.461
3.426
8.750
36.521
44.196
36.894
1.172
HC
MASS
LBS.
16.777
0.0
0.0
0.705
6.181
FUEL
MASS
LBS.
217.38
89.46
234.75
204.66
80.09
826.35
FUEL
MASS
LBS.
217.38
89.48
234.79
204.66
80.09
LB CO /
IK L8 FUEL
109.299
1.493
1.963
16.741
109.299
IB HC /
IK LB FUEL
77.180
0.0
0.0
3.446
77.180
ENERGY
TH-HR
144.40
133.00
395.30
304.00
53.20
989.90
ENERGY
t TH-HR
144.40
133.00
355.30
304.00
53.20
LB CO /
f TH-HR
0.16448
0.00100
0.00130
0.01127
0.16448
LB HC /
t TH-HR
0.11619
0.0
0.0
0.00232
0.11619
TOTAL FOR CYCLE: 23.664
LBS POLLUTANT/IK LB FUEL/CYCLE: 28.636
LBS POLLUTANT/IK LB TH-HR/CVCLE: 23.909
LBS POLLUTANT/1000K LB TH AT T.O.: 0.0
MODE FRACTIONAL
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
POWER
0.040
1.000
0.850
0.400
0.040
POWER
( TH
456.0
11400.0
9690.0
4560.0
496.0
EMISSION
RATE
LB/HR
1.386
153.961
110.304
30.075
1.386
FUEL USAGE
RATE WT FACTOR
LB/HR
686.494
7669.500
6402.168
3069.966
686.454
.000
.000
.000
.000
.000
TIME IN
MODE
MIN.
19.00
0.70
2.20
4.00
7.00
NOX
MASS
LBS.
0.439
1.796
4.044
2.009
0.162
FUEL
MASS
LBS.
217.38
89.48
234.79
204.66
80.09
IB NOX/
IK LB FUEL
2.019
20.074
17.229
9.797
2.019
ENERGY
f TH-HR
144.40
113.00
359.30
304.00
53.20
LB NOX/
t TH-HR
0.00304
0.01351
0.01138
0.00660
0.00104
TOTAL FOR CYCLE: 8.446
LBS POLLUTANT/IK LB FUEL/CYCLE! 10.221
LBS POLLUTANT/IK LB TH-HR/CYCLE: 8.532
LBS POLLUTANT/1000K LB TH AT T.O.I 157.562
989.90
IV-295
-------
DATE: II 2/11
TEST ORGANIZATION! U.S. BUREAU OF MINES
ENGINE SUPPLIER! AMERICAN AIRLINES
ENGINE DATA
CAL ID NUMBER: 1)6
ENGINE TYPE AND MODEL: SPEY 511-1*
SERIAL NUMBER!
RATED THRUST: 11400.
ENGINE TOTAL TIME: 2635. MRS
TINE SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE!
NI COMPRESSOR OVERHAUL: 2no. MRS
N2 COMPRESSOR OVERHAUL! 21)0. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE HOllLf GUIOF VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL! 0. HRS
FUEL! JF.T - A FUEL H/C RATIO: 1.920
OPERATIONAL DATA ««««»****
INLET AIR TEMPERATURE, DEGREES f: START 74.00 FINISH
ATMOSPHERIC PRESSURE: START 29.OK FINISH
INLET AIR HUMIDITY, IBS H20/LB AIR: 0.0110
RELATIVE HUMIDITY: 53.00 PERCFNT
SAMPLE LINE: TEMPERATURE, CFGREFS C: HI.00, FLOM RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.99
NUMBER OF TFSTS: 8
COMMENTS:
H/C CAL ESTIMATED
SAMPLE LINE TFMP. AVERAGED
NEW PROBF CONFIGURATION
79.00
24.08
LOCK
TIME
2)0.00
2)5.00
-0.00
245.00
250.00
255.00
300.00
)05.00
TEST
MODE
I/ 0
2/ 1
2/ 2
3/ 2
4/ 3
5/ 4
hi 5
I/ 6
POWER
THRUST, LBS PERCFNT
OR RATED
SHP
MO. 00
10920.00
11000.00
10500.00
9950.00
94)0.00
7470.00
030.00
T.O.
5
95
96
92
87
82
65
5
ENGINF
SPEED
RPM
NI
2700.00
8480.00
8500.00
83)0.00
8170.00
8010.00
7400.00
2720.00
N2
7660.00
12400.00
12460.00
12290.00
12150.00
12010.00
11660.00
7710.00
MEASURED
FUFL
FLOW
LB/HR
890.00
7070.00
7100.00
6700.00
6200.00
5860.00
4510.00
890.00
CSS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
CALC COMPRESSOR
F/A DISCHARGE
TEMP
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
-0.000000
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
KATIO
EPR
1.06
2.49
2.49
2.4?
2.)b
2.26
1.92
1.06
TURBINE
INLET
TEHP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWFR EXHAUST
PERCFNT GAS
RATED TEMP
T.O. DEGREES F
5
95
96
92
87
H2
65
5
H20.00
I 140.00
11)5.00
1100.00
1075.00
1050.00
9.45
800.00
FXHAUST
GAS
CRFSSURF
PSIA
15.26
35.20
35. )8
34.38
33.26
32.0)
27. IS
15.26
CO
(HETI
PPHV
640.00
30.70
-0.00
57.30
)3..SO
14. )0
44.00
645.00
CO
2
(UFTI
PERCENT V
1.35
3.25
-o.oo
3.18
2.98
2.90
P. 50
1.35
THC
IHFTI
PPMV
1037.00
4.50
-0.00
3.50
3.00
2.80
2.60
734.00
Ntl
(HETI
PPMV
1 .10
172.10
-0.00
158.20
144.40
1)0.7"
81.90
O.C
NO
2
(MET)
PPMV
7 .00
29.00
-0.00
40.00
4). 00
41.00
36.00
8.00
NO
X
IWFTI
PPMV
a. 10
201.00
-0.00
198.20
187.40
171.70
127.90
8.00
ALDEHYDES
-0.00
0.83
-0.00
0.70
0.73
0.68
0.53
41.50
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-c.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
5
95
96
92
87
82
65
5
MASS EMI
cn
LB/IK
LB FUFL
85.))
1 . 90
0.20
2.04
2.28
2.37
3.5)
87.07
MASS EMI
HC
LB/1K
LR FUEL
78.57
0. 16
0.12
0.13
0.12
0.11
0.12
56.75
MASS EMI
N02
LB/IK
LB FUEL
1.52
2.94
0.33
4.15
4.75
4.66
4.74
1.77
MASS EMI
CO 2
LB/IK
LB FUEL
2806.25
3152.47
3155.26
3152.34
3152.00
3151.86
3150.02
286). 40
MASS EMI
NO
LB/IK
LB FUEL
0. 24
17.45
0.)3
16.39
15.97
14.85
10.79
0.0
MASS EMI
NOX
LB/IK
LB FUEL
1.76
20.38
0.66
20. 54
20.72
19.51
16.85
1 .77
MASS EMI
CO
LB/HR
75.95
13.40
1.43
1 3.65
14.11
13.90
15.91
77.49
MASS EMI
HC
LB/HR
69.91
1. 12
0.82
0.85
0.72
0.65
0.54
50.51
MASS EMI
NC12
LB/HR
l.)5
20.79
2.34
27.77
29.48
27.30
21.39
1.58
MASS EMI
CO 2
LB/HR
2497.56
22288.00
22402.34
21120.68
19542. J7
1 8469.88
14206.58
2548.43
MASS EMI
NO
Lfl/HR
0.21
123.38
2.34
104.94
98.99
87.02
48.65
0.0
MASS FMI
NDX
LB/HR
1.57
144. 10
4.68
137.62
128.47
114.32
75.98
1.58
POKES
PERCENT
RATED
T.O.
5
95
96
92
87
82
65
5
CO
LB/IK«TH-HR
12
.502
.227
.1)0
.300
.418
.474
2.1)0
123.004
IB/IK»TH-H»
4094.167
2041.025
2036.577
2011.493
1464.058
1958.630
1901.818
4045.120
THC
LB/IKNTH-HR
I 14.641
0.10)
0.074
0.081
0.072
0.069
0.072
80.168
NU
LO/IK«TH-HR
0.349
11.299
0.213
10.461
9.949
9.228
6.513
0.0
LR/1K«TH-HR
2.219
1.904
0.213
2.645
2.96)
2.895
2.B63
2.506
NO
X
LB/IKHTH-HR
2.568
I).146
0.426
13.106
12.912
12.121
10.171
2.506
IV-296
-------
CAL ID NUMBER: 336 ENGINE TYPE »NO MODEL: SPEY su-u
TEST ORGANIZATION: u.s. BUREAU OF NINES
SERIAL NUMBER I 8091
MODE
TAXI-IOLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
NODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POKER
0.040
1.000
0.850
0.400
0.040
FRACTIONAL
POKER
0.040
1.000
0.850
0.400
0.040
FRACTIONAL
POKER
0.040
I. 000
o.aso
0.400
0.040
POKER
I TH
456.0
11400.0
9690.0
4560.0
456.0
POKER
f TH
456.0
11400.0
9690.0
4560.0
456.0
POWER
> TH
456.0
11400.0
9690.0
4560.0
456.0
EMISSION FUEL I
RATE RATE MT
LB/HR L8/HR
51.274 554.190
18.380 7408.145
16.475 6271.344
32.205 3091.461
51.274 554.190
TOTAL FOR CYCLE:
L8S POLLUTANT/IK LB
IBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
EMISSION FUEL
RATE RATE NT
LB/HR LB/HR
67.567 554.190
0.0 7408.145
0.244 6271.344
1.368 3091.461
67.567 554.190
TOTAL FOR CVCLEl
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS PQLLUTANT/1000K
EMISSION FUEL
RATE RATE NT
LB/HR LB/HR
0.526 554.190
161.744 7408.145
129.085 6271.344
30.586 3091.461
0.526 554.190
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
JSAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLE:
LB TH AT T.O.)
JSAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT T.O.I
USAGE TIKE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE!
TH-HR/CYCLE:
LB TH AT T.O.:
CO
MASS
LBS.
16.237
0.214
0.604
2.147
5.982
25.184
33.023
25.441
1.881
HC
MASS
LBS.
21.396
0.0
0.009
0.091
7.883
29.379
38.524
29.679
0.0
NOX
MASS
LBS.
0.167
1.887
4.733
2.039
0.061
8.887
11.654
8.978
165.528
FUEL
MASS
LBS.
175.49
86.41
229.95
206.10
64.66
762. 62
FUEL
MASS
LBS.
175.49
86.43
229.95
206.10
64.66
762.62
FUEL
MASS
LBS.
175.49
86.43
229.95
206.10
64.66
762.62
LB CO /
IK LB FUEL
92.520
2.4B1
2.627
10.418
92.520
LB HC /
IK LB FUEL
121.920
0.0
0.039
0.442
121.920
LB NOX/
IK L8 FUEL
0.950
21.833
20.583
9.894
0.950
ENERGY
1 TH-HR
144.40
133.00
355.30
304.00
13.20
989.90
ENERGY
t TH-HR
144.40
133.00
355.30
304.00
53.20
989.90
ENERGY
f TH-HR
144.40
133.00
355.30
304.00
53.20
989.90
LB CO /
TH-HR
0.11244
0.00161
0.00170
0.00706
0.11244
LB HC /
t TH-HR
D. 14817
0.0
0.00003
0.00030
0.14817
LB NOX/
TH-HR
0.00115
0.01419
0.01332
0.00671
0.00115
IV-297
-------
0»TE: 7/JO/71
TEST ORGANIZATION: U.S. BUREAU OF MINES
ENGINE SUPPLIER: AMERICAN AIRLINES
ENGINE DATA «««««
CAL ID NUMBERl 411 ENGINE TYPE AND MODEL: SPEY 511-14
RATED THRUST: 11400.
ENGINE TOTAL TIME: 72)7. MRS
TIME SINCE Mar SECTION OVERHAUL: o. MRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 1615. MRS
N2 COMPRESSOR OVERHAUL: 1635. HRS
COHBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NDZ2LE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: 1635. HRS
N2 TURRINE OVERHAUL! 1615. HRS
SERIAL NUMBER:
FUEL H/C RATIO! 1.120
74.00
11.45
FUEL! JET - A
OPERATIONAL DATA «»»
INLET AIR TEMPERATURE, DECREES F: START 72.00 FINISH
ATMOSPHERIC PRESSURE: START 14.45 FINISH
INLET AIR HUMIDITY, LBS H20/IB AIR: 0.0067
RELATIVE HUMIDITY: 54.00 PERCENT
SAMPLE LINE: TEMPERATURE, CECREES C: 1)7.00, FLOW RATE, LITERS/HIM:
SAMPLE LINE TRANSPORT TIME, SEC: 0.99
NUMBER OF TESTS: 10
COMMENTS:
SPEY PROBE 4.6" FROM TAILPIPE FOR FIRST THREE RUN;. PROBE FAILFH AND A
JT3/8 0 PROBE USED FUR REMAINING HUNS BUT LOST ON RUN 5. SMALL SAMPLE FLOW
TAKEN THRU BROKEN SAMPLE LINE FOR REMAINDER OF RUNS.
CLOCK
TIME
1 1)0.00
1135.00
1140.00
1255.00
ino.oo
105.00
110.00
115.00
120.00
125.00
POWER
PERCENT
RATED
T.O.
3
4
99
5
94
94
90
Bb
65
5
POWER
PERCENT
RATED
T.n.
3
4
99
5
99
94
90
B6
65
5
POWER
PERCENT
RATED
T.O.
3
4
99
5
99
94
90
B6
65
5
TEST
NnnE
\l 0
l/ 1
2/ l
I/ 2
21 1
)/ 2
4/ 1
5/ 4
6/ 5
I/ 6
EXHAUST
GAS
TFMP
DEGREES F
870.00
825.00
1170.00
-0.00
1170.00
1135. on
1110.00
1090.00
975.00
(125. 00
MASS EMI
CO
LR/IK
L8 FULL
103.10
101.92
3.32
89.79
2. 78
2.87
2.73
2.84
3.02
90.52
CU
POWER ENGINE MEASURED GAS GEN CALC COMPRESSOR ENGINE TURBINE
THRUST, LBS PERCENT SPEED FUFL AIR FLOW F/A DISCHARGE PRESSURE INLET
OR RATED RPM FLOW LB/SEC TEMP RATIO TEMP
SHP T.O. Nl N2 LB/HR DEGREES F FPR DEGREES f
430.00 3 2500.00 7325.00 870.00 -0.00 -0.000000 -0.00 1.06 -0.00
550.00 4 2590.00 7480.00 890.00 -0.00 -0.000000 -0.00 1.06 -0.00
11350.00 99 8440.00 12280.00 -0.00 -0.00 -0.000000 -0.00 2.54 -0.00
580.00 5 2680.00 7630.00 940.00 -0.00 -0.000000 -0.00 -0.00 -0.00
11360.00 99 8460.00 12350.00 7620.00 -0.00 -0.000000 -0.00 2.56 -0.00
10820.00 94 8280.00 12200.00 7170.00 -0.00 -0.000000 -0.00 2.48 -0.00
10350.00 90 8150.00 12090.00 6800.00 -0.00 -0.000000 -0.00 2.40 -0.00
9830.00 86 B020.00 1IMBO.OO 64)0.00 -0.00 -0.000000 -0.00 2.3) -0.00
7500.00 65 7340.00 11614.00 4800.00 -0.00 -0.000000 -0.00 1.99 -0.00
600.00 5 2710.00 7730.00 920.00 -0.00 -0.000000 -0.00 1.07 -0.00
EXHAUST CG co THC NU NO NO ALOFHYDES SMOKE PARTICULARS
GAS (WETI 2 (WET) IWETI 2 X
PRESSURE PPMV (WETI PPMV PPMV IWET) (WETI
PSIA
15.28
is. an
36.25
-0.00
36.45
35. ?5
34.30
33.25
28. 41
15.43
MASS EMI
HC
LB/1K
LB FUFL
93.63
75.45
0.83
63.2)
-0.00
-0.00
-0.00
-0.00
-0.00
72.69
LB/IKHTH-HR
209.
16*.
-0.
145.
.
.
.
t
138.
012
922
000
516
864
902
796
860
933
796
PERCENT V
860.00 1
735.00 1
45.00 2
710.00 1
)9.20 2
38.20 2
35.30 2
35.10 >
36.30 2
470.00 0
MASS EMI MASS EMI
N02 C02
LB/1K LB/1K
LB FUEL LB FUEL
0.79 2736.70
0.11 2788.77
1.09 3148.40
0.9) 2841.36
1.05 3151.52
1.30 )I51.38
1.40 3151.59
1.52 3151.42
1 . 50 3151.14
2.06 2814.25
CO
2
.45 1361.
.28 950.
.72 19.
.43 873.
.83 -0.
.S7 -0.
.59 -0.
.49 -0.
.41 -0.
.93 659.
"ASS EMI
NO
IB/ IK
LB FUEL
0.0
0.0
17.12
1.12
16.45
15.44
15.16
14.90
10.58
0.0
THC
LR/1KHTH-HR LB/1KHTH-HR
5537.047
4512.742
-0.000
4604.957
2113.963
2088.299
2070.612
2061.407
2016.731
4115.130
1B9.442
122.085
-0.000
102.47)
-0.000
-0.000
-0.000
-0.000
-0.000
1U.457
00 0.
00 0.
70 141.
00 5.
00 141.
00 125.
00 119.
00 112.
00 77.
00 0.
MASS tMI
NOX
LO/1K
LB FUEL
0.79
0.91
18.21
2.06
17.50
16.73
16.56
16.42
12.08
2.06
Nfl
0
0
5n
40
3C
10
20
60
40
0
MASS
CD
PPMV PPMV
4.
4.
9.
4.
9.
10.
11.
11.
11.
6.
EMI
LR/HR
89.
90.
-0.
84.
21.
20.
IB.
18.
14.
83.
3H
71
00
40
17
57
59
28
50
28
LB/ 1KMH-HR
0.
0.
-0.
1.
11.
10.
9.
9.
6.
0.
0
0
000
81H
034
229
962
741
771
0
00 4.00 -0.
00 4.00 -0.
0" 150.50 -0.
50 9.90 -0.
00 ISO. 30 I.
50 135.60 0.
00 130.20 0.
50 124.10 0.
00 88.40 0.
50 6.50 29.
MASS EMI MASS EMI
HC NO 2
LB/HR LB/HR
81.46 0.69
67.15 0.81
-0.00 -0.00
59.43 0.88
-0.00 7.98
-0.00 9.29
-0.00 9.52
-0.00 9.78
-0.00 7.22
66.87 1.89
NO
2
00 -0.
00 -0.
00 -0.
00 -0.
22 -0.
89 -0.
75 -0.
66 -0.
36 -0.
30 -0.
MASS EMI
CO 2
LB/HR
2380.93
2482.01
-0.00
2670.87
24014.61
22595.40
21430.8)
20263.6)
15125.48
2589.11
NO
X
OD -0.00
00 -0.00
00 -C.OO
00 -0.00
00 -0.00
00 -C.OO
00 -0.00
00 -0.00
00 -0.00
00 -0.00
MASS EMI MASS
NO NO
EMI
X
LB/HR LB/HR
0.0 0.
0.0 0.
-0.00 -0.
1.05 1.
125.35 133.
110.67 119.
103.11 112.
95.79 105.
50.78 58.
0.0 1.
69
81
00
91
33
96
62
58
00
89
LB/1KKTH-HR LB/ 1 K» TH-HR
1.597
1.474
-0.000
1.515
0. 70)
0.859
0.919
0.995
0.962
3. 153
1 .597
1.474
-0.000
3.U3
11.7)7
11.087
10.812
10.740
7.733
).153
IV-298
-------
CM. 10 NUMBER: 411 ENGINE TYPE AND MODEL: SPEY 511-14
TEST ORGANIZATION: u.s. BUREAU OF NINES
SERIAL NUMBER: TOM
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
FRACTIONAL
POMER
0.040
1.000
0.650
0.400
0.040
POMER
1 TH
496.
11400.
9690.
4560.
456.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
TT.652 806. OT1
13.666 T669.965
15.938 6397.875
43.075 2878.047
77.652 806.071
MT
TOTAL FOR CYCLE:
IBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROiCH
TAXI-IDLE
FRACTIONAL
POKER
0.040
1.000
0.850
0.400
0.040
POMER
1 TH
456.
11400.
9690.
4560.
496.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
63.808 806.071
0.0 7669.965
0.535 6397.875
3.997 2B78.047
63.808 806. OT1
HT
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
NODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
FRACTIONAL
POMER
0.040
1.000
0.890
0.400
0.040
POWER
TH
456.
11400.
9690.
4560.
456.
0
0
0
0
0
EMISSION FUEL
RATE RATE
LB/HR LB/HR
0.844 806.071
139.044 7669.965
9T.T5B 6397.875
24.203 2878.047
0.844 B06.071
MT
USAGE TIME IN
FACTOR NODE
MIN.
.000 19.00
.000 0. TO
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLEl
LB TH AT T.O.:
USAGE TIME IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 7.00
FUEL/CYCLE:
TH-HR/CYCLE:
LB TH AT t.O.:
USAGE TINE IN
FACTOR MODE
MIN.
.000 19.00
.000 0.70
.000 2.20
.000 4.00
.000 T.OO
TOTAL FOR CYCLE:
LBS POLLUTANT/IK LB FUEL/CYCLE:
LBS POLLUTANT/IK IB TH-HR/CYCLE:
LBS POLLUTANT/IOOOK LB TH AT T.O.:
CO
MASS
LBS.
24.590
0.159
0.584
2.872
9.059
37.265
43.069
37.645
1.399
HC
MASS
LBS.
20.206
0.0
0.020
0.266
7.444
27.936
32.287
28.221
0.0
NOX
MASS
LBS.
0.267
1.622
3.584
1.614
0.099
T.IB6
8.305
7.259
142.296
FUEL
MASS
LBS.
239.26
89.48
234.59
191.87
94.04
865.24
FUEL
MASS
LBS.
255.26
89. 4B
234.59
191.87
94.04
665.24
FUEL
MASS
LBS.
255.26
B9.4B
234.59
191.87
94.04
865.24
LB CO /
IK LB FUEL
96.334
1.7B2
2.491
14.96T
96.334
LB HC /
IK LB FUEL
79.159
0.0
0.084
1.389
79.159
LB NOX/
IK LB FUEL
1.047
18.128
15.280
8.410
1.047
ENERGY
1 TH-HR
144.40
133.00
355.30
304.00
53.20
989.90
ENERGY
f TH-HR
144.40
133.00
355.30
304.00
53.20
989.90
ENERGY
1 TH-HR
144.40
133.00
335.30
304.00
33.20
989.90
LB CO /
TH-HR
0.17029
0.00120
0.00164
0.00945
0.17029
LB HC /
t TH-HR
0.13993
0.0
0.00006
0.0008B
0.13993
LB NOX/
f TH-HR
0.00185
0.01220
0.01009
0.00531
0.00185
IV-299
-------
MODEL T56-A7 TURBOPROP
SAMPLE NUMBER
II.
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
EMISSION
RITE
LB/MR
MEAN 19.268
STD OEV 3.519
MEAN 2. HO
STD OEV I. 281
MIAN 9.009
STD DEV 0.791
MEAN 3.668
STO DEV 0.841
MEAN 15.268
STD OEV 3.319
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
FUEL
RATE
LB/HR
548.004
54.095
2079.317
T7.480
1908.447
25.675
1092.900
23.937
548.004
94.095
FUEL/CYCLE
LBS POLLUTANT/IK MP-HR/CYCLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBDUT
APPROACH
TIKI-IDLE
LBS PQLLUTANT/1000K
EMISSION
RATE
LB/HR
MFAN 6.474
STD OEV 1.612
MEAN 0.430
STD DEV 0.911
MEAN 0.476
STO OEV 0.976
MEAN 0.517
STO DEV 1.004
MEAN 6.4T4
STD DEV 1.612
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
HP-HR AT T.O.
FUEL
RATE
LB/HR
548.004
94.099
2079.317
77.480
1908.447
25.679
1092.900
23.937
54B.004
94.095
FUEL/CYCLE
LBS PrXLUTANT/lK HP-HR/CYCLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
LBS POLLUTANT/1000K
EMISSION
RATE
LB/MR
MEAN 2.161
STD DEV 0.499
MEAN 22.BTB
STD OEV 3.566
MEAN 21.212
STD OEV 2.914
MEAN T.T76
STO OEV 0.913
MEAN 2.161
STD OEV 0.499
TOTAL FOR CYCLE
LAS POLLUTANT/IK LS
HP-HR AT T.O.
FUEL
RATE
LB/HR
948.004
54.095
2079.317
77.480
1908.447
29.675
1092.900
23.9)7
948.004
94.099
FUEL/CYCLE
LBS POLLUTANT/IK HP-MR/CVCLE
LBS POLLUTANT/IOOOK
HP-HR AT T.O.
TIME IN
NODE
MIN.
19.00
0.0
0.30
0.0
2.50
0.0
4.90
0.0
7.00
0.0
MEANI
STD OEV:
NEAN1
STO DEVI
MEANl
STD DEVI
MEANI
STO OEVt
TIME IN
MODE
MIN.
19.00
0.0
0.50
0.0
2.90
0.0
4.50
0.0
7.00
0.0
MEANI
STD DEV;
ME AN i
STD OEVl
MEAN:
STD OEV:
MCANI
STD OEV!
TIME IN
MODE
MIN.
19.00
0.0
0.50
0.0
2.90
0.0
4.50
0.0
7.00
0.0
MEAN:
STB OEVl
MEAN:
STO OEVl
MEANl
STO DEVI
MEAN!
STD OEV:
4
1
0
0
0
0
0
0
1
0
7
1
17
3
23
4
0
0
CO
MASS
IBS.
.835
.119
.018
.011
.125
.033
.273
.063
.781
.411
.033
.502
.064
.970
.033
.917
.477
.283
HC
MASS
LBS.
2
0
0
0
0
0
0
0
0
0
2
0
6
1
9
2
0
2
0
0
0
0
0
0
0
0
0
0
2
0
6
0
a
l
90
7
.050
.511
.004
.008
.020
.041
.039
.075
.795
.188
.868
.709
.970
.745
.390
.309
.955
.021
NOX
MASS
LBS.
.684
.198
.191
.030
.884
.096
.983
.068
.252
.058
.594
.378
.269
.761
.494
.237
.773
.914
FUEL
MASS
LBS.
173.53
17.13
17.33
0.69
79.52
1.08
78.97
1.79
63.93
6.31
413.28
24.11
FUEL
MASS
LBS.
173.53
17.13
17.33
0.65
79.52
1.08
78.97
1.79
63.93
6.31
413.28
24.11
FUEL
MASS
LBS.
173.53
17.13
17.33
0.63
79.52
1.08
78.97
1.79
63.93
6.31
413.28
24.11
IB CO /
IK IB FUEL
28.
6.
1.
0.
1.
0.
3.
0.
28.
6.
101
597
040
627
579
421
482
787
101
597
LB HC /
IK LB FUEL
11.
3.
0.
0.
0.
0.
0.
0.
11.
3.
923
054
207
438
250
512
491
952
923
054
18 NOX/
IK LB FUEL
3.
0.
10.
11.
1.
7.
0.
3.
0.
932
743
984
501
111
194
382
812
932
743
' ENERGY
KP-HR
35.67
0.04
31.29
0.03
14O.81
0.18
- 84.49
0.14
13.14
0.01
305.41
0.0
ENERGY
HP-HR
35.67
0.04
31.29
0.03
140.81
0.18
84.49
0.14
13.14
0.01
305.41
0.0
ENERGY
HP-HR
35.67
0.04
31.29
0.03
140.81
0.18
84.49
0.14
13.14
0.01
305.41
0.0
LB CO /
HP-HR
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
LB
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
LB
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
13353
03124
00097
00034
00089
00023
00326
00075
13553
03124
HC /
HP-HR
05747
01431
00011
00024
00014
00029
00046
00089
05747
01431
NOX/
HP-HR
01918
00443
00609
00095
00628
00068
00690
00081
01918
00443
IV-300
-------
MODEL T56-A15 TURBOPROP
SIMPLE NUMBER
12.
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IOLE
EMISSION
BATE
LB/HR
MEAN 8.735
STD OEV 7.491
MEAN 1.765
STD DEV 1.293
MEAN 1.404
STO DEV 0.801
MEAN 3.489
STD OEV 0.848
MEAN 8.735
STO OEV 7.491
TOTAL FOR CYCLE
LBS POLLUTANT/IK IB
FUEL
RATE
LB/HR
493.001
122.165
2192.661
124.766
2188.467
95.255
1145.895
19.792
493.001
122.165
FUEL/CYCLE
LBS POLLUTANT/IK HP-HR/CVCLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
LBS POLLUTANT/IOOOK
EMISSION
RATE
LB/HR
MEAN 7.3BB
STO OEV 5.338
MFAN 0.440
STD OEV 0.666
MEAN 0.399
STD OEV 0.590
MEAN 0.326
STD OEV 0.321
MFAN 7. 388
STO DEV 5.338
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
HP-HR AT T.O.
FUEL
RATE
LB/HR
493.001
122.165
2392.661
124.766
21BB.46T
95.255
1145.895
19.792
493.001
122.165
FUEL/CYCLE
LBS POLLUTANT/IK HP-HR/CVCLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBC1UT
APPROACH
TAXI-IOLE
LBS POLLUTANT/IOOOK
EMISSION
RATE
LB/HR
MEAN 1.233
STO OEV 0.697
MEAN 27.898
STO OEV 11.532
MEAN 22.201
STD OEV 3.532
MEAN 7.323
STD OEV 1.570
MFAN 1.233
STO OEV 0.697
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
HP-HR AT T.O.
FUEL
RATE
LB/HR
493.001
122.165
2392.661
124.766
21BB.467
95.255
1145.895
19.792
493.001
122.165
FUEL/CYCLE
LBS POLLUTANT/IK HP-HR/CYCLE.
LBS POLLUTANT/IOOOK
HP-HR AT T.O.
TINE IN
MODE
NIN.
19.00
0.0
0.50
0.0
2.50
0.0
4.50
0.0
7.00
0.0
MEAN:
STO DEV:
MEAN:
STO DEV:
MEAN:
STO OEV:
MEAN:
STD DEV:
TIME IN
MODE
NIN.
19.00
0.0
0.50
0.0
2.50
0.0
4.50
0.0
7.00
0.0
MEAN:
STO OEV!
MEAN:
STD OEV:
MEAN:
STO DEV:
MEAN:
STO OEV:
TIME IN
NODE
MIN.
19.00
0.0
0.50
0.0
2.50
0.0
4.50
0.0
7.00
0.0
MEAN:
STO DEV:
MFANi
STO OEV!
MEAN:
STO DEV:
MEAN:
STD DEV:
CO
MASS
LBS.
2.766
2.372
0.031
0.011
0.142
0.033
0.262
0.064
1.019
0.874
4.220
3.248
10.211
7.267
11.302
B.69B
0.6B3
0.235
HC
MASS
LBS.
2.339
1.690
0.004
0.006
0.017
0.025
0.024
0.024
0.862
0.623
3.246
2.305
7.798
5.097
8.693
6.174
0.798
1.210
NOX
MASS
LBS.
0.390
0.221
0.232
0.096
0.925
0.147
0.549
0.116
0.144
0.081
2.241
0.546
5.4)1
0.998
6.002
1.461
50.639
20.932
FUEL
MASS
LBS.
156.12
18.68
19.94
1.04
91.19
3.97
85.94
1.48
57.52
14.25
410.70
54.63
FUEL
MASS
LBS.
156.12
38.68
19.94
1.04
91.19
3.97
85.94
1.48
57.52
14.25
410.70
54.63
FUEL
MASS
LBS.
156.12
38. 6B
19.94
1.04
91.19
3.97
85.94
1.48
57.52
14.25
410.70
54.63
LB CO / .
IK LB FUEL
18.050
13.473
1.565
0.491
1.549
0.317
3.044
0.731
18.050
11.473
LB HC /
IK LB FUEL
15.046
9.232
0.179
0.272
0.179
0.267
0.286
0.2BI
15.046
9.232
LB N0>/
IK LB FUEL
2.446
1.1B1
11.655
4.769
10.141
1.550
6.384
1.324
2.446
1.181
ENERGY
HP-HR
43.61
0.09
18.26
0.05
172.16
O.OB
103.30
0.15
16.07
0.0
373.40
0.52
ENERGY
HP-HR
41.61
0.09
38.26
0.05
172.16
0.08
103.30
0.15
16.07
0.0
373.40
0.52
ENERGY
HP-HR
43.61
0.09
38.26
0.05
172.16
O.OB
103.30
0.15
16.07
0.0
373.40
0.52
LB CO /
HP-HR
0.06342
0.05439
0.00082
0.00028
0.00082
0.00019
0.00253
0.00062
0.06342
0.05439
LB HC /
HP-HB
0.05364
0.03876
0.00010
0.00015
0.00010
0.00014
0.00024
0. 00023
0.05364
0.03B76
LB NOX/
HP-MR
0.00895
0.00506
0.00608
0.00251
0.00537
O.OOOB5
0.00532
0.00114
0.00895
0.00506
IV-301
-------
MODEL TPE-331 TURBOPROP
SAMPLE NUMBER - 3.
MOOE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
EMISSION
RATE
LB/HR
MFAN 3.533
STO DEV 0.640
MEAN 0.393
STO DEV 0.309
MEAN 0.568
STD DEV 0.313
MEAN 2.582
STD DEV 0.443
MFAN 3.533
STD OEV 0.640
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
FUEL
RATE
LB/HR
145.910
16.530
365.419
9.366
339.093
10.361
206.096
7.348
145.910
16.530
FUEL/CYCLE
LBS POLLUTANT/IK HP-HR/CYCLE
MOOE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
LBS POLLUTANT/IOOOK
EMISSION
RATE
LB/HR
MFAN 0.879
STD DEV 0.579
MFAN 0.055
STD OEV 0.062
MFAN 0.053
STO OFV 0.060
MFAN 0.240
STD DEV 0.125
MFAN O.B79
STO OEV 0.579
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
HP-HR AT T.O.
FUEL
RATE
LB/HR
145.910
16.530
365.419
9.166
339.093
10.361
206.096
7.148
145.910
16.530
FUEL/CYCLE
LBS POLLUTANT/IK HP-HR/CYCLE
l>OOE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLF
LBS POLLUTANT/IOOOK
EMISSION
RATE
LB/HR
MFAN 0.955
STD DEV 0.360
MFAN 3.619
STP OEV I .276
MEAN 3.313
STD DEV 1.191
MFAN 1.685
STD OFV 0.593
MEAN 0.955
STD OFV 0.160
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
HP-HR AT T.O.
FUEL
RATE
LB/HR
145.910
16.530
165.419
9.366
319.093
10.361
206.096
7.348
145.910
16.530
FUEL/CYCLE
LBS POLLUTANT/IK HP-HR/CYCLE
LBS POLLUTANT/IOOOK
HP-HR AT T.O.
TIME IN
MODE
MIN.
19.00
0.0
0.50
0.0
2.50
0.0
4.50
0.0
7.00
0.0
NEANI
STO DEV:
MEAN:
STO DEV:
MEAN:
STD OEV:
MEAN:
STO OEV:
TIME IN
MODE
MIN.
19.00
o.o
0.50
0.0
2.50
0.0
4.50
0.0
7.00
0.0
MEAN:
STD DEV:
MFAN:
STD OEV:
MEAN:
STD DEv:
MEAN:
STD OEV:
TIME IN
MODE
MIN.
19.00
0.0
0.50
0.0
2.50
0.0
4.50
0.0
7.00
0.0
MEAN:
STO DEV:
MEAN:
STD OEV:
MEAN:
STO DEV:
MEAN:
STO DEV:
CO
MASS
LBS.
1.119
0.203
0.003
0.003
0.024
0.013
0.194
0.033
0.412
0.075
1.752
0.235
18.310
2.290
31.788
4.764
0.556
0.435
HC
MASS
LBS.
0.278
0.183
0.000
0.001
0.002
0.003
0.018
0.009
0.103
0.067
0.402
0.244
4.215
2.474
7.319
4.557
0.781
0.877
NOX
MASS
LBS.
0.102
0.114
0.030
0.011
0.118
0.050
0.126
0.044
0.111
0.042
0.708
0.239
7.280
1 .956
12.850
4.358
51.975
18.794
FUEL
MASS
LBS.
46.
5.
3.
0.
14.
0.
15.
0.
17.
1.
95.
B.
20
23
05
08
13
43
46
55
02
93
86
08
FUEL
MASS
IBS.
46.
5.
3.
0.
14.
0.
15.
0.
17.
1.
95.
8.
20
21
05
08
13
43
46
55
02
93
86
08
FUEL
MASS
IBS.
46.
5.
3.
0.
14.
0.
15.
0.
17.
1.
95.
8.
20
21
05
08
11
41
46
55
02
91
86
08
LB CO /
IK LB FUEL
24
4
1
0
1
0
12
2
24
4
.351
.413
.082
.848
.684
.936
.537
.145
.351
.413
LB HC /
IK LB FUEL
6
3
0
0
0
0
1
0
6
3
.091
.835
.153
.175
.158
.184
.177
.643
.091
.835
LB NOX/
IK LB FUEL
6
I
9
3
9
3
8
2
6
I
.417
.795
.902
.263
.706
.245
.113
.641
.417
.795
' ENERGY
HP-HR
11.11
0.16
4.87
0.07
21.94
0.32
13.16
0.19
4.09
0.06
55.18
0.87
ENERGY
HP-HR
11.11
0.16
4.87
0.07
21.94
0.32
13.16
0.19
4.09
0.06
55.18
0.82
ENERGY
HP-HR
11.11
0.16
4.87
0.07
21 .94
0.32
13.16
0.19
4.09
0.06
55.18
0.82
LB
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
LB
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
LB
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
CO /
HP-HR
10086
01989
00067
00052
00107
00058
01469
00235
10086
01989
HC /
HP-HR
02520
01695
00009
00011
00010
0001 1
00136
00070
02520
01695
NOX/
HP-HR
02719
01016
00624
00226
00631
00234
00962
00347
02719
01016
IV-302
-------
NOOEL CJ805
SIMPLE NUMBER
MODE
TAXI-IOLE
TAKEOFF
CL IMBOUT
APPROACH
TAXI-IOLE
MOPE
TAXI-IOLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CL IMBOUT
APPROACH
TAXI-IDLE
EMISSION
RATE
IB /MR
MEAN 63.767
STD DEV 13.74*
MEAN 29 .071
STD DEV 4.213
MEAN 28.676
STO DEV 4.992
MFAN 42.829
STO DEV 14.524
MEAN 63.767
STO DEV 13.744
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
EMISSION
RATE
LB/HR
MEAN 27.309
STO OEV 7.638
MEAN 0.556
STO DEV 0.947
MEAN 0.983
STD OEV 0.442
MEAN 2.427
STD DEV 1.882
MFAN 27.309
STD DEV 7.638
TOTAL FOR CYCLE
LBS POLLUTANT/IK IB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOX
EMISSION
RATE
LB/HR
MEAN 1.966
STD OEV 0.490
MEAN 110.632
STO OEV 17.743
MEAN 73.982
STO DEV 6.116
MEAN 17.849
STD DEV 1.362
MEAN 1.966
STD OEV 0.490
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POILUTANT/IOOOK
FUEL
RATE
LB/HR
1000.692
128.982
9999.773
291.241
8290.379
181.826
1776.997
314.310
1000.692
128.982
FUEL /CYCLE
TH-HR /CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
1000.692
128.982
9999.773
291.241
8290.375
181.826
3776.597
314.310
1000.692
12B.982
FUEL /CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
1000.692
128.982
9959.773
291.241
8Z90.375
181.826
3776.597
314.310
1000.692
128.982
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEANI
STO OEV:
MEAN:
STD OEV!
MEAN:
STO OEV:
T.O. MEAN:
STD DEV:
TIME IN
MODE
NIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MFAN:
STD DEV:
MEAN:
STO OEV:
MEAN:
STO OEV:
T.n. MEAN:
STD OEV:
TIME IN
NODE
HIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STO OEV:
MEAN:
STD DEV:
MEAN:
STD DEV:
T.O. MEAN:
STD DEV:
CO
MASS
LBS.
20.193
4.392
0.339
0.049
1.099
0.168
2.899
0.96B
7.440
1.603
31.889
6.947
28.662
4.589
32.786
6.732
3.028
0.439
HC
MASS
LBS.
8.648
2.419
0.006
0.006
0.021
0.016
0.162
0.129
3.186
0.891
12.024
3.297
10.849
2.798
12.363
3.390
0.979
0.970
NOX
MASS
LBS.
0.496
0.143
1.291
0.207
2.713
0.224
1.190
0.091
0.183
0.053
5.872
0.466
5.315
0.376
6.037
0.479
115.242
18.482
FUEL
MASS
LBS.
316.89
40.84
116.20
2.93
303.98
6.67
291.77
20.95
116.75
19.05
1105.98
62.21
FUEL
MASS
LBS.
316.89
40.84
116.20
2.93
303.98
6.67
291.77
20.99
116.79
19.05
1105.58
62.21
FUEL
MASS
LBS.
316.89
40.84
116.20
2.93
303.98
6.67
251.77
20.95
116.75
15.05
1105.58
62.21
LB CO /
IK LB FUEL
63.286
7.634
2.921
0.437
3.488
0.984
11.909
4.613
63.286
7.694
LB HC /
IK LB FUEL
27.147
5. 843
0.056
0.054
0.070
0.053
0.645
0.493
27.147
5.843
LB NOX/
IK LB FUEL
1.547
0.323
11.086
1.569
8.917
0.600
4.739
0.336
1.947
0.323
ENERGY
1 TH-HR
141.87
0.19
130.67
0.13
349.07
0.0
298.67
0.0
32.27
0.06
972.53
1.20
ENERGY
TH-HR
141.87
0.19
130.67
0.13
349.07
0.0
298.67
0.0
52.27
0.06
972.53
1.20
ENERGY
1 TH-HR
141.87
0.19
130.67
0.13
349.07
0.0
298.67
0.0
52.27
0.06
972.53
1.20
LB CO /
f TH-HR
0.14234
0.03068
0.00260
0.00036
0.00303
0.00048
0.00956
0.00324
0.14234
0.03066
LB HC /
1 TH-HR
0.06096
0.01703
0.00005
0.00009
0.00006
0.00009
0.00054
0.00042
0.06096
0.01705
LB NOX/
7H-HR
0.00350
0.00101
0.00988
0.00138
0.00777
0.00064
0.00398
0.00030
0.00350
0.00101
IV-303
-------
MODEL JT)C
SAMPLE NUMBER
toot
TAXt-IDLF
TAKEOFF
ClIHBOUT
APPROACH
T»XI-IDLF
MonE
TAXI-IDLF
TAKFOFF
CLIMBOUT
APPROACH
TAXI-IDLE
"OOF
TAXI-IOLF
TAKEOFF
CLIMBOUT
APPROACH
TAII-IOLF.
EMISSION
RATE
LB/HR
MEAN 9?. 626
SID DEV IB. 370
MEAN 4.0)6
STD OEV 7.846
MFAN 15.957
STD DEV 8.429
MEAN 49.019
STD OEV 23.793
MEAN 92.626
STD OEV 38.370
TOTAL FOR CYCLF
LBS POLLUTANT/IK LB
IBS POLLUTANT/IK LB
LBS POLLUTANT/ IOOOK
EMISSION
RATE
LB/HR
MEAN 92.190
STD DEV 54.930
MFAN 0.855
STO OEV 1.346
MEAN 0.893
STn OEV 0.598
MFAN 8.261
STD DEV 6.687
MEAN 92.190
STD OEV 54.930
TOTAL FOR CYCLE
L"tS P11LUTANT/1K LB
CBS POLLUTANT/IK LB
L3S POLLUTANT/IOOOK
EMISSION
RATE
LB/HR
MEAN 2.489
STO OEV 0.787
MFAN 119.008
STD OEV 25.7B8
MEAN 84.675
STD OEV 13.64?
MEAN 23.212
STD DEV 2.699
MEAN 2. 484
STP OEV 0.787
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LHS POILUTANT/IOOOK
FUEL
RATE
LB/HR
1197.786
89.053
10183.211
413.273
8509.188
342.477
4115.418
245.341
1197.786
89.053
FUEL/CYCLE
TH-HR/CYCLE
Lfl TM-MR AT
FUEL
RATE
18/HR
1197.786
89.053
10183.211
413.273
8509.188
342.477
4119.418
245.341
1 197.786
89.053
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
1197.786
89.053
10183.211
413.273
8509.188
342.477
4115.418
245.341
1197.786
89.053
FUEL/CYCLE
TH-HR /CYCLE
LB TH-HR AT
TIME IN
MODE
NIN.
14.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MFAN:
STO OEV:
NFAN:
STO DEV:
MEAN:
STD DEV:
T.D. MEAN:
STD OEV:
TIME IN
MODE
MIN.
19.00
n.o
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD OEV:
MEAN:
STD DEV:
MEAN:
STD DEV:
r.O. MEANS
STO OEV:
T I ME IN
MODE
NIN.
19.00
0.0
0. 70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STO OEV:
MEAN:
STD nEV:
MEAN:
STD DEV:
T.O. MEAN:
STD OEV:
CO
MASS
LBS.
29.332
12.151
0.105
0.092
0.585
0.309
3.268
1.586
10.806
4.477
44.096
18.172
36.092
14.530
40.766
16.495
0.882
0.764
HC
MASS
LBS.
29.193
17.394
0.010
0.016
0.033
0.022
0.551
0.446
10.755
6.408
40.542
23.891
33.500
20.138
37.926
23.285
0.864
1.362
NOX
MASS
LBS.
0.788
0.249
1.3RH
0.301
3. 105
0.500
1.547
0.180
0.290
0.092
7.119
0.998
5.820
0.837
6.576
0.816
116.722
23.396
FUEL
MASS
LBS.
379.30
28.20
118.80
4.82
312.00
12.56
274.36
16.36
139.74
10.39
1224.21
44.98
FUEL
MASS
LBS.
379.30
28.20
118.80
4.82
312.00
12.56
274.36
16.36
139.74
10.39
1224.21
44.98
FUEL
MASS
LBS.
379.30
28.20
118.80
4.82
312.00
12.56
274.36
16.36
139.74
10.59
1224.21
44.48
LB CO /
IK LB FUEL
77.296
30.070
0.874
0.756
1.873
0.972
12.199
6.355
77.296
30.070
LB MC /
IK LB FUEL
78.505
47.516
0.086
0.135
0.106
0.071
2.018
1.626
78.505
47.516
LB NOX/
IK LB FUEL
2.065
0.578
11.637
2.240
9.929
1.348
5.654
0.734
2.065
0.578
ENERGY
i TH-HR
1B7.74
5.94
138.33
4.41
369. 55
11.78
316.19
10.08
69.17
2.21
1080.97
34.50
ENERGY
TH-HR
187.74
5.99
138.33
4.41
369.55
11.78
316.19
10.08
69.17
2.21
1080.97
34.50
ENERGY
i TH-HR
187.74
5.99
138.33
4.41
364.55
11.78
316.19
10.08
69.17
2.21
1080.97
34.50
LB CO /
TH-HR
0.15618
0.06362
0.00076
0.00066
0.00158
0.00082
0.01030
0.00489
0.15618
0.06362
LB HC /
TH-HR
0.15729
0.09770
0.00007
0.00012
0.00009
0.00006
0.00173
0.00139
0.15729
0.09770
LB NOX/
TH-HR
0.00419
0.00127
0.01000
0.00201
0.00839
0.00122
0.00490
0.00061
0.00419
0 . 00 1 2 7
IV-304
-------
MODEL JTJO
SAMPLE NUMBER 26.
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
EMISSION
RATE
LB/HR
MEAN 101.109
STO OEV 59. 629
MEAN 12.269
STO DEV 8.507
MEAN 15.30}
STD DEV 7.927
MEAN 39.678
STD DEV 19.986
MEAN 109.109
STD DEV 59.629
TOTAL FOR CYCLE
LBS POLLUTANT/ IK IB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION
RATE
LB/N»
MEAN 98.641
STD OEV 58.111
MEAN 4.65*
STO OEV 6.731
MEAN 4.915
STD OEV B. 419
MEAN 7.642
STO OEV 6.332
MEAN 9B.643
STO OEV 58.151
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ 1000K
EMISSION
RATE
LB/HR
MEAN 1.433
STO OEV 0.532
MEAN 148.125
STO DEV 25.842
MEAN 96.216
STD DEV 14. 259
MEAN 21.784
STO OEV 3.099
MEAN 1.433
STD OEV 0.532
TOTAL FOR CYCLE
LBS POLLUTANT/IK IB
LBS POLLUTANT/IK IB
LBS POLLUTANT/IOOOK
FUEL
RATE
LB/HR
871.1)60
196.805
10835.289
821.060
8955.805
662.439
4I3T.551
350.089
871.960
196.805
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
871.960
196.805
10835.289
821.060
8955.805
662.439
4137.551
.150. 089
871.960
196. SOS
FUEL/CYCLE
TM-HR/CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
871.960
196.805
10835.289
821.060
8955.805
662.439
4137.551
350.089
87 1.960
196.805
FUEL/CYCLE
TM-HR/CYCLE
LB TH-HR AT
TINE IN .
NODE
NIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
KEANI
STD DEVI
ME AN I
STD DEV:
MEANl
STO OEV:
T.O. MEAN:
STO OEV:
TINE IN
NODE
NIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STO OEV:
MEAN:
STD DEV:
MEAN:
STO DEVI
T.O. MEAN:
STO DEV:
TIME IN
NODE
NIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD DEV:
MEAN:
STD DEV:
MEAN:
STO OEV:
T.O. MEAN:
STD OEV:
CO
MASS
LBS.
34.551
18.883
0.143
0.099
0.561
0.291
2.645
1.332
I2.T29
6.957
50.630
25.900
45.194
22.182
30.191
15.854
O.T68
0.522
HC
MASS
LBS.
31.237
18.414
0.054
0.102
0.180
0.309
0.523
0.422
11.508
6.784
43.503
25.319
39.030
23.114
25.880
15.438
2.933
5.627
NOX
MASS
LBS.
0.454
0.168
1.728
0.301
3.528
0.523
1.452
0.207
0.167
0.062
7.329
1.090
6.646
0.940
4.335
0.480
93.083
12.371
FUEL
MASS
LBS.
276.12
62.32
126.41
9.58
328.38
24.29
275.84
23.34
101.73
22.96
1108.48
114.52
FUEL
MASS
LBS.
276.12
62.32
126.41
9.5B
328.38
24.29
275.84
23.34
101.73
22.96
1108.48
114.52
FUEL
MASS
IBS.
276.12
62.32
126.41
9.58
328.38
24.29
275.8*
23.34
101.73
22.96
1108.48
114.52
LB CO /
IK LB FUEL
124.010
58.770
1.117
0.761
1.735
0.940
9.634
4.850
124.010
58.770
LB HC /
IK LB FUEL
115.413
70.759
0.416
0.783
0.536
0.912
1.884
1.491
115.413
70.759
LB NOX/
IK LB FUEL
1.664
0.478
13.613
1.656
10.720
1.097
5.277
0.694
1.664
0.478
ENERGY
§ TH-HR
292.91
18.07
215. 83
13.32
576.58
35.57
493.33
30.43
107.92
6.65
1686.58
103.94
ENERGY
1 TH-HR
292.91
16.07
215.83
13.32
576.58
35.57
493.33
30.43
107.92
6.65
1686.58
103.94
ENERGY
TH-HR
292.91
16.07
215.83
13.32
576.58
35.57
493.33
30.43
107.92
6.65
1686.58
103.94
LB CO /
TH-HR
0.11864
0.06647
0.00066
0.00045
0.00098
0.00052
0.00539
0.00280
0.11864
0.06647
LB HC /
f TH-HR
0.10699
0.06461
0.00025
0.00046
0.00031
0.00055
0.00107
0. 00089
0.10699
0.06461
LB NOX/
f TM-HR
0.00155
0.00055
0.00798
0.00106
0.00610
0.00066
0.00294
0.00035
0.00155
0.00055
IV-305
-------
MODEL JT4A
SIMPLE NUMBER ' B.
MODE
TAXI-IDLE
TAKEOFF
CL1NBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKFDFF
CLIMOOUT
APPROACH
TAXI-IDLE
"OOF
TAXI-IOLF
TAKEOFF
r. LI MBOUT
APPROACH
TAXI-IOLF
EMISSION
RATE
LB/HR
MEAN 62.787
STD OEV 17.688
MFAN 18.823
STD OEV 3.994
MFAN 18.277
STD DEV 1.129
MEAN 26.326
STO OEV 9.529
MEAN 62.787
STO OEV 17.688
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
L8S POLLUTANT/IOOOK
EMISSION
RATE
LB/HR
MEAN 64.828
STD OEV 12.819
MEAN 0.674
STD OEV 0.934
MFAN 1.274
STO DEV ?.120
MFAN 3.B34
STP OFV 2.383
MFAN 64.828
STD DEV 12.819
TOTAL FOR CYCLE
LRS POILUTANT/1K LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
EMISSION
RATF
LB/HR
MFAN 2.70R
STO OEV 0.629
MEAN 736.335
STD DEV 78.993
MEAN 155.298
STO OFV 9.813
MEAN 35.859
STD OFV 4.203
MEAN 2.708
STO DEV 0.629
TOTAL FOR CYCLE
LBS PdLLUTANT/lK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
FUEL
RATE
LB/HR
1388.763
103.796
15511.203
427.062
13066.484
240.685
5993.734
324.933
138B.763
103.796
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
1388.763
103.796
15511.201
427.062
13066.484
240.685
5993.734
324.933
1188.763
103.796
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
Lfl/HR
1388.763
103.796
15511.203
477.062
13066.484
240.685
5993. 714
324.931
1188.763
103.796
FUFL/CYCLF
TH-HO/CYCLF
LB TH-HR AT
TIME IN
NODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD DEV:
MEAN:
STD DEV:
MEAN:
STD DEV:
T.n. MEAN:
STD DEV:
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD DEV:
MEAN:
STD OEV:
MEAN:
STO OEV:
T.o. MEAN:
STO DEV:
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD DEv:
MEAN:
STO OEV:
MFAN I
STD DEV:
T.O. MEAN:
STO OEV:
CO
MASS
LBS.
19.882
5.601
0.220
0.047
0.670
0.115
1.755
0.635
7.325
2.064
29.852
8.042
17.971
4.802
18.711
5.041
1.255
0.266
HC
MASS
LBS.
20.529
4.059
0.008
0.011
0.047
0.07B
0.256
0.159
7.563
1.496
28.402
5.487
17.071
3.091
17.80?
3.439
0.449
0.673
NOX
MASS
LBS.
0.857
0.199
2.757
0.338
5.694
0.360
2.391
0.780
0.316
0.073
12.015
0.803
7.731
0.419
7.5M
0.503
157.557
19.379
FUEL
MASS
LBS.
439. 7B
32. 86
180.96
4.98
479.10
8.78
399. 5B
21.66
162.02
12.11
1661.45
47.30
FUFL
MASS
LBS.
439.76
32.86
180.96
4.9R
479.10
8.78
399.58
21.66
162.07
12.11
1661.45
47.30
FUEL
MASS
LBS.
439.78
32.86
180.96
4.98
479.10
B.78
399.58
21.66
162.02
12.11
1661.45
47.30
LB CO /
IK L9 FUEL
45.231
11.907
1.214
0.258
1.399
0.?35
4.412
1.671
45.231
11.907
LB HC /
IK LB FUEL
46.766
8.940
0.043
0.060
0.096
0.160
0.646
0.413
46.766
6.940
LB NOX/
IK LB FUEL
1.941
0.374
15.224
1.714
11.881
0.641
5.976
0.526
1.941
0.174
ENERGY
1 TH-HR
277.08
0.0
, 204.17
0.0
545.42
0.0
466.67
0.0
102.08
0.16
1595.41
1.51
ENERGY
1 TH-HR
277.08
0.0
704.17
0.0
545.4?
0.0
466.67
0.0
102.08
0.16
1595.41
1 .51
ENERGY
i TH-HR
277.08
0.0
204.17
0.0
545.42
0.0
466.67
0.0
102.08
0.16
1595.41
1.51
LB CO /
TH-HR
0.07176
0.02021
0.00108
0.00023
0.00123
0.00021
0.00176
0.00136
0.07176
0.02021
LB HC /
TH-HR
0.07409
0.01465
0.00004
0.00005
0.00009
0.00014
0.00055
0.00034
0.07409
0.01465
L« NOX/
TH-HR
0.00309
0.0007?
0.01350
0.00166
0.01044
0.00066
0.00512
0.00060
0.00309
0.00072
IV-306
-------
MODEL JT8D UNDIl REGULAR
SAMPLE NUMBER
NODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
xnoE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLF
EMISSION
KATE
LB/HR
MEAN 41.395
STD OEV 11. US
MEAN 7.973
STO OEV 1.35*
MEAN 10.621
STO DEV 4.385
MEAN 17.920
STO DEV 1.665
MEAN 41.395
STD DEV 11.1*8
TOTAL FOR CYCLE
L8S POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION
RITE
IB /MR
MEAN 8.322
STD DEV 3.003
MEAN 0.373
STD DEV 0.563
MEAN 0.313
STD OEV 0.459
MEAN 1.171)
STD DEV 1.372
MEAN B.322
STO OEV 3.003
TOTAL FOR CYCLE
IBS POLLUTANT/IK IB
LBS POLLUTANT/IK LB
IBS POLLUTANT/IOOflK
EMISSION
RATE
LB/HR
MEAN 1.T65
STO 05V 0.257
MEAN 101.636
STD DEV 14.360
MEAN 67.746
STO OEV 11.251
MEAN 16.432
STD OEV 2. 870
MEAN 1.T65
STD OEV 0.257
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
L»S POLLUTANT/IK LB
IBS POLLUTANT/ 1000K
FUEL
RITE
LB/HR
823.275
113.528
8517. T2T
165.892
7116.562
93.555
3443.414
1B0.022
823.275
113.528
FUEL/CYCLE
TH-HR/CYCLE
IB TM-M« AT
FUEL
RATE
LB/HR
823.275
113. 528
8517.727
165.892
7116.582
95.555
3445.414
180.022
823.273
113.528
FUEL/CYCLE
TH-HR/CYCLE
18 TH-M» AT
FUEL
RATE
LB/HR
823.273
113.528
8517.727
165.892
7116.582
95.555
3445.414
180.022
823.275
113.528
FUEL/CYCLE
TH-HR/CYCLE
IB TH-HR AT
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEANl
STO OEVl
MEAN:
STO OEVl
MEANi
STD DEVI
T.O. NEANl
STO OEVl
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEANl
STD OEV:
NEANi
STO OEVl
MEAN!
STO DEVI
T.O. MEANl
STO OEV:
TINE IN
NODE
NIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN!
STO OEVl
MEAN!
STO DEV:
MEAN!
STO DEV:
T.O. MEAN:
STO OEVl
CO
MASS
LBS.
13.108
3.530
0.093
0.039
0.1B9
0.161
1.195
0.111
4.829
1.301
19.613
4.967
20.657
4.947
14.671
3.715
0.665
0.279
HC
MASS
LBS.
2.635
0.951
0.004
0.007
0.011
0.017
0.079
0.091
0.971
0.350
3.701
1.276
3.901
1.306
2.768
0.954
0.311
0.469
NOX
MASS
LBS.
0.359
0.081
1.184
0.168
2.464
0.413
1.130
0.191
0.206
0.030
5.565
0.582
5.904
0.805
4.162
0.433
84.697
11.967
FUEL
MASS
LBS.
260.70
33.95
99.37
1.94
260.94
3.31
229.69
12.00
96.05
13.24
946.76
49.19
FUEL
MASS
LBS.
260.70
35.95
99.37
1.94
260.94
3.51
229.69
12.00
96.05
13.24
946.76
49. 19
FUEL
MASS
LBS.
260.70
35.95
99.37
1.94
260.94
3.51
229.69
12.00
96.05
13.24
946.76
49. 19
LB CO /
IK LB FUEL
50.320
13.014
0.934
0.388
1.493
0.617
5.210
0.518
50.320
13.014
LB HC /
IK LB FUEL
10.102
3.399
0.043
0.066
0.044
0.065
0.332
0.368
10.102
3.399
LB NOX/
IK LB FUEL
2.172
0.410
11.930
1.644
9.517
1.559
4.959
1.097
2.172
0.410
» ENERGY
TH-HR
266.00
0.0
163.33
0.0
436.33
0.0
373.33
0.0
98.00
0.14
1337.00
2.08
ENERGY
t TH-HR
266.00
0.0
163.33
0.0
436.33
0.0
373.33
0.0
98.00
0.14
1337.00
2.08
ENERGY
1 TH-HR
266.00
0.0
163.33
0.0
436.33
0.0
373.33
0.0
98.00
0.14
1337.00
2.08
LB CO /
TH-HR
0.04928
0.01327
0.00057
0.00024
0.00089
0.00037
0.00320
0.00030
0.04928
0.01327
LB HC /
* TH-HR
0.00991
0.00357
0.00003
0.00004
0.00003
0.00004
0.00021
0.00024
0.00991
0.00357
LB NOX/
1 TH-HR
0.00210
0.00031
0.00726
0.00103
0.00569
0.00095
0.00303
0.00051
0.00210
0.00031
IV-307
-------
MODEL JTSO UNniL SMOKELESS SIMPLE NUMBER > 18.
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
HOOE
TAXI-IOLF
TAKEOFF
r.LIMBOUT
APPROACH
TAXI-IOLE
MODE
TAXI-IOLF
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
EMISSION
RATE
LB/HR
MFAN 37.369
STD DFV 11 .750
MFAN 5.617
STD OEV 1.997
MEAN 6.204
STD DEV 1.926
MEAN 11.960
STD OEV 4.937
MFAN 37.389
STD OEV 11.750
TOTAL FOR CYCLF
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
FMISSION
RATE
IB/MR
MEAN 6.755
STn DEV 5.75*
MEAN 0.381
STO OEV 0.8*0
MFAN 0.396
STD OFV 0.736
MEAN 0.850
STn OEV 0.913
MEAN 8.755
STn OEV 5.75*
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POILUTANT/1K LB
LBS POLLUTANT/IOOOK
EMISSION
RATE
LB/MR
MFAN 1.8*1
STO OEV 0.597
MEAN 133.295
STD DEV 33.587
MEAN 86.972
STD DFV 19,*T7
MEAN 20.2*2
STD DEV 5.826
MEAN 1.8*1
STO nFV 0.597
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
FUEL
RATE
LB/HR
657.216
11*. 788
8677.555
210.983
7171.270
160.470
3572.512
452.440
857.216
11*. 788
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
857.216
11*. 788
8677.555
210.983
7171.270
160.470
3572.512
*52.*40
657.216
114.788
FUFL/CYCLF
TH-HR/CYCLF
LR TH-HR AT
FUEL
OATF
LB/HR
857.216
114.788
8677.555
210.983
7171.770
160.470
3572.512
452.4*0
857.216
114. 788
FUEL/CYCLE
TH-HR/CYCLF
LB TH-HR AT
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD OEV:
MEAN!
STD DEV:
MEAN:
STD OEV:
T.O. MEAN:
STO DEV:
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STO OEV:
MEAN:
STO DEV:
MEAN:
STD OEV:
T.O. MEAN:
STO DEV:
TIME IN
MOOF
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD OEV:
MEAN:
STD DEV:
MEAN:
STD nEV:
T.n. MFAN:
STD OEV:
CO
MASS
LBS.
11.8*0
3.721
0.066
0.023
0.227
0.071
0.797
0.329
*. 362
1.371
17.292
5.133
17.7*8
5.109
12.488
3.707
0.452
0.161
HC
MASS
LBS.
2.772
1.822
0.00*
0.010
0.015
0.027
0.057
0.061
1.021
0.671
3.669
2.461
3.9*8
2.3**
2.79*
1.792
0.307
0.676
NOI
MASS
LBS.
0.583
0.189
1.555
0.397
3. 189
0.71*
1.349
0.366
0.715
0.070
6.891
1.651
7.076
1.692
4.977
1.192
107.249
27.024
FUEL
MASS
LBS.
271.45
36.35
101.24
2.45
262.95
5.68
238.17
30.16
100.01
13.39
973.61
67.79
FUEL
MASS
LBS.
271.45
36.35
101.24
2.45
262.95
5.88
238.17
30.16
100.01
13.39
973.81
67.79
FUEL
MASS
LBS.
771.45
36.35
101.24
2.45
262.95
5.68
738.17
30. 16
100.01
13.39
973.81
67.79
LB CO /
IK LB FUEL
43.7*6
13.411
0.6*6
0.232
0.867
0.27*
3.420
1.466
43.746
13.411
LB HC /
IK LB FUEL
10.131
5.784
0.044
0.097
0.055
0.096
0.224
0.195
10.131
5.764
LB NOX/
IK LB FUEL
2.157
0.717
15.34*
3.825
12.111
2.631
5.663
2.157
0.717
ENERGY
1 TH-HR
275.50
0.5*
169.17
O.ll
451.92
0.94
366.67
0.59
101.50
0.06
1384.75
1.37
ENERGY
TH-HR
275.50
0.54
169.17
0.11
451.92
0.94
386.67
0.59
101.50
0.06
1384.75
1.37
ENERGY
t TH-HR
275.50
0.54
169.17
O.ll
451.92
0.94
386.67
0.59
101.50
0.06
1384.75
1.37
LB CO /
« TH-HR
0.0*296
0.01351
0.00039
0.0001*
0.00050
0.00016
0.00206
0.00085
0.0*298
0.01351
L8 HC /
< TH-HR
0.01006
0.00661
0.00003
0.00006
0.00003
0.00006
0.00015
0.00016
0.01006
0.00661
L8 NOX/
1 TH-HR
0.00212
0.00069
0.00919
0.00732
0.00706
0.00158
0.003*9
0.00100
0.00712
0.00069
IV-308
-------
MODEL JT8D OIL REGULAR
SAMPLE NUMBER
T.
"DOE
TAXI-IDLE
TAKEOFF
CLINBOAJT
APPROACH
TAXI-IOLE
NODE
TAXI-IOLE
TAKEOFF
CLIHBdUT
APPROACH
TIKI-IDLE
tone
TAXI-IDLE
TAKEOFF
CLIM80UT
APPROACH
TAXI-IOLE
EMISSION
RITE
LB/MR
MEAN 59.563
STD DEV 11.689
MEAN 18.344
STO DEV 19.116
MEAN 19.403
STD DEV 14.906
MEAN 37.329
STD DEV 1.411
MEAN 39.S63
STD DEV 11.689
TOTAL FOR CYCLE
LBS POLLUTANT/IK IB
IBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
EMISSION
RATE
1 6 /MR
NFAN 11.0*8
STD OEV 6.439
MEAN 0.316
srn OEV 0.321
MEAN O.B27
STD DEV 1 .0*2
MFAN 3.343
STO OEV 2.180
MEAN 11.048
STD OEV 6.439
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK IB
LBS POLLUTANT/1000K
EMISSION
RATE
LB/HR
MEAN 2.908
STO OEV 1.494
MEAN 191. 272
STO OEV 21.T03
MFAN 100.144
STO DEV 19.169
MEAN 28.048
srn OEV 3.099
MEAN 2.908
STO OEV 1.494
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANTMOOOK
FUEL
RATE
LB/HR
891.680
213.480
8407.422
181.373
7098.939
179.837
3498.899
208.301
891. 680
213.480
FUEL /CYCLE
TH-HR /CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
891.680
213.480
8407.422
181.373
7098.539
IT9.837
3498.899
208.301
891.680
213.480
FUEL /CYCLE
TM-HR /CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
891.680
213.480
8407.422
181.373
7098.939
179.837
3498.899
208.301
B9I.6BO
213.480
FUEL/CYCLE
TM-MR/CYCLE
LB TH-HR AT
TIME IN
MODE
M1N.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEANl
STO OEV:
MEANl
STD DEVI
MEAN!
STO DEVI
T.O. MEANl
STD DEVt
TINE IN
NODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD OEV:
MEAN!
STD OfV:
MEANl
STD DEVI
T.O. MEAN:
STD DEVI
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEANl
STO DEV:
DEAN:
STD DEVI
MEANl
STO DEVI
T.O. MEANl
STD DEVI
CO
MASS
LBS.
12.92B
3.700
0.216
0.186
0.711
0.932
2.199
0.661
4.616
1.363
20.227
3.222
20.793
4.771
15.128
3.909
1.549
1.326
Mt
MASS
LBS.
3.499
2.039
0.004
0.004
0.030
0.038
0.223
0.149
1.289
0.791
5.044
2. 876
5.026
2.627
3.773
2.151
0.263
0.268
N0>
MASS
LBS.
0.921
0.460
1.765
0.293
3.672
0.703
1.870
0.204
0.339
0.170
B. 967
1.082
8.840
1.194
6.408
0.809
126.060
18.086
FUEL
MASS
LBS.
282.37
67.60
48.09
2.12
260.2B
6.60
230.59
13.89
104.03
24.91
979.39
109.89
FUEL
MASS
LBS.
282.37
67.60
98.09
2.12
260.28
6.60
230.99
13.89
104.03
24.91
979.35
109.89
FUEL
MASS
LBS.
282.37
67.60
98.09
2.12
260.28
6.60
230.59
13.89
104.03
24.91
973.35
109. 89
LB CD / '
IK LB FUEL
45.370
10.694
2.224
1.961
2.T59
2.139
9.468
3.253
43.370
10.694
LB HC /
IK IB FUEL
11.790
9.419
0.03B
0.039
0.117
0.146
0.977
0.636
11.750
9.415
L8 NOX/
IK LB FUEL
3.196
1.016
18.000
2.561
14.116
2.679
8.128
0.997
3.156
1.016
ENERGY
1 TH-MR
266.00
0.0
163.13
0.0
436.33
0.0
373.33
0.0
98.00
0.14
1337.00
2.08
ENERGY
1 TH-HR
266.00
0.0
163.33
0.0
436.33
0.0
373.33
0.0
98.00
0.14
1337.00
2.08
ENERGY
TH-HR
266.00
0.0
163.33
0.0
436.33
0.0
373.33
0.0
98.00
0.14
1337.00
2.08
IB CO /
TH-HR
0.04710
0.01391
0.00132
0.00114
0.00163
0.00122
0.00577
0.00177
0.04710
0.01391
LB HC /
f TM-HR
0.01315
0.00767
0.00002
0.00002
0.00007
0.00009
0.00060
0.00039
0.01315
0.00767
LB NOX/
f TH-HR
0.00346
0.00173
0.01081
0.00153
0.00842
0.00161
0.00501
0.00099
0.00346
0.00173
IV-309
-------
HODEL JT8D Oil SMOKELESS
SAMPLE NUMBER 26.
MORE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIHOOUT
APPROACH
TAXI- IDLE
M10E
T A X 1 - I OL f
TAKEOTF
r. LI "BOUT
APPROACH
TAXI-IDLE
EMISSION
RATE
LB/HR
MEAN 33.402
STD OEV 17.395
MEAN 7.490
STD OEV 5.447
MEAN 8.892
STO DEV 4.848
MEAN 16.184
STD D6V 6.147
MEAN 33.40?
STO DEV 17.385
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IOOOK
EMISSION
RATE
LB/HR
MEAN 6. 994
STO OEV 3.306
MFAN 0.778
STD DFV 1.094
MEAN 0.921
STD OEV 0.994
MFAN 1.753
STD DEV 0.884
MEAN 6.994
STD DEV 3.306
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IDOOK
EMISSION
RATF
LB/HR
MFAN 2.913
STD DEV 1 .232
MEAN 197.74?
STD DFV 15.161
"FAN 131.017
STO HFV 19.775
MEAN 10.B50
STO OEV 4.724
MFAN 2.913
STD nev 1.212
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
FUEL
RATE
LB/HR
959.329
59.663
8754.512
375.860
7336.766
266.697
340B.656
167.198
959.129
59.663
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
959.329
59.663
8754.512
375. B60
7136.766
266.697
1408.656
167.198
959.329
59.663
FUEL/CYCLE
TH-HR/CYCLE
L* TH-HR AT
FUEL
RATE
LB/HR
959.329
59.661
(1754. 512
375. B60
7336.766
266.697
3408.656
167.198
959.329
59.663
F1IFL/CYCLF
TH-HR/CYCLE
LB TH-HR AT
TIME IN
MODE
MtN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEANI
STD OEV:
MEAN:
STD DEV:
MEAN:
STD OEV:
T.O. MEAN:
STO OEV:
TIME IN
MODE
M1N.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STO DEV:
MEAN:
STO OEV:
MEAN:
STO OEV:
T.O. MFAN:
STO OFV:
TIME IN
MOOE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STO DEV:
MEAN:
STO OFV:
MEAN:
STO OFV:
T.O. MFAN:
STD OEV:
CO
MASS
LBS.
10.577
5.505
0.087
0.064
0.326
0.176
1.21?
0.410
1.897
2.028
16.100
7.611
15.741
6.671
11.519
5.036
0.604
0.442
HC
MASS
LBS.
2.215
1.047
0.009
0.013
0.034
0.036
0.117
0.059
0.616
0.386
3.190
1.473
3.139
1.388
2.295
1.027
0.613
0.662
NOX
MASS
LBS.
0.921
0.390
2.307
0.410
4.804
0.725
2.057
n.315
0.340
0.144
10.430
1.594
10.274
1 .4?9
7.520
1.027
156.640
24.647
FUEL
MASS
LBS.
303.79
16.91
102.14
4.38
269.01
9.77
227.24
11.15
1 11 . 92
6.96
1014.10
42.47
FUEL
MASS
LBS.
303.79
16.91
102.14
4.16
269.01
9.77
227.24
11.15
1 1 1 . 92
6.96
1014. 10
42.47
FUEL
MASS
LBS.
303.79
18.91
107. 14
4.38
269.01
9.77
227.24
11.15
111.92
6.96
1014.10
42.47
LB CO /
IK LB FUEL
14.495
IS. 561
0.655
0.629
1.214
0.671
5.335
1.758
34.495
15.561
LB HC /
IK IB FUEL
7.284
3.240
0.067
0.122
0.124
0.134
0.515
0.262
7.264
3.240
LB NOX/
IK LB FUEL
1.051
1.252
22.513
3.391
17.622
2.333
9.055
1. 307
3.051
1.252
ENERGY
1 TH-MR
275.50
9.73
169.17
5.95
451.91
15.92
366.67
13.61
101.50
3.57
1384.75
46.69
ENERGY
1 TH-HR
275.50
9.73
169.17
5.95
451.91
15.92
386.67
13.61
101.50
3.57
1364.75
48.69
ENERGY
1 TH-HR
?75.50
9.73
169.17
5.95
451.91
15.92
166.67
13.61
101.50
3.57
1364.75
46.69
LB CO /
TH-HR
0.03800
0.01835
0.00052
0.00038
0.00072
0.00040
0.00113
0.00105
0.03800
0.01635
L8 HC /
TH-HR
0.00801
0.00167
0.00005
0.00007
0.00007
0.00008
0.00030
0.00015
0.00601
0.00367
LB NOX/
f TH-HR
0.00114
0.00139
0.01360
0.00211
0.01061
0.00140
0.00532
0.00081
0.00334
0.00119
IV-310
-------
MODEL JT90
SAMPLE NUMBER
MODE
TAXI-IDLE
TAKEOFF
CLIMB OUT
APPROACH
TAXI-IDLE
NODE
T»«I-IDLE
TAKEOFF
ClIMBOUT
APPROACH
TAXI-IOLF
HOOE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
EMISSION
RATE
16/HR
MEAN 101.869
STD OEV 27.782
MEAN a. 291
STD DEV 5.363
MEAN 11.7*1
STD DEV 3.670
MEAN 32.570
STD DEV 11.269
MEAN 101.869
STO OEV 27.702
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION
RATE
IB/MR
MFAN 27.313
STO OEV 22.277
MEAN 2.933
STO OEV 2.219
MEAN 2.647
STD OEV 1.806
MEAN 2.997
STO OEV 1.376
MEAN 27.319
STD OEV 22.277
TOTAL FOR CYCLE
LflS POLLUTANT/IK LB
L8S POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION
RATE
LB/HR
MEAN 6.061
STD OEV 2.19*
MFAN 719.951
STO OEV 151.6*2
MEAN 458.604
STD OEV 81.759
MEAN 54.101
STD DEV 5.727
MEAN 6.061
STO DEV 2.19*
TOTAL FOB CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLIUTANT/1000K
FUEL
RATE
LB/MR
1737.835
192.909
17012.313
B21.37S
14316.879
820.809
5203.895
468.229
1737.835
192.909
FUEL/CYCLE
TH-HR/CVClf.
LB TM-HR AT
FUEL
RATE
LB/HR
1737.835
192.909
17052.313
821.375
14316.879
020.809
5203.895
468.229
1737. 835
192.909
FUEL/CYCLE
TH-HR /CYCLE
IB TH-HR AT
FUEL
RATE
LB/HR
1737.835
192.909
17052.313
821.375
14116.B79
820.809
5203.895
468.229
1737.835
192.909
FUEL /CYCLE
TH-HR/CYCLE
LB TH-HR AT
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
NEANl
STO OEV:
MEANl
STO DEVI
MEANt
STD DEVI
T.O. MEAN!
STD OEV:
TIME IN
MOOE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEANl
STO DEVI
MEAN:
STO OEV:
MEAN:
STD DEV:
T.O. MEAN:
STD OEV:
TIME IN
NODE
HIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEANt
STO OEV:
MEAN:
STD DEv:
MFAN:
STO OEV:
T.O. MEAN:
STO OEV:
CO
MASS
IBS.
32.259
8.798
0.097
0.063
0.490
0.13}
2.171
0.751
11.885
1.241
46.842
11.876
25.512
5.061
11.316
3.081
0.218
0.143
HC
MASS
LBS.
8.649
7.054
0.034
0.026
0.097
0.066
0.200
0.092
3.187
2.599
12.167
9.768
6.594
5.021
2.950
2.427
0.779
0.587
NOX
MASS
LBS.
1.919
0.695
8.399
1.769
16.815
2.997
J.607
0.382
0.707
0.256
31.448
5.129
17.227
2.231
7.581
1.31J
IBB. 690
41.875
FUEL
MASS
LBS.
550.31
61.09
198.94
9.58
524.95
30.09
346.93
31.21
202.75
22.51
1823.88
139.32
FUEL
MASS
LBS.
550.31
61.09
198.94
9.58
524.95
30.09
346.93
31.21
202.75
22.51
1823.88
139.32
FUEL
MASS
LBS.
550.31
61.09
198.94
9.58
524.95
30.09
346.93
31.21
202.75
22.51
1023.88
139.32
LB CO /
IK LB FUEL
58.124
11.125
0.407
0.320
0.823
0.264
6.419
2.808
58.124
11.125
LB HC /
IK LB FUEL
15.366
11.403
0.173
0.131
0.104
0.127
0.590
0.280
15.366
11.403
LB NOX/
IK LB FUEL
3.497
1.210
41.990
7.069
11.092
4.201
10.457
1.323
3.497
1.210
' ENERGY
1 TH-HR
988.08
23.39
520.46
12.30
1390.38
32.86
892.22
21.14
364.12
0.60
4156.26
98.25
ENERGY
TH-HR
988.08
23.19
520.46
12.10
1190.10
12.86
092.22
21.14
164.32
0.60
4156.26
98.25
ENERGY
1 TH-HR
988.88
21.39
520.46
12.10
1190.18
32.86
892.22
21.14
164.32
8.60
4156.26
98.25
LB CO /
f TH-HR
0.03277
0.00956
0.00019
0.00012
0.00011
0.00010
0.0024}
0.00080
0.01277
0.00956
LB HC /
TH-HR
0.00881
0.00716
0.00007
0.00005
0.00007
0.00005
0.00022
0.00010
0.00801
0.00736
LB NOX/
1 TH-HR
0.00194
0.00070
0.01617
0.00359
0.01212
0.00231
0.00404
0.00044
0.00194
0.00070
IV-311
-------
MODEL SPFY MK/511
SAMPLE NUMBER
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
T 1 X 1 - I OL E
TAKEOFF
CLIMBOUT
APPROACH
TAXI-miF
MOOE
T«XI-tnLF
TAKEOFF
CLIMBOIJT
APPROACH
TAXI-10LF
EMISSION
RATE
LB/HR
HFAN 60.173
STO OEV 11. MH
MEAN 14.716
STD OEV 2.944
MEAN 15.251
STD OEV 1.604
MEAN 31. 068
STB OEV 10.078
MFAN 60.173
STD DEV 11.601
TOTAL FOR CYCLE
LRS POLLUTANT/IK LB
LBS POILUTANT/1K LB
LBS POLLUTANT/ 1000K
EMISSION
RATE
LB/HO
MEAN 66.051
STO DEV 11 .083
MFAN 0.0
STD DEV 0.0
MEAN 0.242
STO DEV 0.221
MEAN 4.224
STD OEV 4.447
MEAN 66.051
STO OEV 11.083
TOTAl FOR CYCLE
LBS POLLUTANT/IK LB
LBS PDLLUTANT/1K LB
LBS POLLUTANT/1000K
EMISSION
RATE
LB/HR
MEAN 0.849
SID OEV 0.381
MFAN 153.012
STO OEV 9.845
MFAN 114.751
STD DFV 13.724
MFAN 30.446
STD nEV 5.197
MFAN 0.641
STn OEV 0.381
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/1K LB
LBS POLLUTANT/IOOOK
FUEL
R4TF
18/HR
661.542
110.889
7625.230
150.022
6354.934
60.639
1051.668
123.020
661.542
110.889
FUEl/CYCLF
TH-HR/CYCLE
LB TH-HR AT
FUFL
RATE
LB/HR
661.542
110.889
7625.230
150.022
6354.934
60.831
3051.668
123.028
661.547
110.881
FUEl /CYCLE
TH-HR /CYCLE
L8 TH-HR AT
FUEL
RATE
IB/HR
661.542
110. 881
7625.230
150.022
6354.934
60.839
3051.669
127.028
661.542
110.881
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD DEV:
MEAN:
STD OEV:
MFAN:
STO OEV:
T.O. MEAN:
STD OEV:
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD DEV:
MEAN:
STD OEV:
MEAN:
STO OEV:
T.O. MFAN:
STD DEV:
TIME IN
MODE
MIN.
19.00
0.0
n. 70
0.0
2.20
o.o
4.00
0.0
7.00
0.0
MEAN:
STO OEV:
MFAN:
STD OEV:
MEAN:
STO DEV:
T.O. MEAN:
STO DEV:
CO
MASS
LBS.
19.055
6.207
0.166
0.034
0.559
0.066
2.605
0.672
7.020
2.287
29.405
9.054
35.942
9.707
21.705
9.147
1.455
0.301
HC
MASS
LBS.
20.916
3.510
o.o
0.0
0.009
0.008
0.282
0.296
7.706
1.293
29.912
4.542
35.776
6.654
29.207
4.588
0.0
0.0
NOX
MASS
LBS.
0.269
n.121
1.785
0.115
4.208
0.503
2.030
0.346
0.099
0.044
8. 391
0.842
1 0 . 39 7
1.524
8.476
0.850
156.591
10.075
FUEL
MASS
LBS.
201.41
35.12
88.96
1.T5
233.01
2.24
203.44
8.21
TT.1B
12.94
B12.09
43.96
FUEL
MASS
LBS.
209.49
35.12
86.16
1.75
233.01
2.24
203.44
8.21
77.16
12.94
812.09
41.96
FUEL
MASS
LBS.
209.49
35.12
88.16
1.75
233.01
2.24
203.44
8.21
77.18
12.14
612.01
43.96
IB CO /
IK LB FUEL
69.861
20.325
1.870
0.426
2.401
0.298
12.666
3.550
89.861
20.325
Lfl HC /
IK LB FUFL
102.665
26.897
0.0
0.0
0.038
0.035
1.394
1.451
102.665
28.897
LB NOX/
IK LB FUEL
1.271
0.501
20.061
1.519
16.073
2.316
9.939
1.331
1.271
0.501
' ENERGY
1 TH-HR
144.40
0.0
133.00
0.25
355.30
0.0
304.00
0.0
53.20
0.0
189.90
0.0
ENERGY
TH-HR
144.40
0.0
133.00
0.25
355.30
0.0
304.00
0.0
53.20
0.0
989.90
0.0
ENERGY
t TH-HR
144.40
0.0
133.00
0.25
355.30
0.0
304.00
0.0
53.20
0.0
181.90
0.0
LB CO /
1 TH-HR
0.13196
0.04298
0.00125
0.00026
0.00157
0.00019
0.00857
0.00221
0.13196
0.04298
LB HC /
TH-HR
0.14465
0.02430
0.0
0.0
0.00003
0.00002
0.00093
0.00018
0.14485
0.02430
LB NHX/
TH-HR
0.00186
0.00084
0.01342
0.00066
0.01184
0.00142
0.00666
0.00114
0.00166
0.00064
IV-312
-------
DATE! 6/1T/TI
TEST ORGANIIATIONl S W R I KELLY
ENGINE SUPPIIERI USAF, KELLY AFB
ENGINE DATA
CAL ID NUMBER! I ENGINE TYPE AND MODEL: T56-ATB
RATED HORSEPOWER! 3755.
ENGINE TOTAL TIMEl -0. MRS
TIME SINCE HOT SECTION OVERHAULi 0. MRS
TINE SINCE!
Nl COMPRESSOR OVERHAULI 0. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
CONBUSTOR CAN REPLACEMENT! 0. HRS
FIRST STAGE N012LE GUIDE VANE OVERHAULI 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL! -0. HRS
FUEL H/C RATIO! 1.995
SERIAL NUMBER!
AE-102635
FUEL I JP-4
OPERATIONAL DATA »««»»««*»«*»«»
INLET AIR TEMPERATURE. DEGREES F: START 91.00 FINISH 90.00
ATMOSPHERIC PRESSURE! START 28.93 FINISH 28.93
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0166
RELATIVE HUMIDITY! 52.00 PERCENT
SAMPLE LINE! TEMPERATURE. DEGREES Cl 150.00. FLOW RATE, LITERS/HIM:
SAMPLE LINE TRANSPORT TINE, SEC! 0.50
NUMBER OF TESTS! 0
COMMENTS:
F/A CALCULATION BASED ON EXHAUST COMPOSITION 2ND LAST RUN
SHP DATA MAS BACK-CALCULATED
391
ELAPSED
TIME
0.0
5.00
10.50
15.00
18.00
19.50
21.00
24.00
POWER
PERCENT
RATED
T.O.
60
86
93
0
0
0
0
0
POWER
PERCENT
P
RATED
T.O.
60
86
93
0
0
0
0
0
POWER
ERCENT
RATED
T.O.
60
86
93
TEST
MODE
I/ 0
21 1
3/ 2
4/ 3
>/ 4
4/ 5
7/ 4
B/ 7
EXHAUST
GAS
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
CO
LB/IK
LB FUEL
2.41
1.83
1.58
3.60
1.2B
3.56
26.27
4.27
CO
POWER ENGINE MEASURED GAS GEN CALC COMPRESSOR ENGINE TURBINE
THRUST.LBS PERCENT SPEED FUEL AIR FLOW F/A DISCHARGE PRESSURE INLET
OR RATED RPM FLOW LB/SEC TEMP RATIO TEMP
SHP T.O. Nl N2 LB/HR DEGREES F EPK DEGREES f
2268.00 60 13800.00 -0.00 1450.00 30.00 0.013400 -0.00 -0.00 1510.00
3238.00 86 13800.00 -0.00 1800.00 30.00 0.016700 -0.00 -0.00 1700.00
3502.00 93 13800.00 -0.00 1450.00 30.00 0.013400 -0.00 -0.00 1510.00
-0.00 0 13300.00 -0.00 820.00 27.90 0.008200 -0.00 -0.00 1128.00
-0.00 0 14000.00 -0.00 2050.00 30.80 0,018500 -0.00 -0.00 1660.00
-0.00 0 13400.00 -O.OO 810.00 28.40 0.007900 -0.00 -0.00 1120.00
-0.00 0 9950.00 -0.00 560.00 14.70 0.010600 -0.00 -0.00 1150.00
-0.00 0 13300.00 -0.00 705.00 27.90 0.007000 -0.00 -0.00 1050.00
EXHAUST CO CO THC NO NO NO ALOEHVOES SMOKE PARIICULMES
GAS IWEI) 2 IWET) IWET) 2 X
PRESSURE PPCV IWET) PPNV PPMV IWETI INETI
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS ENI
HC
LR/1K
LB FUEL
0.0
0.0
0.0
0.0
0.0
0.0
12.32
0.16
LB/IK HP-HR
1.539
1.015
0.6
*HDRSEPOWER-HR OR
*
HORSEPOWER-HR OR
HORSE
POWER-HR OR
*HORSFPOWER-HR OR
*HORSEPnWER-HR OR
S3
IHRUST-HR
THRUST-HR
THRUST-HR
THRUST-HR
TKRUST-HR
PERCENT V
31.00 2.57 0
28.00 3.06 0
26.00 3.29 0
28.00 1.55 0
24.00 3.74 0
28.00 1.57 0
287.00 2.13 235
30.00 1.40 2
MASS EMI MASS EMI MASS EMI
N02 C02 NO
LB/IK LB/IK LB/IK
L8 FUEL LB FUEL LB FUEL
-0.00 3135.09 -0.00
-0.00 3136.00 -0.00
-0.00 3136.39 -0.00
-0.00 3133.21 -0.00
-0.00 3136.86 -0.00
-0.00 3133.28 -0.00
-0.00 3063.79 -0.00
-0.00 3131.72 -0.00
CO THC
2
LB/IK HP-HR LB/IK HP-HR
2004.356 0.0
1743.298 0.0
1298.621 0 0
BASIS NOT CALCULABLE*
BASIS NOT CALCULABLE*
BASIS NOT CALCULABLE*
BASIS NOT CALCULABLE*
BASIS NOT CALCULABLE*
PPMV PPMV
.0 -0
.0 -0
.0 -0
.0 -0
.0 -0
.0 -0
.00 -0
.00 -0
MASS EMI
NOX
LB/IK
LB FUEL
10.33
12.32
12.36
6.76
11.14
6.68
4.21
6.08
.00
.00
.00
.00
.00
.00
.00
.00
MASS
CO
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
EMI
LB/HR
3.
3.
2.
2.
2.
2.
14.
3.
49
29
29
95
6)
88
71
01
NO
LB/IK
-0
-0
-0
HP-HR
.000
.000
.000
00 81.00 -0
00 115.00 -0
00 124.00 -0
00 32.00 -0
00 127.00 -0
00 32.00 -0
00 28.00 -0
00 26.00 -0
MASS EMI MASS EH]
HC NO 2
LB/HR LB/HR
0.0 -0.00
0.0 -0.00
0.0 -0.00
0.0 -0.00
0.0 -0.00
0.0 -0.00
6.90 -0.00
0.11 -0.00
NO
2
.00 -0
.00 -0
.00 -0
.00 -0
.00 -0
.00 -0
.00 -0
.00 -0
MASS EMI
CO 2
LB/HR
4545.68
5644.30
4547.77
2569.23
6430.55
2537.96
1715.72
2207.06
NO
X
.00 -0.00
.00 -0.00
.00 -0.00
.00 -o.oo
.00 -0.00
.00 -0.00
.00 -o.oo
.00 -0.00
MASS EPI MASS
EMI
NO NOX
L8/HR LB/HH
-0.00 14
-0.00 22
-0.00 17
-0.00 5
-0.00 22
-0.00 5
-0.00 2
-0.00 4
.98
.18
.92
.55
.81
.41
.36
.29
LB/IK HP-HR LB/IK HP-HH
-0.000
-0.000
-0.000
6.604
6.849
5.117
IV-313
-------
DAFE: 7/26/71
TEST ORGANIZATION: UNITED/EPA
ENGINE SUPPLIER: UNITED AIRLINES
ENGINE DAT* »«««»«»«»«««««««»
CAL ID NUMBER: 137 ENGINE TYPE AND MODEL: ji 3C - 7
SERIAL NUMBER:
RATED THRUST: 12000.
ENGINE TOTAL TIME: IB499. MRS
TIME SINCE HOT SECTION OVERHAUL: 2614. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 261*. HRS
N2 COMPRESSOR OVERHAUL: 2614. HRS
COMBUSTOR CAN REPLACEMENT: 2614. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 261*. HRS
Nl TURBINE OVERHAUL: 2614. HRS
N2 TURBINE OVERHAUL: 2614. HRS
FUEL H/C RATIO: 1.920
FUEL: JET - A
OPERATIONAL DATA »«»«»»««»»«««
INLET AIR TEMPERATURE. DEGREES F: START 57.20 FINISH 57.20
ATMOSPHERIC PRESSURE: START 29.94 FINISH 29.93
INLET AIR HUMIDITY, IBS H20/LB AIR: 0.0094
RELATIVE HUMIDITY: 94.00 PERCENT
SAPPLE LINE: TEMPERATURE, CEGREES C: 160.00, FLOW RATE, LITERS/HIN:
SAMPLE LINE TRANSPORT TIME, SEC: 5.00
NUMBER OF TESTS: 3
COMMENTS:
ENGINE OVERHAULED AND CARBO - BLASTED
90 PROBE USED FOR SAMPLING
EXHAUST GAS TEMPERATURE IN DEGREES C
EXHAUST GAS PRESSURE IN INCHES HG.
CLOCK
TIME
0.73
737.00
742.00
POWER
PERCENT
RATED
T.O.
65
76
91
POWER
PERCENT
RATED
T.O.
65
76
91
POWER
PERCENT
RATED
T.O.
65
76
91
TEST POWER ENGINE MEASURED GAS GEN CALC COMPRESSOR ENGINt
MODE THRUST.LBS PERCENT SPEED FUEL AIR FLOW F/A DISCHARGE PRfcSSUKE
OR RATED KPM FLOW LB/SEC TFMP RATIO
SHP T.O. Nl N2 LB/HR DEGREES F EPR
I/ 0 7B34.00 65 5816.00 9164.00 6369.00 -0.00 -0.000000 -0.00 2.14
2/ I 9169.00 76 6055.00 9381.00 7465.00 -0.00 -0.000000 -0.00 2.16
3/ 2 10961.00 91 6416.00 9699.00 9186.00 -0.00 -0.000000 -0.00 2.66
TURBINF
INLET
TEMP
DEGPEfS f
-0.00
-0.00
-0.00
EXHAUST EXHAUST CO CO THC NO NO NO ALDEHYDES SMOKE PAR I ICUL A I ES
GAS GAS (WET) 2 (WETI (WETI 2 X
TEMP PRESSURE PPMV (WET) PPMV PPMV (WET) IUETI
DEGREES F PSIA PERCENT V PPMV PPMV
464.00 62.60
508.00 68.70
576.00 76.80
MASS EMI MASS EMI
CO HC
LB/IK LB/U
LB FUEL LB FUEL
5.23 0.14
4.65 0.11
2.15 0.04
CO
LB/IKHTH-HR
4.248
3.785
1.002
60.00 2.30 2.85 50.40 -0.00 43.00 -0.00 -O.nO
58.00 2.50 2.40 62.00 -0.00 64.20 -0.00 -O.nO
30. 00 2.80 0.90 84.00 -0.00 88. OC -0.00 -0.00
MASS EMI PASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS FMI MASS EMI
N02 C02 N1 NOX CO HC N02 C02 NO
LB/IK L8/1K LB/IK LB/IK L3/HR LB/HR Lfl/HR LB/HR LH/HP
LB FUEL LB FUEL LB FUEL LB FUEL
-0.00 3147.29 7.21 6.15 33.28 0.91 -0.00 20045.09 45. 9,!
-0.00 3148.28 8.16 8.45 34.70 0.82 -C.OO 23501.93 60.93
-0.00 3152.41 9.89 10.36 19.75 0.34 -0.00 28958.03 90. d2
CO THC NO NO Nil
2 2 X
LB/IKdTH-HR Le/IKDTH-HK LB/IKHTM-HR LB/1K«TH-HR L»/ 1 K »TH-HR
2558.730 0.116 5.862 -0.000 5.0'M
2563.194 0.090 6.645 -0.000 6. Hill
2641.915 0.031 B.2R6 -0.000 B.t»\0
-C.OO
-0.00
-0.00
[ 1ASS tMI
NOX
LB/MR
'St. 11
63.09
95. 14
IV-314
-------
DATEI T/ T/Ti
TEST ORGANIZATION! PRATT ( WHITNEY
ENGINE SUPPLIERl PRATT AND WHITNEY
ENGINE DATA
CAL 10 NUMBER: *« ENGINE TYPE AND MODEL: JI3D
RATED THRUST: 21000.
ENGINE TOTAL TINE: -0. HRS
TINE SINCE HOT SECTION OVERHAUL! -0. HRS
TIKE SINCEl
Nl COMPRESSOR OVERHAUL! -0. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
flRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
Nl TURBINE OVERHAUL: -0. HRS
N2 TURBINE OVERHAUL! -0. HRS
SERIAL NUMBER:
FUEL H/C RATIO: 2.000
FINISH
FINISH
87.00
29. 9*
FUEL I JP-4
OPERATIONAL DATA »«»«
INLET AIR TEMPERATURE, DEGREES F: START 85.00
ATMOSPHERIC PRESSURE: START 29.92
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0084
RELATIVE HUMIDITY: 27.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/HIM:
SAMPLE LINE TRANSPORT TIME. SEC: 1.00
NUMBER OF TESTS! 9
COMMENTS:
BURNER 1 BM
CLOCK
TIME
1429.00
1443.00
1443.00
1453.00
1512.00
1518.00
1529.00
1541.00
1551.00
POWER
PERCENT
RATED
T.O.
3
6
8
29
45
55
64
74
83
POWER
PERCENT
RATED
T.O.
3
6
a
29
45
55
64
74
83
POWER
PERCENT
RATED
T.D.
3
6
8
29
45
55
64
74
83
TEST
MODE
I/ 0
21 \
3/ 2
4/ 3
S/ 4
6/ 5
T/ 6
8/ 7
9/ 8
EXHAUST
GAS
TEMP
DEGREES F
585.00
595.00
605.00
655.00
7.25
770.00
825.00
885.00
980.00
MASS EMI
CO
LB/IK
LB FUEL
117.68
84.79
58.80
10.49
3.79
2.29
1.54
1.0)
0.68
CO
POWER ENGINE
THRUST, LBS
OR
SHP
840.00
1350.00
1850.00
6279.00
9597.00
11606.00
13564.00
15550.00
17609. DO
EXHAUST
GAS
PRESSURE
PSIA
15.00
15.19
15.38
17.39
19.36
20.73
22.20
24.12
26.24
MASS EMI
HC
LB/IK
LB FUEL
82.02
34.59
16.40
0.92
0.10
0.27
0.15
0.23
0.16
PERCENT SPEED
RATED RPM
T.O. Nl N2
3 1865.00 5495.00
6 2365.00 6440.00
B 2745.00 7025.00
29 4470.00 8510.00
45 5245.00 9020.00
55 5615.00 9260.00
64 5950.00 9475.00
74 6280.00 9695.00
83 6700.00 10000.00
MEASURED
FUEL
FLOW
LB/HR
1017.00
1266.00
1501.00
3197.00
4559.00
5636.00
6705.00
7924.00
9450.00
CO CO THC NO
GAS GEN
AIR FLOW
LB/SEC
CALC
fit,
COMPRESSOR ENGINF
DISCHA
TEMP
RGE PR
DEGREES F
29.09
40.70
49.26
97.66
125.93
140.66
155.27
170.32
183.25
NO
0.
0.
0.
0.
0.
0.
0.
0.
0.
IWET) 2 IWETI IWETI 2
PPMV IWETI PPMV PPMV I ETI
PERCENT V
867.60 1.28 1055
645.60 1.41 459
455.70 1.48 222
93.50 1.77 14
41.50 2.18 2
27.20 2.37 5
19.70 2.56 3
14.30 2.77 5
.80 1.
.80 1.
.00 4.
.30 28.
.00 0.
.70 0.
.30 0.
.60 0.
10.70 3.13 4.50 0.
MASS EMI MASS EMI MASS EMI
N02 C02 NO
LB/IK LB/1K LB/IK
LB FUEL LB FUEL LB FUEL
0.89 2727.85 0.42
1.14 2909.64 0.22
1.08 3000.36 0.87
1.84 3118.75 5.32
0.44 3131.50 0.0
0.75 3133.40 0.0
0.81 3134.93 0.0
2.02 3135.49 0.0
0.88 3136.22 0.0
CO THC
2
LB/lKfTH-HR LB/1K»TH-MR LB/lKiTH-HR
142.
79.
47.
5.
1.
1.
0.
0.
0.
473
514
705
339
802
111
759
525
366
3302.639 99.298
2728.595 32.434
2434.344 13.310
1587.935 0.468
1487.600 0.050
1521.611 0.133
1549.667 0.073
1597.790 0.118
1683.077 0.088
MASS EMI
NOX
LB/IK
LB FUEL
1.31
1.36
1.95
7.17
0.44
0.75
0.81
2.02
0.88
PMV
90 .00
00 .30
10 .10
90 10.00
0 2.90
0 5.40
0 6.30
0 17.10
0 8.40
MASS EMI MASS
CO
LB/HR
119.68
107.34
88.25
33.52
17.30
12.90
10.29
8.16
6.45
HC
009710
008640
008460
009070
0102BO
011130
012000
012920
014320
NO
X
IKETI
PPMV
5.90
6.30
9.20
38.90
2.90
5.40
6.30
17.10
8.40
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
00
00
00
00
00
00
00
00
00
FSSURE
RATIO
EPR
1.02
1.04
1.05
1.20
1.34
1.44
1.55
1.68
1.84
ALDEHYDES SMOKE
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
-0.
EMI MASS EMI
LB/HR
83.
43.
24.
2.
0.
1.
0.
1.
1.
N3
41
79
62
94
48
55
99
83
55
NO
2
LB/1KKTH-HR LB/ 1K»TH-HR
0.
0.
0.
2.
0.
0.
0.
0.
0.
512
202
705
710
0
0
0
0
0
1.079
1.072
0.877
0.938
0.207
0.362
0.399
1.011
0.472
N02
LB/HR
0.91
1.45
1.62
5.89
1.99
4.21
5.41
16.03
8.31
00 -0
00 -0
00 -0
00 -0
00 -0
00 -0
00 -0
00 -0
00 -0
MASS EMI
C(12
LB/HR
2774.22
3683.60
450.54
9970.64
14276.50
17659.81
21019.68
24845.64
29637.29
NO
X
.00
.00
.00
.00
.00
.00
.00
.00
.00
MASS
NO
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
EMI MASS EMI
NOX
LB/HR LB/HR
0.
0.
1.
17.
0.
0.
0.
0.
0.
43 1.34
27 1.72
30 2.93
02 22.91
0 1.99
0 4.21
0 5.41
0 16.01
0 B.31
LB/IKKTH-HR
1.591
1.275
1.582
3.648
0.207
0.162
0.199
1.031
0.472
IV-315
-------
DATE: 5/29/71
TEST ORGANIZATION: UNITED/EPA
ENGINE SUPPLIER: UNITED AIRLINES
ENGINE DATA »»»««*»»«»»««..
CAL 10 NUMBER: 121 ENGINE TYPE AND MODEL: JT30 -SB
SERIAL NUMBER:
RATED THRUST: 18000.
ENGINE TOTAL TIME: 9199. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 9199. HRS
N2 COMPRESSOR OVERHAUL: 12169. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.920
FINISH
FINISH
66.20
30.35
FUEL: JET - A
OPERATIONAL DATA «»»*««««««««»«««««...*».
INLEI AIR TEMPERATURE, DEGREES F: START 66.00
ATMOSPHERIC PRESSURE: START 29.98
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0105
RELATIVE HUMIDITY: 72.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 160.00, FLOW RATE, LItFBS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 5.00
NUMBER OF TESTS: 4
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES HG
1.50
CLOCK
TIME
1327.00
1335.00
1314.00
1447.00
POWER
PERCENT
RATED
T.O.
51
73
92
5
POWER
PERCENT
RATED
T.O.
51
73
92
5
POWER
PERCENT
RATED
T.O.
51
73
92
5
TEST
MODE
I/ 0
2/ 1
3/ 2
*/ 3
EXHAUST
GAS
TEMP
DEGREES F
721.40
838.40
957.20
555.80
MASS EMI
en
LB/1K
LB FUEL
11.39
6.02
3.88
110.23
CO
POKER ENGINE MEASURED GAS GEN CALC
THRUST, LBS PERCENT SPEED FUEL AIR FLOW F/A
OR RATED RPM FLOW LB/SEC
SHP T.O. Nl N2 LB/HR
9200.00 51 5179.00 8993.00 4857.00 -0.00 -0.000000
13250.00 73 5910.00 9484.00 7145.00 -0.00 -0.000000
16650.00 92 6475.00 98B6.00 9467.00 -0.00 -0.000000
1000.00
EXHAUST
GAS
PRESSURE
PSIA
40.80
47.60
54.70
31.00
MASS EMI
HC
LB/1K
LB FUEL
0.72
0.16
0.11
-0.00
5 1999.00 5810.00 1180.00 -0.00 -0.000000
CO
IWETI
PPMV
130.00
80.00
60.00
900.00
MASS EMI MASS
CO
2
(MET!
PERCENT V
2.28
2.66
3.10
1.55
THC NO
IUFT) IkET)
PPMV PPMV
14.40 45.00
3.60 73.20
5.00 -0.00
-0.00 3.00
EMI MASS EMI MASS CHI MASS
N02 C02 NO
LB/1K LB/1K LB/1K
LB FUEL LB
-0.00 3136
-0.00 3146
-0.00 3149
-0.00 2982
CO
2
LR/lKtTH-HR LB/1KHTH-HR
6.
3.
2.
130.
008
247
206
066
1655.619
1696.467
1790.764
3519.585
NOX CO
NO NO
2 X
IWETI IUET)
PPMV PPMV
COMPRESSOR [NCINF TURBINE
DISCHARGE PRESSURE INLCI
TEMP RATIO TEMP
DEGREES F EPR DEGREES F
-0.00 1.37 -0.00
-0.00 1.61 -0.00
-0.00 I.H4 -0.00
-0.00 -0.00 -0.00
ALDEHYDES SMOKE PARTICULANS
-o.oo 47.00 -o.oo -o.no -o.no
-0.00 74.00
-0.00 -0.00
-0.00 3.50
-o.oo -o.oo -o.no
-0.00 -0.00 -0.00
-0.00 -0.00 -0.00
Ell MASS EMI MASS EMI MUSS FMI MASS EMI '«»SS H>1
HC
LB/IK LB/HR Lfl/HK
N02 CO 2 NO NUX
LB/HP LB/HK Lfi/hP LB/MH
FUEL LB FUEL LB FUEL
.03 6.47
.00 9.05
.49 -0.00
.JO 0.60
THC
LB/ KOTH-HR
0.3R1
0.084
0.063
-0.000
6.76 55.
9.15 43.
-0.00 36.
0.70 I3C.
NO
Lfl/ 1K9IH-HH
3.416
4.H80
-0.000
0.712
27 3.51
03 1.1 t
73 1.05
07 -0.00
NO
2
LB/IKHTH-HR
-0.000
-0.000
-0.000
-n.ooo
-0.00 15231. (,9 31.43 32.02
-0.00 22478.18 64.67 65.37
-0.00 29816.21 -0.00 -0.00
-0.00 3519.58 C.71 0.03
NO
X
LB/1KHTH-HR
3.5A*
4.934
-o.oon
0.831
IV-316
-------
DATE: 6/ »/71
TEST ORGANIZATION: S W R I TWA
ENGINE SUPPLIER: T M A
ENGINE DATA
CAL ID NUMBER! 313
ENGINE TYPE AND MODEL: JT30 -38
SERIAL NUMBER: P64355BB
RATED THRUST: 18000.
ENGINE TOTAL TIME: 4158. MRS
TIME SINCE HOT SECTION OVERHAUL: 4198. HRS
TIME SINCE!
Nl COMPRESSOR OVERHAUL: 4158. HRS
N2 COMPRESSOR OVERHAUL: 4198. HRS
COMBUSTOR CAN REPLACEMENT: 4158. HRS
FIRST STAGE NOIZLE GUIDE VANE OVERHAUL: 4158. HRS
NI TURBINE OVERHAUL: 4158. HRS
N2 TURBINE OVERHAUL: 4158. HRS
FUEL H/C RATIO: 2.020
FINISH
FINISH
67.00
29.05
FUEL: JP-4 TF
OPERATIONAL DATA «»«
INLET AIR TEMPERATURE, DEGREES F: START 68.00
ATMOSPHERIC PRESSURE: START 21.05
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0116
RELATIVE HUMIDITY: 76.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/MIN: 42.
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
N02 DETERMINED BY SUBTRACTION. THIS IS THE FIRST OF THREE TESTS ON THIS ENGINE
THE FUEL USED CONTAINED NO CI-2. HYDROCARBON EMISSIONS FROM THIS ENGINE HERE
ABNORMALLY HIGH DUE TO AN OIL LEAK. NO HYDROCARBON DATA ARE THUS REPORTED FOR
THIS TEST.
ELAPSED
TIMF
0.0
5.00
7.00
11.00
15.00
POWER
PERCENT
RATED
T.O.
50
62
73
85
5
POWER
PERCENT
RATED
T.O.
50
62
73
85
5
POWER
PERCENT
RATED
T.O.
50
62
73
85
5
TEST
MODE
6/ 0
I/ 6
2/ 1
3/ 2
4/ 3
EXHAUST
GAS
TEMP
DEGREES F
716.00
777.00
844.00
439.00
536.00
MASS EMI
CO
LB/IK
LB FUEL
4.17
2.01
0.89
172.72
66.98
CO
POWER
THRUST, LBS
OR
SHP
9000.00
11180.00
13300.00
15420.00
960.00
EXHAUST
GAS
PRESSURE
PSIA
4.60
6.50
8.50
10.90
0.30
MASS EMI
HC
LB/IK
LB FUEL
1.32
1.19
1.10
143.89
75.87
PERCENT
RATED
ENGINE
SPEED
RPM
T.O. Nl N2
50 5380
62 5810
73 62 CO
85 6550
5 -0
CO
IUETI
PPMV
47.00
25.00
12.00
11.00
627.00
MASS EMI MASS
.00 9160.00
.00 9370.00
.00 6930.00
.00 9930.00
.00 5890.00
MEASURED
FUEL
FLOW
LB/HR
5010.00
6310.00
7610.00
9330.00
1000.00
CO THC NO
GAS GEN
AIR FLOW
IB/SEC
CALC
F/A
COMPRESSOR ENGINf
DISCHARGE PRESSURE
TEMP
OFGREES F
126.20
143.60
160.00
174.40
30.80
NG
2 (UETI (UETI 2
(WET) P
PERCENT V
2.24 26
2.48 26
2.69 26
0.01 16
1.68 1240
EMI MASS EMI
N02 C02 NO
LB/IK LB/1K L8/1K
LB FUEL LB FUEL LB FUEL
0.29 3123.
0.40 3126.
0.49 3128.
51. 5B 2467.
0.88 2819.
CO
2
LB/1K«TH-HR LB/IKITH-HR
2.
1.
0.
104.
69.
322
132
508
506
771
1738.505
1764.775
1790.250
1492.750
2937.363
06 4.81
81 5.67
82 6.93
12 2140.67
87 0.53
THC
LB/lKf TH-HR
0.716
0.674
0.631
87.059
79.027
PMV PPM
.00 33.
.00 43.
.00 57.
.00 83.
.00 3.
MASS EMI
NOX
LB/IK
LB FUEL
5.10
6.06
7.42
2142.26
1.40
V IWET)
PPMV
00 2.00
00 3.00
00 4.00
00 2.00
00 5.00
0.011000
0.012200
0.013200
0.014800
0. 009000
NO
X
(WFT)
PPMV
35.00
46.00
61.00
85.00
8.00
-0
-0
-0
-0
-0
.00
.00
.00
.00
.00
RATIO
EPR
1.17
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES SHOKE PARTICULATES
-0
-0
-0
-0
-0
MASS EMI MASS [Ml MASS EMI
CO
LB/HR
20.89
12.66
6.76
HC
LB/HR
6.62
7.54
8.39
N02
LB/HR
1.46
2.50
3.70
1611.48 1342.45 481.26
66.98
NO
75.87
NO
2
LB/1KHTH-HR LB/lK*Th-HR
2.
3.
3.
1295.
0.
677
199
966
232
548
0.162
0.221
0.278
31.210
0.914
0.88
.00 -0
.00 -0
.00 -0
.00 -0
.00 -0
MASS EfM
CO 2
LB/HK
15646.54
19730.18
23810.33
23018.21
2SI9.87
NO
X
.00
.00
.00
.00
.00
MASS EHI
NO
LB/HK
24.10
35.76
52.74
19972.47
0.53
-0.00
-0.00
-0.00
-0.00
-0.00
1ASS EMI
NOX
LB/HR
25.56
38.26
56.44
20453.74
1.40
IB/IK»TH-HR
2.840
3.422
4.244
1326.442
1.462
IV-317
-------
DATE: 8/ 4/71
TEST ORGANIZATION: S W R
ENGINE SUPPLIER: T H A
ENGINE DATA
CAL ID NUMBER: 314
ENGINE TYPE AND MODEL: JT1D -38
SERIAL NUMBER:
RATED THRUST: 18000.
ENGINE TOTAL TIME: MSB. MRS
TIME SINCE HOT SECTION OVERHAUL: 4158. MRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 4198. MRS
N2 COMPRESSOR OVERHAUL: 4158. HRS
COMBUSTOR CAN REPLACEMENT: 4158. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 4158. HRS
NI TURBINE OVERHAUL: 4i5e. HRS
N2 TURBINE OVERHAUL: 4158. HRS
FUEL H/C RATIO: 2.020
FINISH
FINISH
66.00
21.04
FUEL: JP-4 IF
OPERATIONAL DATA »««»...
INLET AIR TEMPERATURE, DEGREES F: START 66.00
ATMOSPHERIC PRESSURE: START 21.04
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0124
RELATIVE HUMIDITY: si.oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/MI*: 42.
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS: 5
COMMENTS:
N02 DETERMINED BY SUBTRACTION. THIS IS THE SECOND OF THREE TESTS ON 1HIS
FNGINE. THE FUEL USED CONTAINED 0.11 BY VOLUME Cl-2. HYDROCARBON DATA ARE 'JOT
REPORTED BECAUSE OF AN OIL LEAK.
ELAPSED
TIME
0.0
6.00
10.00
13.00
16.00
POWER
PERCENT
RATED
T.O.
50
62
74
86
5
POWER
PERCENT
RATED
1.0.
50
62
74
86
5
POWER
PERCENT
RATED
T.O.
50
62
74
86
5
TEST
NUDE
6/ 0
I/ 6
11 1
3/ 2
4/ 3
EXHAUST
GAS
TEMP
DEGREES F
725.00
775.00
844.00
937.00
540.00
MASS EMI
CO
LB/1K
L8 FUEL
5.91
2.73
1.19
0.73
77.81
CO
POWER ENGINE
THRUST, LBS
OH
SHP
9080.00
11200.00
13420.00
15500.00
980.00
EXHAUST
GAS
PRESSURE
PSIA
4.80
6.50
8.50
10.90
0.30
MASS EMI
HC
IB/IK
LB FUEL
-0.00
-0.00
1.19
-0.00
-0.00
PERCENT SPEED
RATED RPM
T.O. Nl N2
50 5390. OC 9020.00
62 5830.00 9370.00
74 6210.00 9630.00
86 6660.00 9930.00
5 2020.00 5880.00
MEASURED GAS GEN
FUEL AIR FLOW
FLOW LB/StC
LB/HR
5100.00 127.30
6300.00 143.70
7660.00 161.00
9340.00 175.40
1030.00 11.80
CO CO THC NO NO
IWETI 2 (W
ETI (WEfl 2
PPMV IHET) PPMV PPMV (WETI
PERCENT V
66.00 2.22 -0
34.00 2.48 -0
16.00 2.68 28
11.00 2.99 -0
674.00 1.66 -0
MASS hHI MASS FM 1 MASS EMI
N02 C02 NO
LB/1K LB/1K LB/1K
LB FUEL LB FUEL LB FUEL
0.29 3125.95 4. 56
0.26 3128.95 5.54
0.37 3128.10 6.71
0.33 3132.09 8.43
0.76 3010.99 0.76
CO THC
2
LB/1K»TH-HR LB/IK«TH-HR L8/1KHTH-HR
3.
1.
0.
0.
91.
320
536
678
442
777
1754.644 -0.000
1760.035 -0.000
1785.490 0.680
1887.335 -0.000
1164.609 -0.000
PPHV
.00 31.00 2.0C
.00 42.00 2.00
.00 55.00 3.00
.00 77.00 3.0'J
.00 4.00 4. CO
CALC
F/A
0.011100
0.012200
0.013200
0.014800
0.009000
NO
X
IUETI
PPMV
33.00
44.00
58.00
80.00
8.00
COMPRESSOR ONG INL
DISCHARGE PRESSUuE
TEMP RATIC
nfiCRFES F EPR
-0.00 1.37
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-o.oo -o.oo
ALOEHYDES SMOKF
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-o.oo -o.no
-0.00 -0.00
MASS EMI MASS FMI MASS EMI MASS EMI MASS EMI MASS
NOX CO
LB/1K Lfl/HR
LB FUEL
4.85 10.15
5.80 17.20
7.08 9.10
fl.76 6.85
1.52 80.14
NO
HC
LB/HR
-0.00
-0.00
9.13
-0.00
-0.00
NO
2
LB/1KITH-HK LR/1KHTH-HK
2.561
3. 116
3.831
5. CHI
0.797
0.165
0. 14ti
0.200
0.19P
C.797
NII2 C02 Nil
TURBINE
INLET
TFMP
DCGREtS F
-0.00
-0.00
-0.00
-0.00
-C.OO
PARIICULATES
-0.00
-n.oo
-0.00
-c.on
-C.OO
FMI MASS EMI
NUX
LB/HR LB/HR LB/HR LP./hR
1.50 15932.16 23.
1.66 19712. 39 34.
2.80 23961.28 SI.
3.07 29253.70 79.
0.7.3 3101.32 0.
NO
X
L6/I KflTH-HH
2.727
1.764
4.040
5.279
1.594
'it. 24.76
90 16.56
41 54.21
76 81.82
7fl l.5t>
IV-318
-------
OATEl 8/ 4/71
TEST ORGANIZATION! S H R I TMA
ENGINE SUPPLIERl T H A
ENGINE DAT*
C»L ID NUMBER: 315
ENGINE TVPE AND MODEL: JT30 -3B
SERIAL NUMBER: P643558B
RATED THRUST: 18000.
ENGINE TOTAL T1ME1 4158. HRS
TINE SINCE HOT SECTION OVERHAUL: 4158. HRS
TINE SINCEI
Nl COMPRESSOR OVERHAUL: 4158. HRS
N2 COMPRESSOR OVERHAUL: 4158. HRS
COMBUSTOR CAN REPLACEMENT: 4158. HRS
FIRST STAGE NOZUE GUIDE VANE OVERHAUL: 4158. HRS
Nl TURBINE OVERHAUL: 4158. HRS
N2 TURBINE OVERHAUL I 4158. HRS
FUEL H/C RATIO: 2.020
FINISH
FINISH
66.00
24.04
FUEL: JP-4 TF
OPERATIONAL DATA »
INLET AIR TEMPERATURE. DEGREES F: START 66.00
ATMOSPHERIC PRESSURE: START 29.04
INLET AIR HUMIDITY, L8S H2D/LB AIR: 0.0124
RELATIVE HUMIDITY: 81.00 PERCENT
SAMPLE LINEl TEMPERATURE. DEGREES C: 150.00, FLOW RATE, LITERS/MIN: 42.
SAMPLE LINE TRANSPORT TINE, SEC: 1.00
NUMBER OF TESTS: 5
COMMENTS!
N02 DETERMINED BY SUBTRACTION. THIS TEST IS THE LAST OF THREE TESTS RUN ON
THIS ENGINE. THE FUEL USED CONTAINED 0.0125* CI-2 BY VOLUME. HYDROCARBON DATA
ARE NOT REPORTED BECAUSE OF AN OIL LEAK.
ELAPSED
TIME
0.0
5.00
9.00
11.10
13.00
TEST
NODE
6/ 0
I/ 6
2/ 1
3/ 2
4/ 3
POHER
THRUST, LBS PERCENT
OR RATED
SHP
9000.00
11250.00
13250.00
15460.00
980.00
T.O.
50
62
73
85
5
ENGINE
SPEED
RPH
Nl
5350.00
5830.00
6200.00
6660.00
2015.00
N2
9020.00
9460.00
9630.00
9950.00
5910.00
MEASURFO
FUEL
FLOW
LB/HR
5120.00
6320.00
7610.00
9360.00
1000.00
GAS GEN
AIR FLOW
LB/SEC
126.30
143.70
160.00
175.40
31.80
CALC COMPRESSOR
F/A DISCHARGE
TEMP
0.011300
0.012200
0.013200
0.014800
0.006700
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
1.37
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
;G69
POKER
PERCENT
RATED
T.O.
50
62
73
85
5
EXHAUST
GAS
TEMP
DEGREES F
714.00
777.00
844.00
939.00
550.00
EXHAUST
GAS
PRESSURE
PSIA
4.DO
6.50
8.50
11.00
0.30
CO
IUEII
PPMV
72.00
53.00
26.00
22.00
675.00
CO
2
(HEM
PERCENT V
2.26
2.47
2.70
3.02
1.62
THC
IMETI
PPMV
-0.00
-0.00
-0.00
-0.00
-0.00
NO
(WETI
PPMV
29.00
45.00
59.00
83.00
4.00
NO
2
IHETI
PPMV
1.00
2.00
3.00
3.00
5.00
NO
X
IHETI
PPHV
30.00
47.00
62.00
66.00
9.00
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POUER
PERCENT
RATED
T.O.
50
62
73
85
5
POKER
PERCENT
RATED
T.O.
50
62
73
85
5
MASS EMI
CO
LB/1K
LB FUEL
6.33
4.2T
1.92
1.45
79.77
MASS EMI
HC
LB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
N02
IS/ IK
LB FUEL
0.14
0.26
0.36
0.33
0.97
MASS EMI
C02
LB/IK
LB FUEL
3123.29
3126.53
3130.23
3130.96
3007.91
MASS EMI
NO
LR/1K
LB FUEL
4.19
5.95
7.15
9.00
0.78
MASS FMI
NOX
LB/IK
IB FUEL
4.33
6.22
7.51
9.32
1.75
MASS EMI
CO
Lfl/HR
32.42
26.98
14.60
13.51
79.77
MASS EMI
HC
Lfl/MR
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EM
NO 2
LB/HR
0.74
1.67
2.77
3.04
0.97
CO
LB/IKITH-HR
3.603
2.399
1.102
0.879
81.394
LB/1K«TH-HR
1776.805
1756.416
1797.813
1895.588
3069.296
THC
LB/IK»TH-HR
-0.000
-0.000
-0.000
-0.000
-0.000
NO
LB/1KHTH-HR
2.363
3.345
4.107
5.446
0.792
LB/IKHTH-HR
0.08?
0.149
0.209
0.197
0.990
MASS EMI
C02
LB/MR
15991.25
19759.68
23821.02
2930-1.79
3007.91
NO
X
LB/IKHTH-HR
2.4S6
3.494
4.316
5.643
1.783
MASS EMI
NO
LB/HR
21.45
37.63
54.42
84.20
0.7fl
MASS FMI
NOX
LB/HR
22.19
39.31
57. 18
87.24
1.75
IV-319
-------
DATE! 7/29/71
TEST ORGANIZATION: U.S. BUREAU OF MINES
ENGINE SUPPLIER: PRATT AND WHITNEY
ENGINE DATA
CAL ID NUMBER: 338
ENGINE TYPE AND MODEL: JT30 -3B
SERIAL NUMBER: 6456*3
RATED THRUST: 18000.
ENGINE TOTAL TIME: 11171. HRS
TIME SINCE HOT SECTION OVERHAUL: 161. HRS
TIME SINCEl
Nl COMPRESSOR OVERHAUL: 11171. HRS
N2 COMPRESSOR OVERHAUL: 5192. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 5192. HRS
Nl TURBINE OVERHAUL: 1317<>. HRS
N2 TURBINE OVERHAUL: 11176. HRS
FUEL H/C RATIO: 1.920
FUELl JET - A
OPERATIONAL DATA «««»«««»««
INLET AIR TEMPERATUREt DEGREES F: START 67.00 FINISH 63.00
ATMOSPHERIC PRESSURE: START 29.11 FINISH 29.11
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0120
RELATIVE HUMIDITY: 78.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 137.00, FLOW RATE, LITtRS/NIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.99
NUMBER OF TESTS: 7
COMMENTS:
H/C CAL EATIMATED
SAMPLE LINE TEMP. AVERAGED
PROBE LOCATED 30" FROM TAILPIPE
LOST SAMPLE FLOW ON LAST RUN
CLOCK
IIME
910.00
1015.00
1020.00
1030.00
1045.00
1050.00
1055.00
POWER
PERCENT
RATED
T.O.
3
4
62
5
60
74
88
POWER
PERCENT
RATED
T.O.
3
4
62
5
60
74
88
POWER
PERCENT
RATED
T.O.
,
4
62
5
60
74
88
TEST POWER ENGINE MEASURED GAS GEN CALC COMPRESSOR ENGINE TURBINE
MODE THRUST, LBS PERCENT SPEED FUEL AIR FLOW F/A DISCHARGE PRESSURE INLET
OR RATED RPM FLOW LB/SEC TEMP RATIO TEMP
SHP T.O. Nl N2 LB/HR DEGREES F EPR DEGREES F
4/ 0 710.00 3 1840.00 5560.00 1060.00 -0.00 -0.000000 -0.00 .02 -0.00
4/ 4 850.00 4 1930.00 5555.00 1060.00 -0.00 -0.000000 -0.00 .02 -0.00
5/ 4 11310.00 62 5760.00 9280.00 6048.00 160.00 -0.000000 -0.00 .5C -0.00
4/ 5 950.00 5 1960.00 5650.00 960.00 -0.00 -0.000000 -0.00 .02 -0.00
I/ 4 10900.00 60 5700.00 9250.00 5770.00 154.00 -0.000000 -0.00 .47 -0.00
2/ 1 13410.00 74 6150.00 9560.00 7210.00 175.00 -0.000000 -0.00 .62 -0.00
3/ 2 16000.00 88 6670.00 9970.00 9100.00 197.00 -0.000000 -0.00 1.87 -0.00
EXHAUST EXHAUST CO CO THC ND NU NO ALDEHYDES SHDKE PART 1CUL ATES
GAS GAS (WETI 2
-------
DATE: 7/29/71
TEST ORGANIZATION! U.S. BUREAU OF MINES
ENGINE SUPPLIER! AMERICAN AIRLINES
ENGINE DATA
CAL ID NUMBER! 342
ENGINE TYPE AND MODEL: JT3D -3B
SERIAL NUMBER: 667944
RATED THRUST: 18000.
ENGINE TOTAL TIME! 9380. MRS
TIME SINCE HOT SECTION OVERHAUL: 2931. HRS
TIME SINCEl
Nl COMPRESSOR OVERHAUL: 9)80. HRS
N2 COMPRESSOR OVERHAUL: 9380. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 2931. HRS
Nl TURBINE OVERHAUL: 9380. HRS
N2 TURBINE OVERHAUL! 9380. HRS
FUEL H/C RATIO: 1.920
FINISH
FINISH
74.00
29.30
FUEL: JET - A
OPERATIONAL DATA «»««»
INLET AIR TEMPERATURE, DEGREES F: START 74.00
ATMOSPHERIC PRESSURE: START 29.30
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.0140
RELATIVE HUMIDITY: 78.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES C: 137.00, FLOW RATE, LITERS/HI*:
SAMPLE LINE TRANSPORT TIME, SEC: 0.99
NUMBER OF TESTS! 1
COMMENTS:
H/C CAL ESTIMATED
SAMPLE LINE TEMP. AVERAGED
DATA FOR UNTRIMMEO IDLE ONLY.
ENGINE SHUTDOWN ( REMOVED FROM TEST CELL DUE TO OIL LEAK.
PROBE 10- DOWNSTREAM
POKER EXHAUST
PERCENT GAS ....
RATED TEMP
T.O. DEGREES F
3 587.00
POWER
THRUST, LBS
OR
SHP
600.00
EXHAUST
GAS .
PRESSURE
PSIA
PERCENT
RATED
T.O.
3
CO
(WET)
PPMV
ENGINE
SPEED
RPM
Nl N2
1720.00 5140.00
CO 1
2 . ...II
IWETI 1
PERCENT V
FUFL
FLOW
LB/MR
AIR FLOW
LB/StC
-0.00 -0.000000
14.63
THC
(MET)
PPHV
0.98 2959.00
NO
IWET)
PPMV
COMPRESSOR
DISCHARGE
TENP
DEGREES F
NO
. 2
IWETI
PPMV
4.00
PRESSURE
RATIO
EPR
IWETI
PPMV
TURBINE
INLET
TEMP
DEGREES f
-0.00
ALDEHYDES SMOKE PARTICULATES
PERCENT CO
RATED LB/1K
T.O. LB FUEL
MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS FMI MASS EMI MASS EMI MISS EMI
HC
LB/1K
LB FUEL
N02
Ift/lK
LB FUEL
C02
LB/1K
LB FUEL
0.95 2233.21
NO
IB/IK
LB FUEL
NOX
LB/1K
LB FUEL
CO
LB/HR
HC
LB/HR
NO 2
LB/HR
CO?
LB/HR
NO
LR/HR
HOI
LO/HR
POWER CO
PERCENT
RATED LB/1KITM-HR
T.O.
3 263.476
CO
2
LB/IKITH-HR
3722.017
THC
LB/IKITH-HR
NO
LR/IK«TH-HR
NO
2
LB/1K«TH-HR
I.5BH
NO
X
L6/IK«TH-HR
IV-321
-------
DATE: 8/18/71
IESI ORGANIZATION! PR»IT L WHITNEY
ENCINE SUPPLIER! PRATT »NO NHITNEr
ENGINE DATA »««».».«
CAL 10 NUMBER: 356 ENGINE TYPE AND MODEL: JT3D -38
RATED THRUST: 18000.
ENGINE TOTAL TINE: -0. HRS
TIME SINCE HOT SECTION OVERHAUL! -0. MRS
TIME SINCE!
Nl COMPRESSOR OVERHAUL: -0. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NO22LE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
N2 TURBINE OVERHAUL: -0. HRS
SERIAL NUMBER:
FUEL H/C RATIO: 2.000
FINISH
FINISH
83.00
29.05
FUEL: jp-4
OPERATIONAL DATA »»«»»««»
INLET AIR TEMPERATURE, DEGREES f: START 86.00
ATMOSPHERIC PRESSURE: START 29.66
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0115
RELATIVE HUMIDITY! -0.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOM RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER OF TESTS! 6
COMMENTS:
CLOCK
TIME
1751.00
1843.00
1850.00
1908.00
1918.00
1923.00
POWER
PERCENT
RATED
T.D.
27
49
59
69
HO
91
POWER
PERCENT
RATED
T.D.
27
49
59
69
80
91
POWER
PERCENT
RATED
T.O.
27
49
59
69
80
91
TEST
MODE
I/ 0
3/ I
4/ 3
5/ 4
6/ 5
7/ 6
EXHAUST
GAS
TEMP
DEGREES F
640.00
725.00
760.00
810.00
870.00
965.00
MASS EMI
CO
LB/IK
LB FUEL
12.75
3.72
2.90
1.72
1.12
0.75
CO
POWER ENGINE
THRUST, LBS
OR
SHP
5000.00
8850.00
10700.00
12600.00
14500.00
16400.00
EXHAUST
GAS
PRESSURE
PSIA
16.91
19.36
20.72
22.29
24.00
26.24
MASS EMI
HC
LB/IK
LB FUEL
0.53
0.35
0.41
0.36
0.33
0.29
PERCENT SPEED
RATED RPM
T.Q. Nl N2
27 4210.00 8315.00
49 5240.00 9015.00
59 5610.00 9240.00
69 5950.00 9460.00
80 6260.00 9680.00
91 6690.00 9975.00
CO CO
MEASURED
THC
IWETI 2 (WET)
PPMV IWETI
PERCENT V
110.60 1.72
48.50 2.60
32.40 2.23
21.60 2.51
15.60 2.79
11.70 3.12
MASS EMI MASS EMI MASS EMI
NQ2 C02 ND
LB/IK LB/IK LB/IK
LB FUEL LB FUEL LB FUEL
0.57 3116.26 4.26
0.98 3130.94 5.15
1.01 3132.07 7.68
0.63 3134.05 8.67
0.75 3135.09 10.36
0.49 3135.77 12.78
CO THC
2
PPMV
8.00
8.00
8.00
8.00
8.00
6.00
FUEL
FLOW
LB/HR
2791.00
4634.00
5559.00
6667.00
7645.00
9408.00
NO
GAS GEN
AIR FLOW
LB/SEC
89.11
125.14
141.44
156.93
170.22
183.99
NC
0.
0.
C.
0.
0.
0.
IWET) 2
PPMV IWETI
22.
40.
52.
66.
88.
121.
MASS EMI
NOX
LB/IK
PPMV
60 .00
90 .80
30 .90
40 .80
20 .40
60 .70
MASS EMI MASS
CO
LB/HR
HC
LB/
CALC
F/A
008700
010290
C10900
011600
012800
014200
NU
X
IWET)
PPMV
25.60
48.70
59.20
71.20
94.60
126.30
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
RATIO
EPR
l.lo
1.34
1.44
1.55
1.66
1.84
ALDEHYDES SMCKE
-0.00 -0.00
-0.00 -0
-C.OO -0
-0.00 -0
-0.00 -0
-0.00 -0
EMI MASS EMI MASS EMI
HR
N02 CO 2
L8/HR LB/HR
.00
.00
.00
.00
.00
MASS
NO
L(V
TURBINE
INLET
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULARS
-0.00
-0.00
-0.00
-0.00
-0.00
-P. 00
EM| MASS EMI
NOX
HR LB/HR
LB FUEL
LB/1KITH-HR LB/1KITH-HR LB/1KITH-HR
7.
1.
1.
119
946
505
0.908
0.
0.
604
429
1739.495 0.295
1639.410 0.104
1627.213 0.213
1658.310 0.193
1696.193 0.177
1798.659 0.166
4.85
6.13
8.69
9.29
11.11
13.27
NO
15.59
17.23
16.10
11.44
6.75
7.04
1.
I.
2.
2.
2.
2.
47
63
28
43
57
76
NO -
2
LB/1K«TH-HR LB/1KHTH-HR
2.
2.
3.
4.
5.
7.
389
696
990
566
606
329
0.317
0.514
0.526
0.332
0.407
0.263
1.59 8697.47
4.55 14503.78
5.63 17411.18
4.18 20894.70
5.90 24594.80
4. (,5 29501.26
NO
X
LB/lKfTH-HR
2.707
3.210
4.516
4.918
6.012
7.613
11.
23.
42.
57.
81.
120.
95 13.53
86 26.41
69 46.32
7fl 61.96
28 87.18
20 124.85
IV-322
-------
DATE! T/ZO/Tl
TEST ORGANIZATION: UNITED/EPA
ENGINE SUPPLIER! UNITED AIRLINES
ENGINE DATA
CAL ID NUMBER: 410
ENGINE TYPE AND MODEL: JT3D-7
SERIAL NUMBER:
RATED THRUST: 19000.
ENGINE TOTAL TINEl 6Z66. HRS
TINE SINCE HOT SECTION OVERHAUL: 6266. HRS
TINE SINCE)
NI COMPRESSOR OVERHAUL: -o. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
Nl TURBINE OVERHAUL: -0. HRS
N2 TURBINE OVERHAUL I -0. HRS
FUEL H/C RATIO: 1.420
FUEL: JET - A
OPERATIONAL DATA ««»«*«»«*
INLET AIR TEMPERATURE, DEGREES F: START 57.74 FINISH 57.20
ATMOSPHERIC PRESSURE: START 29.S3 FINISH 29.61
INLET AIR HUMIDITY. LBS H20/LB AIR: D.0090
RELATIVE HUNIOITY: 86.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 160.00, FLOW RATE. LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 5.00
NUMBER OF TESTS: 3
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES HG.
PROBE LOCATED 15.25 IN. FROM TAILPIPE.
PRE-REPAIR ENGINE.
iu37
i
5
!
5
CLOCK
TINE
2144.00
2151.00
2154.00
POWER
PERCENT
RATED
T.O.
49
73
91
POWER
PERCENT
RATED
T.O.
49
7)
91
POWER
PERCENT
RATED
T.O.
49
73
91
TEST POWER ENGINE
NODE THRUST, LBS PERCENT SPEED
OR RATED RPM
SHP
I/ 0 94)2.00
11 1 13869.00
)/ 2 11441.00
EXHAUST EXHAUST
GAS ... GAS..
TEMP PRESSURE
DEGREES F PSIA
726.60 40.30
631.20 47.10
923.00 53.90
MASS EMI NASS EMI
CO HC
LB/IK LB/IK
LB FUEL LB FUEL
9.96 3.94
5.00 1.11
3.76 0.75
CO
T.O. Nl N2
49 5091.00 8951.00
73 5767.00 9459.00
91 6267.00 9802.00
MEASURED GAS GEN
FUEL AIR FLOW
FLOW LB/SEC
LB/HR
5079.00 -0.00
7474.00 -0.00
9719.00 -0.00
CO CO THC NO NO
IWETI 2 IWETI IWETI 2
PPMV IWETI P
PERCENT V
100.00 2.00 69
70.00 2.60 27
60.00 3.20 21
MASS EHI NASS EMI MASS EMI
N02 C02 NO
LB/IK LB/IK LB/IK
LB FUEL LB FUEL LB FUEL
-0.00 3129.44 5.89
-0.00 3144.99 8.45
-0.00 3147.92 10.90
CO THC
2
LB/lKfTH-HR LB/1KITH-HR LB/1KITH-HR
5.36)
2.693
2.093
1665.162 2.119
1692.395 0.595
1754.179 0.420
PMV PPMV (WETI
PPMV
.00 36.00 -0.00
.00 72.00 -0.00
.00 106.00 -0.00
CALC COMPRESSOR ENGINE
F/A DISCHARGE PRESSURE
TEMP RATIO
DEGREES F EPR
-0.000000 -0
-0.000000 -0
-0.000000 -0
.00 1.36
.00 1.60
.00 1.93
NO ALOEHVDES SMOKE
X
(WETI
PPMV
40.00 -0
76.00 -0
112.00 -0
MASS EHI MASS EMI MASS EMI NASS EHI
NOX co
LB/IK LB/HR
LB FUEL
6.54 50.56
6.92 37.40
11.52 36.51
NO
HC N02
LB/HR LB/HR
19.99 -0.00
B.26 -0.00
7.32 -0.00
NO
2
.00 -0.00
.00 -0.00
.00 -0.00
MASS EM] MASS
CO? NO
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
PARTICULARS
-0.00
-0.00
-0.00
EMI MASS FMI
NOX
LB/HR LB/HR LB/HR
15894. 15 21.
23505.67 63.
30594. 6
-------
OATE1 7/26/71
TEST ORGANIZATION! UNITED/EPA
ENGINE SUPPLIER: UNITED AIRLINES
ENGINE DATA
CAL 10 NUMBER: 139
ENGINE TYPE AND MODEL: JT4A-9
SERIAL NUMBER:
611870
RATED THRUST: 16600.
ENGINE TOTAL TINE: 17591. HRS
TIME SINCE HOT SECTION OVERHAUL: 17581. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: '0. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL M/C RATIO: 1.920
FUEL: JET - A
OPERATIONAL DATA «*»»««.....«..»...........*.<
INLET AIR TEMPERATURE, DEGREES f. START 51.00 FINISH 57.20
ATMOSPHERIC PRESSURE: START 2V.V* FINISH 29.96
INLET AIR HUMIDITYi LBS H20/LB AIR: 0.0090
RELATIVE HUMIDITY: 94.00 PERCENT
SAMPLE LINE: TEMPERATUREi DEGREES C: 160.00, FLON RATE, LITERS/HIM
SAMPLE LINE TRANSPORT TIME, SEC: 5.00
NUMBER OF TESTS: }
COMMENTS:
EXHAUST GAS TEMPERATURE IN DEGREES C
EXHAUST GAS PRESSURE IN INCHES HG.
EXTERNAL OIL LEAK
JI3C-7 PROBE USED
CLOCK
TIME
2156.00
2138.00
2201.00
POWER
PERCENT
RATED
T.O.
64
70
88
POWER
PF.RCENT
RATED
T.O.
64
TO
as
POKER
PERCENT
RATED
r.o.
64
70
86
TEST
MODE
I/ 0
2/ 1
3/ 2
EXHAUST
GAS
TEMP
DEGREES F
438.00
462.00
547.00
MASS EMI
CO
L8/1K
LB FUEL
4.1J
4.95
5.96
POWER
THRUST, LBS PERCENT
OR RATED
SHP T.O.
10855.00 64
11872.00 70
14938.00 66
EXHAUST
GAS
PRESSURE
PSIA
61.60
64.80
74.50
MASS EMI
HC
LB/1K
LB FUEL
0.10
0.10
0.11
EN
S
Nl
5605. OC
5754.00
6252.00
CINE
PEED
RPM
N2
8308.00
8656.00
MEASURED
FUEL
FLON
LB/HR
8450.00
9292.00
12206.00
GAS r,EN
AIR FLOM
LB/SEC
-0.00
-0.00
-0.00
CO CO THC NO NO
INETI 2 IUETI (NFTI 2
PPMV INET) PPMV PPMV INET)
PERCENT V PPMV
60.
60.
70.
MASS EMI
NO 2
LB/1K
LB FUEL
-0.00
-0.00
-0.00
00
00
00
MASS EMI
C02
LB/1K
LB FUEL
3149.10
3147.64
3146.22
2.90
2.43
2.35
MASS EMI
NO
LB/IK
LB FUEL
10.33
8.40
7.98
CO CO THC
2
LB/IKHTH-HR LB/1K»TH-HR LR/1KITH-HR
3.
3.
4.
228
8T2
874
2451.393
2463.761
2570.806
0.079
0.078
0.090
2.55 91.
2.10 62.
2.25 57.
MASS EMI
N0>
LB/IK
LB FUEL
10.90
9.34
8.40
00 -0.00
00 -0.00
oo -o.oo
CALC
F/A
-0.000000
-0.000000
-0.000000
NO
X
INFT)
PPMV
96.00
69.00
60.00
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIC
DEGREES F EPR
-0.00 2.06
-0.00 2.17
-0.00 2.49
TURBINE
INLET
TFMP
DEGREES F
-0.00
-0.00
-0.00
ALDEHYDES SMOKE PART ICULATES
-0.
-0.
-0.
MASS EMI MASS EMI MASS EMI
CO HC NQ2
LB/HR LB/HR LB/HR
35.04
45.97
72.80
0.85
0.92
1.34
NO NO
2
LB/1KSTH-HR LB/1K»TH-HR
8.
6.
6.
042
572
519
-o.ooo
-0.000
-0.000
-0.00
-0.00
-0.00
00 -0.00
00 -0.00
00 -0.00
MASS FN1 MASS EMI
C02 NO
LB/HR LP/HR
26609.87 07.21
29249.77 78.02
38402.72 97.38
-0.00
-0.00
-0.00
(ASS EMI
NOX
LB/HR
92.09
66.83
102.50
NO
X
LB/ 1KHTH-HR
8.483
7.313
6.862
IV-324
-------
DATE: mini
TEST ORGANIZATION! UNITEO/EPA
ENGINE SUPPLIER! UNITED AIRLINES
ENGINE DATA
CAL 10 NUMBER) 1*0 ENGINE TYPE AND MODEL: JT4A-9
RATED THRUST: 16800.
ENGINE TOTAL TIME: 16791. MRS
TIME SINCE HOT SECTION OVERHAUL: 16751. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: -0. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOIILE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
N2 TURBINE OVERHAUL: -0. HRS
SERIAL NUMBER:
FUEL H/C RATIO: 1.120
FUEL: JET - A
OPERATIONAL DATA »»»»«««»««»»»
INLET AIR TEMPERATURE, DEGREES F: START 57.20 FINISH 55.40
ATMOSPHERIC PRESSURE: START 24.97 FINISH 29.96
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.0083
RELATIVE HUMIDITY: 80.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 160.00, FLOW RATE, LITERS/HIM:
SAMPLE LINE TRANSPORT TIME, SEC: 5.00
NUMBER OF TESTS: 3
COMMENTS:
EXHAUST GAS TEMPERATURE IN DEGREES C
EXHAUST GAS PRESSURE IN INCHES HG
JT3C-7 PROBE USED
CLOCK
TIME
1216.00
1222.00
1228.00
TEST
NODE
I/ 0
2/ I
3/ 2
POWER
THRUST, LBS PERCENT
OR RATED
SHP T.O.
10842.00 64
11885.00 70
14757.00 87
ENGINE
SPEED
Off
Nl N2
MEASURED
FUEL
FLOM
LB/HR
GAS GEN
AIR FLOW
LB/SEC
CALC
F/A
5574.00 8308.00 8617.00
5728.00 8421.00 9518.00
6195.00 8763.00 12267.00
-0.00 -0.000000
-0.00 -0.000000
-0.00 -0.000000
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
F.NGINF
PRESSURE
H4T10
EPR
2.05
2.16
2.47
TUKBINE
INLE1
TEMP
DEGREES F
-0.00
-0.00
-0.00
POWER EXHAUST
PERCENT GAS
RATED TFMP
T.O. DEGREES F
64
70
87
440.00
463.00
546.00
EXHAUST
GAS..
PRESSURE
PSIA
61.30
64.70
73.70
CO
I MET I
PPMV
45.00
55.00
55.00
CO
2
IWET)
PERCENT
2.30
2.45
2.75
THC
(MET)
PPMV
1.80
1.50
1.50
NO
LHETI
PPMV
61.00
68.00
94.40
NO
2
(MET)
PPMV
-0.00
-0.00
-0.00
ALDEHYDES SMOKE PART ICULATES
I MET I
PPMV
64.00
72.00
102.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POMER
PERCENT
RATED
T.O.
64
70
87
MASS EMI
CO
LB/1K
LB FUEL
1.92
4.50
4.01
MASS EMI
HC
LB/IK
LB FUEL
0.09
0.07
0.06
MASS EMI
N02
LB/IK
LB FUEL
-0.00
-0.00
-0.00
MASS EMI
C02
LB/IK
LB FUEL
3149.48
3148.63
3149.42
MASS EMI
NO
LB/IK
LB FUEL
8.7)
9.14
11.30
MASS EMI
NOX
LB/IK
LB FUEL
9. If,
9.67
12.21
MASS EMI
CO
LO/HR
33.79
42.82
49.18
MASS EMI
HC
LB/HR
0.77
0.67
0.77
MASS EMI
N02
LB/HR
-0.00
-0.00
-0.00
MASS F.MI
C(12
Lfl/HR
27119.09
29968.63
38631.90
MASS EHI
NO
LB/HP
75.25
86.95
138.64
MASS Ell
NOX
LB/HR
78.95
92.07
149.80
POMER
PERCENT
RATED
T.O.
64
70
87
CO
LB/IKITH-HR
3.117
3.603
1.332
LB/1K(TH-HR
2503.144
2521.551
2618.005
THC
LB/IKITH-HR
0.071
0.056
0.052
NO
LB/IK«TH-HK
6.940
7.316
9.195
L8/1KKTH-HR
-0.000
-0.000
-0.000
LB/lKtlH-HR
7.211
7.747
10.101
IV-325
-------
DATE: 6/ 3/71
TEST ORGANIZATION! U.S. BUREAU OF MINES
ENGINE SUPPLIER! AMERICAN AIRLINES
ENGINE DATA
CAl ID NUMBERI 3*3
ENGINE TVPE AND MODEL: JT8D-1
SERIAL NUMBER: 653435
RATED THRUST: 14000.
ENGINE TOTAL TIME: 11614. MRS
TIME SINCE HOT SECTION OVERHAUL: T27T. MRS
TINE SINCEI
Nl COMPRESSOR OVERHAUL: 11614. HAS
N2 COMPRESSOR OVERHAUL: 11614. HRS
COMBUSTOR CAN REPLACEMENT: 7277. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 2766. HRS
NI TURBINE OVERHAUL: 2768. HRS
N2 TURBINE OVERHAUL! 11614. HRS
FUEL H/C RATIO: 1.920
FUEL I JET - A
OPERATIONAL DATA «»»«*««
INLET AIR TEMPERATURE, DEGREES F: START 75.00 FINISH 76.00
ATMOSPHERIC PRESSURE: START 29.03 FINISH 29.oe
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0140
RELATIVE HUMIDITY: 76.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 133.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.99
NUMBER OF TESTS: 4
COMMENTS:
H/C CAL ESTIMATED
SAMPLE LINE TEMP. AVERAGED
WITHOUT RETROFIT
CLOCK
TIME
1030.00
1035.00
1045.00
1055.00
POWER
PERCENT
RATED
T.n.
63
6
90
6
POWER
PERCENT
RATED
T.O.
68
b
10
6
POWER
PERCENT
RATED
T.O.
68
6
90
A
TEST
MODE
2/ 0
I/ 2
5/ I
I/ 5
EXHAUST
GAS
TEMP
DEGREES F
870.00
695.00
1000.00
695.00
MASS EMI
CO
LB/1K
LB FUEL
3.81
44.48
2.79
41.67
co
POWER
THRUST, LBS
OR
SHP
9550.00
950.00
12700.00
910.00
EXHAUST
GAS
PRESSURE
PS I A
23.19
15.95
27.28
15.95
MASS EMI
HC
LB/IK
LB FUEL
0.17
8.90
0.14
15.00
PERCENT
RATED
r.o.
68
6
90
6
ENGINE
SPEED
Nl
7300.00
2900.00
8060.00
2850.00
CO
IWETI
RPM
N2
11030.00
7180.00
11530.00
707.00
MEASURED
FUEL
FLOW
LB/HR
5630.00
1030.00
7810.00
1060.00
CO THC NO
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
NO
2 (WET) (WET) 2
PPMV IWETI PPMV PPMV (WET)
PERCENT V
34.
105.
33.
73.
MASS EMI
N02
LB/IK
LB FUEL
8.96
3.48
9.45
5.63
CO
2
20
00
00
00
MASS FMI
C02
LB/IK
16 FUEL
3149.45
3061.58
3151.13
3049.26
1.80 2
0.46 36
2.37 2
0.34 45
MASS EMI
NO
LB/IK
LB FUEL
5.49
1.46
8.51
1.50
THC
L8/1KITH-HR LB/1KITH-HR LB/1KITH-HR
2.
48.
1.
48.
245
223
717
536
1856.691
3319.394
1937.820
3551.878
0.098
9.653
0.083
17.478
.60 30.
.70 2.
.80 61.
.90 1.
MASS Ml
NOX
LB/IK
LB FUEL
14.45
4.94
17.96
7.13
NCI
PPMV
00 49.00
10 5.00
20 68.00
60 6.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
NO
X
IWFT)
PPMV
79.00
7.10
129.20
7.60
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
RATIO
EPR
1.63
1.11
1.93
1.11
ALDEHYDES SMOKE
-0.00 -0
-0.00 -0
-0.00 -0
-0.00 -0
MASS EMI MASS EMI PASS EMI MASS EMI
CO
L8/HR
21.44
45.81
21.81
44.17
HC
LB/HR
0.93
9. 17
1.06
15.91
NO
2
Lfl/lK»rH-H» I_8/1K»TH-HR
3.
1.
5.
1.
235
584
231
747
5.284
3.772
5.812
6.553
N02 C02
L6/HR LB/Hrf
50.46 17731. ',0
3.58 3151.42
73.82 24610.31
5.96 3232.21
NO
X
LB/ 1KDTH-HR
8.5H
5.356
11.044
8.300
.00
.00
.00
.00
MASS
NO
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-O.OC
PARTICULATES
-0.00
-0.00
-0.00
-0.00
EM XflSS EMI
NOX
LR/HR LB/HR
30.
1.
66.
1.
89 81.35
50 5.09
44 140.25
59 7.54
IV-326
-------
DATEI II 1/71
TEST ORGANIZATION! UNITED/EPS
ENGINE SUPPLIERI UNITED AIRLINES
ENGINE OAT*
CAL ID NUMBER: 126
ENGINE TYPE AND MODEL: JT8D-T
SERIAL NUMBER:
65*607
RATED THRUST: 14000.
ENGINE TOTAL TINE: 9392. MRS
TIME SINCE HOT SECTION OVERHAUL: 2876. MRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 7351. HRS
N2 COMPRESSOR OVERHAUL: 7304. HRS
COMBUSTOR CAN REPLACEMENT: 2472. HRS
FIRST STAGE NOULE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 1231. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.920
FINISH
FINISH
56.30
29.90
FUEL: JET - A
OPERATIONAL DATA «««««««
INLET AIR TEMPERATURE. DEGREES F: START 56.84
ATMOSPHERIC PRESSURE: START 29.91
INLET AIR HUMIDITY, IBS HZO/LB AIR: 0.0069
RELATIVE HUMIDITY: 69.00 PERCEN1
SAMPLE LINE: TEMPERATURE. DEGREES C: 160.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 5.00
NUMBER OF TESTS: 3
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES HG.
CLOCK
TIME
2031.00
2037.00
2041.00
POKFR
PERCENT
RATED
T.O.
T6
87
96
PQHER
PERCENT
RATED
T.O.
76
87
96
POWER
PERCENT
RATED
T.O.
76
87
96
TEST POWER ENGINE
MODE THRUST, LBS PERCENT SPEED
OR RATED RPM
SHP T.O. Nl N2
I/ 0 10774.00 76 7427.00 11025.00
21 1 12222.00 87 7797.00 11265.00
3/ 2 13521.00 96 8139.00 11502.00
MEASURED GAS GEN CALC COMPRESSOR ENGINE TURBINE
FUEL AIR FLOW F/l DISCHARGE PRESSURE INLET
FLOW LB/SEC TEMP RATIO TEMP
LB/HR DEGREES F EPR DEGREES F
6246.00 -0.00 -0.000000 -0.00 1.72 -0.00
7175.00 -0.00 -0.000000 -0.00 1.B4 -0.00
8140.00 -0.00 -0.000000 -0.00 1.96 -0.00
EXHAUST EXHAUST CO CO THC NO NO NO ALDEHYDES SMOKE PART ICULATES
GAS GAS IWETI 2 IWETI IHETI 2 X
TEMP PRESSURE PPMV IWETI PPMV PPMV IWETI IWFT)
DEGREES F PSIA PERCENT V PPMV PPMV
667.20 51.60
912.20 55.10
962.60 58.60
MASS EMI MASS EMI
CO HC
LB/IK LB/IK
LB FUEL LB FUEL
3.08 0.09
1.62 0.08
1.53 0.08
CO
LB/lKfTM-HR
1.785
0.950
0.922
35.00 2.28
20.00 2.48
20.00 2.62
MASS EMI MASS EMI MASS EMI
N02 CC12 NO
LR/1K LB/IK LB/IK
LB FUEL LB FUEL LB FUEL
-0.00 3150.80 12.42
-0.00 3153.12 14.75
-0.00 3153.27 16.86
CO THC
2
LB/1K«TH-HR LB/1KHIH-HR
1826.612 0.053
1851.056 0.049
1698.349 0.048
l.BO 66.00 -0.00 86.00 -0.00 -0.00 -0.00
1.80 111.00 -0.00 113.00 -0.00 -0.00 -0.00
1.80 134.00 -0.00 137.00 -0.00 -0.00 -0.00
MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI
NOI CO HC N02 C02 NO NOX
LB/IK LB/HR LB/HR LB/HR LB/HR LB/HR LB/HR
LB FUEL
12.71 19.23 0.57 -0.00 19679.92 7^.60 79.41
15.02 11.61 0.60 -0.00 22623.63 105. B6 107.76
17.24 12.47 0.64 -0.00 25667.57 137.24 140.31
NR NO NO
2 X
LB/1MTH-HR LB/lKdTH-HR LB/1KHTH-HR
1.203 -0.000 7.370
8.661 -0.000 8.817
10.150 -0.000 10.377
IV-327
-------
o»re: 11 em
TEST ORGANIZATION! UNITED/EPA
ENGINE SUPPLIER! UNITED AIRLINES
ENGINE DATA »«««««» ».«.«
CAL 10 NUMBER: m ENGINE TYPE AND MODEL: JTSD-T
RATED THRUST: nooo.
ENGINE TOTAL TIME! 4929. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TINE SINCE!
NI COMPRESSOR OVERHAUL: 9008. HRS
N2 COMPRESSOR OVERHAUL: 3404. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL! 0. HRS
N2 TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO: 1.920
FINISH
FINISH
SERIAL NUMBER:
29.99
FUEL! JET - A
OPERATIONAL DATA «»»«»»«
INLET AIR TEMPERATURE, DEGREES F: START 54.86
ATMOSPHERIC PRESSURE! START 30.01
INLET AIR HUMIDITY. LBS H20/LB AIR: -0.0000
RELATIVE HUMIDITY! -0.00 PERCENT
SAMPLE LINE! TEMPERATURE. DEGREES C: -0.00, FLOM RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS! 3
COMMENTS:
EXHAUST GAS PRESSURE IS IN INCHES HG.
CLOCK
TIME
608.00
613.00
616.00
POWER
PERCENT
RATED
T.O.
77
86
46
POWER
PERCENT
RATED
T.O.
77
B6
96
POWER
PERCENT
RATED
r.o.
77
86
96
TEST POWER ENGINE MEASURED GAS GEN CALC COMPRESSOR ENGINE TURBINE
NODE THRUST, LBS PERCENT SPEED FUEL AIR FLOW F/A DISCHARGE PRESSURE INLET
OR RATED RPM FLOW LB/SEC TEMP RATIO TEMP
SHP T.O. Nl N2 LB/HH DEGREES F EP« DEGREES f
\l 0 10817.00 77 7966.00 11053.00 6251.00 -0.00 -0.000000 -0.00 1.73 -0.00
21 \ 12172.00 66 7663.00 11288.00 7111.00 -0.00 -0.000000 -0.00 1.84 -0.00
V 2 13539.00 96 7981.00 11520.00 8054.00 -0.00 -0.000000 -0.00 1.96 -0.00
EXHAUST EXHAUST CO CO THC NO NO NO ALDEHYDES SMOKE PARTICULATES
GAS GAS (WET) 2 IUET) IWETI 2 X
TEMP PRESSURE PPMV (WET1 PPMV PPMV (WET1 IWETI
DEGREES F PSIA PERCENT V PPHV PPMV
B60.00 51.90
905.00 55.20
957.20 58.70
MASS EMI MASS EMI
CO HC
LB/IK LB/1K
LB FUEL LB FUEL
1.02 0.11
0.90 0.11
O.B3 0.10
CO
LB/1KITH-HR
0.5B9
0.528
0.491
10.00 1.97 1.95 81.00 -0.00 86.00 -0.00 -0.
10.00 2.22 2.10 104.00 -0.00 109.00 -0.00 -0.
10.00 2.43 2.10 129.00 -0.00 134.00 -0.00 -0.
MASS FMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS FH1 MASS EMI
N02 C02 NO NOX CO HC NO? C02
LB/IK LB/IK LB/IK LB/IK LB/HR LB/HR LB/KR LB/HR
LB FUEL LB FUEL LB FUEL LB FUEL
-0.00 1153.98 13.56 14.39 6.37 0.71 -0.00 19715.51
-0.00 3154.17 15.45 16.19 6.43 0.77 -0.00 22429.30
-0.00 3154.32 17.51 18.18 6.65 0.80 -0.00 25404.87
CO THC NO NO NO
2 2 X
LB/1KITH-HR LB/1K»IH-HR LB/IKITH-HR LO/1KHTH-HR LB/1KHTH-HR
1822.641 0.066 7.834 -0.000 8.318
1B42.697 0.064 9.024 -0.000 9.458
1876.421 0.059 10.413 -0.000 10.817
00 -0.00
00 -0.00
oo -o.no
MASS EMI MASS EMI
NO NQX
LB/HR LH/HR
84.74 69. 98
109.84 115.1)
14(1.99 146.45
IV-328
-------
DATE: 7/21/71
TEST ORGANIZATION! UNITED/EPA
ENGINE SUPPLIERl UNITED AIRLINES
ENGINE DATA «»«»«»
CAL ID NUMBER! 406 ENGINE TVPE AND MODEL: JT8D-7
SERIAL NUMBER:
RATED THRUST: 14000.
ENGINE TOTAL T1MEI 4005. MRS
TINE SINCE HOT SECTION OVERHAUL: 4005. HRS
TIME SINCE!
Nl COMPRESSOR OVERHAUL: 10914. HRS
N2 COMPRESSOR OVERHAUL: 15004. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.920
FUEL: JET - A
OPERATIONAL DATA »«»»»«»««««
INLET AIR TEMPERATURE, DEGREES F: START 68.00 FINISH 68.00
ATMOSPHERIC PRESSURE: START 2i.ee FINISH 29.96
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0100
RELATIVE HUMIDITY: 63.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 160.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 5.00
NUMBER OF TESTS: 1
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES HG.
ENGINE HAD OIL LEAD INTO CELL
CLOCK
TIME
1500.00
POWER
PERCENT
RATED
T.O.
78
POWER
PERCENT
RATED
T.O.
78
POWER
PERCENT
RATED
TEST
MODE
I/ 0
EXHAUST
GAS
TEMP
DEGREES F
917.60
MASS EMI
CO
LB/IK
LB FUEL
3.73
POWER
THRUST, LBS PERCENT
OR RATED
SHP T.O.
11023.00
EXHAUST
GAS
PRESSURE
PSIA
52.20
MASS EMI
HC
LB/1K
LB FUEL
0.08
70
CO
IWETI
PPHV
40.00
ENGINE
SPEED
RPM
Nl N2
7493.00 11088.00
MEASURED GAS GEN
FUEL AIR FLOW
FLOW LR/SEC
LB/HR
6431.00 -0.00 -0.
CO THC NO NO
2 (WETI IWETI 2
IWET) PPHV PPMV (MET)
PERCENT V PPMV
2.15
MASS EMI MASS EMI MASS EMI
N02 C02 NO
LB/1K LB/1K LB/IK
LB FUEL LB FUEL LB FUEL
-0.00 3149. Bl 13.78
CO CO
2
LB/lKfTH-MR LB/1KITH-HR
THC
LB/lKfTH-HR
1.50 90.00 -0.00
CALC COMPRESSOR ENGINE
F/A DISCHARGE PRESSURE
TEMP RATIO
OFGREES F EPX
000000 -0.00 1.75
NO ALDEHYDES SMOKE
X
iwen
PPMV
98.00 -0.00 -0.00
TURBINE
INLFT
TEMP
OFGREF.S f
-0.00
PARTICULATES
-0.00
MASS EMI MASS EMI MASS EMI MASS EMI MASS FMI MASS EMI MASS [Ml
NOX CO HC NQ2 CU2 NO NOX
LB/1K LB/HR LB/HR LB/HR LB/HR Lfl/HR LH/HH
LB FUEL
15.01 23.99 0.
52 -0.00 20256.42 88.
64 96.52
NO HO NO
2 X
LB/1K#TH-HR LB/1K«TH-HR LB/lK«TM-Mfl
IV-329
-------
DATE: 7/16/71
TEST ORGANIZATION! U.S. BUREAU OF MINES
ENGINE SUPPLIER! AMERICAN AIRLINES
ENGINE DATA
CAL ID NUMBER! 91
ENGINE TYPE AND MODEL: JT8D-1
SERIAL NUMBER: 649416
RATED THRUST: 14000.
ENGINE TOTAL TIME: 2160. HRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE!
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HAS
N2 TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO: 1.920
FUEL: JET - A
OPERATIONAL DATA ««««»»«»«»««««
INLET AIR TEMPERATURE. DEGREES F: START 79.00 FINISH 78.00
ATMOSPHERIC PRESSURE: START 14.39 FINISH 14.35
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.0105
RELATIVE HUMIDITY: 65.00 PERCENT
SAMPLE LINE! TEMPERATURE, DEGREES C: 135.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME. SEC: -0.00
NUMBER OF TESTS: 4
COMMENTS:
H/C IS CAL-E5TIMATED
NEW PROBE CONFIG. USED
SAMPLE LINE TEMP. AVERAGED
NEW PROBE CONFIGURATION USED FOR THIS RUN
WITH RETROFIT
16.00
c.605
CLOCK
TIME
1255.00
100.00
120.00
125.00
POWER
PERCENT
RATED
T.O.
67
7
6
77
POWER
PERCENT
RATED
T.O.
67
7
6
77
POWER
PERCENT
RATED
T.O.
67
7
6
77
TEST
MODE
S/ 0
I/ 5
I/ 1
4/ 1
EXHAUST
GAS
TEMP
DEGREES f
900.00
715.00
715.00
945.00
MASS EMI
CO
LB/1K
LB FUEL
1.75
2B.44
27.75
1.62
CO
POWER ENGINE
THRUST, LBS
OR
SHP
9400.00
990.00
970.00
10800.00
EXHAUST
GAS
PRESSURE
PSIA
32.10
14.75
14.75
24.65
MASS EMI
HC
LB/1K
Lfl FUEL
0.10
6.25
6.14
0.14
PERCENT SPEED
RATED RPM
T.O. Nl N2
67 7215.00 10980.00
7 2910.00 7200.00
6 2860.00 7130.00
77 7510.00 11200.00
MEASURED GAS GEN
FUEL AIR FLOW
FLOW LB/SEC
LB/HR
5540.00 -0.00 -0.
1063.00 -0.00 -0.
1088.00 -0.00 -0.
6450.00 -0.00 -0.
CO CO THC NCI NC
IWETI 2 (WET) IWET) 2
PPMV IWET) P
PFRCENT V
19.50 2.23 I
169.00 1.17 64
162.00 1.15 62
19.50 2.41 3
MASS EMI MASS EMI MASS EMI
NO; C02 NH
LB/IK LB/IK LB/IK
LB FUEL LB FUEL LB FUEL
1.33 3152.66 10.32
1.94 3094.07 1.52
1.69 3095.44 1.15
1.16 3152.95 5.96
CO IHC
2
LB/IKITH-HR LB/IMTH-HR LB/1MTH-HR
1.
30.
31.
0.
034
541
128
970
1858.177 0.058
3322.215 6.707
3471.994 6.889
1883.010 0.085
PMV PPMV IWET)
PPKV
.90 69.80 9.00
.80 5.50 7.00
.60 4.10 6.00
.00 43.70 ». 50
MASS [MI MASS EMI MASS
HOt CO HC
CALC
F/A
000000
000000
000000
000000
NO
X
IWETI
PPMV
78.80
12.50
10.10
52.20
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
RATIO
EPR
1.63
1.03
1.03
1.74
ALDEHYDES SMOKE
0.36 -0
6.36 -0
-0.00 -0
0.29 -0
tMI MASS fMI MASS t*l
N02 C02
LB/IK LR/hR LR/HR LB/HR LB/HR
LB FUEL
11.65 9.72 0.
3.46 30.24 6.
2.64 30.19 6.
7.14 10. 47 0.
NU
54
64
68
92
NO
2
L8/1MTH-HK LB/1K«TH-HR
6.080
1.633
1.294
3.569
0.784
2.078
1.894
0.694
7.3F 17466.87
2.06 3288.99
l.«4 3367.83
7.50 20336.50
NO
I
L9/IKITH-HR
6.664
3.711
3.188
4.264
.00
.00
.00
.00
MASS
no
TURBINE
INLET
TEMP
DEGREES f
14.15
14.13
14.33
14.15
PdRTlCULATFS
-0.00
-0.00
-C.OO
-0.00
EMI MASS IHI
NOX
LG/HK LB/MO
57.
1.
1.
36.
15 64.52
62 3.67
26 3.09
55 46.05
IV-330
-------
DATEt 6/25/71
TEST ORGANIZATION! U.S. BUREAU OF NINES
ENGINE SUPPLIERl AMERICAN AIRLINES
ENGINE DATA
CAL 10 NUNBERl 88
ENGINE TYPE AND MODEL: JT-8D-9
SERIAL NUMBER:
RATED THRUST: 14500.
ENGINE TOTAL TINEl 6589. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE!
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT! 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. MRS
N2 TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO! 1.920
FUEL: JET - A
OPERATIONAL DATA «»»««««
INLET AIR TEMPERATURE, DEGREES F: START 90.00 FINISH 91.00
ATMOSPHERIC PRESSURE! START 14.35 FINISH I*.35
INLET AIR HUMIDITY, IBS H20/LB AIR! 0.0130
RELATIVE HUMIDITY! 42.00 PERCENT
SAMPLE LINE! TEMPERATUREi CEGREES C: 109.00, FLOW RATE, LITERS/HIM:
SAMPLE LINE TRANSPORT TIME, SEC! 0.99
NUMBER OF TESTS: 5
COMMENTS:
H/C IS CAL-ESTIHATED
TEMPERATURE OF SAMPLE LINE AVERAGED
KITH RETROFIT
16.00
CLOCK
TIMF
1110.00
1135.00
1140.00
1145.00
1150.00
PONER
PERCENT
RATED
T.O.
6
92
80
T3
69
POKER
PERCENT
RATED
T.O.
6
92
80
71
69
POKER
PERCENT
RATED
T.O.
6
92
80
73
69
TEST
MODE
I/ 0
2/ 1
3/ 2
»/ 3
?/ 4
EXHAUST
GAS
TEMP
DEGREES F
-0.00
1040.00
975.00
935.00
925.00
MASS EMI
CO
LB/1K
L8 FUEL
23.40
1.31
1.71
2.18
2.29
POWER
THRUST, LBS PERCENT
OR RATED
SHP
920.00
13360.00
11640.00
10600.00
10070.00
EXHAUST
GAS
ENGINE
SPEED
RPM
T.O. Nl
6 2890
92 8120
80 7723
73 7487
69 7377
CO
IHETI
PRESSURE PPNV
PSIA
15.20
28.30
26.10
25.90
23.30
MASS EMI
HC
LB/IK
L8 FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
CO
LB/ IKf TH-HR
28.
0.
1.
1.
1.
228
812
033
306
36*
.00
.00
.00
.00
.00
N2
7210.00
11590.00
11384.00
11217.00
11131.00
MEASURED
FUEL
FLOW
LB/HR
1110.00
8300.00
7040.00
6340.00
5990.00
CO THC NO
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
NO
-0.
-0.
-0.
-0.
-0.
2 (MET) (HEM 2
(NET) PPMV PPMV (WET)
PERCENT V
66.00
20.00
24.00
27.00
28.00
MASS EMI MASS
0
3
2
2
2
EMI
N02 C02
IB/IK LB/
IK
Lfl FUEL LB FUEL
0.87 3119.
0.81 3153.
0.99 3153.
1.20 3152.
1.21 3152.
CO
2
LB/lKf TH-Hft
3763.293
1959.343
1907.093
1885.526
1875.094
13
83
20
46
29
.56 -0
.07 -0
.82 -0
.48 -0
.45 -0
MASS EMI
NO
LB/1K
LB FUEL
3.20
17.93
16.13
15.68
15.06
THC
LB/1KMH-HR
-0.000
-0.000
-0.000
-0.000
-0.000
.00 5.
.00 167.
.00 138.
.00 113.
.00 112.
MASS EMI
HOt
LB/1K
Lfl FUEL
4.03
18.74
17.12
16.88
16.28
PPMV
50 1 . 50
oo 7.50
00 8.50
00 9.00
00 9.00
MASS EMI MASS
CO
LB/HR
25.97
10.85
12.02
13.85
13.73
HC
LB/
-0.
-0.
-0.
-0.
-0.
Nil
CALC
F/A
000000
000000
000000
000000
000000
NO
X
IWET)
PPMV
7.00
174.50
146.50
127.00
121.00
COMPRESSOR CNGINE TURBINE
DISCHARGE PRESSURE INLET
TEMP KATIO IEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
EPR DEGREES F
1.05 14.38
1.98 14.20
1.84 14.20
1.80 14.20
1.63 14.20
ALDEHYDES SMOKE PAPTICULATES
2.76 -0
0.90 -0
1.22 -0
1.59 -0
0.87 -0
EMI MASS EMI MASS EMI
HR
00
00
00
00
00
NO
?
LB/1KIITM-MR LH/1K*TH-HR
3.
11.
9.
9.
a.
864
142
756
379
961
1.054
0.500
0.601
0.715
0.720
N02 CC12
LB/HR LB/HR
0.97 3467.21
6.69 26176.82
6.99 22198.56
7.58 19986.57
7.25 18882.19
NO
X
LB/IK«TM-HR
4. lib
11.643
10.357
10.094
9.6BI
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
MASS EMI MASS EXI
NO NDX
LP/HB LB/HR
3.55 4.52
140.86 195.54
113.56 120.56
99.41 107.00
90.24 97.49
IV-331
-------
DATE! 8/19/71
TEST ORGANIZATION! PRATT I WHITNEY
ENGINE SUPPUERI PRATT AND WHITNEY
ENGINE DATA
CAL 10 NUMBERl 35* ENGINE TYPE AND HODELi JT-80-9
RATED THRUST: 14500.
ENGINE TOTAL TINE: -0. MRS
TINE SINCE HOT SECTION OVERHAUL: -0. HRS
TIME SINCE!
Nl COMPRESSOR OVERHAUL: -0. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. HRS
N2 TURBINE OVERHAUL: -0. HRS
SERIAL NUMBER:
FUEL H/C RATIO: 2.000
FINISH
FINISH
80.00
24.95
FUEL: JP-4
OPERATIONAL DATA ««««««««»«»
INLET AIR TEMPERATURE. DEGREES F: START 84.00
ATMOSPHERIC PRESSURE: START 29.96
INLET AIR HUMIDITY, LBS H20/LB AIR: -0.0000
RELATIVE HUMIDITY! -0.00 PERCENT
SAMPLE LINEI TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LtrtRS/HIN:
SAMPLE LINE TRANSPORT TIME, SEC: 1.00
NUMBER Of TESTSt 6
COMMENTS:
EXHAUST GAS PRESSURE IN INCHES HG
CLOCK
TIME
1713.00
1001.00
IBM. 00
1822.00
1030.00
18*5.00
POWER
PERCENT
RATED
T.O.
14
65
74
82
9*
5
POWER
PERCENT
RATED
T.O.
34
65
74
B2
94
5
POWER
PERCENT
RATED
T.O.
3*
65
74
82
94
5
TEST
MODE
I/ 0
2/ 1
J/ 2
4/ 3
5/ 4
6/ 5
EXHAUST
GAS
TEMP
DEGREES F
710.00
875.00
915.00
950.00
1010.00
685.00
MASS EMI
CO
LB/1K
LB FUEL
5.84
1.55
1.16
0.98
0.72
41.35
CO
IB/Hi
3.
0.
0.
0.
0.
44.
POWER ENGINE
THRUST, LBS PERCENT SPEED
OR RATED RPM
SHP
5040.00
9520.00
10850.00
11950.00
13750.00
840.00
EXHAUST
GAS
PRESSUR
PSIA
38.61
48.26
51.63
54.32
59.29
31.05
MASS EMI
HC
LB/1K
LB FUEL
0.40
0.16
0.14
0.15
0.17
3.77
TH-HR
395
876
662
562
431
849
T.O. Nl
34 5750.00
65 7160.00
74 7460.00
82 7710.00
94 8175.00
5 2590.00
CO
IWETI
E PPMV IW
N2
9880.00
10910.00
11125.00
1U94.00
11590.00
840.00
CO
MEASURED
FUEL
FLOW
LB/HR
2929.00
5375.00
6190.00
6860.00
8195.00
911.00
THC NO
GAS GEN
AIR FLOW
LB/SEC
CALC
F/A
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIO
DEGREES F F.PR
H4.80
121.00
129.00
136.60
150.80
29.90
NO
0.
0.
0.
0.
0.
0.
2 IWETI IWETI 2
ETI
PPMV PPM
PERCENT V
49.30
18.50
15.00
13.20
10.70
195.20
MASS EMI MASS EMI
N02 C02
LB/1K LB/1K
LB FUEL LB FUEL
1.26 3127.47
1.25 3134.87
1.16 3135.53
1.11 3135.80
1.04 3136.13
O.BO 3062.41
CO
2
LB/1KOTH-HR LB
1817.532
1769.952
1788.844
1800.131
1B69.I33
3321.261
1.68
2.38
2.58
2.69
2.95
5.90 0.
3.30 «5.
3.20 105.
3.50 124.
4.50 166.
0.92 31.10 6.
MASS EMI
NO
LB/1K
LB FUEL
0.0
11.81
13.37
15.12
18.45
2.37
THC
/1KHTH-HR
0.233
0.089
0.081
0.085
0. 104
4.092
MASS EMI
NOX
LB/IK
LB FUEL
1.26
13.08
145.22
16.23
19.49
3.17
NO
LB/1KHT
0.
*>.
7.
8.
10.
2.
V IWETI
PPMV
0 6.50
90 9.10
20 9.10
10 9.10
00 9.40
80 2.30
MASS EMI MISS
CO
LB/HR
17.11
B.34
7.18
6.72
5.93
37.67
H-HR Lf
0
678
625
682
995
566
HC
LB/
1.
0.
0.
1.
1.
3.
i/lK
009590
012340
013330
013950
015090
006460
NO
X
IWETI
PPMV
6.50
95.00
1143.00
133.20
175.40
9.10
-0
-0
-0
-0
-0
-0
.00 1.30
.00 1.63
.00 1.75
.00 1.85
.00 2.02
.00 1.04
TURBINE
INLET
TEMP
OFGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES SMOKf PARTICULATES
-0
-0
-0
-0
-0
-0
EMI MASS EMI
HR
17
85
88
02
43
44
XQ
2
KTH-HH
0.735
0.707
0.660
0.637
0.623
0.868
NO 2
LB/HR
3.71
6.74
7. 16
7.61
8.56
0.73
LB
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
MASS F1I MASS EH!
C02 NO
LB/HR L8/HR
9160.16 0.0
16849.94 63.58
19408.95 82.73
21511. 56 103.75
25700.58 151.19
2789.86 2.16
NO
X
/IKHTH-MR
0.715
7.3S6
82.84H
9.319
11.618
3.434
-n.oo
-0.00
-0.00
-0.00
-n.oo
-c.oo
1 .MASS EMI
NOX
Lfl/HH
3.71
70.31
898.90
111.35
159.75
2.88
IV-332
-------
DATE: 8/ 6/Tl
TEST ORGANISATION: U.S. BUREAU OF NINES
ENGINE SUPPLIER! AMERICAN AIRLINES
EN6INE OAIA «««»««««»««««««»«« .««
CAL ID NUMBER: 113 ENGINE TYPE AND MODEL: SPEY
SERIAL NUMBER:
RATED THRUST: 11400.
ENGINE TOTAL TIME: 7861. MRS
TIME SINCE HOT SECTION OVERHAUL: 656. MRS
TIME SINCEI
Nl COMPRESSOR OVERHAUL: 658. HRS
N2 COMPRESSOR OVERHAUL: 658. HRS
COMBUSTOR CAN REPLACEMENT: 658. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 658. HRS
Nl TURBINE OVERHAUL: 656. HRS
N2 TURBINE OVERHAUL: 658. HRS
FUEL H/C RATIO: 1.920
FUELl JET - A
OPERATIONAL DATA «««
INLET AIR TEMPERATURE, DEGREES fi START 72.00 FINISH 72.00
ATMOSPHERIC PRESSURE: START 21.12 FINISH 29.12
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0150
RELATIVE HUMIDITY: 84.oo PERCENT
SAMPLE LINE: TEMPERATURE! DEGREES C: 147.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TINE, SECl 0.99
NUMBER OF TESTS! 7
COMMENTS"
H/C CAL ESTINATED
SAMPLE LINE TENP. AVERAGED
ENGINE RUN 380)71,RETURNED TO SHOP FOR REPAIRS
THEN TO TEST SECOND TIME
PROBE SANE AS USED 08-02-71
.FT. OF SAMPLE LINE NOT HEATED
CLOCK
TIME
920.00
925.00
930.00
935.00
940.00
945.00
950.00
POWER
PERCENT
RATED
T.O.
5
99
95
90
85
65
5
POMER
PERCENT
RATED
T.O.
5
99
95
90
85
65
5
POMER
PERCENT
RATED
T.O.
5
99
95
90
85
65
5
TEST POMER ENGINE MEASURED GAS GEN CALC COMPRESSOR ENGINE TURBINE
NODE THRUST, LBS PERCENT SPEED FUEL AIR FLOH F/A DISCHARGE PRESSURE INLET
OR RATED RPN FLOM LB/SEC TENP RATIO TEMP
SHP T.O. Nl N2 LB/HR DEGREES F EPR DEGREES F
I/ 0 630.00 5 2690.00 7560.00 960.00 -0.00 -0.000000 -0.00 1.06 -0.00
11 1 11)40.00 99 8500.00 12420.00 7480.00 -0.00 -0.000000 -0.00 2.54 -0.00
3/ 2 10900.00 95 8380.00 12320.00 7150.00 -0.00 -0.000000 -0.00 2.48 -0.00
4/ 3 10300.00 90 8190.00 12150.00 6670.00 -0.00 -0.000000 -0.00 2.40 -0.00
5/ 4 9800.00 85 8050.00 12000.00 6290.00 -0.00 -0.000000 -0.00 2.32 -0.00
6/ 5 7500.00 65 7375.00 11550.00 4690.00 -0.00 -0.000000 -0.00 1.98 -0.00
I/ 6 650.00 5 2700.00 7620.00 93.00 -0.00 -0.000000 -0.00 1.06 -0.00
EXHAUST EXHAUST CO CO THC NO NO NU ALDEHYDES SNUKt PARTICIPATES
GAS GAS IMETI 2 (HETI (HETI 2 X
TEHP PRESSURE PPNV (UETI PPHV PPNV IHETI (HETI
DEGREES F PSIA
810.00 15.30
1155.00 35.98
1125.00 35.25
1100.00 34.03
1075.00 32.90
955.00 28.24
820.00 15.30
HASS ENI NASS ENI
CO HC
LB/IK LB/IK
LB FUEL LB FUEL
-0.00 1150.35
2.67 0.19
2.87 0.19
3.13 0.16
3.32 0.17
4.B4 0.15
108.21 52.64
CO
LB/IKITH-HR
-0.000
1.761
1.885
2.026
2.129
3.024
15.482
PERCENT V
-0.00 -0.00 1050
41.00 3. OB 5
43.00 3.00 5
44.00 2.82 4
46.00 2.78 4
56.00 2.32 3
730.00 1.22 620
NASS EHI NASS ENI MASS EHI
N02 C02 NO
LB/IK LB/IK LB/IK
LB FUEL LB FUEL LB FUEL
-0.00 -0.00 -0.00
1.93 1151.18 -0.00
2.42 3150.85 -0.00
3.39 3150.53 -0.00
4.26 3150.22 -0.00
4.68 3147.88 -0.00
1.46 2841.47 -0.00
CO THC
2
LB/IKITH-HR LB/IKITH-HR
-0.005 1752.911
2078.557 0.123
2066.840 0.126
2040.195 0.105
2021.929 0.106
1968.476 0.093
406.548 7.531
PPNV PPHV
.00 -0.00 -0
.00 -0.00 IB
.00 -0.00 22
.00 -0.00 29
.00 -0.00 36
.00 -0.00 33
.00 -0.00 6
NASS ENI MASS ENI
NOX co
LB/IK LB/HR
LB FUEL
-0.00 -0.00
1.93 19.97
2.42 20.55
3.39 20.87
4.26 20.87
4.68 22.68
1.46 10.06
NO
LB/lKfTH-HR
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
-0.000
.00 -0.00 -0.
.00 IB. 00 1.
.00 22.00 0.
.00 29.00 0.
.00 36.00 0.
.00 33.00 0.
.00 6.00 76.
MASS EMI NASS EMI
HC N02
LB/HR LB/HR
1104.33 -0.00
1.39 14.40
1.37 17.27
1.09 22.59
1.04 26.82
0.70 21.95
4.90 0.14
NO
2
00 -0.
25 -0.
66 -0.
46 -0.
48 -0.
44 -0.
10 -0.
NASS ENI
CO 2
LU/HR
-0.00
23570.84
22528.56
21014.00
19314.90
14763.57
264.26
NO
X
DO -0.00
00 -0.00
00 -0.00
00 -0.00
00 -0.00
00 -0.00
oo -n.oo
NASS EMI HASS EMI
NO NOX
Lfl/HB Lt/HR
-0.00 -0.00
-0.00 14.40
-0.00 17.27
-0.00 22.59
-0.00 26.82
-0.00 21.95
-0.00 0.14
LB/IKITH-HR LB/IKITH-HR
-0.000
1.270
1.584
2.193
2.737
2.927
0.209
-o.coo
1.270
1.584
2.193
2.73;
2.927
0.209
IV-333
-------
DATE! 7/27/71
TEST ORGANIZATION) U.S. BUREAU OF MINES
ENGINE SUPPLIER! AMERICAN AIRLINES
ENGINE DATA
CAL 10 NUMBER! 1*1
ENGINE TYPE AND MODEL: SPEY 511-1*
SERIAL NUMBED: 7072
RATED THRUST: 11*00.
ENGINE TOTAL TIME: 7500. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE!
Nl COMPRESSOR OVERHAUL: 7500. HRS
N2 COMPRESSOR OVERHAUL: 7500. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 7500. HRS
N2 TURBINE OVERHAUL! 7500. HRS
FUEL H/C RATIO: 1.920
FUEL: JET - A
OPERATIONAL DATA »»««»»«»««».«««»»»«.
INLET AIR TEMPERATURE, DEGREES f: START 79.00 FINISH 79.00
ATMOSPHERIC PRESSURE: START 29.20 FINISH 29.20
INLET AIR HUMIDITY, LBS M20/LB AIR: 0.0
RELATIVE HUMIDITY: 67.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 135.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.99
NUMBER OF TESTS: I
COMMENTS:
H/C CAL ESTIMATED
SAMPLE LINE TEMP. AVERAGED
PROBE SUPPORT PIPE FAILED AFTER RUN
PROBE LOCATED 13* DOUNSTREAM
CLOCK
TIME
1020.00
POWER
PERCENT
RATED
T.O.
*
POWER
PERCENT
RATED
r.o.
*
POWER
PERCENT
RATED
TEST
MODE
*/ 0
EXHAUST
GAS
TEMP
DEGREES F
B50.00
MASS EMI
CO
LB/IK
LB FUEL
107.5*
POWER
THRUST, LBS PERCENT
OR RATED
SHP T.O.
520.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
MASS EMI
HC
LB/IK
LB FUEL
97.3*
*
CO
(WET)
PPMV
820.00
ENGINE
SPEED
RPM
Nl N2
2680.00 7300.00
MEASURED GAS GEN CALC
FUEL AIR FLOW F/A
FLOW LB/SEC
LB/HR
1130.00 -0.00 -0.000000
CO THC NO NO NO
2 IWETI (WET) 2 X
IWETI PPMV PPMV (WET) (WET)
PERCENT V PPMV PPMV
1.32 1296.00 1.20 3.00 4.20
MASS EM| MASS EMI MASS EMI
N02 C02 NO
LB/IK LB/IK LB/IK
LB FUEL LB FUEL LB FUEL
0.65 2719. 86 0.26
CO CO
2
LB/IKiTH-MR LB/1K»TM-HR
THC
LB/IKHTH-HR
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TCMP RATIO
DECREES F EPR
-0.00 -0.00
ALDEHYDES SMOKE
-0.00 -0.00
TURBINE
INLET
TEMP
OEGREfS F
-0.00
PAPTICULATES
-0.00
MASS EMI MASS FMI MASS EMI MASS EH 1 MASS FMI MASS EMI 1ASS CMI
NOX CO HC N02 C02 NO NDX
LB/IK LB/HR LB/HR LB/HR LB/MR LO/HK LB/HR
LB FUEL
0.90 121.52 109.99
NO NO
2
LB/1KDTH-HR LB/lKfTH-MR
0.73 3073.47 C.
NO
X
I B/l KtTH-MR
21 1.02
IV-334
-------
DATE! II B/Tl
TEST ORGANIZATION! SCOTT/NORFOLK
ENGINE SUPPLIER! PRATT AND MHITNEY
ENGINE DATA
CAL 10 NUMBER! 109
ENGINE TYPE AND MODEL: JS2 - Pat
SERIAL NUMBER:
677106
RATED THRUST: 4300.
ENGINE TOTAL TIME: 474. MRS
TIME SINCE HOT SECTION OVERHAUL: 474. HRS
TIME SINCE!
Nl COMPRESSOR OVERHAUL: 474. HRS
N2 COMPRESSOR OVERHAUL: 474. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 474. HRS
NI TURBINE OVERHAUL: 474. HRS
N2 TURBINE OVERHAUL! 474. HRS
FUEL H/C RATIO: 1.970
FUEL: JP-S
OPERATIONAL DATA ««««««»«««»«»«*»»»»
INLET AIR TEMPERATURE. DEGREES F: START 83.50 FINISH 04.00
ATMOSPHERIC PRESSURE: START jo.ia FINISH 30.is
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0150
RELATIVE HUMIDITY: 59.00 PERCENT
SAMPLE LINE: TEMPERATUREi DEGREES C: 88.BO. FLOW RATE. LITERS/HIM: -0.00
SAMPLE LINE TRANSPORT TIME. SEC: -0.00
NUMBER OF TESTS: 4
COMMENTS:
H/C CAL ESTIMATED
PROBE- 3 HOLE JURY RIG
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
TEST
MODE
I/ 0
21 1
3/ 2
4/ 3
POWER
THRUST>LBS PERCENT
OR RATED
SHP T.O.
4BO.OO
5600.00
7570.00
B230.00
5
60
81
ENGINE
SPEFD
RPM
Nl
0.00
0.00
0.00
0.00
HZ
6898.00
10974.00
11569.00
11774.00
MEASURED
FUEL
FLOW
LB/HR
700.00
4220.00
5850.00
6490.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
CAIC
F/A
0.0
0.0
0.0
0.0
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
0.0
0.0
0.0
0.0
ENGINF
PRESSURE
RATIO
EPR
-0.00
2.04
2.41
2.55
TURBINE
INLET
TEMP
DEGREES F
0.0
0.0
0.0
0.0
POWER
PERCENT
RATED
T.O.
5
60
81
88
EXHAUST
GAS
TEMP
DEGREES F
500.00
880.00
1040.00
1100.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
42.60
46.70
CO
(DRY)
PPMV
410.00
24.00
19.00
24.00
CO
2
IDRV)
PERCENT
1.18
2.30
2.67
2.95
THC
IDRVI
PPMV
309.00
15.00
2.00
1.40
NO
I DRY I
PPMV
9.90
50.00
80.00
90.00
NO
2
IORY)
PPMV
5.00
8.00
7.50
6.00
NO
X
IDRVI
PPMV
14.90
58.00
87.50
96.00
ALDEHYDES SMOKE PARTICULATES
9.00
1.00
3.00
2.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
POWER
PERCENT
RATED
T.O.
60
Bl
88
MASS EMI
CO
LB/1K
LB FUEL
65.54
2. OB
1.42
1.63
MASS EMI
HC
LB/1K
LB FUEL
28.29
0.75
0.09
0.05
MASS EMI
N02
LB/1K
LB FUEL
1.31
1.14
0.92
0.67
MASS EMI
C02
LB/1K
LB FUEL
2963.93
3139.20
3142.05
3141.82
MASS EMI
NO
IB/ IK
LB FUEL
2.60
7.13
9.84
10.02
MASS EMI
NOX
LB/1K
LB FUEL
3.91
8.28
10.76
10.69
MASS EM
CO
LD/KR
45. BB
8.80
a. 32
10.56
MASS EH1
MC
LB/HR
MASS EMI
NO 2
LB/HR
MASS EMI
CO 2
LB/HR
MASS EM
NO
LO/HR
M4SS E»
NDX
LB/HR
19.80
3.15
0.50
0.35
0.92 2074.75
4.82 13247.43
5.40 18381.00
4.34 20390.40
1.9!
30. II
57.57
65.03
2.74
34.92
62.97
69.37
POWER
PERCENT
RATED
T.O.
5
60
ai
88
CO
LB/1KITH-HR
95.585
1.571
1.100
1.283
LB/1KITH-KR
4322.395
2365.613
2428.138
2477.571
THC
LB/IKJTH-HR
41.258
0.562
0.066
0.043
NO
LB/lKfTH-HR
3.791
5.376
7.606
7.902
LB/1K»TH-HR
1.915
0.860
0.713
0.527
NO
X
LH/IKITH-HR
5.706
6.236
8.319
8.429
IV-335
-------
OATEI 7/28/71
TEST ORGANIZATION! SCOTT/NORFOLK
ENGINE SUPPLIER! NORFOLK NAS
ENGINE DATA **»*
CAL 10 NUMBER: 157 ENGINE TYPE AND MODEL: J52 - pet
SERIAL NUMBER:
RATED THRUST: 9300.
ENGINE TOTAL TINE: 1310. MRS
TIME SINCE HOT SECTION OVERHAUL: 328. HRS
TIME SINCE!
Nl COMPRESSOR OVERHAUL: 328. HRS
N2 COMPRESSOR OVERHAUL: 328. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: 328. HRS
N2 TURBINE OVERHAUL: 128. HRS
FUEL H/C RATIO: 1.970
FINISH
FINISH
82.00
30.06
FUEL: JP-S
OPERATIONAL DATA ««««
INLET AIR TEMPERATUREt DEGREES F: START 78.50
ATMOSPHERIC PRESSURE: START 30.06
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0177
RELATIVE HUMIDITY! 77.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 126.00. FLOW RATE, L I rF.RS/NIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER CF TESTS: 4
COMMENTS:
H/C CAL ESTIMATED
J661
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
POMER
PERCENT
RATED
T.O.
5
55
7*
B6
POMER
PERCENT
RATED
T.O.
5
55
74
86
POKER
PFRCENT
RATED
T.O.
5
55
74
86
TEST
MODE
I/ 0
2/ 1
3/ 2
4/ 3
EXHAUST
GAS
TEMP. .
DEGREES F
520.00
845.00
981.00
1085.00
MASS EMI
CO
LB/IK
LB FUEL
88.86
7.83
J.55
1.93
POKER ENGINE MEASURED GAS GEN
THRUST, LBS PERCENT SPEED FUEL AIR FLOM
OR RATED RPM FLOW LB/SEC
SHP T.O. Nl N2 LB/HR
490.00
5200.00
6900.00
8040.00
EXHAUST
GAS
._ .PRESSUR.E
PSIA
-0.00
26.30
35.90
42.10
MASS EMI
HC
LB/IK
Lfl FUEL
la. 59
0.20
0.04
0.02
5 -0
55 -0
74 -0
86 -0
CO
(DRY)
PRMV.
605.00
90.00
57.00
34.00
.00
.00
.00
.00
6742.00
1073.00
11202.00
11582.00
CO THC
2 IDRVI
IDRY) BPJIV
PERCENT V
MASS EMI MASS EMI
N02 C02
LB/IK LB/IK
Lfl FUEL LB FUEL
0.46 2953.
0 . 29 3131.
0.20 3118.
0.19 3141.
CO CO
2
LB/1KITH-HR LB/IKITH-HD
136.
5.
2.
1.
010
980
732
523
4521.281
2390.909
2417.826
24F7.210
91
67
85
45
1.28 221.00
2.29 4.00
3.21 1.00
3.52 0.50
750.00 -0.00
3970.00 -0.00
5315.00 -0.00
6340.00 -0.00
NQ NO
(DRY) 2
. PPMV .(DRY)
PPMV
83.00 1.90
116.00 2.00
133.00 2.00
154.00 2.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
NO
X
IDRY)
PPMV
84.90
118.00
135.00
156. OC
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP PATIO
DEGREES F EPR
-0.00 -0.00
-0.00 1.89
-0.00 2.21
-0.00 2.41
ALDEHYDES SMOKE
2.40 -0.00
0.40 -0.00
0.50 -0.00
0.30 -0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-O.CO
-0.00
-C.OO
-0.00
MASS EMI MASS EMI MASS EMI MASS FMI HISS FHI MASS ffHl MASS EIM MASS EMI
NO NOX CO HC N02 C02 NO NOX
LB/IK LB/IK LB/HR LB/HR LB/HR LI/HI) LX/HK LB/HR
LB FUEL LB FUEL
20.02
16.58
13.60
14.37
THC
LB/lKiTH-HR
28.455
0.152
0.027
0.013
20.48 66.64
16.67 31.10
13.80 18.85
14.55 12.24
13.94
0.79
0.19
0.10
NO NO
2
L3/IKDTH-HR L8/1K«TH-HR
30.649
12.661
10.473
11.330
0.702
0.218
0.157
0.147
0.34 2215.43 15.
1.14 12432.73 65.
1.09 16683.00 72.
1.18 19916.77 91.
NO
X
LB/1K»TH-H»
31.350
12.379
10.630
11.477
02 15.36
84 66.97
26 73.35
09 92.27
IV-336
-------
DATEl 7/28/71
TEST ORGANIZATION! SCOTT/NORFOLK
ENGINE SUPPLIER! NORFOLK N»S
ENGINE OAT*
CAL 10 NUMBER: 156
ENGINE TYPE AND MODEL: J52 - P8A
SERIAL NUMBER:
RATED THRUST: 9300.
ENGINE TOTAL TINE: 88*. MRS
TIME SINCE HOT SECTION OVERHAUL: 511. HRS
TINE SINCE:
Nl COMPRESSOR OVERHAUL: 780. HRS
N2 COMPRESSOR OVERHAUL: 646. HRS
CONBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZILE GUIDE VANE OVERHAUL! -0. HRS
Nl TURBINE OVERHAUL: 511. HRS
NZ TURBINE OVERHAUL: 511. HRS
FUEL H/C RATIO: 1.970
FINISH
FINISH
04.00
30.01
FUEL: JP-5
OPERATIONAL DATA ««»«
INLET AIR TEMPERATURE. DEGREES F: START 82.00
ATMOSPHERIC PRESSURE: START 30.01
INLET AIR HUM I 01 IT, LBS HZO/LB AIR: 0.0189
RELATIVE HUNIOITVi 77.00 PERCENT
SAMPLE LINE: TEMPERATuREi DEGREES C: 121.00. FLOW RATE. LITERS/NIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 4
COMMENTS:
H/C CAL ESTIMATED
CLOCK
TINE
-0.00
-0.00
-0.00
-0.00
TEST
MODE
I/ 0
2/ 1
3/ 2
4/ 3
POWER
THRUST,LBS PERCENT
OR RATED
SHP T.O.
7560.00
5920.00
500.00
8420.00
81
63
5
90
ENGINE
SPEED
RPM
Nl
0.00
0.00
0.00
0.00
N2
11609.00
11160.00
6900.00
11892.00
MEASURED
FUEL
FLOW
LB/HR
5860.00
4470.00
710.00
6670.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
CALC
F/A
-0.000000
-0.000000
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINE:
PRESSURE
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES f
-0.00
-0.00
-O.OC
-0.00
PONER
PERCENT
RATED
T.O.
81
63
5
90
EXHAUST
GAS
TEMP
DEGREES F
1055.00
915.00
510.00
1148.00
EXHAUST
GAS
PRESSURE
PSIA
41.60
31.90
-0.00
46.70
CO
(DRY)
PPMV
365.00
59.00
33.00
32.00
CO
2
I CRY I
PERCENT V
1.21
2.53
2.86
3.14
THC
(DRY)
PPMV
70.00
2.00
0.50
0.49
NO
IORYI
PPMV
8.00
40.00
53.00
76.00
NO
2
(DRY)
PPKV
2.00
3.00
3.00
2.00
NO
X
(DRY)
PPMV
10.00
43.00
56.00
80.00
ALDEHYDES SMOKE PARTICUL»TES
3.40
0.10
0.05
0.40
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
61
63
5
90
MASS EMI
CO
LB/IK
LB FUEL
58.28
4.66
2.31
2.04
MASS EMI
HC
LB/IK
LB FUEL
6.40
0.09
0.02
0.02
MASS EMI
NO 2
LB/IK
LB FUEL
0.52
0.39
0.34
0.21
MASS EMI
C02
LB/IK
LB FUEL
3035.40
31)6.96
3140.85
3141.27
MASS EMI
NO
LB/IK
LB FUEL
2.10
5.16
6.06
8.16
MASS EMI
Nnx
LB/IK
LB FUEL
2.62
5.57
6.43
8.37
MASS EMI
CO
LB/HR
341.49
20.81
1.64
13.59
MASS EMI
HC
L8/HR
37.51
0.40
0.01
0.12
MASS EMI
N02
LB/HR
3.07
1.74
0.24
1.40
MASS EMI
C02
LB/HR
17787.45
14022.?!
2230.00
20952.30
MASS HM
NU
LB/HR
12.29
23. la
4.3?
54.41
MASS EMI
NUX
LB/HR
15.37
24.91
4.56
55.Hl
POWER
PERCENT
RATED
T.O.
81
63
5
90
CO
LB/1KITH-MR
45.171
3.516
3.275
1.614
LB/1KHTH-HK
2352.637
2360.618
4460.000
2488.397
THC
LB/1KHTH-HR
4.961
0.066
0.028
0.014
NO
LB/1K«TH-HR
1.626
J.915
6.640
6.462
LB/1KITH-HR
0.407
0.294
0.4S9
0.166
LB/IK*TH-MR
2.031
4.200
9.129
6.626
IV-337
-------
DATE: it B/TI
TEST ORGANIZATION! SCOTT/NORFOLK
ENGINE SUPPLIER: NORFOLK N«S
ENGINE OAT* .»«»«...»..................».«..,....,....
CAL 10 NUNBERI 98 ENGINE TYPE AND MODEL: J52 -
SERIAL NUMBER:
RATED THRUST: 8500.
ENGINE TOTAL TINE! 310. MRS
TINE SINCE HOT SECTION OVERHAUL: 310. MRS
TIME SINCE!
Nl COMPRESSOR OVERHAUL: 310. MRS
N2 COMPRESSOR OVERHAUL: 310. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE H011LE GUIDE VANE OVERHAUL: 310. HRS
NI TURBINE OVERHAUL: 310. HRS
N2 TURBINE OVERHAUL) 310. HRS
FUEL H/C RATIO: 1.970
FUEL: JP-S
OPERATIONAL DATA *««»»«»««»«*«»«»««»«»»««»«*
INLET AIR TEMPERATURE, DEGREES F: START 86.00 FINISH 85.50
ATMOSPHERIC PRESSURE: START 30.14 FINISH 30.14
INLET AIR HUMIDITY, LBS H20/LB AIRl 0.0120
RELATIVE HUMIDITY: 46.00 PERCENT
SAMPLE LINEl TEMPERATURE, DEGREES C: 93.00, FLOW RATE, LITERS/MINI -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 8
COMMENTS:
H/C CAL ESTIMATED
SMOKELESS COMBUSTOR CAN
;l)39
CLOCK
TINE
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
5
5
0
61
84
85
85
96
POWER
PERCENT
RATED
T.O.
5
5
0
63
84
85
85
96
POWER
PERCENT
RATED
T.O.
5
5
HORSEI
63
84
85
85
96
TEST
MODE
5/ 0
6/ 5
\t 6
2/ I
11 I
a/ 7
9/ 8
101 9
EXHAUST
GAS
TEMP
DEGREES F
500.00
500.00
-0.00
865.00
1009.00
1015.00
1010.00
1120.00
MASS EMI
CO
LB/IK
LB FUEL
62.06
75.06
58.49
2.90
1.78
1.71
1.63
1.44
CO
POWER ENGINE MEASURED GAS GEN CALC COMPRESSOR ENGINE TURBINE
THRUST, LBS PERCENT SPEED FUEL AIR FLOW F/A DISCHARGE PRESSURE INLET
OR RATED RPM FLOW IB/SEC TEMP RATIO TEMP
SHP T.O. Nl N2 LB/HR DEGREES F EPR DEGREES F
470.00 5 -0.00 6870.00 685.00 -0.00 -0.000000 -0.00 -0.00 -0.00
480.00 5 -0.00 6910.00 700.00 -0.00 -0.000000 -0.00 -0.00 -0.00
-0.00 0 -0.00 -0.00 -0.00 -0.00 -0.000000 -0.00 -O.OC -0.00
5360.00 63 -0.00 10958.00 4050.00 -0.00 -0.000000 -0.00 1.9K -0.00
7210.00 84 -0.00 11565.00 5515.00 -0.00 -0.000000 -0.00 -0.00 -0.00
7240.00 85 -0.00 11570.00 5550.00 -0.00 -0.000000 -0.00 -0.00 -0.30
7240.00 85 -0.00 11569.00 5540.00 -0.00 -0.000000 -0.00 -0.00 -0.00
8225.00 96 -0.00 11890.00 6455.00 -0.00 -0.000000 -0.00 -0.00 -0.00
EXHAUST CO CO THC NO NO Ml ALOEHVOES SMOKE PARUCULATES
GAS (ORY1 2 (DRVI (DRY) 2 X
PRESSURE PPMV IORYI PPHV PPHV (DRY) IORY)
PSIA
-0.00
-0.00
-0.00
29.00
40.20
40.40
40.40
46.20
MASS EMI
HC
LB/IK
LB FUEL
23.52
28.45
26.59
1.20
-0.00
-0.00
0.22
0.16
LB/IKITH-HR
90.
109.
POWER-HR 0
2.
1.
1.
I.
1.
444
467
R THRUST-HR
194
363
307
245
129
PERCENT V
340.00
340.00
330.00
32.00
23.00
22.00
21.00
20.00
MASS EMI MASS EMI
N02 C02
LB/IK LB/IK
LB FUEL LB FUEL
2.10 2982.50
2.90 2948.53
2.33 2979.67
1.64 3136.68
1.27 3141.72
1.27 3141.85
1.40 3141.36
1.18 3141.81
CO
2
1.04 225
0.85 225
1.07 262
2.20 23
2.58 -0
2.58 -0
2.58 5
2.78 4
MASS EMI
NO
LB/IK
LB FUEL
1.50
1.81
2.91
8.20
10.82
10.18
9.55
10.63
THC
LB/IKITH-HR LB/IKITH-HR
4346.828
4299.941
BASIS NOT CALCULAB
2370.067
2403.134
2408.459
2403.747
2465.701
34.779
41.489
LE«««
0.903
-0.000
-0.000
0. 170
0.129
.00 5.
.00 5.
.00 10.
.00 54.
.00 85.
.00 80.
.00 75.
.00 90.
MASS EMI
NOX
LB/IK
LB FUEL
14.69
1.78
1.43
8.50
10.18
9.93
9.93
10.63
NO
00
00
00
00
00
00
00
00
MASS
CO
PPMV PPMV
7
B
e
11
10
10
11
10
EMI
LB/H8
42.
52.
-0.
11.
9.
9.
9.
9.
51
54
00
76
83
46
02
29
LB/IKITH-HR
2.
2.
6.
8.
7.
7.
B.
185
644
194
277
807
305
345
.00 49.00 7.
.00 4.90 -0.
.00 4.90 3 .
.00 57.00 -0.
.00 60.00 0.
.00 78.00 -0.
.00 78.00 -0.
.00 90.00 0.
MASS EMI MASS FHI
HC NO 2
LB/HR LB/HR
16.11 1.44
19.91 2.03
-0.00 -0.00
4.84 6.64
-0.00 7.02
-0.00 7.07
1.23 7.76
1.06 7.63
Nn
2
40 -0.
00 -0.
00 -0.
00 -0.
10 -0.
00 -0.
oo -o.
10 -0.
MASS EMI
C02
LB/HR
2043.01
2063.97
-0.00
12703.56
17326.60
17437.24
17403.13
202B0.39
NO
X
00 -0.00
00 -0.00
00 -0.00
00 -0.00
oo -o.oo
00 -0.00
00 -0.00
00 -0.00
MASS EMI MASS
EMI
NO NOX
LB/HR LB/HR
1.03 10.
1.27 1.
-0.00 -0.
33.20 34.
59. 68 56.
56.52 55.
52.89 55.
68.64 6B.
06
24
00
41
16
11
00
64
LB/IKITH-HR LB/IKITH-HR
3.059
4.231
1.239
0.974
0.976
1.071
0.927
21.410
2.591
6.419
7.790
7.612
7.597
B. 345
IV-338
-------
OATEl 7/12/71
TEST ORGANIZATION!
ENGINE SUPPLIER!
SCOTT/NORFOLK
NORFOLK MAS
ENGINE 04F»
CAL 10 NUMBER: 100
ENGINE TYPE AND MODEL: J57 - PIO
SEOUL NUHBFR:
RATED THRUST: 10500.
ENGINE TOTAL TINE: 3395. MRS
TINE SINCE HOT SECTION OVERHAUL: 1074. HRS
TINE SINCEI
Nl COMPRESSOR OVERHAUL: 1074. HRS
N2 COMPRESSOR OVERHAUL! 1074. HRS
CONBUSTOR CAN REPLACEMENT: 1074. HRS
FIRST STAGE NOZILE GUIDE VANE OVERHAUL: 1074. HRS
Nl TURBINE OVERHAUL: 1074. HRS
N2 TURBINE OVERHAUL: 1074. HRS
FUEL H/C RATIO: 1.970
FINISH
FINISH
76.00
30.06
FUEL: JP-S
OPERATIONAL DATA ««»
INLET AIR TENPERATUREi DEGREES F: START 73.50
ATMOSPHERIC PRESSURE: START 30.03
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0134
RELATIVE HUMIDITY: 75.00 PERCENT
SAMPLE LINEl TEMPERATURE, DEGREES C: 115.00, FLOW RATE, LITERS/HIN: -0.00
SAMPLE LINE TRANSPORT TIME. SEC: -0.00
NUMBER OF TESTS: 8 '
COMMENTS:
H/C CAL ESTIMATED
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POKER
PERCENT
RATED
T.O.
0
5
4
60
0
«0
B«
B9
POWER
PERCENT
RATED
T.O.
0
5
4
60
0
90
19
89
POWER
PERCENT
RATED
T.O.
TEST
MODE
I/ 0
ll/ 1
12/11
13/12
14/13
15/14
10/15
16/10
EXHAUST
GAS
TEMP
DEGREES F
-0.00
543.00
543.00
910.00
1040.00
1095.00
IOB5.00
1070.00
MASS EMI
CO
LB/1K
LB FUEL
87.18
88.26
86.66
3. 78
2.61
2.20
2.17
2.2B
CO
POWER ENGINE MEASURED GAS GEN CiLC COMPRESSOR ENGINt ruHBINE
THRUST, LBS PERCENT SPEED FUEL AIR FLOW F/A DISCHARGE PRESSURE INLET
OR RATED RPM FLOW LB/SEC TEMP RAMU TEMP
SHP T.O. Nl N2 IB/MR DFGRFES F [PR DEGREES F
-0.00 0 -0.00 -0.00 -0.00 -0.00 -0.000000 -0.00 -0.00 -0.00
540.00 5 21B5.00 5912.00 1100.00 -0.00 -0.000000 -0.00 -0.00 -0.00
510.00 4 2160.00 5874.00 1080.00 -0.00 -0.000000 -0.00 -0.00 -0.00
6320.00 60 5445.00 8748.00 5300.00 -0.00 -0.000000 -0.00 1.8° -0.00
-0.00 0 5780. OC 9050.00 6900.00 -0.00 -0.000000 -0.00 2.20 -0.00
9540.00 90 5935.00 9228.00 7770.00 -0.00 -0.000000 -0.00 2.37 -0.00
9450.00 89 5935.00 9230.00 777C.OO -0.00 -0.000000 -0.00 -0.00 -0.no
9420.00 89 5930.00 9240.00 7700.00 -0.00 -0.000000 -0.00 -O.OC -0.00
EXHAUST CO CO THC NO NO NO ALDEHYDES SMOKE PARI ICULAFES
GAS IORY) 2 IORYI (DRY) 2 X
PRESSURE PPHV (CRY) PPNV PPMV IORYI IORYI
PSIA
-0.00
-0.00
-0.00
26.50
35.70
40.90
40.80
40.70
MASS EMI
HC
LB/1K
LB FUEL
90.25
84.64
88.50
-0.00
-0.00
-0.00
-0.00
-0.00
IB/IK«TH-HR
HORSEPOWER-MR OR THRUST-HR
5
4
60
HORSEI
90
89
89
179.
183.
3.
POWER-HR 0
1.
1.
1.
796
523
169
R THRUST-HR
789
785
862
PERCENT V
675.00
645.00
645.00
42.00
34.00
30.00
29.00
31.00
MASS EMI MASS EMI
N02 C02
LB/IK Lfl/lK
LB FUEL LB FUEL
1.06 2759.96
0.67 2773.63
0.66 2765.58
0.59 3138.59
0.76 3140.42
0.60 3141.07
0.49 3141.11
0.36 3140.94
cn
2
1.36 1220
1.29 1080
1.31 1150
2.22 -0
2.60 -0
2.73 -0
2.67 -0
2.72 -0
MASS EMI
ND
LB/IK
LB FUEL
1.06
1.10
1.08
5.91
7.58
8.06
7.87
7.61
THC
LB/1KITH-HR LB/IKITH-HR
.00 5
.00 4
.00 4
.00 40
.00 60
.00 67
.00 64
.00 63
MASS EMI
NOX
LB/IK
LB FUEL
2.12
1.10
1.08
5.32
7.07
7.82
7.87
7.71
PPMV
.00 5
.90 3
.90 3
.00 4
.00 6
.00 5
.00 4
.00 3
MASS EMI
CO
LB/HR
-0.00
97.09
93.60
20.03
18.03
17. C7
16.87
17.54
NO
LB/1KITH-HR
.00
.00
.00
.00
.00
.00
.00
.00
PPMV
10.00 -0
4.90 9
4.90 -0
36.00 1
56.00 1
65.00 0
64.00 -0
64.00 -0
MASS EMI MASS EMI
HC
LB/HR
-0.00
93.11
95.57
-0.00
-0.00
-0.00
-0.00
-0.00
NO
N02
LB/HR
-0.00
0.74
0.72
1.13
5.23
4.67
3.82
2.79
2
.00 -0.
.10 -0.
.00 -0.
.30 -0.
.20 -0.
.80 -0.
.00 -0.
.00 -0.
MASS EMI
C02
LB/HR
-0.00
3051.00
2986.83
16634.50
2I66H.87
24406.13
24406.45
24185.26
so
X
no -0.00
00 -0.00
00 -0.00
00 -0.00
00 -0.00
00 -0.00
oo -o.oo
00 -0.00
MASS EMI MASS
EMI
NO NOX
LR/HR LB/HR
-0.00 -0.
1.21 1.
1.17 1.
31.33 26.
52.28 48.
62.62 60.
61.16 61.
58.56 59.
00
21
17
20
79
75
16
49
LB/IKITH-HR Lfl/lK«TH-HR
BASIS NOT CALCULABLE*"
5649.992
5856.520
2632.042
BASIS NOT CALCULAB
2558.295
2582.693
2567.438
172.421
187.402
-0.000
ILE«««
-0.000
-0.000
-0.000
2
2
4
6
6
6
.244
.290
.958
.564
.472
.217
1.
1.
0.
0.
0.
0.
374
402
496
490
404
296
2.244
2.290
4.462
6.368
6.4T2
6.315
IV-339
-------
DATE: 7/15/71
TEST ORGANIZATION! SCOTT/NORFOLK
ENGINE SUPPLIER: NORFOLK HAS
ENGINE DATA «»««««««««««
CAL 10 NUMBER! 103 ENGINE TYPE AND MODEL: J57 - PIO
SERIAL NUMBER:
RATED THRUST: 10500.
ENGINE TOTAL TIMEI 337. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCEl
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMRUSTOR CAN REPLACEMENT: 0. MRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO: 1.970
FINISH
FINISH
83.50
29.66
FUEL: JP-5
OPERATIONAL OATA «««««»««««
INLET AIR TEMPERATURE, DEGREES F: START 83.00
ATMOSPHERIC PRESSURE: START 29.05
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0114
RELATIVE HUMIDITY: 4.70 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 98.00, FLOU RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME. SEC: -0.00
NUMBER OF TESTS: 4
COMMENTS:
H/C CAL ESTIMATED
ICK
ME
0.00
0.00
0.00
0.00
TEST
MODE
I/ 0
11 1
3/ 2
4/ 3
POKER
THRUST ,LBS PERCENT
OR RATED
SHP
-0.00
6076.00
8063.00
-0.00
T.O.
0
57
76
0
ENGINE
SPEED
RPN
Nl
-0.00
5465.00
5800.00
-0.00
N2
5957.00
8915.00
9215.00
9401.00
MEASURED
FUEL
FLOW
LB/HR
-0.00
5130.nO
6630.00
-0.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
FPR
-O.OC
1.79
2.09
-0.00
TURBINE
INLET
IEMP
DEGRFES F
-0.00
-0.00
-0.00
-0.00
.ii/,9
POKER EXHAUST
PERCENT GAS
RATED TEMP
T.O. DEGREES F
0
57
76
0
-0.00
940.00
1050.00
-0.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
23.40
32.30
-0.00
CO
(DRY)
PPNV
5B2.00
53.00
34.00
35.00
CO
2
I DRY)
PERCENT
1.00
2.10
2.46
2.64
THC
(DRY)
PPMV
583.00
7.00
2.00
2.00
NO
IORYI
PPMV
11.00
36.00
68.00
79.00
NO
2
(DRY)
PPHV
2.00
r.oo
4.00
4.00
ALDEHYDES SMOKE PARTICULATES
IDRYI
PPMV
7.00
39.00
61.00
81.00
8.90
1.00
0.30
2.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POUER
PERCENT
RATED
T.O.
0
57
76
0
MASS EMI
CO
LB/1K
LB FUEL
104.32
5.04
2.76
2.65
MASS EMI
HC
LB/IK
LB FUEL
59.85
0.38
0.09
0.09
MASS EMI
N02
LB/IK
LB FUEL
0.59
1.09
0.53
0.50
MASS EMI
C02
LB/IK
LB FUEL
2816.41
3135.57
3139.93
3140.12
MASS EMI
NO
LB/IK
LB FUEL
3.24
5.93
9.07
9.32
MASS EMI
NOX
LB/IK
LB FUEL
2.06
6.09
B. 14
10. or
MASS EM
CO
LB/HR
-0.00
25.84
18.31
-C.OO
MASS EMI
HC
LB/HR
MASS EMI
NO 2
LB/HR
MASS EMI
CU2
LB/HR
MASS EHI
NU
LH/HR
MASS FNI
NOX
LB/HR
-0.00
1.95
0.62
-0.00
-0.00
5.61
3.54
-0.00
-0.00
16085.45
20817.73
-0.00
-0.00
30.4J
60.16
-0.00
-0.00
31.23
53.96
-0.00
POWER CO
PERCENT
RATED LB/lKtTH-HR
T.O.
CO
2
LB/1KKTH-HR
THC
LB/IKHTH-HR
HORSEPOrfER-HK OR THRUST-HR BASIS NOT CALCULABLE***
57 4.252 2647.375 0.322
76 2.271 2581.885 0.077
HORSEPOHER-HR OR THRUST-HR BASIS NOT CALCULABLE***
NO
L8/1HHTH-HR
5.008
7.461
LB/IKDTH-HH
0.923
0.439
NO
X
I.B/IKHTH-HR
5.140
6.693
IV-340
-------
DATE: 7/16/71
TEST ORGANIZATION! SCOTT/NORFOLK
ENGINE SUPPlled! NORFOLK NAS
ENGINE DATA »»»««»»«»»«»»«
C»L 10 NUMBER: 105 ENGINE TYPE AND MODEL:
J57 - P10
SERIAL NUMBER:
P606907
RATED THRUST: losoo.
ENGINE TOTAL TIME: 3*15. MRS
TINE SINCE MOT SECTION OVERHAUL: 586. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 586. HRS
NZ COMPRESSOR OVERHAUL: 536. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOllLl GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: 586. HRS
N2 TURBINE OVERHAUL: 586. HRS
FUEL H/C RATIO: 1.970
FINISH
FINISH
84.50
29.87
FUEL: JP-5
OPERATIONAL DATA «««»»»«
INLET AIR TEMPERATURE, DEGREES F: START 84.00
ATMOSPHERIC PRESSURE: START 29.87
INLET AIR HUMIDITY, LBS H20/LB AIRI 0.0167
RELATIVE HUMIOITTl 67.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 110.00, FLOW RATE. LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 4
COMMENTS:
H/C CAL ESTIMATED
,623
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
4
57
75
89
POKER
PERCENT
RATED
T.O.
4
57
75
89
PONER
PERCENT
RATED
T.O.
4
57
75
89
TEST
MODE
ll/ 0
13/11
14/13
15/14
EXHAUST
GAS
TEMP
DEGREES F
573.00
885.00
990.00
1075.00
MASS EMI
CO
LB/IK
18 FUEL
89.93
3.44
2.21
1.43
POWER
THRUST, LBS PERCENT
OR RATED
SHP
430.00
6080.00
7940.00
9420.00
EXHAUST
GAS
PRESSUR
PSIA
-0.00
24.00
32.40
39.00
MASS EMI
HC
LB/IK
Lfl FUEL
99.52
0.25
0.09
0.08
CO
LB/1KITH-HR
221.
2.
1.
1.
688
846
797
165
T.O.
4
57
75
89
CO
ENGINE
SPEED
«PM
Nl
2150
5500
5820
6060
.00
.00
.00
.00
N2
5900.00
8921.00
9218.00
MEASURED GAS GEN
FUEL AIR FLQM
FLOW Lfl/SF.C
LB/HR
1060.00 -0.00
5030.00 -0.00
6450.00 -0.00
9455.00 7680.00 -0.00
CO
IORYI
E PPM
V
(OR
THC NO NO
2 IORYI IORYI 2
Y)
PERCENT V
590.00
36.00
27.0
0
20.00
MASS EMI
Nf>2
LB/IK
LB FUEL
0.71
0.47
0.40
0.35
CO
2
LB/IKMH-HR
6730.273
2596.424
2551.398
2561.676
MASS
1
2
2
2
EMI
C02
LB/IK
LB FUEL
2730.
3138.
3140.
3142.
21
42
79
at
PPMV PPMV IDRVI
PPMV
.14 1140. 00 7.00 2.90
.09
.44
.80
MASS EMI
NO
LB/IK
LB FUEL
1.75
4.71
5.79
7.86
THC
LB/Uf TH-HR
245.324
0.211
0.076
0.067
4.65 30.00 3.00
2.00 43.00 3.00
2.00 67.00 3.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
NO
X
IDRYI
PPMV
7.00
36.00
56.00
J5.00
COMPRESSOR ENGINF
DISCHARGE PRESSURE
TEMP KATIO
DEGREES
-0.00
-0.00
-0.00
-0.00
F EPR
-0.00
1.81
2.10
2.12
ALDEHYDES SMOKE
IS. 90
1.50
1.10
0.20
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS
NOX CO
LB/1K LB/HR
L8 FUEL
1.75 95.33
5.65 17.31
7.54 14.27
8.80 10. 9r
NO
HC
LB/HR
105.49
1.28
0.61
0.63
MO
2
LB/lK«fH-HR LB/IKITM-HR
4.320
3.896
4.700
6.408
1.790
0.190
0.328
O.?fl7
NO 2
LB/HR
CO 2 NO
IU9BINE
INLET
TEMP
DEGREFS f
-0.00
-0.00
-0.00
-0.00
PART ICULATES
-0.00
-0.00
-0.00
-0.00
EPI MASS EMI
NOX
LB/HR LB/HR LB/HR
0.77 2894.02 1.
2.37 15
7B6.26 21.
2.60 20258.10 17.
2.70 24130.99 60.
86 I.B6
69 28.41
32 48.60
16 67.57
r»n
X
LB/IKHTM-HR
4.320
4.675
6.122
7.17]
IV-341
-------
DATf: 7/ 6/71
TEST ORGANIZATION) SCOTT/NORFOLK
ENGINE SUPPLleRl PRATT AND WHITNEY
ENGINE DATA
CAL ID NUMBER: loa
ENGINE TYPE AND MODEL: J57 - P10
SERIAL NUMBER:
RATED THRUST: 10500.
ENGINE TOTAL TIMEl 3509. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCEI
NI COMPRESSOR OVERHAUL: o. MRS
N2 COMPRESSOR OVERHAUL: 0. MRS
COMBUSTOR CAN REPLACEMENT: 0. MRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. MRS
Nl TURBINE OVERHAUL: 0. MRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.970
FUEL I JP-5
OPERATIONAL DATA «»»**««****««
INLET AIR TEMPERATURE, DEGREES F: START 78.00 FINISH 73.00
ATMOSPHERIC PRESSURE: START 29.84 FINISH 29.65
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.0195
RELATIVE HUMIDITY: 92.00 PERCENT
SAMPLE LINEl TEMPERATURE, DEGREES C: 98.80, FLOW RATE, LITERS/HIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 4
COMMENTS:
H/C CAL ESTIMATED
PROBE- 1 HOLE JURY RIG
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
r.o.
3
60
75
92
POWER
PERCENT
RATED
T.O.
3
60
75
92
POWER
PERCENT
RATED
T.O.
3
60
75
92
TEST POWER ENGINE MEASURED GAS GEN CALC COMPRESSOR ENGINE TURBINE
MODE THRUST.LBS PERCENT SPEED FUEL AIR FLOW F/A DISCHARGE PRESSURE INLET
OR RATED RPM FLOW LB/SEC TEMP RATIO TEMP
SHP T.O. Nl N2 LB/HR DEGREES F EPR DEGREES F
It 0 420.00 3 2140.00 5897.00 1100.00 -0.00 -0.000000 -0.00 -0.00 -0.00
Z/ 1 6334.00 60 5420.00 8893.00 5187.00 -0.00 -0.000000 -0.00 1.84 -0.00
3/ 2 7916.00 75 5780.00 9147.00 6390.00 -0.00 -0.000000 -0.00 2.08 -0.00
4/ 3 9675.00 92 6020.00 9405.00 7770.00 -0.00 -0.000000 -0.00 2.35 -0.00
EXHAUST EXHAUST CO CO THC NO NO NO ALDEHYDES SMOKE PART ICULATES
GAS GAS IDRV) 2 (DRY) (DRY) 2 X
TEMP PRESSURE PPMV ICRY) PPMV PPMV IORVI (DRY!
DEGREES F PSIA
573.00 -0.00
890.00 25.00
980.00 32.00
1080.00 39.90
MASS EMI MASS EMI
CO HC
LB/1K LB/U
LB FUEL LB FUEL
92.39 106.62
5.08 1.92
2.66 1.42
1.88 1.18
CO
LB/1KITH-HR
241.974
4.163
2.148
1.510
PERCENT V
665.00 1
50.00 I
30.00 2
24.00 2
MASS FHI MASS EMI
N02 C02
LB/1K LB/1K
LB FUEL LB FUEL
1.14 2706.85
2.09 3131.27
1.46 3136.44
1.29 3138.35
CO
2
.24 1340.
.96 33.
.25 28.
.55 26.
MASS EMI
NO
LB/1K
LB FUEL
2.28
3.34
4.81
6.69
THC
LB/lKfTH-HR LB/IKHTH-HR
7089.355
2564.237
2531.814
2520.409
279.253
1.574
1. 148
0.944
PPMV PPMV
00 10.00 5.
00 20.00 12.
00 33.00 10.
20 52.00 10.
MASS EMI MASS F.MI
NOX CO
LB/1K LB/HR
LB FUEL
3.42 101.63
5.43 26.37
6.27 17.01
7.98 14.61
NO
LB/1MTH-HR
5.S77
2.735
3.882
5.373
00 15.
50 32.
00 43.
00 62.
MASS EMI
HC
LB/HR
117.29
9.97
9.09
9.13
NO
2
LB/1KHTH-H
2.988
1.710
1.176
1.033
00 2.00 -0
50 1.00 -0
00 0.30 -0
00 0.10 -0
MASS EMI MASS EMI
N02 C02
LB/HR LB/HR
1.26 2977.53
10.83 16241.87
9.31 20041.84
10.00 24384.96
NO
X
R LB/1K»TH-HR
9.965
4.445
5.058
6.406
.00 -0.00
.00 -0.00
.00 -0.00
.00 -0.00
MASS FMI MASS EMI
NO NOX
LB/HR LB/HR
2.51 3.7J
17.33 28.15
30.73 40.04
51.98 61.98
IV-342
-------
DATE: 7/20/71
TCST ORGANIZATION! SCOTT/NORFOLK
ENGINE SUPPLIER! NORFOLK NAS
ENGINE DAT* »*«»*»»»
cu 10 NUMBER: i»* ENGINE TYPE AND MODEL: JST - PIO
SERIAL NUMSER:
RATED THRUST: 10500.
ENGINE TOTAL MNE: SMI. MRS
TINE SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 0. MRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
HZ TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.970
FINISH
FINISH
76.00
29.16
FUELl JP-S
OPERATIONAL DATA *««»«»
INLET AIR TEMPERATURE. DEGREES F: START 79.00
ATMOSPHERIC PRESSURE: START 29.96
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.0154
RELATIVE HUMIDITY: 77.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 115.50, FLOW RATE, LITERS/HIM: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: *
COMMENTS:
ALL H/C CAL ESTIMATED
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
0
61
78
90
POWER
PERCENT
RATED
T.O.
0
61
78
90
POWER
PERCENT
RATED
T.O.
TEST
MODE
I/ 0
2/ 1
3/ 2
4/ 3
EXHAUST
GAS
TEMP
DEGREES F
-0.00
880.00
995.00
1070.00
MASS EMI
CO
LB/1K
LB FUEL
90.41
4. 28
2.55
2.18
POWER ENGINE
THRUST, LBS PERCENT SPEED
OR RATED RPM
SHP T.O. Nl N2
-0.00
6430.00
8218.00
9530.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
25.00
33.20
39.30
MASS EMI
HC
LB/1K
LB FUEL
102.68
0.16
0.04
0.02
0 -0.00 -0.00
61 5535.00 B92B.OO
78 5800.00 9218.00
90 6000.00 9415.00
MEASURED
FUEL
FLOW
LB/HR
-0.00
5120.00
6510.00
7560.00
GAS GEN
AIR FLOW
L8/SEC
-0.00
-0.00
-0.00
-0.00
CO CO THC NO NO
(DRY) 2 (DRY) IDRVI 2
PPMV IORYI PPHV PPMV IDRVI
PERCENT V PPNV
590.00 1.13 1170
45.00 2.10 3
33.00 2.59 1
30.00 2.75 0
MASS EMI MASS EMI MASS EMI
N02 C02 NO
IB/ IK LB/1K 16/lK
LB FUEL LB FUEL LB FUEL
0.4B 2720.76 2.27
0.78 3137.35 5.78
0.51 3140.40 6.72
0.48 3141.04 8.12
CO CO THC
2
LB/UITH-HR LB/1KITH-HR LB/1KITH-HR
HORSEPOWER-HR OR THRUST-HR
61 3.407
78 2.017
90 1.730
BASIS NOT CALCULABLE"*
2498.172 0.130
2487.712 0.035
2491.740 0.016
.00 9.
.00 37.
.00 53.
.49 68.
MASS EMI
NOX
LB/1K
LB FUEL
2.01
6.25
7.61
9.19
00 1.90
00 5.00
00 4.00
00 4.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
NO
X
IORYI
PPMV
8.00
40.00
60.00
77.00
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIO
DEGREES F EPR
-0
-0
-0
-0
.00
.00
.00
.00
-0.
1.
2.
2.
00
84
12
33
ALDEHYDES SMOKE
4
2
0
0
MASS EMI MASS EMI MASS EMI
CO HC N02
LB/HR LB/HR LB/HR
-0.00
21.91
16.58
16.49
-0.00
0.84
0.29
0.15
NO NO
2
LB/1K«TH-HR LB/1KITH-HR
4.
5.
6.
601
322
441
0.622
0.402
0.379
-o.oo
4.00
3.30
3.61
.10 -0
.00 -0
.90 -0
.50 -0
MASS FM1
C02
LB/HR
-o.no
16063.24
20444.01
23746.28
.00
.00
.00
.00
TURBINE
INLET
TFMP
DEGREES F
-0.00
-0.00
-O.OC
-0.00
PART ICULATES
-0.00
-0.00
-0.00
-0.00
MASS EMI M«SS EMI
NU NOX
LB/HR LK/HR
-0.
29.
43.
61.
00 -0.00
59 31.99
73 49.51
38 69.51
NO
X
LB/IK«TM-HR
4.974
6.025
7.2V4
IV-343
-------
0«TEI T/ZZ/T1
TEST ORGANIZATION: SCOTT/NORFOLK
ENGINE SUPPLIER! NORFOLK NAS
ENGINE DATA ».............«.....«.......
CAL ID NUMBER! 145 ENGINE TYPE »NO MODEL: J57 - PIO
SERUL NUMBER:
P604897
RATED THRUST: 10500.
ENGINE TOTAL TINEl 41*6. MRS
TINE SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCEl
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL! 0. HRS
NI TURBINE OVERHAUL: o. HRS
HI TURBINE OVERHAUL: o. HRS
FUEL H/C RATIO:
.970
FINISH
FINISH
BO.00
30.14
FUEL: JP-J
OPERATIONAL DATA *«»*»
INLET AIR TEMPERATURE. DEGREES F: START 7ft.00
ATMOSPHERIC PRESSURE: START 30.12
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.0127
RELATIVE HUMIDITY: 59.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 108.90. FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TINE, SEC: -0.00
NUMBER OF TESTS: 4
COMMENTS:
H/C CAL ESTIMATED
CLOCK
TIME
-O.OD
-0.00
-0.00
-0.00
TEST
MODE
It 0
If 1
3/ 2
*/ 3
POKER
THRUST. LBS
OR
SHP
470.00
6185.00
6161.00
9907.00
PERCENT
RATED
T.O.
4
%n
77
90
ENGINE
SPEED
RPM
Nl N2
2135.00 5926.00
5465.00 8660.00
5600.00 9173.00
6010.00 93BI.OO
MEASURED
FUEL
FLOW
LB/HR
1070.00
5050.00
6510.00
7600.00
GAS GEN
AIR FLOW
IB/SEC
-0.00
-0.00
-0.00
-0.00
CALC COMPRESSOR ENGINE
F/A DISCHARGE PRESSURE
TEMP RATIO
DEGREES F EPR
-0.00
-0.00
-0.00
-0.00
-0.00
1.61
2.11
2.31
TURBINE
INLET
TEMP
OFGREES F
-0.00
-0.00
-0.00
-0.00
POKER
PERCENT
RATED
T.O.
4
58
77
90
EXHAUST
GAS
TEMP
DEGREES F
575.00
919.00
1040.00
1120.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
24. 3O
33.10
39.10
CO
IORVI
PPMV
620.00
58.00
39.00
32.00
CO
2
(DRV)
PERCENT V
1.21
1.96
2.29
2.56
THC
IORVI
PPMV
1240.00
13.00
4.00
2.00
NO
IDRV)
PPMV
10.01
28.0
50.01
68.01
NO
2
I DRY I
PPMV
2.90
3.00
3.00
3.00
NO
X
(DRY)
PPMV
12.90
31.00
53.00
71.00
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POKER
PERCENT
RATED
T.O.
4
58
77
90
MASS EMI
CO
U/IK
LB FUEL
es.ee
S.90
3.40
2.50
MASS EMI
HC
LB/1K
LB FUEL
101.81
0.76
0.20
0.09
MASS EMI
N02
LB/1K
LB FUEL
0.68
0.50
0.43
0.38
MASS EMI
CO 2
L6/IK
LB FUEL
2725.56
3133.17
3138.63
3140.35
MASS EHI
NO
LB/IK
LB FUEL
2.35
4.68
7.16
8.72
MASS FM1
NOX
LB/IK
LB FUEL
3.04
5.18
7.59
9.10
MASS EMI
CO
LB/HR
95.11
29.80
22.15
18.99
MASS EMI
HC
LR/HR
108.94
3.83
1.30
0.68
MASS EMI
N02
LB/HR
0.73
2.53
2. on
2.92
MASS EMI
CO 2
LB/HR
2916.34
15822.52
20432.48
23866.68
MASS Efl
NO
LB/HR
2.52
23.63
46.64
66.27
MASS EMI
NOX
LB/hR
3.25
26. 16
49.44
69.20
POWER
PERCENT
RATED
T.O.
4
58
77
90
CO
LB/lKiTH-HR
202.393
4.818
2.714
1.997
LB/IKITH-HR
6204.984
2558.209
2503.674
2510.432
THC
LB/1K«TH-HR
231.785
0.618
0.159
0.071
NO
LB/l«»rH-HR
5.361
3.821
5.715
6.971
LB/1KHTH-HR
1.555
0.409
0.343
0.308
LB/1KHTH-HR
6.916
4.230
6.058
7.279
IV-344
-------
DATE: 0/70/71
TEST ORGANIiATION: S H R 1 KELLY
ENGINE SUPPLIER! ' USAF. KELLY AFB
ENGINE DATA
OL 10 NUMBER!
ENGINE TYPE AND MODEL 1 J-T9
SERIAL NUMBER: GE 418312*
RATED THRUST: 10350.
ENGINE TOTAL TIME: 1*93. HRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: o. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL H/C RATIO:
I.99S
FINISH
FINISH
89.00
29.34
FUEL: jp-4
OPERATIONAL DATA *«
INLET AIR TEMPERATURE, DEGREES F: START B9.00
ATMOSPHERIC PRESSURE: START 29.34
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.0176
RELATIVE HUMIDITY: 52.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 150.00. FLOW RATE. L1TEKS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.50
NUMBER OF TESTS: 5
COMMENTS:
AIRFLOW DATA NOT AVAILABLE FOR NI LESS THAN 6000. F/A CALCULATED FRDN EXHAUST
CnMP.i NO2 DATA OBTAINED BY SUBTRACTION
42.50
ELAPSED
TIME
0.0
7.15
19.00
29.00
40.30
TEST
MODE
7/ 0
3/ 7
21 3
I/ 2
7/ 1
POWER
THRUST. LBS PERCENT
OR RATED
SHP T.O.
260.00 2
10080.00 97
9250.00 69
6140.00 59
290.00 2
ENI
SI
1
NI
5030.00
7690.00
7360.00
6830.00
5015.00
SPEED
RPM
N2
-0.00
-0.00
-0.00
-0.00
-0.00
MEASURED GAS GEN
FUEL AIR FLOW
FLOW LB/SEC
LB/HR
1200.00
BB50.00
8100.00
5200.00
1150.00
46.30
163.40
[56.00
125.50
44.40
CALC COMPRESSOR ENGINE
F/A DISCHARGE PRESSURE
TEMP RATIO
DEGREES F EPR
0.007200
0.015000
0.014400
0.011500
0.007200
-0.00
-0.00
-0.00
-0.00
-0.00
-o.on
-o.oo
-0.00
-o.oo
-0.00
TURBINE
INLET
TEKP
OFGBEES f
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
2
97
89
59
2
EXHAUST
GAS
TEMP
DEGREES F
666.00
1165.00
1142.00
949.00
680.00
EXHAUST...
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
CO
IWETI
PPMV
317.00
-0.00
-0.00
-0.00
300.00
CO
2
IkET)
PERCENT V
1.45
-0.00
-0.00
-0.00
1.45
THC.
IWETI
PPMV
112.00
-0.00
-0.00
-0.00
80.00
NO
(HEM
PPMV
4.00
-0.00
-0.00
-0.00
a. oo
NO
2
IHET)
PPMV
6.00
-0.00
-0.00
-0.00
4.00
NO
X
IWET)
PPMV
10.00
-0.00
-0.00
-0.00
17.00
ALDEHYDES SMOKE PARTICULATES
-0.00
-0.00
-0.00
-o.oo
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
2
97
89
59
2
MASS EMI
CO
LB/1K
IB FUEL
42.42
0.20
0.20
0.20
40.28
MASS ENI
KC
LB/IK
LB FUEL
8.58
0.11
0.11
0.11
6.15
MASS EMI
N02
LB/IK
LB FUEL
1.32
0.33
0.33
0.33
O.B8
MASS EMI
C02
LB/IK
LB FUEL
3048.67
3138.25
3138.25
3138.25
3058.72
MASS E«l
NO
LB/IK
LB FUEL
0.88
0.33
0.33
0.33
1.76
MASS EMI
NOX
LB/IK
LB FUEL
2.20
0.66
0.66
0.66
2.65
MASS EM
CO
LB/HR
5C.90
1.77
1.62
1.04
46.32
MASS tMI
HC
LB/HR
10.30
1.01
0.93
0.59
7.07
MASS CHI
NO 2
LB/HR
MASS fMI
C02
LB/HR
MASS Erl
NO
LB/HR
MASS CM]
MIX
LB/HR
I.SB
2.90
2.66
1.71
1.01
3658.41
27773.".8
25419.80
16318.88
3517.12
1.06
2.90
?.6h
1.71
?.03
2.64
5.01
5.31
3.41
3.04
POWER
PERCENT
RATED
7.0.
2
97
89
59
2
CO
LB/lKtTH-HR
195.782
0.175
0.175
0.169
159.718
CO
2
LB/1KITH-HR
14070.805
2755.306
2748.086
2657.799
12129.383
THC
LB/1KITH-HR
39.617
0.100
0.100
0.097
24.393
NO
LB/lKfTH-HR
4.050
0.288
0.287
0.278
6.996
LB/IKfTH-HR
6.087
0.288
0.287
0.278
3.498
NO
X
LB/IKN TH-HR
10.145
0.576
0.575
0.556
10.494
IV-345
-------
DATE: 11 1/71
TEST ORGANIZATION! S W R I KELLY
ENGINE SUPPLIERl USAF, KELLY AFB
C»L ID NUMBER! IS ENGINE TYPE AND MODEL) J-79
SERIAL NUMBER: CE 434176
RATED THRUST: 10350.
ENGINE TOTAL TINEl 149;. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCEl
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
NZ TURBINE OVERHAUL: -0. HRS
FUEL H/C RATIO: 1.995
FINISH
FINISH
87.00
2V.il,
FUEL! JP-4
OPERATIONAL DATA »»**
INLET AIR TEMPERATURE, DEGREES H START Be.00
ATMOSPHERIC PRESSURE: START 29.26
INLET AIR HUMIDITY, LBS HJO/LB AIR: 0.0159
RELATIVE HUMIDITY: 53.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: ISO.00, FLOW RATE, LITERS/NIN:
SAMPLE LINE TRANSPORT TINE. SEC: 0.50
NUMBER OF TESTS: 5
COMMENTS'
F/A CALCULATION BASED ON EXHAUST COMPOSITION FOR INITIAL AND FINAL RUNS.
N02 DETERMINED BY SUBTRACTION HC FOR FIRST RUN STILL SLOWLY DECREASING AT END
OF MODE
ELAPSED
TIME
0.0
16.25
27.15
37.45
47.40
POWER
PERCENT
RATED
T.O.
2
64
91
97
2
POWER
PERCENT
RATED
T.O.
2
64
91
97
2
POWER
PERCENT
RATED
T.O.
2
64
91
97
2
TEST
MODE
11 0
I/ 7
2/ 1
3/ 2
7/ 3
EXHAUST
GAS
TEMP
DEGREES F
675.00
960.00
1135.00
1156.00
640.00
MASS EMI
CO
LB/IK
LB FUEL
51.89
3.77
2.10
1.66
46.71
CO
POWER
THRUST, LBS
OR
SHP
275.00
6650.00
9500.00
10100.00
300.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
20.33
0.05
0.0
0.0
4.73
PERCENT
RATED
T.O.
2
64
91
97
2
ENGINE
SPEED
Nl
RPM
N2
5060.00 -0.00
6910.00
7400.00
7660.00
5060.00
CO
IWETI
-0.00
-0.00
-0.00
-0.00
MEASURED GAS GEN
FUEL AIR FLOW
FLOW LB/SEC
LB/HR
1275.00 48.50 0.
5775.00 129.70 0.
8350.00 156.40 0.
8875.00 162.10 0.
1100.00 43.70 0.
CO THC NO NO
2 IWET) IWETI 2
PPMV IHET) PPMV PPMV (WEJI
PERCENT V
402.
44.
29.
23.
339.
MASS EMI
N02
LB/IK
LB FUEL
0.64
0.56
0.72
0.83
0.91
CO
2
00
00
00
00
00
MASS EMI
C02
LB/IK
18 FUEL
3001.57
3132.82
3135.57
3136.27
3052.50
LB/lKfTH-HR LB/lKiTH-HR LB
240.
3.
1.
1.
171.
576
270
850
456
265
13916.387
2720.609
2755.996
2755.879
11192.477
1.48 275
2.33 1
2.75 0
2.77 0
1.41 60
MASS EMI
NO
LB/IK
LB FUEL
1.70
5.48
7.39
B.29
2.49
THC
YlKiTH-HR
94.255
0.043
0.0
0.0
17.361
PPMV
.00 8.00 3.00
.00 39.00 4.00
.0 62.00 6.00
.0 70.00 7.00
.00 11.00 4.00
MASS EMI MASS EMI MASS
NOX CO HC
CALC
F/A
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP
DEGREES f
007300
012400
014800
015200
007000
NO
X
IWET)
PPNV
11.00
43.00
6R.OO
77.00
15.00
-0.
-0.
-0.
-0.
-0.
00
00
00
00
00
»ATIU
EPR
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES SMUKE
-0.
-0.
-0.
-0.
-0.
FMI MASS EMI
LB/IK 18/HR LB/HR
LB FUEL
2.33 66.16 25.
6.04 21.74 0.
8.11 17.57 0.
9.11 14.71 0.
3.39 51.38 5.
NO
92
28
0
0
21
NO
2
LB/lKiTH-HR LB/IKHTH-HR
7.864
4.761
6.496
7.280
9.128
2.949
n.488
0.629
0.728
3.319
N02
LB/HR
0.81
3.25
5.97
7.35
1.00
00 -0
00 -0
00 -0
00 -0
00 -0
MASS EMI
C02
LB/HR
3827.01
18092.05
26181.96
27834.39
3357.74
NO
X
.00
.00
.00
.00
.00
MASS
NO
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
EMI MASS EMI
NQX
LB/HU LB/HH
2.
31.
61.
73.
2.
16 2.97
66 34.90
71 67.68
53 80.89
74 3.73
LB/ IKOTH-HR
10.813
5.249
7.124
8.009
12.447
IV-346
-------
DATE: II 2/71
TEST ORGANIZATION! S W » I KELLY
ENGINE SUPPLIER) USAF, KELLY AFB
ENCINE 0«T»
CAL ID NUMBER:
ENGINE TYPE AND MODEL: J-T9
SERIAL NUMBER: GE-E418975
RATED THRUST: 10350.
ENGINE TOTAL TINE! 2075. HRS
TINE SINCE HOT SECTION OVERHAUL: 0. HRS
TINE SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: -0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE N022LE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL H/C RATIO: 1.995
FINISH
FINISH
89.00
29.26
FUEL I JP-4
OPERATIONAL DATA »«««««.««««..»«.«««..«.....
INLET AIR TEMPERATUREt DEGREES F: START 91.00
ATMOSPHERIC PRESSURE: START 29.26
INLET AIR HUMIDITY, IBS H20/LB AIR: 0.0153
RELATIVE HUMIDITY: 43.00 PERCENT
SAMPLE LINE: TENPERATUREi DEGREES C: 150.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: 0.50
NUMBER OF TESTS: 5
COMMENTS:
F/A CALCULATION BASED ON EXHAUST COMPOSITION FOR INITIAL AND FINAL RUNS.
N02 DETERMINED BY SUBTRACTION
ELAPSED
TINE
0.0
11.05
20.15
30.00
39.30
POWER
PERCENT
RATED
T.O.
3
9
88
59
3
POWER
PERCENT
RATED
T.O.
3
9
88
59
3
POWER
PERCENT
RATED
T.O.
3
9
88
59
3
TEST
MODE
T/ 0
3/ 7
21 3
I/ 2
7/ 1
EXHAUST
GAS
TEMP
DEGREES F
665.00
1157.00
1130.00
909.00
649.00
NASS ENI
CO
LB/1K
LB FUEL
46.92
1.61
3.20
3.46
39.39
CO
POWER
THRUST, L8S
OR
SHP
320.00
1000.00
9200.00
6150.00
340.00
EXHAUST
GAS
PRESSURE
PSIA
-o.oo
-0.00
-0.00
-0.00
-0.00
MASS EHI
HC
LB/1K
LB FUEL
a. 98
0.04
0.04
0.0
4.59
PERCENT
RATED
ENGINE
SPEED
RP
N
T.O. Nl
3 5050
9 7685
88 7380
59 6910
3 5060
CO
IWETI
PPNV
.00
.00
.00
.00
.00
CO
N2
-0.00
-0.00
-0.00
-0.00
-0.00
MEASURED GAS GEN
FUEL AIR FLOW
FLOW L8/SEC
LB/HR
1200.00 43.80
8775.00 161.50
8000.00 153.90
5150.00 12B. 10
1180.00 43.70
THC NO NO
2
(WET)
PERCENT
371.00
23.00
43.00
38.00
305.00
NASS ENI HASS
1.
2.
2.
2.
1.
ENI
53
05
68
19
51
(WET) (WET) 2
PPMV PPNV IWET)
V
124
1
1
0
62
HASS EMI
N02 C02
LB/1K LB/1K
LB FUEL LB FUEL
0.83 3040.
0.5B 3136.
0.61 3133.
0.60 3133.
0.64 3064.
CO
2
LB/1IHTH-HR LB/1KITH-HR
175.
14.
2.
2.
136.
963
135
783
898
720
11401.967
27520.438
2724.961
2623.933
10635.238
50
23
73
43
39
NO
LR/IK
LB FUEL
1.45
8.17
6.85
4.79
1.49
THC
LB/IKHTH-HR
33
0
0
0
15
.683
.352
.037
.0
.917
PPMV
.00 7.00 4.00
.00 71.00 5.00
.00 56.00 5.00
.0 32.00 4.00
.00 7.00 3.00
CALC
F/A
0.007600
0.015100
0.014400
0.011200
0.007500
NO
X
IWETI
PPNV
11.00
76.00
61.00
36.00
I0.no
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
RATIO
EPR
-0.00
-0.00
-0.00
-0.00
-O.OC
ALDEHYDES SMOKE
-0.00 -0.00
-0.00 -0
-0.00 -0
-0.00 -0
-o.oo -o
HASS ENI NASS ENI MASS EMI NASS EHI NASS [.11
NOX CO
LB/1K LB/HR
LB FUEL
2.29 56.31
8. 74 14.14
7.46 25.60
5.38 17.82
2.12 46.48
NO
HC
LB/HR
10.78
0.35
0.34
0.0
5.41
NO
2
L8/1KHTH-HR LH/1KMTH-HR
5.4D3
71.672
5.952
4.008
5.154
3.11ft
5.047
0.531
0.501
2.209
N02 C02
LU/HR LB/HR
1.00 3648.60
5.05 27520.44
4.B9 25069.82
3.08 16137.19
0.75 3615.98
NO
X
LB/1KITH-HR
8.570
76.720
6.484
4.501
7.363
.00
.00
.00
.00
NASS
NO
TURBINF
INLET
IEMP
DEGREES F
-o.no
-0.00
-0.00
-0.00
-0.00
PART ICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
EMI MASS EHI
NOX
LB/HA LB/HR
1.
71 .
54.
24.
1.
75 2.74
61 76.72
76 59.65
65 27.73
75 2.50
IV-347
-------
DATE: II 6/71
TEST ORGANIZATION: S W R I KELLY
ENGINE SUPPLIER: USAF, KELLY AFB
ENGINE DATA
CAL ID NUMBER:
17
ENGINE TYPE AND MODEL: J-79
SERIAL NUMBER: GF -,183128
RATED THRUST: 10350.
ENGINE TOTAL TINE: 2149. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TINE SINCE!
Nl COMPRESSOR OVERHAUL: 0. HRS
NZ COMPRESSOR OVERHAUL: -0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: -0. HRS
FUEL H/C RATIO: 1.995
FINISH
FINISH
B3.00
29.35
FUEL: jp-4
OPERATIONAL DATA ««»«»«*»«««»«»»»
INLET AIR TEMPERATURE, DEGREES F: START 80.00
ATMOSPHERIC PRESSURE: START 29.35
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.0167
RELATIVE HUMIDITY: 66.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 150.00, FLOW RATE, LITERS/MIN: 42
SAMPLE LINE TRANSPORT TIME, SEC: 0.50
NUMBER OF TESTS: 7
COMMENTS:
F/A CALCULATIONS BASED ON EXHAUST COMPOSITION FOR FIRST, FIFTH AND SEVENTH RUNS
N02 DETERMINED BY SUBTRACTION
ELAPSED
TIME
0.0
17.00
34.00
44.00
52.00
54.00
62.30
POWER
PERCENT
RATED
T.O.
2
99
92
60
2
98
2
POWER
PERCENT
RATED
T.O.
2
99
92
60
2
98
2
POWER
PERCENT
RATED
T.O.
2
99
92
60
2
98
2
TEST
NODE
7/ 0
3/ 7
2/ 3
I/ Z
7/ 1
3/ 7
7/ 3
EXHAUST
GAS
TEMP
DEGREES F
654.00
1158.00
1135.00
924.00
652.00
1160.00
654.00
MASS EMI
CO
LB/IK
LB FUEL
51.86
O.BB
2.08
3.62
45.47
0.90
43.13
CO
POWER ENGINE
THRUST, LBS
OR
SHP
230.00
10250.00
9620.00
6310.00
230.00
10200.00
245.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
HC
LB/U
LB FUEL
11.19
0.0
0.04
0.05
8.29
0.0
7.39
MEASURED
PERCENT SPEED
RATED
T.O. Nl
2 4965.00
99 7665.00
92 7380. OC
60 6880.00
2 5000.00
98 7665.00
2 5000.00
CO
IWETI
RPM
CO
2
PPMV IWET)
PERCENT
385.00
13.00
29.00
43.00
352.00
13.00
351.00
MASS EMI MASS EMI
N02 C02
LB/IK L8/1K
LB FUEL LB FUEL
1.11 3026.69
0.66 3137.49
0.71 3135.49
0.69 3133.06
1.27 3044.69
0.91 3137.46
1.21 3050.82
CD
2
1.43
2.96
2.78
2.37
1.50
2.88
1.58
N2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
THC
IWETI
PPMV
V
145.00
0.0
1.00
1.00
112.00
0.0
105.00
FUEL
FLOW
LB/HR
1175.00
8850.00
8200.00
5300.00
1170.00
8850.00
1175.00
NO
IWET
GAS GEN
AIR FLOW
LB/SEC
45.90
163.60
157.80
130.30
43.90
163.60
41.80
NO
1 2
0.
0.
0.
0.
0.
0.
0.
PPMV IWETI
4 .
71.
58.
32.
4.
74.
4.
MASS EMI MASS EMI
NO
LB/IK
NOX
LB/IK
PPMV
00 5.00
00 6.00
00 6.00
00 5.00
00 6.00
00 8.00
00 6.00
MASS EMI MASS
CO
LB/MR
HC
CALC
F/A
007100
015200
014400
011300
007400
015200
007800
NO
X
IWETI
PPMV
9.00
77.00
64.00
37.00
10.00
82.00
10.00
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIO
DEGREES F EPR
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -O.CC
-0.00 -0.00
-0.00 -0.00
TURUINE
INLET
TFMP
DFCRFES F
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES SMOKF PARTICULARS
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
-0.00 -0.00
EMI MASS EMI MASS EMI MASS EMI
LB/HR
NO 2 C02 Nil
LB/HR LB/Hft LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MASS EMI
NUX
LB/HR
LB FUEL LB FUEL
0.89
7.87
6.84
4.42
0.85
8.43
0.81
THC
LB/1KHTH-HR LB/1KITH-HH LB/1KITH-HR
264.
0.
1.
3.
231.
0.
206.
950
757
774
039
370
782
871
15462.453
2708.958
2672.663
2631.568
15488.191
2722.204
14631.484
57
0
0
0
42
0
35
.150
.0
.035
.040
.154
.0
.443
1.99
8.53
7.55
5.11
2.12
9.34
2.02
NO
LB/IKIT
4.
6.
5.
3.
4.
7.
3.
60.94
7.76
17.07
19.17
53.20
7.98
50.68
13.
0.
0.
0.
9.
0.
8.
14
0
34
26
70
0
68
NO
2
H-Hfl LB/1MTH-HR
522
793
829
714
318
312
H72
5.652
0.574
0.603
0.580
6.477
0.790
5.809
1.30 3556.36 1.04
5.88 27766.82 69.63
5.80 25711.02 56.08
3.66 16605.19 23.44
1.49 3562.28 0.99
8.06 27766.48 74.58
1.42 3584.71 C.95
NU
X
LB/1KHTH-HK
10.173
7.367
6.432
4.295
10.794
8.103
9.6HI
2.34
75.51
61.88
27. 10
2.48
82.65
2.37
IV-348
-------
O«TE; i/ 9/Ti
TEST ORGANIZATION: SCOTT/NORFOLK
ENGINE SUPPLIER! NORFOLK N«5
ENGINE DATA
CAL ID NUMBER 1 9T ENGINE TYPE «ND MODEL: TF30 P6C
RATED THRUST: 11500.
ENGINE TOTAL TINE I 1101. MRS
TINE SINCE HOT SECTION OVERHAUL: 851. HRS
TINE SINCEl
Nl CONPRESSOR OVERHAUL: 460. HRS
N2 CONPRESSOR OVERHAUL: 851. HRS
CONBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE Nome GUIDE VANE OVERHAUL: -o. HRS
Nl TURBINE OVERHAUL: 525. HRS
N2 TURBINE OVERHAUL: 7TT. HRS
SERIAL NUMBER:
652017
FUEL H/C RATIO: 1.970
FINISH
FINISH
76.00
30.04
FUEL" JP-5
OPERATIONAL DATA «««««»««««
INLET AIR TEMPERATURE. DEGREES F: START 76.00
ATMOSPHERIC PRESSURE: START 30.0*
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0167
RELATIVE HUMIDITY: 86.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 121.00, FLOW RATE, LITERS/KIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 4
COMMENTS:
H/C CAL ESTIMATED
CK TEST
ME MODE
0.00
0.00
0.00
0.00
I/
z/
3/
4/
0
1
2
)
POKER
THRUST, LBS PERCENT
OR RATED
SHP
-0.
5961.
7905.
11160.
00
00
00
00
T.O.
0
51
68
97
ENGINE
SPEED
RPM
Nl
-0.00
7725.00
8500.00
9697.00
H2
-0.00
12840.00
13451.00
14417.00
MEASURED
FUEL
FLOW
GAS GEN
AIR FLOW
LB/SEC
LB/HR
-0
3410
4550
6915
.00
.00
.00
.00
-0.
-0.
-0.
-0.
00
00
00
00
CALC COMPRESSOR ENGINE
F/A DISCHARGE PRESSURE
TEMP RATIO
DEGREES f EPR
-0.000000
-0.000000
-0.000000
-0.00
-0.00
-0.00
-0.00
-0.00
1.53
1.73
2.07
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POKER
PERCENT
RATED
T.O.
0
il
68
97
EIHAUST
GAS
TEMP
DEGREES f
-0.00
1483.00
1650.00
1990.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
15.50
21.40
31.40
CO
(DRY)
PPMV
815.00
20.00
13.00
11.00
CO
2
(DRY)
PERCENT V
1.84
2.42
2.62
2.88
THC
(DRY I
PPMV
-0.00
-0.00
-0.00
-0.00
NO
(DRY)
PPMV
-0.00
-0.00
-o.oo
-0.00
NO
2
(DRY)
PPMV
3.00
4.00
8.00
4.00
ALDEHYDES SHUKE PARTICULATES
I DRY I
PPNV
3.00
4.00
0.0
4.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POKER
PERCENT
RATED
T.O.
0
51
68
97
MASS ENI
CO
LB/1K
LB FUEL
84.89
1.65
0.99
0.76
MASS EMI
HC
LB/1K
LB FUEL
-0.00
-0.00
-0.00
-0.00
MASS EMI
N02
LB/1K
LB FUEL
0.51
0.54
1.00
0.4&
MASS EMI
C02
L8/IK
LB FUEL
3011.15
3141.93
3142.96
3143.32
MASS EMI
NO
IB/ IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
L8/1K
LB FUEL
0.51
0.54
0.0
0.46
MASS EM
CO
LB/HR
-0.00
5.64
4.52
5.28
MASS EMI
HC
LB/HR
MASS CMI
NO 2
LB/HR
MASS EMI
Cfl2
LB/HH
MASS EMI
NO
LB/HR
MASS EMI
NOX
LB/HR
0.00
-0.00
-0.00
-0.00
-0.00 -0.00
1.85 10713.17
4.5t> 14300.48
3.16 21736.08
o.oo
-o.oo
-o.oo
-c.oo
-o.oo
1.B5
0.0
3.16
POKER
PERCENT
RATED
T.O.
LB/lKiTH-HR
CO
2
L6/IKITH-HR
THC
LB/IKITH-HR
HORSEPOKER-HR OR THRUST-HR BASIS NOT CALCULABLE***
51 0.945 1797.344 -0.000
68 0.571 1809.043 -0.000
97 0.473 1947.677 -0.000
NO
LB/1KITH-HR
-0.000
-0.000
-0.000
LB/1KIITH-HR
0.311
0.577
0.283
NO
X
LB/lKITrt-HR
O.JM
0.0
0.2B3
IV-349
-------
0»TE: 7/ 9/M
TEST ORGANIZATION: SCOTT/NORFOLK
ENGINE SUPPLIER: NORFOLK NAS
ENGINE DATA »»»«««»«««*»»*»»»
C»L ID NUMBER: 11 ENGINE TYPE AND MODEL: TFSO P6C
RATED THRUST: 11500.
ENGINE TOTAL TIME: 0. HRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCEI
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
CONBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO: 1.970
SERIAL NUMBER:
FINISH
FINISH
86.90
30.05
FUEL: JP-S
OPERATIONAL DATA «««»
INLET AIR TEMPERATURE. DEGREES F: START 86.00
ATMOSPHERIC PRESSURE: START 30.oa
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0146
RELATIVE HUMIDITY: 55.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 126.00, FLON RATE, L1TERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS! 6
COMMENTS:
H/C CAL ESTIMATED
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
0
0
5
46
62
96
POWER
PERCENT
RATED
T.O.
0
0
5
46
62
96
POWER
PERCENT
RATED
T.n.
TEST
MODE
I/ 0
I/ I
I/ 1
2/ 1
3/ 2
4/ 3
EXHAUST
GAS
TEMP
DEGREES F
-0.00
-0.00
955.00
1465.00
1635.00
1990.00
MASS EMI
CD
LB/1K
LB FUEL
65.56
64.49
64.01
4.95
2.71
1.91
CO
POWER ENGINE MEASURED
THRUST, LBS PERCENT SPEED FUEL
OR RATED RPM FLOW
SHP
-0.00
-0.00
680.00
5390.00
7156.00
11081.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
-0.00
13.80
18.80
30.80
MASS EMI
HC
IB/IK
LB FUEL
15.32
13.32
13.26
0.64
0.37
0.24
T.O. Nl N2
0 -0.00 -0.00
0 -0.00 -0.00
5 3190.00 8430.00
46 7586.00 12826.00
62 8340. 00 13365.00
96 9998.00 14381.00
CO CO THC
(DRYI 2 (DRY)
PPMV (CRY) PPMV
PERCENT V
625.00 1.82 255.00
610.00 1.81 220.00
622.00 1.86 225.00
62.00 2.50 14.00
38.00 2.80 9.00
32.00 3.35 7.00
LB/HR
-0.00
-0.00
700.00
3120.00
4130.00
6810.00
NO
GAS GEN
AIR FLOW
LB/SFC
-0.
-0.
-0.
-0.
-0.
-0.
IDRY)
00
00
00
00
00
00
NO
2
-0
-0
-0
-0
-0
-0
PPMV (DRY)
5.
10.
4.
46.
65.
135.
MASS EMI MASS EMI MASS EMI MASS fMI
NU2 C02 NO
LB/1K LB/1K LB/1K
NOX
LB/1K
00
00
90
00
00
00
MASS EH
CO
LB/HR
PPMV
4.00
4.00
4.00
8.00
9.00
a. oo
1 MASS
H
CALC COMPRESSOR ENGINE
F/A DISCHARGE PRESSURE
TEMP RATIO
.000000
.000000
.000000
.000000
.000000
.000000
NO
X
IDRY)
PPMV
9.00
5.00
4.90
38.00
60.00
133.00
EMI MASS
C N
DEGREES F EPR
-0.00 -0.00
-0.00 -0.00
-0.00 -O.OC
-0.00 -0.00
-0.00 1.64
-0.00 2.05
ALDEHYDES SMOKE
-0.00 -0.00
-0.00 -0.00
5.90 -0.00
0.90 -0.00
0.90 -0.00
0.90 -0.00
EMI MASS EMI MASS
U2 C02 Ml
TURBINE
INLET
TFMP
DEGREES F
-0
.00
-0.00
-0
-0
.00
.00
-o.no
-0
.00
PARTICULATES
-0.00
-0.00
-0.00
-C.OO
-0.00
-C.OO
EHI MASS
NO
EMI
X
LB/HR LB/HR LB/HR LP/HP LB/HK
LB FUEL LB FUEL LB FUEL LB FUEL
0.69 2999.50 0.86
0.69 3006.65 1.74
0.68 3007.57 0.83
1.05 3135.00 6.03
1.05 3139.25 7.62
0.78 3140.87 13.23
CO THC
2
LB/IKITM-HR LB/U»TH-HR LB/1KHTH-HR
HORSEPOWER-HR OR THRUST-HR
HORSEPOWER-HR OR THRUST-HR
5
46
62
96
65.
2.
1.
1.
894
864
565
174
BASIS NOT CALCULABLE***
BASIS NOT CALCULABLE***
3096.024 13.652
1814.691 0.370
1811.783 0.212
1930.269 0.147
1.55
0.87
0.83
4.98
7.03
13.04
NO
-C.OO
-0.00
44.81
15.44
11.20
13.00
LB/1KKTH-HR
0.
3.
4.
S.
853
491
397
132
-0
-0
9
2
1
1
.00 -0
.00 -0
.28 0
.00 3
.52 4
.63 5
NO
2
LB/1KKTH-HR
0.696
0.607
0.609
0.482
.00 -0.00 -0.
.00 -0.00 -0.
.47 2105.30 0.
.27 9781.18 IS.
.36 12965.12 31.
.34 21389.30 90.
NO
X
LB/1MIH-HR
O.H53
2.884
4.059
a. oil
00 -0.
00 -0.
58 0.
81 15.
46 29.
11 HE.
00
00
58
54
04
77
IV-350
-------
DATE! 6/30/71
TEST ORGANIZATION! SCOTT/NORFOLK
ENGINE SUPPLIER) PRATT AND WHITNEY
ENGINE DATA »«»»»«»«»«««
CAL 10 NUMBER! 107 ENGINE TYPE AND MODEL I TF30 P6C
SERIAL NUMBER:
RATED THRUSH 11900.
ENGINE TOTAL TIME: 1160. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCEl
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
HZ TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO: 1.970
FUEL: JP-S
OPERATIONAL DATA ««»«
INLET AIR TEMPERATUREi DEGREES F: START 86.00 FINISH 87.00
ATMOSPHERIC PRESSURE: START 30.02 FINISH 29.99
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.0180
RELATIVE HUMIDITY: 65.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 118.00. FLOW RATE, LITERS/KIN:
SAMPLE LINE TRANSPORT TINE. SEC: -0.00
NUMBER OF TESTS: 5
COMMENTS:
H/C CAL ESTIMATED
PROBE J57 IEPAI MOD 2
-0.00
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
49
64
64
49
99
POWER
PERCENT
RATED
T.O.
49
64
64
99
99
POWER
PERCENT
RATED
T.O.
49
64
64
99
99
TEST
MODE
2/ 0
3/ 2
3/ 3
4/ 3
4/ 4
EXHAUST
GAS
TEMP
DEGREES F
1349.00
1499.00
1499.00
1865.00
2005.00
MASS EMI
CO
LB/1K
LB FUEL
5.13
2.45
1.86
1.02
1.31
CO
LB/lKf
2.
1.
1.
0.
0.
POWER
THRUST, LBS PERCENT
OR RATED
SHP
5668.00
7443.00
7443.00
11457.00
11430.00
EXHAUST
GAS
PRESSURE
PSIA
14.00
19.00
19.00
31.00
31.00
MASS EMI
HC
IB/IK
LB FUEL
-0.00
-0.00
-0.00
-0.00
-0.00
TH-HR L
839
361
033
615
789
ENGINE MEASURED
SPEED FUEL
RPM FLOW
T.O. Nl
49 7630
64 8370
64 8370
99 9811
99 9811
CO
(DRY)
PPMV
.00
.00
.00
.00
.00
N2
12856.00
13398.00
13398.00
14557.00
14580.00
CO THC
2 IORV)
(DRY) PPMV
LB/HR
3135.00
4130.00
4130.00
6885.00
6865.00
NU
(DRY
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
NO
I 2
-0.
-0.
-0.
-0.
-0.
PPMV IDRYI
PERCENT V
36.00
27.00
19.00
18.00
23.00
MASS EMI MASS
N02 CO
EMI
2
LB/IK LB/1K
LB FUEL LB FUEL
0.94 3136.
0.37 3140.
0.40 3141.
0.47 3142.
0.56 3142.
CO
2
B/IK(TH-HR
1734.791
1742.706
1743.220
1888.712
I8B7.400
46
67
60
92
46
LB
1.40 -0.00
2.20 -0.00
2.04 -0.00
3.52 -0.00
3.50 -0.00
10.
35.
35.
120.
120.
MASS EMI MASS EMI
NO
LB/IK
NOX
LB/IK
PPMV
00 4.00
00 2.50
00 2.50
00 5.00
00 6.00
MASS EMI MASS
CO
LB/HR
HC
CALC
F/A
000000
000000
000000
000000
000000
NO
X
IDRYI
PPMV
14.00
37.50
37.50
125.00
126.00
COMPRESSOR ENGINE
DISCHARGE PRESSUKE
TEMP R1T10
DEGREES F EPR
-0.00 1.48
-0.00 1.65
-0.00 1.65
-0.00 2.06
-0.00 2.06
TURBINE
INLET
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
-0.00
ALDEHYDES SMOKE PARUCULATES
1.00 -0.00
3.00 -0.00
2.00 -0.00
1.00 -0.00
-0.00 -0.00
FMI MASS EMI MASS EMI MASS EMI
LB/HR
N02 C02 NO
LB/HR LB/HR LB/HP
-0.00
-0.00
-c.oo
-c.oo
-0.00
MASS CHI
NOX
LB/HR
LB FUEL LB FUEL
2.34
5.22
5.63
11.20
11.26
THC
,/lK»TH-HR
-0.000
-0.000
-0.000
-0.000
-0.000
3.28
5.60
6.04
11.67
11.83
NO
LB/1KHT
1.
2.
3.
6.
6.
16.09
10. 13
7.69
7.04
9.0?
H-MR L
295
898
127
731
765
-0.
-0.
-0.
-0.
-0.
B/1K
00
00
00
00
OC
NO
2
TH-HR
0.518
0.207
0.223
0.280
0.338
2.94 9832.80 7.34
1.54 12970.96 21.57
1.66 12974.79 21.27
3.21 21638. IB 77.12
3. 87 21572.98 77.32
NO
X
L8/1KITH-HR
1.814
3.105
3.350
7.012
7.103
10.23
Z3.ll
24.93
80.33
81.19
IV-351
-------
OATEl T/l<)/71
TEST ORGANIZATION! SCOTT/NORFOLK
ENGINE SUPPLIER! NORFOLK NAS
ENGINE DATA
CAL ID NUMBER! 142
ENGINE TYPE AND MODEL: TF30 P6C
SERIAL NUMBER:
RATED THRUST: 11500.
ENGINE TOTAL TIME: 110). MRS
TINE SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE!
NI COMPRESSOR OVERHAUL: o. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL! 0. HRS
FUEL H/C RATIO: 1.970
FINISH
FINISH
84.00
29.83
FUEL: JP-S
OPERATIONAL DATA »»«
INLET AIR TEMPERATURE! DEGREES F: START 91.50
ATMOSPHERIC PRESSURE: START 21.83
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.0166
RELATIVE HUMIDITY: 67.oo PERCENT
SAMPLE LINE! TEMPERATURE. DEGREES C: 108.90. FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TINE, SEC: -0.00
NUMBER OF TESTS: 4
COMMENTS:
H/C CAL ESTIMATED
CK TEST
ME MODE
0.00
0.00
0.00
0.00
I/
2/
}/
4/
0
1
2
3
THRUST
OR
SHP
640.
5781.
7618.
11050.
POWER
.LBS PERCENT
RATED
00
00
00
00
T.O.
5
50
66
96
ENGINE
SPEED
RPM
NI
3129
7703
8454
9825
.00
.00
.00
.00
N2
8267.00
12735.00
13266.00
14300.00
MEASURED
FUEL
FLOW
GAS GEN
AIR FLOW
L8/SEC
LB/HR
665
3260
4320
6B95
.00
.00
.00
.00
-0.00
-0.00
-0.00
-0.00
CALC
F/A
-0.000000
-0.000000
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP KATIO
DEGREES F EPR
-0.00
-0.00
-0.00
-0.00
-0.00
1.51
1.7C
-0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POMER
PERCENT
RATED
T.O.
S
50
66
96
EXHAUST
GAS
TEMP
DEGREES F
912.00
1470.00
1635.00
1988.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
14.90
20.50
51.50
CO
(ORYI
PPMV
302.00
70.00
46.00
33.00
CO
2
I DRV I
PERCENT V
0.85
2.46
2.78
3.58
THC
I DRY I
PPHV
-0.00
-0.00
-0.00
-0.00
NO
(DRY)
PPMV
6.00
35.00
53.00
130.00
NO
2
(DRY)
PPMV
1.90
8.00
4.00
4.00
SMOKE (-ARTICULATES
IDRY)
PPMV
4.00
36.00
61.00
132.00
1.70
0.50
0.80
0.50
-0.00
-0.00
-0.00
-0.00
-0.00
-n.oo
-0.00
-0.00
POKER
PERCENT
RATED
T.O.
5
50
66
96
MASS EMI MASS EMI MASS EMI
CO HC
LB/1K LB/U
LB FUEL LB FUEL
6B.6T
5.68
3.31
1.84
-0.00
-0.00
-0.00
-0.00
S EMI
N02
B/1K
1 FUEL
0.71
1.07
0.47
0.37
MASS EMI
C02
LB/1K
LB FUEL
3036.63
3135.60
3139.33
3141.63
MASS EMI
NO
LB/1K
LB FUEL
2.24
4.66
6.26
11.93
MASS EMI
NOX
LB/1K
LB FUEL
1.49
5.06
7.20
12.11
MASS EM
CO
LB/HR
45.66
18.51
14.28
12.71
MASS EMI
HC
LH/HR
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI MASS E.HI MASS EMI
NC12 C02 Nfl NDX
LB/HR LB/HK Lfl/HP Lfl/HR
0.47
3.48
2.04
2.53
2019.36
10222.05
13561.90
21661.52
1.49
15.20
?7.03
82.23
0.99
16.51
31.11
R3.50
POWER
PERCENT
RATED
T.O.
5
50
66
96
CO
LB/IKITH-HR
71.348
3.202
1.875
1.150
LB/1IUTH-HR
3155.251
1768.216
1780.244
1960.319
THC
LB/1KITH-HR
-0.000
-0.000
-0.000
-0.000
NO
LB/IKHTH-HR
2.328
2.630
3.548
7.442
LB/1KHTH-HR
0.737
0.601
0.268
0.229
NO
X
LB/1KITH-HR
1.552
2.855
4.084
7.556
IV-352
-------
DATE: 7/ZJ/71
TEST ORGANIZATION! SCOTT/NORFOLK
ENGINE SUPPLIER: NORFOLK HAS
ENGINE DATA
CAL ID NUMBER) 15*
ENGINE TYPE AND MODEL: TF30 P6C
SERIAL NUMBER!
RATEO THRUST: 11900.
ENGINE TOTAL TINE: 976. MRS
TIME SINCE HOT SECTION OVERHAUL: 279. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 275. HRS
N2 COMPRESSOR OVERHAUL: 275. HRS
COMSUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: 275. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.170
74.00
30. os
FINISH
FINISH
7S.OO
30.05
FUEL! JP-5
OPERATIONAL DATA *»«
INLET AIR TEMPERATURE, DEGREES F: START
ATMOSPHERIC PRESSURE: START
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.0114
RELATIVE HUMIDITY: 89. oo PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 107.00. FLOW RATE. LITERS/HIN: -0.00
SAMPLE LINE TRANSPORT TIME. SEC: -0.00
NUMBER OF TESTS: *
COMMENTS:
H/C CAL ESTIMATED
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATEO
T.O.
5
52
69
97
POWER
PERCENT
RATED
T.O.
5
52
69
97
POWER
PERCENT
RATED
T.O.
5
52
69
97
TEST
MODE
11 0
Zl 1
3/ 2
*/ 3
EXHAUST
GAS
TEMP
DEGREES F
920.00
1470.00
1640.00
1945.00
MASS EMI
CO
LB/IK
LB FUEL
76.14
5.51
3.05
1.99
POWER
THRUST. LBS PERCENT
OR RATED
SHP T.O.
670.00
6046.00
8024.00
11160.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
15.80
21.40
30.90
MASS EMI
HC
LB/IK
LB FUEL
19.30
0.05
0.02
0.02
5
52
69
97
ENGINE
SPEED
RPM
NI N2
3186.00
7790.00
8575.00
9720.00
8369.00
12878.00
13485.00
14348.00
MEASURED
FUEL
FLOW
LB/HR
700.00
3420.00
4570.00
6810.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
CO CO THC NO NO
IDRY) 2 (DRY) (DRY) 2
PPHV (DRY) PPMV PPHV IDRY)
PERCENT V PPMV
314.
66.
43.
34.
MASS EMI
N02
LB/IK
LB FUEL
0.76
1.10
0.58
0.38
CO CO
2
LB/1KITH-HR LB/IKITH-H
79.
3.
1.
1.
553
117
735
213
3104.994
1773.770
1788.179
1916.903
00
00
00
00
MASS EMI
C02
LB/IK
LB FUEL
2971.92
3135.74
3139.68
3141.36
0.78 139.00 2.
2.39 1.00 40.
2.82 0.49 62.
3.42 0.49 125.
MASS EMI
NO
LB/IK
LB FUEL
0.80
5.49
7.22
12.00
THC
R LB/1K(TH-HR
20.169
0.027
0.011
0.010
MASS EMI
NOX
LB/IK
LB FUEL
1.55
6.58
7.80
12.39
NO
LB/IKUT
0.
3.
4.
7.
00 1.90
00 8.00
00 5.00
00 4.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
NO
X
(DRY)
PPMV
3.90
48.00
67.00
129.00
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
ALDEHYDES
2.60
0.70
1.10
1.20
ENGINE
PRESSURE
RATIO
EPK
-0.00
1.54
7.73
2.05
TURBINE
INLET
TEMP
DEGREES 1
-0.00
-0.00
-0.00
-0.00
SMOKE PAKT ICULATES
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI MASS EMI MASS HI MASS EMI
CO HC N02 CU2 NO
LB/HR LB/HP. LB/HR LB/HR LC/HR
53.30
10.85
13.92
13.5*
13.51
0.16
0.09
0.11
NO
2
H-HB LB/IKfTH-HR
B32
103
110
324
0.791
0.621
0.331
0.23*
0.53 2080.
3.75 1072*.
2.66 143*8.
2.62 21392.
NO
X
LB/1KSIH-
35 0.56
21 18.76
35 32.98
64 81.74
HR
-0.00
-0.00
-0.00
-0.00
MASS EMI
NOX
LB/HR
I.OV
22.52
35.6*
8*. 35
1.623
4.4*1
7.559
IV-353
-------
DATE: 7/26/71
TEST ORGANIZATION! SCOTT/NORFOLK
ENGINE SUPPLIERl NORFOLK NAS
ENGINE DATA »**«*«»»»«»««»«««««««««»
CAL 10 NUMBER: 155 ENGINE TYPE AND MODEL: TFSO-PB
SERIAL NUMBER:
RATED THRUST: 12500.
ENGINE TOTAL TIME: 967. MRS
TIME SINCE HOT SECTION OVERHAUL! 967. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 967. HRS
N2 COMPRESSOR OVERHAUL: 967. HRS
CONBUSTOR CAN REPLACEMENT: 967. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 967. HRS
NI TURBINE OVERHAUL: 967. HRS
N2 TURBINE OVERHAUL: 967. HRS
FUEL H/C RATIO: 1.970
FINISH
FINISH
86.SO
29. B6
FUEL: JP-S
OPERATIONAL DATA »««»
INLET AIR TEMPERATUREi DEGREES F: START 86.50
ATMOSPHERIC PRESSURE: START 29.86
INLET AIR HUMIDITY, LBS H2Q/LB AIR: 0.0174
RELATIVE HUMIDITY: 64.00 PERCENT
SAMPLE LINE: TEMPERATUREi DEGREES C: 107.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 3
COMMENTS:
H/C CAL ESTIMATED
-0.00
CLOCK
TIME
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
0
6}
89
POWER
PERCENT
RATED
T.O.
0
63
89
POWER
PERCFNT
RATED
T.O.
TEST
MODE
If 0
3/ 1
4/ 3
EXHAUST
GAS
TEMP
DEGREES F
-0.00
1655.00
1915.00
MASS EMI
CO
LB/IK
16 FUEL
B5.29
1.66
0.57
POWER
THRUST, LBS PERCENT
OR RATED
SHP T.O.
-0.00
7953.00
11237.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
19.60
29.50
MASS EMI
HC
LB/IK
LB FUEL
25.37
0.0*
0.04
0
63
69
ENGINE
SPEED
RPM
Nl N2
-0.00 -0.00
8465.00 13570.00
9640.00 14405.00
MEASURED
FUEL
FLOW
LB/HR
-0.00
4360.00
6520.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
CO CO THC NO NO
(DRY) 2 IORYI IORYI 2
PPMV IORYI PPMV PPMV IORYI
PERCENT V PPMV
360.
22.
9.
MASS EMI
NO?
LB/IK
LB FUEL
0.78
0.37
0.31
00 0.79 187.00 2.
00 2.65 1.00 85.
00 3.15 1.00 150.
MASS EMI MASS EMI
C02 NO
LB/IK LB/IK
LB FUEL LB FUEL
2940.89 0.78
3141.80 10.53
3143.5) 15.65
CO CO THC
2
LB/IK»TH-HR LB/1K4TH-HR Lfl/lKITH-HR
HOSSEPOWER-HR OR THRUST-HR
63 0.910
89 0.332
BASIS NOT
1722.399
1821.956
CALCULABLE"*
0.024
0.021
MASS EMI
NOX
LB/IK
LB FUEL
1.56
10.91
15.96
00 2.00
00 3.00
00 3.00
CALC
F/A
-0.000000
-0.000000
-0.000000
NO
X
IORYI
PPMV
4.00
88.00
153.00
COMPRESSOR ENGINC
DISCHARGE PRESSURE
TEMP RATIO
DEGRFES F EPR
-0.00
-0.00
-0.00
-0.00
1.67
2.01
ALDEHYDES SMOKE
5.70 -0
0.50 -0
0.20 -0
MASS EMI MASS EMI MASS EMI MASS FM[
CO HC N02 CO?
LB/HR LB/HR LB/HR LB/HR
-0.00
7.24
3.73
-0.00
0.19
0.24
Nil NO
2
LB/1MTH-HR L9/1KHTH-HR
5.
9.
775
OBO
0.204
0.1B2
-0.00 -0.00
1.62 13698.24
2.04 20495.79
NU
X
LB/IKllTH-HH
5.979
9.261
.00
.00
.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
MASS EMI MASS EMI
NO NOX
LD/HR LB/HR
-0.
45.
102.
oo -o.oo
93 47.55
03 104.07
IV-354
-------
CUTE! 7/11/11
TEST ORGANIZATION! SCOTT/NORFOLK
ENGINE SUPPLIER! NORFOLK NAS
ENGINE DATA ««««»
CAL ID NUMBER! 106 ENGINE TYPE AND MODEL: J52 - P8A
SERIAL NUMBER:
RATED THRUST: 9300.
ENGINE TOTAL TIME: 369. MRS
TIME SINCE HOT SECTION OVERHAUL: 242. HRS
TIME SINCE)
Nl COMPRESSOR OVERHAUL: 369. HRS
N2 COMPRESSOR OVERHAUL: 369. HRS
COMBUSTOR CAN REPLACEMENT: 369. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL! 369. HRS
Nl TURBINE OVERHAUL: 369. HRS
N2 TURBINE OVERHAUL! 62*. HRS
FUEL H/C RATIO: 1.970
FINISH
FINISH
74.00
29.75
FUEL: JP-5
OPERATIONAL DATA «««»««»««««»
INLET AIR TEMPERATURE, DEGREES F: START 74.00
ATMOSPHERIC PRESSURE: START 29.74
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0116
RELATIVE HUMIDITY: 92.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 104.00, FLOW RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS! 4
COMMENTS:
H/C CAL ESTIMATED
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
TEST
MODE
I/ 0
2/ 1
3f Z
4/ 3
POKER
THRUST,LBS PERCENT
OR RATED
SHP T.O.
-0.00
5920.00
7720.00
8626.00
0
63
03
92
ENGINE
SPEED
RPM
Nl N2
0.00 -0.00
0.00 1106.00
0.00 11628.00
0.00 11909.00
MEASURED
FUEL
FLOM
LB/HR
-0.00
4420.00
5915.00
6BOO.OO
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
CALC
F/A
-0.000000
COMPRESSOR
DISCHARGE
TFMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSUHF
RATIO
EPR
-0.00
2.09
-0.00
-0.00
TURBINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POWER EXHAUST
PERCENT GAS
RATED TEMP
T.O. DEGREES F
0
63
83
92
-0.00
89.50
1048.00
1140.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
32.00
42.60
47.90
CO
I DRY I
PPMV
330.00
70.00
50.00
26.00
CO
2
(DRY)
PERCENT V
1.07
2.36
2.85
3.07
THC
(DRY)
PPMV
-0.00
9.00
-0.00
0.90
NO
IDRVI
PPMV
8.00
35.00
57.00
80.00
NO
2
IDRYI
PPHV
1.90
1.00
3.00
3.00
ALDEHYDES SMOKE PaRTICULSTES
(DRY!
PPMV
8.00
39.00
68.00
85.00
2.10
0.70
0.60
0.50
-0.00
-0.00
-0.00
-0.00
-o.ou
-0.00
-0.00
-o.oo
POWER
PERCENT
RATED
T.O.
0
63
83
92
MASS EMI
CO
LB/1K
LB FUEL
59.88
5.92
3.50
1.69
MASS EMI
HC
LB/1K
LB FUEL
-0.00
0.44
-0.00
0.03
MASS EMI
N02
LB/1K
LB FUEL
0.57
1.11
0.35
0.32
MASS EMI
C02
LB/1K
LB FUEL
3050.44
3134.03
3139.02
3141.77
MASS EMI
NO
LB/1K
LB FUEL
2.18
4.86
6.56
8.5t>
MASS EMI
NOX
LB/1K
LB FUEL
2.38
5.41
7.83
9.09
MASS EMI
CO
LB/HR
-0.00
26.15
20.73
11.52
MASS EMI
HC
LB/HR
0.00
1.93
-0.00
0.23
MASS EMI
NO 2
LB/HR
-0.00
4.91
2.04
2.18
MASS EMI
C02
LB/HR
-0.00
13852.43
18567.28
21364.04
MASS EMI
NO
LR/HR
-0.00
21.48
10.82
50.20
MASS EMI
NQX
LB/HR
-0.00
23.93
46.31
61.84
POWER
PERCENT
RATED
T.O.
L8/1K»TH-HR
LB/1MTH-HR
THC
LB/1KITH-HR
HORSEPOWER-MR OR THRUST-HR BASIS NOT CALCULABLE*"
63 4.417 2339.937 0.325
83 2.685 2405.088 -0.000
92 1.335 2476.703 0.026
NO
LB/IK»TH-HK
3.628
5.029
6.747
LB/ IKHTH-HK
0.829
0.265
0.253
NO
X
LB/1KHTH-HR
4.042
5.999
7. 169
IV-355
-------
DATE: 7/22/71
TEST ORGANIZATION: SCOTT/NORFOLK
ENGINE SUPPLIER: NORFOLK NAS
ENGINE DATA ««*»*««««».«.»».«.«»«««.«»«..»»«...««««»
CAL ID NUMBER: i»6 ENGINE TYPE AND MODEL: TFIO-PSB
SERIAL NUMBER:
P664169
RATED THRUST: 12500.
ENGINE TOTAL TINE: 991. HRS
TINE SINCE HOT SECTION OVERHAUL: 991. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: 552. HRS
N2 COMPRESSOR OVERHAUL: 261. HRS
COMBUSTOR CAN REPLACEMENT: 562. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
Nl TURBINE OVERHAUL: 261. HRS
N2 TURBINE OVERHAUL: 261. HRS
FUEL H/C RATIO: 1.970
FINISH
FINISH
77.00
30.11
FUEL: JP-5
OPERATIONAL DATA *«««»
INLET AIR TEMPERATURE, DEGREES F: START 77.00
ATMOSPHERIC PRESSURE: START 30.11
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0120
RELATIVE HUMIDITY: 62.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 110.00, FLOW RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TINE, SEC: -0.00
NUMBER OF TESTS: 4
COMMENTS:
H/C CAL ESTIMATED
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
5
50
66
91
POWER
PERCENT
RATED
T.O.
5
50
66
91
POWER
PERCENT
RATED
T.O.
5
50
66
91
TEST POWER ENGINE MEASURED GAS GEN
NODE THRUST.LBS
OR
SHP
I/ 0 650.00
2/ 1 6261.00
3/ 2 8313.00
4/ 3 11396.00
EXHAUST EXHAUST
GAS GAS
TEMP PRESSURE
DEGREES F PSIA
915.00 -0.00
1505.00 IS. 20
1670.00 20.70
1930.00 30.30
MASS ENI NASS EMI
CO HC
LB/1K LB/1K
LB FUEL LB FUEL
82.15 26.08
2.00 0.24
1.60 0.04
1.17 0.07
CO
PERCENT SPEED
RATED RPM
T.O. Nl N2
5 3040.00 8460.00
50 7810.00 13160.00
66 6535.00 13665.00
91 9660.00 14505.00
CO CO THC
(DRY) 2 IORY)
PBHV (CRY) . P.PMV
PERCENT V
285.00 0.65 158.00
23.00 2.30 4.90
22.00 2.75 1.00
19.00 3.25 2.00
FUEL AIR FLOW
FLOW LB/SEC
LB/HR
700.00 -0.00
3440.00 -0.00
4570.00 -0.00
6680.00 -0.00
NO NO
IORYI 2
PPNV IORY)
PPMV
4.00 3.00
70.00 7.00
113.00 fl.OO
177.00 6.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
NO
X
IORYI
PPNV
7.00
77.00
121.00
183.00
COMPRESSOR ENGINE TURBINE
DISCHARGE PRESSURE INLET
TEMP RATIO TEMP
DECREES F EPR DEGREFS F
-0.00 -0.00 -0.00
-0.00 1.52 -0.00
-0.00 1.70 -0.00
-0.00 2.03 -0.00
ALDEHYDES SMQKt PAST ICULATES
3.10 -0.00 -0.00
0.90 -0.00 -0.00
1.10 -0.00 -0.00
1.60 -0.00 -0.00
MASS ENI NASS ENI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EK! MASS EMI
HO 2 C02 NO
LB/1K LB/1K L8/1X
NOX CO
LB/1K LB/HK
HC
La/Ma
N02 C02 NO NOX
L8/HD LB/HR L3/HR LB/HH
LB FUEL LB FUEL LB FUEL L8 FUEL
1.42 2943.89 1.89
1. 00 3140.72 9.99
0.96 3141.90 13.50
0.61 3142.49 17.89
CO THC
2
LB/1KITH-HR LB/1KITH-HK LB/1KHTH-HR
88.471
1.098
0.879
0.685
3170.338 28.090
1725.613 0.134
1727.230 0.023
1842.037 0.041
3.31 57.51
10.99 6.88
14.45 7.31
18.50 7.81
NO
IS. 26
0.84
0.19
0.47
NO
2
LB/1K»TH-MH LB/IKHTH-HK
2.040
5.490
7.420
10.487
1.530
0.549
0.525
0.356
0.99 2060.72 1.J3 2.32
3.44 10804.06 34.37 37.81
4.37 14358.46 61. 6K 66.05
4.05 20991.96 119.52 123.57
NO
X
LR/lKiTH-HR
1.469
6.019
7.945
10.843
IV-356
-------
DATE: 7/13/71
TEST ORGANIZATION! SCOTT/NORFOLK
ENCINE SUPPLIER! NORFOLK N»S
ENGINE DATA
CAL 10 NUMBER I 101
ENGINE TYPE AND MODEL: TF30 P40B
SERIAL NUMBER:
RATED THRUST: 13400.
ENGINE TOTAL TIME: 0. MRS
TIME SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: o. MRS
N2 COMPRESSOR OVERHAUL: 0. MRS
COMBUSTOR CAN REPLACEMENT: 0. MRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
HI TURBINE OVERHAUL: 0. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.170
FINISH
FINISH
78.00
29.1)*
FUEL: JP-5
OPERATIONAL DATA »»«««*
INLET AIR TEMPERATURE. DEGREES F: START 78.00
ATMOSPHERIC PRESSURE: START 29.94
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.01S7
RELATIVE HUMIDITY: 76.00 PERCENT
SAMPLE LINEI TEMPERATURE, DEGREES C: 101.00. FLOW RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 4
COMMENTS:
H/C CAL ESTIMATED
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
0
59
79
92
POWER
PERCENT
RATED
T.O.
0
59
79
92
POWER
PERCENT
RATED
T.O.
TEST
MODE
17/ 0
18/17
19/18
10/19
EXHAUST
GAS
TEMP
OEGRFES F
960.00
1645.00
1855.00
2035.00
MASS EMI
CO
LB/IK
LB FUEL
77.00
3.11
1.57
1.29
POWER ENGINE
THRUST, LBS PERCENT SPEED
OR RATED RPM
SHP T.O. Nl N2
-0.00
8023.00
1069B.OO
12417.00
EXHAUST
GAS
PRESSURE
PS I A
-0.00
24.10
33.60
40.00
MASS EMI
HC
LB/IK
LB FUEL
10.91
0.20
0.16
0.15
0 3227.00 8635.00
59 8242.00 13380.00
79 9070.00 14000.00
92 9705.00 14468.00
MEASURED GAS GFN
FUEL AIR FLOW
FLOW LB/SEC
LB/HR
795.00 -0.00
4500.00 -0.00
6210.00 -0.00
7590.00 -0.00
CO CO THC NO NO
(DRY) 2 IORYI IDRYI 2
PPMV IORYI PPMV PPMV IDRYI
PERCENT V PPMV
485.00 1.20 120.00 3.00 5.00
36.00 2.31 4.00 48.00 R.OO
22.00 2.80 4.00 84.00 4.00
20.00 3.10 4.00 130.00 9.00
MASS EMI MASS EMI MASS EMI
N02 C02 NO
LB/IK LB/IK LB/IK
LB FUEL L8 FUEL LB FUEL
1.30 2993.60 0.78
1.14 3139.09 6.82
1.06 3141.61 9.85
0.85 3142.09 13.77
CO CO THC
2
LB/1K(TH-HR LB/1KITH-HR LB/IKKIH-HR
HORSEPOUER-HR OR THRUST-HR
59 1.746
79 0.912
92 O.T89
BASIS NOT CALCULABLE***
1760.675 0.111
1823.647 0.095
1920.632 0.090
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
NO
X
IORYI
PPMV
4.90
49.00
B5.00
132.00
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIO
DEGREES F EPR
-0.00 -0.00
-0.00 I.B2
-0.00 2.15
-0.00 2.37
ALDEHYDES SMOKF
2.20 -0.00
0.40 -0.00
0.30 -0.00
0.40 -0.00
TURBINE
INLET
TEMP
DEGREES f
-0.00
-0.00
-0.00
-0.00
PART ICI1LATCS
-0.00
-0.00
-0.00
-0.00
MASS EMI MASS EMI MASS FMI MASS EMI MASS EMI MASS EMI MASS CMI
NOX CO HC N02 CO? NO NQX
LB/IK LB/HR LB/HK LB/HR L8/HR L6/HR LB/HR
LB FUEL
1.28 61.22
6.96 14.01
9.97 9.76
13.99 9.79
8.67
0.89
1.02
1.12
NU NO
2
LB/IKMTH-HP LB/1KHTH-HR
3.825
5.719
8.420
0.637
0.613
0.518
1.04 2379.91 0.
5.11 14125. U9 30.
6.56 19509.18 61.
6.43 23848.49 104.
NO
X
LB/ 1K4TH-HR
3.404
5. '87
B.S49
62 1.02
69 31.12
19 61.91
55 106.16
IV-357
-------
OATEl 7/14/71
TEST ORGANIZATION! SCOTT/NORFOLK
ENGINE SUPPLIER: NORFOLK NAS
ENGINE DATA »««»»*«»«««*«««»«
C»L ID NUMBER! 102 ENGINE TYPE AND MODEL: TF30 P408
SERIAL NUMBER:
RATED THRUST: 13400.
ENGINE TOTAL TINE: 1021. MRS
TIHE SINCE HOT SECTION OVERHAUL: 0. MRS
TIME SINCEl
Nl COMPRESSOR OVERHAUL: 0. HRS
H2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE N021LE GUIDE VANE OVERHAUL: 0. HRS
Nl TURBINE OVERHAUL: 0. HRS
NZ TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.970
FINISH
FINISH
85.00
29.69
FUEL: JP-S
OPERATIONAL DATA »»»»»»**»»
INLET AIR TEMPERATUREi DEGREES F: START 85.SO
ATMOSPHERIC PRESSURE: START 29.69
INLET AIR HUMIDITY. LBS H20/LB AIR: 0.017}
RELATIVE HUMIDITV: 68.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 96.00, FLOW RATE, LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: *
COMMENTS:
H/C CAL ESTIMATED
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
0
0
7
92
POWER
PERCENT
RATED
T.O.
0
0
7
92
POWER
PERCENT
RATED
T.O.
TEST
MODE
I/ 0
2/ 1
3/ 2
4/ 3
EXHAUST
GAS
TEMP
DEGREES F
980.00
1650.00
1850.00
2020.00
MASS EMI
CO
LB/IK
LB FUEL
71.10
2.32
1.48
1.16
POWER ENGINE MEASURED GAS GEN
THRUST, L8S PERCENT SPEED FUEL AIR FLOW
OR RATED RPM FLOW L8/SEC
SHP T.O. Nl N2 LB/HR
-0.00
8.53
1065.60
12366.00
0 3226.00 8666.00
0 6269.00 13455.00
7 9059.00 14077.00
92 9647.00 14540.00
EXHAUST CO CO THC
GAS (DRY) 2 (DRY)
PRESSURE PPMV (DRY) PPMV
PSIA PERCENT V
-0.00
23.10
32.20
38.50
MASS EMI
HC
LB/IK
LB FUEL
19.61
0.05
0.04
0.04
CO
LB/IKITH-HR
540.00 1.44 260.00
29.00 2.50 I. 00
21.00 2.83 1.00
18.00 3.10 1.00
770.00 -0.00
4375.00 -0.00
5960.00 -0.00
7230.00 -0.00
NO NO
(DRY) 2
PPMV (ORYI
PPMV
11.00 1.90
50.00 5.00
90.00 4.00
135.00 3.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
NO
X
(DRY!
PPMV
6.00
54.00
91.00
135.00
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIC
DEGREES F EPR
-0.00 -0.00
-0.00 I. 80
-0.00 2.11
-0.00 2.33
TURBINE
INLET
TEMP
DEGREES 1
-o.on
-0.00
-0.00
-0.00
ALDEHYDES SMCKE PARTICULATFS
5.20 -0.00
1.20 -0.00
1.20 -0.00
1.10 -0.00
MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS EMI MASS [Ml MASS EMI MASS EMI
N02 C02 NO NOX CO HC N02 CO 2 NO
LB/IK LB/IK LB/IK LB/IK LB/HR LB/HR LB/HR IB/HR LB/HR
LB FUEL LB FUEL LB FUEL LB FUEL
0.41 2979.03 2.36
0.66 3140.76 6.57
0.46 3142.08 10.45
0.32 3142.60 14.31
CO THC
2
LB/IKKTH-HR LB/1KITH-HR
HORSEPOWER-HR OR THRUST-HR 8ASIS NOT CALCULABLE***
0 1189.277 1610879.000 23.487
7 8.300 17573.949 0.226
92 0.679 1837.375 0.022
1.73 54.75
7.09 10.14
10.56 B.8t
14.31 8.40
15.10
0.20
0.24
0.21
NO NO
2
LB/1K«TH-HR LB/lKiTH-HR
3366.025
56.426
8.365
336.602
2.597
0.186
0.32 2293.85 1.83
2.87 13740.80 26.73
2.77 18726.79 62.26
2.30 22720.98 103.44
NO
X
LB/1K«TH-H«
3637.465
59.075
8.365
-0.00
-0.00
-0.00
-c.oo
MASS EMI
NOX
LB/HK
1.33
31.03
62.95
103.44
IV-358
-------
DATE: 7/16/71
TEST ORGANIZATION! SCOTT/NORFOLK
ENGINE SUPPLIER) NORFOLK NtS
ENGINE DATA »«««««»
CAL ID NUMBER: 10* ENGINE TYPE AND MODEL: TF30 P*08
SERIAL NUMBER:
RATED THRUST: 13400.
ENGINE TOTAL TIME: 626. HRS
TIME SINCE HOT SECTION OVERHAUL: 0. HRS
TINE SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: o. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.970
FINISH
FINISH
62.00
29.81
FUEL; JP-S
OPERATIONAL DATA ««»«»«»»««««»«««««
INLET AIR TEMPERATURE, DEGREES F: START BO.SO
ATMOSPHERIC PRESSURE: START 29.89
INLET AIR HUMIDITY, LBS H2D/LB AIRl 0.01*9
RELATIVE HUMIDITY: 65.oo PERCENT
SAMPLE LINE: TEMPERATUREt DEGREES C= 98.00, FLOW RATE. LITERS/MIN:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 2
COMMENTS:
H/C CAL ESTIMATED
.( ft 4
5
1
CLOCK
TIME
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
5
89
POWER
PERCENT
RATED
T.O.
5
89
POWER
PERCENT
RATED
T.O.
5
89
TEST
MODE
I/ 0
*/ 1
EXHAUST
GAS
TEMP
DEGREES F
-0.00
-0.00
MASS EMI
CO
LB/IK
LB FUEL
64.63
1.31
POWER ENGINE MEASURED GAS GEN CALC COMPRESSOR ENGINE
THRUST, LBS PERCENT SPEED FUEL AIR FLOW F/A DISCHARGE PRESSURE
OR RATED RPM FLOW L8/SEC TEMP RATIO
SHP T.O. Nl N2 LB/HR DECREES f EPK
780.00
12060.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
-0.00
MASS EMI
HC
LB/IK
LB FUEL
15.98
0.10
5 3272.00 8713.00 780.00 -0.00 -0.000000 -0.00 -0.00
89 9721.00 1*524.00 7420.00 -0.00 -0.000000 -0.00 -O.OU
CO CO THC NO NO ND ALOEHVOES SMOKC
IDRYI 2 (DRY) IORYI 2 <
PPNV IDRYI PPMV PPNV IDRYI IDRYI
PERCENT V PPMV PPMV
535.00 1.58 231.00 10.00 1.90 10.00 0.50 -0.00
22.00 3.35 3.00 158.00 3.00 166.00 8.50 -0.00
ruReiNC
INLFT
TEMP
DECHEFS F
-0.00
-0.00
PART 1CULATES
-0.00
-0.00
MASS EMI MASS EMI MASS EMI MASS FMI MASS EMI MASS EMI MASS EMI MASS FM[ MASS EMI MASS tMI
N02 C02 NO NOX CC1 HC N02 C02 NO N0«
IB/IK LB/IK LB/IK LB/IK LP/HR Lfl/HR LB/HJi LB/HR LB/HR LB/HR
LB FUEL LB FUEL LB FUEL LB FUEL
0.38 2999.12 1.98 1.98 50.41 12.47 0.29 2331.32 1.
0.29 31*2.18 15.49 16.28 9.74 0.76 2.18 23314.96 114.
55 1.55
96 120.78
CO CO THC NO NO NO
2 2 X
LB/lKtTH-HR LB/IMTH-HR LB/IKITH-HR LB/IKITH-HR LB/imTH-HR LB/IKITH-HR
64.
0.
633
808
2999.12* 15.983 1.984 0.377 1.9a*
1933.247 0.063 9.532 0.181 10.015
IV-359
-------
DATE: 7/20/71
TEST ORGANIZATION: SCOTT/NORFOLK
ENGINE SUPPLIER) NORFOLK NAS
ENGINE DATA «»«««................,,.»....
CAL ID NUMBER: 1*3 ENGINE TYPE AND MODEL: TFIO p*oa
SERIAL NUMBER:
RATED THRUST: 13400.
ENGINE TOTAL TINE: 390. MRS
TINE SINCE HOT SECTION OVERHAUL: 0. HRS
TIME SINCE:
NI COMPRESSOR OVERHAUL: o. HRS
N2 COMPRESSOR OVERHAUL: o. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.970
FINISH
FINISH
80.00
29.63
FUEL: JP-S
OPERATIONAL DATA »«»««*««»«
INLET AIR TEMPERATURE. DEGREES F: START 79.00
ATMOSPHERIC PRESSURE: START 29.82
INIET AIR HUMIDITY, LBS H20/LB AIR: 0.0160
RELATIVE HUMIDITY: 70.00 PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 110.00. FLOM RATE. LITERS/HIM:
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: 4
COMMENTS:
H/C CAL ESTIMATED
-0.00
)CK TEST
IME NODE
POWER
THRUST, LBS PERCENT
OR RATED
SHP
0.00
0.00
0.00
0.00
I/
11
3/
4/
0
1
2
3
795.
7827.
10509.
12264.
00
00
00
00
T.O.
5
58
78
91
ENGINE
SPEED
RPH
NI
3252.00
8202.00
9087.00
9670.00
N2
8688
13365
14027
14497
.00
.00
.00
.00
MEASURFO
FUEL
FLOW
GAS GEN
AIR FLOM
LB/SEC
LB/HR
785.
4375.
6000.
7330.
00
00
00
00
-0.00
-0.00
-0.00
-0.00
CALC COMPRESSOR ENGINE
F/A DISCHARGE PRESSURE
TEMP RATIO
OEGRFES F EPB
-0.00
-0.00
-0.00
-0.00
-0.00
1.79
2.12
2.34
TURBINE
INLET
TCBP
DEGREES F
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
5
58
78
91
EXHAUST
GAS
TEMP
DEGREES F
974.00
1625.00
1840.00
2015.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
2}. 20
32.80
39.20
CO
(DRV)
PPNV
530.00
42.00
26.00
25.00
CO
2
ICRV)
PERCENT V
1.55
2.93
3.10
3.20
THC
IDRY)
PPMV
23.30
1.00
0.90
1.00
NU
I DRY I
PPMV
11.00
54.00
108.00
139.00
NO
2
IDRY)
PPMV
3.00
8.00
7.00
4.00
NO
X
(DRY)
PPHV
10.00
57.00
102.00
143.00
10.10
0.40
0.50
0.50
-0.00
-0.00
-0.00
-0.00
PARTICULARS
-0.00
-0.00
-0.00
-0.00
POMER
PERCENT
RATED
T.O.
5
58
78
91
MASS EMI
CO
LB/1K
LB FUEL
66.07
2.86
1.6B
1.S6
MASS EMI
HC
LB/1K
LB FUEL
1.66
0.04
0.03
0.04
MASS EMI
N02
LB/1K
LB FUEL
0.61
0.90
0.74
0.41
MASS EMI
CO 2
LB/IK
L8 FUEL
3036.14
3139.92
3141.80
3141.97
MASS EMI
NO
IB/ IK
LB FUEL
2.25
6.05
11.44
14.27
MASS EMI
NOX
LB/1K
LB FUEL
2.05
6.39
10.81
14.68
MASS EMI
CO
LB/HR
51.87
12.53
10.06
11.45
MASS EMI
HC
LB/HR
MASS EMI
NO?
LB/HR
MASS C1I
CO 2
LB/HR
MASS FMI
NO
Lfi/HR
MASS EM
NOX
LB/HR
1.31
0.17
0.20
0.26
0.48
3.92
4.45
3.01
2383.37
13737.13
18850.79
23030.64
1.77
26.47
6H.66
104.50
1.61
27.94
64.84
107.59
POWER
PERCENT
RATED
T.O.
5
58
78
91
CO
LB/1KITH-HR
65.243
1.601
0.958
0.934
LB/IP(«TH-HR
2997.954
1755.095
1793.776
1877.906
THC
L6/U«IH-HR
1.643
0.022
0.019
0.021
NO
LB/1MTH-HR
2.224
3.381
6.533
8.527
LB/IKKTH-HR
0.607
0.501
0.423
0.245
LB/IK»TH-HR
2.022
3.569
6.170
8. T73
IV-360
-------
DATE: T/ZT/TI
TEST ORGANIZATION! SCOTT/NORFOLK
ENGINE SUPPLIER! NORFOLK NAS
ENGINE DATA
CAL 10 NUMBER: 156
ENGINE TYPE AND MODEL: TF30 P*08
SERIAL NUMBER:
RATED THRUSI: 13*00.
ENGINE TOTAL TIME: 506. MRS
TINE SINCE HOT SECTION OVERHAUL: . 0. HRS
TIME SINCE:
Nl COMPRESSOR OVERHAUL: 0. HRS
N2 COMPRESSOR OVERHAUL: 0. HRS
COMBUSTOR CAN REPLACEMENT: 0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: 0. HRS
NI TURBINE OVERHAUL: o. HRS
N2 TURBINE OVERHAUL: 0. HRS
FUEL H/C RATIO: 1.470
FINISH
FINISH
63.00
29.93
FUEL: JP-5
OPERATIONAL DATA «»«»«
INLET AIR TEMPERATURE. DEGREES F: START 63.00
ATMOSPHERIC PRESSURE: START 29.93
INLET AIR HUMIDITY, IBS H20/LB AIR: 0.0169
RELATIVE HUMIDITY: 69.oo PERCENT
SAMPLE LINE: TEMPERATURE. DEGREES C: 126.00, FLOW RATE, LITERS/MIN: -0.00
SAMPLE LINE TRANSPORT TIME, SEC: -0.00
NUMBER OF TESTS: *
COMMENTS:
H/C CAL ESTIMATED
CLOCK
II ME
-0.00
-0.00
-0.00
-0.00
POWER
PERCENT
RATED
T.O.
0
57
77
PIIWER
PERCENT
RATED
T.O.
0
57
77
90
POWER
PERCENT
RATED
T.O.
TEST
MODE
I/ 0
2/ 1
3/ 2
*/ 3
EXHAUST
GAS
TEMP
DEGREES F
96*. 00
1655.00
1683.00
2055.00
MASS EMI
CO
LR/1K
LB FUEL
6*. 69
3.02
1.77
1.37
CO
LB/IKITI
POWER ENGINE
THRUST, LBS PERCENT SPEED
OR RATED RPM
SHP T.O. Nl N2
-0.00
771*. DO
103*8.00
12090.00
EXHAUST
GAS
PRESSURE
PSIA
-0.00
22.50
31.60
38.10
MASS EMI
HC
LB/1K
LB FUEL
18.18
0.0*
0.0*
0.03
0 3236.00 8665.00
57 62*3.00 13*01.00
77 9082.00 1*065.00
90 9687.00 1*5*3.00
MEASURED GAS GEN
FUEL AIR FLOW
FLOW LB/SEC
LB/HR
775.00 -0.00
4310.00 -0.00
5970.00 -0.00
7210.00 -0.00
CO CO THC NU NO
(DRY) 2 (DRY) IORY) 2
PPHV ICRY) PPMV PPMV (ORYI
PERCENT V PPMV
5*0.00 1.59 265.00 12.00 2.00
42.00 2.76 1.00 56.00 5.00
28.00 3.17 1.00 ICZ.OO 3.00
2*. 00 3.50 0.90 160.00 4. CO
MASS EMI MASS EMI MASS EMI
N02 C02 Nfl
LB/1K LB/1K LB/1K
LB FUEL LB FUEL LB FUEL
0.39 2992.99 2.36
0.59 3139.67 6.85
0.31 31*1.65 10.57
0.36 3142.29 15.02
CO THC
2
4-HR LR/IK»TH-HR L8/1K0TH-HR
HORSEPOWER-HR OR THRUST-HR
57 1.687
77 1.019
90 0.616
BASIS NOT CALCULABLE*"
1754.206 0.023
1612. *90 0.021
1673.937 0.018
CALC
F/A
-0.000000
-0.000000
-0.000000
-0.000000
NO
X
(DRY)
PPMV
14.00
63.00
105.00
164.00
COMPRESSOR ENGINE
DISCHARGE PRESSURE
TEMP RATIU
DEGREES F EPR
-0.00 -O.OC
-0.00 1.77
-0.00 2.08
-0.00 2.30
ALDEHYDES SN1IKE
0.80 -0.00
0.10 -0.00
0.0* -0.00
0.30 -0.00
TUKDINE
INLET
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
"ARTICULATES
-0.00
-C.OO
-0.00
-0.00
MASS EMI MASS EMI MASS EMI MASS EMI MASS F.HI 1ASS EM "ASS EMI
NOX CO HC NU2 CO? Nl) NOX
LR/1K LB/HR LB/HR LB/HR Lfl/HR LB/HR LB/HK
LB FUEL
2.75 50.1*
7.** 13.01
10.86 10.54
15.39 9.69
14.09
0.18
0.22
0.21
NO NO
2
LB/IK0TH-HR LB/lKfTH-HR
3.B26
6.097
D.955
0.330
0.179
0.224
0.31 2319.57 1.
2.54 13531.96 2
-------
OATEl 7/19/71
TEST ORGANIZATION: UNITED/EPS
ENGINE SUPPLIER: UNITED AIRLINES
ENGINE DATA
CAL in NUMBER:
ENGINE TYPE AND MODEL: JT4A -11
SERIAL NUMBER:
RATED THRUST: 17500.
ENGINE TOTAL TIME: 16271. MRS
TIME SINCE HOT SECTION OVERHAUL: 16271. HRS
TIME SINCE:
M COMPRESSOR OVERHAUL: -o. HRS
N2 COMPRESSOR OVERHAUL: -o. HRS
COMBUSTOR CAN REPLACEMENT: -0. HRS
FIRST STAGE NOZZLE GUIDE VANE OVERHAUL: -0. HRS
NI TURBINE OVERHAUL: -o. MRS
NZ TURBINE OVERHAUL: -o. HRS
FUEL H/C RATIO: 1.920
FUEL: JET - A
OPERATIONAL DATA «««»»»»*»««
INLET AIR TEMPERATURE, DEGREES F: START 59.00 FINISH 57.20
ATMOSPHERIC PRESSURE: START 29.93 FINIS)- 29.95
INLET AIR HUMIDITY, LBS H20/LB AIR: 0.0066
RELATIVE HUMIDITY: 60.00 PERCENT
SAMPLE LINE: TEMPERATURE, DEGREES C: 160.00. FLOW RATE, LITERS/KIN:
SAMPLE LINE TRANSPORT TIME, SEC: 5.00
NUMBER CF TESTS: 5
COMMENTS:
NO ENGINE OPERATIONAL DATA
Cl-2 ADDITIVE USED ON RUNS 1 AND 2
HIGH PROBE BUFFET AT 5000 * THRUST, CRACKEC SUPPORT ROLLEC
PROBE SUPPORT FAILED ON LAST RUN
CLOCK
TIME
-0.00
-0.00
-0.00
-0.00
-0.00
TFST
MODE
5/ 5
4/ 5
I/ 4
POfcFR
THRUST,LBS PERCENT
OP RATED
SHP T.O.
-0.00
-0.00
-0.00
-0.00
-0.03
ENGINE
SPEED
PPM
Nl N2
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
MEASURED
FUEL
FLOW
LB/HR
-0.00
-0.00
-0.00
-0.00
-0.00
GAS GEN
AIR FLOW
LB/SEC
-0.00
-0.00
-0.00
-0.00
-0.00
CALC
F/A
-0.000000
-0.000000
-0.000000
-o.oooooo
-0.000000
COMPRESSOR
DISCHARGE
TEMP
DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
ENGINE
PRESSURE
RATIO
EPR
-0.00
-0.00
-o.oo
-0.00
-0.00
TURBINE
INLET
-0.00
-o.oo
-0.00
-o.oo
-0.00
POWER EXHAUST
PERCENT GAS
RATED TE«P
T.O. DEGREES F
-0.00
-0.00
-0.00
-0.00
-0.00
EXHAUST
GAS
PRESSURE
PSM
-0.00
-0.00
-o.oo
-0.00
-0.00
CO
IWETI
PPMV
660.00
100.00
90.00
560.00
70.00
CD
2
IHETI
PERCENT V
1.35
2.00
1.95
I. 10
2.25
THC
IMETI
PPMV
1200.00
30.00
9.00
1200.00
4.50
NO
IHETI
PPMV
a. co
35.60
44.00
6.00
56.00
NO
2
(MET)
PPMV
-0.00
-o.oo
-0.00
-0.00
-0.00
(MET)
PPMV
a.oo
36.00
46.00
9.00
60.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
-0.00
PARTICULATES
-0.00
-0.00
-0.00
-0.00
-0.00
IV-362
-------
TABLE 3T
TURBINE/TURBOPROP ENGINES
(WEIGHTED PROCESSING)
CONTENTS:
V-2 TO V-14 MODEL SUMMARIES
V-l
-------
MODEL T56-A7 TURBOPROP
SAMPLE NUMBER
"DOE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
EMISSION
RATE
LB/HR
MEAN 5.013
STO DEV 2.968
MEAN 2.150
STD OEV 1.285
MFAN 3. 009
STO OEV 0.791
MEAN 3.66H
STD OEV 0.841
MEAN 5.013
STD DEV 2.96S
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
FUEL .
RATE
LB/HR
636.717
15.T61
2079.317
77.480
1908.447
25.675
1052.900
23.937
636.717
15.761
FUEL/CYCLE
LBS POLLUTANT/IK HP-HR/CYCLE
MODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
LBS POLLUTANT/IOOOK
EMISSION
RATE
LB/HR
MEAN I. 462
STD OEV 1.315
MEAN 0.430
STD OEV 0.911
MEAN 0.476
STO OEV 0.976
MEAN 0.517
STD OEV 1.004
MFAN 1.462
STD f>EV 1.315
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
HP-HR AT T.n.
FUEL
RATE
LB/HR
636.717
15.761
2079.317
77.480
1908.447
25.675
1052.900
23.937
636.717
15.761
FUEL/CYCLE
LflS POLLUTANT/IK HP-HR/CYCLE
MODE
TAXI-IDLF
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
LBS POLLUTANT/IOOOK
EMISSION
RATE
LB/HR
MCAN 3.341
STO DEV 0.357
MEAN 22.878
STO OFV 3.566
MEAN 21.212
STO OEV 2.314
MEAN 7.776
STD OEV 0.913
MEAN 3.343
STO OFV 0.357
TOTAL FOR CYCLE
LBS PHLIUTANT/1K Lfl
HP-HR AT T.O.
FUEL
RATE
LB/HR
(.36. 717
15.761
2079.317
77.480
1908.447
75.675
1052.900
23.937
636.717
15.761
FUEL/CYCLE
LRS POLLUTANT/IK HP-HR/CYCLE
LBS POLLUTANT/IOOOK
HP-HR AT T.O.
TIME IN
NODE
MIN.
19.00
0.0
0.50
0.0
2.50
0.0
4.50
0.0
7.00
0.0
MEAN:
STO DEV:
MEAN:
STO OEV:
MEAN:
STO OEV:
MEAN:
STO OEV:
TIME IN
MODE
MIN.
19.00
0.0
0.50
0.0
2.50
0.0
4.50
0.0
7.00
0.0
MEAN:
STO OEV:
MEAN:
STD OEV:
MEAN:
STD DEV:
MEAN:
STO DEV:
TIME IN
MODE
MIN.
19.00
0.0
0.50
0.0
2.50
0.0
4.50
0.0
7.00
0.0
MEAN:
STD DEVI
MEAN:
STD OEV:
MEAN:
STD DEV:
MEAN:
STD OEV:
CO
MASS
LBS.
0.794
0.470
o.oie
0.011
0.125
0.033
0.275
0.063
0.292
0.173
1.504
0.675
3.329
1.488
4.247
1.907
0.477
0.285
HC
MASS
LBS.
0.232
0.208
0.004
0.008
0.020
0.041
0.039
0.075
0.085
0.077
0.379
0.359
0.842
0.799
1.070
1.014
0.955
2.021
NOX
MASS
LBS.
0.529
0.056
0.191
0.0)0
0.884
0.096
0.583
0.068
0.195
0.021
2.382
0.232
5.269
0.454
6.725
0.654
SO. 773
7.914
FUEL
MASS
LBS.
201.63
4.98
17.33
0.65
79.52
1.08
78.97
1.79
74.28
1.84
451.72
7.42
FUEL
MASS
LBS.
201.63
4.98
17.33
0.65
79.52
l.Ofl
78.97
1.79
74.28
1.84
451.72
7.42
FUEL
MASS
LBS.
201.63
4.98
17.33
0.65
79.52
1.08
78.97
1.79
74.20
1.64
451.72
7.42
LB CO /
IK LB FUEL
7.654
4.590
1.0*0
0.627
1.579
0.421
3.482
0.787
7.854
4.590
LB HC /
IK LB FUEL
2.298
2.056
0.207
0.438
0.250
0.512
0.491
0.952
2.298
2.056
LB NOX/
IK LB FUEL
5.245
0.488
10.984
1.501
11.111
1.154
7.382
O.B12
5.245
0.488
ENERGY
HP-MR
71.3*
0.13
31.29
0.03
1*0.81
0.18
84.49
0.1*
26.28
0.0
35*. 22
0.0
ENERGY
HP-HR
71.3*
0.13
31.29
0.03
1*0.81
0.18
84.49
0.1*
26.28
0.0
35*. 22
0.0
ENERGY
HP-HR
71.3*
0.13
31.29
0.03
140.81
0.18
84.49
0.14
26.28
0.0
354.22
0.0
LB CO /
HP-HR
0.01112
0.006S9
0.00057
0.0001*
0.00089
0.00023
0.00326
0.00075
0.01112
0.00659
LB HC /
HP-HR
0.00325
0.00292
0.00011
0.0002*
0.0001*
0.00029
0.000*6
0.00089
0.00325
0.00292
LB NOX/
HP-HR
0.007*2
0.00079
0.00609
0.00095
0.00628
0.00068
0.00690
0.00081
0.007*2
0.00079
V-2
-------
MODEL T56-A15 TURBOPROP
S«HPLE NUMBER
MODE
.TAXI-IDLE
TAKEOFF
CLIHROUT
APPROACH
TAXI-IDLE
EMISSION
RATE
LB/HR
MEAN 4. 896
STD DEV 0.855
MEAN 3.765
STD DEV 1.293
MEAN 3.404
STO DEV 0.801
MEAN 3. tat
STD DEV 0.848
MEAN 4. 896
STD DEV 0.855
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
FUEL .
RATE
IB/MR
677.688
67.967
2392.661
124.766
2188.467
95.255
1145.895
19.792
677.688
67.967
FUEL/CYCLF.
LBS POLLUTANT/IK MP-HR/CYCLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLF
LBS POLLUTANT/1000K
EMISSION
RATE
LB/HR
MFAN 1.156
STD DEV 1.424
MEAN 0.440
STD DEV 0.666
MEAN 0.399
STO DEV 0.590
MEAN 0.326
sin OEV 0.321
MEAN I.I 58
STD OEV 1.424
TOTAL FOR CYCLF
LBS POLLUTANT/IK L9
HP-HR AT T.O.
FUEL
RATE
LB/HR
677. 6SB
67.967
2192.661
124.766
21B8.467
95.255
1145.895
19.792
677.688
67.967
FUEL/CYCLE
LBS POLLUTANT/ IK MP-HR/CYCLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
L3S POLLUTANT/1000K
FMISSION
RATF
LB/HR
MFAN 2.086
STD OEV 1.654
MEAN 27.898
STD OEV 11.51?
MEAN 22.201
STD DEV 3.532
MF.AN 7.323
STD DEV 1 .5TCI
MEAN 2.886
STD DEV 1.654
TOTAL FHR CYCLE
LBS POLLUTANT/IK LB
HP-HR AT T.O.
FUEL
RATE
LB/HR
677.688
67.967
2197.661
124.766
2180.467
9S.J55
1145.095
19.792
677.688
67.967
FUEL/CYCLE
LBS POLLUTANT/IK HP-HR/CYCLE
LBS POLLUTANT/1000K
HP-HR AT T.O.
TIME IN
MODE
MIN.
19.00
0.0
0.50
0.0
2.50
0.0
4.50
0.0
7.00
0.0
MEAN:
STO DEVI
MEAN!
STD DEVI
MEAN:
STD DEV:
MEAN:
STD DEV:
TIME IN
NODE
MIN.
19.00
0.0
0.50
0.0
2.50
0.0
4.50
0.0
7.00
0.0
MEAN:
STO DEV:
MEAN:
STD OEV:
MEAN:
STD DEV:
MEAN:
STO [JEV:
TIME IN
MODE
HIN.
19.00
0.0
0.50
0.0
2.50
0.0
4.50
0.0
7.00
0.0
MEAN:
STD OEV:
MEAN:
STD OEV:
MEAN:
STD DEV:
MEAN:
STD OEV:
CO
MASS
LBS.
0.775
0.139
0.031
0.011
0.142
0.033
0.262
0.064
0.286
0.050
1.496
0.214
3.045
0.372
3.454
0.494
0.683
0.235
HC
MASS
LBS.
0.183
0.225
0.004
0.006
0.017
0.025
0.024
0.024
0.068
0.083
0.296
0.331
0.592
0.642
0.683
0.765
0.798
1.210
NOX
MASS
LBS.
0.457
0.262
0.232
0.096
0.925
0.147
0.549
0.118
0.168
0.096
2.332
0.605
4.723
1.038
5.305
1.396
50.619
20.932
FUEL
MASS
LBS.
214.60
21.52
19.94
1.04
91.19
3.97
85.94
1.48
79.06
7.93
490.73
30.21
FUEL
MASS
LBS.
214.60
21.52
19.94
1.04
91.19
3.97
85.94
1.48
79.0*
7.93
490.73
30. 21
FUEL
MASS
LBS.
214.60
21.52.
19.94
1.04
91. 19
3.97
85.94
1.48
79.06
7.93
490.73
30.21
LB CO /
IK LB FUEL
7.221
0.992
1.565
0.491
1.549
0.317
3.044
0.731
7.221
0.992
LB HC /
IK LB FUEL
1.687
2.037
0.179
0.272
0. 179
0.267
0.286
0.281
1.687
2.037
LB NOX/
IK LB FUEL
4.181
2.175
11.655
4.769
10.141
1.550
6.384
1.324
4.161
2.175
ENERGY
HP-HR
87.23
0.13
38.26
0.05
172.16
0.08
103.30
0.15
32.14
0.0
433.08
0.43
ENERGY
HP-HB
87.23
0.13
38.26
0.05
172.16
0.08
103.30
0.15
32.14
0.0
433.08
0.43
ENERGY
HP-HR
87.23
0.11
38.26
0.05
172.16
0.08
103.30
0.15
32.14
o.o
413.08
0.43
LB
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
LB
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
LB
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
CO /
HP-HR
00889
00155
00062
00028
00082
00019
00253
00062
00889
00155
HC /
HP-HR
00210
00258
00010
00015
00010
00014
00024
00023
00210
00258
NDX/
HP-HR
00524
00100
00608
00251
00537
00085
00532
00114
00524
00300
V-3
-------
MODEL TPF-331 TURBOPROP
SAMPLE NUMBER 3.
MODE
TIKI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
EMISSION
RATE
LB/HR
MEAN 9.241
Sm OEV 0.286
MEAN 0.393
STD DEV 0.309
MEAN 0.568
STD OEV 0.313
MEAN 2.582
STO DEV 0.4*3
MEAN 1.249
STn DEV 0.286
TOTAL FOR CYCLE
LBS POLLUTANT/IK L8
FUEL
RATE
LB/HR
167.770
11.581
365.419
9.366
339.093
10.361
206.096
7.348
162.770
11.581
FUEL/CYCLE
LBS POLLUTANT/IK HP-HR/CYCLE
MOOE
TAXI-IOLE
TAKEOFF
ClIMBOUT
APPROACH
TAXI-IDLE
LBS POLLUTANT/1000K
EMISSION
RATE
LB/HR
MEAN 0.586
STO DEV 0.226
MEAN 0.055
STD OEV 0.062
MEAN 0.053
STD REV 0.060
HFAN 0.240
STD OEV 0.125
MFAN 0.586
STO OEV 0.226
TOTAL FDR CYCLE
LBS POLLUTANT/IK LB
HP-HR AT T.O.
FUEL
RATE
L8/HR
162.770
11.581
365.419
9.366
339.093
10.361
206.096
7.348
162.770
11.581
FUEL/CYCLE
L6S POLLUTANT/IK HP-HR/CYCLE
"ODE
TAXI-IDLF
TAKEOFF
CLIMBOIIT
APPROACH
TAII-IDLC
L"S PflULUTANT/lOOOK
EMISSION
RATE
LB/HR
MFAN 1.179
STO OEV 0.393
MEAN 3.639
STn OFV 1.276
MEAN 3.313
STO DEV 1.191
MEAN 1.685
STD DEV 0.593
MFAN 1.179
STn DEV 0.393
TOTAL FOR CYCLE
LBS POLLUTANT/IK IB
HP-HR AT T.Q.
FUEL
RATE
LB/HR
162.770
11.581
365.419
9.366
139.093
10.361
206.096
7.348
162.770
11.581
FUEL/CYCLE
IBS POLLUTANT/IK HP-HR/CYCLF
LBS POLLUFANT/1000K
HP-HR AT T.O.
TIME IN
MODE
MIN.
19.00
0.0
0.50
0.0
2.50
0.0
4. 50
0.0
7.00
0.0
MEAN:
STO OEV:
MEAN:
STO OEV!
MEAN:
STD DEV:
MEAN:
STD DEV:
TIME IN
MODE
MIN.
19.00
0.0
0.50
0.0
2.50
0.0
4.50
0.0
7.00
0.0
MEAN:
STO OEV:
MEAN:
STO nEV:
MEAN:
STO OEVI
MEAN:
sro OEV:
TIME IN
MODE
MIN.
19.00
0.0
0.50
0.0
2.50
0.0
4.50
0.0
7.00
0.0
MEAN:
STO OEV:
MEAN:
STD nEV:
MEAN:
STO DEv:
MEAN:
STO OEV:
CO
MASS
LBS.
0.514
0.045
0.003
0.003
0.024
0.013
0. 194
0.033
0.190
0.017
0.924
0.032
8.969
0.241
13.137
0.601
0.556
0.435
HC
MASS
LBS.
0.093
0.036
0.000
0.001
0.002
0.003
0.018
0.009
0.034
0.013
0.14B
0.048
1.444
0.507
2.100
0.695
0.783
0.877
NOK
MASS
LBS.
0.187
0.062
0.030
0.011
0.138
0.050
0.126
0.044
0.069
0.023
0.550
0.185
5.275
1.546
7.831
2.682
51.975
18.794
FUEL
MASS
LBS.
51.54
3.67
3.05
0.08
14.13
0.43
15.46
0.55
18.99
1.35
103.16
5.95
FUEL
MASS
LBS.
51.54
3.67
3.05
0.08
14.13
0.43
15.46
0.55
18.99
1.35
103.16
I 5-"
FUEL
MASS
LBS.
51.54
3.67
3.05
0.08
14.13
0.43
15.46
0.55
18.9>)
1.35
103. 16
5.95
L6 CO /
IK LB FUEL
20.002
1.848
1.082
0.848
1.6S4
0.9)6
12.537
2.145
20.002
1.848
LB HC /
IK LB FUEL
3.640
1.470
0.153
0.175
0. 158
0.1 84
1.177
0.643
3.640
1.470
LB NOK/
IK LB FUEL
7.149
1.976
9.902
3.263
9.706
1.245
8.113
2.641
7.149
1.976
ENERGY
HP -MR
22.23
0.33
4.87
0.07
21.94
0.32
13.16
0.19
8.19
0.12
TO. 39
1.04
ENERGY
HP-HR
22.23
0.33
4.87
0.07
21.94
0.32
13.16
0.19
8.19
0.12
70.39
1.04
ENERGY
HP-HR
22.23
0.33
4.H7
0.07
21.94
0.32
13.16
0.19
8.19
0.12
70.39
1.04
LB CO /
HP-HR
0.02316
0.00240
0.0006T
0.00052
0.0010T
0.00058
0.01469
0.00235
0.02316
0.00240
LB HC /
HP-HR
0.00418
0.00166
0.00009
0.00011
0.00010
0.00011
0.00136
0.00070
0.00418
0.00166
L3 NOI/
HP-HR
0.00841
0.00283
0.00624
0.00226
0.00631
0.00234
0.00962
0.00347
0.00841
0.00283
V-4
-------
MODEL CJ805
SAMPLE NUMBER
NODE
TA»I-IDLF
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CUMBOUT
APPROACH
TAXt-IDLfi
HQOE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IOLE
EMISSION
RATE
LB/HR
HEAN 61.252
STO OEV 10.965
HEAN 29.071
STO OFV 4.213
HEAN 28.876
STO OF.V 4.592
MEAN 42.825
STO OEV 14.524
HEAN 61.252
STO OEV 10.965
TOTAL FOR CYCLE
LBS POLLUTANT/IK LS
LBS POLLUTANT/IK LI
IBS POLLUTANT/100DK
EMISSION
RITE
LB/HR
MEAN 15.426
Sfn DEV 6.589
MEAN 0.556
STO OEV 0.547
MEAN 0.583
Sro OF.V 0.442
MFAN ?.427
STO OFV 1.982
MFAN 15.426
STO (1EV 6. 589
TOTAL FPR CYCLF
LBS POLLUTANT/IK LB
IBS POLLUTANT/IK LB
LBS POLLUTANT/1000*
EMISSION
RATE
LB/HR
HEAN 2.822
STI1 OEV 0.374
MFAN 110.632
STD DEV 17.743
HEAN 73.982
srn OEV 6.116
MEAN 17.845
STO OEV 1.362
MEAN 2.822
STO OEV 0.374
TOTAL FOR CYCLE
L»S POLLUTANT/IK LR
LBS POLLUTANT/IK 11
L9S POLLUTANT/ IOOOK
FUEL
RATE
LB/HR
1358.432
80.474
9959.773
251.241
8290.375
181.826
3776.597
314.310
1358.432
DO. 474
FUEL/CYCLE
FH-HR/CYCLE
LB TM-HR AT
FUEL
RATE
LB/HR
1358.432
90.474
9959.773
251.241
8290.375
181.826
3776.597
314.310
135*. 432
90.474
FUEL/CYCLE
TH-MR/CYCLE
L« TH-HR AT
FUEL
RATE
LB/HR
1358.43?
80.474
9959.773
251.241
8290.375
181.826
3776.597
314.310
1358.432
80.474
FUFL/CYCLE
TM-HR/CYCLE
L9 TH-HR AT
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STO DEV:
MEAN:
STO OEV:
MEAN:
STO OEv:
r.n. MEAN:
STO OEV:
TINE IN
HOOE
MIN.
19.00
0.0
0.70
o.o
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD OEV:
MEAN:
STO OEV:
MEAN:
STO OEV:
T.o. MEAN:
STO OEV:
T 1 ME IN
MODE
HIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
HEAN:
STO DEv:
HEAN:
STft OEV:
HEAN:
STO OEV:
r.O. MFAN:
STD OEV:
CO
MASS
LBS.
9.698
1.736
0.339
0.049
1.059
0.168
2.855
0.968
3.573
0.640
17.524
3.140
13.921
2.622
15.021
2.692
3.028
0.439
HC
MASS
LBS.
2.442
1.043
0.006
0.006
0.021
0.016
0.162
0.125
0.900
0.3B4
3.532
1.520
2.794
1.185
3.027
1.303
0.579
0.570
NOK
MASS
LBS.
0.447
0.059
1.291
0.207
2.713
0.224
1.190
0.091
0.165
0.02?
5.804
0.334
4.610
0.301
4.975
0.286
115.242
18. 482
FUEL
MASS
LBS.
430.17
25.48
. 116.20
2.93
303.98
6.67
251.77
20.95
158.48
9.39
1260.60
51.81
FUEL
MASS
LBS.
430.17
25.4(1
116.20
2.93
303.98
6.67
251.77
20.95
158.48
9.39
1260.60
51.81
FUEL
MASS
IBS.
430.17
25.48
116.20
2.93
303.98
6.67
251.77
20.95
158.48
9.39
1260.60
51.81
L8 CO /
IK LB FUEL
45.150
8.210
2.921
0.437
3.488
0.584
11.509
4.613
45.190
8.210
LB HC /
IK LB FUEL
11.306
4.718
0.056
0.054
0.070
0.053
0.645
0.493
11.306
4.718
LB N(1X/
IK LB FUEL
2.072
0.181
11.086
1.565
8.917
0.600
4.739
0.336
2.072
0. 181
ENERGY
1 TH-HR
283.73
0.0
130.67
0.13
349.07
0.0
298.67
0.0
104.53
0.09
1166.66
1.81
ENERGY
1 TH-HR
283.73
0.0
130.67
0.13
349.07
0.0
298.67
0.0
104.53
0.09
1166.66
1.81
ENERGY
IH-MR
283.73
0.0
110.67
0.13
349.07
0.0
298.67
0.0
104.53
0.09
1166.66
1.81
IB CO /
TH-HR
0.03418
0.00612
0.00260
0.00038
0.00303
0.00048
0.00956
0.00324
0.03419
0.00612
LB HC /
1 TH-HR
0.00861
0.00368
0.00003
0.00005
0.00006
0.00005
0.00054
0.00042
0.00861
0.00368
LB N0«/
1 TH-HR
0.00157
0.00021
0.00988
0. 00158
0.00777
0.00064
0.00398
0.00030
0.00157
0.00021
V-5
-------
MODEL JTK
SAMPLE NUMBER
NODE
r»xi-ir>LE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
r«KI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
EMISSION
RATE
Lfl/HR
MEAN 79.964
STD OEV 42.60)
MEAN 9.036
STD OEV 7.896
MEAN 15.957
STD OEV 8.429
MEAN 49.015
STO OEV 23.793
MEAN 79.964
STD OEV 42.60}
TOTAL FDR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION
RATE
LB/HR
MEAN 34.294
STO 06V 34.950
MFAN 0.855
STD OEV 1.346
MEAN 0.893
STD DEV 0.598
MEAN 8.261
STD REV 6.687
MEAN 34.294
STO OEV 34.950
TOTAL FHR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
L1S POLLUTANT/IOOOK
EMISSION
RATE
L8/HR
MFAN 4.16B
STD OEV 0.764
MEAN 119.008
STO OFV 75.788
MEAN 84.675
STD OEV 13.642
MEAN 23.212
STP nEV 2.698
MEAN 4.168
STD DEV 0.764
TOTAL FUR CYCLE
LBS POLLUTANT/IK LB
LBS PflLLUTANT/lK LB
LRS POLLUTANT/IOOOK
FUEL
RATE .
LB/HR
1613.686
85.354
10183.211
413.273
8509.188
342.477
4115.418
245.341
1613.686
85.354
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
1613.686
85.354
10183.211
413.273
8509.188
342.477
4115.418
245.341
1613.686
85.354
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
Lfl/HO
1613.606
85.354
10103.211
413.273
8509.188
342.477
4115.418
245.341
1613.686
85.354
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD DEV:
MEANI
STD DEV:
MEAN:
STO OEV:
T.O. MEAN:
STO OEV:
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STO OEV:
MEAN:
STO DEV:
MEAN:
STD OEV:
T.O. MEAN:
STD OEV:
TIMF IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD DEv:
MEANI
STO OEV:
MEAN:
STO OEV:
T.n. MEAN:
STD DEV:
CO
MASS
LBS.
12.661
6.745
0.105
0.092
0.5B5
0.309
3.268
1.586
4.665
2.4B5
21.284
10.969
15.309
7.957
15.682
8.038
O.BB2
0.764
HC
MASS
LBS.
5.430
5.534
0.010
0.016
0.033
0.022
0.551
0.446
2.001
2.039
8.024
7.979
5.7)5
5.565
5.964
5.871
0.864
1.362
NOX
MASS
LBS.
0.660
0.121
1.388
0.301
3.105
0.500
1.547
O.lflO
0.243
0.045
6.944
0.970
4.953
0.750
5.183
0.649
116.72?
23.396
FUEL
MASS
LBS.
511.00
27.02
118.80
4.82
312.00
12.56
274.36
16.36
188.26
9.96
1404.43
57.76
FUEL
MASS
LBS.
511.00
27.02
118.80
4.82
312.00
12.56
274.36
16.36
188.26
9.96
1404.43
57.76
FUEL
MASS
LBS.
511.00
27.02
118.80
4. 82
312.00
12.56
274.36
16.36
188.26
9.96
1404.43
57.76
LB CO /
IK LB FUEL
50.073
26.690
0.879
0.756
1.873
0.972
12.199
6.355
50.073
26.690
L6 HC /
IK LB FUEL
21.355
21.049
0.086
0.135
0.106
0.071
2.018
1.626
21.355
21.049
LB NOX/
IK LB FUEL
2.596
0.530
11.637
2.240
9.929
1.398
5.654
0.7)4
2.596
0.530
ENERGY
TH-HR
375.48
11.97
138.33
4.41
369.55
11.78
316.19
10.08
138.33
4.41
1337.88
42.69
ENERGY
1 TH-HR
375.48
11.97
138.33
4.41
369.55
11.78
316.19
10.08
138. 33
4.41
1337. BB
42.69
ENF.RGY
1 TH-HR
375.48
11.97
138.33
4.41
369.55
11.78
316.19
10.08
138.33
4.41
1337.88
42.69
LB CO /
TH-HR
0.03368
0.01765
0.00076
0.00066
0.00158
0.00082
0.01030
0.00489
0.03368
0.01765
LB HC /
TH-HR
0.01438
0.01451
0.00007
0.00012
0.00009
0.00006
0.00173
0.00139
0.01438
0.01451
LB NOX/
t TH-HR
0.00176
0.00030
0.01000
0.00201
0.00839
0.00122
0.00490
0.00061
0.00176
0.00030
V-6
-------
MODEL JT3D
SAMPLE NUMBER 26.
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIHBOUT
APPROACH
TAXI-IDLE
EMISSION
RATE
LB/HR
MEAN 68.835
STD OEV 37.515
MEAN 12.269
STO DEV 6.507
MEAN 15.303
STO DEV T.92T
MEAN 39.678
STO OEV 19.966
MEAN 68.835
STD OEV 37. SIS
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
EMISSION
RATE
LB/HR
MEAN 41.22;
STD DEV 28.7*8
MEAN 4.65*
STO OEV 8.731
MEAN 4.915
STD OEV 8.419
MEAN 7.842
STO 1EV 6.332
MEAN 41.225
STD OEV 28.748
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
EMISSION
RATE
LB/HR
MEAN 3.208
STO riEV 0.801
MEAN 148.125
STO OEV 25.842
MEAN 96.218
STD OEV 14.259
MFAN 21.784
STO OEV 3.099
MEAN 3.20R
STO OEV 0.801
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOOOK
FUEL
RATE
LB/HR
1379.321
241.812
10835.269
821.060
89SS.805
662.439
41)7.551
350.089
1379.321
241.612
FUEL/CYCLE
TM-HR/CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
1)79.321
241.812
10835.289
821.060
8955.805
662.439
4137.551
350.089
1379.321
241.812
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
1379.321
241.812
10835.289
821.060
8955.805
662.439
41)7.551
350.089
1379.321
241.812
FUEL/CYCLE
TH-HR/CYCLE
IB TH-HR AT
TIME IN
NODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD OEV:
MEAN:
STO DEV:
MEAN:
STO DEV:
T.O. MEAN:
STO OEV:
TIME IN
NODE
NIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD DEV:
MEAN:
STD OEV:
MEAN:
STO OEV:
T.O. MEAN:
STO OEV:
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD OEV:
MEAN!
STO DEV:
MEAN:
STD DEV:
T.O. MEAN:
STO OEV:
CO
MASS
LBS.
10.699
5.940
0.143
0.099
0.561
0.291
2.645
1.332
4.015
2.188
18.264
8.963
I3.S48
6.031
8.734
4.290
0.768
0.522
HC
MASS
LBS.
6.527
4.552
0.054
0.102
0.180
0.309
0.523
0.422
2.405
1.677
9.669
6.206
7.256
4.498
4.642
2.961
2.933
5.627
NOX
MASS
LBS.
0.508
0.127
1.728
0.301
3.528
0.523
1.452
0.207
0.187
0.047
7.404
1.072
5.596
0.729
).538
0.375
93.083
12.371
FUEL
MASS
LBS.
436.78
76.S6
126.41
9.58
326.38
24.29
275.64
23.34
160.92
28.21
1326.33
138.11
FUEL
MASS
LBS.
436.78
76.58
126.41
9.58
326.36
24.29
275.84
23.34
160.92
28.21
1328.33
138.11
FUEL
MASS
LBS.
436.78
76.58
126.41
9.58
328.38
24.29
275.84
23.34
160.92
28.21
1328.33
1)8. 11
LB CO /
IK LB FUEL
46.865
22.791
1.137
0.7B1
1.735
0.940
9.634
4.650
48.665
22.791
LB HC /
IK 18 FUEL
30.301
20.478
0.416
0.783
0.536
0.912
1.884
1.491
30.301
20.478
LB NOX/
IK LB FUEL
2.)42
0.528
13.613
1.656
10.720
1.097
5.277
0.694
2.342
0.528
ENERGY
» TH-HR
565.83
36.14
215.83
13.32
576.56
35.57
493.33
30.43
215.83
13.32
2087.41
128.65
ENERGY
TH-HR
585.83
36.14
215.83
13.32
576.58
35.57
493.33
30.43
215.83
13.32
2087.41
126.65
ENERGY
f TH-HR
585.83
36.14
215.83
1).)2
576.58
35.57
493.3)
30.4)
215.83
13.32
2087.41
128.65
LB CO /
1 TH-HR
0.01855
0.01007
0.00066
0.00045
0.00098
0.00052
0.00539
0. 00280
0.01655
0.01007
LB HC /
TH-HR
0.0111)
0.00773
0. 00025
0.00048
0.00031
0.00055
0.00107
0.00089
0.01113
0.00773
LB NOX/
t TH-HR
0.00087
0.00020
0.00798
0.00106
0.00610
0.00066
0.00294
0.00035
0.00087
0.00020
V-7
-------
HnnFL JT4A
SAMPLF. NUMBER
none
.TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IOIF
TAKEOFF
r.LIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
EMISSION
RITE
LB/HR
MFAN 45.917
STD DEV 2*. 398
MEAN 18.823
STn OEV 3. 914
MFAN 18.277
STn OEV J.I29
MEAN 26.326
STO OEV 9.529
MEAN 45.917
STD OEV 24.398
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS PflLLUTANT/lOOOK
EMISSION
DATE
LB/HR
MEAN 23.0IB
STD DEV 14.995
MFAN 0.674
STO OEV 0.934
MEAN 1.274
STn DEV 2.120
MEAN 3.834
STR OEV 7.383
MEAN 23.01ft
STO OEV 14.995
TOTAL FPR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLL UT ANT/ 1000K
EMISSION
RATE
LP/HR
MFAN 5.608
STO DFV 0.754
MEAN 236. J35
STO OEV 28.993
MFAN 155.298
STD DFV 9.813
MEAN 35.859
STO OEV 4.203
MEAN 5.60B
STR OEV 0.754
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/IOHOK
FUEL
RATE
Lfl/HR
2061.813
107.011
15511.203
427.062
13066.484
240.685
5993.734
324.933
2061.813
107.011
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
Lfl/HR
2061.813
107.011
15511.203
427.062
13066.484
240.685
5993.734
324.933
2061.813
107.011
FUEL/CYCLE
TH-HR/CYCLE
FUEL
RATE
LB/HR
2061.81)
107.011
15511.203
427.062
13066.484
240. 685
5993.734
324.933
2061.813
107.011
FUEL/CYCLE
TH-HR/CYCLE
L>» TH-HR AT
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STO DEVI
MEAN1
STD DEV:
MEAN:
STD OEV1
1.0. MEANI
STD DEV.
TIME IN
MODE
MIN.
19.00
0.0
0.70
o.n
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD OEv:
MFANl
STO OEV:
MEAN:
STO DEV:
STO OEv:
TIME IN
MOOS
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD HEV:
MEAN:
STD DEV:
MEAN:
STD f>EV:
1.0. MEAN:
sro nEv:
CO
MASS
LBS.
7.270
3.863
0.220
0.047
0.670
0.115
1.755
0.635
2.678
1.423
12.513
5.922
6.462
3.067
6.378
2.999
1.255
0.266
HC
MASS
LBS.
3.645
2.374
0.008
0.011
0.047
0.078
0.256
0.159
1.343
0.875
5.297
3.378
2.711
1.733
2.683
1.711
0.623
NOX
MASS
LBS.
0.888
0.119
2.757
0.338
5.694
0.360
2.391
0.280
0.327
0.044
12.057
0.669
6.176
0.340
6.106
0.331
157.557
19.321
FUEL
MASS
LBS.
652.11
33.81
180.16
4.98
479.10
8.78
399.58
21.66
240. 54
12.41
1153.10
71.33
FUEL
MASS
LBS.
652.91
33.89
180.96
4.98
4T9.IO
8.78
399.58
21.66
240.54
12.41
1953.10
71.33
FUEL
MASS
IBS.
652.91
33.89
180.16
4.18
479. 10
8.76
399.58
71.66
240.54
12.41
1153.10
71.33
LB CO /
IK LB FUEL
22.282
11.867
1.214
0.218
1.311
0.235
4.412
1.67I
22.282
1 1. 867
LB HC /
IK LB FUEL
11.183
7.427
0.043
0.060
0.096
0.160
0.646
0.413
11.183
7.427
LB NOX/
IK LB FUEL
2.714
0.270
15.224
1.714
11.881
0.641
5.976
0.526
2.714
0.270
ENERGY
TH-HR
554.17
0.38
204.17
0.0
545.42
0.0
466.67
0.0
204.17
0.0
1174.58
2.62
ENERGY
1 TH-HR
554.17
0.38
204.17
0.0
545.42
0.0
466.67
0.0
204.17
0.0
1974.58
2.62
ENERGY
* TH-HR
554.17
0.38
204.17
0.0
545.42
0.0
466.67
0.0
704.17
0.0
1974.58
2.67
LB CO /
» TH-HR
0.01312
0.00697
o.ooioe
0.00023
0.00123
0.00021
0.00376
0.00136
0.01312
0.00697
LB HC /
TH-HR
0.00658
0.00428
0.00004
0.00005
0. 00009
0.00014
0.00055
0.00034
0.00658
0.00428
LB 1QX/
TH-HR
0.00160
0.00022
0.01350
0.00166
0.01044
0.00066
0.00512
0.00060
0.00160
0.00022
V-8
-------
MODEL JTBO UNDIl REGULAR
SAMPLE NUMBER
HOOE
.TAXI-IDLE
TAKEOFF
CLIM80UT
APPROACH
TAXI-IOLF
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLINBOUT
APPROACH
TAXI-IDLE
EMISSION
RATE
LB/HR
MEAN 38.771
STO OEV 6. MO
MEAN 7.175
STO DEV 3.35*
MEAN 10.621
STO DEV 4.385
MEAN 17.920
STD OEV 1.665
MEAN 18.771
STD OEV 6.410
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
IBS POLLUTANT/IK LB
LBS POLLUTANT /1000K
EMISSION
RATE
LB/HR
MEAN 6.199
STD DEV 1.506
MEAN (1.171
STD OEV 0.563
MEAN 0.313
STO OEV 0.459
MEAN 1.179
STn OEV 1.372
MEAN 6.199
STO OEV 1 .506
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/ IOOOK
EMISSION
RATE
LB/HR
MEAN 2. 958
STD OFV 0.349
MEAN 101.636
STO OEV 14.360
MEAN 67.746
STO HEV 11.251
MEAN 16.952
STD OEV 2.870
MEAN 2.958
STO DEV 0.349
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/ IK LB
LBS POLLUTANT/1000K
FUEL .
RATE
LB/HR
1130.935
66.837
8517.727
165. B92
7116.582
95.555
3445.414
180.022
1130.935
66.837
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
1130.935
66.837
8517.727
165.892
7116.582
95.555
3445.414
180.022
1130.915
66.817
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATF
LB/HR
1130.935
66.837
8517.727
165.892
7116.582
95.555
1445.414
190.022
1130.935
66.837
FUEL/CYCLE
TH-HR/CYCLE
L9 TH-HR AT
TIKE IN
MODE
NIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STO OEVl
MEAN:
STD DEV:
MEAN:
STO OEV:
T.O. MEAN:
STO OEV:
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STO OEV:
MEAN:
STO OEV:
MEAN:
STD DEV:
T.O. MEAN:
STO DEV:
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
NEAN:
STD OEV:
MEAN:
STO OEV:
MEAN:
STD DEV:
T.O. MEAN:
STO DEV:
cn
MASS
LBS.
8.189
1.354
0.093
0.039
0.389
0.161
1.195
0.111
3.017
0.499
12.883
2.020
11.905
1.659
8.481
1.330
0.665
0.279
HC
MASS
LBS.
1.309
0.318
0.004
0.007
0.011
0.017
0.079
0.091
0.482
0.117
1.886
0.444
1.751
0.432
1.242
0.292
0.311
0.469
NOX
MASS
LBS.
0.625
0.074
1.186
0.168
2.484
0.413
1. 130
0.191
0.230
0.027
5.655 .
0.631
5.249
0.701
3.723
0.415
84.697
11.967
FUEL
MASS
LBS.
358.13
21.16
99.37
1.94
260.94
3.51
229.69
12.00
131.94
7.80
1080.08
30.02
FUEL
MASS
LBS.
358.13
21.16
99.37
1.94
260.94
3.51
229.69
12.00
131.94
7.80
1080.08
30.02
FUEL
MASS
LBS.
358.13
21.16
99.37
1.94
260.94
3.51
229.69
12.00
111.94
7.80
1080. OB
30.02
LB CO /
IK LB FUEL
34.
4.
0.
0.
1.
0.
5.
0.
34.
4.
153
333
934
388
493
617
210
518
153
315
LB HC /
IK IB FUEL
5.
I.
0.
0.
0.
0.
0.
0.
5.
1.
515
449
043
066
044
065
332
368
515
449
LB NOX/
u LB FUEL
2.
0.
11.
1.
9.
1.
4.
1.
2.
0.
624
152
930
644
517
559
959
097
624
352
ENERGY
1 TH-HR
199.00
0.0
163.13
0.0
416.13
0.0
373.33
0.0
147.00
0.10
1519.00
2.15
ENERGY
TH-HR
399.00
0.0
163.33
0.0
436.33
0.0
373.33
0.0
147.00
0.10
1519.00
2.35
ENERGY
1 TH-HR
399.00
0.0
163.13
0.0
416.33
0.0
373.33
0.0
147.00
0.10
1519.00
2.15
LB
1
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
LB
1
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
LB
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
CO /
TH-HR
02052
00319
00057
00024
00089
00037
00320
00010
02052
00119
HC /
TH-«R
00328
00080
00003
00004
00003
00004
00021
00024
00328
00080
NOX/
TH-HR
00157
00018
00726
00103
00569
00095
00103
00051
00157
00018
V-9
-------
MODEL jren UNOIL SHORELESS SAMPLE NUMBFR - is.
NODE
.TA«I-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
MORE
TAXI-IDLF
TAKEOFF
CLIMfldUr
APPROACH
TAXI-IOLF
EMISSION
RATE
LB/HR
MFAN 2*. 677
STD OEV 10.147
MFAN 5.617
STO DEV I. Ill
MEAN 6.204
Sm DEV 1.978
MEAN 11.960
STO OEV 4.937
MEAN 2*. 677
srn DEV 10.147
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
FM1SSION
RATE
LB/HR
MEAN 5.422
STO OFV 7.066
MEAN 0.3HI
STD OEV 0.040
MEAN 0.396
STO DEV 0.736
MEAN 0.850
STD OEV 0.913
MEAN 5.422
STO flEV 7.066
TOTAL FOR CYCLF
LBS POLLUTANT/IK L9
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION
PATE
LB/HR
MFAN 2.90R
STO OEV 0.708
MEAN U3.295
STF1 OEV 33.587
MFAN 86.972
STD DEV 19.477
MEAN 20.242
STD OFV 5.826
MEAN 2.908
STD DEV 0.708
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LRS POLLUTANT/IK LB
LRS POLLUTANT/1000K
FUEL.
RATE
LB/HR
1134.241
107. 2B7
8677.555
210.983
7171.270
160.470
3572.512
452.440
1134.241
107.287
FUEL/CYCLE
TH-HR/CYCLE
IB TH-HR AT
FUEL
RATE
LB/HR
1134.241
107.287
B677.555
210.9B3
7171.770
160.470
3572.512
452.440
1134.241
107.287
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
1134.241
107.287
8677.555
210. 983
7171.270
160.470
1572.512
452.440
1134.241
107.787
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD OEV:
MEAN:
STD DEV:
DEAN:
STD DEV:
T.O. MEAN:
STD DEV:
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD DEV:
MEAN:
STD DEV:
MEAN:
STD DEV:
T.O. KEAN:
STD DEV:
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD DEV:
MEAN:
STO DEV:
MFAN:
STD OEV:
T.O. MEAN:
STD DEV:
CO
MASS
LBS.
5.212
2.143
0.066
0.023
0.727
0.071
0.797
0.329
1.920
0.790
8.223
3.201
7.610
3.020
5.227
2.034
0.452
0.161
HC
MASS
LBS.
1.145
1.492
0.004
0.010
0.015
0.027
0.057
0.061
0.422
0.550
1.643
2.045
1.538
2.025
1.044
1.300
0.307
0.676
NOX
MASS
LBS.
0.614
0.150
1.555
0.392
3.189
0.714
1.349
(1.368
0.7.76
D.055
6.934
1.607
6.34A
1.538
4.407
1.07.7
107.249
27.024
FUEL
MASS
LBS.
359.18
33.97
101.24
2.45
262.95
5. 88
238.17
30.16
132.33
12.52
1093.86
66.40
FUEL
MASS
LBS.
359.18
33.97
101.24
2.45
262.95
5.88
238.17
30.16
132.33
12.52
1093.86
66.40
FUEL
MASS
LBS.
359.18
33.97
101.24
2.45
262.95
5.88
238. 17
30.16
132.33
12.52
1093.86
66.40
LB CO /
IK LB FUEL
7.2.
9.
0.
0.
0.
0.
3.
1.
22.
9.
234
223
648
232
867
274
420
486
234
223
LB HC /
IK L9 FUEL
5.
7.
0.
0.
0.
0.
0.
0.
5.
7.
013
130
044
097
055
098
224
195
013
130
LB NOX/
IK LB FUEL
2.
0.
15.
3.
12.
2.
5.
1.
2.
0.
5K4
718
344
825
111
631
663
509
584
718
ENERGY
1 TH-HR
413.25
1.11
169.17
0.11
451.92
0.94
386.67
0.59
152.25
0.12
1573.25
1.68
ENERGY
1 TH-HR
413.25
1.11
169.17
0.11
451.92
0.94
386.67
0.59
152.25
0.12
1573.25
1.68
ENERGY
f TH-HP
413.25
1.11
169.17
0.11
451.92
0.94
386.67
0.59
152.25
0.12
1573.25
1.68
LB CO /
TH-HR
0.01261
0.00519
0.00039
0.00014
0.00050
0.00016
0.00206
0.00085
0.01261
0.00519
LB HC /
1 TH-HR
0.00277
0.00361
0.00003
0.00006
0.00001
0.00006
0.00015
0.00016
0.00277
0.00361
LB NOX/
* TH-HR
0.00149
0.00036
0.00919
0.00232
0.00706
0. 00153
0.00349
0.00100
0.00149
0.00036
v-io
-------
MODEL JTBI> OIL REGULAR
SAMPLE NUMBER
MODE
.TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MROE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IOLE
MOOF
TAXI-IDLE
TAKEOFF
CLIMRflUT
APPROACH
TAXI-IDLE
EMISSION
RATE
UP/MS
MEAN 42.965
STD OEV 10.107
MEAN 18.54*
STD OEV 15.916
MEAN 19.401
STD OEV 14.506
MEAN 32.325
STD OEV 9.911
MEAN 42.965
STD DEV 10.107
TOTAL FC1R CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
IBS POLLUTANT/1000K
FMISSION
RATE
LB/HR
MEAN 8. 845
STD OEV 4.791
MEAN 0.316
STO OFV 0.321
MEAN 0.827
STO OEV 1.042
MEAN 3.341
STD 1EV 2.130
MFAN 8.845
STO DEV 4.791
TOTAL FOR CYCLE
L*S POLLUTANT/IK LB
LBS POLLUTANT/IK LB
IIS PDLLUTANT/IOOOK
EMISSION
RATE
LB/HR
MEAN 4.391
STO DEV 1.608
MEAN 151.272
STO DFV 21.703
MEAN 100.144
STO OEV 19.169
MFAN 28.048
STO OEV 3.055
MEAN 4.393
STD DEV 1 .60R
TOTAL FOB CYCLE
LBS POLLUTANT/IK IB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
FUEL .
RATE
LB/HR
1158.716
210.721
8407.422
181.373
7098.539
179.837
1456.895
208.301
1158.716
210.721
FUEL /CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
1158.716
210.721
8407.422
181.173
7098.539
179.817
3458.895
208.301
1158.716
210.771
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
1158.716
210.721
8407.422
181.373
7098.519
179.837
1458.895
20B.301
1158.716
210.721
FUEL/CYCLE
TH-HH/CYCLE
LB TH-HR AT
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEANl
STO OEV:
MEAN!
STO DEV:
MEAN:
STO OEV:
T.O. MEAN:
STO OEV:
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
stn OEV:
MEAN:
STO OEV:
MEAN!
STD OEV:
T.O. MEAN:
STO DEV:
TIME IN
MOOF
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MFAN:
STD OEV:
MEAN:
STD DEVI
MEAN:
STO OEV:
T.O. MEAN:
STD DEV:
CO
MASS
LBS.
9.075
2.115
0.216
0.186
0.711
0.532
2.155
0.661
3.343
0.786
15.501
3.356
14.363
3.457
10.205
2.210
1.545
1.326
HC
MASS
IBS.
1.868
1.012
0.004
0.004
0.030
0.038
0.223
0.145
0.688
0.173
2.813
1.495
2.533
1.281
1.852
0.984
0.263
0.268
NOX
MASS
LBS.
0.928
0.340
1.765
0.253
3.672
0.703
1.870
0.204
0.342
0.125
9.576
1.077
7.913
1.121
5.646
0.709
126.060
18.086
FUEL
MASS
LBS.
366.93
66.71
96.09
2.12
260.28
6.60
230.59
13.89
135.18
24.58
1091.07
105.81
FUEL
MASS
LBS.
366.93
66.73
98.09
2.12
260.28
6.60
230.59
13.89
115.18
24.58
1091.07
105.81
FUEL
MASS
LBS.
366.93
66.73
98.09
2.1?
260.28
6.60
210.59
13.89
115.18
24.58
1091.07
105.81
LB CO /
IK LB FUEL
17.890
9.091
2.224
1.961
2.759
2.115
9.468
3.253
37.890
9.093
LB HC /
IK LH FUEL
7.391
3.565
0.038
0.019
0.117
0.146
0.977
0.656
7.391
3.565
LB NOI/
IK LB FUEL
3.732
0.923
18.000
2.561
14.116
2.679
8.128
0.957
1.732
0.923
ENERGY
1 TH-HR
199.00
0.0
163.11
0.0
416.13
0.0
171.13
0.0
147.00
0.10
1519.00
2.35
ENERGY
t TH-HR
399.00
0.0
163.11
0.0
436.11
0.0
171.11
0.0
147.00
0.10
1519.00
2.35
ENERGY
1 TH-HR
399.00
0.0
163.33
0.0
436.33
0.0
373.33
0.0
147.00
0.10
1519.00
2.35
LB CO /
1 TH-HR
0.02274
0.00535
0.00112
0.00114
0.00163
0.00122
0.00577
0.00177
0.02274
0.00535
LB HC /
TH-HR
0.00468
0.00254
0.00002
0.00002
0.00007
0.00009
0.00060
0.00039
0.00468
0.00254
LB NOX/
t TH-HR
0.00213
0.00085
0.01081
0.00155
0.00842
0.00161
0.00501
0.00055
0.00233
0.00085
V-ll
-------
MODEL JT8D Oil SMOKELESS
SAMPLE NUMBER » 26.
MODE
TAXI-IOLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAX1-IOLE
TAKEOFF
CLIMROUT
APPROACH
TAXI-IOLE
MC10E
TAXI-IOLF
TAKEOFF
CLIMBOUT
APPROACH
IAXI-IOLF
EMISSION
RATE
LB/HR
MEAN 31.429
STn OEV 13.034
MEAN 7.490
STD BEV 5.447
MEAN 8.892
STD OEV 4.648
MEAN 18.184
STO nEV 6.147
MEAN 11.429
STO OEV 13.034
TOTAL FOR CYCLE
IBS POLLUTANT/IK IB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
FMISS10N
RATE
LB/HR
MFAN 5.126
STD DFV 2.307
MFAN 0.778
STD DEV 1.094
MEAN 0.921
STO OEV 0.994
MEAN 1.753
STD DFV O.B84
MFAN 5.126
STO DEV 2.307
TOTAL FOR CYCLE
LRS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION
RATE
LB/HR
MEAN 4.596
STO OFV 1.524
MEAN 197.742
STO DEV 35.161
MEAN 131.017
STO OEV 19.775
MEAN 30.850
STO OEV 4.724
MFAN 4.596
STO OEV 1 .524
TOTAL FOR CYCLE
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
FUEL
RATE
LB/HR
1216.623
51.803
8754.512
375.860
73)6.766
266.697
3408.656
167.198
1216.623
51.803
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
LB/HR
1216. (.23
51.B03
8754.512
375.860
7336.766
266.697
3408.656
167.198
1216.623
51.803
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATE
LR/HR
1216.623
51.B03
8754.512
375.860
7336. 766
266.697
340B.656
167. 19B
1216.623
5I.H03
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STO DEV:
MEAN:
STO OEV:
MEAN:
STO OEV:
T.O. MEAN:
STO OEV:
T1HF IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STO OEV:
MEAN:
STO OEV:
MEAN:
STO DEV:
T.O. MEAN:
STO OEV:
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STO OEV:
MEAN:
STO OEV:
MEAN:
STO OEV:
T.O. MEAN:
STD OEV:
CO
MASS
LBS.
6.63B
2.753
0.087
0.064
0.326
0.178
1.212
0.410
2.446
1.014
10.710
3.974
9.494
3.308
6.775
2.372
0.604
0.442
HC
MASS
LBS.
1.0B3
0.487
0.009
0.013
0.034
0.036
0.117
0.059
0.399
0.180
1.641
0.720
1.461
0.640
1.043
0.457
0.613
0.862
NOX
MASS
IRS.
0.971
0.322
2.307
0.410
4.804
0.725
2.057
0.315
0.358
0.119
10.496
1.547
9.320
1.291
6.662
0.880
158.640
24.647
FUEL
MASS
LBS.
383.26
16.43
102.14
4.38
269.01
9.77
227.24
11.15
141.94
6.05
1125.60
39.53
FUEL
MASS
LBS.
3B5.26
16.43
102.14
4.38
269.01
9.77
227.24
11. 15
141.94
6.05
1125.60
39.53
FUFL
MASS
LBS.
365.26
16.41
102.14
4.38
269.01
9.77
227.24
11.15
141.94
6.05
1125.60
39.53
LB CO /
IK LB FUEL
25.641
9.996
0.855
0.629
1.214
0.671
5. 335
1.758
25.841
9.996
LB HC /
IK LB FUEL
4.234
1.903
0.067
0.122
0.124
0.134
0.515
0.262
4.234
1.903
LB NOX/
IK LB FUEL
3.796
1.263
22.513
3.393
17.822
2.133
9.055
1.307
3.796
1.263
ENERGY
1 TH-HR
413.25
14.59
169.17
3.95
451.91
15.92
386.67
13.61
152.25
5.36
1573.25
55.33
ENERGY
t TH-HR
413.25
14.59
169.17
5.95
431.91
15.92
366.67
13.61
152.25
5.36
1573.25
55.33
ENERGY
f TH-HR
413.25
14.59
169.17
5.95
451.91
15.92
366.67
13.61
152.25
5.36
1573.25
55.33
LB CO /
TH-HR
0.01597
0.0062J
0.00052
0.00036
0.00072
0.00040
0.00313
0.00105
0.01397
0.00623
LB HC /
< TH-HR
0.00262
0.00118
0.00005
0.00007
0.00007
0.00008
0.00030
0.00015
0.00262
0.00118
LB NOX/
TH-HR
0.00235
0.00077
0.01360
0.00211
0.01061
0.00140
0.00532
0.00081
0.00235
0.00077
V-12
-------
MODEL JT90
SAMPLE NUMBER
MODE
.TAXI-IDLE
TAKEOFF
ClIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IOLF
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
MODE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
EMISSION
RATC
LB/HR
MEAN 76.41%
STn nEV 16.204
MEAN 8.291
STD DEV 5.363
MEAN 11.741
STD OEV 3.670
MEAN 12.570
STO DEV 11.269
MEAN 78.415
STD DEV 16.204
TOTAL FOR CYCLF
LBS POLLUTANT/IK LB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION
RATE
LB/HR
MEAN 11.359
STO OEV 3.099
MEAN 2.953
STO OEV 2.215
MFAN 2.647
STO DF.V 1.806
MFAN 2.997
STO DEV 1.376
MFAN 11.359
STB OFV 3.099
TOTAL FOR CYCLE
L8S POLLUTANT/IK Lfl
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
FMISSION
RATE
Lfl/HR
MFAN 10.323
STD OF.V 2.594
MFAN 719.951
STn 1EV 151.642
MEAN 458.604
STn !>EV 81 .739
MEAN 54.101
Sin OFV 5.727
MEAN 10.323
STn DF.V 2.594
TOTAL FOR CYCLE
LflS PtJLI UTANT/lIt LB
LBS POLLUTANT/IK LB
LflS POLLUTANT/1000K
FUEL
RATE
LB/HR
2294.865
207.822
17052.313
821.375
14316.879
820.809
5203. B95
46B.229
2294.865
207.822
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RATF
LB/HR
2294. B65
207.822
17052.313
821.375
14316.879
820.809
5203. 695
468.229
2294.865
207.822
FUEL/CYCLE
TM-HR/CYCLE
LB TH-HR AT
FUF.L
RATE
LB/HR
2294.665
207.822
17052.313
821.375
14316.879
820.609
5203.695
46H.229
2294.865
207.622
FUEL/CYCLE
TM-HR/CYCLE
LB TH-HR AT
TINE IN
MODE
NIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD DEV:
MEAN:
STO DEV:
MEAN!
STO DEV:
T.O. MEAN:
STD DEV:
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD OEV:
MEAN:
STD DEV:
MEAN:
STD DEV:
T.O. MEAN:
STD DEV:
TIME IN
MODE
MIN.
19.00
0.0
0.70
0.0
2.70
0.0
4.00
0.0
7.00
0.0
MEAN:
STD OFV:
MEAN!
STD nEV:
MFAN:
STD nEV:
T.O. MEAN:
STD nEV:
CO
MASS
LBS.
16.563
3.422
0.097
0.063
0.430
0.135
2.171
0.751
6.102
1.261
25.363
4.698
12.258
1.866
5.263
1.062
0.218
0.143
HC
MASS
LBS.
2.399
0.655
0.034
0.026
0.097
0.066
0.200
0.092
0.864
0.241
3.615
0.881
1.756
0.431
0.749
0.186
0.779
0.587
NOX
MASS
LBS.
2.180
0.548
8.399
1.769
16.815
2.997
3.607
0.382
0.603
0.202
31.605
5.075
15.386
1.952
6.593
1.135
188.690
41.875
FUEL
MASS
LBS.
726.71
69.82
198.94
9.58
524.95
30.09
346.93
31.21
267.73
24.24
2065.26
152.07
FUEL
MASS
L6S.
726.71
65.82
196.94
9.56
524.95
30.09
346.93
31.21
267.73
24.24
2065.26
152.07
FUEL
MASS
LBS.
726.71
65.62
198.94
9. 59
524.95
30.09
346.93
31.21
267.73
24.24
2065.26
152.07
LB CO /
IK LB FUEL
34.027
5.209
0.487
0.320
0.823
0.264
6.419
2.808
34.027
5.209
LB HC /
IK LB FUEL
4.965
1.304
0.173
0.131
0. 164
0.127
0.590
0.286
4.965
1.304
L8 NOX/
IK LB FUEL
4.535
1.198
41.990
7.069
31.892
4.201
10.457
1.323
4.535
1.198
ENERGY
f TH-HR
1483.32
35.13
520.46
12.30
1390.38
32.86
892.22
21.14
546.49
12.92
4832.86
114.19
ENERGY
TH-HR
1483.32
35.13
520.46
17.30
1390.38
32.86
892.22
21.14
546.49
12.92
4832.86
114.19
ENERGY
1 TH-HR
1483.32
35.13
520.46
12.30
1390.38
32.86
692.22
21.14
546.49
17.92
4832.66
114.19
LB CO /
1 TH-HR
0.01120
0.00252
0.00019
0.00012
0.00031
0.00010
0.00243
0.00080
0.01120
0.00252
Lfl HC /
TH-HR
0.00162
0.00045
0.00007
.0.00005
0.00007
0.00005
0.00022
0.00010
0.00162
0.00045
LB NOX/
1 TH-HR
0.00147
0.00036
0.01617
0.00359
0.01212
0.00233
0.00404
0.000*4
0.00147
0.00036
V-13
-------
MODEL SPET MK/511
SAMPLE NUMBER
MCIOE
TAXI-IDLE
TAKEOFF
CLIMBOUT
APPROACH
TAXI-IDLE
NODE
TAXI-IOLF.
TAKEOFF
CLIMflOUT
APPROACH
TAXI-IDLE
NOOF.
TAXI-IDLE
'AKEOFF
CLIMROUT
APPROACH
TAXl-IDLF
EMISSION
RATE
IB/MR
MEAN 72.437
STO DEV 19.468
MEAN 14.218
STO HFV 2.944
MEAN 15.251
STD nfv I.B04
MEAN 39.068
STD OFV 10.078
MEAN 72.437
STO DEV 19.468
TOTAL FOR CYCLE
LBS POLLUTANT/IK IB
LBS POLLUTANT/IK LB
LBS POLLUTANT/1000K
EMISSION
RATE
L8/HR
MEAN 32.473
STD DEV 17.225
MEAN 0.0
STD OEV 0.0
MEAN 0.242
STO DEV 0.221
MEAN 4.224
STD 1EV 4.447
MEAN 32.473
STD OFV 17.225
TOTAL FOR CVCLE
LBS PQLLIITANT/1K LB
L3S POLLUTANT/IK LB
L«S POLLUTANT/1000K
EMISSION
RMTf
LB/HR
MFAN 2.493
STD DEV 0.597
MEAN 153.012
STO OF.V 9. 845
MEAN 114.759
STD OEV 11.72',
MEAN 30.446
STO DEV 5.197
MFAN 2.493
STD OEV 0.597
TOTAL FOR CYCLE
L1S POLLUTANT/IK LH
L3S POLLUTANT/IK LB
L«S POLLUTANT/1000K
FUEL
RATE
LB/HR
IOBB.944
30.210
7625.230
150.022
6354.934
60.839
3051.668
123. 020
10BB.944
30.210
FUEL/CYCLE
TH-HR/CYCLE
LB TH-HR AT
FUEL
RAT;
LB/HR
IOB8.944
30.210
7625.230
150.022
6354.934
60.839
3051. 66H
123.021
1088.9*4
30.210
FUEL /CYCLE
TH-HR/CYCLE
LB TH-HO AT
FUFL
RATE
LB/HR
1089.944
30.210
7625.230
150.022
6354.934
60.839
3D51.669
123.021
1188.944
30.210
FUEL/CYCLE
TH-HK/CYCLE
LB TH-HR AT
TIME IN
MOOf
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MEAN:
STD DEV:
MEAN!
STD OEV:
MFAN:
STD DFv:
T.O. MEAN:
STD DEV:
TIME IN
NdOE
MIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MF.AN:
STD OEV:
MEAN:
STD DEV:
MEAN:
STO OEV:
1.0. MEAN:
STO DEV:
TIME IN
«OD£
HIN.
19.00
0.0
0.70
0.0
2.20
0.0
4.00
0.0
7.00
0.0
MFAN:
STD OEV!
MEAN:
STD DFV:
MEAN:
sro DEV:
T.O. MEAN:
STO DEV:
cn
MASS
LBS.
11.469
3. 082
0.166
0.034
0.559
0.066
2.605
0.672
4.226
1.136
19.024
4.775
19.117
4.932
16.021
4.021
1.455
0.301
HC
MASS
LBS.
5.142
2.727
0.0
0.0
0.009
0.001
0.2B2
0.296
1.694
1.005
7.326
4.017
7.372
4.055
6.170
3.382
0.0
0.0
NOX
MASS
LBS.
0.395
0.094
1.7B5
0.115
4.208
0.503
2.030
0.346
0. 145
0.035
1.563
0.910
fl.575
0. 75R
7.211
0.766
156.591
10.075
FUEL
MASS
L6S.
344.63
9.55
88.96
1.75
233.01
2.24
203.44
8.21
127.04
3.52
997.30
19.64
FUEL
MASS
LBS.
344.83
9.55
68.96
1.75
233.01
2.24
203.44
B.2I
127.04
3.52
997.30
19.64
FUEL
MASS
LBS.
344.83
9.55
88.96
1.75
233.01
2.24
203.44
8.21
127.04
3.52
997.30
19. 84
Lfl CO /
IK L8 FUEL
66.737
18.639
1.870
0.426
2.401
0.298
12.868
3.550
66.737
18.639
LB HC /
IK LB FUEL
30.000
16.121
0.0
0.0
0.038
0.035
1.394
1.451
30.000
16.121
LB NOX/
IK LH fUEL
2.289
0.546
20.081
1.519
18.073
2.316
9.939
1. 331
2.289
0.546
ENERGY
< TH-HR
288.80
0.0
133.00
0.25
355.30
0.0
304.00
0.0
106.40
0.06
1187.50
0.0
ENERGY
TH-HR
288.60
0.0
133.00
0.25
355.30
0.0
304.00
0.0
106.40
0.06
1187.50
0.0
ENERGY
f TH-HR
268.60
0.0
133.00
0.25
355.30
0.0
304.00
0.0
106.40
0.06
1187.50
0.0
LB CO /
TH-HR
0.03971
0.01067
0.00125
0.00026
0.00157
0.00019
0.00857
0.00221
0.03971
0.01067
LB HC /
t TH-HR
0.01780
0.00944
0.0
0.0
0.00003
0.00002
0.00093
0.0009B
0.01760
0.00944
LB NOX/
TH-MR
0.00137
0.00033
0.01342
0.00086
0.011B4
0.00142
0.00666
0.00114
0.00137
0.00033
V-14
------- |