Determination of Effects of Ambient Conditions on Aircraft Engine Emissions Engine Testing

EPA-460/3-76-009-b
March 1976
                     DETERMINATION
                           OF EFFECTS
            OF AMBIENT CONDITIONS
                ON AIRCRAFT ENGINE
                             EMISSIONS
                    ENGINE TESTING -
                         GTCP 85 APU,
                TPE 331  TURBOPROP
                              VOLUME 2
      I .S. {ENVIRONMENTAL PROTECTION AGENCY
          Oilier of Air and Waste Management
       Offiee of Mobile Sonree Air Pollution Control
         Emission Control Technology Division
            Ann Arbor, Miebigan 48105

-------
                          EPA-460/3-76-009-b
    DETERMINATION OF EFFECTS
      OF AMBIENT CONDITIONS
 ON AIRCRAFT ENGINE EMISSIONS
           ENGINE TESTING -
GTCP 85 APU, TPE 331 TURBOPROP
                VOLUME 2
                      by

               G.A. Slogar and R.C. Holder

           AiResearch Manufacturing Company of Ari/.ona
              A Division of The Garretl Corporation
                 402 South 36th Street
                 Phoenix, Arizona 85034


                 Contract No. 68-03-2156


               EPA Project Officer: Gary Austin


                    Prepared for

            ENVIRONMENTAL PROTECTION AGENCY
              Office of Air and Waste Management
            Office of Mobile Source Air Pollution Control
              Emission Control Technology Division
                Ann Arbor, Michigan 48105

                    March 1976

-------
This report is issued by the Environmental Protection Agency to report technical
data of interest to a limited number of readers.  Copies are available free of
charge to Federal employees, current contractors and grantees, and nonprofit
organizations - as  supplies permit - from the Air Pollution Technical Information
Center, Environmental Protection Agency, Research Triangle Park, North
Carolina 27711; or, for a fee, from the National Technical Information Service,
5285 Port Royal Road, Springfield, Virginia 22161.
This report was furnished to the Environmental Protection Agency by AiResearch
Manufacturing Company of Arizona, Phoenix, Arizona 85034, in fulfillment
of Contract No. 68-03-2156.  The contents of this report are reproduced
herein as received from AiResearch Manufacturing Company of Arizona.
The opinions, findings, and conclusions  expressed are those of the
author and not necessarily those of the Environmental Protection Agency.
Mention of company or product names is not to be considered as an endorsement
by the Environmental Protection Agency.
                       Publication No. EPA-460/3-76-009-b
                                  11

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                      DETERMINATION OF EFFECTS
                       OF AMBIENT CONDITIONS
                    ON AIRCRAFT ENGINE EMISSIONS
                           ENGINE TESTING
                    GTCP85 APU, TPE331 TURBOPROP
1.0  INTRODUCTION

     The aircraft engine emissions measurement test program outlined
herein was performed by AiResearch Manufacturing Company of Arizona, A
Division of The Garrett Corporation, to determine the effect of ambient
conditions on aircraft engine emissions under Contract 68-03-2156 for
the Environmental Protection Agency, Emission Control Technology
Division, Ann Arbor, Michigan.

     The purpose of this program was to measure exhaust emissions of
hydrocarbons, carbon monoxide, smoke, and oxides of nitrogen from an
AiResearch Turboprop Engine Model TPE331, and a Gas Turbine Auxiliary
Power Unit (APU) GTCP85, when tested under controlled ambient condi-
tions of humidity, temperature, and pressure.  The test program ini-
tially was to be 8 months.  A supplemental program was subsequently
added to investigate the necessary modifications to the turboprop en-
gine fuel management system required to meet 1979 EPA aircraft engine
emissions standards, and the program was extended to 12 months.

     The ultimate application of data generated in the program will be
the specification of correction factors for the effect of ambient con-
ditions on small gas turbine engine exhaust emissions.  Definition of
these correction factors by Calspan Corporation may eliminate the
requirement for controlled-environment testing of production engines
to determine compliance with the EPA 1979 Aircraft and Aircraft Engine
Emissions Standards after the humidity/emissions relationship is char-
acterized for that particular engine type or model.
                                  Page 1

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     Therefore, all data gathered during this program was transmitted
to the Calspan Corporation, Buffalo,  New York, where the data was
subjected to statistical analysis to  assist in deriving an empirical
correlation between variations in ambient conditions and exhaust emis-
sions for each candidate test engine.
                               Page 2

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2. 0  SUMMARY

     This report volume comprises all final engine load conditions, and
gaseous and particulate, emissions data reduction computer output for
an 85 Series APU and TPE331 turboprop engine related to this test pro-
gram.  APU output data is presented first, followed by similar format
TPE331 engine output data reduction results.

     The APU was operated at each of the 16 ambient test conditions
listed in Table 1.  Three consecutive engine load cycles Ceach cycle
defined as the engine loads shown in Table 2)  were run and the 240 test
data points were catalogued herein, as shown in Table 3.

     Similarly, the TPE331 turboprop engine was subjected to 7 engine
load conditions (specified in Table 4) and repeated two additional
times to comprise 3 consecutive load cycles.  Approximately 336 test
data points were reduced and catalogued herein, as indicated by
Table 5.

     All measured emissions data was reduced in the AiResearch CDC
6400 computer using AiResearch-developed emissions data reduction pro-
grams.  The gaseous emissions and smoke data reduction procedures con-
form to those outlined in the Federal Register, Volume 38,  Number 136.
                                Page 3

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        TABLE 1




AMBIENT TEST CONDITIONS
Test
Point
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
Temperature
°C
-7.0
-7.0
4.0
4.0
15.0
1
33.0
I
15.0
I
oF
19
19
39
39
59
I
91
I
59
1
Humidity
Grams H2O/
Kilogram Air
1.0
2.0
2.0
5.0
2.0
5.0
7.5
10.0
10.0
15.0
20.0
25.0
7.5
1
Grains H20/
Pound Air
7.0
14.0
14.0
35.0
14.0
35.0
52.5
70.0
70.0
105.0
140.0
175.0
52.5
1
Barometric Pressure
mm Hg
Hold co
inches Hg
nstant at
standard condition,
as specified in U.S.
Standard Atmosphere,
1962, for test cell
altitude.



1
580
660
740
500



1
22.83
25.98
29.13
19.69
    Page 4

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                TABLE 2
     APU Engine Load Conditions
(Corrected  to  59°F  and  29.92  in.  Hg  abs)
Condition
1
2
3
4
5
Load
Idle
Pure Shaft Power
Rated Power
Pure Bleed
Combination
Horsepower
Shaft
-
79.5
198.6
-
45.7
Bleed-Air
-
0
0
245.0
214.3
Total
'
79.5
198.6
245.0
260.0
                Page 5

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        TABLE 3




TEST DATA POINT/CYCLES
Test
Point
(Table 1)
1




2




3
4
5
6
7
8
9
10
11
12
13
14
15
16




Data Tests

Cycle 1
1 - Cond 1*
2 - Cond 2*
3 - Cond 3*
4 - Cond 4*
5 - Cond 5*
16 - Cond 1
17 - Cond 2
18 - Cond 3
19 - Cond 4
20 - Cond 5
31 - 35
46 - 50
61 - 65
76 - 80
91 - 95
106 - 110
121 - 125
136 - 140
151 - 155
166 - 170
181 - 185
196 - 200
211 - 215
226 - Cond 1
227 - Cond 2
228 - Cond 3
229 - Cond 4
230 « Cond 5

Cycle 2
6 - Cond 1
7 - Cond 2
8 - Cond 3
9 - Cond 5
10 - Cond 5
21 - Cond 1
22' - Cond 2
23 - Cond 3
24 - Cond 4
25 - Cond 5
36 - 40
51 - 55
66 - 70
81 - 85
96 - 100
111 - 115
126 - 130
141 - 145
156 - 160
171 - 175
186 - 190
201 - 205
216 - 220
231 - Cond 1
232 - Cond 2
233 - Cond 3
234 - Cond 4
235 - Cond 5


Cycle 3
11 - Cond 1
12 - Cond 2
13 - Cond 3
14 - Cond 4
15 - Cond 5
26 - Cond 1
27 - Cond 2
28 - Cond 3
29 - Cond 4
30 - Cond 5
41 - 45
56 - 60
71 - 75
86 - 90
101 - 105
116 - 120
131 - 135
146 - 150
161 - 165
176 - 180
191 - 195
206 - 210
221 - 225
236 - Cond 1
237 - Cond 2
238 - Cond 3
239 - Cond 4
240 - Cond 5
"Conditions 1 through 5 of Table 2
»_^____— 	 • 	 mt
      Page  6

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TABLE 4







TPE 331 ENGINE LOAD CONDITIONS
(Corrected to 59 °F and 29.92 in. Hg abs)
Condition
1*
2*
3*
4
5
6
7 **
Load
(Taxi) Idle
1.5 x Idle
2.0 x Idle
Approach
Cruise
Climb-Out
Takeoff
Percent of
Rated Power
5
7.5
10.0
30.0
70.0
90.0
100.0
Corrected
Total Shaft
Horsepower
42
63
84
252
588
756
840
*Engine operation on primary fuel atomizers only.
**A derated takeoff load of 706 shp//66 was necessary to protect
the engine from turbine interstage overtemperature.







Page 7

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TABLE 5
TEST DATA POINT/CYCLES
Test
Point
(Table 1)
1






2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
Data Tests
Cycle 1
1 - Cond 1*
2 - Cond 2*
3 - Cond 3*
4 - Cond 4*
5 - Cond 5*
6 - Cond 6*
7 - Cond 7*
22 - 28
43 - 49
64 - 70
885 - 91
106 - 112
127 - 133
148 - 154
169 - 175
190 - 196
211 - 217
232 - 238
253 - 259
274 - 280
295 - 301
316 - 322
Cycle 2
8 - Cond 1
9 - Cond 2
10 - Cond 3
11 - Cond 4
12 - Cond 5
13 - Cond 6
14 - Cond 7
29 - 35
50 - 56
71 - 77
92 - 98
113 - 119
134 - 140
155 - 161
176 - 182
197 - 203
218 - 224
239 - 245
260 - 266
281 - 287
302 - 308
323 - 329
Cycle 3
15 - Cond 1
16 - Cond 2
17 - Cond 3
18 - Cond 4
19 - Cond 5
20 - Cond 6
21 - Cond 7
36 - 42
57 - 63
78 - 84
99 - 105
120 - 126
141 - 147
162 - 168
183 - 189
204 - 210
225 - 231
246 - 252
267 - 273
288 - 294
309 - 315
330 - 336
"Conditions 1 through 7 of Table 4
Page 8

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10
"> ENGINE MFR.! AIRESEARCH TEST FACILITY!
MODEL NO.! GTCP85-96CK S/NI 36179
MAX SHP 20
^ FUEL! AST M 01655-73 ATOMIC H/C R

HYDROCARBONS (HC AS CH4)
> CARSON MONOXIDE (CO)
OXIDES OF NITROGEN (NOX AS
PHX LACC2
ENGINc
0. + BLEED A]
ATIO! 1.92(
K OUTPUT •• C
IONS COMPUTED
.K
1*. 7«
N02) 4.91
COHBUSTOR TYPEI TANGENTIAL CAN P/NS 638168-3 SU5
ENGINE TOTAL SERVICE! 0.0 HR. TIME SINCE ENGINE OVE5
"> ENGINc ASSEMBLY AND MAINTENANCE INFORMATION!
AIRCRAFT INSTALLATION **• MFR. 1
)
l GASEOUS EMISSION TEST NO. 1 1 DATE! 6-17-75 TIC
AMBIENT AIR TEMP.! 19.0 OEG. F "E.ATIVE HUMIDITY!
AMBIENT AIR QUALITY HYDROCARBONS (HOI 0.0 PPMC CAR
SAMPLE LINE •" TEMP.! 300.00 DEG. F. FiOHRATE! 14.1
TEST CONDITION
) POWER SETTING, CORRECTED HP.
Nl SPEED. RPM
FUEL FLON (MEAS.I LB./HR.
> ENGINE CORE INLET AIRFLCH (CALC. ) LB./SEC.
COMPRESSOR INLET TEMP., OEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
) COMPRESSOR DISCHARGE AIR TcMP. , DEG. F
COMPRESSOR BLEED AIRFLOM (MEAS.) LB./SEC.
BLEED AIR PRESSURE, PSIA
> BLEED AIR TEMPERATURE, OEG. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION. MET ANALYSIS
) HYDROCARBON ( HC AS CH4) , PPMC
CARBON MONOXIDE (CO) , PPMV
TOTAL OXIDES OF NITROGEN (NOX) , PPMV
) CARBON DIOXIDE (C02) , PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
) HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
) EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
) TOTAL OXIDES OF NITROGEN (NOX AS N02)
ENGINE NORK OUTPUT, MEAS. SHP
ENGINE HORK OUTPUT, ISENTROPIC AIR HP
) ENGINE MORK OUTPUT, TOTA. HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EHISSIONSI
1
0.00
41610.00
142.00
6.13
20.0
60.88
364.00
0.00
0.00
-0.00
470.0
130.500
249.616
16.000
1.306
10.500
11.139
37.276
3.925
1.562
5.293
.557
0.00
0.00
0.00
96.15
.086
INSTR.
TfPE (CIA!
R EXTRACT]
LHVI
ODE OF FEE
FROM TES1
3 -B. POL
7 LB. POL
3 wB. POL
c. DESCRIP1
FACE/VOLUf
HAU^I
MODEL NO.
TEST DAT*
E< 9.0S
49. 00 PERC
BON MONOXI
6 LITERS/*
£0 EHISSIO
2
79.52
«1470.00
175.00
5.76
21.0
61.13
369.00
0.00
0.00
-0.00
570.0
68.500
282.571
22.900
1.729
17.000
5.749
32.112
4.275
1.006
5.620
.748
72.84
0.00
72.64
96.74
.008
DESCRIP. 1
iS) 1 APU
ON TO 1
18470.
ERAL REGUL
CONDITION
LUTANT PER
LUTANT PER
LUTANT PER
FEDERAL D
150. DEG.
BTU/iB.
ATIONS TIT
NO. 5
1000 HP.-
1000 MP.-
1000 HP.-
EG V38 N136 CALC. DATE! 6-17-75
CALC. I.D.I 1
F EGT
ADDITIVES! NONE

HR.
HR.
HR.
IE! .725 SQ IN/CU IN FUEL INJ. TYPEI DUAL ORIFICE
0.0 HR.
1 - -- USER1
BARO. PRESS.! 28.470 IN. HCA.
ENT SPECIFIC HUMIDITY! .001000 LB. H20/LB. DRY AIR
0£ (CO)! 0.0 PPHV OXIDES OF NITROGEN (NOX)I 1.0 PPHV
IN. TRANSPORT TIME! 6.50 SEC. LENGTH! 50.00 FT.
3
197.79
41150.00
236.00
5.44
21.0
60.15
378.00
0.00
0.00
-0.00
792.0
24.600
265.169
38.500
2.498
37.000
1.116
22.634
5.019
.263
5.342
1.185
181.16
0.00
161.16
99.37
.012
4
0.00
41070.00
252.00
7.09
20.0
56.37
339.00
2.12
55.14
359.00
870.0
39.010
410.646
42.000
2.916
39.300
1.510
27.624
4.675
.361
7.012
1.176
0.00
244.54
244.54
99.21
.014
5
45.68
41000.00 	
256.08
6.94
21.0
58.18
541.00
1.89 .._._ 	 	 ... 	
56.96
361.00
870.8 	
22.508
298.30% 	
45.800
2.957
42.208
.864
21.032
4.964
• ZZ3 ........ _ . .
5.168
1.281
41.77
219.42
261.19
99.*5 	
.014

-------
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                    ENBINE= GTCP8S-98CK      S/N* 36179
                   RAT SMP*   ZOO.    RA EGT,F= 1150.
              I   FUEL M/C» 1.9ZSO    STOI F/A= .06822
•"•••  AIRESEARCH EMISSION TEST SUMMARY
  COMB P/N* 696168-3 TEST DATE  6-17-75
 RAT SPD- 41600.     OcH PT,F=   8.
   L H V* 18470.     S LN T.Fs 300.0
     FUEL*AV. KERO.    P SARO» 28.47
REL *UM=  49.00    SPEC HUN» .001001
FLO.L/M«  14.160   SL TIH,S«  6.5100
 3


b
DATA POINT NUMBER
PERCENT KAX. CORRECTED POWER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., DEG.F
SHAFT SPEED. Nl, RPM
COMPRESSOR OSCHG. PRES..PSIA
COMPRESSOR OSCHG. TEMP, DEC F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOH, LB/SEC
COMPRESSOR MAP FLOW, LB/SEC
FA RATIO BASED ON HAP FLOH
CORRECTED FUEu FLOW , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING N/F»»N/V/EIT/540I
COMB EFFIC FROM EMISSIONS
CARSON DIOXIDE
PERCENT BY VOLUME, HET
L3. COZ PER LB. OF FUEL
HEIGHT FLOM, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
UN BURNED HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE INO) - HEIGHTS AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE IN02)
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.

0.
0.
0.
470.
41610.
60.
364.0
13.5H
0.000
6.03
.0065
142.0
.0864
.894
.396
98.146

1.31
3.06
435. Z

249.6
37.278
5.293
CARBON,
130.5
11.139
1.582
.2988
N02
10.5
2.576
.366

5.5
1.349
.192
2
39.
79.
72.
570.
41470.
61.1
369.0
13.60
0.000
5.57
.0087
175.8
.0084
.124
.361
98.748

1.73
3.09
540.4

282.6
32.112
5.620
HEIGHTS AS
88.5
5.749
1.886
.1790

17.0
3.173
.555

5.9
1.101
.193
3
98.9
197.8
181.2
792.0
41150.0
60.1
378.0
13.7,
0.001
5.17
.0127
236.0
.0120
.177
.338
99.370

Z.50
3.12
735.2

255.2
22.634
5.342
CH4
24.6
1.116
.263
.0493

37.0
4.824
1.138

1.5
.196
.046
4
8.
0.
0.
070.
41078.
56.4
339.0
13.71
2.130
6.77
.0150
252.0
.0141
.206
.367
99.213
REDUCED
2.92
3.11
702.0

418.6
27.824
7.012

39.0
1.510
.301
.0543

39.3
4.374
1.102

2.7
.301
.076
5
22.0
45.6
41.0
070.0
41000.0
58.2
341.0
13.72
1.915 " " 	 ~ 	
6.73
.0140
256.0 -• •"- 	 -' 	 - 	 - 	 	 -
.0142
.288
.360 	
99.453

2.96
3.12 	
005.0 . -

298.3 	 _ 	 	
20.032 " .
5.160

22.5
.064
.«3 _. ..... 	
.0431

42.2
4. 655
1.281

2.0
. 389
.080 	 ... _
TOTAL OXIDES OF NITROGEN «NO*N02I .AS N02 '
PPK BY VOLUNE. HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMCKE MEASUREMENT DATA
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED WEIGHT FLOW
SMCKE NUMBER
CORRECTED HEIGHT FLOW
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMCKE NUMBER
SMOKE NUMBER AT HA=0.023
16.0
3.925
.557

.00694
25.00
.82083
40.50
.03470
46.40
.04866
54.80
42.20
2Z.9
4.275
.748

.00695
26.21
.02086
42.90
.03477
50.00
.04866
57.11
44.68
38.5
5.019
1.185

.00695
26.20
.82085
41.70
.1)3473
50.00
.04861
57.10
4L. 30
42.0
4.675
1.170

.00695
36.90
.02883
53.60
.03470
66.70
.04859
71.40
57.00
45.0
4.964
1.281

.00694
25.10
.02082
45.21
.13467
51.20
.04852 _. . .
59.50
45.80
                 NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE  HET  VALUES.                                                                	
                       2.EQUIVALENCE RATIO CALCULATED FROM  COZ,CO,AND HC DATA AND FUEL  COMPOSITION.
                       3.MASS EMISSIONS OF MO. N02. AND NO»N02  CALCULATED AS N02 FROM CONCENTRATIONS  KITH MOLECULAR HEIGHT OF N02 (46.01).
                       4.COMBUSTION EFFICIENCY CALCULATED FROM  CO.AND JHC AS VAPORIZED  ORIGINAL FUEL  ON  LB/ LB FUEL OASIS.
                                                          f

-------
na
PJ
IQ
(D
                                              S/N= 36179
                                                             ••••   AIRESEARCH EMISSION TEST  SUMMARY
                                                              COMB P/N= 698168-3 TEST DATE   6-17-75
                     ENGINE' GTCP65-98CK
                   DATA POINT NUMBER
                   EHISSIOK RATE LB/HR
                       CARBON MONOXIDE
                       UNBURNEO HYDROCARBONS
                       OXIDES OF NITROGEN
                       NITRIC OXIDE
                   POMER LEVEL HP
                   TOTAL CORRECTED HORSEPOHER
                   BRAKE SPECIFIC EMISSION INDEX L3/1000HP-HR
                       CARBON MONOXIDE
                       UNBURNEO HYDROCARBONS
                       OXIDES OF NITROGEN
                       NITRIC OXIOE
                       NOT£"0. APPEARING IN BRAKE SPECIFIC  EMISSION INDEX COLUMN DENOTES AN  IDLE CONDITION
                                                                                                           FUEL'AV. KERB.
                                                                                                                             P BAUD' 28.«,7
5.293
1.582
.557
.366
0.00
0.00
'lOOOHf
0.000
0.000
0.000
0.000
5.620
1.006
.7*8
.555
72.8*
79.52
'-MR
77.11,9
13.811
10.270
7.621.
5.3*2
.263
1.185
1.138
181.18
197.79

29.1,82
1 . *»5*
6.538
6.2A3
7.012
.381
1.178
1.102
2**«5*
2*7.15

28.673
1.556
*.»17
*.507
5.168
.223
1.281
1.201
261.19
267.59

19.787
.853
I,. 913
*. 598

-------
                 1     ENGINE  MFS.I  AIRESEARCH
                     MODEL  NO.I   GTCP85-98CK

                 )    FUEL I  ASTH  01655-73
 TEST FACILITY I PHX LACC2       INSTR.  DESCRIP.t   FEDERAL  REG V38 N156    C*LC.
 S/NI  36179          ENGINE TYPE (CLASS)I  APU               CALC. I.O.I     Z
HAX SHP       200. » 8LEEO 1IA EXTRACTION TO    1150.  DEC. f EGT
    ATOMIC H/C RATI01   1.926    LHVI     181.70. BTU/LB.      ADDITIVES! NONE
OATEI  6-17-75
                                EXHAUST EMISSIONS P£* EPA RATED WORK OUTPUT •• COJc OF FEDERAL REGULATIONS TITLE  ".0  PART 87
                               .............................. eMtsSIONS COMPUTED F50M TEST CONDITION NO.  5    •••••••••»•»•«
                                        HYDROCARBONS IHC AS CH4»             .732  LB. POLiUTANT PER 1000 HP.-Hft.
                                        CARBON MONOXIDE (COI               20.120  -B. POLLUTANT PER 1000 HP.-HR.
                                        OXIDES. OF NITROGEN INOX AS NOZI     "..963  LB. POLLUTANT PER 1000 HP.-HR.
                                                                             17 JULY 1973
                    »*•••***»**>••*»»•*••••»*»»•»•*•••*•••*.»«•»•»•*•»..  ENGINE DESCRIPTION  •••»••••••••••••
                    COMBUSTOR  TYPEI  TANGENTIAL CAM          P/NJ  698163-3  SURFACE/VOLUME I  .725 SO. IN/CU  IN
                    ENGINE  TOTAL  SERVICE!     0.0  HR.   TIME SINCE ENGINE OVERHAULI      0.0 HR.
                    ENGINE  ASSEMBLY  AND MAINTENANCE INFORNATIONI
                    AIRCRAFT  INSTALLATION **• NFR. 1
                                                                                 MODEL NO.I
                                                                FUEL INJ. TYPEI
                                                                                                                         USERt
                                                                                    DUAL ORIFICE
                                                                                 TEST OATA SUMMARY »•»••»»*••••••»»••••••»«...»».•»..»»...«..»,....
                    GASEOUS  EMISSION TEST NO. I      1    OATEt  6-17-7S      TINE!    10.15      BARO. PRESS. I   Z8.470 IN.  HGA.
                    AMBIENT  AIR  TEMP.:  19.0   Oct.  F        RELATIVE HUMIDITY!  1.9.00 PERCENT       SPECIFIC  HUHIDITYI  .101001  LB. HZO/LB. DRY AIR
                    AMBIENT  AIR  QUALITY   HYDROCARBONS (HCII 0.0   PPHC    CARSON MONOXIDE (COII 0.0   PPMV     OXIDES OF  NITROGEN INOXII O.I   PPMV
                    SAMPLE LINE  »»•  TEMP.I  3(0.03 DEC. F.     FLOMRATEl   11.16 LITERS/MIN.     TRANSPORT  TIMet    6.50 SEC.      LENGTHI   50.11 FT.
pi
0>
I-1
K>
TEST CONDITION
PONER SETTINGt CORRECTED HP.
Ml SPEED, RPH
FUEL FLCM (MEAS.) LB./HR.
ENGINE CORE INLET AIRFLOM (CA..C. » L8./SEC.
COMPRESSOR INLET TEMP., OEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR T£NP., OEG. F
COMPRESSOR BLEED AIRFLOW (MEAS.) L3./SEC.
BLEED AIR PRESSURE, PSIA
BLEED AIR TEMPERATURE, OEG. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION, NET ANALYSIS
HYDROCARBON (HC AS CH4) , PPNC
CARBON MONOXIDE (CO), PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPMV
CARBON DIOXIDE IC02), P£*C£NT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSION INDCjX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
EMISSICI. RATE, LB. POLLUTANT/H4.
HYDROCARBONS (HC AS CH4I
CARBON MONOXIDE (CO)
TOT At OXIDES OF NITROGEN (NOX AS NOZI
ENGINE HORK OUTPUT. MEAS. SHP
ENGINE HORK OUTPUT, ISENTROPIC AIR HP
ENGINE HORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS!
676
0.00
41630.00
140.00
6.04
Zl.O
61.37
365.09
G.09
0.00
-0.80
471.0

121.500
252.100
16.500
1.306
14.0GO

10.376
37.667
4.050

1.453
5.273
.567
8.00
0.81
0.08
98.28
.186
79.60
1.11.70.00
175.00
5.88
20.0
61.28
368.00
8.00
0.00
-0.00
571.0

84.008
281.017
23.508
1.694
17.588

5.569
32.593
4.477

.975
5.704
.784
72.84
0.80
72.84
98.74
.008
197.74
41141.00
238.80
5.41
Zl.O
60.15
377.00
0.00
0.00
-0.08
789.0

25.200
295.657
39.088
2.534
36.508

1.127
23.126
5.011

.268
5.504
1.193
181.14
8.00
181.14
99.36
.812
9
8.01
41040.00
250.11
7.06
Zl.O
56.42
338.88
2.12
55.14
358.00
867.0

39.000
404.399
41.500
2.918
89.001

1.511
27.417
4.621

.371
6.852
1.155
(.00
244.81
244.81
99.22
.114
11
45.64
40990.11
- 257.01
6.89
20. 8
57.94
31.8.88
1.89
56.81
368.11
678.1

19.581
306.306
46.111
2.974 •
43.008 ._!__. 	

.744
21.451
5.145

• 191-
5.256
1.296
41.76
219.45
261.21
99.45
.114

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 •0
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iQ
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ENGINE^ GTCP85-98CK S/N* 36179
RAT SHP= ZOO. RA EGT,F=
FUEL */C= 1.9280 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POUER
CORRECTED SHAFT -HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., DEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR OSCHG. PRES. ,PSIA
COMPRESSOR DSCHG. TEMP, BEG F
EXHAUST GAS PRESS.. PSIA
CORRECTED BLEED FLOM, LB/SEC
COMPRESSOR MAP FLOM.LB/SEC
FA RATIO BASED ON MAP FLOH
CORRECTED FUEL FLOW , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P**N/V/ECT/540I
COM3 £FFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON HONOXIOE
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUE..
HEIGHT FLOH. LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE .4
27.407
fc.852

39.0
1.511
.378
.0551

89.0
9.908
Z.1,77

-47.5
-5.288
-1.322

41.5
4.620
1.155

.00696
35.70
.02191
54.80
.03483
66.70
.04875
73.80
58.30
8. REL HUH' 49.00 SPEC HUM* .001000
300.0 FLO.L/H* 14.160 SL TIM, S* 6.5000
18
22.
45. . 	
41.
670.
40990.
57.
340.0
13.71
1.913
6.72
.0148
257.0
.0143
.209
.362
99.454

Z.97
3.12 . . . . . .......
601.8

306.3 ....... 	
20.450
5.256
. .. . 	 _
19.5
.744
.191 ...........
.0364

43.0 .. ... .. 	 	 	 	 _.
4.716
1.Z1Z
_ ..
3.0
.329
.085

46.0
5.045 	
1.296

.00697 . . ... . 	
28.60
.02095
42.90 	
.03490
53.60
.04885
59. SO
46.60

                        NOTES 1.  ALL EMISSIONS CONCENTRATIONS  ARE  MET  VALUES.

                              2.EQUIVALENCE RATIO CALCULATED FROM  C02.CO.ANO HC DATA AND FUEk COMPOSITION.

                              3.MASS EMISSIONS OF NO, NOZ,  AND NO»N02  CALCULATED AS NOZ FROM CONCENTRATIONS MITH MOLECULAR HEIGHT OF NOZ 146.011.

                              4.COMBUSTION EFFICIENCY CALCULATED FROM  CO,AND UHC AS VAPORIZED ORIGINAL  FUEL ON LB/ LB FUEL BASIS.           .

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ENGINE: STCP85-98CK S/N
DATA POINT NUMBER
EMISSIOK RATE LB/HR
CARBON MONOXIDE
UNBURNED HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIDE
POWER LEVEL HP
TOTAL CORRECTED HORSEPOWER
BRAKE SPECIFIC EMISSION INDEX
CARBON MONOXIDE
UNBURNEO HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIDE
* 36179
6

5.273
1.453
.567
.401
0.00
0.00
LB/1000HP-HR
0.000
0.000
0.000
0.030
CONS P/NS
7

5.704
.975
.704
.513
72.04
79.60

78.304
13.379
10.756
0.010
698168-3
0

5.504
.268
1.193
1.116
101.14
197.74

30.305
1.480
6.504
6.16Z
TEST DATE
9

6.852
.371
1.155
2.477
244.00
2n7.41

27.948
1.543
4.711
10.110
6-17-75
10

5.256
.191
1.296
1.21Z
261.21
267.4]

20.120
.732
4.963
4.640
                                                                                                          FU£L=A».  KERO.
                                                                                                                            P BARO«
                        NOTE"9. APPEARING IN 3R«<£ SPECIFIC EMISSION INDEX COtUHN DENOTES AN IDLE CONDITION

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                    ">    ENGINE  MFR.l  AIRESEARCH
                        MODEL  NO.I   6TCP65-98CK

                        FUELI  ASTH  01655-73
                                TEST FACILITYl PHX LACC2        INSTR.  OESCRIP.l   FEDERAL «G V38 N136    CALC.
                                S/NI  36179          ENGINE  TYPE  (CLASS)I   AFU               CALC. I.D.I     3
                               MAX SHP       200. » BLEED AIR EXTRACTION TO    1150. DEC. F EGT
                                   ATOMIC H/C RATIO!   1.928    LHW1     18<>70.  BTU/LB.      AOOITIVESI NONE
                                                                                                                                        OATEI  6-17-75
                                   EXHAUST EMISSIONS PER EPA RATED  WORK  OUTPUT  ••  CODE OF FEDERAL REGULATIONS TITLE  ".0  PART  67
                                  ..it........................... EMISSIONS  COMPUTED FROM TEST CONDITION NO.  5    ••••••»•••••••
                                           HYDROCARBONS (HC AS  CHI,)              .735  LB. POLLUTANT PER 1000 HP.-HR.
                                           CARBON MONOXIDE  (CO)               20.207  LB. POLLUTANT PER 1000 HP.-HR.
                                           OXIDES OF NITROGEN  (NOX  AS N02)      *.97l,  LB. POLLUTANT PER 1000 HP.-HR.
                                                                                                                                    17 JULY 1973
[[[  ENGIN£ DESCRIPTION  • ""••••""•"
COMBUSTOR TYPE I TANGENTIAL  CAN          P/NI  691893-3  SURFACE/VOLUME I   .725  SO. IN/CU IN
ENGINE TOTAL SERVICE!     0.0   MR.   TIME SINCE ENGINE OVERHAULI       0.0  HR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                       AIRCRAFT  INSTALLATION »»• MFR.l
                                                                                     MODEL NO.I
                                                                                                                       FUEL  INJ.  TYPE!
                                                                                                                             USER!
                                                                                                                                           DUAL ORIFICE
                       •••••••••••••••••••"••••••••••••••••••••"•••••OPERATIONAL TEST DATA SUMMARY •""••"•""""""""""•"""•""•""•
                       GASEOJS EMISSION TEST NO.I     1    DATE I   6-17-75       TIMEI                BARD. PRESS.I   28.1,70  IN.  HGA.
                       AMBIENT AIR  TEHP.t  19.0  OEG. F        RELATIVE  HUMIDITY!   «9.00 PERCENT       SPECIFIC HUMIDITY!   .001000  LB. H20/LB. DRY AIR
                       AMBIENT AIR  QUALITY    HYDROCARBONS (HOI  0.0    PPMC     CARBON MONOXIDE (CO)! 0.0   PPMV     OXIDES OF  NITROGEN (NOX)I 0.0   PPMV
                       SAMPLE LINE  ••*  TEMP. I  300.00 DEG. F.      FLOWRtTEl    11.. 16 iITERS/HIN.     TRANSPORT  TIME!     6.50 SEC.      LENGTHI   50.01 FT.

CARBON HONOXIOE ICO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CHI,)
CARBON HONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02I
ENGINE HORK OUTPUT, MEAS. SHP
ENGINE WORK OUTPUT, ISENTROPIC AIR HP
ENGINE WORK OUTPUT. TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS)
11 12 13 1*
0.00
1,1620.00
11.0.00
6.01.
21.0
61.1.7
365.00
0.00
0.00
-0.00
1,69.0

121.500
251.. 593
17.000
1.306
I*. 000

10.371.
36.032
<>.172

1.1.52
5.325
.581.
0.00
0.00
0.00
96.26
.006
79.75
1,11,69.00
17%. 00
5.91
16.0
61.62
366.00
0.00
0.00
-0.00
565.0

82.500
272.273
23.500
1.677
17.000

5.528
31.920
4.525

.962
5.55*
.787
72.62
I. 00
72.82
96.76
.006
198.11
1,1130.00
237.00
5.1.5
19.0
60.20
376.00
0.00
0.00
-0.00
767.0

2i>. 000
295.657
39.500
2.503
36.000

1.006
23.1,10
5.137

.257
5.51.8
1.216
161.09
0.00
181.09
99.35
.012
0.00
1,1020.00
250.00
7.07
21.0
56.32
339.00
2.12
55. 1*
359.00
866.0

39.000
i.1 0.61.6
42.800
2.906
39.000

1.516
27.930
4.782

.379
6.982
1.195
1.00
2 1,1.. 32
21,1,. 32
93.21
.014
IS
1.5.66
1.0970.00
256.00
6.89
19.1 	
58.09
338.01
1.89 	 ._
56.81
358.10
868.1 	

19.506
306.306
1.5.900
2.986
1,2.900

.7*1
20.373 	 _ . .
5.115

.191

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(D
ENGINE' GTCP85-98CK S/N= 36179
RAT SHP= ZOO. RA EGT,F<
FUEL H/C' 1.9280 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., DEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR OSCHG. PRES.tPSIA
COMPRESSOR DSCHG. TEMP, DEC F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOH. LB/SEC
COMPRESSOR MAP FLOH, LB/SEC
FA RATIO BASED ON MAP FLOW
CORRECTED FUEL FLON , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING M/P»*N/V/E(T/540I
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNED HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, tB./HR.
RATIO LB HC/ia CO
1150.
.06822
11
0.0
0.0
0.0
469.0
416ZO.O
61.5
365.0
13.54
0.000
5.90
.0065
140.0
.0064
.094
.386
98.195

1.31
3.07
4Z9.Z

254.6
38.03Z
5.325
CARBON,
1Z1.5
10.374
1.452
.2728
COMB P/N' 691898-3 T£ST DATE 6-17-75 FUEL=AV. KtRO. P BARO' 20.47
RAT SPO»
L H V»
12
39.9
79.7
72.0
565.0
41460.0
61.6
366.0
13.60
0.000
5.57
.0087
170.0
.0002
.120
.357
98.764

1.60
3.09
537.4

272.3
31.920
5.554
HEIGHTS AS
02.5
5.528
.962
.1732
41600. OEM PT, '
18470. S
13
99.1
190.1
181.1
787.0
41130.0
60. Z
376.0
13.72
0.000
5.67
.0116
237.0
.0121
.177
.372
99.354
•SUMMARY OF
2.50
3.11
738.1

295.7
23.410
5.540
CH4
24. 0
1.006
.257
.0464
LN T, =
1
0.
0.
0.
060.
..1020.
56.
339.
13.71
2.145
6.04
.0147
250.0
.0140
.206
.373
99.210
REDUCED
Z.91
3.11
776.5

410.6
27.930
6.90Z

39.0
1.516
.379
.0543
8. REi HUH' 49.00 SPEC HUM* .001000
300.0 FLO.L/H* 14.160 SL TIH.S* 6.5000
15
ZZ.
45.
41.
060.
40970.
50.
330.
13.72
1.907
6.74
.0140 	 .__ 	 _
256.0
.0143
.210 ._
.364
99.456

2.99
3.12. _ 	 _ 	 	 ..
005.0

306.3
20.373
5.256

19.5
.741
.191
.0364
NITRIC OXIDE (NO) - HEIGHTS AS N02
PPM BY VOLUME, HET
L3. PER 1000 ..6. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE (NO2I
PPM BY VOLUME, NET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
14.0
3.435
.401

3.0
.736
.103
17.0
3.Z74
.570

6.5
1.252
.218
TOTAL OXIDES OF NITROGEN (NC+NOZI AS N02
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLON
SMOKE NUMBER
CORRECTED HEIGHT FLON
SMOKE NUMBER
CORRECTED HEIGHT FLOM
SMOKE NUMBER
CORRECTED HEIGHT FLON
SMOKE NUMBER
SMOKE NUMBER AT HA'0.023
17.0
4.17Z
.504

.00698
26.20
.02097
41.70
.03495
48.80
.04092
56.00
43.60
23.5
4.5Z5
.787

.00699
27.40
.02097
41.70
.03492
52.48
.04009
50.30
45.40
36.0
4.612
1.110

3.5
.455
.100

39.5
5.137
1.210

.00699
26. 20
.02097
42.90
.03492
51.20
.04000
57.10
44.00
39.0
4.357
1.009

3.0
.425
.106

42.0
4.702
1.195

.00699
38.10
.02095
57.10
.03490
66.70
.04003
75.00
59.00
42. 9 	 	 	 .........'....
4.687
1.209

3.0
.320
.005 .. . .. . 	 	 . .. 	 : 	 	 . --

45.9
5.015 .... _ 	 .._. ..
1.294

.00697 	 ._ . .. 	 ... ..
28.60
.02091
46.40 . ._. _. 	 _. . .. - - ...... - - - 	 -
.03404
S7.10
.04076 _.. 	 .._ __. - 	 -
61.90
49.00
                                                                                                                                                             h
                  NOTES 1. AU. EMISSIONS CONCENTRATIONS ARE HET VALUES.                                   	   		
                        Z.EQUIVALENCE RATIO CALCU.ATED FROM COZ.CO.ANO HC DATA AND FUEL COMPOSITION.
                        3.MASS EMISSIONS OF NC, NOZ. AND NO+N02 CALCULATED AS N02 FROM CONCENTRATIONS HITH MOLECULAR HEIGHT OF  N02  (46.011.
                        4.COMBUSTION EFFICIENCY C,ALCU;.AT£0 FROM CO.AND UHC AS VAPORIZED ORIGINAL FUEL ON LB/ LB  FUEL BASIS.           .  . . .

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                                                                  »•"  AIRESEAKCH EMISSION  TEST  SUMMARY
                                                                   COM3 P/N= 691898-3 TEST DATE   6-17-75
  ENGINE' GTCP85-9«CK       S/N= 36179
OATA POINT NUMBER                    11        12         13         !«.        15
EMISSION RATE LB/HR
    CARBON MONOXIDE               5.325     5.551,     5.5<>8      6.982     5.256
    UNBURNED HYDROCARBONS         1.1.52      .962      .257       .379      .191
    OXIDES OF NITROGEN             .5S<,      ,7fT     1.21S      1.195     1.291,
    NITRIC OXIDE                   .1,51      .570     1.110      1.089     1.209
POWER LEVEL HP        .            0.00     72.82    191.09     2<,58     <>.6<>9
    NOTE**0. APPEARING IN  3R4KE SPECIFIC EMISSION INDEX  COLUMN DENOTES AN IDLE CONDITION
                                                                                                                FUEL=»V. KERO.
                                                                                                                                   P  B4RO- 28.1.7


\->
*J
                                                                                                                                                                       )

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D
•>

•>

•>

i
                        ENGINE  MFR.I AIRESEARCH
                       MODEL  NO.I   GTCPI5-90CK

                       FUEL!  ASTM  01655-73
 TEST FACILITY! PHX LACCZ       INSTR. OESCRIP.I  FEOcRtL  REG  V30 N136
 S/NI  36179          ENGINE TYPE (CLASS!I APU               CALC. I.O.I
MAX SHP       zoo. » BLEED AIR EXTRACTION TO    nso. OEG. F EGT
    ATOMIC H/C KATIOI   1.9ZO    LHVI     18470. BTU/LB.     ADDITIVES! NONE
CALC. DATEt
   1
             6-17-75
                                  EXHAUST EMISSIONS PER EPA RATED NORK OUTPUT •• CODE OF FEDERAL REGULATIONS TITLE  40  PART 07
                                 .............................. £MISSIONS COMPUTED FROM TEST CONDITION NO.  5   ..»....•..«»..
                                          HYDROCARBONS (HC AS CH4I             .073  LB. POLLUTANT PER 1000 HP.-HR.
                                          CARBON  MONOXIDE ICO»               20.904  LB. POLLUTANT PER 1000 HP.-HR.
                                          OXIDES  OF NITROGEN (NOX AS NOZ)     5.009  uB..POLLUTANT PER 1000 HP.-HR.
                                                                             17 JULY 1973
                       [[[  EN6IN£
                       COMBUSTOR TYPE!  TANGENTIAL CAN          P/NI  690160-3  SURFACE/VOLUME I  .725 SO IN/CJ IN
                       ENGINE  TOTAL SERVICE!      0.0   Ht.   TINE SINCE ENGINE OVERHAUL!      0.0 MR.
                       ENGINE  ASSEMBLY  AND MAINTENANCE INFORMATION!
                       AIRCRAFT  INSTALLATION •»•  MFR.I
                                                                                   MODEL NO.I
                                                                FUEL  INJ.  TYPE I
                                                                                                                           USER!
                                                                                    DUAL ORIFICE
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                      ................................................OPERATIONAL TEST DATA SUMMARY •••••»•••••••»•»•»•»•••••»••••••••»•••»»••••••••
                   )   GASEOUS  EMISSION TEST  NO. I      2    DATE!  6-17-75      TIME!    13.45      BARO. PRESS.I  Z8.470  IN.  HCA.
                      AMBIENT  AIR  TEMP.I  19.0   OEG.  F        RELATIVE HUMIDITY! 100.00 PERCENT       SPECIFIC HUMIDITY!   .002000  LB.  H20/LB.  DRY AIR
                      AMBIENT  AIR  QUALITY   HYDROCARBONS (HCI1 0.0   PPMC    CARBON MONOXIDE (COI1 0.0   PPMV    OXIDES OF  NITROGEN  (NOXII  0.0   PPMV
                   )   SAMPLE LINE  ••»  TEKP.l   300.00  OEG. F.      FLOHRATEI   14.16 LITERS/HIM.     TRANSPORT TIME!     6.50 SEC.     LEN6THI    50.00 FT.
TEST CONDITION
POWER SETTING, CORRECTED HP.
Ml SPEED. RPM
FUEL FLON IHEAS.I LB./HR.
ENGINE CORE INLET AIRFLCMICALC.) LB./SEC.
COMPRESSOR INLET TEMP., OEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP., DEG. F
COMPRESSOR BLEED AIRFLOW (MEAS.) LB./SEC.
BLEED AIR PRESSURE. PSIA
BLEED AIR TEMPERATURE, DEG. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION, MET .ANALYSIS
HYDROCARBON (HC AS CH4I , PPMC
CARBON MONOXIDE (CO), PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPHV
CARBON DIOXIDE (COZ) , PERCENT BY VOL.
NITRIC OXIDE (NO), PPHV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS N02I
ENGINE NORK OUTPUT, NEAS. SHP
ENGINE NORK OUTPUT, ISENTROPIC AIR HP
ENGINE NORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS)
16 17 10
0.00
41600.00
142.00
6.08
18.0
62.36
362.00
0.00
0.00
-0.00
467.0

121.500
252.108
16.500
1.316
13.000

10.282
37.326
4.013

1.460
5.300
.570
0.00
0.00
o.oo
98.22
.006
79.46
'•1448.00
175.00
5.88
21.0
61.37
368.00
0.00
0.00
-0.10
571.0

76.500
274.834
23.300
1.694
17.500

5.075
31.901
4.443

.888
5.583
.777
72.79
0.00
7Z.79
90.00
.000
197.65
".1120.00
232.00
5.31
Zl.O
60.15
376.00
0.00
0.00
-0.00
775.0

13.500
207.086
40. ZOO
2.529
37.700

.607
16.294
5.196

.141
3.780
1.205
101.05
0.00
181.05
99.56
.012
19
0.00
41000.00
250.00
7.01
19.0
56.07
335.10
2.17
54.75
355.10
801.0

33.000
410.646
43.000
2.974
40.000

1.254
27.309
4.697

.114
6.8Z7
1.174
0.00
240.74
248.74
99.25
.014
20
45.54
40950.00
258.01
7.00
21.1
57.69 	
339.01
1.89
56.56 "" " ~" - - -
358.00
861.1
"»**_•• ™— 	 .... 	 __—_,,„ _ _ 	 __ _
22.500
306.994
44.900
2.910
. 41.100

.875
21.120
5.117

.226

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ENGINE' GTCP85-98CK S/N« 36179 COHB P/N« 696166-3 TEST DATE 6-17-75 FUEL'AV. KERO. P BARO« Z8.47 4
RAT SHP» 200. RA EGT.F* 1150. RAT SPO< 41600.
1 FUEL H/C* 1.9280 STOI F/A* .06822 L H V» 18476.
DATA POINT NUMBER 16 17 16
> PERCENT HAX. CORRECTED POHER 6. 39.7 96.
CORRECTED SHAFT HP 6. 79.5 197.
MEASURED SHAFT HP 8. 72.8 181.
> EXHAUST GAS TEMP., DEG.F 467. 571.6 775.
SHAFT SPEED, NI, RPM 41600. 41440.0 41120.
COMPRESSOR OSCHG. PRES. .PSIA 62.4 61.4 60.
> COMPRESSOR OSCHG. TEMP, DEC F 362.0 368.6 376.
EXHAU3T GAS PRESS., PSIA 13.53 13.59 13.71
CORRECTED BLEED FLOH, LB/SEC 6.006 0.000 6.660
•> COMPRESSOR NAP FLOH, LB/SEC 6.87 5.57 5.16
FA RATIO BASED ON NAP FLOH .6065 .0067 .6125
CORRECTED FUEL FLOH , LB/HR 1.2.0 175.0 232.6
) FA RATIO CALC. FROM EMISSION .8065 .8083 .6121
EQUIVALENCE RATIO .095 .121 .17*
LOADING M/P**N/V/E(T/54tl .364 .359 .348
OEH PT.F' 19. RE*. HUH' 100.00 SPEC HUM" .062000
S <-H T,F« 360.0 FLO,L/H» 14.160 SL TIH.S* 6.5000
19 26
0. 22.8
6. 45.5 . 	 	 -
0. *>!.?
661. 661.6
41000. 40950.0 	 -
56.1 57.7
335.0 339.8
13.72 13.72 . . .
2.192 1.906
6.6Z 6.67
.6149 .8158 	 •_.. 	 . . .
258.0 256. 6
.6143 .8148
.218 .266 	 	
.372 .362
) COMB EFFIC FROM EMISSIONS 98.226 98.604 99.563 99.248 99.429 ._...,
CARBON DIOXIDE
) PERCENT BY VOLUME, HET 1.32 1.69 2.53
L3. C02 PcR LB. OF FUEL 3.07 3.89 3.13
HEIGHT FLOM, LB./HR. 435.5 546.7 725.4
) CARBON MONOXIDE
PPM BY VOLUME. HET 252.1 274.8 207.1
LB. PER 1088 LB. OF FU£L 37.326 31.901 16.294
HEIGHT FLOH, LB./HR. 5.360 5.583 3.788
UNBURNEO HYDROCARBONS— PPM AS CARBCN, HEIGHTS AS CHn
PPM BY VOLUME, NET 121.5 76.5 13.5
LB. PER 1086 LB. OF FUEL 10.282 5.075 .667
HEIGHT FLOM, LB./HR. 1.460 .866 .141
RATIO L6 HC/LB CO .2755 .1591 .8373
NITRIC OXIDE (MO) - HEIGHTS AS N02
' PPM BY VOLUME, HET 13.6 17.5 37.7
LB. PER 1060 LB. OF FUEL 3.162 3.337 4.673
, HEIGHT FLOH, LB./HR. .4*9 .564 1.136
NITROGEN DIOXIDE (NOZ)
PPM BY VOLUME, HET 3.5 5.6 2.5
) LB. PER 1608 LB. OF FUEL .851 1.186 .323
HEIGHT FLOH, LB./HR. .121 .194 .075
TOTAL OXIDES OF NITROGEN  AS NOZ
l PPM BY VOLUME, HET 16.5 23.3 40. Z
L3. PER 1600 LB. OF FUEL 4.013 4.443 5.196
HEIGHT FLOH. LB./HR. .570 .777 1.205
! SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLCM .00696 .00695 .00697
SNOKE NUMBER 22.60 26.20 15.50
, CORRECTED HEIGHT FLCH .62089 .02066 .02689
SHOKE NUMBER 36.10 38.10 28.68
CORRECTED HEIGHT FLCM .03482 .03474 .03479
) SNOKE NUMBER 46.48 48.88 . 39.30
CORRECTED HEIGHT FLCH .04872 .04862 .04678
SMOKE NUMBER 51.20 54.88 48.68
) SMOKE NUMBER AT HA'6.8Z3 40.00 42.40 33.60
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE H£T VALUES.
Z. EQUIVALENCE RATIO CALCULATED FROM C02,CO,AND HC DATA
)' 3. MASS EMISSIONS OF NO, NOZ, AND NO»N02 CALCULATED AS
J ,. rnKHiicTTKU rrCTr.TFUTV CALCULATFD FROM CO. AND UHC AS
2.97 2.92
3.11 3.12 ._ __ 	 . .
776.9 664.6

418.6 389.8 	 ........
27.389 21.020
6.827 5.423

33.8 22.5
1.254 .875
.314 .226 . -
.6459 .0416

40.0 41.1
4.369 4.593
1.692 1.185

3.8 3.6
.328 .425
.062 .110

43.8 44.9
4.697 5.017 .._ .. .... . 	 __ ... 	
1.174 1.294

.00696 .00695 . _ 	 _ 	 	
31.00 25.06
.02067 .02084
54.66 46.58 - . -
.03477 .03472
60.70 52.46
.04665 .04859 	 	 	
72.60 56.36
55.48 44.60
	 . 	 	 	 	 • — .. —
AND FUEL COMPOSITION.
NOZ FROM CONCENTRATIONS HITH MOLECULAR HEIGHT OF NOZ (46.011.
VAPORI2EO ORIGINAL FUEL ON LB/ LB FUEL BASIS. . .








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  ENGINE: GTCPB5-98CK
DATA POINT NUMBER
EMISSION RATE LB/HR
    CARBON MONOXIDE
    U40URNED HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OX IDE
POMER LEVEL HP
TOTAL CORRECTED HORSEPOWER
                                         S/N =
36179
    16

 5.300
 1.1.68
  .570

 oloo
 0.00
                                                       ••••   AIRESEARCH  EMISSION TEST SUMMARY
                                                        COMB  P/N= 6S8160-3 TEST DATE  6-17-75
                                                            17
                                                                       16
                                                                                 19
                                                                                           Zt
                                                                                                     FUEL=AV. KERO.
                                                                                                                       P BARO« Z0.*7
5.503
.000
.777
.500
7Z.79
79.1.6
76.690
12.203
10.601
8.022
3.780
• 11.1
1.205
1.130
101.05
197.65
20.080
.778
6.658
6.21.1.
6.827
.111.
1.17*
1.99Z
2.8.71.
251.13
27.1.1.7
1.261
<*.7Z1
fc.39Z
5.1.23
.226
1.291*
1.185
258.1.1.
261.. 80
Z0.90<>
.073
5.009
"..585
              BRAVE SPECIFIC EMISSION INDEX '.8/1000HP-HR
                  CARBON MONOXIDE              0.000
                  UNBURNEO HYDROCARBONS        0.000
                  OXIDES OF NITROGEN           0.000
                  NITRIC OXIDE                 0.000
                  NOTE**0. APPEARING IN 3RAKE SPECIFIC EMISSION  INDEX  COtU.IN DENOTES AN ICLE CONDITION
0>

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                        ENGINE NFR.I AIRESEARCH
                       MODEL NO.I  GTCP85-98CK

                       FUEL! ASIN 01655-73
 TEST FACILITY! PHX LACC2       INSTR. OtSCRIP.I  FEDERAL REG  V38  N136    CALC.
 S/NI  36179          ENGINE TYPE  (CLASS!I  APU              CALC.  I.D.I    2
MAX SH°       ZOO. » BLEtD AIR EXTRACTION TO    115«. DEC. F E6T
    ATONIC H/C RATIO!   1.928    LHV1     18470. BTU/LB.     ADDITIVES! NONE
                                                                                                                                      DATEI  6-17-75
                                  EXHAUST EMISSIONS  PE4 EPA RATES  NORK  OUTPUT ••  CODE  OF FEDERAL  REGULATIONS  TITLE 40 PART 67
                                 .............................. EMISSIONS COHPUTED  FROM TEST  CONDITION  NO.  5   •••»•••»»•••»»
                                          HYDROCARBONS IHC AS CM*)              .742 -B. POLLUTANT  PER  1010 rtP.-HR.
                                          CARBON MONOXIDE (CO)               31.117 .8. POLLUTANT  PER  1000 HP.-HR.
                                          OXIDES OF  NITROGEN (NOX  AS N02>     5.06". ^B. POLLUTANT  PER  1000 HP.-HR.      _  _
                                                                                                                                  17 JULY 1973
                       [[[  ENGINE  DESCRIPTION  »•••»•••••»»»»••
                       COMBUSTOR TYPE! TANGENTIAL CAN          P/N1  698168-3  SURFACE/VOLUMEI   .72$  SB IN/CU IN
                       ENGINE TOTAL SERVICE!     0.0  HR.   TIME SINCE ENGINE OVERHAUL!       0.0 HR.
                       ENGINc ASSEMBLY AND MAINTENANCE INFORMATION!
                                                                FUEL  INJ.  TYPE!
                                                                                    DUAL  ORIFICE
                       AIRCRAFT INSTALLATION •»• HFR.I
                                                                                    MODEL NO.I
                                                                                                                           USER!
 0)
03
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                       ••...».....»»•..•••*••.»..•.»»••..*•••••••••.••OPERATIONAL  TEST  OATA  SUMMARY  »»•»•»••»»»»»••••••»•»••••••••••••••»•••••••••••
                       GASEOUS EMISSION TEST NO. I    Z     DATE!   6-17-75      TIME!   1».<.5        BARO.  PRESS.!  28.
317.124 _ _ _. 	 .. 	
46.300
2.974 )
42.900 	 . 	 _._ 	 	

.744 J
21.164 	 	 	 	
5.076 "
.. >
.192 	 	 	 	
5.460

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ENGINE' GTCP85-98CK S/N= 36179
RAT SHP» 200. RA EGT,F= 1150.
FUEL H/C« 1.9280 STOI F/A= .06822
DATA POINT NUMBER . 21
PERCENT MAX. CORRECTED POWER 0.0
CORRECTED SHAFT HP 0.0
MEASURED SHAFT HP 0.0
EXHAUST GAS TEMP., OEG.F 464.0
SHAFT SPEED, Nl, RPN 41608.0
COMPRESSOR OSCHG. PRES. .PSIA 61.9
COMPRESSOR DSCHG. TEMP, DEC F 364.0
EXHAUST GAS PRESS., PSIA 13.54
CORRECTED BLEED FLOW, LB/SEC 0.100
COHPRESSOR MAP FLOW, LB/SEC 6.02
FA RATIO BASED ON NAP FLOW .0065
CORRECTED FUEL FLOW . LB/HR 140.0
FA RATIO CALC. FROH EMISSION .0064
EQUIVALENCE RATIO .093
LOADING W/P»»N/V/E(T/54fll .315
COMB EFFIC FRON EMISSIONS 98.257
COMB P/N= 698168-3 T£ST DATE 6-17-75 FUEL»A». KERO. P BARO« 20.47
RAT SPO* 41600. DEW PT, « 19. REL HUM= 101.00 SPEC HUM» .002008
L M V- 18470. S LN T, « 308.8 FLO.L/M- 14.160 SL TIM.S- 6.5080
22 23 2 25 " 	
39.8 99.0 0. 22.8
79.5 198.1 8. 45.6
72.8 ISO. 8. 41.7 	 " 	 "
567.0 780. 879. 860.8
41440.0 41880. 40980. 48940.0
61.4 60.
366.8 372.
13.60 13.73
0.088 8.000
5.57 5.25
.8087 .0124
171.. 0 235.0
.0081 .8119
.119 .174
.360 .343
98.780 99.561
CARBON DIOXIDE
PERCENT BY VOLUHE. WET 1.29 1.66
IS. C02 PER LB. OF FUEL 3.07 3.09
WEIGHT FLOW, LB./HR. 429.6 537.5
CARBON MONOXIDE
PPM BY VOLUHE, WET 244.7 273.8
LB. PER 1000 LB. OF FUEL 36.930 32.153
WEIGHT FLON, LB./HR. 5.170 5.629
UNBURNEO HYDROCARBONS- PPH AS CARBON. WEIGHTS AS
PPM BY VOLUHE, WET 115.5 77.4
LB. PER 1000 LB. OF FUEL 9.965 5.227
HEIGHT FLOW, LB./HR. 1.395 .910
RATIO LB HC/LB CO .2698 .1616
NITRIC OXIDE (NO) - HEIGHTS AS N02
PPH BY VOLUHE. WET 13.5 16.5
LB. PER 1000 LB. OF FUEL 3.347 3.202
WEIGHT FLOW, LB./HR. .469 .657
NITROGEN DIOXIDE (N02)
PPH BY VOLUME. NET 3.5 6.7
LB. PER 1000 LB. OF FUEL .868 1.388
HEIGHT FLOW, LB./HR. .121 .226
TOTAL OXIDES OF NITROGEN (MO»N02I AS N02
PPM BY VOLUHE, NET 17.0 23.2
L3. PER 1000 LB. OF FUEL 4.215 4.503
WEIGHT FLOW, LB./HR. .590 .784
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOW .00695 .00694
SMOKE NUMBER 22.60 28.60
CORRECTED WEIGHT FLOW .02185 .02082
SMOKE NUHBER 36.90 48.58
CORRECTED WEIGHT FLOW .03476 .03468
SNOKE HUHBER 46.40 47.60
CORRECTED WEIGHT FLCW .04064 .04(53
SMOKE NUMBER 47.60 52.40
SMOKE NUHBER AT WA'0.023 38.80 42.70
2.47
3.13
734.7
20 6-. 1
16.590
3.899
CH4
12.1
.552
.130
.0333
37.2
4.918
1.156
2.8
.378
.037
48. a
5.288
1.243
.00694
19.08
.02081
33.38
.03467
40.58
.04852
53.68
37.28
56.
332.
13.71
2.194
6.77
.0155
256.0
.8144
.211
.370
99.254
REDUCED
2.98
3,11
795.6
410.6
27.259
6.978
31.5
1.195
.386
.8436
40.5
4.416
1.131
3.8
.327
..084
43.5
4.763
1.214
. 08693
53.60
.02079
59.50
.03464
67.90
.04847
71.40
63.40
57.6
338.0
13.72
1.982
6.77
.8147
256.0
.8143
.289
.372 	 " " " ' : -----
99.437
2.97
3.12 _ 	 	 	 _
«84.6 . ......
21.164
5.468
19.9 ."~ 	
.744
.192. ... . /_ .
.8351
42.9
4.783 - ""
1.213
3.4 	 " ' 	
.373
.096
46.3
5.076
1.310
.00694
29.60 " " -—-"-- 	 ..-...-.
.02080
41.78
.83464
52.48
.84047
61.98
47.88
                                                                                                                                                                   ' )
                        NOTES  1.  ALL  EMISSIONS CONCENTRATIONS ARE WET VALUES.                                                       _

                              2.EQUIVALENCE  RATIO  CALCULATED FROH C02.CO,AND HC OAT* AND FUEL  COMPOSITION.                       "

                              3.MASS  EMISSIONS OF  NO,  N02.  AND NO*N02 CALCULATED AS N02  FRON CONCENTRATIONS WITH  MOLECULAR WEIGHT OF N02  (46.011.

                              4.COMBUST!ON EFFICIENCY  CALCULATED  FROM CO,AND UNC AS VAPORIZED  ORIGINAL FUEL ON LB/ LB FUEL BASIS.

-------
                      ENGINE-  GTCP85-98CK
                    DATA POINT NUHBER
                    ENISSION RATE LB/HR
                        CARBON MONOXIDE
                        UNBURNEO HYDROCARBONS
                        OXIDES OF NITROGEN
                        NITRIC OXIDE
                    POKER LEVEL HP
                    TOTAL CORRECTED HORSEPOWER
                                               S/M*
36179
    Zl
  .395
  .590
  .469
  .00
  .80
                                                             ••••  ilRESEARCH EMISSION TEST SUMMARY
                                                              COMB P/N« 698168-3 TEST DATE  6-17-75
                                                                                                          FUEL«*V.  KERO.
                                                                                                                            P BA«0»  28.47
                    BRAKE SPECIFIC EMISSION INDEX LB/ OflOHP-HR
                        CARBON MONOXIDE
                        UNBURNEO HYDROCARBONS
                        OXIDES OF NITROGEN
                        NITRIC OXIDE
  .000
   000
   000
   • 00
     ZZ

  5.629
   .911
   .784
   .557
 7Z.79
 79.55
I
 77.339
 12.496
 10.76".
  7.655
     23

  3.899
   .130
  1.Z43
  1.156
188.87
198.07

 21.555
   .717
  6.870
  6.389
     Z4

  6.978
   .306
  1.214
  1.131
247.7*
249.90

 28.163
  1.235
  4.900
  4.562
     ts

  5.460
   .19Z
  1.318
  1.Z13
258.58
Zbc.. 76

 21.117
   .742
  5.064
  4.6*2
                        NOTE>*0.  APPEARING IN BRAKE SPECIFIC ENISSION INDEX COLUMN DENOTES AN IDLE CONDITION
UQ
CD
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                        ENGINE  MFR. 1  AIRESEARCH
                      HOOEL  NO. 1   GTCPSS-98CK

                      FUE-t  ASTH  01655-73
                               TEST FACILITY! PHX LACC2       INSTR.  DESCRIP.I   FEDERAL  REG V30 N136    CALC. DATE I
                               S/NI  36179          ENGINE TYPE  (CLASSI1  APU               CALC. I.D.I      3__
                              MAX SHP       ZOO. » BLEED AIR EXTRACTION TO    1150.  DEG.  F  EGT
                                  ATOMIC H/C RATIO!   1.928    LHVI     18470.  6TU/L3.      ADDITIVES! NONE
                                                                                                                                            6-10-73
                                  EXHAUST EMISSIONS PE3 EPA RATES HOSK OUTPUT •• CODE OF FcOERAL REGULATIONS TITLE 40 PART  87
                                 .............................. EMISSIONS CONFUTED FROM TEST CONDITION NO.  5   ••••••••••»••«
                                          HYDROCARBONS IHC AS CH4>              .805  LB. POLLUTANT PER 1000 HP.-HR.
                                          CARBON MONOXIDE (COI               21.645  uB. POLLUTANT PER 1000 HP.-HR.
                                          OXIDES OF NITROGEN (NOX AS N02)     4.960  LB. POLLUTANT PER 1000 HP.-HR.
                                                                                                                                 17 JULY  1973
[[[  £NGINE DESCRIPTION  ••••••••••••»•••
CONBUSTOR TYPEI TANGENTIAL CAN          P/N!  698166-3  SURFACE/VOLUME!   .725  SO  IN/CU  IN
ENGINE TOTAL SERVICE!     0.0  HR.   TIKE SINCE ENGINE OVERHAUL!       0.0 HR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                       AIRCRAFT INSTALLATION •»» MFR. 1
                                                                                   HOOEL NO.I
                                                                                                                    FUEL  INJ. TVPEI
                                                                                                                          USERt
                                                                                                                                        DUAL  ORIFICE
(D
                       ..........................,...................»<0p£RATIONAL T£ST BAI« SUMMARY ••»»••••••«••»••••••••••»••••••••••••••••»••••••
                       GASEOUS EMISSION TEST NO.I     2    3ATE!  6-16-73      TINEI    8.45       BARO. PRESS.I  26.440 IN. HGA.
                       AMBIENT AIR TEMP.! 19.0  DEG.  F        RELATIVE HUMIDITY I 100.00 PERCENT       SPECIFIC HUMIDITY!   .002000 LB. HZO/LB.  DRY  AIR
                       AMBIENT AIR QUALITY    HYDROCARBONS (HCM 0.0   PPHC    CARBON MONOXIDE (COM 0.0   PPHV    OXIDES  OF NITROGEN INOXIt  0.0    PPHV
                       SAMPLE LINE •" TEMP.l  300.00 DEC. F.     FLOM*AT£!   14.16 LITERS/MIN.     TRANSPORT TIME!     6.50 SEC.     LENGTH!    50.00 FT.

TEST CONDITION
PONER SETTING, CORRECTED HP.
Nl SPEED. RPM
FUEL FLCN (MEAS.I LB./HR.
ENGINE CORE INLET AIRFLCMICALC.) ..B.SSEC.
COMPRESSOR INLET TEMP., DEG. F
COMPRESSOR DISCHARGE AIR PRESSURE. PSIA
COMPRESSOR DISCHARGE AIR TEMP., DEC. F
COMPRESSOR BLEED AIRFLOW (MEAS.) '.3. /SEC.
9LEEO AIR PRESSURE, PSIA
BLEED AIR TEMPERATURE, DEG. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION, NET ANALYSIS
HYDROCARBON (HC AS CH4I . PPNC
CARBON MONOXIDE (COI. PPMV
TOTAL OXIDES OF NITROGEN INOXI , PPHV
CARBON DIOXIDE ICOZ) , PERCENT BY VOL.
NITRIC OXIDE (NOI. PPHV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4I
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02I
EMI SSI OK RATE, LS. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02I
ENGINE HORK OUTPUT, MEAS. SHP
ENGINE HORK OUTPUT. ISENTROPIC AIR HP
ENGINE HOIK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A lEMISSIONSI

26
0.00
41660.00
142.00
fc.23
18.0
62.65
362.00
0.00
0.00
-0.00
462.0
126.000
237.311
16.000
1.206
9.500
10.935
36.032
3.990
1.553
5.116
.567
0.00
0.00
0.00
90.19
.006
£0 EMISSIO
27
79.01
414SO.OO
175.00
5.91
19.0
61.87
367.00
0.00
0.00
-0.00
565.0
Bl.OOO
277.404
23.200
1.666
15.900
5.399
32.350
4.444
.945
5.661
.778
72.66
0.00
72.08
90.77
.000
--
28
198.56
41180.00
236.00
5.53
19.0
60.68
375.00
0.00
0.00
-0.00
774.0
12.300
208.502
39.000
2.480
35.500
.562
16.675
5.124
.134
3.969
1.219
181.31
0.00
161.31
99.56
.012

29
0.00
41060.00
256.00
7.14
1%.0
56.71
334.00
2.10
55.56
355.00
060.0
33.000
416.952
42.300
2.976
39.010
1.254
27.722
6.620
.321
7.097
1.103
0.00
249. 09
249.09
99.26
.016

30
45.79
61040.01
262.00
6.99
19.0
58.53
336.00
1.90
57.20 '
357.00
063.0 . ,
21.000 ' '
322.590 1
45.000 '
2.976
40.500
.801
21.525 	 	 1
4.932
.210

-------
              o
 (o
03
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 10
 U1
                      ENGINE* GTCP85-98CK      S/N« 16179
                     RAT SHP»   ZOO.    R» EGT,F« 1150.
                    FUEL «/C« 1.9ZOO    STOI F/A«
                    OAT* .POINT NUMBER                   26
                    PERCENT H*X. CORRECTED POKER       0.
                    CORRECTED SHAFT HP                 •.
                    HE* SURE 0 SHAFT HP                  0.
                    EXHAUST CAS TEMP., DEC.F         462.
                    SHAFT SPEED i Nl. RPM           41660.
                    COMPRESSOR OSCHS. PRES. ,PSIA      62.
                    COMPRESSOR OSCHS. TEHP.OEG F     362.0
                    EXHAUST CAS PRESS.. PSIA         13. 52
                    CORRECTED BLEED FLON, LB/SEC     0.000
                    COMPRESSOR MAP FLOW, LB/SEC        6.07
                    FA RATIO BASED ON HAP FLON       .0065
                    CORRECTED FUEL FLOH t LB/HR      142.0
                    FA RATIO CALC. FROM EHISSIOH     .0063
                    EQUIVALENCE RATIO                 .093
                    LOA9ING  H/P»»N/V/E«T/5*0»        .379
                    COHB EFFIC FROM EMISSIONS       90.193
                                                             »•*•  AIRESEARCH EMISSION TEST SUMMARY
                                                              COHB PfM* 698160-3 TEST DATE  6-18-73
RAT SPO» 41600.
  t H W« 10470.
OEH PT.
S LN T
     27
   39.9
   79.8
   72.9
  565.8
41<>90.0
   61.9
  167.0
  13.51
  0.000
   5.57
  .00(7
  175.0
  .0802
   .121'
   .35%
 91.765
   CARBON DIOXIDE
)      PERCENT BY  VOLUME,  HET         1.29      1.69
       LB. C02 PER LB.  OF  FUEL        3.87      3.89
       HEIGHT FLOH, LB./HR.          435.6     540.5
)  CARBON MONOXIDE
       PPM BY VOLUME, HET            237.3     277.4
       L8. PER 1080 LB. OF FUEL     36.832    33.351
       HEIGHT FLOH. LB./HR.          5.116     5.661
       28
     99.3
    198.6
    181.3
    774.1
  41180.0
     60.9
    375.0
    13.72
    0.000
     5.25
    .0126
    230.0
    .0120
     .175
     .330
   99.550
•SUMMARY OF

     2.49
     3.13
    744.1

    208.5
   16.67S
    3.969
                                                                           19.
                                                                          300.0
                                     FUEL«AV.  KERO.     P  BARO« 20.44
                                REL  HUH>  100.00    SPEC HUM-  .102000
                                FLO.L/N-   14.168   SL  TIH.S"   6.5000
                                                                     Z
                                                                     0.
                                                                     0.
                                                                     1.
                                                                   061.
                                                                 410(0.
                                                                    56.
                                                                   334.
                                                                   13.70
                                                                   2.204
                                                                    6.07
                                                                   .0152
                                                                   256.1
                                                                   .0143
                                                                    .211
                                                                    .369
                                                                  99.230
                                                                 REDUCED
   UNBURNEO HYDROCARBONS-  PPM  AS  CARBON,  HEIGHTS AS CH4
       PPM BY  VOLUME. MET            126.0      81.1      12.1
       LB. PER 1000 LB.  OF FUEL     10.935     5.399      .562
       HEIGHT  FLOH. LB./HR.          1.553      .945      .134
       RATIO U8 HC/LB CO            .1035     .1669     .03*7
   NITRIC OXIDE (NOI - HEIGHTS AS N02
       PPM BY  VOLUME, HET              9.5      15.9      35.5
       LB. PER 1000 LB.  OF FUEL      2.369     3.046     4.664
       HEIGHT  FLON, LB./HR.           .316      .533     1.110
   NITROGEN DIOXIDE INOZI                             .
       PPM BY  VOLUME. NET              6.5       7.3       3.5
       LB. PER 1010 LB.  OF FUEL      1.621     1.390      .460
       HEIGHT  FLON, LB./HR.           .231  .  _ .245	 .109
   TOTAL OXIDES OF NITROGEN  INO«NOZ>  AS NOZ
       PPM BY  VOLUME, HET             16.1      23.2      39.0
       LB. PER 1888 LB.  Of FUEL      3.998     4.444     5.124
       HEIGHT  FLON, LB./HR.           .567      .771     1.219
       SMOKE MEASUREMENT DATA
       CORRECTED  HEIGHT  FLOH        .04706    .00707    .00707
       SMOKE NUMBER                  26.ZO     27.40     ZZ.60
       CORRECTED  HEIGHT  FLOH        .02117    .1Z121    .1Z1ZO
       SMOKE NUMBER                  31.11     41.71     41.50
       CORRECTED  HEIGHT  FLOH        .03521    .13534    .03532
       SMOKE NUMBER                  »8.8I     47.68     45.28
       CORRECTED  HEIGHT  FLON        .14911    .14947    .14942
       SMOKE NUMBER                  51.Zl     56.11     56.BO
       SMOKE NUMBER AT HA*0.123      41.30     41.40     41.30
   NOTES 1. ALL EMISSIONS  CONCENTRATIONS ARE HET VALUES.
         Z.EQUIVALENCE RATIO CALCULATED FROM C02.CO.ANO HC DATA
         3.MASS EMISSIONS  OF NO.  N02, AND NO*NOZ CALCULATED AS
         4.CONBUSTION EFFICIENCY  CALCULATED FROM CO.AND UHC AS
                       2.97
                       1.11
                      795.%

                      417.0
                     27.722
                      7.097

                       33.0
                      1.Z54
                       .121
                      .0452

                       39.0
                      4.Z59
                      1.090
                30
              22.9
              45.8 _  __.
              41.8
             663.0
           41040.0
              50.5
             330.0
             13.78
             1.918
              6.74
             .8158
             262.0
             .8143
              .219
              .358
            99.423
         EMISSION  DATA*

              2.97
              3.12
             •16.9

             322.6
            21.SIS
             5.639
                                                                                              21.0
                                                                                              .801
                                                                                             _..»•-
                                                                                             .•372

                                                                                              40.5
                                                                                             4.439
                                                                                             1.163
                        3.3
                       .368
                       ..!«_

                       42.3
                      4.620
                      1.103

                     .00705
                      34.50
                     .02115
                      53.60
                     .03524
                      63.10
                     .04931
                      72.60
                      56.10
                                                                                               4.5
                                                                                              .493
                                                                                              45.0
                                                                                             4.932
                                                                                             1.292

                                                                                            .00704
                                                                                             27.40
                                                                                            .02111
                                                                                             44.00
                                                                                            .03517
                                                                                             54.86
                                                                                            .04921
                                                                                             63.16
                                                                                             47.71
                                                                                 AND FUEL COMPOSITION.
                                                                                N02 FROM CONCENTRATIONS KITH MOLECULAR HEIGHT OF N02 I46.B11.
                                                                                VAPORIZED ORIGINAL FUEL ON LB/ LB FUEL BASIS.	•  _

-------
ENGINE' GTCP85-98CK S/N« .36179
DATA POINT NUMBER
EHISSIOK RATE LB/HR
CARBON MONOXIDE
UNBURNEO HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIDE
POWER LEVEL HP
TOTAL CORRECTED HORSEPONER
BRAKE SPECIFIC EMISSION INDEX
CARBON MONOXIDE
UNBURNEO HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIDE


5.
1.
•
*
a.
0.
26

116
553
567
336
88
88
••• AIRESEARCH EMISSION TEST SUMMARY
COMB P/N« 691168-3 TEST DATE 6-18-73


5.
•
•
•
72.
79.
27

661
9*5
778
533
8t
81


3

1
1
181
198


•
*
f)
m
•
*
28

969
13*
219
118
31
56


7

1
1
2*9
25Z
29

.897
.321
.183
.898
.89
.55


5

1
1
26B
266
38

.639
.218
.292
.163
.5*
.•5
L8/1888HP-HR
8,
8.
8.
8.
888
080
888
888
77.
12.
18.
7.
682
965
672
31".
NOTE**0. APPEARING IN 8RAKE SPECIFIC EMISSION
21

6
6
•
.
•
•
INDEX
889
738
725
122
28
1
.*88
.285
*.733
*
.36*
COLUMN DENOTES
21

«.
4>
AN
.6*5
.•85
.968
.«.6*
IDLE C
                                                                                                            FUEL*AV.  KERO.
                                                                                                                               P  BARO' 21. I*
 >
b
                                                                                                     CONDITION
 0)
iQ
 (D

 to
 en
                )


                )

-------
 ENGINE MFR. 1 AIRESEARCH
MODEL NO.t  6TCPOS-98CK

FUEL* ASTM 01655-73
                               TEST FACILITY!  PHX LACC2        INSTft.  OESCRIF.I   FEDERAL  REG  ¥38 N136    CALC.  0*TE«
                               S/NI  36179          ENGINE TYPE (CLASSI 1   APU              CALC. I.O.t ...... i._._.
                              MAX  SHP       201.  » BLEED AIR EXTRACTION  TO   1151.  DEC. F E6T
                                  ATONIC H/C RATIOI   1.926    LHVI     16670.  BTU/LB.     ADDITIVES! NONE
                                                                                                                     6-13-75
                                                                              .
                                                                              T
                                                                              1 '
           EXHAUST EMISSIONS PER EPA RATEO WORK OUTPUT *• CODE OF FEDERAL REGULATIONS TITLE 60 PART »7
          ...•••.•••••..**.•*•»••*•••••• ^MISSIONS COMPUTED FROM TEST CONDITION NO.  5   •••••••••••»••
                   HYDROCARBONS (HC AS CH6I             .371  LB. POLLUTANT PER 1000 HP.-HR.
                   CARSON MONOXIDE ICOI               17.889  LB. POLLUTANT PER 1000 HP.-HR.
                   OXIDES OF NITROGEN INOX AS N02I     5.276  LB. POLLUTANT PER 1000 HP.-HR.     	._
                                                                                                          17 JULT 1973 •••»••••••
,...•.•.....*•.•••••*..••..••.••.••••»*••••••••••.,•  £NGIN£ DESCRIPTION  •••••••••••»<
CON8U3TOR TYPEI TANGENTIAL CAN          P/NI  698168-3  SURFACE/VOLUME I   .725  SO. IN/CU
ENGINE TOTAL SERVICE!      0.0 HR.   TINE SINCE ENGINE OVERHAUL!       0. HR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                                                                                       IN
                                                                                             FUEL INJ, TYPE!
                                                                                                                 DUAL ORIFICE
AIRCRAFT INSTALLATION **• NFR. 1
                                                            MODEL NO** -
                                                                                                   USER!
».»•»»»»•.,••••»»»»•»».•»••••».•••••••••••••••••OPERATIONAL TEST DATA SUMMARY ••••••••••••••••••••••••••••••••••••••••••••••••
GASEOJS EMISSION TEST NO.l     3    BATE!  6-13-75      TIMEI    10.15      8ARO.  PRESS.I  20.760 IN, HGA.
AMBIENT AIR TEMP. I 39.0  OEG. F        RELATIVE HUMIDITY!  41). 00 PERCENT       SPECIFIC HUMIDITY!  .102000 LB. H20/LB. DRY AIR  . .
AMBIENT AIR QUALITY    HYO*OC»R30NS (HCM 0.0   PPMC    CAR8DN MONOXIDE ICOI1 0.0   PPMV    OXIDES OF NITROGEN INOXII 0.0   PW«
SAMPLE LINE •*• TEMP.1  300.00 OEG. F.     FLONRATEI   16.16 LITERS/NIK.     TRANSPORT TIME!    6.50 SEC.     LENGTHI   50.00 FT.
TEST CONDITION
POWER SETTING, CORRECTED HP.
Nl SPEED. RPM
FUEL FLCM IKEA-S.) LB./HR.
ENGINE CORE INLET AIRFLOWICAwC.I LB./SEC.
COMPRESSOR INLET TEMP.. DEC. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP., OEG. F
COMPRESSOR BLEED AIRFLOW IMEAS.I LB./SEC.
BLEED AIR PRESSURE. PSIA
BLEED AIR TEMPERATURE. DEG. F
ENGINE EXHAUST GAS TEMP.. OEG. F
EMISSION CONCENTRATION. NET ANALYSIS
     HYDROCARBON IHC AS CH6I. PPMC
     CARBON MONOXIDE ICOI, PPMV
     TCTAL OXIDES OF NITROGEN (NOXI. PPMV
     CARBON DIOXIDE IC02I, PERCENT BY VOL.'
     NITRIC OXIDE INOI, PPMV
EMISSIOK INDEX, LB. POLLUTANT/1000 LB. FUEL
     HYDROCARBONS IHC AS CH6I
     CARBON MONOXIDE ICOI
     TOTAL OXIDES OF NITROGEN (NOX AS N02I
EMISSIOK RATE, LB. POLLUTANT/HR.
     HYDROCARBONS IHC AS CH6I
     CAKBON MONOXIDE ICOI
     TOTAL OXIDES OF NITROGEN INOX AS N02I
ENGINE WORK OUTPUT, MEAS. SHP
ENGINE WORK OUTPUT, ISENTROPIC AIR i»
ENGINE WORK OUTPUT, TOTAL HP
COM3U3TION EFFICIENCY, PERCENT (EMISSIONS)
F/A {EMISSIONS!
                                                     COMPUTED EMISSIONS
                                                        31        32
                                                      O.BO     79.60
                                                  61630.00  *1678.00
                                                    160.00    175.00
                                                      5.99      5.74
                                                      39.0      39.0
                                                     60.00     60.39
                                                    381.BO    385.BO
                                                      O.BO      0.00
                                                      0.00      0.00
                                                     -0.08     -0.00
                                                     606.0     596.0
                                                  123.000
                                                  252.100
                                                   17.900
                                                    1.318
                                                   10.600
                                                   37.322
                                                    6.353

                                                    1.657
                                                    5.225
                                                     .609
                                                      O.BO
                                                      O.BB
                                                      0.00
                                                     90.21
                                                      .006
 74.600
200.500
 25.600
  1.730
 16.000

  6.013
 31.767
  4.722

   .042
  5.556
   .826
   76.70
    O.BO
   76.70
   90.03
    .000

33
199.06
260.00
5.31
39. B
59.66
395.00
0.00
B.BB
-0.00
038. B
9.000
196.635
63.000
2.610
39.000
.391
14.793
5.376
.094
3.550
1.290
107.69
0.00
187.69
99.62
.013

36
O.OB
61000.00
25B. 00
6.90
38. B
55.68
351. OB
2.12
56.35
372.00
903.0
21.000
366.957
65.500
2.976
37.500
.000
22.999
6.903
.200
5.750
1.266
B.BB
261.67
241.67
99.19
.01*

35
45.61
41040.01
250.BB
6.06
39.B
57.B5
357.00
1.8* 	
5S.B3
377.00
.... 912.0 	 	 	 .
9.6BB
266.666
67.5BB
2.9BB
39.200
.366
17.66S . 	 ... . .
5.2BB :
.09* 	 ..... ._. _ 	 	
6.55B
1.366
62,77 	 	 	
212.BO '
256.77
99.55 _ .
.016
                                                                                                                                           £

-------
 fu
0.023
17.9
*.3S3
.609

.00699
18.10
.02095
31.30
.03*79
*0.*0
.0*870
50.60
35.60
25.*
*.722
.826

.00698
10.10
.02095
3*.30
.03*89
*3.*0
.0<*883
51.80
37.*B
*1600.
16*70.
33
99.5
199.1
187.5
838.0
1.1160.0
59.7
395.0
13.86
0.000
5.15
.0129
2*0.0
.0126
.10*
.331
99.618

2.62
3.13
751.1

19*.*
U.793
3.550
CH*
9.0
.391
.09*
.0265

39.0
*.87*
1.170

*.o
.500
.120

*3.0
5.37*
1.290

.00698
15.70
.0209*
28.90
.03*87
*0.*0
.0*079
*8.20
33.80
OEM PT.F
* 19. REL HUH* ".0.00 SPEC HUM' .002000
S LN T,F= 300.0 FLO.L/H* 1*.160 SL TIM.S* 6.5000
3*
1.0
0.0
0.0
903.0
1.1080.0
55.7
351.0
13.85
2.16*
6.7*
.0150
250.0
.01*3
.210
.36*
99.389
OF REOUCEC
2.97
3.12
778.9

3*5. B
22.999
5.750

21.0
.000
.200
.03*8

37.5
*.107
1.027

8.0
.876
.219

*5.5
*.983
1.2*6

.00698
30.10
.02093
*5.80
.03*06
5*.ZO
.0*878
60.10
SB. IB
35
22.7
*5.
*2.
912.
4.10*0.
57.
357.
13.06
1.878
6.62
.0150
258.0
.01*3
.209
.357
99.552

2.98
3.13 _ 	 ..... ..
806.3

26*. 6
17.665
*.5S8

9.6
.366
.09*
.0207

39.2 .._ 	 .. 	 	
*.298
1.109

8.3
.910
.235

*7.5
5.200. ... . 	 	 _. 	 	 , 	 ... .. . ...
1.3**

.00700 	 	 	 _ 	 ._ ...
19.30
.02101
36.10
.03*98
*5.80
.0*898 ...'._
51.21
30.50
                                                                                                                                            3


                                                                                                                                            3
                                                                                                                                                                3


                                                                                                                                                                3


                                                                                                                                                                3


                                                                                                                                                                3
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARC HET VALUES
      2.EQUIVALENCE RATIO CALCULATED FROM COZ.CO.AND HC DATA AND FUEL COMPOSITION.
      3.MASS EMISSIONS OF NC, N02, AND NO*N02 CALCULATED AS N02 FROM CONCENTRATIONS  KITH MOLECULAR MEICnT  OF MB
     I..COHBUSTIOM  EFFICIENCY CALCULATED F*OH CO,MO UHC AS VtPOtlZEO OKI61MAL FUEL  OH LI/ 10  FUEL  IASJS.
                                                                                                                                      U6.fl).
 j


£

-------
)   .......................................
      ENGINE'  6TCP15-91CK      S/N=  16179
    DATA  POINT NUMBER                   31
>   EMISSION RATE LB/HR
       CARBON MONOXIDE              5.225
       UNBURNEO HYDROCARBONS         l.*57
>      OXIDES OF NITROGEN            .619
       NITRIC OXIDE                  .306
    POKER LEVEL HP                   0.11
1   TOTAL CORRECTED HORSEPOHER       1.10     	
    BRAKE SPECIFIC EMISSION INDEX  IB/lllIHP-HR
       CARBON MONOXIDE              0.109    7*.291
       UNBURNEO HYDROCARBONS         0.810    11.263
       OXIDES OF NITROGEN           1.101    11.051
       NITRIC OXIDE                 0.111     6.961
                                                                  •**  AIRESEARCH EMISSION TEST SUMMARY
                                                                  COMB P/N< 69S16S-3 TEST DATE  6-13-75
                                                                      32

                                                                   5.556
                                                                    .81,2
                                                                    .826
                                                                    .5Z1
                                                                  7<>.76
     33

  3.550
   .09<»
  1.291
  1.179
187.1.9
199.16

 11.936
   .511
  6.879
  6.239
   3d

5.751
 .211
1.2*6
1.027
                                                                                      23.792
                                                                                        .121
                                                                                       5.155
                                                                                                    35
          1.189
        Z54..77
        261.12

         17.419
           .371
          5.27*
          t.353
                                                                                                              FUEL

-------
                       ENGINE HFR. I AIRESEARCH
                      MODEL NO. t  GTCP8S-98CK
                      FUEL I ASTM 01655-73
 TEST FACILITYl PHX LACC2        INSTR.  OESCRIP.I   FEDERAL REG V38 N136    CALC. OATEI
 S/NI  36179          ENGINE  TYPE  (CLASS*I  APU               CALC. I.O.I     Z
MAX SHP       ZOO. * BLEED  AIR EXTRACTION TO    1151. DEC. F E6T
    ATONIC H/C RATIOI   1.928   LHVI      18470.  BTU/LB.      AOOITIVESI NONE
6-13-75
                                 EXHAUST EMISSIONS PER EPA RATED WORK  OUTPUT ••  CODE OF FEDERAL REGULATIONS TITLE 1.0 PART 87
                                •••••••••••••••••••••••••••••I ^MISSIONS COMPUTED  FSOM TEST CONDITION NO.  5   •»»•»»»»»»«»»«
                                         HYDROCARBONS (HC AS CH«I              .1.55  '.B. POLLUTANT PER 1000 HP.-HR.
                                         CARBON MONOXIDE (COI               17.6*0  LB. POLLUTANT PtR 1000 HP.-HR.
                                         OXIDES OF NITROGEN (NOX AS NOZ)     5.334  LB. POLLUTANT PER 1000 HP.-HR.
                                                                             17 JULY 197]
                      [[[  £NGINE  DESCRIPTION  ••••••••••••••••
                      CONBUSTOR TYPE! TANGENTIAL CAN          P/N>  698164-3   SURFACE/VOLUME I   .725 SQ IN/CU IN
                      ENGINE TOTAL SERVICE!      0.0 HR.   TIME SINCE ENGINE OVERHAUL'        0. HR.
                      ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                      AIRCRAFT INSTALLATION »•* MFR.I
                                                                                   MODEL  NO.I
                                                                FUEL INJ. TYPE I
                                                                                                                          USERI
                                                                                    DUAL ORIFICE
 0)
vQ
                      »••*••»»«••••*•»•••••..•.•.».••••»••«.*•»*«•••••OPERATIONAL  TtST  DATA  SUMMARY •••••••••••••••••»•••••»••••••••••»•••••••••••••
                      GASEOUS EMISSION TEST NO. I     3    OATEI  6-13-75      TIMES     12.1.5      BARO.  PRESS.I  Z8.740 IN. H6A.
                      AMBIENT AIR TEMP.I 39.0  DEC. F        RELATIVE HUHIOITYI  «D.OO  PERCENT       SPECIFIC HUMIOITTI  .OOZOOO L8. HZO/LB. DRV AIR
                      AMBIENT AIR QUALITY    HYDROCARBONS IHCII 0.0   PPMC    CARBON  MONOXIDE (COil 0.0    PPHV    OXIDES OF NITROGEN INOXII 0.0   PPMV
                      SAMPLE LINE •*• TEMP.I  300.00 DEC. F.     FLOMRATEI   tfc.lb LITERS/MIN.     TRANSPORT TIME I    6.50 SEC.     -LENGTH!   50.00 FT.
 u>
 o
TEST CONDITION
POWER SETTING, CORRECTED HP.
Nl SPEED, RPN
FUEL FLOW IMEAS.I LB./HR.
ENGINE CORE INLET AIRFLOW (CALC. 1 LB./SEC.
COMPRESSOR INLET TEMP., DEC. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP., OEG. F
COMPRESSOR BLEED AIRFLOW IMEAS.I LB./SEC.
• lEEO AIR PRESSURE, PSIA
BLEED AIR TEMPERATURE, DEG. F
ENGINE EXHAUST GAS TEMP., OEG. F
ERISSION CONCENTRATION, WET ANALYSIS
HYDROCARBON (HC AS CH4I , PPNC
CARBON MONOXIDE (COI , PPMV
TOTAL OXIDES OF NITROGEN (NOXI , PPNV
CARBON DIOXIDE ICOZI , PERCENT BY VOL.
NITRIC OXIDE (NOI, PPNV
EMISSION INDEX, LB. POLLUTANT/1000 LS. FUEL
HYDROCARBONS IHC AS CH4I
CARBON MONOXIDE ICOI
TOTAL OXIDES OF NITROGEN INOX AS N02I
EMISSIOK RATE. LB. POLLUTANT/HR.
HYDROCARBONS INC AS CH4I
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS NOZI
ENGINe WORK OUTPUT, MEAS. SHP
ENGINE WORK OUTPUT, ISENTROPIC AIR HP
ENGINE WORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS!
F/A lEMISSIONSI
36 37 38
0.11
41630.00
139.00
5.95
40.0
60.39
383.00
0.00
0.00
-0.10
••85.1

1ZO.OOI
Z5Z.100
18.000
1.318
9.001

10.157
37.330
4.378

1.412
5.189
.609
1.11
1.11
0.01
91.23
.116
• 79.28
• 414SO.OO
175.00
5.77
40.1
61.15
387.00
0.00
0.01
-1.00
595. 0

73.500
Z69.Z12
25.800
1.729
16.201
•
4.712
30.643
4.824

.837
5.363
.844
74.75
0.01
74.75
91.16
.111
199.12
41130.00
238.00
5.24
38.0
59.66
394.10
0.10
1. 10
-0.00
131.1

9.000
189.790
44.300
2.634
38.200

.389
14.356
5.504

.093
3.417
1.311
117.35
1.18
117.35
99.63
.•13
39
0.00
41160.00
252.01
6.97
31.1
55.31
353.11
2.12
54.11
373.11
913.1

21.111
354.666
45.511
3.103
38.511

.793
23.156
4.935

.211
5.135
1«2*>%
1.00
242. 46
242.46
99.39
.114
41
45.37
41011.11
256.1* "
6.76
39.*
56.81
357.1*
1.14
55.63 	 	 	
377.11
9*9.1

12.111
266.164
49.111
3.114
41.111

.451
17.564

-------
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ENGINE' GTCP05-98CK S/N* 36179
RAT SHP> 200. RA EGT,F« 1150.
FUEL H/C* 1.9280 STOI F/A- .06822
DATA POINT NUMBER 36
PERCENT MAX. CORRECTED POMER 0.0
CORRECTED SHAFT HP 0.
'MEASURED SHAFT HP o.
EXHAUST GAS TEMP., OEG.F 485.
SHAFT SPEED, Nl, RPM 41610.
COMPRESSOR DSCHG. PRES..PSIA 60.
COMPRESSOR OSCHG. TENP.OEG F 382.
EXHAUST GAS PRESS., PSIA 13.69
CORRECTED BLEED FLOM, LB/SEC 0.000
COMPRESSOR HAP FLOM, LB/SEC 5.92
Fl RATIO BASED ON MAP FLOM .0065
CORRECTED FUEi. FLOM , LB/HR 139.0
FA RATIO CALC. FROM EMISSION .0065
EQUIVALENCE RATIO .095
LOADING M/P**N/V/E(T/5*OI .382
COMB EFFIC' FROM EMISSIONS 98.231
CARBON DIOXIDE
PERCENT BY VOLUME, MET
LB. C02 PER LB. OF FUEL
MEIGHT FLOM, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
NEIGHT FLOM, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE INO) - NEIGMTS AS
PPM BY VOLUME, MET
LB. PER 10BO LB. OF FUEL
MEIGHT FLOM. LB./HR.
NITROGEN DIOXIDE CN02I
COMB P/N* 698168-3 TEST DATE 6-13-75 FUEL'AV. KERO. P BARO« 28.7%
RAT SPO' 41600. DEM PT , * 19. REL HUM* 40.01 SPEC HUM' .002000
L H V* 18*70. S LN T, ' 300.0 FLO,L/M* 14. 1M SL TIM, S« 6.5000
37 30
39.6 99.
79.3 199.
74.7 187.
5*5.0 831.
*1*50.0 41130.
60.1 59.
387.0 394.
13.73 13.06
0.000 0.000
5.65 5.08
.0006 .0130
175.0 238.8
.0084 .0126
.12* .185
.36% .327
98.860 99.620
1.32 1.73
3.07 3.09
1.26.4 5*1.2
252.1 269.2
37.330 38.6*3
5.189 5.363
CARBON. HEIGHTS AS
120.0 73.5
10.157 4.782
l.%12 .*37
.2721 .1561
M02
9.0 16.2
2.109 3.029
.30* .530
PPM BY VOLUME, MET 9.0
LB. PER 1000 LB. OF FUEL 2.189
NEIGHT FLOM, LB./HR. .30%
TOTAL OXIDES OF NITROGEN (N04N02I AS N02
•PPM BY VOLUME, MET 10.0
LB. PER 1000 LB. OF FUEL 4.378
MEIGHT FLOM, LB./HR. .609
SMOKE MEASUREMENT DATA
CORRECTED MEIGHT FLOM .00786
SMOKE NUMBER 16.90
CORRECTED MEIGHT FLOM .02110
SMOKE NUMBER 33.70
CORRECTED NEIGHT FLOM .03528
SMOKE NUMBER 42.20
CORRECTED MEIGHT FLOM .0*939
SMOKE NUMBER 48.20
SMOKE NUMBER AT MA«0.023 35.50
9.6
1.795
.31%
25.0
%.82%
.8*%
.0070%
19.30
.02113
33.70
.03521
%3.%0
.8*927
51.20
37.20
2.63
3.13
7*5.0
169.0
14.356
3.417
CH4 .
9.0
.309
.093
.0271
30.2
4.7*6
1.130
6.1
.750
.100
44.3
5.50«
1.310
.0070%
13.30
.02113
31.30
.03519
39.80
.0*925
44.60
32.60
3
0.
0.
0.
903.
41060.
55.%
353.0
13.05
2.16%
6.67
.015%
252.0
.01%*
.212
.360
99.306
REDUCED
3.00
3.12
705.1
350.7
23.156
5.035
21.0
.793
.200
.0342
30.5
4.176
1.052
7.0
.759
.191
*5.5
%.935
.00703
31.30
.02109
40.20
.03512
. 60.20
.0*913
69.90
52.00
*8
22.7
*z!7 ~" " 	 "" '
909.0
41080.0 _ 	 	
56.8
357.0
13.85
1.879
6.59
.0150
256.8
.81%4
.212
.357
99.5*7
3.01
3.13

266.2 .
17.56%
%.*96
12.0
.»S3
.116 :
.0250
*.*77
1.1*6
.035
*9.8 '
5.111
1.360
.00702 !
19.30
.02107
3*. 90 ;
.03510
**.60
.0*911
52. %0
30.20
                                                                                                                                                                >
                     MOTES  1.  ALL EMISSIONS  CONCENTRATIONS ARE MET VALUES.	
                           2.EQUIVALENCE RATIO CALCULATED FROM CO2.CO.ANO HC  DATA  AND FUEL  COMPOSITION.
                           3.MASS EMISSIONS  OF NO,  N02, AND NO»H02 CALCULATED AS N02 FROM CONCENTRATIONS MITH MOLECULAR NEIGHT OF N02 1*6.811.
                           %.COMBUSTION EFFICIENCY  CALCULATED FROM CO.tNC UHC AS VAPORIZED  ORIGINAL FUEL ON LB/ LB FUEL BASIS.

-------
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U3
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 to
  ENGINE. GTCP85-98CK      S/N- 36179
DATA POINT NUMBER                   36        37
EMISSION RATE LB/HR
    CARBON MONOXIDE              5.189     5.363
    UNBURNEO HYDROCARBONS        1.413       .837
    OXIDES OF NITROCEN            .609       .844
    NITRIC OXIDE                  .304       .530
PONER LEVEL HP                   0.00     74.75
TOTAL CORRECTED HORSEPONER       0.10     79.38
BRAKE SPECIFIC EMISSION INDEX LB/1IOOHP-HR
    CARBON MONOXIDE              0.010    71.741
    UN6URNEO HYDROCARBONS        0.000    11.195
    OXIDES OF NITROCEN           0.000    11.Z94
    NITRIC OXIDE                 0.000     7.091
                                                                ••••   AIRESEARCH  EMISSION TEST SUMMARY
                                                                COMB  P/N= 696168-3  TEST  DATE  6-13-75
                                                                              30

                                                                           3.417
                                                                            .093
                                                                           1.310
                                                                           1.130
                                                                         187.35
                                                                         199.12

                                                                          18.Z37
                                                                            .494
                                                                           6.993
                                                                           6.0Z9
     39

  5.835
   .ZOO
  1.344
  l.OSZ
Z4Z.46
Z»7.Z5

 24.068
   .834
  5.130
  4.341
                                                                                                             FUEL-AV. KERO.
     41

  4.496
   .116
  1.360
  1.1*6
Z54.90
361.95

 17.640
   .455
  5.33*
  4.496
                                                                                                                               P BAROs 20.7*
                          NOTE**0. APPEARING IN BRAKE SPECIFIC EMISSION INDEX COLUMN DENOTES AN IDLE CONDITION

-------
                          ENGINE  MFR. t  AIRESEARCH
                         MODEL  NO. 1   GTCP15-91CK

                         FUCL<  ASTH  01655-73
                               TES.T FACILIITI PHX LACCZ        INSTR.  OESCRIP.I   FEDERAL REC ¥38 N136    CALC. DATE!
                               S/NI  36179          ENGINE  TYPE  (CLASS! I   APU               CALC. I.0.«     3
                              MAX SHP       zoo. » BLEED  AIR EXTRACTION TO    lift. DEC. F EST
                                  ATONIC H/C RATIO!   1.921   LHVI     11071.  BTU/LB.      AOOITIVESI NONE
                                                                                                                      6-13-75
                                    EXHAUST EMISSIONS PER EPA RATED WORK OUTPUT •• CODE OF FEDERAL REGULATIONS  TITLE  00 PART  17
                                   »•••••••»•••»•••••••»»»»•••»•• EMISSIONS COMPUTED FROK TEST CONDITION NO.  5    »»•••«•»•»••»•
                                            HYDROCARBONS (HC AS CHOI             .350  LB. POLLUTANT PER 1181 HP.-MR.
                                            CARBON MONOXIDE (CO)               17.606  <.B. POLLUTANT PER 1081 HP.-MR.
                                            OXIDES OF NITROGEN (NOX AS NOZI     5.305  LB. POLLUTANT PER 1881 HP.-Hit.
                                                                                                           17 JULY 1973
[[[  EN6IM£  DESCRIPTION  ••••••••••••••••
COMBUSTOR TYPE) TANGENTIAL CAN          P/NI   691168-3   SURFACi/VOLUME I   .725  SO. IN/CU IN
ENGINE TOTAL SERVICE!      0.0 HR.   TINE SINCE ENGINE  OVERHAUL!        I.  MR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                         AIRCRAFT  INSTALLATION ••• MFR. 1 "
                                                                                     MODEL NO. I
                                                                                                                       FUEL INJ.  TYPEI
                                                                                                                             USER!
                                                                                                                                           DUAL ORIFICE
 •o
 0)
*
 Co
 Co
) GASEOUS EMISSION TEST NO. 1 3 3ATEI 6-13-75 TINE< 13.01 BARO. PRESS. 1 21.701 IN. MCA.
AMBIENT AIR TEMP.I 39.0 DEC. F RELATIVE HUMIOITY1 00.00 PERCENT SPECIFIC HUMIDITY! .082881 LB. H20/LB. DRY AIR
AMBIENT AIR QUALITY HYDROCARBONS (HCI I 0.0 PPHC CARSON MONOXIDE ICO) 1 O.t PPNV OXIDES OF NITROGEN (NOX1I 8.8 PPMV
) SAMPLE LINE ••• TEMP.I 300.10 OEG. F. FLOWRATEI 1O.16 I.ITERS/NIN. TRANSPORT TIHEI 6.51 SEC. LENGTHI 51.11 FT.
>
TEST CONDITION
PONER SETTING. CORRECTED HP.
Nl SPEED, RPM
FUEL FLOW (MEAS.I LB./HR.
) ENGINE CORE INI.ET AIRFLOW ICALC. 1 LB./SEC.
COMPRESSOR INLET TEMP.. DEC. F
COMPRESSOR DISCHARGE AIR PRESSURE. PSIA
) COMPRESSOR DISCHARGE AIR TEMP., OEG. f
COMPRESSOR BLEED AIRFLOW (NEAS. ) LB./SEC.
BLEED AIR PRESSURE, PSIA
) BLEED AIR TEMPERATURE. OEG. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSIOK CONCENTRATION, NET ANALYSIS
) HYDROCARBON (HC AS CHOI. PPNC
CARBON MONOXIDE (COI . PPHV
TOTAL OXIDES OF NITROGEN (NOXI, PPHV
) CARBON DIOXIDE (C02) . PERCENT BY VOL.
NITRIC OXIDE (NOI, PPMV
EMISSION INDEX, LB. POLLUTANT/1100 LB. FUEL
) HYDROCARBONS (HC AS CHOI
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS N92)
) EMISSION RATE, LB. POlLUTANT/HR.
HYDROCARBONS (HC AS CHOI
CARBON MONOXIDE (COI
> TOTAL OXIDES OF NITROGEN (NOX AS N02)
ENGINE WORK OUTPUT, MEAS. SHP
ENGINE WORK OUTPUT, ISENTROPIC AIR HP
) ENGINE WORK OUTPUT, TOTAL HP
COH3USTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS!
01
0.11
01620.00
131.10
5.97
39.1
60.39
380.11
l.ll
1.81
-1.00
016.0
103.500
17! 718
1.316
11.111
i.iso
36.919
0.352
1.222
5.110
.601
l.ll
1.81
0.88
91.35
.186
EO EMISSIC
02
79.30
175.81
5.11
39.1
61.15
310.11
8.80
8.81
-0.80
595.0
67.510
2S.888
1.721
16.111
31.001
0.808
.772
5.502
.808
70.73
1.81
70.73
91.17
.118

03
198.67
01120.81
201.11
5.33
01.1
59.01
395.01
l.ll
l.ll
-1.81
130.1.
7.511
119.791
z!eoi
31.111
.321
10.511
5.623
.179
3.011
1.309
117.31
l.ll
117.31
. 99.63
.113

oo
i.ii
251.' II
6.95
08.8
50.99
353.18
2.12
53.62
370.18
916.8
19.581
362.Z36
05.511
2.991
31.511
.739
20.113
0.952
.185
6.881
1.231
l.ll
201.59
201.59
99.37
.110

05
05.35
Z56.*ll ~~
6.77
39.8
56.56
356.88
1.84
55.31
376.88
921. 8 _ ...__. _. 	 	 ;.
9.318
01.111 ~ ~
3.118
61.388
.351
17.499
5.319
..898 	 .

-------
 0)
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 0)

 U>
 4*.
ENGINE* GTCP85-96CK S/N
RAT SHF> 210. RA EGT.Fr
FUEL H/C* 1.9210 STOI F/A*
DATA POINT NUMBER
PERCENT MAX. CORRECTED POWER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR DSCHG. TEMP, KG f
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOH, LB/SEC
CORRECTED FUEL FLOH , L6/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P**N/V/E(T/540)
COMB EFFIC FROM EMISSIONS
« 36179
1150.
.06822
*1
1.1
0.0
0.0
416.1
•,1621.0
60.*
311.0
13.69
1.001
138.0
.0064
.894
0.
99.353
CONS ffH* 696161-3 TEST DATE 6-13-75 FUEl'AV. ««O. P 8ARO* 21.7*
RAT SPO* 41600. DEH PT.F« 19. REu HUM* 40.00 SPEC HUM* .112101
L H V* 11*70. S .N T.FB 300.0 FLO.L/M* 14.160 SL TIN.S* 6.5118
*2 *3 ** *5
39.7 99.3 1. 22.7
79.3 191.7 1. 45.3
74.7 117.3 1. *2.
595.1 13*. 1 916. 921.
«1*40.1 41121.1 41040. 41911.
60.1 59.* 55. 56.
314.1 395.1 353. 356.
13.74 13.17 13.14 13.15
0.000 1.110 2.167 1.176
175.1 2<.0.1 251.1 256.1
.001* .1125 .11** .11**
.123 .113
.366 .331
98.S73 99.630
CARBON DIOXIDE
PERCENT BY VOLUTE, HET 1.31 1.72
Li. COZ PER LB. OF FUEL 3.17 3.19
HEIGHT FLOH, LB./HR. 42J.9 5*1.2
CARBON MONOXIDE
PPM BY VOLUME, HET 2*7.1 274.1
LB. P£R 1101 LB. OF FUEL 36.919 31.4*1
HEIGHT FLOH, LB./HR. 5.11* 5.502
UNBURNED HYDROCARBONS- PPM AS ;ARBON, HEIGHTS AS
PPM BY VOLUME, HET 103.5 67.5
L3. PER 1110 LB. OF FUEL 1.15* «.*!*
HEIGHT FLOH, LB./HR. 1.222 .772
RATIO L6 HC/LB CO .239* .1414
NITRIC OXIDE INOI - HEIGHTS AS NOZ
PPM BY VOLUME, HET 11.0 16.1
Li. PER 1010 LB. OF FUEL 2.70* 3.017
HEIGHT FLOH, LB./HR. .373 .526
NITROGEN DIOXIDE (N02I
PPM BY VOLUME, HET 6.7 9.1
LI. PER 1011 LB. OF FUEL 1.6*7 1.1*2
HEIGHT FLON, LB./HR. .227 .322
TOTAL OXIDES OF NITROGEN (NC»M32I AS N02
PPM BY VOLUME, HET 17.7 25. I
LI. PER 1110 LB. OF FUEL 4.352 4'.841
HEIGHT FLOH, LB./HR. .611 .1*1
SMOKE MEASUREMENT OAT*
CORRECTED HEIGHT FLCH .10712 .00702
SMOKE NUMBER 16.30 21.71
CORRECTED HEIGHT FLCH .02115 .02115
SMOKE NUMBER 36.11 37.31
CORRECTED HEIGHT FiCH .13511 .03507
SMOKE NUMBER *3.»0 45.81
CORRECTED HEIGHT FLCH .0*909 .04919
SMOKE NUMBER 50.60 5*. 20
SMOKE NUMBER AT HA»I.023 37.11 41.11
2.61
3.13
751.3
119.1
14.501
3.400
CH*
7.5
.321
.079
.1226
38.1
4.769
1.145
6.1
.153
.215
44.8
5.623
1.3*9
.00700
21.71
.12111
32.51
.03*99
42.20
.0*197
46.41
36.11
.211
.367
99.371
REDUCED
2.99
3.11
771.6
362.2
24.013
6.011
19.5
.739
.115
.0311
11.5
4.191
1.1*1
7.1
.762
.191
45.5
4.952
1.231
.10700
31.30
.02101
51.10
. 03*97
61.41
.0*197
71.51
54.31
.211 	 	
.357
99-551
3.11
3.13
808.2
264. 6
17.499
*.*••
9.3
.151
.190
«12B1
41.3
*.4I6
1.1*1
7.5
.11$
.219
48.1
5.311
1.357
.11711
21.51
.12111 . . .. .'. _ 	 	
37.31
.13491
*6.*1 ........ ; . .. ... . . -•
.1*191
53.11
39.fl . . „ . ........... : 	 . _'.. 	 	 	 . ..-.. . ..
                      NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE  HET  VALUES.
                            Z.EQUIVALENCE RATIO CALCU.ATEO FROM  COZ,CO.AND HC  DATA AND FUEL COMPOSITION.
                            3.MASS EMISSIONS OF NO, N02, AND NO«N02  CALCU.ATEO AS N02 FROM CONCENTRATIONS MITH MOLECULAR HEIGHT OF NOZ (46.11>.
                            *.COMBUSTION EFFICIENCY CALCULATED FROM  CO.AND UHC AS VAPORIZED ORIGINAL  FUEL ON LB/ LB FUEL BASIS.

-------
                                                  S/N-  36179
                         ENGINE' GTCP85-98CK
                       DATA POINT NUMBER
                       EMISSION RATE LB/HR
                           CARBON MONOXIDE
                           UNBURNEO HYDROCARBONS
                           OXIDES OF NITROGEN
                           NITRIC OXIDE
                       POMtR LEVEL HP
                       TOTAL CORRECTED HORSEPOWER
                       BRAKE SPECIFIC EMISSION INDEX  LB/1000HP-HR
                           CARBON MONOXIDE               0.000    73.625
                           UNBURNED HYDROCARBONS         1.000    10.336
                           OXIDES OF NITROGEN            0.000    11.353
                           NITRIC OXIDE                  0.000     7.0<>1
                                                                  »•*  AIRESEARCH EMISSION  TEST  SUMMARY
                                                                  COMB P/N« 69«16»-3 TEST DATE   6-13-75
                                                      FUEL'AV. KERO.
                                                                        P BARO«
5.10".
l.ZZZ
 .611
 .373
0.01
 .00
 5.502
  .77Z
  .81.8
  .5Z6
Tl,.73
79.3%
  3.000
   .079
  1.31.9
  1.K.5
187.31
198.67

 18.581
   .420
  7.201.
  6.111
  6.OBI
   .185
  1.Z38
  1.01.8
Z<.1.55
2<>6.B2

 2
-------
                                                                                                                                                                 S:
                      ENGINE NFR.I AIRESEARCH
                     N00EL MO.I  CTCP6S-98CK
                     FUEL! ASTM 01655-73
                                TEST FACILITY! PHX LACC2       INSTR. OESCRIP.»  FEDERAL REG V38 N136
                                S/NI  16179          ENGINE TYPE (CLASS) 1  »PU              C»LC. I.O.I
                               MAX SMP       ZOO. » BLE£D AIR EXTRACTION TO    1159. DEC. F £61
                                   ATOMIC H/C RATIOI   1.921    LHVI     181.71). BTU/LS.     ADDITIVES! NONE
C*LC. OATE«  6-14-7S
   1
            EXHAUST EMISSIONS PER EPA RATED NORK OUTPUT •• CODE OF FEDERAL REGULATIONS TITLE 40 PART 87
           .............................. £HjSSIONS COMPUTED FSOM TEST CONDITION NO.  S   ..............
                    HYDROCARBONS (HC AS CH4I             .334  LB. POLLUTANT PER 1008 HP.-HR.
                    CARBON MONOXIDE (CO)               19.179  LB. POLLUTANT PER 1001 HP.-HR.
                    OXIDES OF NITROGEN (NOX AS N02)     4.191  LB. POLLUTANT PER 1000 HP.-HR.
                                                                                                                               17 JOLT 1973
 [[[  ENGIN£ JESCRIPTION  •»••»••••»».»...
 COMBUSTOR TYPE! TANGENTIAL CAN          P/Nt  69816D-3  SURFACE/VOLUME I  .725 SQ IN/CU IN
 ENGINt TOTAL SERVICE!     0.0  HR.   TIME SINCE ENGINE OVERHAULI       0. HR.
 ENGINE ASSEMBLY AND MAINTENANCE INFORMATION I
                     AIRCRAFT INSTALLATION **• MFR.t
                                                                                 MODEL NO. I
                                                                                                                  FUEL INJ. TYPE'
                                                                                                                        USERI
                                                                                                                                      DUAL ORIFICE
01
                     ................................................OPEHATJONAL TEiT OATA SUMMARY ••»••»»•»»•••»••••«••••••••••••»••»•••»••««»••••
                     GASEOUS EMISSION TEST NO.I     4    DATEI  6-14-75      TIMtt    07.45      BtRO.  PRESS.I  28.768 IN. HGA.
                     AMBIENT AIR TEMP.I  39.0  OEG.  F        RELATIVE HUMIOITYI 103.00 PERCENT       SPECIFIC HUMIOITYI  .005011 L8. H20/LB. DRY AIR
                     AMBIENT AIR QUALITY    HYDROCARBONS (HOI 0.0   PPHC    CARBON HONOXIDE (CO) I 0.0    PPHV    OXIDES OF NITROGEN (NOX) I 0.0   PPHV
                     SAMPLE LINE •»• TEMP.I  300.00 DEC. F.     FtOMRATEi   14.16 LITERS/MIN.     TRANSPORT TIMEI    6.SO SEC.     LENGTH!   50.01 FT.
U)
o\
                                                                          COMPUTED EMISSIONS
                )


                )
 TEST CONDITION                                          46        47        48        49        SI
 POWER SETTING. CORRECTED HP.                           t.OO     79.34    198.97      1.18     45.18
 Nl SPEED,  RPM                                     41650.00  -.1518.00  41170.00  41090.00  41041.11
 FUEL FLON  (MEAS.)  LB./HR.                           1*5.11    178.11    251.11    261.11    265.11
 ENGINE CORE INLET  AIRFLONtCALC.)  LB./SEC.             6.21      5.85      5.46      6.97      6.77
 COMPRESSOR INLET TEMP.,  OEG.  F                        48.8      41.8      39.1      18.1      39.1
 COMPRESSOR DISCHARGE AIR PRESSURE, PSIA              62.46     61.47     61.49     55.48     57.2B
 COMPRESSOR DISCHARGE AIR TEMP.,  DEC. F              373.10    377.11    384.80    341.11    345.11
 COMPRESSOR BLEED AIRFLON (MEAS.)  LB./SEC.             0.10      1.10      0.00      2.21      1.93
 BLEED AIR  PRESSURE,  PSIA                              l.ll      0.00      0.81     50.21     56.17
 BLEED AIR  TEMPERATURE, DEC. F                        -l.ll     -1.11     -1.11    361.11    364.11
 ENGINE EXHAUST CAS TEMP., OEG. F                      471.1     586.0     832.8     925.1     931.B
 EMISSION CONCENTRATION,  NET ANALYSIS
      HYDROCARBON (HC AS  -CH4), PPHC                121.581    72.101     9.Ill    15.118     9.181
      CARBON MONOXIDE (CO). PPMV                    2*4.671   277.404   196.299   317.124   Z95.657_
      TOTAL OXIDES  OF NITROGEN (NOXI, PPNV          16.700    23.208    40.900    45.501    45.901
      CARBON DIOXIDE (C02), PERCENT BY VOL.          1.318     1.734     2.655     3.154     3.171
      NITRIC OXIDE  (NO).  PPHV                         8.800    14.700    34.500    38.001    39.381
 EMISSION INDEX,  LB.  POLLUTANT/1800 LB. FUEL
      HYDROCARBONS  (HC AS CH4)                      10.288     4.671      .366      .541      .121
      CARBON MONOXIDE (CO)                          36.2*6    31.485    14.727    19.976    18.537
      TOTAL OXIDES  OF NITROSEN (NOX AS N02)          4.864     4.325     5.841     4.718     4.727
 EMISSION RATE,  LB.  POLLUTANT/HR.  •
      HYDROCARBONS  (HC AS CH4)                        1.492      .831      .196      .141      .815
      CARBON HONOXIDE (CO)                            5.256     5.604     3.682     5.194     4.912"
      TOTAL OXIDES  OF NITROGEN (NOX AS N02)           .519      .771     1.261     1.224     1.253
 ENGINE NORK OUTPUT,  MEAS.  SMP                         0.11     74.86    187.54      l.ll     42.77
 ENGINE NORK OUTPUT,  ISENTROPIC AIR HP                 8.11      g.QO      l.ll    241.21    213.15
 ENGINE NORK OUTPUT,  TOTAL  HP                           0.81     74.86    187.So    241.28    256.12
COMBUSTION  EFFICIENCY, PERCENT (EMISSIONS)            98.24     98.85     99.62    .99.48   ~  99.54
-------
 •o
 fu
U3
 ID

 U)
ENGINE' GTCP05-90CK S/N* 36179
RAT SHP« 200. RA E6T.F*
FUEL H/C« 1.9208 STOI F/A«
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OEG.F
SHAFT SPEED. Nl, RPH
COMPRESSOR OSCHG. PRES. .PSIA
COMPRESSOR OSCHG. TEMPtOEG F
EXHAUST GAS PRESS. • PSIA
CORRECTED BLEED FLOH, LB/SEC
COMPRESSOR HAP FLOM, LB/SEC
FA RATIO BASED ON HAP FLOH
CORRECTED FUEL FLOH , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING N/P**N/V/EIT/5*OI
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
LB. C02 PER LB. OF FUEL
HEIGHT FLON, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, HET
LB. PER 1000 L8. OF FUEL
NEIGHT FLON, LB./HR.
UNBURNEO HYDROCARBONS* PPM AS
PPH BY VOLUHE, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
RATIO LB HC/LB CO
1150.
.06022
*6
8.
0.
0.
*71.
-.1650.
62.5
373.0
13.69
0.000
6.10
.0066
1*5.0
.0065
.095
.377
90.2*5
CONB P/Nx 690160-3 TEST DATE 6-l*-75 FUEL«AV. KERO. P BARO- 20.76
RAT SPO« *1600.
L H V« 10*70.
*7 *0
39.7 99.5
79.3 199.0
7*.9 107.5
506.8 032.0
1.1510.0 *1170.0
61.5 60.5
377.0 30*. 0
11.75 13.86
0.000 0.000
5.75 5.17
.0006 .013*
176.0 250.0
.0005 .0127
.12* .107
.363 .332
OEM PI, *
S ..N T, »
*
0.
0.
0.
925.
*1090.
55.5
3*1.8
13.8*
2.239
6.77
.8156
260.0
.0151
.222
.369
98.850 99.620 99.1.83

1.32
3.07
**s.o

2**. 7
36.2*6
5.256
CARBON H£l
121.5
10.280
1 . *92
.2030
1.73 2.66
3.89 3.13
550.3 702.5

277.* 196.3
31.*05 1*.727
5.60* 3.602
&HTS AS CH*V
72.8 9.8
*.671 .366
.031 .096
.1*0* .8262
3.15
3.12
611.5

317.1
19.976
5.19*

15.0
.5*8
.1*8
.8278
*0. REL HUH' 100.00 SPEC HUH> .185668
300.0 FLO.L/M* 1*.160 SL TIM,S« 6.5868
58
22.7
*5.* ...._..
*2.6
938.8
1.16*6.0 	 	 .. ._ . ... . .._ 	 .
57.2
3*5.0
13.85 . . _
1.96*
6.67
.0155 _ 	 	 	 ._.....
265.0
.0152
.223 . ... 	 	 	 . . . . 	 	 _ .... .
.360
99.536

3.17
3.12 	 . 	 : 	 : 	 	 ...._.. 	 	 .
627.9

. 295.7 	 	 	 J 	 _•_.. 	
16.537
*.912

9.0
.321
.065
.017*
NITRIC OXIDE INOI - HEIGHTS AS N02
PPM BY VOLUME, HET
L*. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE (M02I
PPK BY VOLUME, NET
L3. PER 1000 LB. OF FUEL
HEIGHT FLON, LB./HR.
6.0
2.1*1
.311

7.9
1.922
.fro
TOTAL OXIDES OF NITROGEN (NO*N02> AS N02
PPM BY VOLUME, HET
LB. PER 1008 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLON
SMOKE NUMBER
CORRECTED NEIGHT FLOH
SMOKE NUMBER
SMOKE NUMBER AT NA»0.023
NOTES 1. ALL EMISSIONS CONCEN1
. 16.7
*.B6*
.569

.00710
10.10
.02131
32.50
.03550
tl.OS
.0*970
*S.B8
3*. 58
SAT TOMS ARE
2. EQUIVALENCE RATIO CALCULATED FROM
3. MASS EMISSIONS OF NO,
*. COMBUSTION EFFICIENCY
1*.7 3*. 5
2.7*1 *.252
,*00 1.863

0.5 6.*
1.585 .709
.202 «.197

23.2 *0.9
*.3Z5 5.0*8
.770 1.260

.00710 .00711
17.58 15.78
.82131 .0213*
33.78 38.78
.03550 .03555
*Z.20 30.68
.8*978 .6*976
51.68 *6.*8
36.56 33.08
HET VALUES.
COZ.CO.ANO HC DATA
N02, AND NO»NOZ CALCULATED AS
CALCULATED
FRON CO, AND UMC AS
30.0
3.932
1.022

7.5
.776
.202

*5.5
*.706
1.Z2*

.00711
19.30
.0213*
38.66
.035*6
«.9.*0
.0*965
59.66
*1.98

AND FUEL
39.3
*.8*7
1.873

6.6
.686
.100

*5.9
*.727 	 	
VZ53

.00703
21.70
.02110
36.18 .
.83507
*8.26
.0*988 • .__ 	 	 	 ...._....._ 	 - .
56.68
kl.10

COMPOSITION.
NOZ FROM CONCENTRATIONS HITH MOLECULAR HEIGHT OF N02 l*6.01>.
VAPORIZED
ORIGINAL FUEL ON LI/ LI FUEL OASIS.
                                                                                                                                                                                                   I
                                                                                                                                                                                                   1
-------
t»
                      ENGINE' GTCP45-90CK
                    DAT* POINT NUMBER
                    EHISSIOK RATE LB/HR
                        CARBON MONOXIDE
                        UNBURNEO HYDROCARBONS
                        OXIDES OF NITROGEN
                        NITRIC OXIDE
                    POMER LEVEL HP
                    TOTAL CORRECTED HORSEPOHER
                                               S/N«
36179
    t
  .831
  .770
  .<.*B
7<>.86
79.3%
                    BRAKE SPECIFIC EMISSION INDEX LB/llODHP-HR
                        CARBON MONOXIDE              0.000    7<.. 06*
                        UNBURNEO HYDROCARBONS        0.000    11.107
                        OXIDES OF NITROGEN           0.000    10.ZOS
                        NITRIC OXIDE                 0.000      6.517
     lt»

  3.682
   .096
  1.Z60
  1.063
1B7. 5*
196.97

 19.63Z
   .51*
  6.719
  5.66*
     l>9

  5.19*
   .Itt
  l.ZZIi
  1.1Z2
Z<»1.28
Z45.06

 Z1.SZ6
   .SOZ
  5.073
  .91Z
   .815
  1.Z5J
  1.079
ZS6.1Z
Z63.ll

 19.179
 '  .33*
  4.891
  *.180
AN IDLE CONDITION
 5


b
co
oo
-------

                          ENGINE HFR.t AIRESEARCH
                         HODEL NO.t  GTCP85-98CK

                         FUELI ASTN 01655-73
                               TEST FACILITY! PHX LACC2       INSTR. DESCRIP.I  FEDERAL  REG  V38  N136    CALC.  OATEI
                               S/N1  36179          ENGINE TYPE  (CLASS) I  API)              CALC. I.O.I      2
                              MAX SHP       ZOO. » BLEED AIR EXTRACTION TO    11SI. OEG.  f ECT
                                  ATOMIC H/C RATIOI   1.921    LHVI     181.70. BTU/LB.     AODITIVESI TANGENTIAL CAN
                                                                                                                                               6-14-T5
13
(I)
iQ
(D

U)
                                     EXHAUST EMISSIONS P£R EPA RATED HORK OUTPUT »• CODE OF FEDERAL REGULATIONS TITLE ".0 PART
                                    .............................. £MIssiONS COMPUTED FROM TEST CONDITION NO.  5   • «»»»•«»••<
                                            HYDROCARBONS  (HC AS CHI.I             .450  LB. POLLUTANT PER 1000 HP.-HR.
                                            CARBON  MONOXIDE ICOI                19.066  LB. POLLUTANT PER 1000 HP.-HR.
                                            OXIDES  OF NITROGEN (NOX AS NOZI     4.961  LB. POLLUTANT PER 1000 HP.-HR.
                                                                                                                              87
                                                                                                                                    17 JULY 1973
                         [[[  EN6iNE DESCRIPTION  •»•»••••••••••••
                         COH9USTOR  TYPEI  NONE                     P/NI  698166-3  SURFACE/VOLUME I  .725 SQ IN/CU IN
                         ENGINE  TOTAL  SERVICEI           HR.   TIME SINCE ENGINE OVERHAUL!          HR.
                         ENGINE  ASSEMBLY  AND MAINTENANCE INFORMATION!
                          AIRCRAFT  INSTALLATION  •»•  MFR.I
                                                                                      MODEL NO.I
                                                                                              FUEL INJ. TYPE!
                                                                                                                             USER!
.............................................,..0p£RAnoNAL  T£ST  OATA  SUMMARY  ••»•»••••••»••••••••••••••••••»»•»••••••••••••••
GASEOUS EMISSION TEST NO.t     4    DATE!   6-14-75       TIMEI     08.45      BARO.  PRESS.!   28.760 IN. HGA.
AMBIENT AIR TEMP.I 39.0  OEG. F         RELATIVE  HUNIOITri  100.00  PERCENT       SPECIFIC  HUHIOITVI  .005000 LB. H20/LB. DRY AIR
AMBIENT AIR QUALITY    HYDROCARBONS (HCIt  0.0    PPNC     CARBON  MONOXIDE  ICOI!  0.0    PPHV    OXIDES OF NITROGEN (NOXII 0.0   PPNV
SAMPLE LINE "• TEMP.I  300.00 OEG. F.      FLOMRATEI    14.16 LITERS/HIN.    TRANSPORT  TIMEI    6.50 SEC.     LENGTH!   50.00 FT.
                                                     COMPUTED  EMISSIONS
                         TEST CONDITION                                           51        52        53        54        55
                         POKER SETTING, CORRECTED HP.                           0.00     79.                           37.060     30.665    14.858    19.699    18.411 	
                              TOTAL OXIDES OF NITROGEN (NOX  AS N02)           4.024      4.380     5.008     4.648     4.791
                         EMISSION RATE. LB. POLLUTANT/HR.
                              HYDROCARBONS (HC AS CH4I                        1.569       .809      .099     ..143 .  __  .115 '  .
                              CARBON MONOXIDE 
-------
^
\


















)

)


)





1





)


)


ENGINE* GTCP85-98CK S/N
RAT SHP* zaa. RA EGT.F:
FUEL H/C« 1.9260 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OEG.F
SHAFT SPEED, HI, RPH
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR DSCHC. TEMP.OEG F
EXHAUST GAS PRtSS.. PSIA
CORRECTED BLEED FLOM, LB/SEC
COMPRESSOR NAP FLOM, LB/SEC
FA RATIO BASED ON HAP FLOM
CORRECTED FUEL FiOM , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P*»N/V/E(T/5*0>
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
LB. C02 PER LB. OF FUEL
HEIGHT FLON, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, MET
IS. PER 1008 LB. OF FUEL
HEIGHT FLOM, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, MET
L«. PER 1800 LB. OF FUEL
HEIGHT FLOM, LB./HR.
RATIO LB HC/uB CO
NITRIC CXIOE (NO) - HEIGHTS AS
PPM BY VOLUME, MET
L9. PER 1088 LB. OF FUEL
HEIGHT FLOM, LB./HR.
NITROGEN BIOXIK 1*021
PPM BY VOLUME, MET
LB. PER 1088 LB. OF FUEL
HEIGHT FLOM. LB./HR.
> 36179
1150.
.06822
51
0.0
0.0
o.a
*72.0
*1670.8
62.6
370.0
13.68
a.oaa
6.18
.0066
1*5.0
.0065
.095
.378
98.179

1.31
3.07
***.6

2*9.6
37.060
5.374

COM3 P/N* 698168-3 TEST DATE 6-1W-75 FUEL=AV. KERO. P BARO' 28.76
RAT SPO* 1.1600. OEM PT.FC to. RE.. HUM* 100.00 SPEC HUM* .oosaea
L M V*
52
39.7
79.*
7*. 9
586.8
*1518.8
61.6
375.0
13.75
8.060
5.72
.0067
180.8
.0086
.126
.361
98.66*

1.76-
3.09
556.6

27*. 6
30.66*
5.520
CARBON. HEIGHTS AS
127.5
10.828
1.569
.2920
NOZ
18.8
Z.*39
.35*

6.5
1.585
.230
78.5
*.*96
.669
.1*66

15.8
2.7*9
.*95

8.9
1.631
.29*
16*70.
53
99.5
199.0
167.6
828.0
*1188.8
60.6
38*. 0
13.87
0.808
5.16
.0133
2*6.0
.8127
.166
.330
99.615
•SUMMARY
2.6*
3.13
776.1

196.6
1*.858
3.683
CM*
9.3
«*01
.899
.0270

35.8
*.339
1.076

5.*
.669
.166
S LN T,F=
5*
0.
0.
0.
92*.
*H9fl.
55.5
3*2.6
13.85
2.2*3
6.77
.8150
268.0
.01 wo
.217
.366
99.*68
OF REDUCED
3.09
3.12
611.6

306.3
19.699
5.122

15.6
.551
.1*3
.0260

38.5
*.067
1.857

5.5
.581
.151
300.0 FLO.L/M* i*.i60 SL TIN.S* 6.5088
55
22.7
*5.*
*2.8
928.8
*18Z6.8
57.1
3*5.8
13.65
1.959
6.67
.615*
26*. 0
.8156
. .228
.362
. 99.529

3.1*
3.12
62*. 7

298.*
18.*11
*.661

iz.e
.*35
. .115 ._ . . _„. _ . . 	 _... ,._. 	
.6236

39.9 . . .. . .. 	 	 .
*.155
1.097

6.1
.635
.166
TOTAL OXIOeS OF NITROGEN INO*NO2I AS NOZ
)


;





i


)
PPM BY VOLUME, MET
LB. PER 11108 LB. OF FUEL
HEIGHT FLOM, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOM
SMOKE NUMBER
CORRECTED HEIGHT FLOM
SMOKE NUMBER
CORRECTED HEIGHT FLOM
SMOKE NUMBER
CORRECTED MEIGNT FLOM
SMOKE NUMBER
SMOKE NUMBER AT NA*8.8Z3
16.5
*.OZ*
.583

.08699
2*. 70
.820)6
38.00
.03*95
**.oo
.0*860
*9.*a
39. *0
23.9
*.368
.786

.08781
19.38
.0210*
35.50
.03511
1.6.28
.8*913
51.80
39.10
*6.%
5.086
1.2*2

.00705
15.78
.82115
38.10
.8352*
*0.*8
.0*931
*7.IO
33.66
**.e
4*»6*t0
1.289

.86785
22.96
.02117
*3.*6
.83526
53.68
.0*937
59.60
*5.18
*6.fl
*.791
1.265

.60787 '..... _ 	 	 ._
28.56
.82122
36.66 . . _ 	 	 . ..
.83534
*6.68
.0*9** ...... . 	 _
56.68
*1.*6
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE MET VALUES.		.	
      2.EQUIVALENCE RATIO CALCULATED FROM COZ.CO.ANO HC  DATA AND FUEL  COMPOSITION.
      3.MASS EMISSIONS OF MO,  NOZ,  AMD NO»NOZ CALCULATED AS NOZ  FROM CONCENTRATIONS MITH MOLECULAR HEIGHT OF N02 U6.81I.
      *.COMBUSTION EFFICIENCY  CALCULITEO FROM CO,AND UHC AS VAPORIZED  ORIGINAL FUEl ON LB/ LB FUEL BASIS.
-------

ENGINE' GTCP85-9CCK S/N=
DATA POINT NUMBER
EMISSION RATE LB/HR
CARBON MONOXIDE
UNBURNEO HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIDE
POWER LEVEL HP
TOTAL CORRECTED HORSEPOWER
36173
51

5.37<»
1.569
.583
.351.
0.00
0.00
COH3 Pi
52

5.520
.809
.788
.t*95
71.. 86
79.1.2
                                                                     AIRESEARCH EMISSION  TEST  SUMMARY
                                                                          698168-3 TEST DATE   6-1I.-75
                                                                              53
                                                                                        51.
                                                                                                   55
5.520
.809
.788
.t*95
It. 86
'9.1.2
'3.737
0.811
.0.533
fc.611
3.683
.099
1.21.2
1.076
187.58
199.02
19.633
.530
6.621
5.736
5.122
.1*3
1.209
1.057
211.* 3
2.9AV. KERO.
                                                                                                                               P 8ARO= 38.76
                     3RAKE SPECIFIC EMISSION INDEX  LB/1000HP-HR
                         CARBON MONOXIDE               0.000
                         UNBURNEO HYDROCARBONS         0.000
                         OXIDES OF NITROGEN            0.000
                         NITRIC OXIDE                  0.000
                         NOTE*»0. APPEARING IN  BRAKE SPECIFIC EMISSION INDEX COLUMN  DENOTES AN IDLE CONDITION
 fl)
VQ
 0>
-------
13
PJ
to
                       FMGTNF HFR  1 AIRFSEARCH

                      HOOEL NO  1   6TCP8S-98CK
                            nu.    »1oro» »=
                      FUELI ASTM 01655-73
                               TEST FACILITri PHX L ACCZ       INSTR. OESCRIP.I  FEDERAL REG V38 N136    CALC. OATEi

                               S/NI  «l"          ENGINE TYPE ICLASSI 1  APU              CALC. I.D.I     3
                              N4J( SMf>       280> ^ 8LEEO 4IR EXTRACTION TO    1150. DEC . f EGT

                                  ATONIC H/C RATIOI   1.9ZJ    LHVI     181,70. BTU/LB.     ADDITIVES! NONE
                                                                                                                                            6-l»-7S
                                  FKHAUST EMISSIONS  P£R EPA  R»TEO WORK OUTPUT •• COOE OF FEDERAL REGULATIONS  TITLE  «.D  PART  87     17  JULY  1973
                                 .;..,.;».•...»•»•»•****•••**•*  EMISSIONS COMPUTED FROM TEST CONDITION  NO.  5   »«••»•••••••••••»•••••••••••••

                                         HYDROCARBONS  
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!

AIRCRAFT INSTALLATION ••• MFR.«
                                                                                  HOOEL NO. 1
                                                                                                                    FUEL  INJ.  TYPE!
                                                                                                                         ~USERt
                                                                                                                                        DUAL  ORIFICE
•»......»»»»••».»••••••»•••»»•»••••'••••••••••••OPERATIONAL TEST DATA SUMMARY ••••••••••••••»••»»••••»••••••••••»•••••••••••••
CASFOUS FMISSION TEST NO. I     *>    DATE!  6-l%-75      TIHEI    08.50      BARO. PRESS.I  Z8.7<>0 IN. HGA.
AMBIENT AIR TEMP I 39 0  OEG. F        RELATIVE HUMIDITY! 100.00 PERCENT       SPECIFIC HUMIDITY!  .005000 LB. H20/LB. DRY AIR
iMBiFNT AIR QUALITY  * HYDROCARBONS (HOI o.o   PPMC    CARBON MONOXIDE CCOM o.o   PPMV    OXIDES OF NITROGEN INOXII o.o   PPMV
SAMPLE LINE ••• TEMP I  300.00 DEC. F.     FLOMRATEI   1<>.16 LITERS/MIN.     TRANSPORT TIME!    6.50 SEC.     LENGTHI   50.00 FT.
TEST CONDITION
POWER SETTING, CORRECTED HP.
Nl SPEED, RPM
FUEL FLOW IMEAS.I LB./HR.
ENGINE CORE INLET AIRFLOWIC4LC.I LB./SEC.
COMPRESSOR INLET TEMP.. OEG. f
COMPRESSOR DISCHARGE »IR PRESSURE, PSIA
) COMPRESSOR DISCHARGE AIR TEMP.. OEG. F
COMPRESSOR BLEED AIRFLOW IM£»S.I LB./SEC.
8LEtO AIR PRESSURE. PSIA
) 1LEED AIR TEMPCTANJRE, OEG. F
ENGINE EXHAUST GAS TEMP.. OE6. F
EHISSIOK CONCENTRATION, W£T^ A ^^
*»* ortij MnunvTnr rpm PPMV
TOTAL OXIDES OF NITROGEN INOXI, PPMV
) CARBON DIOXIDE CCOZI , PERCENT BY VOL.
NITRIC OXIDE INOI , PPHV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
> HYDROCARBONS IHC AS CHJ.I
CARBON MONOXIDE ICOI
TOTAL OXIDES OF NITROGEN INOX »S NOZI
EMISSION R*TE, LB. POLLUT»*T/«R.
HYDROCARBONS IHC AS CHI»I
t TOTAL OXIDES OF NITROGEN INOX AS NOZI
ENGINE WORK OUTPUT, M£AS. SHP _
ENGINE WORK OUTPUT, ISENTROPIC AIR HP
1 ENGINE MORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT IEHISSIONSI
F/A IEHISSIONSI
56 57 58
0.00 79.36 198.91
1,1660.00 1,11,90.00 <«1170.00
40.0
62.1.6
371.00
0.00
0.00
-0.00
1,76.0
117.000
21,2.211 2
16.600
1.306
11.000
10.003
36.228
l,.078
1.1. ".0
1587
0.10
0.00
0.00
98.27
.116
5.85
1,0.0
61.77
376.00
0.00
0.00
-0.00
588.0
72.001
7S.861
21.. 000
1.731,
15.000
%.671
31.312
.031
!?97
oloo
98^85

<>0.0
60.29
385.00
0.00
0.00
-0.10
8Z6.0
9.900
197.232
1,1.311
2.661
35.800
11..766
5.179
3!&6Z
l!z61
oloo
187.51.
99.62

59
0.10
1,1070.00
260.00
6.96
1.0.1
55.3<>
31.3.00
2.20
5*. 11
362.00
926.8
19.510
306.306
1.5.501
3.165
39.510
.701
19.ZZ7
1..6S1
.182
i.'zzo
0.10
99.\9
.015
61
1.5.31 )
1,0990.11
Z66.ll
6. SI )
57.05 " 	 "
31.6.01 • )
1-9Z 	 ._..
55.97
36%. It )
12.300 )
285.169
1.6.501 .
3.15% )
17l?83 	 	 _ . .. 	
1..817
.111 . . .. ....... .. .. 	 	 -»
1..783
1.281 , )
212.36
Z55.ll . )
99.5%^ 	 	 _ 	 	
.015 . '

-------
VQ
 (D
 CO
P . •


ENGINE* GTCP85-98CK S/S* 36179 COMB P/N* 698168-3 TEST DATE 6-14-75 FUEL*AV. HERO. P BARO« 28.7%
RAT SHP= 200. RA EGT.F- 1150. RAT SPD* 41600.
) FUEL H7C* 1.9280 STOI F/A* .86822 L H V 18470.
DATA POINT NUMBER 56 57 58
PERCENT MAX. CORRECTED POHER 8.0 39.7 99.5
CORRECTED SHAFT HP 8.0 79.4 198.9
MEASURED SHAFT HP 0.0 74.8 187.5
EXHAUST GAS TEMP., OEG.F 476.0 588.0 826.0
SHAFT SPEED, Nl, RPH 41660.0 41490.0 41170.0
COMPRESSOR OSCHG. PRES..PSIA 62.5 61.8 60.3
COMPRESSOR OSCHG. TEMP.DEG F 371.0 376.0 385.0
, EXHAUST GAS PRESS., PSIA 13.69 13.75 13.87
CORRECTED BwEEO FLOM, LB/SEC 0.000 0.000 0.000
COMPRESSOR HAP FLOH.LB/SEC 6.07 5.70 5.18
FA RATIO BASED ON MAP FLOH .0056 .0087 .0133
CORRECTED FUEL FLOM , LB/HR 144.0 178.0 248.0
FA RATIO CALC. FROM EMISSION .0061, .0085 .0128
EQUIVALENCE RATIO .094 .124 .187
LOA3ING N/P»»N/V/E(T/S40) .377 .357 .333
OEM PT,F=
S LN T.F'
59
0.0
0.0
0.8
926.8
41078.0
55.3
343.0
13.84
2.248
6.77
.0158
260.0
.0152
.222
.369
1 COMB EFFIC FROM EMISSIONS 98.270 98.854 99.615 99.486
CARBON DIOXIDE
) PERCENT BY VOLUME, MET 1.31 1.73 2,66
LB. C02 PER LB. OF FUEL 3.87 3.09 3.13
HEIGHT FLOM, LB./HR. 442.0 550.4 776.2
) CARBON MONOXIDE
PPM BY VOLUME, MET 242.2 275.9 197.2
LB. PER 1000 LB. OF FUEL 36.228 31.312 14.766
HEIGHT FLOM, LB./HR. 5.217 5.574 3.662
UNBURNEO HYDROCARBONS- PPM AS CARBON, HEIGHTS AS CH4
PPM BY VOLUME, MET 117.8 72.8 9.9
! ) 13. PER 1000 LB. OF FUEL 10.013 4.671 .424
HEIGHT FLOH, LB./HR. 1.440 .831 .105
RATIO LB HC/LB CO .2761 .1492 .0287
) NITRIC OXIDE INOi - HEIGHTS AS N02
PPM BY VOLUME, MET 11.0 15.0 35.8
LB. PER 1000 LB. OF FUEL 2.703 2.797 4.403
) HEIGHT FLOH, LB./HR. .389 .498 1.992
NITROGEN DIOXIDE IN02*
PPM BY VOLUME, NET 5.6 9.8 5.5
) LB. PER 1000 LB. OF FUEL 1.376 1.678 .676
HEIGHT FLOH, LB./HR. .198 .299 .168
TOTAL OXIDES OF NITROGEN 
-------
                        ENGINE* GTCP85-98CK
                      OAT« POINT NUMBER
                      EMISSION RATE LB/HR
                          CARBON MONOXIDE
                          UNBURNED HYDROCARBONS
                          OXIDES OF NITROCEN
                          NITRIC OXIDE
                      POKER LEVEL HP
                      TOTAL CORRECTED HORSEPOWER
                                                  S/H=
36174
    56

 5.217
 1.440
  .587
  .319
 0.00
 0.00
••••  AIRESEARCH EMISSION  TEST  SUMMARY
 COM8 P/N= 694168-3 TEST DATE   6-14-75
     57        51        59        68
FUELzAV. KERO.
                  P BARO* 28.74
                      BRAKE SPECIFIC EMISSION INDEX  LB/1000HP-HR
                          CARBON MONOXIDE               0.000
                          UNBURNEO HYDROCARBONS         0.000
                          OXIDES OF NITROGEN            0.000
                          NITRIC OXIDE                  0.000
                          NOTE>*0. APPEARING IN  BRAKE  SPECIFIC EMISSION INDEX COLUMN DENOTES
5.574
.831
.797
• 49S
74.82
79.36
1
74.494
11.113
10.646
6.654
3.662
.105
1.260
1.092
187.54
198.91
19.527
.560
6.717
5.822
4.999
.182
1.220
1.059
241.57
246.84
20.694
.753
5.049
4.363
4.783
.118
1.281
1.116
255.08
262.38
18.752
.462
5.023
4.375
*
-------
 ENGINE. MFR.I  AIRESEARCH
MODEL NO.I  GTCPS5-9CK
FUEL I ASTM  01655-73
 TEST FACILITY! PHX LACCZ        INSIR. DESCRIP. I
 S/Nl  36179           ENGINE  TYPE (CLASS)! APU
MAX SHP       ZOO. »  BLEED  AIR EXTRACTION TO
    ATONIC H/C RATIO'    1.928    LHtfl     181,70.
  FEDERAL REG.V38 N136    CALC.
             CALC.  I.O.I      1
1150. DEC. f ECT
 8TU/L8.     ADDITIVES! NONE
                                                                                                                 DATE I  6-18-75
            EXHAUST EMISSIONS PER EPA RATED  MORK OUTPUT •« CODE OF FEDERAL REGULATIONS TITLE  ".0 PART 17
           ,..........,....,..,..,„..,...  ^MISSIONS COMPUTED FROM TEST CONDITION NO.  5    ••»•»»»•••••••
                    HYDROCARBONS  IHC AS  CHit)              .329  LB. POLLUTANT PER 1000 HP.-HR.
                    CARBON MONOXIDE (C01                16.783  LB. POLLUTANT PER 1000 HP.-HR.
                    OXIDES OF NITROGEN  (NOX  AS NOZI     5,38$  LB. POLLUTANT PER 1000 HP.-HR.
                                                                                                             17 JULY 1973
 [[[  tNSINE DESCRIPTION  »»»»»»»•»»»»»»»»
 COMBUSTOR TYPE! TANGENTIAL CAN           P/NI   693166-3  SURFACE/VOLUME!  .725 SQ  IN/CJ  IN
 ENGINE  TOTAL SERVICE!     0.0  HR.    TIME  SINCE ENGINE OVERHAULI       0.0 HR.
 ENGINE  ASSEMBLY AND MAINTENANCE INFORMATION!
 AIRCRAFT INSTALLATION »»» MFR.I
                                                              MODEL NO.I
                                                                 FUEL INJ. TYPEI
                                                                                                      USER I
                                                                                     DUAL ORIFICE
 ..,........>........,...,........,•»»»»»»»*»»»•«»0pER»TjONAL IEST D4TA SUMMARY •••••»••»•••••»•»»••»•••••••••••••»»•••»••»•••••
 GASEOUS  EMISSION TEST 140.1     5     3ATEI   6-10-75      TIMEI    10 30      SARD. PRESS.!   28.660 IN. H6A.
 AM3IENT  AIR TEMP.! 59.0  DEG. F         RE.ATIVE  HUMIDITY!  20.00 PERCENT       SPECIFIC  HUMIDITY!  .002000 LB. HZO/LB. DRY  AIR
 AMBIENT  AIR QUALITY    HYDROCARBONS  (HC)!  0.0    PPMC    CARSON HONOXIO£ (CO)I 0.0   PPMV    OXIDES OF NITROGEN (NOX)I 0.0    PPHV
 SAMPLE LINE **• TEMP.!  300.00 DEG.  F.      FLONRATEI   Hi.16 LlTERS/MIN.     TRANSPORT TIME!    6.50 SEC.     LENGTH!    SO.00 FT.
                                                       COMPUTED EMISSIONS
 TEST  CONDITION                                           61        62        63        6".         65
 POKER SETTING, CORRECTED HP.                           0.00     79.05    198.01      0.00      1.5.79
 Nl  SPEED,  RPH                                      1(1700.00  ".IBiO.OO  ".1220.00  1)1090.00  1.1090. 00 _
 FUEL  FLCH  IMEAS.) LB./HR.                            130.00    167.00    230.00    Z53.00     258.01
 ENGINE CORE  INLET AIRFLCH(CALC.I LB./SEC.              5.90      5.66      5.36      6.67       6.57
 COMPRESSOR INLET TEMP., DEG. F                         61.0      60.1      60.0      58.1 ..     61.•
 COMPRESSOR DISCHARGE AIR PRESSURE, PSIA               60.15     59.1.1     59.61     52.78      5<>.6      1.367
ENGINc.  NORK  OUTPUT, MEAS. SHP                          0.00     75.85    189.98      0.00      1.3.9.8
ENGINE  MORK  OUTPUT, ISENTROPIC AIR HP                  0.00      0.00      0.00    238.96     209.86
ENGINE  WORK  OUTPUT, TOTAL HP                           0.00     75.85    189.98    238.96     253'.6%
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)            98.37     98.91     99.1.6     99.39      99.58
F/A (EMISSIONS*                                         .006      .008      .012      .015       .(15
-------
 0)
U3
 (D
\

oar GTCP85-9CK S/NS 36179 COMB P/N= 6961 61



I
'

i

)


)



)

)

)
DATA POINT NUMBER
PERCENT MAX. CORRECTED POWER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR OSCHG. PRES..PSIA
COMPRESSOR OSCHG. TEMP.OEG F
EXHAUST GAS PRESS.. PSIA
CORRECTED BLtED FLOW, LB/SEC
COMPRESSOR MAP FLOW.LB/SEC
FA RATIO BASEO ON MAP FLOW
CORRECTED FUEL FLOW , LB/MR
FA RATIO CAi.C. FROM EMISSION
EQUIVALENCE RATIO
LOADING W/P»«N/V/E«T/540I

CARBON DIOXIDE
PERCENT BY VOLUME, WET
LB. C02 PER LB. OF FUEL
WEIGHT FLOW, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, WET
LB. PER 1000 LB. OF FUEL
WEIGHT FLOW, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS

LB. PER 1000 LB. OF FUEL
WEIGHT FLOW, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NO) - WEIGHTS AS
PPM BY VOLUME. WET
LB. PER 1000 LB. OF FUEL
WEIGHT FLOW, LB./HR.
NITROGEN DIOXIDE (N02I
PPM BY VOLUME, NET
L8. PER 1000 LB. OF FUEL
61
0.0
0.0
1.0
480.0
41709.0
60.1
401.0
13.66
0.000
6.11
.0060
130.0
.0061
.090
.377

1.25
3.07
399.6
222.8
35.003
k n T
62
39.5
79.1
75.8
593.0
41520.1
59.4
412.0
13.70
0.001
5.67
.0082
167.0
.0092
.120
.363

1.68
3.10
516.9
254.6
29.831
4.550 4.982
CARBON, WEIGHTS AS

1U£. 0
9.160
1 . 191
N02
8.5
2.194
.285
_ —
2.194
WEIGHT FLOW, LB./HR. .285
)

; )
•

j

.)
i
-V.HI. vn&wc.d ur raiiKuutN INU*flU£l «5 NUZ
PPM BY VOLUME, WET 17.0
L3. PER 1000 LB. OF FUEL
SMOKE MEASUREMENT DATA
CORRECTED WEIGHT FLOW
SMOKE NUMBER
CORRECTED WEIGHT FLOW
SMOKE NUMBER
CORRECTED WEIGHT FLOW
SMOKE NUMBER
CORRECTIO WEIGHT FLOW
SMOKE NUMBER
4.387

.00702
7.20
.02107
10.40
.03505
16.90
.04907
21.70
SMOKE NUMBER AT HAcO.023 14.30
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE
2. EQUIVALENCE RATIO CALCULATED FROM
3. MASS EMISSIONS OF NO, N02. Al*3 NO*
4.COMBUSTION EFFICIENCY CALCULATED F

66. 0
.738
.14»2
16.1
3.079
.514
n m
1.732
.2(9
25.1
4.812
• 80**
.01700
15.70
.02099
31.30
.03492
41.00
.04889
47.11


-3 TEST DATE 6-10-75 FUEL=AV. KERO. P BARO* 28.68
= lOHru. 5 LN T,F= 300.0 FLO,L/M= 14.160 SL TIM S» 6 5101
t» -i »,. 	
°* O4
99.1 o.o
198 .0 An

812.1
41220.0
59.6
412.0
13.83
0.000
5.32
.0120
230.0
.0119
.175
.332

2.48
3.12
717.8
247.1
19.812
4.557
CH4

18.0
.825
.190
.0416
36.5
4.806
1.105

.751

42.2
5.557
1.278
.00698
16.30
.02094
32.50
.03484
39.80
.04077
46.40
34.21 34.20
WET VALUES.
w. u
.
52!
366.
13.81
2.200
6. 62
.0156
253.0
.0154
.226
.379
99.391
OF R£OUC£D
3.21
3.12
788. 2
377.0
23.310
5.897

19.5
.689
.174
. 0296
42.0
4.266
1.179

6.5
.660
.167
48.5
4.926
1.246
.00698
26.59
.02094
45.89
.03482
59* 08
.14871
64.51
49.50
O9
22.
45.
44.
970.
41090.
54.4
375.0
13.82
1.914
.0154
258.0 	
.0151
.222
.366
99.583
3. 16
3.13
606.8 	 -
262
16 512
4.260

9.0 	 -
!084
.8196 — _ - . . 	 	 .__ ..
43.6

4.532 -.---. . . -
1.169
	 . 	 .. _ 	 	 	
. 766
.198
51.2

1.367 	
.00714
18.10
.02113
33.70
**•*• 	 — - - . _ ... _ . 	 	 _
* - -
.04929 	
51.61 ~ "" "" 	 "" "~ " ~ 	
36.61
C02,CO,AND MC DATA AND FUEL COMPOSITION. r " " * ~
2™ rJLSifn*T£° *S NBZ ™OH CONCENTRATIONS WITH NOi.ECUL«R WEIGHT OF N02 (46.111.
ROM CO, AND UHC AS VAPORIZED oeicINAL ruft ntt \ a/ i u run oicr*
-------
                                                 S/N=
                                                      S6179
                                                          61

                                                       I..550
                                                       1.191
                                                        .570
                                                        .285
                                                       0.00
                                                       0.00
•••  AIRESEARCH EMISSION TEST SUMMARY
COM3 P/N= 696166-3 TEST O.ATt  6-10-75
    62
              63
                        6«,
                                  65
  ENGINE* GTCP65-9CK
DATA POINT NUMBER
EMISSION RATE LB/HR
    CARBON MONOXIDE
    UNBURNEO HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIDE
PONER LEVEL HP
TOTAL CORRECTED HORSEPOWER
3RAKE SPECIFIC EMISSION INDEX L8/1000HP-HR
    CARBON MONOXIDE              0.000
    UNBURNEO HYDROCARBONS        0.000
    OXIDES OF NITROGEN           0.000
    NITRIC OXIDE                 0.000
    NOTE»»0. APPEARING IN BRAKE SPECIFIC EMISSION INDEX COLUMN  DENOTES  AN IDLE CONDITION
4.962
.738
.804
.514
75.85
79.05
65.681
9.732
10.594
6.760
4.557
.190
1.278
1.105
189.96
198.01
23.984
.996
6.727
5.619
5.897
.174
1.246
1.079
236.96
249.05
24.660
.730
5.216
4.517
4.260
.084
1.367
1.169
253.84
265.14
16. 763
.329
5.385
4. 607
                                            FUEL=AV.  KERO.
                                                              P BARO=  26.66
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                    '    ENGINE MFR.I AIRESEARCH
                       NOOEL NO.I  GTCP85-98CK

                   )   FUEL! ASTM 01655-73
                                TEST FACILITYl PHX LACC2       INSTR. OESCRIP.I   FLOcRAL  REG V38 N136   CALC. OATEI  6-11-75
                                S/NI   36179         ENGINE TYPE (CLASS)I  APU               CALC. I.D.I      2
                              HAX  SHP       200.  * BLEED AIR EXTRACTION TO    nso. OEG.  F  EGT
                                   ATOMIC H/C RATIOI    1.928    LHVi     18*70. BTU/VB.      ADDITIVESI NONE
                                  EXHAUST EMISSIONS PER EPA  RATED  NOR<  OUTPUT  "  CODE OF FEDERAL REGULATIONS TITLE  *0  PART  87
                                 ..............I...............  £MISSIONS  COMPUTED FROM TEST CONDITION NO.  5   ..............
                                          HYDROCARBONS (HC AS  CH,)              .308  LB. POLLUTANT PER 1000 HP.-HR.
                                          CARBON MONOXIDE  (CO)               16.19-.  LB. POLLUTANT PER 1000 HP.-HR.
                                          OXIDES OF NITROGEN (NOX  AS  N02)      S.*13  LB. POLLUTANT PER 1000 HP.-HR.
                                                                                                            17 JULY 1973

[[[   £N6IN£ DESCRIPTION  •»»»•»•»»»...»..
COM3USTOR TYPEI TANGENTIAL CAN           P/NI   698168-3  SURFACE/VOLUME I  .725 SQ IN/CU  IN
ENGINE TOTAL SERVICE!     0.0  HR.    TIME  SINCE  ENGINc OVERHAULI      0.0 HR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                       AIRCRAFT INSTALLATION ••• NFR.I
                                                                                    NOOEL NO. I
                                                                                                                     FUEL  INJ.  TTPEI
                                                                                                                            USER!
                                                                                                                                          DUAL ORIFICE
                                                                                                                                               ORIFICE
                       GASEOUS EMISSION TEST NO. 1     5
                       AMBIENT AIR TcMP.I 59. 0  DEG. F
                       AMBIENT AIR QUALITY    HYOROC4R30NS  CHC) »  0 . 0    PPMC
                   )   SAMPLE LINE «• TEMP.I  300.00 OEG. F.      FLOHRATE.
                                     ...... ""..OPERATIONAL TEST DATA SUMMARY »'»»»»»»»»»**»•»»»..•»..»...»..»»..»....».»».»..
                                     OATEI   6-11-75       TIMEI   09.25       BARO. PRESS.I  28.760  IN.  HGA.
                                        RE-ATIVE  HUMIDITYI   20.00 PERCENT       SPECIFIC  HUMIOITYI   .002000  LB.  H20/LB. OR» AIR
                                                         CARBON MONOXIDE (CO)I 0.0   PPMV     OXIDES OF  NITROGEN (NOX)t 0.0   PPNV
                                                        1*.16 .ITERS/MIN.     TRANSPORT TIMEI     6.50 SEC.      LENGTH*   50.00 FT.



i



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TEST CONDITION
POHER SETTING, CORRECTED HP.
Nl SPEED, RPM
FUEL FLOW (MEAS.) LB./HR.
ENGINE CORE INLET AIRFLOW (CALC. ) LB./SEC.
COMPRESSOR INLET TEMP., OEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR T£MP., OEG. F
COMPR£SSOR BLEED AIRFLON (MEAS.) LB./SEC.
BLEED AIR PRESSURE, PSIA
BLEED AIR TEMPERATURE, OEG. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION, MET ANALYSIS
HYDROCARBON (HC AS CH*I , PPMC
CARBON MONOXIDE (CO) , PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPNV
CARBON DIOXIDE (C02), PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV,
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH*)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH*)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
ENGINE WORK OUTPUT, MEAS. SHP
ENGINE WORK OUTPUT, ISENTROPIC AIR MP
ENGINE MORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/« (EMISSIONS)
66 67 68
0.00
1.1640.00
130.00
5.81
61.0
60.6*
1.01.00
0.00
0.00
-0.00
*80.0

97.500
222.787
16.500
1.265
•10.000

8.622
3*.*68
*.193

1.121
fc.*81
.5*5
0.01
0.00
0.00
98. *3
.116
78.53
1.1510.00
168.00
5.76
61.0
59. *1
1.03.00
0.00
0.00
-0.00
596.0

66.000
257.093
2*. 000
1.66*
1*.SOO

*.*65
30.*28
V.666

.751
5.112
.78*
75.63
0.00
75.63
91.19
.018
197.22
*1210.00
230.00
5.3*
61.0
59.66
*1*.00
0.00
0.00
-0.00
815.0

18.001
2*9.616
*2.000
2.*88
3*. 500

.821
19.926
5.507

.189
I..5B3
1.267
189.9*
0.11
189.9*
99.lt6
.112
69
0.00
1.1110.00
252.00
6.66
60.0
52.78
368.00
2.12
51.55
392.00
968.0

21.110
366.000
*B.tia
3.217
*0.500

.7*2
23.839
*.87*

.187
6.013
1.228
1. 01
239. *8
239.*!
99.37
.115
70
*5.9*
*1070.00
257.01
6.57
61.0
5*. 50
375.00
1.83
53.1.2
396.01
968.0

a.*oo
252.100
51.300
3.1*8
**.*00

.30*
15.9*5
5.331

-------
                                                                                                                                                                    5?
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     ENGINE- GTCP85-98CK       S/N-   36179
    RAT SHP*   ZOO.     RA EGT.F-  1150.
1   FUEL H/C= 1.9280     STOI  F/A=  .86822

   DATA POINT  NUMBER                    66
   PERCENT  MAX.  CORRECTED POHER       0.0
   CORRECTED SHAFT HP                  0.0
   MEASURED SHAFT HP                   0.0
1   EXHAUST  GAS TEMP.,  OEG.F          480.0
   SHAFT  SPEED,  Nl, RPH           41680.0
   COMPRESSOR  OSCHG. PRES.,PSIA      60.6
   COMPRESSOR  OSCHG. TcHP.DEG F     401.0
   EXHAUST  GAS PRESS., PSIA          13.70
   CORRECTED BLEED FLOH,  LB/SEC     0.000
   COMPRESSOR  MAP FLOH.L3/SEC        6.07
   FA RATIO BASED ON HAP  FLOH       .0059
   CORRECTED FUEL FLOH ,  LB/HR      130.0
   FA RATIO CALC. FROM EMISSION     .0062
   EQUIVALENCE RATIO                  .891
   LOADING  H/P»»N/V/EtT/54fl»         .375
   COMB EFFIC  FROM EMISSIONS       98.433
'•»»»  AIRESEARCH EMISSION TEST SUMMARY
  COMB P/N- 698168-3 TiST DATE  6-11-75
 RAT SPO* 41600.    OEM PT,F>  19.
   L H V- 18470.    S LN T,F> 300.0
                                                                                                              FUEL'AV. KERO.    P BARO» 28.76
                                                                                                         REL HUN=  20.00    SPEC HUM*  .002080
                                                                                                         FLO.L/M"  lit. 160   SL  TIH,S«  6.5000
                                                                      67
                                                                    39.3
                                                                    78.5
                                                                    75.6
                                                                   596.0
                                                                 41510.0
                                                                    59.4
                                                                   403.0

                                                                   0.000
                                                                    5.65
                                                                   .0083
                                                                   168.0
                                                                   .0081
                                                                    .119
                                                                    .361
                                                                  98.893
                68
              98.6
             197.2
             189.9
             815.0
           41210.0
              59.7
             414.0
             13.88
             0.000
              5.32
             .0130
             330.0
             .0130
              .176
              .331
            99.459
     69
    0.
    0.
    0.
  968.
41110.
   52.
  368.
  13.85
  2.203
   6.64
  .0155
  252.0
  .0154
   .Z26
   .379
 99.374
   23.0
   45.9
   44.2
  968.1
41870.1
   54.5
  375.0
  13.86
  1.905
   6.49
  .0153
  257.0
  .0151
   .221
   .365
 99.598
                                                                                                                                             I J

                                                                                                                                              >
                                                                                                                                              '


                                                                                                                                              )


                                                                                                                                              )


                                                                                                                                              )
                                                                         •SUMMARY OF REDUCED EMISSION DATA*
CARBCN DIOXIDE
    PERCENT  BY  VOLUME,  MET         1.Z7      1.66
    L3. C02  PER LB.  OF  FUEL        3.98      3.09
    HEIGHT FLOH,  LB./HR.          399.9     519.8
CARBON MONOXIDE
    PPM BY VOLUME, NET            Z22.S     257.1
    LB. PER  1000  LB.  OF FUEL     34.468    50.1(28
    HEIGHT FLOW,  LB./HR.          4.1.81     5.112
                                                          Z.l>9
                                                          3.1Z
                                                         717.7

                                                         31.9.6
                                                        19.926
                                                         4.563
                        3.21
                        3.11
                       784.9

                       386.0
                      23.859
                       6.013
             3.15
             3.13
            8*3.9

            252.1
           15.945
            4.098
UNBURNED HYDROCARBONS- PPM  AS  CARBON, HEIGHTS AS CH4                       .  	
    PPM BY  VOLUME, HET             97.5      66.0      18.0      21.0       8.4
    L3. PER 1000 LB. OF FUEL      8.622     4.465      .821      .742       .304                                                               3
    HEIGHT  FtOH, LB./HR.          1.121      .750      .189      .187       .078	,.	;    ;
    RATIO LB  HC/LB CO             .2501     .1467     .0412     .0311     .0190
NITRIC OXIOE  (NO) - HEIGHTS AS N02                                                    -                                                       ):
    PPM BY  VOLUME, HET             10.0      14.5      34.5      40.5       44.4    _   	     „.		  ..	  .     >
    L3. PER 1000 LB. OF FUEL      2.541     Z.819     4.534     4.11Z     4.613                                                                 :
    HEIGHT  FLOH, LB./HR.           .330      .474     1.041     1.036     1.186                                                               J;
NITROGEN DIOXIDE (NOZ)	_.    :
    PPM BY  VOLUME, HET              6.5       9.5       7.5       7.5       6.9                                                                 :
    LB. PER 1000 LB. OF FUEL      1.652     1.847      .983      .762       .717                                                               )-
    HEIGHT  FLOH, LB./HR.         .  .215  ....  .310      .Z.Z6    .  .19Z	.184__  ___	;    :
TOTAL OXIDES  OF NITROGEN  (NO*N02I  AS N02     '                                                                                                  ;
    PPM BY  VOLUME, HET             16.5      24.0      42.0      48.1       51.3                                                               ) ••
    L3. PER 1000 LB. OF FUEL      4.193     4.666     5.507     4.674. ... $.331	.	    ;
    HEIGHT  FLOH, LB./HR.           .545      .784     1.267     1.238     1.370
    SMCKE MEASUREMENT DATA                                                                                                                    )
    CORRECTED HEIGHT FLOH        .00702    .00699    .00698    .00696    .00695      _    	 	  .	             ......
    SMOKE NUMBER                   9.60     18.10     15.10     30.10     16.90
    CORRECTED HEIGHT FLOH        .02106    .02094    .02094    .02088    .02065                                                               )
    SMOKE NUMBER                  16.90     3Z.50     31.30     50.60     34.90  _	    .;	  .  	 	 .'   .  .._•  	   ,.
    CORRECTED HEIGHT FLOH        .03503    .03484    .03482    .03472    .03473
    SMOKE NUMBER                  22.30     42.80     41.00     60.20     43.40                                                             ,)
    CORRECTED HEIGHT FLOH        .04895    .04877    .04866    .04850    .04854               _     	          ..   _	     __  »
    SMOKE NUMBER                  25.90     49.40     45.60     65.10     56.30
    SMOKE NUMBER AT HA=0.023      18.90     36.20     33.80     52.10     37.60                                                               )
NOTES 1. ALL  EMISSIONS CONCENTRATIONS ARE HET VALUES.                                        __             	 ._.,	 .
      Z.EQUIVALENCE RATIO CALCULATED FROM COZ.CO.ANO HC DATA AND FUEL COMPOSITION.                                                         ,
      3.MASS  EMISSIONS OF NO,  NOZ, AND NO+NOZ CALCULATED AS N02 FRON CONCENTRATIONS HITH MOLECULAR HEIGHT OF NOZ  146.611.                    J
      4.COMBUSTION EFFICIENCY  CALCULATED FROM CO,AND JHC AS VAPORIZED ORIGINAL FUEL ON LB/ LB FUEL BASIS.          _           _   	
-------
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  ENGINE* GTCP85-98CK
DATA POINT NUMBER
EMISSION RATE IB/HR
    CARBON MONOXIDE
    UNBURNEO HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIDE
POHER LEVEL HP
TOTAL CORRECTED HORSEPOWER
                                               S/N=
36179
   66

4.481
1.121
 .545
 .330
0.00
0.00
*•»»  AIK£SEARCM EMISSION TEST SUMMARY
 COMB P/N* 698165-3 TEST DATE  6-11-75
                                                                   67
                                                                                       69
                                                                                                 7»
5.112
.751
.784
.474
75.63
78.53
[
67.5*8
9.917
10.364
6.262
4.583
.189
1.267
1.041
189.94
197.22
24.129
.995
6.669
5.478
6.013
.187
1.228
1.036
239.48
249.38
25.107
.781
5.128
4.327
4.098
.078
1.378
1.186
253.05
263.58
16.194
.301
5.413
4.685
                                                                                                           FUEL*AY. KERO.
                                                                                                                             P BARO< 28.76
 •>
h
                    BRAKE SPECIFIC EMISSION INDEX L3/1000HP-HR
                        CARBON MONOXIDE              O.BOO
                        UNBURNED HYDROCARBONS        0.000
                        OXIDES OF NITROGEN           0.010
                        NITRIC OXIOE                 0.000
                        NOTE"0. APPEARING IN BRAKE SPECIFIC EMISSION INDEX COLUMN DENOTES  AN^IOLE CONDITION
-------
                       ENGINE MFD.I AIRESEARCH
                      MODEL NO.I  GTCP8S-98CK
                      FUELI ASTH 01655-73
 TEST FACILITY! PHX LACCZ        INSTR.  DESCRIP.I   FEDERAL REG. V38 N136   CALC.
 S/Nt  36179          ENGINE  TYPE  (CLASS)I   APU               CALC. I.O.I     3
MAX SHP       ZOO. » BLEED  AIR EXTRACTION TO    1151. OEG. F ECT
    ATOMIC H/C RATIOS    1.9Z8   LHVI     18470.  BTU/LB.      ADDITIVES! NONE
                                                                                                                                     DATEI  6-11-75
                                 EXHAUST EMISSIONS  PER  EPA RATED HORK OUTPUT •» CODE OF FEDERAL REGULATIONS TITLE  -.0  PART  87
                                 .............................. EMISSIONS COMPUTED FROM TEST CONDITION NO.  5    ...»«»»»».»...
                                         HYDROCARBONS  (HC AS CH4)             .214  LB. POLLUTANT PER 1000 HP.-HR.
                                         CARBON  MONOXIDE (COI               14.827  uB. POLLUTANT PER 1000 HP.-HR.
                                         .OXIDES  OF  NITROGEN (NOX AS NO2)     5.491  LB. POLLUTANT PER 1000 HP.-HR.
                                                                                                                                  17 JULY  1973
                      [[[  ENGINE JESCRIPTION  •••••»•••••••»»•»•••«•••••••»•••••
                      COM3USTOR  TYPEI  TANGENTIAL  CAN           P/NJ  698168-3  SURFACE/VOLUME I  .725 SO.  IN/CJ  IN     FUEL INJ.  TYPE«
                      ENGINE  TOTAL  SERVICE*       0.0  HR.    TIME SINCE ENGINE OVERHAULI      0.0 HR.
                      ENGINE  ASSEMBLY  AND  MAINTENANCE INFORMATIONI
                                                                                    DUAL  ORIFICE
                       AIRCRAFT  INSTALLATION  **•  HFR.I
                                                                                   MODEL NO.I
                                                                                                                           USERI
                      ................................................OPERATIONAL TEST DATA SUMMARY •»»»»»»*»•»»»».»»»»*»•••»••*•••»»»•»•»»••»»••»••
                      GASEOUS  EMISSION TEST  NO. I      5     OAT£1  6-11-75      TIME«    10.15      8ARO.  PRESS.!   28.760 IN. HGA.
                      AMBIENT  AIR  TEMP.I  59.0   0-G.  F        R£^ATIKE HUMIDITY!  ZO.OO PERCENT        SPECIFIC  HUMIDITY!  .002000  L8. H20/LB. DRV AIR
                      AMBIENT  AIR  QUALITY   HYDROCARBONS (HC)I 0.0   PPMC    CARBON MONOXIDE  (CO)I 0.0    P?MV    OXIDES OF NITROGEN (NOX)t 0.1   PPM*
                      SAMPLE LINE  •••  TEMF.I  300.00 OEG. F.     FLOHRATE!   14.16 LITERS/NIN.     TRANSPORT  TIMEI    6.50 SEC.     LENGTH!   50.01 FT.
 0)
iQ
 0)
TEST CONDITION
POWER SETTING, CORRECTED HP.
Nl SPEED, RPM
FUE'. FLOH (HEAS.) LB./HR.
ENGINE CORE INLET AIRFLCM (CALC.) LB./SEC.
COMPRESSOR INLET TEMP., DEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COHPRESSOR DISCHARGE AIR TEMP., OEG. F
COHPRESSOR BLcED A IRF '• OH 1 ME AS « ) uB«/SEC«
BLEED AIR PRESSURE. PSIA
BLEED AIR TEMPERATURE, OEG. F
ENGINE EXHAUST GAS TEMP., DEG. F
EMISSION CONCENTRATION, WET ANALYSIS
HYDROCARBON (HC AS CH4I , PPHC
CARBON MONOXIDE (CO) * PPMV
TCTAL OXIDES OF NITROGEN (NOX), PPMV
CARBON DIOXIDE (COZ) , PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSION INDEX, 1.3. POi.LUTANT/1000 L3. FUEL
HYDROCARBONS (HC AS CH4I
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN INOX AS NOZ>
EMISSION RATE, L3. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN INOX AS NOZ)
ENGINE WORK OUTPUT, MEAS. SHP
ENGINE DORK OUTPUT, ISENTROPIC AIR HP
ENGINE MORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY* PERCENT (EMISSIONS)
F/A (EMISSIONS)
71 72 73
0.00
41660.00
130.00
6.00
60.0
60.39
399.00
0.00
0.00
-0.00
480.0

97.500
217.999
16.400
1.ZZ5
8.500

8.903
34.827
4.304

1.157
4.5Z7
.559
0.00
0.00
0.00
98.40
.006
78.87
41500.00
167.00
5.73
59.0
59.66
401.00
0.00
' 0.00
-0.00
595.0

63.000
247.140
24.300
1.664
14.700

4.Z65
Z9.Z72
v.728

.712
4.689
.790
75.81
0.00
75.81
98.9*
.008
197. 1Z
41190.00
230.00
5.35
61.0
59.41
,16.00
0.00
0.00
-0.00
8ZZ.1

16.500
192.111
42.500
Z.488
34.500

.755
15.372
5.586

• 174
3.536
1.265
189.85
0.00
189.45
99.57
.012
74
1.00
41090.00
Z53.01
6.59
60.0
52.51.
372.00
2.09
51.16
395.00
986.0

9.600
249.616
52.501
3.267
46.100

.335
15.Z18
5.258

.085
3.850
1.330
1.11
239.07
Z39.07
99.61
.016
75
45.69
41030.00
261.01
6.45
59.1 	 	 .._ 	
54.26
376.01
1.82
53.13
397.00
986.1 	 . ...._. 	 ..._ _

6.000
237.311 . . ...
53.501
3.267
47.500

.219
14.475
5.361

.054
3.763
1.394
43.91 -
209.91
253.82
99.64 	 	 	 . .
.016
-------
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ENGINE2 GTCP85-98CK S/N= 36179
RAT SHP— 200. RA EGT»Fa
FUEL H/C« 1.9280 STOI F/A*
DATA POINT NUHBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OEG.F
SHAFT SPEED, HI, RPM
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR DSCHG. TEMP, BEG F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOH, LB/SEC
COMPRESSOR HAP FLOH.LB/SEC
FA RATIO BASED ON MAP FLOH
CORRECTED FUEL FLOH , L8/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P**N/V/EIT/540)
COM3 EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
La. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNED HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
LB. PER 1800 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE INO) - HEIGHTS AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH. LB./HR.
NITROGEN DIOXIDE (NO2)
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
TOTAL OXIDES OF NITROGEN INO+N
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
S1CKE MEASUREMENT DATA
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMCKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
SMOKE NUHBER AT HA=fl.D23
1190.
.06822
71
o.o
0.0
0.0
480.0
41660.0
60.4
399.0
13.70
0.000
6.02
.0060
130.0
.0068
.088
.376
98.400

1.Z2
3.07
399.7

218.0
34.827
4.527




COMB P/N= 698168-3 TEST DATE 5-11-75 FUEL=AV. KERO. P BARO« 28.76
RAT SPC
L H V
72
39.4
78.9
75.8
595.0
41500.0
59.7
401.0
13.74
0.000
5.53
.0084
167.0
.0081
.119
.352
98.937

1.66
3.10
517.1

247.1
29.272
4.889
CARBON, HEIGHTS AS
97.5
8.903
1.157
.2556
NOZ
8.5
2.231
.298

7.9
2.873
.270
>2I AS NOZ
16.4
4.304
.559

.00694
7.20
.02083
15.70
.03465
22.30
.04833
26.50
18.30
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE
63.0
4.265
.712
.1457

14.7
2.860
.478

9.6
1.868
.312

24.3
4.728
.798

.80693
16.90
.02079
31.90
.03459
41.60
.04833
50.00
35.70
* 41600.
* 18470.
73
98.6
197.1
189.8
822.0
41190.0
59.4
416.0
13.88
0.000
5.32
.0128
230.0
.0119
.175
.332
99.572

2.49
3.13
719.4

192.1
15.372
3.536
CH4
16.5
.755
.174
.0491

34.5
4.535
1.843

8.0
1.051
.242

42.5
5.586
1.285

.00693
16.98
.82079
32.58
.03463
43.40
.04840
47.00
35. SO
DEN PT,F=
S LN T,F*
74
0.0
0.0
0.8
966.0
41090.0
52.5
372.8
13.85
Z.179
6.57
.0157
253.0
.0156
.229
.375
19. REL HUM- 20.00 SPEC HUM* 002000
300.0 FLO.L/H* 14.160 SL TIM.S- 6. 5000
75 ~ 	
22.
45.
43. " 	 -- - - -
986.
41030.
54.3 " - - • - 	 	 	
376.0
13.86
1.895
6.47
.0155
268.0
.0156
.229
.366 	 ' 	 	
99.613 99.641

>

A
! )
• - 	 --
•»
-*

)'


i

• -
•»




	 	
1

3.27
3.13
791.7

249.6
15.218
3.850

9.6
.335
.085
.0220

46.1
4.617
1.168

6.4
.641
.162

52.5
5.258
1.330

.00695
21.78
.02085
37.30
.03476
47.00
.04855
50.60
39.71
3.27
3.13
614.0

237.3
14.475
3.763

6.0
.209
..•54
.0145

47.5 ... ......
4.759
1.237

6.0
.601
.156

53.5
5.360
1.394

.00694
26.58
.02082
31.36
.03467
42.20
.04854
50.68
36.71
HET VALUES.
>'

	 	 	 :



. -v


)'

•
% .
• •*

•k
*

-*

* •
^


^
'

1 J

• *
* >


:. 1

                         Z.EQUIVAL£NCE RATIO CALCULATED FROM COZ,CO,AND HC DATA AND FUEL COMPOSITION.
                         S.HtSS  EMISSIONS OF HO, HOi, tHO KO+H02 ULULATED AS HOI  FKOH COHCIH1MTIOMS *ITH HOLKULUt NEKMT Of MOt H6.HI.
                         i>.coinusiioH eFFiciewr ctLcuLtreo FKOH CO.MO we *s nmiZEo nuciMi. run. on t»v LB FUU> MSI*.
-------
                         ENSINE* STCPS5-98CK      S/N= 36179
                       DATA POINT NUMBER                    '1         72
                       EMISSION RATE LB/HR
                           CARBON MONOXIDE               "..527      U.889
                           UNBURNEO HYDROCARBONS         1.157       .712
                           OXICES OF NITROGEN             .559       .790
                           NITRIC OXIDE                   .290       .<<78
                       POMER LEVEL HP                    0.00      75.81
                       TOTAL CORRECTED HORSEPOWER        0.00      78.87
                       BRAKE SPECIFIC EMISSION INDEX LB/1000HP-HR
                           CARBON MONOXIDE               0.000     6*.*S*
                           UNBURNEO HYDROCARBONS         0.000      9.396
                           OXIDES OF NITROGEN            0.000     10. US
                           NITRIC OXIDE                  0.000      6.300
                                                                  COMB  P/N=  698164-3 TEST D»TE  6-11-75
                                                                                                              FUEL-Atf.  KERO.
                                                                                                                                 P BARO* 28.76
     73

  3.536
   .171.
  1.285
  1.01.3
189.65
197.12

 18.623
   .91<>
  6.768
  5.1.91.
     71.

  3.851
   .085
  1.330
  1.168
239.07
21.8.95
 16
    105
    35".
  5.56*
  I.. 866
                           NOTE>*0. APPEARING IN BRAKE SPECIFIC EMISSION INDEX COLUMN DENOTES
     75

  3.763
   .05*
  1.39*
  1.237
253.82
26*. 15
       ....         _
 1*.827
   .21*
  5.*91         _
  «..875
AN IDLE CONDITION
I )
(D

Ui
CO
-------
                        ~>    ENGINE MFR.l AIKESEARCH
                           MODEL NO.I  GTCP8S-98CK

                        '   FUELl »TSN 01655-73
 TEST FACILITY I PHX LACC2        INSTR.  OESCRIP.:   FEDERAL REG V38 N136
 S/NI  36179          ENGINE  TYPE  (CLASS)I   APU              CALC. I.D.I
MAX SHP       200. * BLEED AIR EXTRACTION  TO    nso. DEC. F EST
    ATONIC ri/C RATIOI   1.928    LHVI      18470.  BTU/LB.      AOOITIVESI NONE
                                                                                                          CALC.  OATEI
                                                                                                             1
                                                                                                                       6-11-75
                                      EXHAUST EMISSIONS  PER EPA ^ATEO NOR* OUTPUT '• CODE OF FEDERAL REGULATIONS  TITLE 40  PART 87
                                     .............................. £MISSIONS COMPUTED FROM TEST CONDITION  NO.  5   »«.»»»..»»«.••
                                              HYDROCARdONS  (HC AS CH<.)              .221  LB. POLLUTANT PER  1000 HP.-HR.
                                              CARBON  MONOXIDE ICOI               15.-.70  LB. POLLUTANT PER  1000 HP.-HR.
                                              OXIDES  OF  NITROGEN (NOX AS N02I     5.352  LB. POLLUTANT PER  1000 HP.-HR.

»••».....«.>..».....................................   EN6iNE DESCRIPTION  »•»»»»»»»»»»»».»
COHBUSTOR TYPEI TANGENTIAL CAN           P/NI   698168-3  SURFACE/VOLUMEI  .725 SQ IN/CJ  IN
ENGINE TOTAL SERVICEI      0.0 HR.    TINE  SINCE  ENGINE OVERHAUL I      0.0 HR.
ENGINE ASSEMBLY AND MAINTENANCE  INFORMATION!
                           AIRCRAFT INSTALLATION ••»  MFR.l
                                                                                        MODEL NO.I
                                                                                                                          FUEL INJ. TYPE!
                                                                                                                                USER!
                                                                                                                                              DUAL ORIFICE
 (U
va
 (D
 tn
                           ..»..»..»....,..,...,.»....,..,........,.....,,»0pERjTIONAL TEST OSTA sumiARY • •».»*.»...».„.».»...,..»....,,...»».„,..„.,».
                           GASEOUS EMISSION TEST NO.I      6    OAT£I   6-11-75      TIME!   13100       BARO.  PRESS.I   28.760 IN.  USA.
                           AMBIENT AIR TEMP.I 59.0   DEC.  F        RELATIVE HUMIDITYI  49.00 PERCENT       SPECIFIC  HUMIDITYI  .005000  L8. H20/LB. ORT AIR
                           AMBIENT AIR QUALITY    HYDROCARBONS (HC):  0.0   PPMC    CAR3ON MONOXIDE  (COII 0.0    PPMV     OXIDES OF  NITROGEN (NOX)I 0.0   PPHV
                           SAMPLE LINE ••• TEMP.I  300.00  OEG. F.      FLOMHATEI   14.16 LITERS/MIN.     TRANSPORT  TIMEI    6.50 SEC.      LENGTHI   50.(0 FT.
TEST CONDITION
PONER SETTING, CORRECTED HP.
Nl SPEED, RPM
FUEL FLON (MEAS.I LB./HR.
ENGINE CORE INLET AIRFLOH (CALC . 1 LB./SEC.
COMPRESSOR INLET TEMP.. OEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP., DEC. F
COMPRESSOR BLEED AIRFLOH (HEAS. > LB./SEC.
BLEED AIR PRESSURE. PSIA
BLEED AIR TEMPERATURE, OEG. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION, MET ANALYSIS
HYDROCARBON (HC AS CH4I , PPMC
CARBON MONOXIDE ICOI , PPMV
TOTAL OXIDES OF NITROGEN INOXI, PPMV
CARBON DIOXIDE (C02I, PERCENT BY VOL.
NITRIC OXIDE (NOI. PPNV
EMISSION INDEX, LB. POLLUTANT/1010 LS. FUEL
HYDROCARBONS (HC AS CH4I
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS N02I
EMISSION «AT€, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4I
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02I
ENGINE WORK OUTPUT, MEAS. SMP
ENGINE NORK OUTPUT, ISENTROPIC AIR HP
ENGINE HORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS*
76 77 78
0.00
41600.00
140.00
5.91
59.0
59.66
390.00
0.00
0.00
•0.00
500.0

115.500
242.211
17.000
1.339
10.300

9.640
35.369
4.076

1.350
4.952
.571
0.00
0.00
0.00
98.12
.117
76.68
41440.00
175.00
5.70
60.0
56.62
393.00
0.00
0.00
-0.00
623.0

66.000
269.721
25.000
1.751
17.000

4.243
30.334
4.616

.742
5.306
.806
75.70
0.00
75.70
96.91
.119
197.13
41110.00
242 • 00
5.02
60.0
57.94
401.00
0.00
0.00
-0.00
884.0

9.300
166.552
43.900
2.796
38.000

.379
13.302
5.142

.092
3.219
1.244
169.67
0.00
169.67
99.65
.113
79
0.00
40010.00
262.00
6.79
61.0
52.29
360.00
2.16
51.16
362.00
998.0

6.000
249.616
51.000
3.237
45.000

.207
15.081
5.061

.054
3.951
1.326
0.00
236.21
236.21
99.63
.(16
80
44.44
40950.00
266.01
6.69
56.1
54.70 ~
360.00
1.92
53.52 " "" 	
360.01
993.1

6.000
239.757
50.500
3.267
44.700

.209
14.623
5.059

.156
3.919
1.356
42.66
218.65
253.33
99.64
.016
-------
0)
iQ
CD

L7\
01
ENGINE* GTCP85-48CK S/N= 36179
RAT SHP« ZOO. RA EGT.F*
FUEL H/C= 1.9Z80 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POMER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR DSCHG. TEMP.OEG F
EXHAUST GAS PRESS.. PSIA
CORRECTED BLEED F..OH, LB/SEC
COMPRESSOR MAP FLOM, LB/SEC
FA RATIO BASED ON MAP FLOM
CORRECTED FUEL FLOM , LB/HR
FA RATIO CAiC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P»»N/V/E(T/S40I
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
LB. COZ PER L3. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
MtlGHT FLOM, LB./HR.
UNBURNED HYDROCARBONS- PPM AS
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
RATIO LB HC/LB CO
1150.
.06822
76
0.0
0.0
0.0
500.0
41600.0
59.7
390.0
13.70
0.000
5.97
.0065
140.0
.0066
.096
.388
98.322
COMB P/M= 698168-3 TEST DATE 6-11-75 FUEL'AV. KERO. P B»RO» Z8.76
%AT SPDs
L H V =
77
39.3
78.7
75.7
6Z3.0
41440.0
58.8
393.0
13.75
0.000
5.57
.0087
175.0
.0085
.1Z5
.369
96.914
41600.
18470.
78
98.6
197.1
189.7
884.0
41110.0
57.9
401.0
13.88
0.000
5.07
.0133
243.0
.0134
.196
.339
OEM PT,F=
S .N T.F*
79
0.
0.
0.
998.
40010.
52.3
360.0
13.85
2.268
6.62
.0164
262.0
.0158
.331
.384
99.654 99.637

1.34
3.07
430.1

21.2.3
35.369
4.953
1.75
3.09
5*1.6

Z69.7
30.334
5.308
CARBON. HEIGHTS AS
115.5
9.61,0
1.350
.2736
66.0
"..343
.74Z
.1399
z.ao
3.13
758.0

186.6
13.302
3.219
CH4
9.3
.379
.092
.0285
NITRIC OXIDE (NOI - HEIGHTS AS NOZ
PPM BY VOLUME. WET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
NITROGEN DIOXIDE (NOZ)
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
TOTAL OXIDES OF NITROGEN (NO*
PPM BY VOLUME, MET
LB. PER 1000 -B. OF FUEL
MEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA.
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOM
SMOKE NUMBER
CORRECTED HEIGHT FLOM
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
SMCKE NUMBER AT MA*0.023
10.3
Z.471
.346
6.7
1.607
.2Z5
NOZ) AS NOZ
17.0
4.078
.571

.00781
13.30
.02104
28.30
.03536
37.30
.04999
43.40
30.90
17.0
3.141
.550
S.fl
1.478
.259

25. •
4.618
.808

.00699
14.50
.02096
31.90
.03*92
41.00
.04877
49.40
34.70
38.0
4.451
1.077
5.9
.691
. .167

43.9
5. 142
1.31.4

.00698
13.30
.02094
29.50
.03490
38.60
.04865
46.48
32.40
itf e*
3.38
3.13
820.1

249.6
15.081
3.951.

6.0
.207
.054
.0137

45.0
4.466
1.170
6.0
.595
.156

51.0
5.061
1.3Z6

.00700
20.50
.03099
44.60
.03495
49.40
.04683
56.60
43.38
40. REL HUM= 49.00 SPEC HUM' .085000
300.0 FLO.L/M* 14.160 SL TIM,S» 6.5000
68
23. Z
4*,. 4 ._......-.. -
42.7
993.8
40958.8 	 _ 	
54.7
360.8
13.86 	 ... _
1.994
6.57
.0160 ......
268.0
.8156
.2Z9 _ .
.372
99.638

3. 27
3.13 . _. ......
839.8

239.8
14.623
3.919
	 . . _ .- 	 	 -^ 	 	
6.8
. 209
.056 	 	 	 	 -
.0143

44.7 • - 	 	 	 — 	
4.478
1.200
5.8
.581
.156 - ..-. — .--


50.5
5.059 _ . ._. . 	 	 	 —
1.356

.00698 .. 	 ...... ...... --. - -. .
19.30
.82098
36.70 ' 	
.03463
47.00
.04876 _.._... ._...__ .. . - 	 	 • - -
53.80
39.50
                                                                                                                                                                     ;>
                       NOTES 1. ALL EMISSIONS  CONttMii»i ions »Kt mi vamta.
                             2 EQUIVALENCE  RATIO CALCULATED FROM C02,CO,ANO HC  DATA ANO FUEL COMPOSITION.
                             3 MASS EH'S'IONS  OF NO, N32, AND MO*N02 CALCULATED AS M02 FROM CONCENTRATIONS MITH MOLECULAR HEIGHT OF NOZ  (46.81),

                             4lcOMBUSTI3M EFFICIENCY CALCULATED FROM C3.ANO UHC AS VAPORIZED ORIGINAL FUEL ON LB/ LB FUEL BASIS.      . .        .
-------
to
iQ
o>
Ul
  ENGINE* GICP85-98CK      S/N*  36179
DATA POINT NUMBER                    76        77
ENISSIOK RATE LB/HR
    CARBON MONOXIDE               <>.952     5.308
    UNBURNEO HYDROCARBONS         1.350      .7*2
    OXIDES OF NITROGEN             .571      .808
    NITRIC OXIOE                   .3
    UNBURNEO HYDROCARBONS         0.000     9.808
    OXIDES OF NITROGEN            0.000    10.677
    NITRIC OXIOE                  0.000     7.260
                                                                  •••  AIRESEARCH EMISSION TEST SUMMARY
                                                                  COMB P/N= 698168-3 TEST DATE  6-11-75
                                                                                78

                                                                             3.219
                                                                              .09Z
                                                                             1. Zl.lt
                                                                             1.077
                                                                           189.67
                                                                           197.13

                                                                            16.972
                                                                              .
-------
 ENGINE MFR.I A I RE SEARCH
MODEL NO.l  GTCP8S-96CK
FUEL! ASTM 01655-73
                               TEST  FACILITYI  PHX LACC2       INSTR. OESCRIP.!  FEDERAL  REG.  V38 N136   CALC.
                               S/NI   36179          ENGINE TYPE (CLASS)«  APU               CALC. I.O.I     2
                              MAX  SHP       200.  » BLEED AIR EXTRACTION TO    1150.  OEG.  F EGT
                                   ATOMIC H/C RATIOI   1.928    LHVI     181,70. BTU/LB.      AOOITIVESI NONE
                                                                                                                DATE!  6-11-75
           EXHAUST EMISSIONS  PER  EPA RATED HORK OUTPUT *• COOE OF FEDERAL REGULATIONS  TITLE 1.0 PART
          .............................. ,;MISsIONS COMPUTED FROM TEST  CONDITION  NO.  5   • •»•»»«•»•<
                   HYDROCARBONS  IHC AS CH<.)             .160  LB. POLuUTANT PER  1000 HP.-HR.
                   CARBON  MONOXIDE (CO!                It.758  i_B. POLLUTANT PER  1060 HP.-HR.
                   OXIDES  OF  NITROGEN INOX AS N02)     5.312  LB. POLLUTANT PER  1000 HP.-HR.
                                                                                                      67
                                                                                                            17 JULY 1973
[[[  ENGINE DESCRIPTION  •»••»••••»••»•••
COM3USTOR TYPEI  TANGENTIAL  CAN           P/NI  698165-3  SURFACE/VOLUME 1   .725  SO.  IN/CU  IN
ENGINE TOTAL SERVICE!       0.0  HR.    TIME SINCE ENGINE OVERHAUL!       0.0 HR.
ENGINE ASSEMBLY  AND MAINTENANCE  INFORMATION!
AIRCRAFT INSTALLATION ••»  NFR. «
                                                             MODEL NO.I
                                                                                               FUEL INJ. TYPEI
                                                                                                     USERI
                                                                                                                   DUAL ORIFICE
.............................,.............,...,OPER&nONAL T£ST DAIA  slJMNARIf  ,.......,,.....................................>
GASEOUS EMISSION TEST NO.I     6     DATE!  6-11-75      TIME!    IfcllS      BARO.  PRESS.I   28.706 IN. HGA.
AMBIENT AIR TEMP.I 59.0   OEG. f         RELATIVE HUMIDITY!  ".9.00 PERCENT        SPECIFIC HUMIDITY!  .005000 LB. H20/LB. DRY AIR
AMBIENT AIR QUALITY    HY3ROCAR80NS  (HCII 0.0   PPMC    CARBON MONOXIDE  (CO) I  0.0    PPMV     OXIDES OF NITROGEN (NOX)I 0.0   PPMV
SAMPLE LINE »»» TEMP.I  309.09 OEG.  F.      FLOH3ATEI   It.16 LITERS/MIN.     TRANSPORT  TIMEI    6.50 SEC.     LENGTHI   50.00 FT.
)


)


)


)


)


>
TEST CONDITION
POKER SETTING, CORRECTED HP.
Nl SPcEO, RPH
FUEL FLOW (MEAS.I LB./H9.
ENGINE CORE INLET AIRFLCM(CALC. ) LB./SEC.
COMPRESSOR INLET TEMP., OES. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP., DEG. F
COMPRESSOR BLEED AIRFLOW (*£A5.) LB./SEC.
BLEED AIR PRESSURE, PSIA
BLEED AIR TEMPERATURE, OEG. F
ENGINE EXHAUST GAS TEMP., DEG. F
EMISSION CONCENTRATION, NET ANALYSIS
HYDROCARBON IHC AS CHOI, PPMC
CARBON MONOXIDE (CO), PPMV
TOTAL OXIDES OF NITROGEN (NOXI, PPMV
CARBON DIOXIDE (C02). PERCENT BY VOL.
NITRIC OXIDE (NO), PP.1V
EMISSION INDEX, LB. POLLUTANT/1600 LB. FUEL
HYDROCARBONS (HC AS CHt)
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS N02)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CHtl
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS N02)
ENGINE WORK OUTPUT, HEAS. SHP
ENGINE NORK OUTPUT, ISENTROPIC AIR HP
ENGINE HORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PE*CEhT (EMISSIONS)
F/A (EMISSIONS!
61 62 83
0.08
1.1610.00
138.00
5.93
59.0
59.71
390.00
0.00
0.00
-0.00
t9t.O

105.000
239.757
18.000
1.31",
10.500

8.932
35.682
t.too

1.233
t.92t
.607
0.00
0.00
0.00
98.36
.006
78.99
tli.tO.00
172.00
5.1.9
58.0
58.92
392.00
0.00
0.00
-0.00
615.0

6«.5flO
27t.63t
25.080
1.787
16.300

<*.065
30.301
t.528

.699
5.212
.779
75.70
0.00
75.70
96.93
.009
197.35
1.1110.00
21.2.00
5.06
61.0
57.79
t02.00
0.00
0.00
-0.00
183.0

6.600
187.1.76
tt.708
2.763
39.000

.272
13.526
5.298

.066
3.273
1.282
119.67
0.60
189.67
99.66
.013
8t
0.00
tiooo.oo
262.00
6.66
59.6
52.78
357.00
2.19
51.55
380.00
997.0

7.500
259.612
51.500
3.389
t6.000

.252
15.259
t.972

.066
3.996
1.303
0.00
239. t 8
239. t6
99.62
.016
65
i.S.39
1.091.0.00
268.00
6.51
61.6 . .__•. 	 .... _ 	
St. 26
363.66
1.91 	 	 . _ . . _ _.. ..
• 53.13
381.. 00
1005.6 	 . .. _ .... 	

t.500
237.311 	 L_ ._ 	 	 	 ..
52.066
3.389
•.6.506 	 	 	 	 _

.151 .
13.959 	 	
s.ozt

.Otl ... _ 	 	 	
3. 7tl
1.3t6
-------
(D

tn
oo
ENGINE* GTCP8S-98CK 3/tt- 36179
RAT SHf* itt. RA E6T,F« 1150.
FUEL H/C* 1.9260 STOI F/«- .06822
DATA .POINT NUMBER 81
PERCENT MAX. CORRECTED POWER 8.0
CORRECTED SHAFT HP 0.
MEASURED SHAFT HP 0.
EXHAUST GAS TEMP.. OEG.F 1.91,.
SHAFT SPEED, Nl, RPM k!610.
COMPRESSOR DSCHG. PRES. ,PSIA 59.
COMPRESSOR DSCHG. TEMP.DES F 390.
EXHAUST GAS PRESS., PSIA 13.67
CORRECTED BLEED FLOH, LB/SEC 0.000
COMPRESSOR MAP FLON, LB/SEC 5.97
FA RATIO BASED ON MAP FLOH .0061.
CORRECTED FUEL FLOH , LB/HR 138.0
FA RATIO CALC. FROM EMISSION .0065
EQUIVALENCE RATIO .095
LOADING H/P»»N/V/EIT/5k8) .387
COMB EFFIC FROM EMISSIONS 96.377
CARBON DIOXIDE
PERCENT BY VOLUME. NET 1.31
L3. C02 PER LB. OF FUEL 3.67
HEIGHT FLOW, LB./HR. 1.21.. 1
CARBON MONOXIDE
PPM BY VOLUME, NET 239.8
LB. PER 1080 LB. OF FUEL 35.682
HEIGHT FLOH. LB./HR. *.92k
COMB P/N= 696168-3 TEST DATE b-ll-7S FUEL'AV. KERO. P BARO« 26.78
RAT SPO
L H V
62
39.5
79.0
75.7
615.0
1.11. 1.0.0
58.9
392.0
13.72
0.008
5.57
.0086
172.6
.0067
.126
.366
98.931

1.79
3.16
532.1,

27*. 8
30.301
5.212
UNBURNEO HYDROCARBONS- PPM AS C4R30N, HEIGHTS AS
PPH BY VOLUME, NET 105.0
LB. PER 1060 LB. OF FUEL 8.932
HEIGHT FLOH, LB./HR. 1.233
RATIO LB HC/LB CO .2503
NITRIC OXIDE (NOI - HEIGHTS AS N02
PPH BY VOLUME, MET 18.5
L3. PER 1800 iB. OF FUEL 2.567
HEIGHT FLOH, LB./HR. .35
-------
  ENGINE' GTCP85-98CK
DATA POINT NUMBER
EMISSION RATE LB/HR
    CARBON MONOXIDE
    UNBURNEO HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIDE
POHER LEVEL HP
TOTAL CORRECTED HORSEPOWER
                                                    S/N=
36179
    81

 •..92".
 1.233
  .607
  .351.
 0.00
 0.00
                                                                         AIRESEARCH EMISSION TEST  SUMMARY
                                                                         P/N* 696168-3 TEST DATE   6-11-75
                                                                                                                 FUEL'AV. KERO.
                                                                                                                                   P BAUD- Z8.7S
    82

 5.212
  .649
  .779
  .508
75.70
78.99
BRAKE SPECIFIC EMISSION INDEX  L3/10DOHP-HR
    CARBON MONOXIDE               0.000    68.8<>a
    UNBURNED HYDROCARBONS         0.000
    OXIDES OF NITROGEN
    NITRIC OXIDE
    NOTE**0. APPEARING IN  BRAKE
           9.235
 0.000    10.267
 0.000     6.707
SPECIFIC EMISSION
                                                                                  S3

                                                                               3.273
                                                                                .066
                                                                               1.282
                                                                               1.119
                                                                             189.67
                                                                             197.35
                                   8".

                                3.998
                                 .066
                                1.313
                                1.16%
                              239.1.8
                              249.66
                                                                              17.258    16.693
                                                                                .31.7       .276
                                                                               6.759     S.^ltO
                                                                               5.997     fc.»59
                                                                            INDEX COLUMN DENOTES
     85

  3.71.1

  1.3*6

25jl 1.9
261,. 60

 W.756
   .168
  5.312
  1..75B
AN IDLE CONDITION
                                                                                                                                              I,
 &)
Ifl
 fD
-------
                 o
(U
                        ENGINE HFR. « AIRESEARCH
                       MODEL NO. I  GTCP85-98CK

                       FUEL! ASTM 01655-73
 TEST FACILITYl PHX LACCZ        INSTR.  OESCRIP.I    FEDERAL REG V38 N136   CALC.
 S/NI  36179          ENGINE TYPE  (CLASSII   APU              CALC..I.D.I     3
MAX SHP       ZOO. » BLEED AI« EXTRACTION TO    1150.  DEG. F EGT
    ATONIC H/C RATIOI   1.928    LHVI     181.70.  BTU/LB.      AODITIVESI NOME
                                                                                                                DATEI  6-11-75
                                  EXHAUST EMISSIONS PtR EPA RATED  HORK  OUTPUT  ••  CODE OF FEDERAL REGULATIONS TITLE 1.0 PART 87
                                 .............................. EMISSIONS  COMPUTED FROM TEST CONDITION NO.  5   »••»».»».....•
                                          HYDROCARBONS IHC AS  CH4I              .190  LB. POLLUTANT PER 1000 HP.-HR.
                                          CARBON MONOXIDE  (COI               11.. 760  LB. POLLUTANT PER 1000 HP.-HR.
                                          OXIDES OF NITROGEN (NOX  AS NOZI      5.157  LB. POLLUTANT PER 1000 HP.-MR.

...............I....................................   £N6INE DESCRIPTION  •••••»••»•»••••»
COHBUSTOR TYPEI TANGENTIAL CAN          P/NI   698168-3  SURFACE/VOLUME!   .725 SO. IN/CJ IN
ENGINt TOTAL SERVICEI      0.0 MR.   TIME SINCE ENGINE OVERHAUL!      (.0 HR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                       AIRCRAFT INSTALLATION ••» MFR. 1
                                                                                    MODEL NO.I
                                                                                                                     FUEL INJ. TYPEI
                                                                                                                           USERI
                                                                                                                                         DUAL  ORIFICE
                       "••"•"•••"••"••••••••••••"•••••••••••"••'OPERATIONAL TEST DATA SUMMARY ••••••»•»•••»»•»••••••••••••»•»»•••••••»•»•»••••
                       GASEOUS EMISSION TEST NO.I     6    3ATEI  6-11-75       TIME!     3115       BARO. PRESS.I  28.700 IN. HGA.
                       AMBIENT AIR TEMP. 1 59.0  DEG. F         RELATIVE  HUMIDITY!   1.9.00 PERCENT       SPECIFIC HUMIOITY1  .005000 LB. H2O/LB.  DRY AIR
                       AMBIENT AIR QUALITY    HYDROCARBONS (HCII 0.0    PPMC     CARBON MONOXIDE (COII 0.0   PPMV    OXIDES OF NITROGEN (NOX)I  (.0    PPMV
                       SAMPLE LINE •" TEMP. I  3(0.00 OEG. F.     FLOHWEI    lit.16 LITERS/NIN.     TRANSPORT TIMEI    6.50 SEC.     LENGTHI    50.00 FT.
                                                                                                                                             >


                                                                                                                                             )


                                                                                                                                             )
TEST CONDITION
POWER SETTING, CORRECTED HP.
Nl SPEED. RPN
FUEL FLCM (HEAS.I LB./HR.
ENGIN£ CORE IN.ET AIRFLCM (CALC. 1 LB./SEC.
COMPRESSOR INLET TEMP., OEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP. , OEG. F
COMPRESSOR BLEED AIRFLON (NEAS. 1 LB./SEC.
BLEED AIR PRESSURE. PSIA
BLEED AIR TEMPERATURE, OEG. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION. MET ANALYSIS
HYDROCARBON IHC AS CW.I , PPMC
CARBON MONOXIDE (COI, PPMV
TOTAL OXIDES OF NITROGEN (NOX). PPHV
CARBON DIOXIDE (C02I , PERCENT BY VOL.
NITRIC OXIDE (NOI, PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CHI,)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS NOZI
EMISSION RATE. LB. POLLUTANT/MR.
HYDROCARBONS (HC AS CM*)
CARBON MONOXIDE ICOI
TOTAL OXIDES OF NITROGEN INOX AS NOZI
ENGINE WORK OUTPUT, HEAS. SHF
ENGINE WORK OUTPUT, ISENTROPIC AIR HP
ENGINE WORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS)
86 87 as
0.00
1.1610. 00
138.00
5.80
62.0
59.17
392.00
0.00
0.00
-0.00
1.98.0

96.000
Z-.lt. 179
17.800
1.31.7
.12.600

7.975
35.1.89
.I..250

1.101
It. 898
.586
0.00
0.00
0.01
98.1.7
.(•7
78.77
1.11.1.0.00
175.00
5.59
61.0
58.67
391,. 00
(.00
1.00
-o.oa
621.0

61.500
269.721
2 (..500
1.787
17.000

3.877
29.751
fc.1.39

.679
5.206
.777
75.70
(.00
75.70
98.96
.••9
197.76
1.1090.00
2*2.00
5.07
61.0
57.91,
1.02.00
0.00
0.00
-0.00
879.0

6.000
185.167
1.3.500
2.768
38.000

.21.7
13.335
5.11.6

.•60
3.227
1.245
190.16
0.00
190.06
99.66
.•13
89
0.00
(.0990.00
262. 00
6.66
58.0
52.78
356.00
2.18
51.1.6
378.00
998.0

7.500
251..593
50.500
3.1.01
1.5.800

.251
14.912


.066
3.907
1.273
0.10
237.90
237.91
99.63
.116
90
1.5.97
(
3.75Z ...-.-... ......
1.311
tii. (9 " _ . ,
211.11
25*.2I
. 99.6* , . ... ,... . . .... 	 •
.•10 •
-------
as
ENGINE: GTCP85-96CK S/N= 36179















;


)

)


)


)


)


)


)


)

RAT SHP= 280. RA EGT,F=
FUEL H/C« 1.9Z80 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POMER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR DSCHG. TEMP.DEG F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOM, LB/SEC
COMPRESSOR NAP FLOM, LB/SEC
FA RATIO BASED ON HAP FLOM
CORRECTED FUEL FLOM , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P*»N/V/E(T/540J
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
LB. C02 PER LB. OF FUEL
MEIGHT FLOM, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, MET
LB. PER 1080 LB. OF FUEL
MEIGHT FLOM, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NO) - HEIGHTS AS
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
NITROGEN DIOXIDE (NOZ)
PPK BY VOLUME, MET
..B. PER 1080 LB. OF FUEL
MEIGHT FLOM, LB./HR.
1150.
.06822
86
0.0
0.0
0.0
498.0
41610.0
59.2
392.0
13.68
0.000
5.9Z
.0065
138.0
.0066
.097
.369
98.466

1.35
3.08
424.5

244. Z
35.489
4.498
COMB P/NE 696168-3 TEST DATE t-11-75 FUELsAV. KERO. P 8»RO« 28.78
RAT SPD-
= 41600.
L H V* 18470.
87
39.4
78.8
75.7
621.1
41440.4
58.7
394.0
13.72
0.000
5.57
.0087
175.0
.0087
.127
.370
98.960

1.79
3.10
541.9

269.7
29.751
5.206
CARBON, HEIGHTS AS
96.0
7.975
1.101
.2247
NOZ
12.6
3.808
.415

5.2
1.241
.171
61.5
3.877
.679
.1303

17.0
3.080
.539

7.5
1.359
.Z38
88
98.9
197.8
190.1
879.0
-.1090.0
57.9
402.0
13.85
0.000
5.03
.0134
242.0
.0133
.194
.336
99.665

2.77
3.13
758.0

185. Z
13.335
3.227
CH4
6.0
.247
.068
.0185

38.0
4.495
1.088

5.5
.651
.157
OEM PT,F= 40. REL HUM: 49.88 SPEC HUM' .885888
S LN T,F
• 9
0.0
0.0
0.0
998.8
48998.8
52.6
356.0
13.63
2.271
6.62
.0164
262.0
.0162
.238
.360
99.627
REDUCED
3.48
3.13
820.0

254.6
14.912
3.987

7.5
.251
.066
.0168

45.8
4.338
1.134

5.5
.529
.139
- 300.8 FLO.L/H* 14.168 SL.TIH.S* 6.5888
98
23.0
46.0
44.1
1003.8
40930.8 	
54.4
361.8
13.83
1.989
6.47
.8163
268.8
.0163
.239
.366
99.655

3.41
3.13
639.3

239.8 	 . . _. _
14.088
3.752

~5.V " 	
.168
.848
.0129

45.5
4.364
1.178

5.5
.528
.1*1 	 _. 	 . 	
TOTAL CXIOES OF NITROGEN (NO-fNOZI AS NOZ
)


)


)


;


)
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED MEIGHT FLCM
SMOKE NUMBER
CORRECTED HEIGHT FLCM
SMOKE NUMBER
CJRRECTED MEIGHT FLCM
S40KE NUMBER
CORRECTED MEIGHT FLCM
SMOKE NUMBER
SMOKE NUMBER AT HA=O.OZ3
17.8
4.258
•.586

.08699
14.58
.02096
31.38
.03481
39.20
.04873
44.60
32.80
24.5
4.439
.777

.00696
16.70
.02041
32.50
.03481
43.40
.04973
47.08
35.90
43.5
5.146
1.245

.00695
15.78
.02098
30.10
.83484
36.70
.34686
43.48
31.98
50.5
4.859
1.273

.08788
22.98
.02099
41.68
.03495
46.68
.04983
68.28
43.98
51.8
4.692 _ 	 	
1.311

.08788
19.31
.02101
38.68 ....._ .......
.03581
44.66
.84981
58.88
36.58
                                                                                                                                                                    t)
                      NOTES 1. ALL EMISSIONS  CONCENTRATIONS ARE MET VALUES.
                            Z.EQUIVALENCE  RATIO  CALCULATED FP.ON C02,CO,ANO HC DATA  AND FUEL COMPOSITION.
                            3.MASS EMISSIONS  OF  NO,  NOZ, AND NO»N02 CALCULATED AS NOZ FROM CONCENTRATIONS HITH MOLECULAR MEIGHT OF NOZ (46.111.
                            4.COMBUSTION EFFICIENCY  CALCULATED FROM CO,AND UHC AS VAPORIZED ORIGINAL  FUEL ON LB/ LB FUEL BASIS.
-------
                                                        s'N=
AIRESEARCH EMISSION TEST SUMMARY
           1-3 TtST
                             EMISSION RATE LB/HR
                                 C&REON NOMOXIOE              <..898     5.Z06     3.22^
                                 UNBURNEO HYDROCARBONS        1.101      .679      .060
                                 OXIDES OF NITROGEN            .586      .777     1.2
-------
1    ENGINE  MFR.I  AIRESEARCH
   MODEL  NO.I   GTCP65-96CK

'<   FUEL!  ASTH  D1655-73
                                                        TEST FACILITYI PHX LACC2       INSTR. DESCRIP.l   FEDERAL KEG ¥38 N136    CALC. OATEt
                                                        S/NI  36179          ENGINE TYPE  ICLASSII    APU              CALC. I.D.I     1
                                                       MAX SHP       200. » BLEED AIR EXTRACTION TO   1150. OEC. F EGT
                                                           ATONIC H/C RATIOI   1.926    LHVI     181.70.  BTU/LB.      AODITIVESI NONE
                                    EXHAUST EMISSIONS  PER EPA RATED WORK OUTPUT *• COQE  OF  FEDERAL  REGULATIONS TITLE 40 PART 67
                                   ...,...........,..,.„,„...... EMISSIONS COMPUTED FROM TEST  CONDITION NO.   5   ..»»»»»»»..»..
                                           HYDROCARBONS (HC AS CH*I              .322  LB.  POLLUTANT  PER 1000 HP.-MR.
                                           CARBON  MONOXIDE ICO)               16.726  LB.  POLLUTANT  PER 1080 HP.-MR.
                                           OXIDES  OF  NITROGEN (NOX AS NO?)     4.623  LB.  POLLUTANT  PER 1100 HP.-MR.
                                                                                                                                    17 JULY 1973
                        ,.„,.,...»..........,,..,,..„,.,...........,,....„  ENGINE DESCRIPTION
                        CON8USTOR  TYPE!  TANGENTIAL CAN          P/NI  698168-3  SURFACE/WOLUMtI   .
                        ENGINE TOTAL  SERVICE:      0.0 HR.   TIMc SINCE ENGINE OVERHAULI       D.B
                        ENGINE ASSEMBLY  AND MAINTENANCE INFORMATION!
                                                                               725 SO IN/CJ
                                                                               HR.
                                                                                            IN
                        AIRCRAFT INSTALLATION •»•  NFR. I
                                                                                     MODEL  NO.I
                                                                                                  FUEL  INJ.  TYPEI
                                                                                                                             USERI
                                                                                                                       DUAL  ORIFICE
                        ..».»..•...•••».•»•.........•..00..•••..•.....».0p£RtTIONAL  TEST OATA  SUMMARY  ••»••»»•••••••••»••••»••»••••••»•••••»••••••••••
                        GASEOUS EMISSION TEST  NO.I      7    OATEl  6-12-75      TIME!                BARO.  PRESS.I  2S.700 IN. MSA.
                        AMBIENT AIR TEMP.I  59.0   OEG.  F        RE.ATIVE HUMIDITY*  49.00 PERCENT        SPECIFIC HUMIDITY!  .007900 LB. H20/LB. DRY AIR
                        AMBIENT AIR QUALITY    MYDROCARSONS (HOI 0.0   PPMC    CARBON MONOXIDE  (CO) I  0.0    PPMV    OXIDES OF NITROGEN (NOX)I 0.0   PPMV
                        SAMPLE LINE ••» TEMP. I  300.00  DEC. F.     FLOM3ATEI   lit.16 LITERS/HIM.     TRANSPORT HUE I    6.50 SEC.     LENGTHI   SO.01 FT.
(D

CTl
U)
TEST CONDITION
POWER SETTING, CORRECTED HP.
Nl SPEED, RPN
FUEL FLON (MEAS.) LB./HR.
ENGINE CORE INLET AIRFLON (CALC. > LB./SEC.
COMPRESSOR INLET TEMP., OEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP.. OEG. f
COMPRESSOR BLEED AIRFLOH (HtAS.) LB./SEC.
BLEED AIR PRESSURE, PSIA
BLEED AIR TEMPERATURE, DEC. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION, WET ANALYSIS
HYDROCARBON (HC AS CHI,), PPHC
CARBON MONOXIDE (CO) , PPMV
TOTAL OXIDES OF NITROGEN (NOX) , PPMV
CARBON DIOXIDE (C02) , PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSION INDEX, LS. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02I
ENGINE WORK OUTPUT, MEAS. SHP
ENGINE WORK OUTPUT, ISENTROPIC AIR HP
ENGINE WORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS!
91 92 93
0.00
41600.00
140.00
6.01
61.0
61.13
382.01
0.00
0.00
-0.00
483.0

123.000
244.179
15.000
1.314
9.000

10.446
36.280
3.661

1.462
5.079
.513
0.00
0.00
0.00
96.23
.006
78.99
41460.00
178.00
5.75
59.1
60.15
384.00
0.00
1.00
-0.00
610.0

70.500
273.608
22.500
1.765
13.800

4.496
30.552
4.124

.801
5.438
.734
75.77
0.00
75.77
96.89
.009
197.59
41160.00
240.00
5.11
61.1
59.17
392.10
0.11
1.10
-0.00
655.0

8.700
192.111
39.500
2.725
33.300

.364
14.149
4.745

.167
3.372
1.139
169.90
0.01
189.90
99.64
.013
94
0.00
41030.00
265.00
6.66
56.1
53.37
351.11
2.Z6
52.11
370.00
992.1

5.400
213.231
49.401
3.352
43.500

.184
12.666
4.826

.049
3.362
1.281
0.00
239.97
239.97
99.69
.016
95
45.55
40960.00
274.11
6.61
51.1
55.24
351.01
1.97.. 	
53.91
371.11
993.1 _ 	 ..._

9.111
267.179 	 	 	
46.900
3. 432
41.800 	 	 	 	

.296
15.513
4.471

.162 , _.._....
4.246
1.225
43.65
210.32
253.96
99.61
.116
-------
                  •1 /
ft)
ENGINE' GTCP85-96CK S/N= 36179
RAT SHP- 280. RA E6T,F=
FUEL H/C' 1.9280 STOI F/A*
DATA POINT NUMBER
PERCENT MAX. CORRECTED POWER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP.. OtG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR OSCHG. TENP.OEG F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOW, IB/ SEC
COMPRESSOR MAP FLOW.LB/SEC
FA RATIO BASED ON MAP FLOW
CORRECTED FUEL FLOW , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P**N/V/E«T/54fll
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME. WET
L8. C02 PER LB. OF FUEL
WEIGHT FLOW, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, WET
LB. PER 1000 LB. OF FUEL
WEIGHT FLOW, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPH BY VOLUME, WET
LB. PER 1000 LB. OF FUEL
WEIGHT FLOW, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE INOI - WEIGHTS AS
PPH BY VOLUME, WET
LB. PER 1110 LB. OF FUEL
WEIGHT FLOW, LB./HR.
NITROGEN DIOXIDE INOZI
PPH BY VOLUME, WET
LB. PER 1000 LB. OF FUEL
WEIGHT FLOW, LB./HR.
1150.
.06022
91
0.
0.
0.
463.
41600.
61.
362.
13.67
0.000
6.09
.1064
141.0
.0065
.095
.39*
96.210

1.31
3.07
429.6

244.2
36.26t
5.079
COM3 P/N* 698166-3 TEST DATE 6-12-75 FUEL*AV.KERO. P BARO* 26.71
RAT SPO=
L H V*
92
39.5
79.0
75.8
600.1
41460.0
60.1
364.0
13.73
0.000
5.67
.0007
176.0
.0086
.126
.367
98.687

1.76
3.09
550.7

273.8
30.552
5.436
CARBON, HEIGHTS AS
123.0
10.446
1.462
.2679
N02
9.0
2.197
.308

6.0
1.464
.205
70.5
4.496
.800
.1472

13.8
2.529
.450

8.7
1.595
.284
41600.
16470.
93
96.8
197.6
169.9
655.0
41160.0
59.2
392.1
13.64
0.000
5.16
.0129
240.1
.0131
.191
.Sol
99.638

2.72
3.13
751.4

192.1
14.049
3.372
CH4
6.7
.364
.067
.0259

33.3
4. Ill
.961

6.2
.745
.179
OEH PT.F*
S LN T,F=
94
0.0
JO.O
0.0
992.0
41030.0
53.4
351.0
13.64
2.349
6.67
.0167
265.0
.0160
.234
.374
99.615
OF DEDUCED
3.35
3.13
830.4

213.2
12.668
3.362

5.4
.114
.049
.1145

43.5
4.252
1.127

5.9
.5/7
.153
50. REL HUM* 49.00 SPEC HUM' .007518
300.0 FLO,L/M= 14.160 SL TIM.S* 6.5000
95
22.8
45.5
43.6
993.0
40960.0
55.2
351.0
13.63
2.052
6.59
.0165
274.0
.0164
.248
.369
99.689

3.43
3.13
857.3

267.2
15.513
4.246

9.1
.291
.112
.0193

_. 41.6... 	 	 _ 	 	 	
3.984
1.092

5.1
.466
.133
TOTAL OXIDES OF NITROGEN CN04NO2I AS N02
PPH BY VOLUME, WET
LB. PER 1000 LB. OF FUEL
WEIGHT FLOW, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOW
SMOKE NUMBER
CORRECTED WEIGHT FLOW
SMOKE NUMBER
CORRECTED WEIGHT FLOW
SHOKE NUMBER
CORRECTED WEIGHT FLOW
SMOKE NUMBER
SMOKE NUMBER AT HA*0.02J
15.1
3.661
.513

.01706
16.90
.02124
29.50
.03539
39.80
.04945
48.20
33.81
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE
22.5
4.124
.734

.00706
19.90
.02119
32.50
.03532
4«.60
.04943
51.80
37.50
39.5
4.745
1.139

.00715
10.60
.02111
26.91
.13515
39.80
.04921
47.00
32.01
49.4
4.628
1.288

.11703
27.11
.02119
42.21
.13517
51.60
.04911
61.40
46.11
46.9
4.471
1.225

.00702 . . ._ . .......
21.71
.12115
39.81 ...... . . 	 _
.03506
45.01
.04906
57.01
41.71 .
WET VALUES. 	 	 	 	 _.

                             2.EQUIVALENCE RATIO CALCULATED FROM C02.CO.ANO HC DATA AND FUEL COMPOSITION.
                             3.MASS EMISSIONS OF MO, N02, AND NO»N02 CALCULATED AS N02 FROM CONCENTRATIONS WITH MOLECULAR WEIGHT OF N02 (46.11).
                             4.COMBUSTION EFFICIENCY CALCULATED FROM CO,MIS UMC AS VAPORIZED ORIGINAL  FUEL ON LB/ L8 FUEL BASIS.
-------
                                                                                                                                                                      I
                                                    S/N
                                                         36179
                                                             91

                                                          5.179
                                                          1.<>6Z
                                                           .513
                                                           .301
                                                          0. 00
                                                          0.00
•*»  AIRESEARCM EMISSION TEST
COM3 P/N= b9616t-3 TEST DATE
    9Z
              93
                        94
                              6-12-7S
                                  95
»•••»»»»»»»»•»»»»»•»»»
  ENGINE' GTCP85-98CK
DATA POINT NUMBER
EMISSION RATE LB/HR
    CARBON MONOXIDE
    UNBURNEO HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIDE
POWER LEVEL HP
TOTAL CORRECTED HORSEPOWER
BRAKE SPECIFIC EMISSION  INDEX LB/1000HP-HR
    CARBON MONOXIDE               0.000
    UNBURNED HYDROCARBONS         0.000
    OXIDES OF NITROGEN            0.000
    NITRIC OXIDE                  0.000
    NOTE»»0. APPEARING IN BRAiCE  SPECIFIC EMISSION INDEX  COLUMN DENOTES AN IDLE CONDITION
                                                                                                               FUEL'AV.KERO.
                                                                                                                                  P  BARO* 21. 7B
5.1.38
.500
.73<>
.".SO
75.77
78.99
71.770
10.562
9.699
5.9*2
3.372
.087
1.139
.960
189.90
197.59
17.755
.1(60
5.997
5.056
3.362
.Oi>9
1.280
1.127
239.97
21.9.93
14.012
.203
5.332
4.695
4.248
.082
1.225
1.092
253.96
264.59
16. 726
.322
4.823
4.298
 ft)
ua
 (D
 Ul
-------
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VQ
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                           ENGINE HFR.t AIRESEARCH
                          MODEL NO. 1  GTCP8S-90CK

                          FUEL! ASTM 01655-73
 TEST FACILITYI PMX LACCZ        INSTR.  OESCRIP.I   FEDERAL  REG ¥38 N136    CALC. DATE!
 S/NI  36179          ENGINE  TYPE  (CLASS)I  APU               CALC. I.O.I     I
MAX SHP       ZOO. * BLEED AIR  EXTRACTION TO    1150.  DEC.  F EGT
    ATONIC H/C RATIOI   1.9Z8    LHVI     18*70.  BTU/LB.      ADDITIVES! NONE
                                                                                                                       6-12-75
                                     EXHAUST EMISSIONS PER EPA RATED WORK OUTPUT •• CODE OF FEDERAL REGULATIONS  TITLE *0 PART 87
                                    .............................. tMISSIONS COMPUTED FROM  TEST CONDITION  NO.  5   »»..»»»•••••••
                                             HYDROCARBONS (HC AS CH*I             .338  LB. POLLUTANT PER  1000 HP.-HR.
                                             CARBON MONOXIDE (CO)               16.838  LB. POLLUTANT PER  1000 HP.-HR.
                                             OXIDES OF NITROGEN (NOX AS NOZ)     5.006  LB. POLLUTANT PER  1000 HP.-HR.

 [[[  £NtINe  DESCRIPTION  ••»•••»••«••«
 COHBUSTOR TYPEI TANGENTIAL CAN          P/NI  698168-3   SURFACE/VOLUME I   .725 SU IN/CU
 ENGINE TOTAL SERVICE!      0.0 HR.   TIHE SINCE ENGINE OVERHAULI       0.0 HR.
 ENGINE ASSEMBLY AND MAINTENANCE INFORMATION*
                                                                                                                  IN
                                                                                                                        FUEL INJ.  TYPEI
                                                                                                                                            DUAL ORIFICE
                          AIRCRAFT INSTALLATION  •••  NFR. I
                                                                                      MODEL NO.I
 ...............................»»»»••*»...»»...,0pEi,ATJOMAL  T£ST  OATA SUMM4Ry ..........*................................„.„

 GASEOUS EMISSION TEST NO.I     7    DATEl  6-12-75       TIMtl     10.10      BARD.  PRESS.I  Z8.711 IN. HGA.
 AMBIENT AIR TEMP.I 59.0  OEG. F        RELATIVE HUMIDITY.   70.00  PERCENT       SPECIFIC HUMIDITY!  .017500 LB. HZO/LB. DRY AIR
 AMBIENT AIR QUALITY    HYDROCARBONS (HCII 0.0   PPMC     CARBON MONOXIDE (CO)I 0.0    PPMV    OXIDES OF NITROGEN (NOXII 0.0   PPNV
 SAMPLE LINE «• TEMP.I  300.00 OES. F.     FLOMKATEI    1*.16 LITERS/MIN.     TRANSPORT TIME!    6.50 SEC.     LEN6THI   50.01 FT.
                                                                               COMPUTED EMISSIONS
                                                                                                                                                                       )


                                                                                                                                                                       >
 TEST CONDITION                                           96         97        98        99       110
 POWER SETTING. CORRECTED HP.                           0.00      78.91    197.95      0.01     1.5.1.6
 HI SPEED, RPM                                     1,1620.00   *1*50.00  1.1130.00  1,1000.00  1.191.1.01
 FUEL FLOW (MEAS.) L6./HR.                           1*0.00     177.00    2*2.00    265.00    275.00
 ENGINE CORE INLET AIRFLOW(CALC.) LS./SEC.              5.91       5.71      5.18      6.80      6.6*
 COMPRESSOR INLET TEMP., OEG. F                         58.1       59.0      51.0      51.0      59.1
 COMPRESSOR DISCHARGE AIR PRESSURE, PSIA              61.13      61.10     59.26     53.37"   55.2*
 COMPRESSOR DISCHARGE AIR TEMP., DEC. F              378.10     36*.00    390.00    3*8.01    351.11
 COMPRESSOR BLEED AIRFLOW (MEAS.I LB./SEC.              0.00       0.00      0.00      Z.Z*      1.97
 BLEED AIR PRESSURE. PSIA                               0.01       0.01      0.11     52.1*     53.91
 BLEED AIR TEMPERATURE. OEG. F                        -0.00      -0.60     -0.10    368.00    369.00
 ENGINE EXHAUST CAS TEMP., OEG. F                     1*12.0      600.0     850.1     993.1     989.1
 EMISSION CONCENTRATION, HET ANALYSIS
      HYDROCARBON (HCASCH*!. PPNC                115.500     70.500      9.000      5.700     9.301
      CARBON MONOXIDE (CO), PPNV                   2*3.686    273.888    189.790    217.999   26*.6**	
      TOTAL OXIDES OF NITROGEN (NOXI , PPMV          15.911     22.901     39.500     1.1.511    *7.90i
      CARBON DIOXIDE (COZI, PERCENT BY VOL.          1.323      1.769      2.719      3.389     3.*19
      NITRIC OXIDE (NO), PPHV                       11.710     1S.*00     3*.211     1*3.500    *2.000
 EMISSION INDEX, LB. POLLUTANT/1010 L3. FUEL                                              - -     -  _
      HYDRCCARBONS (HC AS CM*)                       9.756      *.*85       .378       .192      .311
      CARBON MONOXIDE (CO)                          36.010     39.*77     13.963     12.830    15.*1Z
      TOTAL OXIDES OF NITROSEN (NOX AS NOZI          3.859      *.187      *.773      d.689     *.58Z
 EMISSION RATE, LB.  POLLUTANT/MR.
      HYDROCARBONS 
-------
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VQ
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 (Ti
ENGINE' GTCP85-98CK S/N* J6179 COMB P/N* 698168-3 TEST DATE 6-12-75 FUEL«AV.KERO. / "R°* "t™
RAT SHP. ZOO. RA EGT.F- 1150. RAT SPO- 41600. OtH PT.F- 50. REL HUM= 78.08 SPEC MUM* .8875.8
) FUEL H/C= 1.9288 STOI F/A= .86822 L H V= 16470. S LN T,F= 308.8 FLO.L/M« 14.160 SL TIM.S- 6.5101
DATA POINT NUMBER 96
" PERCENT MAX. CORRECTED POHCR 0.0
CORRECTED SHAFT HP 8.0
MEASURED SHAFT HP 8.8
EXHAUST GAS TEMP., OEG.F 482.0
97 98
39.5 99.
78.9 198.
75.7 189.
600.0 850.
SHAFT SPEED, Nl, RPM 1.1628.0 *1*50.8 *1130.
COMPRESSOR OSCHG. PRES.,PSIA 61.1
i COMPRESSOR OSCHG. TEMP, DEC F 378.0
EXHAUST GAS PRESS., PSIA 13.67
CORRECTED BLEED FLOH, LB/SEC 0.808
COMPRESSOR HAP FLOM,LB/SEC 6.87
FA RATIO BASED ON MAP FLOH .1864
CORRECTED FUEL FLOH , LB/HR 1*0.8
1 FA RATIO CALC. FROM EMISSION .0065
EQUIVALENCE RATIO .095
LOADING H/P>*N/V/EIT/540t .386
COMB EFFIC FROM EMISSIONS 98.297
CARBON DIOXIDE
) PERCENT BY VOLUME, NET 1.32
L3. C02 PER LB. OF FUEL 3.07
HEIGHT FLOH, LB./HR. 429.9
) CARBON MONOXIDE
PPM BY VOLUME, MET 2*3.7
L3. PER 1000 LB. OF FUEL 36.018
HEIGHT FLOH, LB./HR. 5.0*1
60.1 59.3
38*.* 398.0
13.73 13.8**
0.000 0.888
5.67 5. IS
.0087 .8131
177.0 2*2.0
.0086 .8130
.126 .190
.368 .338
98.890 99.638

1.77 2.71
3.09 3.13
5*7.6 757.7

273.8 189.8
30.477 13.963
5.39* 3.379
UNBURNEO HYDROCARBONS- PPM AS CARBON, HEIGHTS AS CH*
PPM BY VOLUME, HET 115.5
1 LB. PER 1888 LB. OF FUEL 9.756
HEIGHT FLOM, LB./HR. 1.366
RATIO LB HC/LB CO .2709
1 NITRIC OXIDE INOI - HEIGHTS AS N02
PPM BY VOLUME, HET 11.7
LB. PER 1000 LB. OF FUEL 2.8*0
) HEIGHT FLOH, LB./HR. .398
NITROGEN DIOXIDE IN02I 	
PPM BY VOLUME, MET 4.2
) LB. PER 1000 LB. OF FUEL 1.019.
HEIGHT FLOM, LB./HR. .143
TOTAL OXIDES OF NITROGEN INO*N02> AS NOZ
. PPM BY VOLUME. MET i.S.9
• LB. PER 1008 LB. OF FUEL 3.859
HEIGHT FLOH, LB./HR. .5*0
) SMOKE MEASUREMENT DAT*
CORRECTED HEIGHT FLOH .00781
SMOKE NUMBER 14.10
) CORRECTED HEIGHT FLOM .OZ104
SMOKE NUMBER 32.58
CORRECTED HEIGHT FLCH .03585
) SMOKE NUMBER 41.00
CORRECTED HEIGHT FLOM .8*907
SMOKE NUMBER 49.40
) SMOKE NUMBER AT HA*8.823 35.60
_P_ . ALL EMISSIONS CONCENTRATIONS ARE
2IEQUIVALENCE RATIO CALCULATED FROM
) 3. MASS EMISSIONS OF NO, N02, AND NO
4. COMBUSTION EFFICIENCY CALCULATED
70.5 9.0
*.*85 .378
.1*72 .0271

15.* 34.2
2.816 *.133
.1.98 1.080
7.5 5.3
1.371 .640
.Z43 .155

22.9 39.5
4.187 4.773
.7*1 1.155

.00700 .08701
16.90 16.90
.02180 .02103
32.50 28.90
.03521 .03502
43.40 41.01
.0*89* .0*902
1.8.80 1.8.80
35.80 34.30
HET VALUES.
C02,CO,ANO HC DATA
»N02 CALCULATED AS
FROM CO, AND UHC AS
99
0.1
0.0
1.1
993.0
41000.0
53.4
3*8.8
13.8*
2.337
6.72
.0165
265.0
.0162
.237
.381
111
22.7
45.5 _. 	
43.6
989.1
40948.1 	 	 -
55.2
351.1
13..83 __ . ......_.....
2.851
6.52
.1168 . ... _ 	 .._....
275.8
.1163
.248 . 	 _ . ....._ - ._ ....
.363
99.681 99.618 f ,.,,„,

3.39
3.13
830.3

216.0
12.838
3.408

5.7
.192
. 851
.81*9

43.5
4.205
1.114
5.8
.483
.128

48.5
4.689
1.2*2

.01784
28.50
.82111
45.88
.03515
54. ZO
.04917
57.80
45.00

AND FUEL
NO 2 FROM
VAPORIZED
3.4Z
3.13 ... _ 	 	 	 	 •.. — - - - 	
860.5

264.6 _ 	 ... 	
15.412
4.238
. . 	 -...-. - - . . .- .
9.3
.311
.DAS
• «w^ 	 	 	 -.. — . 	 — - — •• - 	 	 — —
.8201

42.0 .. _ 	 	
4.018
1.18$
5.9
.564
-•155 	 . 	 	 	 	 	 	

47.9
4. 582 ......
1.260

.08784 . ._...__-
24.18
.12111
39.80 . . . _ ...... 	 .. . ..
.03514
49.40
.0*921 ......
57.68
43.11
.. _ _ ... -• — 	 	
COMPOSITION.
CONCENTRATIONS HITH MOLECULAR HEIGHT OF N02 (46.111.
ORIGINAL FUEL ON LB/ L 3 FUEL BASIS. 	 _....._- 	 -
-------
Vfi
 >
.791.
.71,1
.U9S
75.72
78.91
71.2M
10.1.8$
9.787
6.582
3.379.
.092
1.155
1.000
189.76
197.95
17.806
.1.83
6.087
5.271
3.1,00
.051
1.2<>2
1.111.
237.30
2*7.06
It. 327
.21<>
5.Z36
>>. 696
<>.238
.085
1.260
1.105
251.72
262.33
16.838
.338
5.006
it. 369
                                                                                                               FUEL^AV.KERO.
                                                                                                                                  P  BARO=  28.71
                         BRAKE  SPECIFIC EMISSION INDEX LB/1000HP-HR
                             CARBON MONOXIDE              0.000
                             UNBURNEO HYDROCARBONS        0.000
                             OXIDES OF NITROGEN           0.000
                             NITRIC OXIDE                 0.000
                             NOTE"0. APPEARING IN BRAKE SPECIFIC EMISSION INDEX COLUMN DENOTES AN IDLE CONDITION
-------
                          ENGINE  HFR.t  AIRESEARCH
                         HOOEc  NO. I   GTCP85-98CK

                         FUEL I  ASTM D16S5-73
 TEST FACILITY I PHX LACCZ       INSTR.  DESCRIP.I   FEDERAL  REG V38 N136    CALC. DATE!
 S/Nt  36197          ENGINE TYPE  ICLASSIt  »PU               CAtC. I.O.I  	3L 	
MAX SUP       280. * BLEcO AIR EXTRACTION TO    1150.  DEG. F EGT                •
    ATOMIC M/C RATIO!   1.928    LHVI     18*78.  BTO/LB.      AOOITIVESt NOME
                                                                                                                                               6-12-75
13
D>
VO
                                    EXHAUST EMISSIONS PER EPA  RATED  WORK OUTPUT •• CODE  OF FEDERAL REGULATIONS TITLE *fl PART 87
                                   ...».....»..»..»»»»»»»»»•»•»»»  EMISSIONS  COMPUTED  FROM  TEST CONDITION NO.  5   ••»»••••••••»»
                                            HYDROCARBONS IHC AS  CH*t              .310 LB. POLLUTANT  PER 1000 HP.-HR.
                                            CARBON MONOXIDE  (COI               16.680 LB. POLLUTANT  PER 1000 HP.-HR.
                                            OXIDES OF NITROGEN (NOX  AS  N02)     *.9fl2 LB. POLLUTANT  PER 1008 HP.-HR.      _
                                                                                                                                    17 JULY 1973
                         ,».»..»»»»»•»»»».»»•»••••»»••*»•»••»»••«•••••»••••»   ENGINE .DESCRIPTION  •••••••••••»«
                         COMBUSTOR TYPEI TANGENTIAL CAM           P/NI   698168-3  SURFACE/VOLUME I  .72SSO.IN/CJ
                         ENGIN^ TOTAL SERVICEI      0.0 HR.    TIME  SINCE ENGINE OVERHAULI      8.8 MR.
                         ENGINE ASSEMBLY AND MAINTENANCE INFORMATIONS
                                                          IN
                         AIRCRAFT INSTALLATION ••» MFR.I
                                                                                      MODEL NO.I
                                                                FUEL INJ. TYPE I
                                                                                                                             USERI
                                                                                    DUAL ORIFICE
GASEOUS EMISSION TEST NO. 1 7 OATEI 6-12-75 TIME! 11*05 BARD. PRESS. 1 28.710 IN. H6A. ' „„„_
AMBIENT AIR TEMP.t 59.0 DEG. F RELATIVE HUHIOITYI 70.00 PERCENT SPECIFIC HUMIOITYI .007500 LB. HZO/LB. DRY AIR
AMBIENT AIR QUALITY HYDROCARBONS (HCI I 0.0 PPMC CARBON MONOXIDE (COI 1 0.0 PPHV OXIDES OF NITROGEN (NOAH 0.8 PPHV
SAMPLE LINE ••» TEMP.I 308.00 DEG. F. FtOHWTEl !*.!(> LITERS/MIN. TRANSPORT TIME! 6.50 SEC. CENGTHI 58.80 FT.
TEST CONDITION
POWER SETTING, CORRECTED HP.
Nl SPEED, RPM
FUEL FLCM (MEAS.) LB./HR.
ENGINE CORE INLET AIRFLOMCCALC. 1 L3./SEC.
COMPRESSOR INLET TEMP., OEG. F
COMPRESSOR DISCHARGE AIR PRESSURE. PSIA
COMPRESSOR DISCHARGE AIR TEMP., OEG. F
COMPRESSOR BLEED AIRFLOH (MEAS.) LB./SEC.
BLEED AIR PRESSURE, PSIA
BLEED AIR TEMPERATURE, OEG. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION, NET ANALYSIS
HYCROCAR30N (HC AS CH*I , PPMC

TOTAL OXIDES OF NITROGEN (NOXI , PPMV
CARBON DIOXIDE (C02I , PERCENT BY VOL.
NITRIC OXIDE (N0>, PPNV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH*I
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02I
EMISSION RATE, L3. POLLUTANT/HR.
HYDROCARBONS (HC AS CH*I
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS N02)
ENGINE HORK OUTPUT, MEAS. SHP
ENGINE WORK OUTPUT, ISENTROPIC AIR HP
ENGINE NORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS)
101 102 103
0.08 78.91 197.86
*1620.DO -,1*50.00 1,1150.00
1*0.00
5.96
61.18
379.00
0.00
0.00
-0.00
*82.0

117.000

15.90(1
1.327
12.100

9.851
36.0*0
3.8*7
1.379
5.0*6
.539
0.00
0.00
0.00
98.29
178.00
5.73
60.10
38*. 00
0.00
0.00
-0.00
602.0

69.000

23.000
1.773
15.880

•..380
30.125
*.196
.780
5.362
.7*7
75.72
0.00
75.72
98.91
.009
2*2.00
5.12
59.0
59.17
391.00
0.00
0.00
-0.00
8*5.0

8.700
191.181
39.500
2.7*1
33.008

.362
13.899
*. 717
.087
3.36*
1.1*2
169.85
189.85
99.6*
.013
10*
0.00
*1030.00
265.08
6.81
58. 0
53.32
3*9.00
2.2*
52.1*
369.00
987.8

6.800
220.390
*8.800
3.376
1,3.900

.203
13.016
*.73*
.05*
3.*i*9
1.255
0.08
237.95
237.95
99.68
.816
105
*5.*9
*0960.«0 	 	 	
27*. Ot
6.59
59«*
55.19
352.01
	 1.97_ 	 	
53.91
372.00



8.700
767.179
*7.800
3.4*%
*2.300


.288
15.**8 	 	 	 - - 	
*.540
. .. .079 	 	 	
*.233
1.2**
*3.65 	 	 . —

210.11 '
253. 75
,99.61 	 	 •
.016
-------
                         .».,........,...,...,.......,,..„.„..,...,.  AIRESEARCH EMISSION TEST SUMMARY  ••»••••••••••»•••••••••••»•••••••••••
                           ENGINE* GTCP85-98CK      S/N* 36197     COM3 P/N= 696168-3 TEST DATE  6-12-75       FUEL-AV. KERO.    P BARO« 28.71
                          RAT SHP=   200.     RA EGT,F= 1150.      RAT SPO- 41600.     OEH PT.F*  50.       REL HUM:  70.00    SPEC HUM' .107508
                         FUEL H/C* 1.9280     STOI F/A* .06822       L H V= 18470.     S LN T,F= 300.8      FLO.L/M*  14.160   SL TIM.S'  6.5880
 fa
-J
O
DATA POINT NUMBER
PERCENT MAX. CORRECTED POMER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., DEG.F
SHAFT SPEED. Nl, RPM
COMPRESSOR OSCHG. PRES..PSIA
COMPRESSOR DSCHG. TEHP,OtG F
EXHAUST GAS PRESS., PSIA
CORRECTED 3uEEO FLOH, LB/SEC
COMPRESSOR MAP FLOH, LB/SEC
FA RATIO BASED ON MAP FLOH
CORRECTED FUEL FLOH , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P»»N/¥/E«T/540l
COMB EFFIC FROM EMISSIONS
101
0.0
8.0
0.1
482.0
41620.0
61.1
379.0
13.67
0.101
6.85
.0064
140.0
.0065
.096
.146
98.288
102
39.5
78.9
75.7
602.1
41450.0
60.1
384.0
13.73
0.080
5.67
.0087
178.0
.0086
.127
.139
98.907
                                                                                103
                                                                               98.9
                                                                              197.9
                                                                              189.9
                                                                              845.0
                                                                            <•! 150.0
                                                                               59.2
                                                                              391.1
                                                                              13.85
                                                                              0.000
                                                                               5.15
                                                                              .0131
                                                                              242.1
                                                                              .1131
                                                                               .192
                                                                               .128
                                                                             99.641
                                                                                          104
                                                                987.
                                                              41030.
                                                                 53.
                                                                349.
                                                                13.84
                                                                2.336
                                                                 6.67
                                                                .0166
                                                                265.0
                                                                .0161
                                                                 .236
                                                                 .143
                                                               99.676
              105
            22.7
            45.5
            43.6
           991.8
         40961.1
            55.2
           352.8
           13.83
           2.151
            6.57
           .1165
           274.1
           .0165
            .241
            .139
          99.611
 CARBON DIOXIDE
     PERCENT BY VOLUME, NET
     LB. C02 PER LB. OF FUEL
     HEIGHT FLOH, LB./HR.
 CARBON MONOXIDE
     PPM BY VOLUME,  HET
     LB. PER 1000 LB. OF FUEL
     HEIGHT FLOH, LB./HR.
 UN3URNED HYDROCARBONS- PPM
     PPM BY VOLUME,  HET
     LB. PER 1000 LB. OF FUEL
     HEIGHT FLOH, LB./HR.
     RATIO LB HC/LB  CO
 NITRIC OXIDE INOI - HEIGHTS AS
     PPM BY VOLUME,  HET
     LB. PER 1100 LB. OF FUEL
     HEIGHT FLON. LB./HR.
 NITROGEN DIOXIDE IN02I
     PPM BY VOLUME,  NET
     LB. PER 1000 LB. OF FUEL
     HEIGHT FLOH, LB./HR.
 TOTAL OXIDES OF NITROGEN
     PPM BY VOLUME,  NET
     LB. PER 1000 LB. OF FUEL
     HEIGHT FLOH, LB./HR.
     SMOKE MEASUREMENT DATA
     CORRECTED HEIGHT FLOH
     SMOKE NUMBER
     CORRECTc.0 HEIGHT FLOH
     SMOKE  NUMBER
     CORRECTED HEIGHT FLCH
     SMOKE  NUMBER
    CORRECTED  HEIGHT  FLCU
    SMOKE NUMBER
    SMOKE NUMBER AT  HAM. 123
                                                                           SUMMARY OF REDUCED EMISSION DATA*
1.33
3.07
429.9
244.7
!L 36.040
5.046
AS CARBON,
117.0
:L 9.851
1.379
.2733
1 AS N02
12.1
L 2.928
.410
3.8
:L .919
.129
1.77
3.09
550.9
271.3
30.125
5.362
HEIGHTS AS
69.0
4.380
.781
.1454

15.8
2.882
.513
7.2
1.313
_ .234
2.74
3.13
757.8
191.2
13.899
3.364
CH4
8.7
.362
.087
.0260

33.1
3.941
.954
6.5
.776
.118
IC*N02t AS NO2
15.9
L 3.847
.539
.00704
15.70
.02112
32.50
.03519
39.80
.84925
45.80
I 31.81
23.1
4.196
.747
.00703
16.91
.12108
31.90
.0350*
41.00
.04912
49.40
35.21
39.5
4.717
1.142
.00702
21.71
.02115
33.71
.03518
39.81
.04911
45.21
35.40
   3.31
   3.13
 830.3

 220.4
 13.016
 3.449

   6.0
   .203
   .054
 .1156

   43.9
 4.259
 1.129

   4.y
   .475
 ..126

   48.8
 4.734
 1.255

 .00702
 24.11
 .12115
 44.61
 .03516
 51.81
.14908
 68.21
 45.60
  3.44
  3.13
 857.3

 267.2
15.448
 4.233

   8.7
  .288
  .879
 .8186

  42.3
 4.117
 1.111

   5.5
  .522
  .143_

  47.8
 4.541
 1.244

.11711
 21.51
.82111
 41.11
.03510
 51.68
.14911
 56.68
 42.68
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE HET VALUES.                     _	
      2.EQUIVALENCE RATIO CALCULATED FROM C02.CO.AND HC DATA AND FUEL COMPOSITION.
      3.MASS EMISSIONS OF NO, H02, AND N3+N02 CALCULATED AS N02 FROM CONCENTRATIONS KITH MOLECULAR
      4.COMBUSTION  EFFICIENCY CALCULATED FROM CO,AND UHC AS VAPORIZED ORIGINAL FUEL ON LtV LB FUEL
                                                                                                                           HEICHT OF NO*
                                                                                                                           MSIS*
-------
(D
~J
ENGIMt« GTCP85-9SCK S/N= 36197
DATA POINT NUMBER
EMISSION RATE LB/HR
CARBON MONOXIDE
UNBURNEO HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXI3E
POWER LEVEL HP
TOTAL CORRECTED HORSEPOHER
BRAKE SPECIFIC EMISSION INDEX
CARBON MONOXIDE
UNBURNcD HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIDE
101

5.046
1.379
.539
.

3.M.9
.OS*
1.255
1.129
237.95
2«.7.7i.
6-12-7$ • FUEL=AV. HERO. P BARO» 26.71
185

I..Z33 . ..__....
.079
1.2<»»
l.lil ...... • ... 	
253.75
26%. 45
L3/HOOMP-HR . 	 	 . . _
a.oao
0.090
g.ooo
o.oao
KOTE"0. APPEARING IN BRAKE SPECIFIC
70.818
10.297
9.861.
6.776
EMISSION
17.717
.%61
6.013
5.023
1<>.<.96
.226
5.272
I..71.3
INDEX COLUMN DENOTES
16.680
.311
*.902 	
4.338
AN IDLE CONDITION
                                                                                                                                                                                                         t>
-------
0)
10
                          ENGINE MFR.I AIRESEARCH
                         MODEL NO.I  GTCPS5-9BCK

                         FUEL I ASTM 01655-73
 TEST FACILITYI PHX LACC2        INSTR.  DESCRIP.I   FEDERAL REG V38 N136
 S/NI  36179          ENGINE  TYPE  (CLASS) 1   APU              CALC. I.D.I
MAX SHP       200. » BLEED  AIR EXTRACTION  TO    1150. DEC. F EGT
    ATONIC M/C RATIOI   1.9Z«   LHVI      181.70.  BTU/LB.      ADDITIVES! NONE
                                                                                                                                   CALC.  OATEI  6-12-75
                                    EXHAUST EMISSIONS ?ER  EPA  RATED  WORK OUTPUT •» CODE OF FEDERAL REGULATIONS TITLE  40  PART 87
                                   ..............................  EMISSIONS COMPUTED FROM TEST CONDITION NO.  5    »••»»••»••»»•»
                                            HYDROCARBONS  CMC AS  CH4)              .,29  LB. POLLUTANT PER 1000 HP.-HR.
                                            CARBON MONOXIDE  (CO)                17.511  LB. POLLUTANT PER 1000 HP.-HR.
                                            OXIDES OF'NITROGEN INOX  AS N02>     4.623  LB. POLLUTANT PER 1000 HP.-HR.
                                                                                                                                     17  JULY 1973
                         [[[  ENGIN£ DESCRIPTION  •»»•»••»»»..»*..
                         COMBUSTOR TYPE! TANGENTIAL CAN           P/Nt  69«16d-3  SURFACE/VOLUME!  .725 SQ  IN/CJ  IN
                         ENGINE TOTA* SERVICE!      0.3 HR.    TIME SINCE ENGINE OVERHAUL!      0.0 HR.
                         ENGINE ASSEMBLY AND MAINTENANCE  INFORMATION!
                         AIRCRAFT INSTALLATION •»» MFR. !
                                                                                      MODEL NO.I
                                                                FUEL INJ. TYPEI
                                                                                                                              USER I
                                                                                    DUAL  ORIFICE
                         GASEOUS EMISSION TEST NO. I      ft     OATEI  fc-12-75      TIME!    13.1.5      3ARO.  PRESS.!   24.71H IN.  HGA.
                         AMBUNT AIR TEMP. I 59.0   DEC.  F        RELATIVE HUMIDITY!  95.00 PERCENT        SPECIFIC  HUMIDITY!  .010000  LB. H20/LB. DRY AIR
                         AMBIENT 1IR QUALITY    HYDROCi^BONS (HCII 0.0   PPHC    CARBON HONOXIO:  (CO)I  0.0    PPMV    OXIDES OF  NITROGEN (NOXII 0.0   PPHV
                         SAMPLE LINE »»• TEHP.I  300.03  OEG. F.      FLOW^ATEI   m.16 tlTE^S/MIN.     TRANSPORT TIME!    6.50 SEC.      LENGTH!  '50.00 FT.




1


)


)


)


)


1


)


)


)


}
TEST CONDITION
POWER SETTING, CORRECTED HP.
Nl SPEED, RPM
FUEL FLCU (MEAS.I LB./HR.
cNGINc CORE INLET AIRFLOW (CALC. 1 LB./SEC.
COMPRESSOR INLET TEMP., OEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP., OEG. F
COMPRESSOR BLEED AIRFLOW (MEAS. ) LB./SEC.
BLEED AIR "RESSURE, PSIA
BLEED AIR TEMPERATURE. OEG. F
ENGINE EXHAUST GAS TEMP., DEG. F
EMISSICK CONCENTRATION, WET ANALYSIS
HYDROCARBON (HC AS CH4) , PPMC
CARBON MONOXIDE (CO) , PPMV
TOTAL. OXIDES OF NITROGEN (NOXI , PPMV
CARBON DIOXIDE (C02), PERCENT BY VOL.
NITRIC OXIDE (NOI , PPNV
EHISSIOK INDEX, IB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02I
EMISSION RATE. LB. POLLUTANT/MR.
HYDROCARBONS (HC AS CH4I
CARSON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
ENGINE WOR< OUTPUT, MEAS. SHP
ENGINE WGft< OUTPUT. ISENTROPIC AIR HP
ENGINE WOR< OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/t (EMISSIONS)

106 107 108
0.00
41590.00
143.00
6.01
61.0
61.23
371.00
0.00
0.00
-0.00
478.0

132.000
2-7.140
15.000
1.343
8.100

10.967
35.925
3.562

1.568
5.137
.512
1.00
0.10
0.88
91.19
.(•7

76.76
41410.00
176.00
5.75
60.0
60.66
371.00
0.00
0.00
-0.00
568.0

75.000
273.608
22.100
1.765
14.000

4.762
30.544
4.050

.851
5.437
.721
75.65
0.10
75.65
90.86
.009

197.57
41090.00
246.00
5.27
59.0
59.66
379.00
0.00
0.00
-0.00
843.8

10.500
157.699
38.000
2.703
33.000

.442
14.566
4.600

.109
3«56J»
1.132
169.50
0.00
189.50
99.62


109
0.08
40960.00
265.00
6.61
59.8
53.27
336.01
2.30
52.00
359.00
1000.6

6.000
222.387
47.900
3.419
43.008

.200
12. 964
4.586

.053
3.435
1.216
0.00
235.17
235.17
99.60
.(16

110
45.35
40880.00
272.01
6.60
60.1
55.24
341.00
2.02
54.11
361.00
995.0

12.000
279.963
45.000
3.451
40.801

.396
16.152
4.264

.106
4.393
1.160
-------
U)
ENGINE- GTCP85-96CK S/N* 36179 COMB P/N= 698168-3
RAT SHP» ZOO. RA EGT,F= 1150. RAT SPO* 41600. (
FUEL H/C= 1.9Z80 STOI F/A= .06822 L H V= 18470. !
DATA POINT NUMBER 106 107 108
PERCENT MAX. CORRECTED POHER 0.0 39.4 98.
CORRECTED SHAFT HP 0.0 78.8 197.
MEASURED SHAFT HP 0.0 75.6 189.
EXHAUST GAS TEMP., OEG.F 478.0 588.0 843.
SHAFT SPEED, Nl, RPM 41590.0 41410.0 41090.
COMPRESSOR OSCHG. PRES..PSIA 61.2 60.9 59.
COMPRESSOR OSCHG. TEHP.DEG F 371.0 371.0 379.
EXHAUST GAS PRESS., PSIA 13.66 13.73 13.85
CORRECTED BLEED FLOH. LB/SEC 0.000 0.000 0.000
COMPRESSOR MAP FLOH, LB/SEC 6.10 5.72 5.20
FA RATIO BASED ON MAP FLOH .0065 .0086 .0131
CORRECTED FUEL FLOH , LB/HR 143.0 178.0 246.0
FA RATIO CALC. FROM EMISSION .0066 .0086 .0130
EQUIVALENCE RATIO .097 .126 .190
LOADING H/P«»N/V/ECT/54fl» .392 .371 .345
COMB EFFIC FROM EMISSIONS 98.193 98.862 99.618
CARBON DIOXIDE
PERCENT BY VOLUME, HET 1.34 1.76 2.70
L3. C02 PER LB. OF FUEL 3.07 3.09 3.13
HEIGHT FLOH, LB./HR. 438.6 550.5 770.0
CARBON MONOXIDE
PPM BY VOLUME, HET 247. 1 273. 8 197.7
LB. FER 1000 LB. OF FUEL 35.9Z5 30.544 14.568
HEIGHT FLOH, LB./HR. 5.137 5.437 3.584
UNBURNEC HYDROCARBONS- PPM AS CARBON, HEIGHTS AS CH4
PPM BY VOLUME, HET 132.0 75.0 10.5
L3. PER 1000 LB. OF FUEL 10.967 4.782 .442
HEIGHT FLOH, LB./HR. 1.568 .851 .109
RATIO LB HC/LB CO .3053 .1566 .0304
NITRIC OXIDE INO) - HEIGHTS AS NOZ
PPM BY VOLUHE. HET 8.1 14.0 33.0
LB. PER 1000 LB. OF FUEL 1.934 2.565 3.994
HEIGHT FLOH, LB./HR. .277 .457 .983
NITROGEN DIOXIDE  LN T,F>
119
0.0
0.0
0.0
1000.0
40960.0
53.3
336.0
13.84
2.396
6.68
.0168
265.0
.0163
.239
.304
99.677
REDUCED
3.42
3.13
830.3
222.3
12.964
3.435
6.0
.ZOO
.053
.0154
43.0
4.119
1.092
4.9
.469
.124
47.9
4.588
1.216
.00698
25.90
.02094
46.40
.03485
55.40
.04879
65.18
48.80
E 6-12-75 FUEL-AV. KERO. P BARD* 28.71
57. REL HUM' 95.10 SPEC HUM' .110111
= 300.0 FLO.L/M* 14.160 SL TIN.S' 6.5000
in 	 " " " 	 " ' ;
22.7
45 4 '
43.6 •--•••-
995.0
40880.1
55.2
341.0
13.84 	 ......
2.107
6.62
.0164
272.1
.0165 :
!374 ' ~ ~ " " """ " ' " " "|
99. 585 :
I
3. 45
3.13 .... 1
850.7
zsfl.i 	 . _ . _;
16.152
4.393
12. 1
.396
.116 i
.0245
40.1 I
3.866 j
1.052
4.2 • !
.398
.. . .108 	 	 LJ
45.1
4.264
1.160 >
.00691
24.11
.02094
42.20 >
.03487
50.10
.04881 >
61.40
45.01
                             2.EQUIVALENCE RATIO CALCULATED FROM C02,CO,ANO HC DATA AND FUEL COMPOSITION.
                             3.MASS EMISSIONS OF NO, N02, AND NO+N02 CALCULATED AS NOZ FROM CONCENTRATIONS MITH  MOLECULAR HEIGHT OF  NOZ  (46.111.
                             4.COMBUSTION EFFICIENCY CALCULATED FROM CO,AND UHC AS VAPORIZED ORIGINAL FUEL ON LB/ LB FUEL BASIS.	
-------
                                                                  •»»»   AIRESEARCH EMISSION TEST SUMMARY
                                                                   COMB P/N= 69816S-3 TEST DATE  6-12-75
                                                                      107
                                                                                108
                                                                                          109
                                                                                                    110
  ENGINE- GTCP85-98CK      S/N-  36179
DATA POINT NUMBER                   1)6
EMISSION RATE LB/HR
    CARBON MONOXIDE               5.137
    UNBURNED HYDROCARBONS         1.568
    OXIDES OF NITROGEN             .512
    NITRIC OXIDE                   .277
POHER LEVEL HP                    0.00
TOTAL CORRECTED HORSEPOWER        0.09
BRAKE SPECIFIC EMISSION INDEX L3/1000HP-HR
    CARBON MONOXIDE               0.000
    UNBURNEO HYDROCARBONS         0.000
    OXIDES OF NITROGEN            0.090
    NITRIC OXIDE                  0.000
    NOTE"fl. APPEARING IN BRAKE  SPECIFIC  EMISSION INDEX COLUMN DENOTES AN IDLE CONDITION
                                                                                                                FUEL=AV.  KERO.
                                                                                                                                  P BARO= 28.71
5.437
.851
.721
.-.57
75.65
78.76
71.873
11.253
9.529
6.037
3.58<>
.109
1.132
.983
189.58
197.57
18.904
.57*
5.969
5.183
3.1(35
.053
1.216
1.092
235.17
2 1,5. 08
14. 608
.ZZ5
5.170
4.641
4.393
.108
1.160
1.052
250.88
261.62
17.511
.4Z9
4.623
4.192
(D
                                                                                                                                                                     ,10
-------
                        ENGINE HFR. I AIRESEARCH
                       MODEL NO.I  GTCP65-98CK

                       FUEL I ASTH 01655-73
 TEST FACILITY I PHX LACCZ        INSTR.  OESCRIP.I   FEDERAL REG V38 N136    C»LC. DATEI
 S/NI  36179          ENGINE  TYPE  (CLASS)I  APU              CALC. I.D.I     Z
MAI SHP       200. * BLEED  AIR EXTRACTION  TO    1150. D£G. f EGT
    ATOMIC H/C RATIOI    1.938    LHVI      181.78.  BTU/LB.     AOOITIVESI NONE
6-1Z-75
                                  C.XHAUST EMISSIONS  PER  EPA  R4TEO HORK OUTPUT *» CODE OF FEOERA.. REGULATIONS TITLE  40 PART 87
                                 ........I..................... EMISSIONS COMPUTED FROM TEST CONDITION NO.  5    »»»•».».»»»»..
                                          HYDROCARBONS  (HC AS  CHI, I              .375  .8. POLLUTANT PER 1000 HP.-HR.
                                          CARBON MONOXIDE  (COI                17.160  LB. POLLUTANT PER 1100 HP.-HR.
                                          OXIDES OF  NITROGEN (NOX AS N02>     it.738  LB. POLLUTANT PER 1000 HP.-HR.
                                                                                                                                   17 JULY 1973
                       I....,.*.................,...........................  £NGINE DESCRIPTION  ••»»•»•»•»•»••••
                       CONBUSTCR TYPE1 TANGENTIAL CAN           P/Ni  698168-3  SURFACE/VOLUME I   .725 SQ IN/CU  IN
                       ENGINE TOTAL SERVICE*      0.0  H
76.13
0.00
76.13
98.69
.009
197.76
1.1090.00
21,2.00
5.22
56.0
59.75
380.10
o.ot
0.00
-0.10
81.2.0

10.500
200.505
36.500
2.667
33.000

.1.1.5
li.. 861
1..6B7

.101
3.596
1.131,
189.56
0.00
119.58
99.61
.013
111.
0.11
1,0951.11
266.01
6.77
60.1
53.03
331.110
2.30
52.15
361.11
1013.0

5.700
215.616
1,9.200
3.1.63
i.S.000

.111
12.V19
<>.655

.151
3.303
1.231
1.10
231.. 90
23k. 90
99.69
.117
115
i>5.33
.4,0910. 10 	 	 	 	
272.11
6.61
61.1 . .. .. _
55.24
342.11
Z.K 	 	 	 	
53.91
363.01
1002.1

10.501
271,. 63«, 	 	
1.6.201
3.1.51
<>1.60I .. . . 	 	 	 . . . .. _

.346
15.151 _ . _. 	 	
4.379

... -.194 . _ __ ..___'._ 	 	
4.313
1.191
43.51 	 	 	 ...:_.... 	 . ...
217.71
251.16
99.61
.016
                                                                                                                                                                     J?
-------
(D

~J
cn
•)


ENGINE: GTCP85-98CK S/M= 36179
RAT SHP* 200. RA FET.Fc 11«0.









)
)


)



)

)

)
FUEL H/C= 1.9288 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POWER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., DEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR OSCHG. PRES. ,PSIA
COMPRESSOR OSCHG. TEMP, DEC F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOH, LB/SEC
COMPRESSOR MAP FLOH, LB/SEC
FA RATIO BASED OH MAP FLOH
CORRECTED FUEL FLOH , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P»»N/V/E IT/540)
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
LB. CC2 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, HET
L8. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, NET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC CXIOE (NO) - HEIGHTS AS
PPM BY VOLUME, HET
LB« PEA 1000 LB OF FUeL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE IN02)
PPM BY VOLUME, HET
.06822
111
0.0
0.
0.
476.
41590.
61.
370.
13.66
0.000
6.07
.0064
140.0
.0065
.096
.389
98.234

1.33
3.87
429.6
346.3
36.136


I HPS
113
39.6
79.3
76.1
595.1
41410.0
60.6
376.0
13.73
8.000
5.77
.0086
178.0
.00)6
.127
.374
98.885

1.77
3.09
550.7
273.3
30.344
5.058 5.411
CARSON. HEIGHTS AS
124. 5
10.444
1.462
.2891
NOZ
11.0
2. 652
.371
4.4
LB. PER 1000 LB. OF FUEL. 1.061
HEIGHT FLOH, LB./HR.- .149
TftTAI nv TnC"C ftc urrcnrf u *UM..US«<** • *• *.
 2.EQJIVA..ENCE RATIO CALSU.ATED FROM C02.CO.ANO HC DATA ANO FUEL COMPOSITION.
 J.HASS EMISSIONS OF HC, NOZ, ANO NO»NOZ CALCULATED AS «0* FROM CONCENTRATION
*.CO«e«STION EFFICIENCY CALCULATED FRON C0.4NO UHC AS          CONCENTRATION.
CONCENTRATIONS MITH MOLECULAR HEIGHT OF NOZ I4t.UI.
 OUCINAL  FUEL ON IB/ L0 FUEL MSIS,
                                                                                                                                                              •Jg
                                                                                                                                                               -1Q
-------
                                                                                                                                                                        V
ENGINE' GTCP85-96CK S/N= 36179 COMB P/N* 698168-3 TEST DATE 6-12-75
DATA POINT NUMBER
EMISSION RATE LB/MR
CARBON MONOXIDE
UNBURNEO HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIDE
POHcR LEVEL HP
TOTAL CORRECTED HORSEPONER
BRAKE SPECIFIC EMISSION INDEX
CARBON MONOXIDE
UNBURNED HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIDE
111

5.058
l.<>62
.520
.371
0.00
0.00
L3/1DOOHP-HR
0.000
0.000
0.000
0.000
112

5.1*01
.613
.71U
.
1.191
1.078
251.36
262.28

17.160
.375
It. 738
I..287
                                                                                                                 FUEL*AV.  KERO.
                                                                                                                                    P  BARO« Z6.71
                             NOTE»»8. APPEARING  IN  BRAKE SPECIFIC EMISSION INDEX  COLUMN DENOTES AN IDLE CONDITION
 pj
vQ
 (D
-------
                         ENGINE MFR.I AIRESEARCH
                        H03EL NO.I  GTCP85-98CK
                        FUEL I ASTM 01655-73
                               TEST  FACILITY I  PMX  LACC2       INSTR. OiSCRIP.I FEOERA. REG  V38 N136     CALC. DATEI
                               S/Nt    36197          ENGINE TYPE I CLASS)« APU                C4LC.  I.O.I      3
                              HAX  SHP       200.  » BLEED AIR EXTRACTION TO    1150. OEG. F  EGT
                                   ATONIC  H/C RATIOI    1.928    LHVI     18<»70. BTU/L8.      AOOITIVESI NONE
6-13-75
(D

^1
CO
                                   EXHAUST EMISSIONS PER EPA  RATEJ  MORK  OUTPUT  »»  COOE OF FEOERA,. REGULATIONS TITLE 40 PART 87
                                  .............................. £MISSIONS  COMPUTED FROM TEST CONDITION NO.  5   »•••»••••»«•••
                                           HYDROCARBONS IMC AS CH4)              .398  LB. POLLUTANT PER 1800 HP.-HR.
                                           CARBON MONOXIDE ICOI               17.239  LB. POLLUTANT PER 1000 rtP.-HR.
                                           OXIDES OF NITROGEN (NOX  AS  N02I      -..670  LB. POLLUTANT PER 1000 HP.-HR.
                                                                                                            17  JULT  1973
[[[  £N6INe DESCRIPTION  .............
COMBUSTOR TYPEI TANGENTIAL CAN           P/NI   698168-3  SURFACE/VOLUME I  .725 SQ IN/CU
ENGINE TOTAL SERVICEI      0.0 MR.    TIME  SINCE  ENGINE OVERHAUL 1       0. HR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATIONI
                                                                                                                IN
                        AIRCRAFT INSTALLATION •»• NFR. 1
                                                                                     MODEL NO. 1
                                                                                                                      FUEL INJ. TYPES
                                                                                                                            USER!
                                                                                                                                          DUAL  ORIFICE
                        .................................,..»...,..»..,.0pERATIONSL T£ST 0&TA SUNMA(?y ................................................

                        GASEOUS EMISSION TEST .NO.I     a    DATEI   6-13-75       TIMEI      8.25      BARO. PRESS.!  28.740 IN. H6A.
                        AMBIENT AIR TEMP.I 59.0  DEG. F         RELATIVE HUMIDITY I   95.00 PERCENT       SPECIFIC HUMIDITY!  .010000 LB. H20/LB.  DRY  AIR
                        AMBIENT AIR QUALITY    HYDROCARBONS (HOI  0.0   PPMC     CARBON MONOXI3£ (COM 0.0   PPMV    OXIDES OF NITROGEN (NOX)I  0.0    PPMV
>
•>







)


)


,


)


)


)








SAMPLE LINE ••• TEMP. 1 300.00 DEG. F. FLOKRATE 1 14.16 LlTERS/MIN. TRANSPORT TIMEI 6.50 SEC. LENGTHI 50.08 FT.

TEST CONDITION
POMER SETTING, CORRECTED MP.
Nl SPEED. RPH
FUEL FLCN (MEAS.) LB./HR.
ENGINE CORE INLET AIRFLOH (CALC. ) LB./SEC.
COMPRESSOR INLET TEMP., OEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP., OEG. F
COMPRESSOR BLEED AIRFLON (MEAS.) LB./SEC.
BLEED AIR PRESSURE. PSIA
BtEED AIR TEMPERATURE, OCG. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION, MET ANALYSIS
HYDROCARBON (HC AS CH4I . PPMC
CARBON MONOXIDE (CO) , PPMV
TOTAL OXIDES OF NITROGEN (NOX) , PPMV
CARBON DIOXIDE (C02I, PERCENT BY VOL.
NITRIC OXIDE (NOI , PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (NC AS CH4I
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
ENISSIOK RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4I
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02I
ENGINE WORK OUTPUT, MEAS. SHP
ENGINE NORK OUTfUT, ISENTROPIC AIR HP
ENGINE HORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS!
116 117 118
0.00
41600.00
11(3.00
6.03
58.0
61.96
371.00
0.00
0.00
-0.80
475.0

124.500
2 41.. 179
14.500
1.339
10.000

10.383
35.626
3.475

1.485
5.095
.497
0.00
0.08
0.80
98.25
.887
76.71
41.70.00
178.00
5.75
61.0
60.98
577.00
0.00
0.00
-0.00
591.0

76.500
261.. 644
21.800
1.765
1-..100

4.880
29.535
3.996

.869
5.257
.711
75.76
0.00
75.76
96.66
.669
197.46
41150.00
246.00
5.20
60.0
60.00
383.00
0.00
0.00
-0.00
841.0

9.908
199.101
37.200
2.741
31.900

.411
14.470
4.441

.101
3.560
1.093
169.85
0.66
189.65
99.62
.813
119
o.oo
41020.00
270.00
6.82
61. 0
53.76
340.00
2.31
52.29
361.00
1800.0

5.700
217.999
46.000
3.482
43.000

.187
12.486
4.517

.050
3.372
1.228
6.00
235.81
235.81
99.69
.017
120
45.55
40920.00
278.06
6.52
68.8
55.48
342.08
2.02
54.26
362.80
1008.8 	

11.400
282.571 .. 	
46.606
3.596
41.900

.361
15.647
4.239

.106 _ „
-------
                                                                                                                                                                      >
                                                                                                                                                                       «*-
LQ
 ro
ENGINE* GTCP85-98CK S/N= 36197
RAT SMP* ZOO. RA EGT,F«
FUEL H/C= 1.9280 STOI F/As
DATA POINT NUMBER
PERCENT MAX. CORRECTED POWER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OEG.F
SHAFT SFEED, Nl , RPM
COMPRESSOR 3SCHG. PRES..PSIA
COMPRESSOR OSCHG. TEMP, DEC F
EXHAUST GAS PRESS., PSIA
CORRECTED 3LE.ED FLOM, L8/SEC
COMPRESSOR HAP FLOM.LB/SEC
FA RATIO EASED ON MAP FLOM
CORRECTED FUEL FcOM , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING M/P»»N/V/ECT/540I
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
L3. C02 PER 1.8. OF FUEL
MEIGHT FLOM, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, MET
L3. PER 1000 LB. OF FUEL
MEIGHT FLOW, LB./HR;
UN3URNEC HYDROCARBONS- -PPM AS
PPM 3Y VOLUME, MET
L3. PER 1300 LB. OF FUEL
MEIGHT FLOM, LB./HR.
RATIO -8 HC/LB CO
NITRIC OXIDE (NO! - HEIGHTS AS
PPM BY VOLUME, MET
La. PER 1300 LB. OF FUEL
MEIGHT F..OM, LB./HR.
NITROGEN DIOXIDE CN02I
PPM BY VOLUME, NET
L3. PER 1000 LB. OF FUEL
MEIGMT FLOM, LB./HR.
1150.
.06832
116
0.0
0.0
. 0.0
475.0
416*00.0
62.0
371.0
13.68
0.000
6.10
.0065
143. C
.0066
.097
.384
98.251

1.34
3.07
438.9

244. Z
35.626
5.095
CARBON,
1Z4.5
10.383
1.485
.2914
NO 2
10.0
2.397
.343

4.5
1.079
. 1SL
COM3 P/N« 698168-3 TEST DATE 6-13-75 FUEL-AV.KtRO. P BARO« 28.74
RAT SPO>
L H »=
117
39.4
78.7
75.8
591.0
-*1*70«0
61.0
377.0
13.75
0.000
5.7Z
.OCB6
178.0
.0086
.126
.366
98.877

1.76
3.09
550.8

264.6
29.535
5.257
HEIGHTS AS
76.5
4.880
.869
.1652

14.1
2.585
.460

7.7
1.412
.751
TOTAL OXIDES OF NITROGEN (NC+NOZI AS NOZ
PPM BY VOLUME, MET
L8. PER 1000 LB. OF FUEL
MEIGHT FLOM, uB./HRf
SMOKE MEASUREMENT DATA
CORRECTED WEIGHT FLCM
SMOKE NUMBER
CORRECTED MEIGHT FLOM
SMOKE NUMBER
CORRECTED WEIGHT FLCM
SMOKE NUMBER
CORRECTED MEIGHT FLCN
SMOKE NUMBER
SHOKE NUMBER AT MA=0.023
NOTES i. ALL EMISSIONS CONCENT
14.5
3.475
.497

.00701
16.90
.021*4
32.50
.03507
42.20
.04907
48. ZO
35.30
21.8
3. 996
.711

.00703
19.30
.02108
37.30
.03511
4». 60
.04916
51.80
39.60
41600.
18470.
118
98.7
197.5
189.9
841.0
-.1150.0
60.0
383.0
13.87
0.000
5.20
.0131
246.0
.0131
.193
.339
99.624

2.74
3.13
770.0

199.1
14.470
3.560
CH4
9.9
.411
.101
.0284

31.9
3.808
.937

5.3
.633
.156

37. Z
. . , d
1.093

.00701
15.70
.02103
31.30
.03509
42. ZO
.04912
48. ZO
34.70
DEM PT.Fi
S LN T.F*
119
D.O
0.0
0.0
1000.0
41020.0
53.8
340.0
13.86
2.404
6.74
.0169
270.0
.0166
.243
.379
99.690
OF REDUCED
3.48
3.13
846. Z

218.0
12.488
3.37Z

5.7
.187
.050
.0149

43.0
4.046
1.992

5.0
.470
.127

48.0
4.517
1.220

.00702
26.50
.02105
45.80
.03499
55.40
.04897
61.40
47.70
RATIONS ARE NcT VALUES.
57. REL HUM' 95.00 SPEC HUH' .010000
300.0 FLO.L/H' 14.160 SL TIM,S« 6.5000
120
22.
45. 	 ........ 	
43.
1008.
409ZO. .._....._..
55.5
342.0
13.85 	 	 _....... 	 . . .
2.110
6.6Z
.0168 ._
278.0
.0172
.252 	 _
.379
99.600

3.60
3.13
B69.7

282.6 ......
15.647
4.350

11.4
.361
.100 _... 	 	 ... 	 . 	 .
.0231 .

41.9 . _ 	 _. 	 	 . .. : 	 — 	
3.811
1.059

4.7
.427
.119 . . .. . ... - . 	 . ..

46.6
4.239
1.178

.00701 ....... . _ . .
22.99
.02102
43.49 . ... . . . .._. 	
.03501
53.00
.04899 . __• . . . 	 	
60. ZO
45.40

r rtMoncTTTnu .
                                                                                                                                                                       );


                                                                                                                                                                       y
                              Z.EQUIVALENCE  RATIO CALCULATED FROM C02.C3.AN3 HC DATA  AND FUEL  COMPOSITION.

                              3.MASS  EMISSIONS Of NO, NOZ, AND NO+N02 CALCULATED  AS NOZ  FROM CONCENTRATIONS MITH MOLECULAR MEIGMT OF NOZ (46.011.

                              4.COMBUSTION EFFICIENCY CALCULATED FROM CO,AND UHC  AS VAPORIZED  ORIGINAL  FUEL ON LB/ L8 FUEL BASIS.
-------
                          ENGINE:  GTCP8S-98CK
                        OAT* POINT NUMBER
                        EMISSION RITE LB/HR
                            CARBON MONOXIDE
                            UNBURNEO HYDROCARBONS
                            OXIDES OF NITROGEN
                            NITRIC OXIDE
                        PONER  LEVEL HP
                        TOTAL  CORRECTED HORSEPOWER
                                                    S/N=
36197
  116

5.095
1.1.85
 .1.97
 .31.3
0.00
0.00
••»•  AISEiEARCH EMISSION  TEST  SUMMARY
 COMd P/N= 698168-3  T£ST DATE   6-13-7S
                        119
   117

 5. 357
  .869
  .711
  .1.60
75.76
76.71
                                                                                                                 FUEL=AV.KERO.
                                                                                                                                           28.7k
    118

  3.560
   .111
  1.893
   .937
1*9.65
197.1.6
                       3.372
                        .050
                       1.22C
                       1.092
                    235.81
                         BRAKE  SPECIFIC EMISSION INDEX LBSlOOOnP-HR
                            CARBON MONOXIDE              0.000    69.397     18.750    1<>.Z99
                            UNBURNEO MYOROCARBONS        0.000    ll.<»66       .S3]      .211.
                            OXIDES OF NITROGEN           0.000      9.390      5.75<.     5.172
                            NITRIC OXIDE                 0.000      6.073      "..935     U.633
                            HOTt"0. APPEARING IN BRAKE SPECIFIC  EMISSION INDEX COLUMN DENOTES
    120

  I.. 350
   .100
  1.178
  1.059

262.85

 17.239
   .398
  1..670
  ».199
AN IDLE CONDITION
 13
 0)
VQ
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 00
 O
                                                                                                                                                                        jg
                                                                                                                                                                       .'JO.
-------
                       EMGINt HFR. 1 AIRESEARCH
                      HOOEL NO.I  GTCP15-9ICK
                      FUELI ASTM 01655-73
 TEST FACILITYI PHX LACC2        INSTR.  OtSCRlP.I   FEDERAL
 S/N!  36179          ENGINE  TYPE  (CLASS)t  APU
MAX SHP        200. »  BLEED  AIR EXTRACTION TO    1151. DEC.
    ATONIC H/C RATIO!    1.928    LHVI      18470.  8TU/LB.
                                                                                           REG. V38 N136 CALC.  DATEI
                                                                                            CALC.  I.O.I     1
                                                                                          F EGT
                                                                                            ADDITIVES! NONE
                                                                                                                                             6-5-75
                                 EXHAUST EMISSIONS  PER  EPA RATED WORK OUTPUT »» CODE OF FEDERAL REGULATIONS TITLE 40 PART 07
                                 .............................. £MISSIONS COMPUTED FROM TEST CONDITION  NO.  5    •••»••»•••»»»»
                                         HYDROCARBONS  (HC AS CH4)             .298  LB. POLLUTANT PLR  1800 HP.-HR.
                                         CARBON MONOXIDE (CO)                12.951  LB. POLLUTANT PER  1000 -IP.-MR.
                                         OXIDES OF  NITROGEN (NOX AS N02)     5.203  1.8. POLLUTANT PER  1DOO 4P.-HR.
                                                                                                                                  17 JULY 1973 ••••••••••
[[[  £NG1Nl; QESCRIPTION  •»»••••••»»»••••
COM3USTOR TYPEI TANGENTIAL CAN           P/NI 698166-3   SURFACE/VOLUME!   .725 SQ  IN/CJ  IN
ENGINE TOTAL SERVICE!   0.0    HR.    TIME SINCE ENGINE OVERHAUL!      0.0 HR.
ENGINE ASSEMBLY AND MAINTENANCE  INFORMATION!
                      AIRCRAFT INSTALLATION •••  HFR. t
                                                                                   MODEL NO.I
                                                                                                                     FUEL INJ. TYPEI
                                                                                                                           USERi
                                                                                                                                         DUAL ORIFICE
13
...............«».»»....»»»».»»»»«.».»,»»»...»..OPERATION4L T£SI OATA SUMMARY •••»•••••»••••*•»•••••••»••••••••••••»••••••••••
GASEOUS EMISSION TEST NO.I     9     DATE!   6-5-75       TIME!    7.00       BARO. PRESS.!   28.610  IN.  HG*.
AMBIENT AIR TEMP.I 91.0  DEC. F         RELATIVE HJHIDITYI  32.00 PERCENT       SPECIFIC HUMIBITTI   .010000  LB.  H20/LB.  DRY AIR
AMBIENT AIR QUALITY    HYDROCARBONS  (HOI  0.0    PPMC    CARBON MONOXIDE  (CO)I 0.0   P3MV     OXIDES OF  NITROGEN  (NOXII  0.0   PPNV
SAMPLE LINE ••• TEMP.I  300.00 DEC.  F.      FLOURATEI   14.16 LITERS/HI*.     TRANSPORT TIME I     6.50  SEC.     LENGTHI    50.00 FT.
(D

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TEST CONDITION
PONER SETTING, CORRECTED HP.
Nl SPEED, RPM
FUEL FLOH (MEAS.I LB./HR.
ENGINE CORE INLET AIRFLOW (CALC .) LB./SEC.
COMPRESSOR INLET TEMP., DEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TcMF., OEG. F
COMPRESSOR BLEED AIRFLOW IMcAS.) LB./SEC.
BLEED AIR PRESSURE, PSIA
BLEED AIR TEMPERATURE, CEG. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION. NET ANALYSIS
HYDROCARBON (HC AS CH4) , PPNC
CARBON MONOXIDE (CO), PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPMV
CARBON DIOXIDE (C02) , PERCENT BY VOL.
NITRIC OXIDE (NO), PPNV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4I
CARBON HONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
EMISSION RATE, LB. POLLUIANT/HR.
HYDROCARBONS (HC AS CH4I
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS N02I
ENGINE WORK OUTPUT, MEAS. SMP
ENGINE WORK OUTPUT, ISENTROPIC AIR HP
ENGINE WORK OUTPUT, TOTAt. HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS)
121 122 123
0.00
41740.00
140.00
6.02
91.0
60.39
397.00
0.00
0.00
-0.00
401.0

123.000
232.442
14.000
1.314
5.300

10.455
34.566
3.420

1.464
4.839
.479
0.00
0.00
0.00
98.27
.006
79.92
41610.00
169.00
5.58
91.0
58.72
431.00
0.00
0.00
-0.00
659.0

69.000
25».593
21.000
1.729
12.000

4.494
£9.010
3.931

.759
4.903
.664
78.74
0.00
78.74
98.92
.008
198.55
41250.00
244.00
5.28
91.0
59.90
408.00
0.00
0.00
-0.00
829.0

18.000
262.119
36.500
2.671
29.500

.765
19.494
4.459

.187
4.756
1.068
195.63
0.00
195.63
99.47
.013
124
0.00
41110.00
270.00
6.42
92.0
50.82
369.00
2.24
49.44
389.00
1063.0

4.500
189.790 .
54.500
3.771
50.000

.136
10.051
4.741

.037
2.714
1.280
0.00
226.42
226.42
99.75
.018
125
45.19
41060.00
276.00
6.37
91.0
52.39
367.00
1.95
52.14
390.00
. 1023.0 	 _. . „ 	 	 . ._

8.400
208.502 	 	 	 	
51.000
3.641
46.500

.263
11.420
4.592

.073
3.15%
1.267
44.52 	 ._..... 	 	
199.02
243.55
99.71 . 	 „ 	 	 . . ;
.017
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ENGINE: GTCPS5-96CK S/N= J6179
RAT SHP= ZOO. RA EGT.F- 1150.
FUEL H/C= 1.9280 STOI F/A-
DATA POINT NUMBER
PERCENT MAX. CORRECTED PONER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., DEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR OSCHG. PRES..PSIA
COMPRESSOR OSCHG. TEMP.DEG F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLON, LB/SEC
COMPRESSOR MAP FLON, LB/SEC
FA RATIO BASED ON HAP FLOH
CORRECTED FUEL FLON , L8/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P«»N/V/E«T/540I
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
LB. COZ PER LB. OF FUEL
NEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPH f>Y VOLUME. MET
LB. PER 1000 LB. OF FUEc
NEIGHT FLOH, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPH BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, Lfi./HR.
RATIO LB HC/LB CO
.06822
121
0.0
0.0
0.0
401.0
41740.0
60.1.
397.0
13.63
a. ooo
6.07
.0064
148.0
.0065
.035
.391
98.270

1.31
3.07
429.9

232.4
34.566
4.839

COM3 P/N*698168-3 TEST DATE 6-5-75 FUEL*AV. KERO. P BARO* 28.61
RAT SPO= 41600. DEN PT.F* 57. REL HUH* 32.00 SPEC HUM* .010(00
L H V-
122
40.0
79.9
78.7
659.0
,1610.0
58.7
431.0
13.69
0.000
5.52
.0085
169.0
.0084
.125
.342*
98.923

1.73
3.10
523.2

254.6
29.011
4.903
CARBON, HEIGHTS AS
123.0
10.455
1.464
.3025
69.1
4.494
.759
.1549
18470.
123
99.3
198.6
195.6
829.0
41250.0
59.9
408.0
13.78
0.000
5.28
.0120
244.0
.0128
.180
.330
99.474

2.67
3.12
761.6

262.1
19.494
4.756
CH4
18.0
.765
.187
.0393
S LN T,F*
124
0.
0.
0.
1063.
41110.
50.
369.
13.76
Z.411
6.62
.0171
270.0
.0179
.263
.392
99.752
OF RcDUCED
3.77
3.14
847.2

189.8
10.051
2.714

4.5
.136
.037
.0136
300.0 FLO,L/M= 14.160 SL TIH,S= 6.5000
125
22.6
45.2
44.5
1023.0
41060.0 .
52.4
367.0
13.77
2.103
6.57
.0166
Z76.0
.0173
.254
.393
99.708

3.64
3.14
865.4

288.5
11.428
3.154

8.4 " ' -------- . .^
.263
.073
.0230
NITRIC OXIDE INO) - HEIGHTS AS NOZ
Ff>M BY VOLUME, MET
LB. PER 1000 L6. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE (NOZ)
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
NEIGHT FLOH, LB./HR.
TOTAL OXIDES OF NITROGEN CNO+
PPH BY VOLUME, MET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
SMOKE NUMBER AT HA=0.023
5.3
1.295
.181

8.7
2.125
.298
NOZ) AS NOZ
14.0
3.4ZO
.479

.00706
11.00
.02117
26.00
.53529
34.80
.04940
41.00
28. BO
12.0
2.246
.300

9.8
1.685
.285

21. 0
3.931
.664

.00704
17.10
.02112
32.90
.03520
41.50
.04928
47.60
35.10
29.5
3.604
.879

7.0
.855
.209

36.5
4.459
1.068

.00705
18.30
.02116
32.30
.03527
44.50
.04937
47.60
36.00
50.0
4.349
1.174

4.5
.391
.106

54.5
4.741
1.280

.00705
20.70
.02115
39.80
.03525
49.40
.04935
56.11
41.71
46.5
4.1(6
1.155

4.5 "" ~ "
.405
. 112

51.0
4.592
1.267

.00704 . _- •
18.90
.02112
28.70 . --.-- 	
.03519
45.70
.04936 	 ... 	 .
55.50
37.60

                       NOTES 1. ALL EMISSIONS CONCENTRATIONS A?£  MET VALUES,

                             Z.EQUIVALENCE RATIO CALCULATED  FROM  C02,CO,*NO HC  DATA AND FUEL  COMPOSITION.

                             3.MASS EMISSIONS OF NO. NOZ.  AND NO»M02 CALCULATED AS  NOZ  FROM CONCENTRATIONS  HITH MOLECULAR HEKHT  Of H02 ft6.ll>.
                             4.CONBUSTION EFFICIENCY CALCULATED FROM CO.ANO UHC AS  VAPORIZED  ORIGINAL FUEL  ON LB/  LB FUEL BASIS*
-------
                                                   S/N=  36179
                                                         0.839
                                                         l.HB*
                                                          .*79
                                                          .191
                                                         0.00
                                                         0.09
                                                                     122
  ENGINE* GTCP85-9BCK
DATA POINT NUMBER
EMISSION RATE LB/HR
    CARBON MONOXIDE
    UNBURNED HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIDE
POWER LEVEL HP
TOTAL CORRECTED HORSEPOWER
BRAKE SPECIFIC EMISSION  INDEX L3/1000HP-HR
    CARBON MONOXIDE               0.000
    UNBURNED HYDROCARBONS         3.000
    OXIDES OF NITROGEN            0.000
    NITRIC OXIDE                  0.000      *.8Z1
                                          ••»   AIRESEARCH  EMISSION TEST SUMMARY
                                          CONB  P/N*698168-3  TEST DATE  6-5-75
                                                                               123
                                                                                         12",
                                                                              ",.»95
                                                                                        5.187
                                                                                                    125
*.903
.759
.66*
.380
78.7*
79.92
62.265
9.6*6
8.1.36
*.7S6
.187
1.088
.879
195.63
198.55
ZU. 31*
.95*
5.561
2.71*
.037
1.280
1.17*
2Z6.*2
Z*<>.20
11.985
.162
5.653
3.15*
.073
1.Z67
1.155
2*3.55
259.65
12.951
.298
5.203
                                                                                                               FUEL-»». KERO.
                                                                                                                                 P B»RO» 28.61,
 )
t)
                            NOTE"0. APPE4RIN6 IN 3RA<- SPECIFIC EMISSION  INDEX  COLUMN DENOTES AN IDLE CONDITION
 0)
iQ
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 CO
 Co
                                                                                                                                                                      co
-------
                          ENGINE  MFR.t  AIRESEARCH
                         NOOEL  NO. 1   6TCP65-98CK

                         FUELI  ASTH  01655-73
                                TEST  FACILITY*  PHX LACCZ       INSTR. DESCRIP.I  FEDERAL  REG.  V38  N136    CALC.  DATE!
                                S/NI   36179           ENGINE TYPE (CLASS) 1  APU               CALC.  I.O.t      Z
                              HAX  SHP       ZOO.  » BLEED AIR EXTRACTION TO    1150. DEC. F  EGT
                                   ATOMIC  H/C RATIOI   1.9Z6    LHV 1     18470. BTU/LB.      ADDITIVES! NONE
                                                                                                                                                6-5-79
                                     EXHAUST EMISSIONS PER EPA RATED WORK OUTPUT  ••  CODE  OF FEDERAL REGULATIONS TITLE 40 PART 87
                                    .............................. EMISSIONS COMPUTED FROM TEST CONDITION NO.  5   ».......».»•»•
                                             HYDROCARBONS (HC AS CH4)              .195  LB. POLLUTANT PER 1000 rfP.-HR.
                                             CARBON MONOXIDE (CO)               12.907  LB. POLLUTANT PER 1000 HP.-HR.
                                             OXIDES OF NITROGEN  (NOX AS NOZ)      5.098  LB. POLLUTANT PER 1000 HP.-HR.
                                                                                                                                     17  JULY  1973
[[[  ENGINE OESCRIPTION  ................
COHBUSTOR TYPE! TANGENTIAL CAN           P/NI 696168-3   SURFACE/VOLUME!  .725 SO.  IN/CJ  IN
ENGINE TOTAL SERVICE!     0.0    HR.    TIME SINCE ENGINE OVERHAUL!      0.0 MR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                          AIRCRAFT INSTALLATION ••• MFR. I
                                                                                       MODEL NO. 1
                                                                                                                        FUEL  INJ.  TYPEI
                                                                                                                               USER!
                                                                                                                                             DUAL  ORIFICE
XQ
 (D
 oo
                          ................................•••••••••••••.••OPERATIONAL TEST DATA SUMMARY ••••»•••••••••••••••••••••••••»••••••«*•••••••••
                          GASEOUS EMISSION TEST NO.I     9    DATE!   6-9-75        TIH£t    06.50      8ARO. PRESS.!   28.610  IN.  HGA.
                          AMBIENT AIR TEMP.I 91.0  DEG. F         RELATIVE  HUMIDITY!   3Z.OO PERCENT       SPECIFIC  HUMIOITYI   .010000  LB. HZO/LB. DRY AIR
                          AMBIENT AIR QUALITY    HYDROCARBONS  (HO!  0.0    PPNC    CARBON MONOXIDE (CO) I 0.0   PPMV    OXIDES OF  NITROGEN (NOX)I 0.0   PPMV
) SAMPLE LINE ••• TEMP. 1 360.00 DEG. F. FLOURATE! 14.16 LITERS/HIN. TRANSPORT TIME! 6.50 SEC. LENGTHS 50.00 FT.
TEST CONDITION
) POWER SETTING, CORRECTED HP.
Nl SPEED, RPM
FUEL FLOW (MEAS.I LB./HR.
) ENGINE CORE INLET AIRFLCM (CALC.) LB./SEC.
COMPRESSOR INLET TEMP., DEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
) COMPRESSOR DISCHARGE AIR TEMP., OEG. F
COMPRESSOR BLEED AIRFLOW (MEAS.I LB./SEC.
BLEED AIR PRESSURE. PSIA
) BtEEO AIR TEMPERATURE. DEG. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION, MET ANALYSIS
) HYDROCARBON (HC AS CH4I , PPMC
CARBON MONOXIDE (CO) , PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPMV
) CARBON DIOXIDE (COZ) . PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSION INDEX, LB. POLLUTANT/1000 L3. FUEL
) HYDROCARBONS IHC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02I
) EMISSION RATE, IB. POLLUTANT/HR.
HYDROCARBONS IHC AS CH4)
CARBON MONOXIDE (CO)
1 TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
ENGINE WORK OUTPUT* MEAS. SHP
ENGINE WORK OUTPUT, ISENTROPIC AIR HP
1 ENGINE WORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS!
126 127 128
0.00 79.56 196.49
41720.00 41550.00 41200.00
137.00
5.72
93.0
60.15
400.00
0.00
0.00
-0.00
475.0

117.000
227.600
15.000
1.355
11.000

9.659
3Z.673
3.559

1.323
4.504
.466
0.00
0.00
0.00
98.36
.•17
174.00
5.61
90.0
69.64
-.01.00
0.00
0.00
-0.00
585.0

75.000
254.593
22.000
1.707
13.000

4.945
29.366
4.166

.660
5.110
.7Z5
76.33
0.00
76.33
98.68
.001
242.00
5.34
90.0
59.66
408.00
0.00
0.00
-0.00
830.0

15.000
249.616
36.000
2.618
31.800

.651
18.946
4.736

.157
4. 565
1.147
195.39
0.00
195.39
99.50
.(11
1Z9
0.00
41050.00
270.00
6.51
92.0
S0.8Z
362.00
Z.ZS
49.35
369.00
1062.0

4.500
167.476
54.000
3.706
49.800

.139
10.103
4.760

.037
2.726
1.231
1.10
228.04
228.04
99.75
.116
130
45.01
41020.00 	 	 ... .._..
274.00
6.47
92.0
5J.Z7
365.00
1.97 	 :.. 	 .._
51.95
369.00
1026.0 ..... . ...:

5.400
203.790
49.000
3.545
45.500

.17*
11.473
4.531

.0*6 . 	 	
3.143
1.242
4* .36
199.16
243.54
.. 99.71-. . .. 	 ' 	 '_ 	 . 	 •. 	 .
.117 ••
                                                                                                                                                                       '£
-------
CO
Ul
ENGINE* GTCP65-96CK S/N« 36179
RAT SHP* 200. RA EGT.F*
FUEL H/C* 1.9280 STOI F/A>
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., DEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR OSCHG. PRES..PSIA
COMPRESSOR DSCHG. TEMP, DEC F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOH, LB/SEC
COMPRESSOR MAP FLOH, LB/SEC
FA RATIO BASED ON MAP FLOH
CORRECTED FUEL. FLOH . LB/HR
FA RATIO CAL.C. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P»»N/V/E(T/540)
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNED HYDROCARBONS- PPM AS
PPM BY VOLUME, NET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
1150.
.06822
126
0.
0.
0.
475.
41720.
60.
400.
13.63
0.000
6.07
.0063
137.0
.0067
.098
.381
98.379

1.36
3.08
4Z1.4

227.6
32.873
4.504
COMB P/N«b98168-3 TEST DATE 6-5-75 FUEL«AV. KERO. P BARO» 28.61
RAT SPD*
L H »*
127
39.6
79.6
78.3
565.0
41550.0
60.6
401.0
13.66
0.000
5.54
.0087
171.0
.0063
.122
.342
98.875

1.71
3.09
538.4

254.6
29.366
5.110
CARBON, HEIGHTS AS
117.0 ,
9.659
1.323
.2938
75.0
4.945
.860
.1664
41600. OEH PT,F*
18470. S
128
99.2
198.5
195.4
830.0
41200.0
59.7
406.0
13.78
0.000
5.50
.0122
242.0
.0126
.164
.345
99.497

2.62
3.12
755.6

249.6
18.948
1.585
CH4
15.0
.651
.157
.0343
LN T,F-
129
0.
0.
0.
1062.
41050.
50.
362.
13.77
2.420
6.63
.0171
270.0
.0176
.256
.396
99.750
REDUCED
3.71
3.14
647.2

167.5
10.103
2.728

4.5
.139
.037
.0137
57. REL MUM* 32.00 SPEC HUH- .010(100
300.0 FLO.L/M* 14.160 SL TIN.S* 6.5100
130
22. 5
45.0 •...__ 	 	 	 _ . . .. _ 	 	 ..
44.4
1026.0
41020.0
53.3
365.0
13.77 _. _. . .... ..., ..
2.121
6.49
.0166 . . 	
274.0
.0169
.246 	
.375
99.715

3.54
3.14 	 ...... ._ 	 .. 	 -- 	 ..._.....
659.1

203.6 .. 	 	 	 _.. ..._,....-... 	
11.473
3.143
_ 	 . . . - -
5.4
.174
.046 .. 	 	
.0151
NITRIC OXIDE (NO) - HEIGHTS AS N02
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
NITROGEN DIOXIDE IN02)
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
TOTAL OXIDES OF NITROGEN INC*
PPM BY VOLUME, HET
1 ft DPP IRDfl 1 B f\F FUFL
LB* " t K 1 U U U L D • Ur r UCk.
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOM
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
SMOKE NUMBER AT HA=0.023
11.0
2.610
.356

4.0
.949
.130
N02I AS N02
15.0
3. 559
.468

.00704
15.90
.02112
28.00
.03520
39.00
.04919
43.90
32.00
13.0
2.463
.429

9.0
1.705
.Z97

22.0
4.168
.725

.00701
20.10
.02102
35.40
.03503
43.30
.04904
50.00
37.60
31.6
3.965
.960

6.2
.773
.167

30.0
4. 738
1.147

.00700
15.90
.02100
32.90
.03500
41.50
.04900
50.00
35.50
49.8
4.409
1.190

4.2
..372
.100

54.0
4.780
1.291

.00702
23.20
.02107
37.60
.03512
47.00
.04917
57.30
41.70
45.5

4.206
1.153
	 .. 	 	 . — 	 	 	 	
3.5
.324
.069


49.0
4.531 _ . . - -
1.242

.00704
21.31
.02111
36.60 . -
.03516
47.61
.04926 _
53.70
40.10
 3
!)

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  ):
  );
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                          NOTES 1.  ALL  EMISSIONS  CONCENTRATIONS ARE  HET  VALUES.                                                   	
                                2.EQUIVALENCE  RATIO  CALCULATED FROM  C02,CO,ANO HC  DATA AND FUEL  COMPOSITION.
                                3.MASS  EMISSIONS  OF  NO,  N02,  ANO NOtNOZ  CALCULATED AS NOZ  FROM CONCENTRAT IONS  HITH MOLECULAR  HEIGHT  OF  NOZ  146.011.
                                4.COMBUSTION EFFICIENCY  CALCULATED FROM  CO,AND UHC AS KAPORIZEO  ORIGINAu  FUEL  ON  LB/ LB FUEL  BASIS.  ... .  		
-------
ENGINE* GTCP85-98CK S/N = 36179
DATA POINT NUMBER
EMISSION RATE L8/HR
CARBON MONOXIDE
UNBURNEO HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIDE
POMER LEVEL HP
TOTAL CORRECTED HORSEPOWER
BRAKE SPECIFIC EMISSION INDEX
CARBON MONOXIDE
UNBURNEO HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIDE
126

5.95

11.963
.161.
5.660
5.220
130

3.1<>3
.01.8
1.2«
1.153
21.3.51.
259.81

12.907
.195
5.098
I.. 73*
                                                                                                              FUEL=AV.  KERO.
                                                                                                                                 P BARO= 28.61
                            NOTE"0.  APPEARING  IN  BRAKE SPECIFIC EMISSION INDEX COLUMN DENOTES AN IDLE CONDITION
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-------
                   >    EN6INE  HFR.I  AIRESEHRCH
                       MODEL  KG. 1   GTCPI5-98CK

                    )   FUELI  ASTH  01655-73
                                                                                                                                                                  I
 TEST FACILITYl PHX LACCZ       INSIR. DESCRIP.I   FEDERAL REG.  V38 N136   CW.C.
 S/NI  36179          ENGINE TYPt ( CLASS) t  tPU              CALC. I.O.I     3
MAX SHP       ZOO. * BLEED AIR EXTRACTION TO    1150. 9EG. F EGT
    ATOMIC H/C RATIO!   1.926    LHV 1     18470.  BTU/LB.     ADDITIVES! NONE
                                                                                DATE!  6-5-TJ
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> •••••»»••• EXHAUST EMISSIONS PER EPA RATED WORK OUTPUT •• CODE OF FEDERAL REGULATIONS TITLE 40 PART 87 17 JULY 1973 •••»»•••••
HYDROCARBONS ( HC AS CM«) .159 _B. POLLUTANT PER 1800 HP.-HR. '
) CARBON NONOXIOE (CO) 13.006 LB. POLLUTANT PER 1000 HP.-HR.
OXIDES OF NITROGEN (NOX AS N02) 5.116 LB. POLLUTANT PER 1000 HP.-HR. 	 	
COMBUSTOR TYPE! TANGENTIAL CAN P/NI 698168-3 SURFACE/VOLUME 1 .725 SO IN/CJ IN FUEL INJ. TYPE! DUAL ORIFICE
ENGINE TOTAL SERVICE! 0.0 HR. TIME SINCE ENGINE OVERHAUL! 0.0 HR.
) ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
AIRCRAFT INSTALLATION *»» MFR. I
MODEL NO. 1 USERI
) GASEOUS EMISSION TEST NO. 1 9 DAT..! 6-5-75 TIME! 10.25 BARO. PRESS.! 28.610 IN. HGA.
AMBIENT AI
CARBON MONOXIDE (CO) •
> TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
ENGINE WORK OUTPUT, MEAS. SHP
cNGINE WORK OUTPUT, ISENTROPIC AIR HP
> ENGINE HO^K OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS)
;
131 132 133 134 135
0.00 79.57 197.89 0.00 45.33
41690.00 41520.00 41190.00 41040.00 41010.00
136.00 168.00 242.00 270.00 274.01
5.97 5.61 5.Z1 6.45 6.41
92.0 92. 0 92.0 91.0 91.1 i
60.15 60.29 59.51 50.82 53.42
400.00 403.00 406.00 361.00 364.01
0.00 0.00 0.00 Z.27 1.98
0.00 0.00 0.00 49.35 49.35
-0.00 -0.00 -0.00 389.00 369.01 ;
477.0 587.0 826.8 1063.0 1828.0
114.000 72.000 15.000 3.300 4.500
230.017 259.602 259.602 195.832 210.867 |
15.000 22.000 38.500 55.500 50.500
1.286 1.707 2.687 3.771 3.609
11.500 13.000 32.000 50.5110 46.101
9.908 4.746 .634 .100 .142
34.975 29.940 19.196 10.369 11.661
3.747 4.168 4.676 4.827 4.587
1.347 .797 .153 .127 .039
4.757 5.030 4.646 2.800 3.195
.510 .700 1.132 1.303 1.257
0.00 78.47 195.15 0.00 44.66
0.00 0.00 0.00 230.29 ZOO. 99
0.00 78.47 195. 15 230.29 245.65
98.31 98.88 99.49 99.75 99.71 	 	
.006 .008 .013 .018 .017 ,
-------
(U
CO
CO
                   ENGINE*  GTCP05-98CK      S/N= 36179
                  RAT  SHP*    ZOO.     RA EGT,F= 1150.
                FUEL  H/C*  1.9280     STOI F/A= .06822
.....  AIRtSEARCM EMISSION TEST SUMMARY
  CONS »/N=69816B-3  TtST DATE  b-5-75
 RAT SPO= 41600.    BE* PT,F*  57.
   L H V= 18470.    S .-N T,F* 300.0
     FU£L=AV. KERO.    P BARO> 28.61
REL HUM =  32.00    SPEC HUH-  .010000
FLO.L/H*  14.168   SL TIM.S-  6.5000
i>
DATA POINT NUMBER
' PERCENT MAX. CORRECTED POWER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OEG.F
SHAFT SPEED. Nl. RPH
COMPRESSOR OSCHG. PRES..PSIA
) COMPRESSOR OSCHG. TEMP, 066 F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOH, LB/SEC
) COMPRESSOR MAP FLOM, LB/SEC
FA RATIO BASED ON MAP FLOH
CORRECTED FUEL FLOH , LB/HR
) FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P»»N/V/E(T/540»
) COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
) PERCENT BY VOLUME, HET
LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
) CARBON MONOXIDE
PPM 8Y VOLUME, HET
LB. PER 1000 LB. OF FUEL
) HEIGHT FLOH, LB./HR.
UNBURNED HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
) LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/L6 CO
131
0.0
0.0
0.0
477.0
41690.0
60.1
400.0
13.64
0.000
6.04
.0862
136.0
.0063
.0)3
.380
98.308
132
39.8
79.6
78.5
587.0
41520.0
60.3
403.0
13.64
0.000
5.77
.0081
168.0
.0083
.122
.359
98.879
133
98.9
197.9
195.2
826.0
41190.0
59.5
408.0
13.77
0.000
5.20
.0127
242.0
.0129
.189
.333
134
0.
0.
0.
1063.
•.1040.
50.
361.
13.77
2.442
6.59
.0173
270.0
.0179
.263
.393
99.493 99.747

1.29
3.07
417.8

230.0
34.975
4.757
1.71
3.09
519.8

259.6
29.940
5.030
CARBON, HEIGHTS AS
114.0
9.908
1.347
.2033
72.0
4.746
.797
.1585
2.69
3.12
755. 6

259. 6
19.196
4.646
CH4
15.0
.634
.153
.0330
3.77
3.14
847.1

195.0
10.369
2.800

3.3
.100
.027
.0096
135
22.7
45*3 ... .. 	 	 	 	 _ - -- _ 	 	 - .
44.7
1028.0
41010.0 _
53.4
364.0
13.77
2.131
6.37
.0173 	 	
274.0
.0172
.252
.363
99.713

3.61
3.14 	 	 	 	 . 	 	
•59.1

210.9
11.660
3.195

4.5
.142
.039
.0122
) NITRIC OXIDE INOI - HEIGHTS AS N02
PPH BY VOLUME, HET
L8. PER 1000 LB. OF FUEL
) HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE (N02)
PPM BY VOLUME, HET
) LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
11.5
2. 872
.391

3.5
.874
.119
TOTAL OXIDES OF NITROGEN (NC»N02I AS N02
} PPH BY VOLUME, HET
L9. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
i SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLCM
SMOKE NUMBER
; CORRECT tO HEIGHT FLOH
SMOKE NUMBER
CORSfCftO HEIGHT FLOU
) SMOKE NUMBER
CORRECTED HEIGHT FLCH
SMOKE NUMBER
) SMOKE NUMBER AT HAsO.023
NOTES 1. ALL EMISSIONS CONCEN1
15.0
3.747
.510

.00704
10. -.0
.02112
22.00
,03520
30.50
.04928
34.80
24.60
PRATIONS ARE
Z. EQUIVALENCE RATIO CALCULATED FROM
) 3. MASS EMISSIONS OF NO,
4. COMBUSTION EFFICIENCY
13.0
2.463
.414

9.0
1.705
.286

22.0
4.168
.700

.00701
13.40
.02104
31.10
.03507
37.80
.04910
47.00
32.70
NET VAL
32.0
3.807
.941

6.5
.790
..191

38.5
4.676
1.132

.00703
14.60
.02100
30.50
.03513
38.40
.04918
47.60
33.10
UES.
50.5
4.392
1.106

5.0
.435
.117

55.5
4.827
1.303

.00703
20.70
.02100
37.60
.03513
47.60
.04918
56.10
38.20

46.0
4.178
1.145

4.5
.409
.112 _

$••5
4.58? 	 	 ._
1.257

.00703
20.70
.02108
37.60 	 .
.03513
47.60
.04918 ' 	 _ _ 	 	 	 	
56.11
38.20

C02.CO.ANO HC DATA AND FUEL COMPOSITION.
N02, AW NO* NO? CALCULATED AS
CALCULATED FROM CO.
AND UHC AS
HOZ FROM
VAPORIZED
CONCENTRATIONS MITH MOLECULAR HEIGHT OF N02 1*6.111.
ORIGINAL FUEL ON IS/ L8 FUEL BASIS. 	 :......_..

-------
                                             S/N«
                                                  36179
                                                     131
»•••  AIRESEARCH EMISSION TEST  SUMMARY
 COMB P/N.69816B-S  TEST DATE  6-5-75
    13Z
              133
                        13*
                                  135
  ENGINE' GTCPS5-98CK
DATA POINT NUMBER
EMISSION RATE LB/HR
    CARBON MONOXIDE
    UNBURNEO HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIDE
POHcR LEVEL HP
TOTAL CORRECTED HORSEPOWER
BRAKE SPECIFIC EMISSION  INDEX LB/IBOflrtP-HR
    CARBON MONOXIDE               0.000
    UMBURNED HYDROCARBONS         0.000
    OXIDES OF NITROGEN            0.000

    HoTE-or.p'pEARUG  IN BRAKE  SPECIFIC EHIS»~ON  INDE^'COLUMN  DENOTES  AN  IDLE CONDITION
                                                                                                        FUEL«AV. HERO.     P  B»RO«  Z8.61
                                                   H.75T
                                                   1.3li7
                                                     .51B
                                                     -3«
                                                   0.30
                                                   0.00
5.030
.797
.700
.bid

79.57
6W. 099
10.161
8.923
5.273
t.6%6
.153
1.132
.9U1
195.15
197.89
23.805
.786
5.799
I..820
3.800
.027
1.303
1.186
230.29
248.16
12»157
.117
5.659
5.150
3.195
.039
1.257
1.11.5
2".5. b5
261.91
13.006
.159
5.116
"..660
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(£1
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O
                          ENGINE  HFR.I  AIRESEARCH
                         NOOEL NO.I   GTCP05-98CK
                         FUELI  ASTM  01655-73
                                TEST FACILITY) PHX LACC2       INSTR.  DcSCRIP.I   FEDERAL  REG V30 N136    CALC. OATEI
                                S/NI  36179          ENGINE TYPE  (CLASS)!  APU                CALC. I.D.I     1
                               NAX  SHP       ZOO. * BLEED AIR EXTRACTION TO     1150.  DEG. F EGT
                                   ATONIC H/C RATIO!   1.920    LHVI     18<>70.  BTU/LB.      ADDITIVES! NONE
                                                                                                                                                 6-6-75
                                     EXHAUST  EMISSIONS PER EPA RATED HORK OUTPUT  »•  C03E OF FEOERA,. REGULATIONS TITLE 1.0 PART  87
                                    ••«•*••••*•••••••••»•••»•...•• EMISSIONS COMPUTED FROM TEST CONDITION NO.  5   ••••»•••••••••
                                             HYOROCARBOMS (HC AS CHI.)              .29b  LB. POLLUTANT PER 1000 HP.-HR.
                                             CARBON MONOXIDE (COI               17.930  LB. POLLUTANT PER 1000 HP.-HR.
                                             OXIDES OF NITROGEN (NOX AS N02)      "..478  _B. POLLUTANT PER 1000 HP.-HR.
                                                                                                                                      17  JULY 1973  »»••»•»•»•
•••.•.*.••.*•.*...•**.....••••.••».»•.••».•••.••••••  ENGINE DESCRIPTION  »«»»»»»»»»«»»•»*
COHBUSTOR TYPE! TANGENTIAL CAN           P/NI  698168-3  SURFACE/VOLUME 1   .725  SO IN/CJ  IN
ENGINE TOTAL SERVICE!     0.0   HR.    TINE SINCE ENGINE OVERHAUL!       0.0 HR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                          AIRCRAFT  INSTALLATION
                                                    NFR. 1
                                                                                       HOOEL NO.I
                                                                                                                        FUEL  INJ.  TYPE!
                                                                                                                               USER1
                                                                                                                                             DUAL ORIFICE
                         •...•.*.•....,,.,•••.•...•*••••••..••••••*.•••••OPERATIONAL TEST DATA SUHNARY ••••••••••••••••••••»•••••••••»•••••••»•••»•»•»•
                      )   GASEOUS EMISSION TEST NO.I    10    DAT£I  6-6-75        TIME!   05IZ5       BARO. PRESS.I   28.600  IN.  HGA.
                         AMBIENT AIR TEHP.I 91.0  OEG. F         RELATIVE  HUH10ITYI  1.4.00 PERCENT       SPECIFIC  HUMIDITY!   .015000  LB. H20/LB. DRY AIR
                         AMBIENT AIR QUALITY    HYOROCAR30NS (HOI  0.0    PPNC     CARBON MONOXIDE (CO)! 0.0   P?NV     OXIDES OF  NITROGEN (NOX)I 0.0   PPNV
                      )   SAMPLE  LINE ••• TEHP.I  300.00 OEG. F.     FLOHftATE!    14.16 LITERS/MIN.     TRANSPORT  TIME!    6.50 SEC.     LENGTHI   50.00 FT.




)


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}
TEST CONDITION
POMER SETTING, CORRECTED HP.
Nl SPEED, RPM
FUEL FLOW (MEAS.) LB./HR.
ENGINE CORE INLET BIRFLCH (CALC. ) LB./SEC.
COMPRESSOR INLET TEMP., DEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP., OEG. F
COMPRESSOR BLEED AIRFLOW (MEAS.) L3./SEC.
BLEED AIR PRESSURE, PSIA
BLEED AIR TEMPERATURE, OEG. F
ENGINE EXHAUST GAS TEMP., DEC. F
EMISSION CONCENTRATION, MET ANALYSIS
HYDROCARBON (HC AS CH".) , PPHC
CARBON HONOXIDE (CO) . PPMV
TOTAL OXIDES OF NITROGEN (NOXI , PPMV
CARBON DIOXIDE (C02) , PERCENT BY VOL.
NITRIC OXIDE (NO) , PPNV
EMISSION INDEX, LB. POLLUTANT/1000 L3. FUEL
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
CHISSIOK RATE, L3. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
ENGINE WORK OUTPUT, MEAS. SHP
ENGINE WORK OUTPUT, ISENTROPIC AIR HP
cNCINE NOftK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS!

136 137 138
0.00
1.1730.00
11.6.00
6.27
92.0
61.07
375.00
0.00
0.00
-0.00
1.70.0

132.000
237.311
13.500
1.311.
5.506

11.208
35.251.
3.291.

1.636
5.11.7
.".81
0.00
0.00
0.0*
90.19
.((6

79.63
-.1560.00
185.00
6.16
91.0
62.60
379.00
0.00
0.00
-0.00
570.0

109.500
257.093
19.000
1.707
10.500

7.20*
29.592
3.592

1.333
5.474
.665
78.65
0.00
78.65
98.67
.118

198. OZ
1,121.0.00
254.00
5.66
91.0
62.60
385.00
0.00
0.00
-0.00
700.0

19.500
277.1.6*
33.000
2.592
26.500

.851.
21. 242
4.1SI

.217
5.396
1.054
195.50
0.00
195. SO
99.43
.MZ

139
0.00
1.1120.00
200.00
6.67
91.0
52.05
350.00
2.26
50.02
375.00
1014.0

3.600
217.999
47.000
3.706
43.000

.111
11.739
4.220

.031
3.207
1.104
0.00
219.07
219.87
99.71
.lit

140
45.79
41090.00
200.08
6.61
	 91.8 	 	 	
54.70
342.08
1.97
53.67
366.00
977.8

7.500
259.602 	 	 	
43.000
3.513
30.008

.243
14.721 .
4.005

.060
4.122
1.122
45.23
184.67
229.90
99.M. 	 ._ .
.017


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ENGINE' GTCP85-98CK S/N* 36179 COMB P/N« 698168-3 TEST DATE 6-6-75
RAT SHP« 2DO. RA EGT.F* 1150. RAT 3PO* *1730. DEH PT.F* 68. REL
FUEL H/C* 1.9Z88 STOI F/A« .068ZZ L H V* 18*70. S LN T,F« 300.8 FLO
DATA POINT NUMBER 136 137 138 139 1*8
PERCENT MAX. CORRECTED POHER 0.0 39.8 99.0 0.8 ZZ.9
CORRECTED SHAFT HP 0.0 79.6 198.0 0.8 *».» _
MEASURED SHAFT HP 0.0 78.6 195.6 0.0 *5.Z
EXHAUST GAS TEMP., DEG.F *70.0 570.0 780.0 101*. 0 977.8
SHAFT SPEED, Nl, RPM 1.1730.0 *1550.0 *1Z*0.0 *11Z8.0 *1890.8 	
COMPRESSOR DSCHG. PRES..PSIA 61.9 62.6 6Z.6
> COMPRESSOR OSCHG. TEMP.DEG F 375.0 379.0 385.0
EXHAUST GAS PRESS., PSIA 13.65 13.69 13.81
i CORRECTED BLEED FLOH, LB/SEC 0.000 0. 000 0.000
1 COMPRESSOR MAP FLOM, LB/SEC 6.19 6.Z2 5.52
FA RATIO BASED ON MAP FLOH .0066 .0083 .0128
CORRECTED FUEL FLOH , LB/HR 1*6.0 185.0 25».0
•1 FA RATIO CALC. FROM EMISSION .0065 .0083 .0125
EQUIVALENCE RATIO .095 -I22 • 183
LOADING H/P"»N/V/EIT/5*fl> -3»B .379 .332
1 COMB EFFIC FROM EMISSIONS 98.188 98.672 99.*25
CARBON DIOXIDE
) PERCENT BY VOLUME, HET 1.31 1.71 2.59
LB. C02 PER LB. OF FUEL 3.«7 3.09 3.12
HEIGHT FLOM, LB./HR. **7.9 571.2 792.1
) CARBON MONOXIDE
PPM 6Y VOLUME, MET 237. 3 257.1 277.*
L3. PER 1000 LB. OF FUEL 35.25* Z9.592 21.2*2
) HEIGHT FLOH, LB./HR. 5.1*7 5.*7* 5.396
UN6URNED HYDROCARBONS- PPM AS CARBON, HEIGHTS AS CM*
PPM BY VOLUME, MET 132.0 109.5 19.5
) L9. PER 1000 LB. OF FUEL 11.208 7.ZO* .85*
HEIGHT FLOM, LB./HR. 1.636 1.333 .Z17
RATIO LB HC/LB CO .3179 .2*3* .0*02
) NITRIC OXIDE  - HEIGHTS AS NOZ
PPM BY VOLUME, HET 5,5 10.5 26.5
LB. PER 1000 LB. OF FUEL 1.3*2 1.985 3.333
) HEIGHT FLOH. LB./HR. .196 .367 .8*7
NITROGEN DIOXIDE IN02I
PPM BY VOLUME, MET 8.0 8.5 6.5
) L3. PER 1000 LB. OF FUEL 1.952 1.607 .818
HEIGHT FLOH, LB./HR. .285 .297 .208
TOTAL OXIDES OF NITROGEN INO»N02I AS NOZ
} PPM BY VOLUME, HET 13.5 19.8 33.0
LB. PER 1080 LB. OF FUEL 3.29* 3.592 *.151
HEIGHT FLOH, LB./HR. .*81 .665 1.05*
) SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOH .00716 ,00715 .00715
SMOKE NUMBER I*-?" lt.59 18.10
> CORRECTED HEIGHT FLOH .021*9 .021*5 .021**
SMOKE NUMBER 28.90 31.30 33.70
CORRECTED HEIGHT FLOH .03592 .03575 .03573
) SMOKE NUMBER 38.00 39.80 fc3;ij
CORRECTED HEIGHT FLOM .0501* .05005 .05002
SMOKE NUMBER '•S.fcfl "•'•»» 58'6a
) SMOKE NUMBER AT HA=8.823 32.00 33. Z8 36.58
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE HET VALUES.
2. EQUIVALENCE RATIO CALCULATED FROM COZ.CO.AND HC DATA
") 3 MASS EMISSIONS OF NO, NOZ, AND NO*NOZ CALCULATED AS
*. COMBUSTION EFFICIENCY CALCULATED FROM CO. AND UHC AS
52. D
358.0
13.79
2.*32
6.67
.0177
280.0
.0176

.391
?*•*
3*2.8
13.88
2.117
6.57
.0169 	
280.0
.0168
.2*6

.388
FUEL'AV. KERO. P BARO- 28.68
HUM- 1.8.00 SPEC HUH- .015888 T-
,L/M- l*.16fl SL TIM.S- 6.5808 1 -»
>

"^

	 	 . 	 . 	 	 . — - — - 	
}


~y

— — _ . .
)


3.71

877.9
218.0
11.739
3.287

3.6
.111

.009*


3.88*
1.065


.*25
.119

*7.8
*.2Z8
1.18*
.00713
21.78
.02139
i.1.00
.03565
51.20
.0*990
56.60
".2.80
AND FUEL
NOZ FROM
VAPORIZED
4.91

876.5
259.6 	

*.12Z
.. - - -

.2*3

.0165


3.5*8
.991



.138 .

*.B85
1.1Z2
.00713
18.18
.821*0

.83566
1.5.80
.0*993
53.80

COMPOSITION.
CONCENTRATIONS
ORIGINAL FUEL

— . — 	 ...
)

— 	 -
\

	 	 - — 	 	 •-- 	 "~ "
)

.
) ;
'
___ ... _ .
) :

- • — 	 - . —
3

	 	 	 f
) •
'.
— - — — — 	 ... - .
)




i )
y

&
HITH MOLECULAR HEIGHT OF NOZ «*6.01I. J-*
ON LB/ LB FUEL BASIS. „ 	 . . . .., 	 , ... - .fc."

-------
                                                               •»*•  AKESEARCH EMISSION  TEST  SUMMARY
                                                                COMB P/Ns 091168-3 TtST DATE   6-6-75
                                                                   137
                                                                             138
                                                                                       139
  ENGINE* GTCP85-98CK      S/N* 36179
DATA POINT NUMBER                   136
EMISSION RATE LB/HR
    CARBON MONOXIDE              5.11,7
    UNBURNEO HYDROCARBONS        1.636
    OXIDES OF NITROGEN             .",81
    NITRIC OXIDE                   .196
POKER LEVEL HP                   0.00
TOTAL CORRECTLO HORSEPONER       0.00
BRAKE SPECIFIC EMISSION INDEX  L3/1000HP-HR
    CARBON MONOXIDE              0.000
    UNBURNED HYDROCARBONS        0.000
    OXIDES OF NITROGEN           0.000
    NITRIC OXIDE                 0.100
    NOTE**0. APPEARING  IN BRAKE SPECIFIC EMISSION INO£X COLUMN DENOTES
5.1.7»
1.333
.665
.367
78.65
79.63
69.609
16.91,6
8.1.5*
I.. 670
5.396
.217
1.051.
.81.7
195. SB
198.02
27.567
1.108
5.391
1..329
3.2B7
.031
1.181.
1.065
219.07
235.1,8
15.001.
.11.2
5.1,01.
1..861
I..122
.068
1.122
.991
229.90
21.1.. 31
17.930
.296
I..87S
4.311
                                                                                                             FUEl-AV. KERO.
                                                                                                                               P BARO= 38.68
ft)

-vo
M
-------
                       ENtilMt MFR.I AIRESEARCH
                      MODEL NO.I  CTCP65-96CK
                      FUEL I ASTH 01655-73
 TEST FACIwITYl PHX LACC2       INSTR.  OESCRIP.I   FEDERAL  RLG V36 N136    CALC. DATE!
 S/NI  3617)          ENGINE TYPE  (CLASS)I   APU               C*LC. I.D.I     Z
MAX SHP       ZOO. » BLEED AIR EXTRACTION TO    1150. JEG. F EGT
    ATONIC H/C RATIOI   1.928    LHVI     16470.  BTU/LB.     ADDITIVES! NONE
                                 EXHAUST EMISSIONS  PER  EPA  RATED WORK OUTPUT  •» CODE OF FEDERAL REGULATIONS TITLE  40  PART  87
                                ..............................  ENISSIONS CONFUTED FROM TEST CONDITION NO.  5   •••»••»••«••»•
                                         HYDROCARBONS  IHC AS CH4)              .248  ^B. POLLUTANT PtR 1000 HP.-HR.
                                         CARBON  MONOXIDE  (C01                17.717  LB. POLLUTANT PER 1000 HP.-HR.
                                         OXIDES  OF  NITROGEN (MOX AS N02I     4.981  LB. POLLUTANT PER .1000 HP.-HR.
                                                                                                                                  17  JULY 1973
                      ...........................................I........   ENGJN£ DESCRIPTION  •»»•••»••••».•»•
                      COM3USTOR TYPEI TANGENTIAL  CAN           P/N! 693168-3   SURFACE./VOLUME«  .725 SQ IN/CJ IN
                      ENGINE TOTAL SERVICEI       0.0  HR.    TIME SINCE ENGINE OVERHAUL!      0.0 HR.
                      ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                                                                FUEL INJ. TYPEI
                                                                                     DUAL  ORIFICE
                      AIRCRAFT INSTALLATION »••  HFR.1
                                                                                   MODEL NO.I
n>
vo
cu
                      ...................................,............OPERArIONAL T£3T QATA
                      GASEOUS EMISSION TEST NO. I     10     DATil  6-6-75       TIME)   06I* TEMP.!  300.00 DEC.  F.      FLOH3ATEI   14.16 LITERS/MIN.     TRANSPORT TIME!     6.50 SEC.      LENGTHS   50.00 FT.

TEST CONDITION
POKER SETTING, CORRECTED HP.
Nl SPEED, RPM
FUEL FLOW (KEAS.l LB./HR.
ENGINE CORE INLET AIRFLOW (CALC.) L3./SEC.
COMPRESSOR INLET TEMP.. DEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP., D£S. F
COMPRESSOR BLEED AIRFLON 1MEAS.I LB./SEC.
BLEED AIR PRESSURE. PSIA
BLEED AIR TEMPERATURE, OEG. f
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION, MET ANALYSIS
HYDROCARBON (HC AS CHI.I. PPMC
CARBON MONOXIDE (CO*, PPMV
TOTA,. OXIDES OF NITROGEN (NOXI, PPMV
CARBON DIOXIDE (C02) , PERCENT BY VOL.
NITRIC OXIDE (NOI, PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS IHC AS CH3
0.00
1.1730.00
1«6.00
6.21
91.0
62.01
370.00
0.00
0.00
-0.00
1(56.0

129.000
239.757
13.500
1.327
10.500

10.855
35.298
3.265

1.585
5.154
."•77
0.00
0.00
0.00
98.22
.007
79.61.
••1550.01
164.00
6.14
91.0
62.70
377.00
0.00
0.00
-0.00
563.0

84.000
257.093
19.000
1.707
11.000
•
5.534
29.635
3.59*

1.018
5.453
.662
76.63
0.00
78.63
98.62
.008
198.25
41250.00
250.00
5.57
90.0
62.11
367.00
0.00
0.00
-0.00
782.0

21.000
274.834
32.200
2.592
25.800

.919
21.D46
lt.050

.230
5.262
1.013
195.63
0.00
195.63
99.42
.012
144
0.00
41090.00
280.00
. 6.65
90.0
52.29
338.00
2.28
50.82
367.00
1021.0

3.600
217.999
48.500
3.736
45.001

.111
11.637
4.253

.031
3.258
1.191
0.80
215.06
215.06
99.72
.018
145
45.68
41080.00
280.01
6.61
91.1
54.75
347.00
1.97 	 	
53.76
367.01
978.0

6.300
257.093 	 	 	 	 	 	
44.000
3.513
38.500

.204
14.586^ ______
4.099

.057
4.063
1.146
45.12
185.30
230.42
99.6* 	 	 . 	 _._ 	 .
.017
-------
13
(1)
id
 FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P»»N/V/E(T/540I
) COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
) PERCENT BY VOLUME. MET
LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
) CARBON MONOXIDE
PPK BY VOLUME, MET
LB. PER 1000 LB. OF FUE.
) HEIGHT FLOH, LB./HR.
UNBURNED HYDROCARBONS- PPM AS
PPM BY VOLUME, MET
) LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO wB HC/LB CO
.06822
141
0.0
0.0
0.0
456.0
41730.0
62.0
370.0
13.55
0.000
6.2f
.0065
146.0
.0065
.096
.395
96.217
COM3 P/N-t>9dl66-3 TEST DATE 6-6-75 FUEL=AV. KERO. P BARO* 28.66
SAT SPO= 41730. OEM PT,F= 66. REL HUH: 48.00 SPEC HUM' .015060
L H V= 18470.
142
39.6
79.6
78.fr
563.0
41550.0
62.7
377.0
13.69
0.000
6.02
.0085
184.0
.0083
.122
.367
98.817
143
99.1
198.2
195.6
782.0
41250.0
62.1
367.0
13.82
a. ooo
5.47
.0127
250.0
.0125
.183
.333
99.424
S LN T.Fs
144
0.0
1.0
0.0
1021.0
41090.0
52.3
338.0
13.79
2.445
6. 62
.0179
260.0
.0178
.261
.391
99.717

1.33
3.97
448.0

339.8
35.293
5.154
1.71
3.09
569.0

257.1
29.635
5.453
CARBON, HEIGHTS AS
129.0
10.655
1.565
.3075
84.0
5.534
1.018
.1866
2.59
3.12
779.6

274.8
21.046
5.262
CH4
21.0
.919
.230
.0437
3.74
3.14
677.9

218.0
11.637
3.258

3.6
.110
.031
.0094
300.0 FLO,L/M= 14.160 SL TIN.S* 6.5111
145
22.6
45.7
45.1
976.1
41080.0
54.7
347.1
13.79
2.116
6.53
.1171
280.0
.0168
.246
.373
99.639

3.51
3.13
676.6

257.1
14.560
4.063

6.3
.204 '
.057 .. _ 	 _.._.
.0140
) NITRIC OXIOE (NO) - HEIGHTS AS N02
PPM BY VOLUME. MET
LB. PER 1010 LB. OF FUEL
) HEIGHT FLON, LB./HR.
NITROGEN DIOXIDE IN02I
PPM BY VOLUME. MET
) LB. PER 1000 LB. OF FUEL
HEIGHT FLOM. LB./HR.
TOTAL OXIDES OF NITROGEN INC*
) PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOM
SMOKE NUMBER
; CORRECTED HEIGHT FLOM
SMOKE NUMBER
CORRECTED HEIGHT FLON
) SMOKE NUMBER
CORRECTED HEIGHT FLOH
SNOKE NUMBER
) SMOKE NUMBER AT HAzl.123
10.5
2.539
.371

3.0
.726
.106
N02) AS N02
13.5
3.265
.477

. 30712
15.10
.02137
30.10
.03562
40.40
.04936
4«.60
32.71
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE
2. EQUIVALENCE RATIO CALCULATED FROM
) 3. MASS EMISSIONS OF NO.
*.COTeuSTIIM EFFICIENCY
11.0
2.083
.383

8.0
1.515
.279

19.0
3.596
.662

.00711
15.10
.02133
30.70
.03555
42.20
,«»977
46.60
34.41
25.8
3.245
.611

6.4
.80S
.201

32.2
4.050
1.013

.00709
16.10
.02127
34.90
.03545
44.61
.04963
53.60
38.11
45.1
3.946
1.185

3.5
.317
.086

48.5
4.253
1.191

.00709
21.70
.02127
39.10
.03545
52.41
.04963
59.61
43.61
36.5
3.567
1.104

5.5
.512
.143

44.1
4.199
1.146

.00708
16.11
.12124
34.90
.13541
44.61
.04956
53.11
37.91
MET VALUES. . ... __ 	 	 _
C02.CO,
ANO HC DATA ANO FUEL
NOZ. ANO MO«N02 CALCULATED AS
CALCULATED FROM CO, MO UMC AS
COMPOSITION.
N02 FROM CONCENTRATIONS MITH MOLECULAR MEICHT OF N02 (46.111.
MPORIZE0
ORieiNAi. FUEL ON L*/ LI FUEL 0ASIS. 	
-------
                    ENGINE' GTCP85-9SCK
                  OAT* POINT  NUMBER
                  EMISSION RATE IB/MR
                      CARBON  MONOXIDE
                      UNBURNEO HYDROCARBONS
                      OXIDES  OF NITROGEN
                      NITRIC  OXIDE
                  POWER LEVEL HP
                  TOTAL CORRECTED HORSEPOWER
                                              S/N =
36179
   I'll

 5.15k
 1.515
  .»77
  .371
 9.00
 0.00
         »•••  AIRESEARCM  EMISSION TEST SUMMARY
          COMB P/N»t>9S16»-3   TEST  DATE  6-6-75
                                                                                                          FUEL'AV. «RO.
                                                                                                                            P BARO«
 5.1.53
 1.018
  .66Z
  .3B3
78.63
79.61
                   BRAKE  SPECIFIC EMISSION INDEX LB/100«HP-HR
                       CARBON MONOXIDE              0.000    69.351
                       UNBURNEO HYDROCARBONS        0.090    12.952
                       OXIDES OF NITROGEN           8.000      e.<»19
                       NITRIC OXIDE                 0.030
  5.26Z
   .230
  1.013
   .011
195.63
198.25

 Z6.896
  1.175
  5.176
  "..I". 7
  3.25«
   .031
  1.191
  1.105
215.06
230.97

 15.151
   .1*3
  5.537
  5.137
  t.oas
   .057
  !.!<>»
  1.IO*
230. «
ZM.I7

 17.717
   .?<.»
  11.981
  •..358
                       NOTE**0.  APPEARING IN BRAKE SPECIFIC EMISSION INDEX COLUMN DENOTES AN IDLE CONDITION
ft"
V£>
U1
                                                                                                                                                                  x
                                                                                                                                                                  *
-------
                      ENGINE MFR.I AIRESEARCH
                     NOOEi. NO. 1  GTCPS5-9SCK
                     FUEL" ASTH 01655-73
                               TEST FACILITY! PHX LACC2       INSTR.  OESCRIP.t   FEDERAL  REG V36 N136    CALC. DATE!
                               S/Nt  36179          ENGINE TYPE  (CLASS) 1  API)               CALC.  I.O.I      3
                              1AX SUP       200. » BLEED AIR EXTRACTION TO    1150.  BEG.  F E6T
                                  ATONIC H/C RATIO!   1.926    CHV<     18470.  BTU/L3.      ADDITIVES! NONE
                                                                                                                                           6-6-7$
(D
vo
O\
                                EXHAUST EMISSIONS PER EPA RATED WORK OUTPUT •» CODE  CF  FEDERAL REGULATIONS TITLE 40 PART 67
                               ....................*.,..,..., ^MISSIONS COMPUTED  FROM TEST  CCNOITION NO.   5   «•»»•*»••»•«».
                                        HYDROCARBONS (HC AS CH«)              .249 LB.  POLLUTANT  PER 1000 HP.-HR.
                                        CARBON MONOXIDE (COI               17.942 i.B.  POLLUTANT  PER 1000 HP.-HR.
                                        OXIDES OF NITROGEN INOX AS N02I     4.791 LB.  POLLUTANT  PER 1000 rtf>.-HR.
                                                                                                                                17 JULY 1973
[[[  EN6INE  DESCRIPTION  ••••••••»»•»»»»»
CONBUSTOR TYPE! TANGENTIAL CAN          P/N1  696166-3  SURFACE/VOLUME I   .725  SO IN/CJ IN
ENGINE TOTAL SERVICEI     0.0  HR.   TINE SINCE ENGINE OVERHAUL!       0.0 MR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                     AIRCRAFT INSTALLATION ••* NFR. t
                                                                                  MODEL NO. 1
                                                                                                                   FUEL INJ. TYPEI
                                                                                                                         USER!
                                                                                                                                       DUAL ORIFICE
)
) GASEOUS EMISSION TEST NO.! 10 OATt:

6-6-75 TIME* 07155 BARO. PRESS.!

26.680 IN. MGA.
AMBIENT AIH TEMP. 1 91.0 OEG. F RELATIVE HUMIOITYI 48.80 PERCENT SPECIFIC HUMIDITY! .015000 LB. H2O/LB. DRY AIR
AMBIENT AIR QUALITY HYDROCARBONS (HCI 1 0
3 SAMPLE LINE ••» TEMP.! 300.00 OEG. F.
)
TEST CONDITION
) POWER SETTING, CORRECTED HP.
Nl SPEED, RPM
FUEL FLOW (MEAS.I LB./HR.
) ENGINE CORE INLET AIRFLCM (CAiC. > LB./SEC.
COMPRESSOR INLET TEMP., OEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
) COMPRESSOR DISCHARGE AIR TEMP.. OEG. F
COMPRESSOR BLEED AIRFLOW (NEAS.) LB./SEC.
BLEED AIR PRESSURE. PSIA
) BLEED AIR TEMPERATURE, DEG. F
ENGINE EXHAUST GAS TEMP., DEG. F
EMISSION CONCENTRATION, WET ANALYSIS
) HYDROCARBON (HC AS CH4I, PPMC
CARBON MONOXIDE (CO) , PPMV
TOTAL OXIDES OF NITROGEN (NOXI, PPMV
) CARBON DIOXIDE (C02). PERCENT BY VOL.
NITRIC OXIDE CNOI. PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CM4I
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS NOZI
) EMISSION RATE, L3. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4)
CA4BON MONOXIDE (COI
) TOTAL OXIDES OF NITROGEN (NOX AS NOZI
ENGINE WORK OUTPUT, MEAS. SHf
ENGINE NORK OUTPUT. ISENTROPIC AIR HP
) ENGINE WORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS!
F/» (EMISSIONS!
}
.0 PPMC CARBON MONOXIDE (CO) 1 0.0 PPMV
OXIDES OF NITROGEN (NOXII 0.0 PPMV
FLOWRATE! 14.16 LlTERS/MIN. TRANSPORT TIME! 6.50 SEC. LENGTHI 50.00 FT.

146 147 148 149
0.00 79.74 196.11 0.00
41690.00 1,1530.00 412ZO.OO 41050.00
146. 08 162.00 246.00 260.00
6.15 6.03 5.47 6i69
90.0 90.0 90.0 90.0
62.36 62.60 61.87 52.29
367.00 375.00 387.00 335.00
0.08 0.00 0.00 2.28
0.00 0.00 0.00 50.72
-0.00 -0.00 -0.00 365.08
456.8 563.0 785.8 1621.0

129.080 64.800 22.500 3.080
243.686 260.608 262.571 215.616
13.700 16.500 32.000 47.000
1.339 1.721 . 2.618 3.706
10.200 10.500 26.200 62.500

10.755 5.492 .975 .092
35.545 29.609 21.416 11.612
3.263 3.676 3.984 4.150

1.570 1.000 .2*2 .026
5.190 5.425 5.311 3.251
.479 .633 .988 1.166
8.00 76.69 195.49 8.11
0.00 0.08 0.00 213.75
•.It 78.69 195.69 213.75
98.22 98.02 99.61 99.72
.117 .III .III .fit


150
45.69
41050.00
260.00
6.60
90.0
54.70
341.01
1.96
53.27
366.00
979.0 	 _1 	 _.

6.300
259.602
42.201
3.513
38.008

.284
14.72Z . .... _ .'-.
.3.911

. . .857 	
4. 122
1.101
45.09 ... . .„„ 	 ._. . _ 	 _. . . .
-------
                   »*•••*•**•»»•••••»•••••••.••.,..„•„»••,,.,  AIRESEARCH  EMISSION TEST SUMMARY  •••»••»••••••••»••••••••»••••••••••••

                   .?!ISJ!*! 6T5!!S-"C5	5'"?.?'1"    _9S"!_r'V.»?•"••»  ««» DATE  6-6-75        FUEL«AV. KERO.    P B«*O. 20.60
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RAT SMP« 200. RA EGT.F> 1150. RAT SPO« O1730.
FUEL H/C* 1.9200 STOI F/Ar .06022 L H «« 16070.
DATA POINT NUMBER 106 107 100
PERCENT MAX. CORRECTED POKER o. 39.9 99.1
CORRECTED SHAFT HP fl. 79.7 190.1
MEASURED SHAFT HP 0. 70.7 195.
EXHAUST GAS TEMP., OEG.F 056. 563.0 765.
SHAFT SPEED. Nl, RPM 01690. O1S30.0 01220.
CCNPRESSOR DSCHG. PRES..PSIA 62. 62.6 61.
COMPRESSOR OSCHG. TEMP, DEC F 367. 375.0 367.
EXHAUST GAS PRESS., PSIA 13.61 13.69 13.61
CORRECTED BLEED FLOM. LB/SEC 0.000 0.000 0.000
COMPRESSOR HAP FLOH, LB/SEC 6.27 6.22 5.07
FA RATIO BASED ON HAP FLOH .0065 .0861 .0126
CORRECTED FUEL FLOM , LB/HR 106.0 102.0 200.0
FA 3AT10 CALC. FROM EMISSION .0066 .006O .0126
EQUIVALENCE RATIO .097 .123 .105
LOADING M/P"N/V/E IT/5001 .393 .301 .335
CO«B EFFIC FROM EMISSIONS 90.220 90.817 99.011
CARBON DIOXIDE
PERCENT BY VOLUME. HET 1.3O 1.72 2.62
LB. C02 PER LB. OF FUEL 3.07 3.09 3.12
HEIGHT FLOH. LB./HR. OO6.0 562.0 773.2
CARBON MONOXIDE
PPM BY VOLUME. NET 203.7 260.6 202.6
LB. PER 1000 LB. OF FUEL 35.505 29.009 21.016
HEIGHT FLOH, LB./HR. 5.190 5.025 5.311
UNBURNEO HYDROCARBONS- PPM AS CARBON, HEIGHTS AS CHO
PPM BY VOLUME, HET 129.0 00.0 22.5
LB. PER 1000 LB. OF FUEL 10.755 5.092 .975
HEIGHT FLOM, LB./HR. 1.570 1.000 .202
RATIO LB HC/LB CO .3026 .10O2 .0055
NITRIC OXIDE INOI - HEIGHTS AS N02
PPM BY VOLUME, MET 10.2 10.5 26.2
LB. PER 10BO LB. OF FUEL 2.000 1.973 3.262
HEIGHT FLOM. Lfi./HR. .357 .359 .009
NITROGEN DIOXIDE (N02I
PPM BY VOLUME. HET 3.5 0.0 5.0
L8. PER 1000 LB. OF FUEL .039 1.503 .722
HEIGHT FLOH, LB./HR. .122 .270 .179
TOTAL OXIDES OF NITROGEN INONOZI AS N02
PPft BY VOLUME, HET 13.7 10.5 32.0
LB. PER 1000 LB. OF FUEL 3.203 3.076 3.900
HEIGHT FLOH, LB./HR. .079 .633 .960
.SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOH .00700 .00707 .00700
SMOKE NUMBER 10.50 16.90 19.30
CORRECTED I.EIGHT FLCH .02125 .02122 .02125
SMOKE NUMBER 29.50 29.50 3O.30
CORRECTED HEIGHT FLCH .03502 .03537 .03501
SMOKE NUMBER 39.20 03.00 05. ZO
CORRECTED HEIGHT FLCH .00959 .00952 .00957
SNOKE NUMBER 00.60 O9.00 5O.20
SMOKE NUMBER AT MAM.B23 32.10 35.10 30.50
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE MET VALUES.
Z. EQUIVALENCE RATIO CALCULATED FROM C02.CO.AND HC DATA
OEM PT,F<
S LN T.F
109
0.0
0.0
0.0
1021.0
01050.0
52.3
335,0
13.79
2.006
6.67
.0177
200.0
.0176
.259
.397
99.719
REDUCED
3.71
3.10
670.0
215.6
11.612
3.251
3.0
.092
.026
.0000
02.5
3.760
1.053
0.5
.390
• 111.
07.0
0.150
1.160
.00707
22.90
.02120
02.20
.03533
51. ZO
.00907
59.00
02.10
AND FUEL
' 60. REL HUN' 06.00 SPEC HUM- .015000
• 300.0 FLO.L/H' 10.160 SL TIM.S- 6.5800 ,
150
22.0
05.7
05.1 . " ~r •- - " 	
979.0
01050.0
50.7 ' - • 	 	 	 -- 	 -;
301.0
13.00
2.107 - .- - .—
6.57
.0169
200.0 	 ~- 	 -• -" "
.0160
.206
.301
99.636
3.51
3.13
076.5 . -- - - - _
259.6. ...
10.722
0.122
6.3 . " '" •" ' 	 -V
.2*0
.0139
34.0
3.500
.991
0.2 '•
.391
.110 	 	 .
02.2
3.931 	 . ... . . 	
1.101
.00707
19.30
.OZ120
37.30
.03533
00.20
•«*907 	 	 	 	 	
50.20
39.00
COMPOSITION.
                       3.MASS EMISSIONS OF NO. NOZ. AMD NO»N02 CALCULATED AS N02  FROM  CONCENTRATIONS HITH MOLECULAR HEIGHT OF M02 (O6.01I.
                       0.COMBUSTION EFFICIENCY CALCULATED FROM CO.AND UHC AS VAPORIZED ORIGINAL FUEL ON LBV Li FUEL BASIS.
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                       ENGINE' GTCP8S-98CK
                     DATA POINT  NUHBER
                     EMISSION RATE  LB/HR
                         CARBON  MONOXIDE
                         UNBURNEO HYDROCARBONS
                         OXIDES  OF  NITROGEN
                         NITRIC  OXIDE
                     POWER LEVEL HP
                     TOTAL CORRECTED HORSEPOWER
                                                S/N=
36179
   146

 5.190
 1.570
  .479
  .357
 0.00
 0.00
                                                               ••••  AIRESEARCH EMISSION TEST
                                                                COM3 P/Nc  698168-3 TEST DATE
   147

 5.425
 1.011
  .633
  .359
78.69
79.74
                     BRAKE SPECIFIC EMISSION INDEX LB/1000HP-HR
                         CARBON  MONOXIDE               0.000     68.948
                         UNBURNEO HYDROCARBONS         O.OOB     12.703
                         OXIDES  OF NITROGEN     -       0.800      8.040
                         NITRIC  OXIDE                  0.000      4.563
    148

  5.311
   .242
   .9*8
   .•09
195.49
198.11

 27.169
  1.237
  5.054
   .138
    149

  3.251
   .026
  1.164
  1.053
213.75
229.56

 15.210
   .121
  5.446
  4.925
 SUMMARY
 6-6-75
    151

  4.122
   .057
  1.101
   .991
229.74
244.10

 17.942
   .249
  4.791
  4.314
                                                                                                            FUEL=AV. KERO.
                                                                                                                              P BARO* 26.68
                         NOU"0. APPEARING IN BRAKE SPECIFIC  EMISSION INDEX COLUMN DENOTES AN IDLE CONDITION
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                     1    ENGINE HFR.I AIRESEARCH
                         MODEL NO. 1  GTCP»S-«»CK
                     .
                      '   FOELI ASTN 01655-73
                               TEST FACILITY! PrtX LACC2       INSTR. OESCRIP. 1   FEDERAL REG V3C N136   C»LC. DATE!
                               S/Ht  36179          ENGINE TYPE ICLASSII   APU             CALC. I.O.I     1
                              HAX SH»       200. * BLEED AIR EXTRACTION TO    iiso. DEC. F EGT
                                  ATONIC H/C RATIO!   1.921    LMVI     lti>7l. BTU/LB.     ADDITIVES! NONE
*-*-«
           EXHAUST EMISSIONS PE» EPA R4TEO NORK OUTPUT •• CODE OF FEDERAL REGULATIONS TITLE *fl PART 07
          .............................. EMjSSIOMS COMPUTED FROM TEST CONDITION NO.  5   ••••»••••«••••
                   HYOROCARBONS IHC AS CH»)             .030  .6. POLLUTANT PER 100) HP.-HR.
                   CARBON MONOXIDE ICO)               10.870  LB. POLLUTANT PER 1000 HP.-MR.
                   OXIDES OF NITROGEN INOX AS N02)     *.861  LB. POLLUTANT PER 1000 HP.-MR.
                                                                                                                                   17 JULY 1973 ••••••••••
.................................................  £N6IHE DESCRIPTION  •».•»»»•••»••».•
COMBUSTOR TYPE! TANGENTIAL CAN          P/NI  690168-3  SURFACE/VOLUME!  .725 SQ IN/CJ IN
ENGINE TOTAL SERVICE!     0.0  HR.   TIME SINCE ENGINE OVERHAUL!      0.0 HR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                         AIRCRAFT INSTALLATION
                                                   HFR. 1
                                                                                     MODEL NO. I
                                                                                                                      FUEL INJ. TYPEI
                                                                                                                            USER!
                                                                                                                                          DUAL ORIFICE
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                         ................................................op£(e|lIIONJlL rEST MM SUMMARY ••••»»••••»•»•••»»»»«*»»»••»••••••••»»»»•»-••••••'
                         GASEOUS EMISSION TEST NO.I     11    OATEI  6-7-7S       TIMEI    101*5      BARO. PRESS.!  20.560 IN. HGA.
                         AMBIENT AIR TEMP.l  91.0   OEG.  F        RELATIVE HUHIDITYI  63.00 PERCENT       SPECIFIC HUHIDITYI  .020000 LB. H20/LB. DRY AIR
                         AHBIENT AIR OUALITY   HYOROCARBONS IHC)! 0.0   PPMC    CARBON MONOXIDE ICO)I O.i   PPHV    OXIDES OF NITROGEN INOX)! 0.0   PPHV
                         SAMPLE LINE **•  TEMP.!  300.00 OEG. F.     FLOWUTEI   1*.16 LlTERS/MIN.     TRANSPORT TIME!    6.50 SEC.     LENGTH!   50.00 FT.
                                                     COMPUTES EMISSIONS
                         TEST  CONDITION                                          151       152       153       15*       155
                         PONER SETTING, CORRECTED  HP.                           0.00     70.92    190.62      0.00     *5.79
                         Nl  SPEED.  RPN                                      *1500.00  *1*30.00  *1090.00  *0910.00  *0000.00
                         FUEL  FLOW  IMEAS.I LB./HR.                            1*0.00    105.00    25*.00    295.BO    305.00
                         ENGINE CORE  INLET AIRFLCNICALC.)  LB./SCC.              6.15      6.02      S.*3      6.*9      6.**
                         COMPRESSOR INLET TEMP., OEG. F                         90.0      91.0      91.B      91.0      9B.B
                         COMPRESSOR DISCHARGE AIR  PRESSURE.  PSIA              61.07     62.36     61.37     50.67     52.70
                         COMPRESSOR DISCHARGE AIR  TEMP.. OEG.  F              33*.00    3*2.00    3*3.00    306.BO    307.BB
                         COMPRESSOR BLEED AIRFLON  INEAS.I  LB./SEC.              o.oo      B.BO      B.OO      2.*9      2.27
                         BLEED AIR  PRESSURE. PSIA                               0.00      O.BO      B.OO     09.35     50.«
                         BLEED AIR  TEMPERATURE, OEG. F                         -0.00     -B.BO     -B.BO    3*1.00    3*2.00
                         ENGINE EXHAUST CAS TEMP.. BEG. F                      *S9.0     562.0     795.B    1135.0    1132.0
                         EMISSION CONCENTRATION. MET ANALYSIS
                              HYDROCARBON IHC AS CH*I, PPMC                 1*7.000     07.00V    22.500      2.700       .900
                              CARBON  MONOXIDE ICO), PPNV                    ZS5.59Z    272.273   293.020    196.765    103.70*
                              TOTAL OXIDES OF NITROGEN INOX),  PPHV           12.*00     17.500    31.000     5B.1BO     SB.BOB
                              CARBON DIOXIDE IC02), PERCENT  BY VOL.           1.355      1.751     2.690      *.3Z3      *.207
                              NITRIC  OXIOE INO). PPNV                         6.000     10.000    25.000     *3.0BO     *7.SOB
                        EMISSION INDEX. LB. POLLUTANT/1000  LB.  FUEL
                              HYOROCARBONS IHC AS CH*>                       12.005      5.505      .9*6       .071       .02*
                             CARBON MONOXIDE ICO)                           36.763     30.581    21.550      9.095      0.569
                              TOTAL OXIDES OF NITROGEN INOX  AS N02)           2.930      3.229     3.7*5      3.00*      3.029
                        EMISSION RATE, LB. POLLUTANT/H*.
                             HYOROCARBONS IHC AS CH*I         .  .             1.709      1.033      .2*0       .021       .007
                             CARBON MONOXIDE ICC)                            S.**l      5.657     S.*7*      2.603      2.61*
                              TOTAL OXIDES OF NITROGEN INOX  AS N02)            .*3*       .597      .951      1.122      1.160
                        ENGINE WORK OUTPUT, HEAS. SHP                          g.oi      77.62    195.35      B.OO     *5.0B
                        ENGINE MORK OUTPUT. ISENTROPIC AIR  HP                 0.00       0.00      0.00    212.22    195.25
                        ENGINE NORK OUTPUT. TOTAL HP                           0.00      77.62    195.35    212.22    2*0.25
                        COMBUSTION EFFICIENCY. PERCENT {EMISSIONS)            9B.OO      9B.79     S9.*i     99.70     99.BB
                        F/A  (EMISSIONS!                                         .007       .009      .013      .020      .020
-------
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ENGINE' GTCP85-98CK S/N- 36179
RAT SHP* ZOO. RA EGT.F*
FUEL H/C= 1.9280 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POWER
CORRECTED SNAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OEG.F
SHAFT SPEED. Nl, RPM
COMPRESSOR OSCHG. PRES. .PSIA
1 COMPRESSOR OSCHG. TEHP.OEG F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOM, LB/SEC
1 COMPRESSOR MAP FLOM.LS/SEC
FA RATIO BASED ON HAP FLOH
CORRECTED FUEL FLOM , LB/HR
) FA RATIO CAt.C. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P**N/V/EIT/5%OI
1 COM3 EFFIC FROM EMISSIONS
CARBON DIOXIDE
) PERCENT BY VOLUME, MET
LO. COZ PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
) CARBON MONOXIDE
PPN BY VOLUME. HET
LB. PER 1000 IB. OF FUEL
' MEIGHT FLOM, '.B./HR.
UNBURNED HYDROCARBONS- PFH AS
PPf BY VOLUME, MET
) LB. PER 1000 LB. OF FUEL
MEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
) NITRIC OXIDE (NO) - HEIGHTS AS
PPH BY VOLUME. MET
La. PER 1000 LB. OF FUEL
) MEIGHT FLOM, LB./HR.
NITROGEN DIOXIDE INOZI
PPM BY VOLUME, HET
) L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, L6./HR.
1150.
.06822
151
0.1
0.0
0.0
%59.0
%1580.0
61.9
33%. 0
13.59
0.000
6. 29
.0065
1%8.0
.0067
.090
.1.25
90.075

1.36
3.06
%53.3

255.6
36.763
5.%«1
CARBON, Mil
11.7.0
12.085
1.719
.32*7
NOZ
6.0
l.%18
.210

6.%
1.512
.22%
COM3 P/N= 698168-3 TEST DATE 6-7-75 FUEL* AV. KERO. P BARO* 28.56
RAT SPO
L H V
152
39.5
70.9
77.6
562.0
%1%30.0
62. %
3%Z.O
13.6%
0.000
6.07
.0085
185.0
.0085
.125
.399
98.791

1.75
3.09
571.0

272. 3
30.581
5.657
iMTS AS
07.0
5.585
1.033
.1826

10.0
1.81.5
.3%1

7.5
1.38%
.256
> %1730.
c 18%70.
153
99.3
190.6
195.%
795.0
1.1090.0
61.%
31.3.0
13.76
0.000
5.28
.013%
25%. 0
.0130
.190
.356
99.1.10

2.70
3.12
791.9

293.0
21.550
5.%7«
CH%
22.5
.9%6
.2%0
.0%39

25.0
3.020
.767

6.0
.725
.18%
DEM PT.F*
s ,.N r.F*
15%
0.0
O.I
0.1
1139.0
-.0910.0
50.7
306.0
13.76
2.687
6.%7
.0206
295.0
.0205
.300
.%02
99.780
RECUCEO
%.3Z
3.1%
926.2

196.8
9.095
2.60,1

Z".7
.071
.OZI
.0070

1.3.8
3.326
.981

6.3
.1.78
.141
77. REL HUM* 65.00 SPEC HUH* .020000
300.0 FLO.L/H* 1I..160 SL TIH.S* 6.5000
155
22.9
%5.1
1.5.0
1132.0
%0800.0.
52.0
307.0
13.76
2.1.50
6,%2
.020%
305.0
.0203
.298
.389
99.796

%.29
3.1%
957.9

183.8
8.569
2.61%

Bg " ' ' ' ~
.02%
.117
.0028

%7.S
3.638 	 ' " 	 "
1.110

Z.5 --^-- ----.•= - --- 	 --
.191
.158
TOTAL OXIDES OF NITROGEN INO»N02I AS NOZ
) P»N BY VOLUME, NET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
) SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOM
SMOKE NUMBER
) CORRECTED MEIGHT FLON
SMOKE NUNBER
CORRECTED MEIGHT FLOM
> SMOKE NUMBER
CORRECTED HEIGHT FLOM
SMOKE NUNSER
; SMOKE NUNSER AT MAM. 023
1Z.%
2.930
• %3%

.0073%
11.1.0
.02111
25.30
.03519
32.50
.0%926
30.40
27.21
17.5
3.Z29
.597

.00705
15.10
.02111
31.30
.03525
30.60
.0%935
i.S.80
33.11
31.0
3.7%5
.951

.00705
15.70
.02115
32.50
.03525
%1.11
,01.933
%7.00
3%. 31
50.1
3.81%
1.122

.00707
22.90
.02122
%2.0I
.03536
52.%fl
«Q%951
61.21
%%.!!
51.1
3.829
1. 168

.01717
2%. 11
.OZI 21
%3.%0
.13535
5%. 20
.0%9%8
61. %l
46.11 ,
                    NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE NET VALUES.
                          2.EQUIVALENCE RATIO CALCULATED FRON CaZ.CO.ANO NC DATA AND FUEL COMPOSITION.
                          3.NASS EKISSICNS Of NO,  HOI,  »t3 NO»N02 CIRCULATED AS HO 2 FRON COHCEMTUI IONS OTH MOLECULAR UEICHT OF NOZ (tt.lll.
                          *.COM$USriON CFFICZENCr  CALCULATED UGH C3.ANO UMC AJ HPO*I2£0 OWSJAJAL FUEL ON  It/ It fUfi MSIS.
-------
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(D
ENGINE* GTCP05-9BCK S/N« 36179
DATA POINT NUMBER 151
EMISSION RATE LB/MR
CARBON MONOXIDE S.ttl
UNBURNEO HYDROCARBONS 1.709
OXIDES OF NITROGEN .63*
NITRIC OXIDE .Z10
POWER LEVEL HP
TOTAL CORRECTED HORSEPOWER
BRAKE SPECIFIC EMISSION INDEX LBS
CARBON MONOXIDE
UNBURNEO HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIDE
.00
.00
COMB P/N« o90160-3 TEST DATE 6-7-75
152

5.657
1.033
.597
.31.1
77.62
78. 9Z
153

5.6.74
.Z40
.951
.767
195.35
190.62
154

Z.603
.021
1.1 ZZ
.901
Z1Z.ZZ
229.00
OOOHP-HR
.000
.000
.000
.000
72. to*
13.311
7.695
4.397
zo.ozo
1.Z30
0.069
3.9Z7
!Z.6

b
                          NOTE»0. APPEARING  IN BRAKE SPECIFIC  EMISSION INDEX  COLUMN DENOTES AN IDLE CONDITION
 )


 >
                                                                                                                                                          	•    :
-------
                    )    ENGINE  MFR.I  AIRESEARCH
                       MODEL NO.I   GTCP85-98CK

                    )   FUEL I ASTM 01655-73
 TEST FACILITY! PMX LACC2        INSTR.  OESCRIP.I    FEDERAL  REG V38 N136
 S/NI  36179          ENGINE  TYPE  (CLASS)I   APU               CALC. I.O.I
MAX SHP       200. * BLEtO AIR EXTRACTION  TO   1151.  OEG.  F  E6T
    ATOMIC H/C RATIOI   1.928   LHVI      18471.  BTU/LB.      ADDITIVES! NONE
CALC. DATE! 6-7-75
   2
                       II         EXHAUST  EMISSIONS  PER  EPA  RATED WORK OUTPUT •• CODE OF FEDERAL REGULATIONS TITLE 40 PART 87
                       ..........,..,.......,„.,......,...,»... £MISSIONS COMPUTED FROM TEST CONDITION NO.  5   »»»•»»...».»..
                                           HYDROCARBONS  (HC AS  CH»)              .050  L8. POLLUTANT PER 1100 HP.-HR.
                    J                       CARBON  MONOXIDE  (CO)                10.937  I.B. POLLUTANT PER 1000 HP.-HR.
                                           OXIDES  OF  NITROGEN (NOX AS ND2)      4.911  LB. POLLUTANT PER 1110 .HP.-HR.
                                                                             17 JULY 197J ••••»•••••
                                                                            •*»«*»*•*•«•«•»»**»*•«••
                    ,   ,., .,,„..„„„.„„„„............................  EN6INE DESCRIPTION  •»••••••••••••»»
                       COMBUSTOR TYPE!  TANGENTIAL C»N           P/N1 698168-3   SURFACE/VOLUME I  .725 SD IN/CJ IN
                       ENGINE TOTAL SERVICE!     0.0   HR.    TIME  SINCE ENGINE OVERHAUL!      O.I HR.
                    )   ENGINE ASSEMBLY  AND  MAINTENANCE INFORMATION!
                       AIRCRAFT INSTALLATION »•• MFR.I
                                                                                    MODEL NO.I
                                                                FUEL INJ. TYPE!
                                                                                                                           USERI
                                                                                    DUAL ORIFICE
                       »..............................,..*......»»»»»»»oPERATIONAL TEST DATA SUMMARY *••••»*••••••••»•»»••••••••••»•••••»•»••»••»•»••
                       «flf?«? ^roS?-2S  IE!I  «°'»rr   I1     OATE1  6-7-75        TIMEI    21110      BARO. PRESS.!  28.560  IN. HGA.
                       AMBIENT AIR  TeMP.I  91.0   DEG.  F         RELATIVE HUMIDITY!  65.00 PERCENT       SPECIFIC HUMIDITY!   .020001 LB.  H20/LB.  DRY AM
                       AMBIENT AIR  8UALITY   HYDROCARBONS  (HOI  0.0   PPMC    CARBON MONOXIDE (CO) 1 0.0   PPMV    OXIDES OF NITROGEN  (NOXM  0.0   PPHV
                    )   SAMPLE LINE  •« TEMP.I   301.01 DEG.  F.      FLOM1ATEI   14.16 LITERS/MIN.     TRANSPORT TIME!    6.50 SEC.     LENGTH!    50.11 FT.
(D
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to
TEST CONDITION
) POKER SETTING, CORRECTED HP.
Nl SPEED, RPH
FUEL FLOW (MEAS.) LB./HR.
) ENGINE CORE INLET AIRFLOMICALC.) LB./SEC.
COMPRESSOR INLET TEMP., DEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
) COMPRESSOR DISCHARGE AIR T£MP., OEG. F
COMPRESSOR BLEED AIRFLOW (MEAS.) LB./SEC.
BLEED AIR PRESSURE. PSIA
) BLEED AIR TEMPERATURE, DEG. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION, MET ANALYSIS
> HYDROCARBON (HC AS CH4) . PPNC
CARBON MONOXIDE (CO) , PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPMV
CARBON DIOXIDE (C02). PERCENT BY VOL.
NITRIC OXIDE (NO), PPNV
EMISSION INDEX, LB. POLLUTANT/1011 LB. FUEL
HYDROCARBONS (HC AS CH4I
CARSON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS N02)
EMISSION RATE, LB. POLLUTANT/H*.
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
' TOTAL OXIDES OF NITROGEN (NOX AS N02I
ENGINE WORK OUTPUT, MEAS. SHP
ENGINE HORK OUTPUT, ISENTROPIC AIR HP
ENGINE NORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS!
156 157 158
0.01
41630.00
150.00
6.24
90.1
61.87
338.10
0.11
1.80
-0.81
452.0

145.500
252,101
13.000
1.355
9.201

11.966
36.274
3.173

1.795
5.441
.461
0.01
O.I*
0,88
91. li
.117
79.54

185.00
5.91
91.0
62.60
342.81
1.11
0.00
-0.10
562.0

87.001

17.111
1.782
11.211

5.489
38.338
3.181

1.116
5.612
.574
78.16
8.81
78.16
98.11
.189
198.94
41160.00
254.80

91.1
61.62
357.10
1.11
1.10
-0.00
.712.0

23.700
287.776
38.200
2.671
24.801

1.006
21.377
3.685

.256
5.431
.936
195.49

195.49
99.41
.113
159
1.11
40930.10
295.00
6.56
90.1
50.82
306.01
2.58

342.00
1122.8

3.300
199.101
58.111

4/!lOO

.889
9.357
3.867

.826
2.768
1.141
1.11
214.71

99^77
.828
161
45.71
40870.11
305.01
6.42
90.1
52.81 	 --
308.11
2.21
51.92
343.01
1131.1

1.511
116.552
51.888
4.388
48.888
.
.848
8.654
3.886 	

.812
2.639
1.185
44.99
196.35 	 "
241.34
99.79
" .Mi"" ~ ~ ~~" " '"
                                                                                                                                                                    )
                                                                                                                                                                    3
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ENGINE" GTCP05-9SCK S/N* 36171
RAT SHP» 268. RA EGT,F"
FUEL H/C> 1.9260 STOI F/A»
DATA POINT NUHBER
PERCENT MAX. CORRECTED POMES
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEHP. , DEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR OSCHG. PRES..PSIA
1 COMPRESSOR CSCHG. TEHP, DEC F
EXHAUST GAS PRESS., PSIA
CORRECTED BcEEO FLON, LB/SEC
COHPRESSOR PAP FLON.LB/SEC
FA RATIO BASED ON HAP FLOH
CORRECTED FUEL FLOH , LB/HR
) FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P"N/V/E
-------

ENGINE- GTCP85-98CK S/N= 36179
DATA POINT NUNBER
EHISSION RATE LB/HR
CARBON MONOXIDE
UNEURNED HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIDE
POWER LEVEL HP
TOTAL CORRECTED HORSEPOWER
BRAKE SPECIFIC EHISSION INDEX
CARBON MONOXIDE
UNGURNED HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIDE
156

E .441
1.795
.461
.326
0.00
0.00
L8/1IOOHP-HR
0.000
0.000
0.000
0.000
C019 P/N=698168-3
157

5.61Z
1.016
.57*
.376
78.16
79.54

71.804
1Z.99Z
7.33)
4.807
158

5.430
.256
.916
.769
195.49
198.94

27.775
1.307

j! 932
TEST DATE 6-7-75
159

2.760
.026
1.141
1.070
214.70
231.55

12.856
.1Z2
5.314
4.985
160

2.639
.012
1.185
1.116

257.54

10.937
.050

kl 622
                                                                                                              FUEL=AV. KERO
                                                                                                                                P BARD* ZS.S6
                                                                                                                                                                  I)
                                               IN  BRAKE  SPECIFIC  EMISSION  INOcX  COtUrtN  DENOTES AN IDLE CONDITION
to
U3
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                   ''    ENGINE HFR. I AI RESEARCH
                       MODEL NO.I  GTCP15-98CK

                       FUEL I ASTM 01655-73
 TEST FACUITYI PHX LACC2       INSTR. DESCRIP.I   FEDERAL  REG  V36  NlSfe    CALC.  OATEI
 S/NI  36179          ENGINE TYPE  (CLASS)t  APU              CALC.  I.D.I      S
HAX SMP       zoo. » BLEED AIR EXTRACTION TO    11SI.  OEG.  F EGT
    ATOMIC H/C RATIOI   1.928    LHVI     18470.  BTU/LB.     ADDITIVES! NONE
                                                                                       6-7-rs
                                  EXHAUST EMISSIONS PER EPA RATED  WORK  OUTPUT ••  CODE  OF FEDERAL  REGULATIONS TITLE 40 PART «7
                                 .............................. £HISSIONS  COMPUTED FROM TEST  CONDITION NO.   5   •»•*•••»••»•••
                                          HYDROCARBONS IHC AS CHM              .051 -B. POLLUTANT PER 1080  HP.-HR.
                                          CARBON MONOXIDE  ICOI               10.929 LB. POLLUTANT PER 1000  HP.-HR.
                                          OXIDES OF NITROGEN  (NOX  AS  NOZI     i>.»5>> LB. POLLUTANT PER 1000  HP.-HR.
                                                                                                                                  17 JULY 1973 »•••••••••
                       [[[   EN6IN£ DESCRIPTION  •••••••»••••••••
                       COHBUSTOR TYPE1 TANGENTIAL CAN          P/NI  698166-3    SURFACE/VOLUME I   .725 SQ IN/CU IN
                       ENGINE TOTAL SERVICE:     0.0  HR.   TIME  SINCE  ENGINE  OVERHAULI       0.0 HR.
                       ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                       AIRCRAFT INSTALLATION '•• NFR.I
                                                                                    MODEL  NO.I
                                                                FUEL INJ.  TYPE!
                                                                                                                           USER I
                                                                                    DUAL ORIFICE
 13
 PJ
vO-
 (D
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                       ......................................... •••••OPERATIONAL  TEST  DATA  SUMMARY  »•*•»»••••••*•••»•••••••••••»•••••»••••»••••••••
                       GASEOUS EMISSION TEST NO.I    11    DATE!  6-7-7S        TIME!     22130      BARO.  PRESS.I   28.580 IN.  HGA.
                       AMBIENT AIR TEMP.! 91.0  DEC. F        RELATIVE HUMIDITY!  65.00  PERCENT        SPECIFIC  HUMIDITY!  .020000  LB.  H20/LB.  DRV AIR
                       AMBIENT AIR QUALITY    HYDROCARBONS (HOI 0.0   PPMC     CARBON  MONOXIDE  (COII  0.0    PPMV     OXIDES OF  NITROGEN (NOXII  0.0   PPMV
                       SAMPLE LINE ••• TEMP.!  300.10 DEC. F.     FLOMRATEl    It.16 LITERS/NIN.     TRANSPORT  TIME!    6.50 SEC.      LENGTHS    50.11 FT.
TEST CONDITION
POWER SETTING, CORRECTED HP.
Nl SPEED. RPM
FUEL FLCM (MEAS.I LB./HR.
ENGINE CORE INLET AIRFLCMICALC.I LB./SEC.
COMPRESSOR INLET TEMP., OEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP., DEG. F
COMPRESSOR BLEED AIRFLON (NEAS.I LB./SEC.
BLEED AIR PRESSURE. PSIA
BLEED AIR TEMPERATURE. OEG. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION, MET ANALYSIS
HYDROCARBON (HC AS CHI.I , PPMC
CARBON MONOXIDE (COI , PPMV
TOTAL OXIDES OF NITROGEN (NOXI , PPMV
CARBON DIOXIDE (C02I , PERCENT BY VOL.
NITRIC OXIDE (NOI, PPMV
EMISSION INDEX, LB. POLLUTANT/1001 LB. FUEL
HYDROCARBONS (HC AS CHitl
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
EMISSION RATE. L8. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4»
CARSON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02I
ENGINE MOR< OUTPUT, MEAS. SHP
ENGINE WORK OUTPUT. IStNTROPIC AIR HP
ENGINE WORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS)
161 162 163
0.00
<>16



                                                                                                                                                                  '>


-------
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o
at
ENGINE' GTCP8S-98CK S/N= 36179
RAT SHP* 200. RA EGT.F- 1150.
FUEL H/C* 1.9260 STOI F/A*
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SMAFT HP
EXHAUST GAS TEMP., DEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR OSCHG. PRES..PSIA
COMPRESSOR OSCHG. TEHP.DEG F
EXHAUST GAS PRESS.. PSIA
CORRECTED BLEED FLOH, LB/SEC
COMPRESSOR KAP FLOH, LB/SEC
FA RATIC BASED ON MAP FLOH
CORRECTED FUEL FLOH , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P**N/V/EIT/540>
COM3 EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, NET
Li. C02 PER LB. OF FUEL
HEIGHT FLdU. LB./HR.
CARBON HONOXIDE
PPM BY VOLUME. HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, MET
L9. PER 1000 LB. OF FUEL
HEIGHT FLON, LB./HR.
RATIO L8 HC/L8 CO
.06822
161
0.
0.
0.
453.
416*6.
61.
337.
13.59
1.000
6.11
.0068
150.0
.0166
.100
.410
98.010

1.39
3.06
459.1

267.2
37.483
5.622
CARBON,
157.5
12.630
1.694
.3369
COMB P/N=698168-3 TEST DATE 6-7-75 FUEL«AV. HERO. P BARO. 28.56
RAT SPO'
L H V
162
39.9
79.9
78.6
568.0
41460.0
62.6
340.0
13.64
0.101
5.91
.0067
166.6
.6087
.127
.367
96.743

1.76
3.09
574.4

215.2
31.527
5.866
HEIGHTS AS
93.1
5.877
1.093
.166*
41730.
16470.
163
99.4
198.
195.
782.
41160.
61.
357.
13.75
0.080
5.36
.0132
254.0
.0129
.166
.349
99.419
•SUMMARY OF
2.67
3.12
792.1

262.6
21.995
5.333
CH4
23.4
.994
.252
.0473
OEM PT,F* 77. REL HUM: 65.00 SPEC HUM- .020101
S .N T,F« 300.0 FLO.L/Hs 14.160 SL TIM.S' 6.5011
164
1.
0.
0.
1116.
40920.
50.
305.
13. 76
2.701
6.47
.0207
295.0
.1201
.295
.399
99.775
REDUCED
4.24
3.14
926.1

196.6
9.263
2.733

3.0
.061
.126
.1067
165
23.1
46.2
45.5
1123.0
40860.0
53.6
306.6
13.76
2.456 	 	
6.42
.0207
366.0 " 	 	
.0205
.310
.385 ---..-_.
99.795

4.32
3.14
967.3 " ~" ' '

165.2
6.562 	
2.637

1.5 - - ' 	
.640
.112
.0046
NITRIC OXIDE (NOI - HEIGMTS AS N02
PPM BY VOLUME. NET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE (N02I
PPM BY VOLUME, HET
LS. PER 1000 LB. OF FUEL
HEIGHT FLON, LB./HR.
TOTAL OXIOES OF NITROGEN INO*
PPM BY VOLUME, MET
LB. PER 100B LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOU
SMOKE NUMBER
CORRECTED HEIGHT FLON
SMOKE NUMBER
CORRECTtO HEIGHT FLON
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
SMOKE NUMBER AT N*«8.123
18.5
2.426
.363

2.7
.622
.093
N02) AS N
13.2
3.142
.456

.11705
9.60
.02115
26.50
.03525
33.71
.06935
40.41
27. M
12.1
2.197
.469

5.6
1.017
.189
02
17.7
3.216
.596

.00715
15.70
.02115
38.11
.03525
39.60
.04944
45.68
33.11
26.1
3.185
.619

4.9
.598
• 152

31.6
3.763
.961

.10705
16.36
.1211*
32.50
.03530
42.20
.04942
47.61
34.91
47.4
3.665
1.161

2.7
.219
.162

56.1
3.674
1.143

.60704
22.30
.02112
41.00
.03527
51.61
.04931
59.61
43.71
46.6
3.646
1.123

3.1 	 	 •- 	 - -• 	 ' 	
.235
.073
•
51.1
3.161
1.195

.00716
27.10 ' ----- 	 	 _ ,
.12111
44.61
.03531
54.11
.14939
61.40 . ' " ----- 	 	 - -- - -
07.31
                  MOTES 1. ALL EMISSIONS CONCENTRATIONS ARE NET VALUES.
                        2.EQUIVALENCE S4TI0 CALCULATED FROM COZ.CO,MO MC DATA AND fW£t COMPOSITION.         '"""
                       i.HtSS MISSIONS OF MO, HOZ, AND NO»N02 CUCU^TfO AS ttOZ flUM COMCCNflUTIONS MTH NOLCCvlA* NHCHT Of *» <4*,fll.
                       k.conousno* imcitnci c«i.ew.«w r*w co.tw one ts MFCUUW M»I«U rag on t*v LI no. ustt.       .
-------
                                               S/N«
                                                    3617)
                                                        161
                                                              COM3 P/N*69816a-3   TEST 0»T£
                                                                  16Z
                                                                            163
                                                                                      16".
SUMMARY
6-7-75
   165
  ENGINE* GTCPB5-98CK
DATA POINT NUMBER
EMISSION RATE LB/HR
    CARBON MONOXIDE
    UNEURNEO HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIDE
PONcR LEVEL HP
TOTAL CORRECTED HORSEPOMER
BRAKE SPECIFIC EMISSION INDEX L3/1000HP-HR
    CARBON MONOXIDE              0.100
    UNBURNEO HYDROCARBONS        0.000
    OXIDES OF NITR06EN           0.000
    NITRIC OXIDE                 0.000
    NOTE"0. APPEARING IN BRAKE SPECIFIC EMISSION  INDEX COLOHN DENOTES  AN  IDLE CONDITION
                                                                                                          FUEL«AV.  KERO.
                                                                                                                             f 8»RO« Zt.51
                                                      5.622
                                                      1.89%
                                                       .456
                                                       .363
                                                      0.00
                                                      o.oo
5.864
1.093
.$98
.409
78.55
79.88
74. 651
13.915
7.611
5.203
5.333
.252
.961
.809
195.68
198.82
27.251
1.290
4.911
».13S
2.733
.020
1.103
l.Otl
210.53
231.21
12.737
.111
5.327
s.ooo
2.637
.012
1.195
1.123
241.27
257.01
10.929
.051
0.950
O. 650
pi
-------
                    )    ENGINE NFR.I AIRESEARCH
                       MODEL NO. >  GTCP05-98CK
                       FUEL I ASTH 01655-73
                               TEST FACILITY! PHX ..ACCZ        INSTR.  OcSCKIP.t   FEDERAL  REG V38 N136
                               S/NI  36179          ENGINE  TYPE  (CLASS) 1  APU               CALC. I.O.I
                              NAX SHP       ZOO. »  BLEED  AIR EXTRACTION TO    1150. DEC.  F  E6T
                                  ATONIC H/C RATIO!   1.92*   LHVI     18470. 8TU/L3.      AOOITIVESI NONE
C»LC. 0»TE« 6-18-75
   1
                                  EXHAUST EMISSIONS  PER  EPA  RATED  NORK  OUTPUT  >*  CODE  OF FEDERAL REGULATIONS  TITLE 40 PART 07
                                 ..............................  £HISSIONS  COMPUTED FROM TEST CONDITION NO.  5    ••••••••••••••
                                          HYDROCARBONS  (HC  AS  CH4I              .207  LB. POLLUTANT PER 1000 HP.-HR.
                                          CARBON  MONOXIDE  (COI               12.188  LB. POLLUTANT PER 1000 HP.-HR.
                                          OXIDES  OF  NITROGEN (NOX  AS N02)      4.770  LB. POLLUTANT PER 1000 HP.-HR.
                                                                                                                                  17 JULY 1973
[[[  EN6IM£  DESCRIPTION  ••••••»•••••••••
COM3USTOR TYPEI TANGENTIAL CAN          P/NI 698168-3    SURFACE/VOLUME I   .725 SO.  IN/CU  IN
ENGINE TOTAL SERVICEI     /.O  HR.   TIME  SINCE  ENGINE  OVERHAUL I       0.0 HR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                                                                                                                     FUEL INJ. TYPE!
                                                                                                                                         DUAL ORIFICE
                       AIRCRAFT INSTALLATION  *••  HFR.
                                                                                    MODEL NO. 1
                                                                                                                           USERI
13
fU
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                       ...,.............................».»•»..........OPERATIONAL TEST DATA SUMMARY • •••••••»•»•••»•«•»•»»••••»••••»•»•»••••••••»•••
                       GASEOUS EMISSION  TEST  N0.<     12    OATEI 6-18-75       TINE!    10.45      BARO. PRESS.I  28.440 IN. NGA.
                       AMBIENT AIR  TcHP.t  91.0   DEG.  F         RELATIVE HUMIDITYI  79.00 PERCENT       SPECIFIC HUMIDITY!  .025000 LB. HZO/LB. DRV AIR
                       AMBIENT AIR  QUALITY   HYDROCARBONS (HOI 0.0   PPHC    CARdON MONOXIDE (CO)I 0.0   P»NV    OXIDES OF NITROGEN (NOX)I 0.0   PPMV
                    1   SAMPLE LINE  **• TEMP.I  300.00 OEG. F.     FLONXATE!   14.16 LITERS/MIN.     TRANSPORT TIME!    6.50 SEC.     LENGTH!   50.00 FT.
-
TEST CONDITION
PONER SETTING, CORRECTED HP.
Nl SPEED, RPN
FUEL FLON (NEAS.I LB./NR.
) ENGINE CORE INLET AIRFLOW (CALC.) LB./SEC.
COMPRESSOR INLET TEMP., OEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
) COMPRESSOR DISCHARGE AIR TEMP., DEG. F
COMPRESSOR BLEED AIRFLON (NEAS.I ..B./SEC.
BLEED AIR PRESSURE, PSIA
) BLEED AIR TEMPERATURE. OEG. F
ENGINE EXHAUST GAS TEMP.. OEG. F
EMISSION CONCENTRATION, NET ANALYSIS
> HYDROCARBON (HC AS CH4I , PPNC
CARSON MONOXIDE (COI , PPNV
TOTAL OXIDES OF NITROGEN (NOX), PPMV
) CARBON DIOXIDE (C02I , PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSIOK INDEX, LB. POLLUTANT/1000 LB. FUEL
' HYDROCARBONS (HC AS CH4)
CARSON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS N02)
EMISSION RATE. LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CM
) TOTAL OXIDES OF NITROGEN (NOX AS N02)
ENGINE MORK OUTPUT, HE AS. SHP
ENGINE NORK OUTPUT, ISENTROPIC AIR HP
) ENGINE NOftK OUTPUT, TOTAL HP
CON8USIION EFFICIENCY, PERCENT (EMISSIONS)
FYA (EMISSIONS!

166
0.00
41590.00
155.00
6.09
91.0
61.96
331.00
0.00
0.00
-0.00
470.0
177.000
282.571
12.000
1.430
It. 000
13.761
38.434
2.681
2.133
5.957
.416
8.86
8.88
8.86
. 97.69
.167
ED EMISSIO
167
79.58
41180.00
190.00
5.66
92.0
61.67
336.00
0.00
0.00
-0.00
503.0
109.500
328.118
16.000
1.040
9.806
6.668
34.950
2.800
1.267
6.642
.532
76.61
0.66
76.61
96.59
.•69

168
198.22
41010.00
260.00
5.25
93.0
60.15
327.00
0.00
0.00
-•.00
830.0
27.000
306.306
29.000
2.862
28.500
1.070
21.238
3.303
.270
5.522
.859
194.49
1.66
194.49
99.41
.614

169
0.68
40820.00
295.00
6.45
91.0.
50.97
302.00
2.52
49.35
342.00
1147.0
7.500
203.798
47.006
4.J95
47.000
.195
9.263
3.589
.057
2.733
1.035
6.66
215.49
215.49
. 99. «u
.621

170
45.05
40720.00 	 	 	 .... _ 	 _ .._ _
310.08
6.42
09. •
53.27
260.08
2.29
51.31
330.68
1140.8
6.008 :
201.443
40.006
4.395
40.008
.156
9.157
3.506 • .,
.846 .
2.639
1.111
-------
 P>
iQ
 0>
O
vo
ENGINE* GTCPB5-98CK S/N' 3617)
RAT SHP< ZOO. RA E6T,F»
FUEL H/C* 1.9210 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OEG.F
SHAFT SPEED. Nl , RPM
COMPRESSOR DSCHG. PRES. .PSIA
COMPRESSOR OSCHG. TEMP, DEC F
EXHAUST GAS PRESS., PSIA
CORRECTED 8..EED FLO*. LB/SEC
COMPRESSOR MAP FLOH, LB/SEC
FA RATIO BASED ON MAP FLOH
CORRECTED FUEL FLOU . LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P**N/V/E(T/540I
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME. HET
LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME. HET
L3. PER 1010 LB. OF FUEL
HEIGHT FLOW, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
LB. PER 1001 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NOI - HEIGHTS AS
PPM BY VOLUME, HET
LB. PER 1101 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE (N02I
PPM 3Y VOLUME, HET
LB. PER 1101 LB. OF FUEL
HEIGHT FLOH, LB./HR.
1150.
.06822
166
0.
8.
8.
470.
41590.
62.
331.
13.53
0.008
5.74
.1175
155.0
.0071
.104
.389
97.889

1.43
3.06
473.7

282.6
38.434
5.957
COMB P/N«69B168-3 TEST DATE 6-18-75 FUEL-AV. KERO. P BARO« 28.44
RAT SPO> 41610. 3EH PT,F«
L H V'
167
39.
79.
78.
583.
41380.
61.7
336.1
13.61
I. Ill
5.49
.0096
190.0
.0090
.132
.371
91.593

1.84
3.18
585.4

328.1
34.958
6.642
CARBON. HEIGHTS AS
177.0
13.761
2.133
.3580
N02
11. 1
2.234
.346

2.0
.467
.069
TOTAL OXIDES OF NITROGEN INO«N02I AS NOZ
PPM BY VOLUME, HET
LB. PER 1111 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMCKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOW
SHCKE NUMBER
SMOKE NUMBER AT HA«1.023
12.1
2.681
.416

.00710
25.30
.02129
3Z.5I
.03548
42.20
.04968
47.10
36.90
119.5
6.661
1.267
.1917

9.8
1.715
.326

6.2
1.185
.206

16.0
2.181
.532

.00708
21.70
.02125
36.10
.03542
47.81
.84966
54.20
41.01
• 18471. S
161
99.1
198.2
194.5
830.0
1.1018.0
61.1
3Z7.1
13.75
1.811
4.96
.1146
268.0
.0138
.202
.357
99.407

2.86
3.12
810.6

306.3
21.238
5.522
CM*
27.8
1.078
.278
.0514

21.5
3.266
.164

~.S
.157
.115

29.1
3.313
.859

.08708
31.30
.121Z3
44.61
.03538
47.11
.04955
56.61
45.10
LN T,F»
169
0.0
O.I
1.0
1147.1
40820.0
51.0
302.0
13.74
2.729
6.17
.1224
295.0
.1218
.315
.368
99.765
REDUCED
6.48
3.16
926.1

203.8
9.263
2.733

7.5
.195
.057
.1211

67.1
3.519
1.035

0.0
0.110
1.111

47.8
3.589 .
1.135

.00716
27.71
.02119
44.68
.03532
56.68
.86951
66.30
49.11
84. «EL HUM- 79.11 SPEC HUM- .125001
300.0 FLO.L/H* 14.160 SL TIM,S» 6.5181
171
22.9
45.8 	
44.1
1146.8
40721.0
53.3
288.8
13.73
2.477
6.11
.8226
318.1
.1211
.315 . .... 	 	 	 	 	
.365
99. 771

4.41
3.14 . _• . .. 	 . ._ .. 	 ..
973.2

201.4 _ . _ _ .........._.._
9.157
2.839

6.1
.156
.848 . . ...... ...._ 	 	 	 	
.0178

68.8
3.586
1.111

1.1
8.880
1.881

48.8
3.586 . .
1.111

.81715
28.91
.12115
47.18 	
.13532
59.11
.14931 „ _..
68.71
51.31
                       NOTES 1. ALL EMISSIONS CONCENTRATIONS  ARE HET VALUES.
                             2.EQUIVALENCE RATIO CALCU-ATEO FROM C02,CO,ANO HC DATA AND FUEL  COMPOSITION.
                             3.MASS EMISSIONS OF NO, NOZ.  AND NO*NO2 CALCULATED  AS NOZ FROM CONCENTRATIONS  KITH MOLECULAR HEIGHT  OF  N02 166.111.
                             4.COMBUSTION EFFICIENCY CALCULATED FROM CO,AND UHC  AS VAPORIZED  ORIGINAL FUEL  ON  LB/ LB FUEL BASIS.
-------
                             ENGINE' GTCP85-91CK
                           OAT* POINT  NUMBER
                           EMISSION RATE IB/HR
                               CARBON  MONOXIDE
                               UNBURNEO HYDROCARBONS
                               OXIDES  OF NITROGEN
                               NITRIC  OXIDE
                           POHER LEVEL HP
                           TOTAL CORRECTED HORSEPOWER
                                                       S/H-
36179
   166

 5.957
 3. US
  .1.16
  .31.6
 0.00
 0.00
                                                                     ••*•  AIRESEARCH EMISSION TEST  SUMMARY
                                                                      COMB P/N*698168-3  TEST DATE 6-11-75
   167

 6.61.2
 1.267
  .532
  .336
78.01
79.58
                           BRAKE SPECIFIC EMISSION  INDEX  L3/1000HP-HR
                               CARBON MONOXIDE               0.000    15.134
                               UNBURN£0 HYDROCARBONS         0.000    16.31.0
                               OXIDES OF NITROGEN            0.000     6.120
                               NITRIC OXIDE                  0.000     ».177
    168

  5.522
   .271
   .859
   .8.10
-------
 (U
<£
 (D
                          EN6INE MFR.I AIRESEARCH
                         MODEL NO.I  GTCP85-98CK

                         FUCLI ASTM 01655-73
                               TEST FACILITY I PNX LACC2        INSTR.  OESCRIP.I   FEDERAL  REG V36 N136    CALC. DATE!
                               S/NI  36179          ENGINE TYPE  (CLASS)I  APU               CALC. I.D.I      2
                              MAX SHP       210. » BLEED AIR EXTRACTION TO    1158.  DEG. F EGT
                                  ATOMIC H/C RATIOI   1.928    LHVI     16471.  BTU/LB.      ADDITIVES* NONE
                                                                                                                                               6-18-75
                                    EXHAUST EMISSIONS PER  EPA RATED WORK  OUTPUT  *» CODE OF FEDERAL REGULATIONS TITLE 40 PART 87
                                    •*.•»»***»•*»•••»•*•»»»*»*»*»•  EMISSIONS COMPUTED FROM TEST CONDITION NO.  5   •••••••••••••«
                                            HYDROCARBONS  (HC AS  CH41              .211  ,.8. POLLUTANT PER 1000 HP.-HR.
                                            CARSON MONOXIDE  (COI               19.501  LB. POLLUTANT PER 1000 HP.-HR.
                                            OXIDES OF NITROGEN (NOX AS N3Z)      4.596  1.8. POLLUTANT PER 1000 rIP.-HR.
                                                                                                                                    17 JULY 1973
[[[  ENGINE  DESCRIPTION  •••••••••••••»••
COM3USTOR TYPEI TANGENTIAL CAN          P/NI  698168-3   SURFACE/VOLUME I   .725- SO. IN/CU IN
ENGINE TOTAL SERVICEI     0.0  HR.   TIME SINCE ENGINE OVERHAUL!       0.8 HR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                         AIRCRAFT INSTALLATION ••• MFR.I
                                                                                      MODEL NO.I
                                                                                                                       FULL INJ. TYPEI
                                                                                                                             USER!
                                                                                                                                           DUAL ORIFICE
                         ***>.••*..••»•«*.****»*»»»**«»>*»»»»*>*****>*»oPE*ATIONAL UST DATA SUMMARY •••••»»••»»•«»••»••»•»••••••»•••••••»»••••»•••••
                         GASEOUS EMISSION TEST NO. I    12     OATEJ   6-18-75       TIME!    13.15      BARO. PRESS.I. 28.440 IN. HGA.
                         AMBIENT AIR TEMP.! 91.0   DEG. F         RELATIVE  HUMIDITY!   79.00 PERCENT       SPECIFIC HUMIDITY!  .025000 LB. HZO/LB. DRY AIR
                         AMBIENT AIR QUALITY    HYDROCARBONS  (HC)I  0.0    PPMC     CARBON MONOXIDE (CO)I 0.0   PPNV    OXIDES OF NITROGEN (NOXII I.I   PPMV
                         SAMPLE LINE ••* TEMP.!  300.00 DEG.  F.      FLOHRATE!    14.16 LITERS/MIN.     TRANSPORT TIME!    6.50 SEC.     LENGTHS   50.01 FT.
TEST CONDITION
PONE* SETTING, CORRECTED HP.
Nl SPEED, RPM
FUEL FLCN (MEAS.I L6./HR.
ENGINE CORE INLET AIRFLCH ICALC.) LB./SEC.
COMPRESSOR INLET TEMP., DEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP., OEG. F
COMPRESSOR BLEED AIRFLOH (NEAS.I LB./SEC.
BLEED AIR PRESSURE. PSIA
8LE-0 AIR TEMPERATURE, OEG. F
ENGINE EXHAUST GAS TE1P., OEG. F
EMISSION CONCENTRATION, NET ANALYSIS
HYDROCARBON (HC AS CH4) , PPNC
CAPBON MONOXIDE (CO), PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPNV
CARBON 01 OX IDE (COZ) . PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSION INDEX, LB. POLLUTANT/1008 LB. FUEL
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS N02I
EMISSION RATE. LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4I
CARBON MONOXIDE (CO)
TOTAL DXIOES OF NITROGEN (NOX AS N02I
ENGINE HORK OUTPUT, MEAS. SMP
ENGINE NOR< OUTPUT, ISENTROPIC AIR HP
ENGINE HORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS)
171 17Z 173
0.08
41550.00
153.00
5.65
90.8
61.62
330.00
0.01
0.00
-1.00
472.0

165.001
290.393
13.001
1.472
13.011

12.476
36.428
2.625

1.989
5.878
.432
0.81
0.11
1.18
98.00
.117
79.56
41370.00
190.00
5.69
92. 0
61.37
334.10
0.00
0.00
-1.11
585.8

109.508
339.296
17.101
1.699
16.101

6.463
35.136
2.884

1.226
6.657
.5*6
77.99
0.11
77.99
96.61
.119
196.35
41010.00
260.00
5.20
92.1
59.90
342.00
0.00
0.00
-1.11
838.0

24.080
311.693
30.001
2.698
30.818

.942
21.484
3.16)1

.245
5.565
.686
194.44
8.10
194.44
99.41
.814
174
8.00
40620.00
294.08
6.49
92.0
50.77
315.68
2.50
46.95
356.06
1157.6

6.111
196.765
52.111
.4.323
52.111

.159
9.195
3.948

.047
2.674
1.161
1.10
220.24
221.24
99.77
.821
175
45.71
40710.00 	 __ 	
310.01
6.32
92. 1
53.27
268.68
2.23
51.71
331.61
1154.1 _.. 	 	

6.111
317.124
45.511
4.432
45.518

.154
14.261 	 	 	 _ 	
3.361

.146
4.421
1.642
-------
13
0)
vQ
0>
 ro
ENGINE' GTCP15-98CK S/N= 36179
RAT SHP* 200. RA EGT.F*
FUEL H/C* 1.9210 STOI F/A*
DATA POINT NUMBER
PERCENT MAX. CORRECTED POMER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OEG.F
SHAFT SPEEO, Nl, RPH
COMPRESSOR OSCHG. PRES.,PSIA
COMPRESSOR OSCHG. TEMP, DEC F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOH. LB/ScC
COMPRESSOR MAP FLOM.LB/SEC
FA RATIO BAStO ON MAP FLOM
CORRECTED FUEL FLOH , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING M/P"N/V/EIT/5*II
COM3 EFFIC FROM EMISSIOKS
CARBON DIOXIDE
PERCENT BV VOLUME, MET
LB. C02 PER LB. OF FUEL
HEIGHT FLOM, LB./HR.
CARBON MONOXIDE
PPM BV VOLUME. MET
L3. PER llOt 4.8. OF FUE^
HEIGHT FLOM, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME. MET
LB. PER 111* LS. OF FUEL
HEIGHT FLOM, LB./HR.
RATIO LB HC/LB CO
NITRIC CXIOE INOI - HEIGHTS AS
PPM BV VOLUME, HET
LB. PER 1080 LB. OF FUEL
HEIGHT FLOM, LB./HR.
NITROGEN DIOXIDE CN02I
PPM BY VOLUME, HET
LB. PER lOOt LB. OF FUEL
HEIGHT FLOM, LB./HR.
1150.
.06822
171
1.
0.
0.
472.
01550.
61.
330.0
13.54
0.810
5.76
.117*
153.0
.0073
.106
.395
98.002

l.«7
3.16
461.1

291.4
38.420
5.178
CONB P/N* 698161-3 TEST DATE 6-18-75 FUELMV. KERO. P BARO« 2(.4h
RAT SPO<
L H »s
172
19.
79.
78.
585.
41370.
61.4
334.0
13.61
0.01*
5.49
.0196
191.0
.0093
.136
.376
98.609

1.91
3.1*
585.%

339.1
35.036
6.657
CtRSON. HEIGHTS AS
165.1
12.478
1.919
.32*1
N02
13.1
2.125
.*32

0.1
0.110
0.010
109.5
6.463
1.221
.184$

16.1
2.71%
.516

1.0
.171
.032
• 41600. DEM PT.F* 84. R£L HUH* 79.10 SPEC HUH» .125001 t
= 18*70. S LN T,F* 300.0 FLO.L/M* 14.160 SL TIN,S* 6.5111 1 )
173
99.2
191.*
19*.*
831.1
41000.0
$9.9
342.0
13.7*
0.000
4.93
.01*6
260.0
.0139
.20*
.3*1
99.414

2.19
3.12
111.6

311.7
21.41*
5.565
CH4
2*.l
.942
.2*5
.1441

31.1
3.314
.111

1.0
0.111
0.011
17*
0.
8.
1.
1157.
40120.
50.
315.
13.74
2.716
6.15
.122*
294.1
.1215
.300
.361
99.772
REDUCED
4.32
3.1*
923.0

196.1
9.195
2.67*

6.1
.159
.1*7
.117*

52.1
3.9*8
1.161

I.I
I. Ill
0.011
TOTAL OXIDES OF NITROGEN INO*N02I AS N02
PPM BV VOLUME, HET
LB. PER 1010 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DAT*
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLON
SMOKE NUMBER
SMOKE NUMBER AT HOI. 129
unrce « At i CMrc'crnMC «*nui*f *JTS
13.0
2.125
.*32

.01716
16.91
.02118
31.11
.13529
37.31
.0*934
45.11
32.11
Arrnu* «a^
17.0
2.114
.548

.00706
22.9*
.02117
38.6*
.03527
49.40
.1494*
56.61
42.21
Ltr 9 u« i *
31.1
3.31*
.811

.11705
24.11
.12116
39.81
.03527
50.61
.1*935
57.11
43.41
52.1
3.9*1
1.161

.11715
21.91
.12115
41.21
. 13521
61.21
.0*939
6J. It
51. If
175
22.9 )
45.7
44.8 ' 	 " •
1154.1 )
40711.0
53.3
211.1 )
13.76
2.422 	 	 ' " 	 ' 	 ' '
6.16 )
.0225
311.1 " 	 "•"• - -• ' - - " 	 -
.1211 )
.319
.366
99.651 • )

*.*3 )
3.13
970.7 . ---.-.. ,

317.1
i4.26i " ~ •:
4.421 )

6.0
.154 . )
.1*1
.1111 " - .. . .
•\:
*5.5 '
J.36! — 	 -..-—-—.. 	 .
1.1*2 )j

•' 1.1 ' '—' "- - 	 ' - — 	 - - - — : 1
i.in ):
i.iii 	 r 	 	 	 . .. ;

*5.5 : )!
3.361 :
1.1*2 . .

.11714
27.71 ' :n
•12111 ',. J
41.21
.13522
56.61 ' >
.14939
63.91
*».51 >
NOTES 1. ALL EMISSIONS CONCENTgAUONS 4 Re HIT VALUES.
     Z.EOI/miENCC MTIO CH.CU.tTCO  FROM C02.C0.4NO HC OtTt 4NO FUEl CCNPOSITION.
     S.N4SS EMISSIONS OF MO.  N02, 4NO HO*It02 C44.CU.4TCO tS N02 MOM COWCMT-WTIOMS UlTH HOt.KW.Ut
     «.c0Mvm0M emcic*cr  ctt.cut.tTio no* co,tno one u vtrouzu MKINM. mi on is/ LI ntt
                                                                                                                 MCI6MT Of HOI
                                                                                                                 MSIS.
4*6.11*.
-------
•••  AIRESEARCH EMISSION TEST  SUMMARY
COMB P/N= 690160-3 TEST DATE   6-16-75
   172       173       171.        17S
  ENGINE' GTCP05-90CK      S/N*  36179
DATA POINT NUMBER                   171
EMISSION RATE LB/HR
    CARBON MONOXIDE               5.071     6.657
    UNBURNEO HYDROCARBONS         1.909     l.ZZO
    OXIDES OF NITROGEN            '.432      .51.8
    NITRIC OXIDE                   .432      .516
POWER LEVEL HP                    0.00     77.99
TOTAL CORRECTED HORSEPOWER        0.10     79.S6
BRAKE SPECIFIC EMISSION  INDEX  L3/1000HP-HR
    CARBON MONOXIDE               0.000    85.31,9
    UNBURNEO HYDROCARBONS         0.000    15.744
    OXIDES OF NITROGEN            0.000     7.021.
    NITRIC OXIDE                  0.000     6.611      	
    NOTE«0. APPEARING IN MAKE  SPECIFIC EMISSION INDEX COLUMN DENOTES AN IDLE CONDITION
                                                                                                              FUEL'AV. KERO.
                                                                                                                                P 6ARO«  2t.M>
5.565
• Z45
.800
.too
194. 1.1.
190.35
28.620
1.260
4.525
It. 525
2.67k
.01.7
1.161
1.161
220.21.
218.96
12.11.0
.212
5.270
5.270
4.421
.048
l.Qi.2
1.042
226.71
243.07
19.501
.211
4.596
4. 596
0)
-------
                        HOo
                        MODEL NO. 1

                     )   CUF. i »^TM n,,.« «
                     )   FUELt ASTM 01655-73
                                    0£SCRIP-1   "DEIttL *EG V38 N136    CALC.  0»TE.
                  ENGINE  TrPE  (CLASS) 1   AFU               CALC. I.D.I     3

?UP       "'* * 8CEE°  *IR  «™CnON TO   1150. DEC. F ECT
ATOMIC H/C R*TIOI   1.928    LHVI     18*70.  BTU/LB.      ADOITIVESI NONE
                                                                                                                                               6-18-75

                                   EXHAUST EMISSIONS  PER  EPA RATED KORK OUTPUT •• CODE OF FEDERAL REGULATIONS  TITLE 40 PART 87
                                  .**......*.*.....»............ EMISSIONS COMPUTED FROM TEST CONDITION  NO.   5   ..............

                                           HYDROCARBONS  IHC AS CH4»             .205  uB. POLLUTANT PER  1000  HP.-MR.

                                           Si?22c H?NOXiDE  CC01                18.291  LB. POLLUTANT PER  1000  HP.-HR.
                                           OXIDES OF  NITROGEN «NOX AS N02)     4.463  LB. POLLUTANT PER  1000  HP.-HR.
                                                                         17 JULY  1973 »»«»••»»••
                                                                               ENGINE DESCRIPTION
                                                  ,0   HR.
                        ENGINE ASSEMBLY AND MAINTENANCE INFOitHATIONI

                        AIRCRAFT INSTALLATION •»• MFR. 1
                                       0-HR5
                                                                                                                                                 °«"«
                                                                                     MOOEL N0.,
                                                                                                                             USER§
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AMBIENT AIR TEMP. 1 91.0 OEG. F RELATIVE HUMIDITY! 74.00 PERCENT SPECIFIC ' HUHIOITt 1 .025000 LB. H20/LB OR* AIM
AMBIENT AIR QUALITY HYDROCARBONS CHCH 0.0 PPKC CARBON MONOXIDE (COI1 0.0 PPMV OXIDES OF NITROGEN INOXIl'o 0 PPM*
) SAMPLE LINE *•• TEMP.I 300.00 OEG. F. FLONRATEI 14.16 LlTERS/MIN. TRANSPORT TIMEI 6.50 SEC. LENGTHI *50.00 FT. )
TEST CONDITION
1 PONER SETTING, CORRECTED HP.
Nl SPEED, RPM
FUEL FLON .
>-
>:
. :
- y
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• j.
I «yh
£
. ,*?
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ENGINE- GTCP85-98CK S/N
RAT SHP* 200. RA EGT,F=
FUEL H/C- 1.9200 STOI F/A-
OATA POINT NUMBER
PERCENT MAX. CORRECTED POMER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., DEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR DSCHG. PRES. ,PSIA
COMPRESSOR DSCHG. TEMP, DEC F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOM. LB/SEC
COMPRESSOR HAP FLOM.LB/SEC
FA RATIO BASED ON MAP FLOH
CORRECTED FUEL FLOM , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING M/P"N/V/E(T/5*0)
COM3 EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
L3. C02 PER LB. OF FUEL
MEIGHT FLOM, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, MET
L3. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
UNBURNEO HYCROCAR80NS- PPM AS
PPH BY VOLUHE, MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
RATIO LB HC/LB CO
NITRIC CXIOE (NO) - HEIGHTS AS
PPM BY VOLUHE, MET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
NITROGEN DIOXIDE IN02I
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUE..
MEIGHT FLOH, LB./HR.
> 36179
1150.
.06822
176
0.
0.
0.
*77.
1.1500.
61.
328.0
13.5*
0.000
5.72
.0075
155.0
.0072
.106
.396
97.955

1.1.6
3.06
1.73.9

Z95.7
39.312
6.093
CARBON, ME
168.0
12.768
1.979
.32*8
N02
10.0
2.18*
.339

.3
.066
.010
COMB P/N* 698166-3 TEST DATE 6-18-75 FUEL*AV. HERO. f BARD* 28.**
RAT SPO=
L H V =
177
39.8
79.5
77.9
585.0
*1 320.0
61.3
331.0
13.62
0.000
5.**
.0097
190.0
.0092
.136
.376
98.698

1.89
3.09
586.3

319.9
33.15*
6.299
[GHTS AS
100.5
5.95*
1.131
.1796

15.3
2.605
..95

1.2
.20*
.039
1.1600.
18*70.
178
99.1
198.3
19*. 3
839.0
-.0980.0
59.9
3*3.0
13.7*
0.000
*.87
.01*7
258.0
.01*0
.206
.3*2
99.1.01

2.92
3.12
00*. 2

322.6
21.93*
5.659
CH*
2*. 3
.9**
.2**
.0*31

30.0
3.351
.86*

0.0
0.000
0.000
DEM PT,F«
S LN T,F*
179
0.0
0.0
0.0
1158.0
1.0770.0
51.0
302.0
13.7*
2.737
6.15
.0227
297.0
.0211
.310
.365
99.762
OF REDUCED
*.*6
3.1*
932.2

213.3
9.5*9
2.836

6.0
.15*
.0*6
.0161

*7.5
3.*9*
1.030

0.0
0.000
0.000
6*. RE- MUM' 79.00 SPEC HUH' .025000
300.0 FLO.L/M' 1*.160 SL TIN.S- 6.5000
180
22.9
*5.7 	 	 	 	
**.e
1160.0
*C680.0 	 	
53.2
291.0
13.77 ........... 	
2.*15
6.00
.0223 . .. .. . ..; 	 	 ... _
310.0
.0216
.316 . .. __ 	
.360
99.670

*.S*
3.13 . 	 __ 1 ......
971.1

306.3 __ . . _._ 	 _...-..
13.**5
*.160

6.0
.151
.0*7 ......... 	 . .. .
.0112

*5.5
3. 281
1.017

0.0
0.000
0.000 	 . . ... ... . ..,._. .... . ..
TOTAL OXIDES OF NITROGEN (NC»N02> AS N02
PPM BY VOLUME. MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
SMOKE MEASUREMENT OAT*
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED MEIGHT FLOM
SMOKE NUMBER
CORRECTED MEIGHT FLCH
SMOKE NUMBER
CORRECTED MEIGHT FLON
SNCKE NUMBER
SMOKE NUMBER AT MA*0.023
10.3
2.250
.3*9

.00703
10.10
.02110
28.90
.03522
*1.00
.0*9*0
1.7.00
3*. 00
16.5
2.809
.53*

.00707
21.70
.02121
38.60
.0353*
*9.*0
.0*957
5*.20
1.1.20
30.0
3.351
.86*

.OC708
22.90
.02123
.1.00
.035*1
50.60
.3*961
56.60
*3.0fl
*7.5
3.1.9*
1.03B

.00700
32.50
.02123
50.60
.03536
57.00
.0*957
67.50
52.*!
1.5.5
3. £01
1.017

.00709 	 	 	
27.71
.02126
*5.80
.035*2
57.61
.0*967 . . .. .
65.11
*9.*0
                       NOTES 1.  ALL  EMISSIONS CONCENTRATIONS ARE MET VALUES.                           .     .      			
                             2.EQUIVALENCE RATIO CALCULATED FROM C02,C3,ANCi HC DATA AND FUEL COMPOSITION.
                             3.MASS  EMISSIONS OF NO, N32, AND NO*NOZ CAi;U-4T£D AS N02 FROM CONCENTRATIONS MITH  MOLECULAR  MEIGHT  OF  NO2 1*6.011.
                             *.COMBUSTION EFFICIENCY CALCULATED FROM CO.AND JHC AS VAPORIZED ORIGINAL FUEL ON LB/ LB  FUEL  BASIS. .            ...
-------
                                                                                                                                                                  j?
S/N= 36179
        176

      6.093
      1.979
       .3«9
       .339
      0.01
      0.10
                                                                     AIRESEARCH  EMISSION  TEST  SUMMARY
                                                                COMB P/N= 698168-3  TEST DATE   6-18-75
                                                                   177
                                                                             17S
                                                                                        179
                                                                                                  180
  ENGINE' GTCP85-98CK
DATA POINT NUMBER
ENISSION RATE LB/HR
    CARBON MONOXIDE
    UNBURNED HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIDE
POKER LEVEL HP
TOTAL CORRECTED HORSEPOWER
BRAKE SPECIFIC EMISSION INDEX LB/1000HP-MR
    CARBON MONOXIDE              0.000
    UNBURNED HYDROCARBONS        0.080
    OXIDES OF NITROGEN           0.000
    NITRIC OXIDE                 0.0(0
    NOTE"0. APPEARING IN BRAKE SPECIFIC EMISSION INDEX COLUMN DENOTES AN IDLE CONDITION
                                                                                                             FUEL'AV.  KERO.
                                                                                                                               P  BARO'  20.**
6.299
1.131
.53*
.1.95
77.90
79.5%
80.861,
It. 523
6.852
6.351,
5.659
.21.1,
.861,
.861,
191.. 35
198.25
29.118
1.25%
1,. 1.1.8
<».i»<»8
2.836
«0%6
1.138
1.038
Z 06. 1.2
223.97
13.739
.221
5.027
5.027
<». 168
.01,7
1.017
1.017
227.87
21,',. 19
18.291
.205
1..1.63
<>.<,63
(U
-------
                           ENGINE HFR.I AIRESEARCH
                          MODEL NO. 1  GTCP85-96CK
                          FUEtl ASTN 01655-73
                               TEST FAClLlTYl PMX LACCZ        INSIR.  DESCRIP.I   FEDERAL REG V38 N136    C»LC. 0»TEI  6-19-75
                               S/NI   36179          ENGINE  TYPE  (CLASS) I   APU              CAuC. I.O.I      1
                              MAX  SHP       zoo. »  BI.ELO  AIR EXTRACTION TO    lisa. DEC. r EGT
                                   ATOMIC  H/C RATIOI    1.939    LHVI      181.71).  BTU/LB.      AOOITIVESt NOME
                                     EXHAUST EMISSIONS  PER  EPA RATED MORlC OUTPUT •• CODE OF FEOERAi REGULATIONS TITLE 40 PART 87
                                    .............................. EMISSIONS COMPUTED FROM TEST CONDITION NO.  5   ••»•••••••••••
                                             HYDROCARBONS  (HC AS CH4)              .661  LB. POLLUTANT PER 1000 HP.-MR.
                                             CARBON MONOXIDE (CO)                20.906  LB. POLLUTANT PER 1000 HP.-MR.
                                             OXIDES OF  NITROGEN (NOX AS N02)     4.855  uB. POLLUTANT PER 1000 HP.-HR.
                                                                                                                                     17 JULY 1973
[[[   £NGIME DESCRIPTION  ..»»«»»..».».»».
COMBUSTOR TYPE! TANGENTIAL CAN           P/NI   698168-3  SURFACE/VOLUME 1  .725 SO IN/CU IN
ENGINE TOTAL SERVICES     0.0  HR.   TIME  SINCE ENGINE OVERHAUL!      0.0 HR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                          AIRCRAFT INSTALLATION ••* NFR. 1
                                                                                       MODEL NO. 1
                                                                                                                        FUEL INJ. TTPEI
                                                                                                                              USER*
                                                                                                                                            DUAL ORIFICE
 Hi
U3
 (D
                          .................................................OPERATIONAL TEST DATA SUMMARY ••»•»•»»••.••*»••••••••••»•••••••••••»•••»•»»•••
                          GASEOUS EMISSION TEST NO.I    13     DATE!   6-19-75       TIHEI    12.40      BARO. PRESS.!  22.130 IN. HGA.
                          AMBIENT AIR TEMP.I 59.0  0£G. F         RELATIVE  HUMIDITY!   70.00 PERCENT       SPECIFIC HUMIDITY!  .007500 LB. HZO/LB. DRY AIR
                          AMBIENT AIR QUALITY    HYDROCARBONS  (HCII  0.0    PPMC     CARBON MONOXIDE (CO) I 0.0   PPM I/    OXIDES OF NITROGEN (NOX)I 0.0   PPMV
                          SAMPLE LINE *•• TEMP.I  300.00 OEG.  F.      FLOURATEI    14.16 .ITERS/MIN.     TRANSPORT TIHEI    6.50 SEC.     LENGTH!   50.01 FT.
                          [[[ COHpUT£0 EMISSIONS
                          TEST CONDITION                                         101        182
                          POWER SETTING, CORRECTED MP.                           0.00      79.13
                          Nl SPEED, RPM                                     41770.00   41620.00
                          FUEL FLOM (HEAS.)  LB./MR.                           115.00     145.00
                          ENGINE CORE INLET  AIRFLOW(CALC.> LB./SEC.              4.79       4.65
                          COMPRESSOR INLET TEMP., DEG. F                         61.0       60.0
                          COMPRESSOR DISCHARGE AIR PRESSURE, PSIA              48.61      47.87
                          COMPRESSOR DISCHARGE AIR TEMP.. OEG. F              388.00     309.00
                          COMPRESSOR BLEED AIRFLOW (NcAS.) LB./SEC.              0.01       0.00
                          BLEED AIR PRESSURE, PSIA                               0.00       0.00
                          BLEED AIR TEMPERATURE, OEG. F                        -0.00      -0.00
                          ENGINE EXHAUST GAS TEMP., OEG. F                     499.0      617.0
                          EMISSION CONCENTRATION, WET ANALYSIS
                               HYDROCARBON (HC AS CH4), PPMC                178.500    106.500
                               CARBON MONOXIDE (CO),  PPMV                   31)6.306    347.806
                               TOTAc OXIDES  OF NITROGEN (NOX), PPMV          15.000     21.800
                               CARBON DIOXIDE (COZ),  PERCENT BY VOL.          1.343      1.769
                               NITRIC OXIDE  (NO), PPMV                       13.000     19.400
                          EMISSION INDEX,  LB. POLLUTANT/1000 LB. FUEL
                               HYDROCARBONS  (HC AS CH4)                      14.718      6.735
                               CARBON MONOXIDE (CO)                          44.100     38.479
                               TOTAL OXIDES  OF NITROGEN (NOX AS NOZ)          3.554      3.962
                          EMISSION RATE, LB.  POLLUTANT/HR.
                               HYDROCARBONS  (HC AS CH4)                       1.693       .977
                               CARBON MONOXIDE. (CO)                           5.082      5.579
                               TOTAL OXIDES  OF NITROGEN (NOX AS NOZ)           .409       .574
                          ENGINE  MORK OUTPUT, MEAS. SHP                         0.00      60.43
                          ENGINE  WORK OUTPUT, ISENTROPIC AIR HP                 0.00       0.00
                          ENGINE  WORK OUTPUT, TOTAL HP                          0.00      60.43
                          COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)           97.67      90.50
                          F/A  (EMISSIONS!                                        .007       .009
                                                                            103
                                                                         197.40
                                                                       41360.00
                                                                         200.00
                                                                          4.29
                                                                          59.0
                                                                         47.48
                                                                         390.00
                                                                          0.00
                                                                          0.10
                                                                         -0.00
                                                                         852.0

                                                                       16.500
                                                                       225.190
                                                                       37.500
                                                                         2.690
                                                                       37.000

                                                                         .695
                                                                       16.606
                                                                         4.542

                                                                         .139
                                                                         3.321
                                                                         .900
                                                                         150.62
                                                                          0.00
                                                                         150.62
                                                                         99.55
                                                                          .013
     104
    0.00
41250.08
  228.00
    5.52
    61.0
   42.47
  359.00
    1.04
   41.49
  383.00
  1040.0

  9.600
244.671
 51.000
  3.482
 51.000

   .314
 14.004
  4.795

   .069
  3.081
  1.055
    0.00
  Z02.44
  202.44
   99.64
    .017
     185
   45.46
41220.00
  228.00
    5.36
  _ 61. •
   44.19
  362.00
    l..SS_
   43.06
  306.11
  1000.0

 18.000
325.353_
 46.000
  3.327
 46.000 ._

-------
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1



)

)

)
FUEL H/C* 1.9280 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR DSCHG. PRES. ,PSIA
COMPRESSOR DSCH6. TEMP, DEC F
EXHAUST GAS PRESS. , PSIA
CORRECTED 3LEED FLOH, LB/SEC
COMPRESSOR MAP FLOH, LB/SEC
FA RATIO BASED ON HAP FLOH
CORRECTED FUEL FLOH , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING N/P»»N/V/E«T/54fl)
.COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, NET
LB. C02 PER LB. OF FUEL
PPM SY VOLUME, HET
HEIGHT FLOH, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, NET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITRIC OXIDE INOI - HEIGHTS AS
PPM BY VOLUME. HET
HEIGHT FLON, LB./HR.
NITROGEN DIOXIDE (N02I
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
.06822
181
0.0
0.0
0.0
1.99.0
*1770.0
*8.6
388.0
13.7*
0.000
*.59
.0070
115.0
.0067
.098
.428


1.3*
3.0*
306.3
*A.T uPS* ?i?i!' °L" PTtF= 51* REl- MUHs 7"'°'1 *SPEC HUM* .007500
L H V- 18*70. S LN T,F« 300.0 FLO.L/H: 1*.160 SL TIM,S« 6.5000
182
79.1
60.*
617.0
*1620.0
*7.9
389.0
13.79
0.000
*.33
.0093
1*5.0
.0887
.127



1.77
3.08
3*7.8
5.0S2 5.57J
CARBON. HEIGHTS AS
178.5
1*.718
1.693
N02
13.0
.35*
2.0
.47*
HEIGHT FLOH, LB./HR. .055
) PPM BY VOLUME, NET 15.0
LB. PER 1000 LB. OF FUEL 3.55*
HEIGHT FLOH, LB./HR. .1,09
)


1

>



SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
SMOKE NUMBER AT HA'0.023

.0070*
18.10
.02113
28.90
.03521
30,60
.0*920
*1.»0
31.90
106.5
6.735
.977
.1750
19.*
3.526
.511
2.*
.436
.063
21.8
3.962
.57*

.00703
18.10
.02109
30.10
.0351*
30.60
.0*911
*3.*fl
32.00
183
98 7

150.6
852.0
1.1360.0
*7.5
398.0
13. 88

3.95
.0129
377


2.70
3.13
225.2
16.606
3.321
CHI.
16.5
.695
.139
.0*19
37.0
*.*82
.896
.5
.061
.012
37.5
4.5*2
.908

.00703
19.30
.02108
32.50
.03513
3*. 90
.0*910
39.00
31.91
18*
«*B
0.0
42*5
359.0
9 1.91
* 7
.0187
220.0
.0166

99.6*3
REDUCED
3.46
3.13
24*. 7
3.081
9.6

.069
.0224
51.0
•..795
1.055
0.0
0.000
0.000
51.0
*.795
1.055

.00704
20.50
.02112
36.10
.03520
45.60
.04926
5*. 00
39.«
185
ZK"K
34.8
1000.0
41220.0
«••* 	 . _

.8182
220.0
.8159
*3»«
99.*89


s-iz .. . ._.._ . 	 • 	 :.._.
325.4
19.*26 ------ 	
4.27*
18.8 " ' " ~ 	 " 	 ~ " 	 ~ - - .-
.614

.0316 " 	
*'•» 	 	
*.S12 -' " ' "
.993
o.o 	 ~ 	 -
8. 000
0.000
46.0
4. 512
• 9jB3

.00703
15.71 . 	 	 -• -..-..
.02100
33.70
.03520
42.21
.04927
*5.80 • ' ~ ' " v " ' "
34.70 .
                                                                                                                                                >


                                                                                                                                                )
                        !'ff.uf^5f.!;rff fftC!fi!T£?.™°" ««.w.«o w DATA «ND FUEI. conPostrzoH.                -      —	

                                                       «££ f^f L"M ts *°z r*°* w&xiwva* HITM HOUCIM.M HCICNT or not uc.iii.
                                                       MW CO.tMO UHC it MWW/W MZCIKAV fltO. OH If/ If fUO, lUlIf
-------
  ENGINE* CTCP65-96CK      S/N« 36171
DATA POINT NUMBER                  111       10Z
EMISSION RATE L6/HR
    CARBON MONOXIDE              5.08Z     5.579
    UNEURNEO HYDROCARBONS        1.693       .977
    OXIDES OF NITROGEN             .i>09       .57%
    NITRIC OXIDE                   .35*       .511
POWER LEVEL HP                   0.00      60.1.3
TOTAL CORRECTED MORSEFONER       0.00      79.13
BRAKE SPECIFIC EMISSION INDEX LB/1003HP-HR
    CARBON MONOXIDE              0.000     93.323
    UNBURNEO HYDROCARBONS        0.000     16.159
    OXIDES OF NITROGEN           0.000     9.505
    NITRIC OXIDE                 0.090     6.i<59
                                                                   •••  AIRESEARCH EMISSION TEST SUHPARY
                                                                   COMB P/N. 696166-3 TEST DATE  6-19-75
                                                                                163

                                                                              3.3Z1
                                                                                .139
                                                                                .900
                                                                                .696
                                                                             150.62
                                                                             197.40

                                                                              22.050
                                                                                .923
                                                                              6.032
                                                                              S.951
    16*

  3.001
   .069
  1.055
  1.055
Z02.ll*
265.12

 15.219
   .3*1
  5.211
  S.Z11
                                                                                                                FUEL'AW.  HERO.
    1*5

  *.Z7*
   .135
   .993
   .993
20*.**
260.21

 Z0.906
   .661
  *.6S5
  *.65S
                                                                                                                                  P BARO» ZZ.tS
                             NOTE**0.  APPEARING  IN  BRAKE  SPECIFIC  EMISSION  INDEX  COLUMN  DENOTES AN  IDLE  CONDITION
0)
-------
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                          ENGINE MFR.I AIRESEARCH
                         MODEL NO. 1  GTCP85-98CK

                         FUEL! ASTM 01655-73
 TEST FACILITY! PHX LACC2        INSTR.  DESCRIP.I   FEDERAL  REG V38 N136
 S/Nl  36173          ENGINE  TYPE  (CLASS)I   APU               CALC. I.O.I
MAX SHP       200. » BLEED AIR EXTRACTION TO   1150.  OEG.  F EGT
    ATOMIC H/C RATIOI   1.928    LHVJ     18470.  BTU/LB.      ADDITIVES! NONE
                                                                                                         CALC.
                                                                                                            2
                                                                                                               OATEI 6-19-75
                                    EXHAUST EMISSIONS PL* EPA RATE3 WORK OUTPUT ••  CODE OF FEDERAL  REGULATIONS TITLE 40 PART 87
                                   .............................. EMISSIONS COMPUTED  FROM TEST  CONDITION  NO.   5   ..............
                                            HYDROCARBONS (HC AS CH»>            1.214 LB. POLLUTANT  PER  1000 HP.-HR.
                                            CARBON MONOXIDE (CO)               24.460 LB. POLLUTANT  PER  1000 HP.-HR.
                                            OXIDES OF NITROGEN INOX AS N02)     4.705 LB. POLLUTANT  PER  1101 HP.-HR.
                                                                                                           17-JULY 1973 »»»•«•»»»•
                                                                                                          .........«....««••*•*•«•
F2??«CST?STrP«or?r6ENTIACnCAN          P/Nt  "•««-3EMSURFACE/5"uNE?N .72"s"lN/CU*l"
ENGINE TOTAL SERVICE!     0.0  HR.   TIME SINCE ENGINE  OVERHAUL!       0.0 HR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                         AIRCRAFT INSTALLATION •••  HFR. 1
                                                                                     MODEL NO.I
                                                                                                                       FUEL INJ.  TYPEI
                                                                                                                             USER!
                                                                                                                                           DUAL ORIFICE
»«fruT ^roS5c2S TEH U°'Lr " 0»TEI 6-19-75 TIMEI 14125 BARO. PRESS.! 22.830 IN. HGA.
AMBIENT AIR TEMP, 1 59.0 OEG. F RE.ATIVE HUMIDITY! 70.00 PERCENT SPECIFIC HUMIDITYI .007500 LB H20/LB DRY ATB
AMBIENT AIR QUALITY MYOROCAR30NS (HC) 1 0.0 PPMC CARBON MONOXIDE (CO) 1 0.0 PPMV OXIDES OF NITROGEN OWXMO™ PP«V~ 	
SAMPLE LINE •» TEMP.I 300.00 OEG. F. FLOHUTEI 14.16 LITERS/MIN. TRANSPORT TI«EI 6.50 SEC. LENGTm Sfl.Ol™.

TEST CONDITION
POKER SETTING, CORRECTED HP.
Nl SPEED, RPH
FUEL FLOW (MEAS.) LB./HR.
ENGINE CORE INLET AIRFLON (CALC. ) LB./SEC.
COMPRESSOR INLET TEMP., DEC. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP., OEG. F
COMPRESSOR BLEED AIRFLON (MEAS.) LB./SEC.
BLEED AIR PRESSURE, PSIA
BLEED AIR TEMPERATURE. OEG. F
ENGINE EXHAUST GAS TEMP., DEG. F
EMISSION CONCENTRATION, NET ANALYSIS
HYDROCARBON (HC AS CHI,), PPMC
CARBON MONOXIDE (CO), PPMV
TOTAL OXIDES OF NITROGEN (NOX) , PPMV
CARBON DIOXIDE IC02). PERCENT BY VOL.
NITRIC OXIDE (NO), PPNV
EMISSION INDEX. LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS INC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN INOX AS N02)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS NO2)
ENGINE WORK OUTPUT, HEAS. SHP
ENGINE WORK OUTPUT, ISENTROPIC AIR HP
ENGINE WORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/t (EMISSIONS/
186 187 188
0.00
41760.00
114.00
4.73
60.0
48.36
386.00
0.00
0.00
-0.00
501.0
186.000
317.124
15.300
1.347
11.500
15.272
45.554
3.618

1.741
5.193
.412
0.01
0.00
0.18
97.59
.807
79.34
01610.00
144.00
4.60
57.0
48.12
388.00
0.00
0.00
-0.00
608.0
109.500
362.236
21.800
1.773
1C. 000
6.901
39.939
3.948

.994
5.751
.569
60.42
0.88
68.42
98.46
.8(9
196.97
41310.00
200.00
4.35
60.0
47.38
398.00
0.10
0.00
-0.00
852.0
17.4GO
222.787
38.000
2.661
37.001
.744
16.659
4.668

.149
3.332
.934
150.44
1.08
150.44
99.54
.813 .
189
0.00
1.1210.00
220.00
5.53
61.1
42.57
354.10
1.85
41. 49
379.10
1022.0
12.600
244.671
51.581
3.482
51.501
.412
14.103
4.841

.891
3.881
1.865
8.88
201.48
281.48
99.63
.817
191 ""' -------- --
45.51
41190*00
220.18 '"• 	
5.36
59.1
1,1.. 53
358.01
1,5* 	
43.31
381.08
992.1
33. BOO
379.978
44.500
3.327
44.000 	 	
1.124
22.643
4.356

.247
4.982 ---•--• - — -
.958
34. 73
168.93 	 --....
283.66
99.37
.816
                                                                                                                                                                    JQ
-------
01
                            ENGINE* GTCPB5-96CK      S/N' 36179
                           RAT SHf>*   200.     RA EGT.F* 1150.
                          FUEL H/C* 1.9210     STOI F/A= .06122
•••••   »IRESEARCH EMISSION TEST SUMKARY
  COMB f>/N« 698160-3 TEST DATE 6-19-75
 RAI SPO* 41600.    DEM PT,F»  51.
   L H V« 11470.    S LN T,F« 300.0
     FUcL'AV. KERO.    P BARO- 22.11
REL HUM«  70.00    SPEC HUM. .007511
FLO.L/N'  14.160   SL TIN.S«  6.5101
DATA POINT NUMBER
PERCENT MAX. CORRECTED POMER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., DEG.F
SHAFT SFEED, Nl, RPM
COMPRESSOR DSCHG. PRES. ,PSIA
COMPRESSOR DSCHG. TEMP, DEC F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOH, LB/SEC
COMPRESSOR HAP FLOM, LB/SEC
FA RATIO BASED ON MAP FLOH
CORRECTED FUEL FLON , LB/HR
FA RATIO C1LC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P"N/V/EIT/540I
COMB EFFIC FROM EMISSIOKS
CARBON OIOKIOE
PERCENT BY VOLUME, NET
L3. C02 PcR LB. OF FUEL
HEIGHT FLOM, LB./HR.
CARBON MONOXIDE
. PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM. LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, MET
LB. PER 1300 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NO) - HEIGHTS AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE (N02I
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
106
0.
0.
1.
501.
41760.
41.4
388.0
13.75
1.000
4.63
.0061
114.0
.0067
.091
.436
97.519

1.35
3.14
346.6

317.1
45.554
5.193
107
39.7
79.3
60.4
608.0
41610.0
41.1
388.0
13.10
0.011
4.27
.0094
144.0
.0017
.121
.416
91.455

1.77
3.07
4*2.4

362.2
39.939
5.751
CARBON, HEIGHTS AS
116.0
15.272
1.741
.3352
N02
11.5
2.714
.319

3.1
.197
.112
109.5
6.901
.994
.1721

11.0
3.260
.469

3.1
.618
.199
111
91.5
197.1
150.4
152.1
41310.1
47. «
390.0
13.00
0.000
3.95
.0141
200.0
.0121
.117
.370
99.543

2.66
3.13
625.2

222.1
16.659
3.332
CH4
17.4
.744
.149
.0446

37.1
4.545
.919

1.0
.123
.025
119
1.
0.
0.
1022.
41210.
42.
354.
13.10
2.430
5.09
.0109
220.1
.1166
.244
.405
99.634
REDUCED
3.41
3.13
611.1

244.7
14.003
3.011

12.6
.412
.091
.0294

51.5
4.041
1.065

0.0
0.000
0.010
190
22.1
45.5
34.7
992.1
41191.1
44.5
358.1
13.11
2.016
5.01
.0176
220.0
.0160
.234
.399
99. 369

3.33
3.12 	
615.4

311.1
22.643
4.912

33.1
1.124
.247
.1496

44.1
4.317
.941

.5 	 	 ~ " 	 "
.149
.on ' _. .. 	 _. 	 . :. 	 	 _. ... . . 	
TOTAL OXIDES OF NITROGEN 
-------

                             EMISSION RATE LB/Hft
                                 CARBON HONOXIOE
                                 UNBURNEO HYDROCARBONS
                                 OXIDES OF NITROGEN
                                 NITRIC OXIOE
                             POWER LEVEL HP
                             TOTAL CORRECTED HORSEPOMER
                             BRAKE SPECIFIC EMISSION INOeX  L3/1000HP-HR
                                 CARSON HONOXIOE
                                 UNBURNEO HYDROCARBONS
                                 OXIDES OF NITROGEN
                                 NITRIC OXIOE
                                 NOTE»»0. APPEARING IN BRAKE  SPECIFIC  EHISSION INOEX COLONN DENOTES AN IDLE CONDITION
5.193
1.7*1
.
.569
.*69
60.1.2
79.3*
•-HR
95.109
16.**7
9.*10
7.770
3.33Z
.1*9
.93*
.909
ISO.**
196.97

22. 1*7
.909
6.205
6.0*2
3.001
.091
1.06S
1.065
201. *0
26*. 30

15.290
.*50
5. 207
5.2*7
*.9SZ
.2*7
.950
.9*0
203.66
266.91

Z*.*60
1.21*
*.705
*.652
 TJ
 PJ
vQ
 n>
 to
 to

                                                                                                                                                                         I)
                                                                                                                                                                         I)
-------
 (U
03
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 to
 co
                       ENGINE HFR.I AIRESEARCH
                      MODEL NO.I  GTCP8S-98CK

                      FUELI ASTM 01655-73
                               TEST FACILITY! PHX  LACC2        INSTR. OESCRIP.I   FEDERAL REG V38 N136    C»LC. OATEI
                               S/NI   36179           ENGINE TYPE ICLASS)I  APU              CALC. I.O.I     3
                              MAX  SHP       200.  » BLEED AIR EXTRACTION  TO    usi. DEG. F EGT
                                   ATOMIC  H/C RATIOI   1.928    LHVI     18471.  BTU/L8.     AODITIVESI NONE
6-i»-7§
                                                                                                                                                                    >    A
           EXHAUST EMISSIONS PER  EPA RATED WORK OUTPUT •• CODE OF FEDERAL REGULATIONS TITLE 40 PART 87
          .............................. £MISSIONS COMPUTED FROM TEST CONDITION NO.  5   •••••••••••••«
                   HYDROCARBONS  (HC  AS  CH4)             1.3Z*  LB. POLLUTANT PER 1000 HP.-HR.
                   CARBON MONOXIDE  ICO)                Z8.487  LB. POLLUTANT PER 1000 4P.-HR.
                   OXIDES OF NITROGEN INOX AS NOZ)      4.597  LB. POLLUTANT PER 1000 HP.-HR.
                                                                                                                                  17  JULY 1973
                   )   ••
      ..............................................   £NGIN£ DESCRIPTION  ••••••••»•••••»•
COMBUSTOR TYPEI TANGENTIAL CAN           P/NI   698168-3  SURFACE/VOLUME!  .7Z5 SQ IN/CJ IN
ENGINE TOTAL SERVICE!     0.0  HR.    TIME SINCE  ENGINE OVERHAUL!      0.1 MR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                                                                                                                    FUEL  INJ.  TYPE!
                                                                                                                                         DUAL ORIFICE
                      AIRCRAFT INSTALLATION *•* !1FR. 1
                                                                                   MODEL NO.l
                      ........,.........,......„.....».».„„».......op£
TEST CONDITION
POWER SETTING, CORRECTED HP.
Nl SPEED, RPM
FUEL FLOW (KEAS.I L8./HR.
i ENGINE CORE INLET AIRFLOW ICALC. I L3./SEC.
COMPRESSOR INLET TEMP., DEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
) COMPRESSOR DISCHARGE AIR TEMP., DEG. F
COMPRESSOR BLEED AIRFLOW IMEAS.I LB./SEC.
BLEED AIR PRESSURE, PSIA
) BLEED AIR TEMPERATURE, DEG. F
ENGINE EXHAUST GAS TEMP., DEG. F
EMISSION CONCENTRATION. NET ANALYSIS
) HYDROCARBON IHC AS CH4) , PPHC
CARBON MONOXIDE ICO) , PPMV
TOTAL OXIDES OF NITROGEN INOX), PPMV
) CARBON DIOXIDE (C02) , PERCENT BY VOL.
NITRIC OXIDE INOI, PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
) HYDROCARBONS IHC AS CH4)
CA5BON MONOXIDE ICO)
TOTAL OXIDES OF NITROGEN INOX AS NOZ)
) EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS IHC AS CH4)
CARBON MONOXIDE ICO)
TOTAL OXIDES OF NITROGEN INOX AS NOZ)
ENGINE WORK OUTPUT, MEAS. SHF
ENGINE WORK OUTPUT, ISENTROPIC AIR HP
ENGINE WORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS)
191 192 193
0.00
41770.10
115.00
4.9Z
58.8
48.71
384.01
0.00
0.08
-0.08
488.0

183.000
314.403
15.000
1.306
12.800

15.486
-.6.51.7
3.648

1.781'
5.353
.419
0.00
0.81
0.00
97.55
.806
79.11
41610. BO
145.00
4.63
60.1
47.87
389.00
0.00
0.00
. -0.11
610.0

105.000
356.1,26
21.800
1.773
18.100

6.621
33.321
3.950

.960
5.702
.573
60.42
1.00
60.42
98.49
.809
196.74
41300.01
ZOO. 00
4.29
61.0
47.38
398.80
0.00
0.80
-0.01
857.0

16.500
222.787
38.008
Z.698
37.000

.696
16.431
4.603

.139
3.286
.921
150.41
8.01
150.41
99.55
.013
194
0.00
41210.10
zia.oi
5.49
59.8
42.52
352.01
1.85
41.34
377.80
1022.0

12.301
Z49.616
51.111
3.4)2
SI. 110 .

.402
14.284
4.794

.188
3.114
1.845
1.10
200.28
200.28
99.63
.017

~ - -
195 '
45.53
41171.11
2ZO.fl
5.38 -
56.8
44.34
357.18
1.54
43.48
381.08
987.8 	

36.811
44Z.773 	 : 	 	
43.511
3.319
43.118 	 	 	

1.231
26.477 	 .. . 	 _. ...
4.273
j
.271
5.825
.941
34.71 .........
169.76
204.47
99.27 ....._ 	 1_ _
.016 ,
-------
                                                                                                                                                                    V;
(D

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to
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 )


)
ENGINE- GTCP85-98CK S/N=
: 36179
RAT SHP* ZOO. RA EGT.F* 1150.
FUEL H/C= 1.9280 STOI F/As .
DATA POINT NUMBER
PERCENT MAX. CORRECTED POMER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP.. DEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR OSCHG. PRES. ,PSIA
COMPRESSOR OSCHG. TEMP, DEC F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOM, LB/SEC
COMPRESSOR HAP FLOH, LB/SEC
FA RATIO BASED ON HAP FLOM
CORRECTED FUEL FLOH , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P»»N/V/EIT/540»
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, WET
LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
06822
191
0.0
0.0
0.0
488.0
41770.0
48.7
384.0
13.75
0.000
4.58
.0070
115.0
.0065
.095
.428
97.547

1.31
3.04
349.4

314.4
46.547
5.353
COMB P/N= 698168-3 TEST DATE 6-1S-75 FUEL'AK. KERO. P BARO« 22.83 4
RAT SPD*
> 41600. OEM PT,F=
L H V* 18470. S i-N T,F*
192
39.6
79.1
60.4
610.0
41610.0
47.9
389.1
13.79
0.000
4.42
.0091
145.0
.0087
.127
.4Z3
98.494

1.77
3.07
445.7

356.4
39.321
5.702
UNBURNEO HYDROCARBONS- PPM AS CARBON. HEIGHTS AS
PPM BY VOLUME, HET
LB. PER 1010 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE INOI - HEIGHTS AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE IN02)
FPM BY VOLUME, HET
LB. PER 1800 LB. OF FUEL
HEIGHT FLOH, LB./HR.
183.0
15.486
1.781
.3327
N02
12. S
3.113
.358

Z.Z
.535
.062
105.0
6.621
.960
.1684

18.1
3.280
.476

3.7
.670
.097
193
98.4
196.7
150.4
857.0
41300.0
47.4
398.0
13.90
0.0*1
3.95
.0141
200.0
.0129
.190
.378
99.552

2.70
3.13
6Z5.3

Z22.8
16.431
3.286
CH4
16.5
.696
.139
.0423

37.1
4.48Z
.896

1.0
.121
,OZ4 _
194
0.0
0.0
0.8
1022.0
1.1210.0
42.5
352.0
13.89
Z.421
5.09
.0187
218.0
.0166
.244
.408
99.629
REDUCED
3.48
3.13
682.5

249.6
14.284
3.114

12.3
.402
.088
.0282

51.0
4.794
1.045

0.0
0.000
1.000
51. REL HUM= 70.00 SPEC HUM* .UifSUB
300.0 FLO, L/ MI 14.160 SL TIMtS* 6.5081
195
22.8
45.5 	
34.7
987.1
41171.0
44.3
357.0
13.89
Z.018
4.97
.0178
220.0
.0159
.233 ......
.398
99.269

3.31
3.11 . 	 	 _ . .
684.0

442.8 . . 	 	 - - 	
26.477
5.825
_ __ 	 	 - _ 	 	 	 —
36.0
1.231
• 2* X ..... 	 _. 	 . 	 . - — - -.-- 	 — . -- — -
.1465

43.1 ....'._._. . . 	
4.224
.929
_ _ 	 - . . ..._..-
.5
.049
.111 ' 	 . 	 J 	 ... ._
TOTAL OXIDES OF NITROGEN (NO+N02) AS NO 2
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOW, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOM
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOM
SMOKE NUMBER
15.0
3.648
.419

.00702
15.70
.02105
30.10
.03501
33.00
.14912
44.61
SMOKE NUMBER AT MA'1.023 32.41
NOTES 1. ALL EMISSIONS CONCENTS"*""" *"
2. EQUIVALENCE RATIO CALCU
X.MJSS EMISSIONS OF HOt Ni
«I.1VI» AtlC
LA TED FRUM
02, ANO M0<
21.8
3.950
.573

.01)702
18.11
.02115
31.30
.03501
39.81
.04912
47.01
38.0
4.603
.921

.00702
14.50
.02115
25.30
.13501
32.51
.14911
41.11
34.41 21.61
UCT tfAl 'tff
WET »*L
COZ, CO,
UtOZ CAL
vc?«
ANO HC OATA
CULATED AS N
51.1
4.794
1.145

.00712
21.70
.12115
36.71
.03518
47.61
.14909
53.01
40.11

ANO FUEL
02 FROM <
43.5
4.273 .. . 	
.941

.10701

24.11
.12114
43.41 .....__.__....
.13507
51.61


59.11
44.71

COMPOSITION.
JONCENTRATIONS NITM MOIECW.AR NEI6HT OF N02 (44.11I.
1 »
'

*

•\
f

•\
J


.









^
'



_ _ . - —


.. 	 _ 	 —
^
; '
,. _ 	 _





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^
*



17

. - - "
>'
.
	 •._ 	 .'
*
: 9

J>
                                 .                     ,
                               t.coNM/sriON efficiency CALCULATED FRO« CO.ANO UHC AS VAPORIZED ORICINAL FUEL ON it/ LB FUEL BASIS.
-------
                     •)   •*..
                                                    S/S*
                                                         36179
                                                            191

                                                          5.353
                                                          1.781
                                                            .1,19
                                                            .35a
                                                          O.Oa
                                                          0.00
•••  AIRESEARCH EMISSION TEST SUMMARY
COMB P/N« 698166-3 TEST DATE  6-19-75
   19Z
             191
                       19*
                                 195
SU
^
(D
NJ
UI
  ENGINE' GTCP65-96CK
DATA POINT NUMBER
EMISSION RATE LB/HR
    CARBON MONOXIDE
    UNBURNEO HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIDE
PONER LEVEL HP
TOTAL CORRECTED HORSEPOWER
BRAKE SPECIFIC EMISSION INDEX L3/1000HP-HR
    CARBON MONOXIDE              8.000
    UNBURNED HYDROCARBONS        0.000
    OXIDES OF NITROGEN           0.000
    NITRIC OXIDE                 0.090
    NOTE«0. APPEARING IN 8RAK£ SPECIFIC EMISSION INDEX COLUMN DENOTES AN~IJ>LE CONDITION
                                            FUEL'AV. KERO.
                                                              P BARO» 22.83
S.782
.960
.573
.476
60.42
79.11
94.367
15.890
9.461
7.872
3.266
.139
.921
.896
150.41
196.7*
21.8*8
.925
6.121
5.960
3.11*
.066
1.0*5
1.0*5
200.28
262. *6
15.5*7
.*36
5.216
5.218
5.625
.271
.9*1
.929
28*. 47
267.60
26.487
1.32*
4.597
4.5*4
                                                                                                                                                                   '£
-------
                          ENGINE HF*.<  AIRESEARCH
                         MODEL NO.I  GTCP85-98CK
                         FUEL I ASTN  01655-73
 TEST FACILITY! PHX LACC2        INSTR. DESCRIP.:  FEDERAL REG V38 N136
 S/Nt  36179          ENGINE  TYPE (CLASS)I  APU              CALC. I.O.I
MAX SHf>       ZOO. * BLEED  AIR  EXTRACTION TO    1150. OEG. F EGT
    ATONIC H/C RATIOI   1.9Z8    LHVI      18470. 6TU/L8.     AOOITIVESI NOME
CALC.
   1
      OATEt  6-19-75
                                     EXHAUST EMISSIONS  PER EPA RATED WORK OUTPUT •• CODE OF FEDERAL  REGULATIONS TITLE 40 PART 87
                                    .............................. EMISSIONS COMPUTED FROM TEST CONDITION  NO.   5   •••»•»••••••••
                                            HYDROCARBONS (HC AS CH-.)             .790  ^8. POLLUTANT PER  1000  HP.-MR.
                                            CARBON  MONOXIDE ICO)                CARBON DIOXIDE (CO2). PERCENT BY VOL.
NITRIC OXIDE (NO), PPNV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
.' EMISSION RATE, LB. POU.UTANT/HR.
HYDROCARBONS IHC AS CH4I
CARBON MONOXIDE (CO)
J TOTAL OXIDES OF NITROSEN (NOX AS NOZ)
ENGINE MOR< OUTPUT, NEAS. SHP
ENGINE WORK OUTPUT, ISENTROPIC AIR HP
>• ENGINE N0« OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/t CEHIUUMC*
)
196 197 198
0.00
417ZO.OO
132.00
5.53
61.0
55.48
386.00
0.00
0.00
-0.00
488.0

154.500
273.808
15.000
1.343
13.000

12.791
39.661
3.569

1.6«0
5.235
.471
o.oa
0.00
0.01
97.94
.117

79.24
-.1750.00
162.00
5.22
61.0
54.75
391.00
0.00
0.00
-0.00
609.0

88.500
306.306
21.500
1.765
20.000

5.629
34.082
3.930

.912
5.521
.637
68.93
0.00
68.93
90.70
.109

198.36
41240.00
228.00
4.90
60.0
54.01
396.00
0.00
0.00
-0.00
839.0

15.000
199.101
39.000
2.698
38.000

.633
14.697
4.729

.144
3.351
1.078
172.40
0.00
172.40
99.60
.013

199
0.00
41170.00
242.00
6.27
61.0
48.85
354.00
1.98
47.77
376.00
972.0

19.500
342.121
44.500
3.267
43.500

.677
20.793
4.443

.164
5.032
1.075
0.00
212. 96
212.96
99.45
.116

200
45.53
41130.00
250.10
6.14
58.0
50.72
355.00
1.74
49.35
377.01
981.0

21.100
317.124
44.500
3.297
44.000 	

.723
19.113
4.405

-------
(D
M
to
',
„„,»,„.„,.„„.„„„.„„..,.„„.„„„ mtSEIKCH EMISSION TEST SUMMARY .•**••..**••...*..•..........................
| ENGINE* GTCP85-98CK S/N> 36179
1 RAT SHP« ZOO. RA EGT,F> 1150.
FUEL H/C« 1.9200 STOI F/At .06822






)


3





)

)


)


1


!





)


)


)


1





1



OATA POINT NUMBER
PERCENT MAX. CORRECTED PONEM
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR DSCHG* PRES* *FSXA
COMPRESSOR DSCHG. TEMP, DEC F
EXHAUST GAS PRESS.. PSIA
CORRECTED BLEED FLOH, LB/SEC
COMPRESSOR MAP FLOH, LB/SEC
FA RATIO BASED ON MAP FLON
CORRECTED FUEL Fi.OH , LB/HR
FA RATIO CAcC. FROM EMISSION
EQUIVALENCE RATIO
LOADING N/P**N/V/E IT/5*OI
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BT VOLUME, NET
LB. PER 100P LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNEO HYDROCARBONS- PFN AS
PPH BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLO*, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NOI - HEIGHTS AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE INOZI
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
TOTAL OXIDES OF NITROGEN IHC+N
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT OATA
CORRECTED HEIGHT FLOH
SHOKE NUMBER
CORRECTED HEIGHT FLOW
SMOKE NUMBER
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
SMOKE NUMBER AT HAM. 023
196
0.
0.
0.
0«8.
01720.
55.5
386.0
13.60
0.000
5.23
.0070
132.0
.0066
.097
.388
97.9*5

1.3*
3.06
003.5

273.0
39.661
5.235
COHB P/N. 690166-3TEST DATE 6-19-75 FUEL««. KERO. P MRO- IS.«»
RAT SPO« 01600. DEN PT, . 51. REL HUM- 70.00 SPEC MUM. .•0750*
L H V« 18*70. S 4.N T, « 300.0 FLO.L/M- lo.l&fl SL TW.S- 6.5000
197
39.6
79. Z
60.
609.
01750.
5*.
391.
U.71
0.000
0.93
.0091
162.0
.0086
.126
.371
90.705

1.76
3.09
099.8

306.3
30.012
5.521
CARBON. HEIGHTS AS
150.5
12.791
1.688
.3225
N02
13.0
3.093
.008

2.0
.076
.063
021 AS NOZ
15.0
3.569
.071

.00712
16.30
.02136
27.70
.03558
01.00
.00980
03.00
32.20
88.5
5.629
.912
.1651

20.0
3.655
.592

1.5
.27*
.0**

21.5
3.930
.637

.00709
17.50
.02126
30.90
.035*2
.1.60
.04959
09.OO
36.10
190
99.2
198.*
172.*
839.0
012*0.0
so.o
396.0
13.11
0.000
0.07

228.0
.0129
.190
.302
99.599

2.70
3.13
713.5

199.1
10.697
3.351
CHO
15.0
.633
.144
.0*31

38.0
0.600
1.051

1.0
.121
.024

39.0
0.729
1.07*

.00707
13.30
.02121
26.50
.03535
31.90
.00907
Ol.OO
20.00
19
0.
0.
0.
972.
01170.
*8.
35*.
13.81
2.288
5.85
.017*
2*2.0
.0157
.230
.361
99.051
RtOUCEO
3.27
3.12
75*. 9

3*2.1
20.793
5.032

19.5
.677
.16*
.0326

03.5
4.343
1.051

1.0
.100
.024

00.5
4.4*3
1.075

.00707
20.50
.02121
39.80
.03535
50.00
.0*9*7
55.40
41.70
•-•jgg- ' - 	 	 •-- 	 - 	
zz.o
05.5
'39.5" ' ~ 	 	 	 -' -
901.0
41130.0
50.7
355.0
13.00
2.003 	 	 .-.--.. 	
5.70
.0175
250.0 	 	 	
.0150
.232
.365 " 	
99.407

3.30
3.12
780.5 '• ~ "" "

317.1
19.113 " 	 '" """"
4.776

21.0
.723
.101 	 _
.0379

44.8
4.356
1.009

.5 --.-.. 	
.049
.««

44.5
4.405
1.101

.00707
19.30 - 	
.02121
30.60 ..
.03534 " "" "" 	
47.60
.0*946
54.20
40.20
                                                                                                                                                                 )
                                                                                                                                                                 )
                                                                                                                                                                 )
                                                                                                                                                                 :>
                   NOTES 1.  ALL EMISSIONS CONCENTRATIONS ARE HET VALUES.
                         2.EQUIVALENCE RATIO CALCU-ATEO FROM C02.CO.AND HC OATA AND FUEL COMPOSITION.
                         3.MASS EMISSIONS OF NO, N02, AND NO»N02 CALCULATED AS N02 FROM CONCENTRATIONS H1TH MOLECULAR HEIGHT OF N02 (46.011.
                         O.COMBUSTION EFFICIENCY CALCULATED FROM CO.ANO UHC AS VAPORIZED ORIGINAL  FUEL ON  LB/ LB FUEL BASIS.        «**••"•
-------
                                                S/H=
                                                     36179
                                                        196
  ENGINE: GTCP8S-98CK
DATA POINT NUMBER
EMISSION RATE LB/HR
    CARBON MONOXIDE
    UNBURNEO HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIDE
POWER LEVEL HP
TOTAL CORRECTED HORSEPOM£R
BRAKE SPECIFIC EMISSION INDEX Vd/1000HP-MR
    CARBON MONOXIDE               O.ODO     80
    UNBURNEO HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIOE
                                                                •••   tIRESEARCH EMISSION TEST SUMMARY
                                                                COM3  P/N-  696168-3TEST DATE  6-19-75
                                                      5.235
                                                      1.688
                                                       .<«71
                                                       .".08
                                                      0.00
                                                      0.00
   197

 5.521
  .912
  .637
  .593
68.93
79.2*
                                                      O.ODO
                                                      0.000
                                                      0.000
   097
13.2Z8
 9.235
 8.591
    198

  3.351
   . l
  6. 094
    199

  5.032
   .161.
  1.075
  1.051
212.96
2-.S.72

 23.629
   .770
  5.0V8
  <>.93S
    200

  "..778
   . lai
  1.101
  1.089
228.89
263. ".3
                                                                                              20
    875
   .790
  0. APPEARING IN BRAKE SPECIFIC  EMISSION INDEX COLUMN DENOTES AN IDLE CONDITION
 to
vQ
 n>
 to
 CO
-------
> •   ENGINE NFR.I AIRESEARCH
    MODEL NO.I  GTCP1S-98CK

    FUEL! ASTH 01655-73
                                                    TEST FACILITY I PHX LACCZ        INSTR. OESCRIP.*   FEDERAL REG V3« N138    CAIC. DATE*
                                                    S/NI  3617)          ENGINE  TYPE ICLASS)I  APU              CALC. I.D.I     Z
                                                   HAX SHP        200.  »  BLEED AIR EXTRACTION TO    1158. DEG. F E6T
                                                       ATOMIC H/C RATIOS   1.928    LHVI     18471.  BTU/LB.     ADOITIVtSI NONE
                                EXHAUST-EMISSIONS FS.1  EPA RATED U04K OUTPUT •• CODE OF FEDERAL REGULATIONS TITLE •
                               .«**.**.*...*»•>»•*••••**•»»•* EMISSIONS COMPUTED FROM TEST CONDITION NO.  5   •••'
                                        HYDROCARBONS  IHC AS CH4)              .863  LB. POLLUTANT PER 1800 HP.-HR.
                                        CARBON MONOXIDE  (CO)                21.654  LB. POLLUTANT PER 1881 HP.-HR.
                                        OXIDES OF NITROGEN INOX AS N02)     4.851  LB. POLLUTANT PER 111! HP.-HR.
                                                                                                                   0 PART 87
                                                                                                                                 17  JULY  1973
                     [[[  £NGINE DESCRIPTION  *••••••••»»•••••
                     COMBUSTOR TYPE I TANGENTIAL CAN           P/N:  698166-3  SURFAC£/VOLUHt!  .735 SO. IN/CU IN
                     ENGINE TOTAL SERVICEI     0.0  HR.    TINE SINCE ENGINE OVERHAU.I      8.0 HR.
                     ENGINE ASSEMBLY AND MAINTENANCE  INFORMATION!
                     AIRCRAFT INSTALLATION ••• MFR.I
                                                                                  MODEL NO.I
                                                                                                  FUEL  INJ.  TYPE>
                                                                                                                         USERI
                                                                                                                       DUAL ORIFICE
                     ................................................Qp^ATjONAL TtST DATA SUMMARY ••••»••*••»••••.•»»•»»»••«••••••»•••»•»•••••••••
                     GASEOUS EMISSION TEST N0.«    14     OATEI   6-19-7$      T-IMEI    9.45       BARO. PRESS.I  25.980  IN. HGA.
                     AMBIENT AIR TEMP.I 59.0  DEG. F         RELATIVE HUMIDITY!  70.00 PERCENT       SPECIFIC HUMIDITY!   .107511 LB.  H2O/LB.  DRV AIR
                     AMBIENT AIR QUALITY    HYDROCARBONS  (HCI!  0.0   PPHC    CARBON MONOXIOt (CO)I 0.0   PPMV    OXIDES  OF NITROGEN  (NOXII  B.I   PPMV
                     SAMPLE LINE ••» TEHP.t  380.00 DEG.  F.      FLOHRATE:   14.16 I.ITERS/HIN.     TRANSPORT TIME!    6.51 SEC.     LENGTH!    50.18 FT.
 13
 fo
iQ
 (D
 to
 vo
TEST CONDITION
POWER SETTING. CORRECTED HP.
Nl SPEED. RPM
FUEL FLOW (PEAS.) LB./HR.
ENGINE CORE INLET AIRFLOW (CAtC.) LB./SEC.
COMPRESSOR INLET TEMP., OEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP., DEG. F
COMPRESSOR BLEED AIRFLOW IHEAS.) LB./SEC.
BLEED AIR PRESSURE. PSIA
BLEED AIR TEMPERATURE. DEG. r
ENGINE EXHAUST GAS TEMP., DEG. F
EMISSION CONCENTRATION, WET ANALYSIS
HYDROCARBON IHC AS CH4I . PPMC
CARBON MONOXIDE (CO) , PPMV
TOTAL OXIDES OF NITROGEN INOXt, PPHV
CARBON DIOXIDE (COZ) , PERCENT BY VOL.
NITRIC OXIDE (NO) , PPNV
EMISSION INDEX, LB. POLLUTANT/1800 LB. FUEL
HYDROCARBONS IHC AS CH4)
CARBON MONOXIDE ICO)
TOTAL OXIDES OF NITROGEN INOX AS N02)
EMISSION RATE, LB. POLLUTANT/MR.
HYDROCARBONS IHC AS CH4)
CARBON MONOXIDE ICOI
TOTAL OXIDES OF NITROGEN INOX AS N02)
ENGINE WORK OUTPUT, MEAS. SHP
ENGINE WORK OUTPUT, ISENTROPIC AIR HP
ENGINE WORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS)
201 202 213
0.00
41740.00
130.00
5.55
59.1
55.73
384.11
0.00
0.00
-0.11
491.0

154.511
279.983
14.880
1.314
14.588

13.056
Hi. 393
3.594

1.697
5.381
.467
0.00
0.00
0.00
97.88
.887
78.86
41558.00
163.88
5.2«
61.8
54.70
389.00
0.80
0.08
-1.81
618.8

88.588
306.306
20.500
1.769
19.018

5.615
33.999
3.738

.915
5.542
.619
68.68
8.81
68.60
98.71
.119
191.48
41250.00
228.01
4.88
68.1
53.86
394.10
1.80
0.08
-8.11
852.1

15.908
206.143
37.800
2.709
36.808

.668
IS. 153
4.l>68

.152
3.455
1.819
172.44
8. 11
172.44
99.58
.013
284
8.18
41448.81
242.81
6.29
58.8
48.85
352.01
1.99
47.87
374.88
975.8

21.118
347.806
43.581
3.255
42.581

.732
21.211
4.358

.177
5.133
1.855
8.88
214.14
214.14
99.44
.116
285
45.36
41180.11 .' 	 ._ 	
258.01
6.22
61. B
51.31
358.81
	 1.7* 	
49.69
379.11
978.B

22.511
322.598
44.888
3.237
43.588 	 	

.789
19.796
4.435

-------
(D
U)
O
ENGINE* GTCP85-98CK S/N= 36179
RAT SHP« ZOO. RA EGT,F= 1150.
FUEL M/C= 1.9Z80 STOI F/A* .06822
OATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR OSCHG. PRES..PSIA
COMPRESSOR DSCHG. TENP.OcG F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOH, LB/SEC
COMPRESSOR MAP FLOH, LB/SEC
FA RATIO BASED ON MAP FLOH
CORRECTED FUEL FLOH , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING W/P»»N/V/E(T/540)
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
LB. COZ PER LB. OF FUEL
HEIGHT FLOM, LB./HR.
CARBON HONOXIOE
PPM BY VOLUME. HET
L9. PER 1000 LB. OF FUE..
HEIGHT FLOH, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NOI - HEIGHTS AS
PPM BY VOLUME, HET
1.3. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
NITROGEN DIOXIDE 
PPM BY VOLUME, WET
LB. PER 1000 LB. OF FUEL
WEIGHT FLOH, LB./HR.
201
0.0
0.0
0.0
490.0
41740.0
55.7
384.0
13.64
o.oao
5.Z7
.0069
130.0
.0065
.095
.390
97.881

1.31
3.05
396.9

280.0
41.393
5.381
COMB P/N= 598168-3 TEST DATE b-19-75 FUEL=AV. KERO. P BARO« 25.98
RAT SPO* 41600. DEH PT.F= 51. REL HUM= 70.00 SPEC MUM« .007500
L H V= 19470. S LN T,F« 300.0 FLO,L/M= 14.160 SL TIM.S» 6.5000
202
39.4
78.9
68.6
610.0
41550.0
54.7
389.0
13.70
0.009
5.01
'.0090
163.0
.0386
.127
.390
98.708

1.77
3.09
592.9

306.3
33.9.9
5.542
CARBON, HEIGHTS AS
154.5
13.056
1.697
.3154
N02
14.5
3.521
.458

.3
.073
.009
88.5
5.615
.915
.1651

19.0
3.46*
.565

1.5
.273
.045
TOTAL OXIDES OF NITROGEN (NO»N02) AS N02
PPM BY VOLUME, MET
IB. PER 1010 L8. OF FUEL
HEIGHT FLOM, LB./HR.
SMOKE MEASUREMENT OATA
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOM
SMOKE NUMBER
CORRECTED HEIGHT FLCM
SMOKE NUMBER
CORRECTED HEIGHT FLOM
SMOKE NUMBER
SMOKE NUMBER AT HA*I.123
I"»T-TC 4 *i I fTMTCCTflki^ f i*--Uf»c AJT A ,
14.8
3.594
.467

.00706
15.70
.02118
30.10
.03530
38.00
.04941
48.60
33.41
tVTAU<*> * f*f
20.5
3.730
.609

.00705
16.90
.02114
34.90
.03522
44.60
.04929
50.61
37.11
203
99.2
198.4
172.4
852.0
41250.0
53.9
394.0
13.81
0.000
4.49
.0141
228.0
.0130
.190
.346
99.585

2.71
3.13
713.3

206.1
15.153
3.455
CH4
15.9
.668
.152
.0441

36.0
4.347
.991

1.0
.121
.028

37.0
4.468
1.019

.00703
13.30
.02109
28.90
.03514
37.30
.84929
19.11
30.11
204
0.0
0.0
0.0
975.0
41440.0
48.9
352.0
13.81
2.206
5.85
.0174
24Z.O
.0156
.229
.382
99.437
REDUCED
3.25
3. 12
754.7

347.8
21.211
5.133

21.0
.732
.177
.0345

42.5
4.257
1.030

1.0
.100
.024

43.5
4.358
1.055

.00703
22.90
.02109
42.20
.03513
51.80
.04919
60.21
44.70
205
22.7
45.4
39.5 ~ ' 	 -.-__._
978.0
41100.0
50.3
358.0
13.81
2.012 "
5.70
.0175
250.0 ' '" ' 	
.0155
.220
.367
99.465

3.24
3.1Z
780.2 - _ 	 _ 	

322.6
19.796 ~ ~ - -- - 	 	 	 	
4.949

2Z.5 . ----- .. . 	 	 __
.709
.197
.0399 ' V 	 	

43.5

4.385 	 	 	
1.096

.5 	 - - - ' -- - • -•
.050
.013
• w*» 	 ..____ _ --_.__. 	 	 	 	 	
44.0
4.435
1.109 	 	 	 	 	 ;

.00704
22.38 " 	 ------
.02113
39.88
.13520 	 : " " 	 ••• — •
50.68 • •
.04928
57.21 .-.--...- ..
42.81
    ALL  EMISSIONS CONCENTRATIONS ARE MET VALUES.
2.EOUIV41ENCE  R4TI0 C4lCUi4rEO FROM C02,C3,MO HC DATA AND FUEL COMPOSITION.
3.M4SS EMISSIONS  OF HO, N02,  4*0 NO»N02 CA4.O/..4TEO AS N02 FHOH CONCENTJUnONS «IM MOUCUL4H
•• 	*"- EFFICUNCf C4LCU4.4TEO  FKOH C0.4NO UMC «S »4PO«IZEO OW6IN41 FUCL ON  "iVtS FWEt
                                                                                                                     HCItHt Of HOI
                                                                                                                     MIS.
146.111.
-------
                      •»•••»••»••«*••*•»•.»*.•«•»•••.*••••.•».*....   URESEftuCH EMISSION TEST SUMMARY  •••••
                                                 S/N« 3617*
  ENGINE- CTCP85-98CK
OATA POINT NUMBER
EMISSION RATE LB/HR
    CARBON MONOXIDE
    UNBURNEO HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIDE
POMES LEVEL HP
TOTAL CORRECTED HORSEPOWER
BRAKE SPECIFIC EMISSION INDEX LB/1000HP-HR
    CARBON MONOXIDE               0.080    88.781
    UNBURNEO HYDROCARBONS         8.888    13.3*1
    OXIDES OF NITROGEN            8.011     8.881
    NITRIC OXIDE                  8.880     B.Z31
                                                                COHB P/N- 69*161-3 TEST DATE
                                                       5.3*1
                                                       1.697
                                                        .1.67
                                                        .1.58
                                                       8.88
                                                       0.8*
   zoz

 5.5I.Z
  .915
  .6*9
  .565
68.68
78.86
    Z*3

  3.655
   .1SZ
  1.119
   .991
i7z.*<>
194.1.8

 20.035
   .883
  5.9*7
  5.7*7
    Zt*

  5.133
   .177
  1.155
  1.13*
Zl*.l*
Z*6.38

 23.978
   .8Z7
  *.9Z5
  11.811
                                                                                              6-19-T5
                                                                                                 2BS
                                                                                                            FUEL-AX. KEKO.
                                                             »••••••••••••••••••••••
                                                              P BARO- SS.M
   .197
  1.1*9
  1.896
ZZ8.55
Z63.56

 21.65*
   .864
  6.851
  I.. 796
                          NOTE»»B. APPEARING IN BRAKE SPECIFIC EMISSION INDEX COLUMN DENOTES AN IDLE CONDITION
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                                                                                                                                                                  3-
                                                                                                                                                                  CD
-------
                       ENGINE  HFR.I AIRESEARCH
                      MODEL  NO.I  GTCP65-98CK

                      FUEL I  ASTM 01655-73
                                l,l\  «««      * L CCZ       INSTR'  °£SCRIP-'   FEDERAL REG V36 N136
                                S/N»  36179          ENGINE TYPE  (CLASSII  APU               CALC. 1.0 «
                               MAX  SHP       200. » BLEED AIR EXTRACTION TO    1150.  OEG. F EGT
                                   ATOMIC H/C RATIOI   1.926    LHVI     18470.  BTU/LB.      ADDITIVES. NONE
                                             CALC. DATEI 6-19-75
                                                3
                                                «.?" S" RATE° HORI< OUTPUr "  COD£  OF  FEDERAL REGULATIONS TITLE 40 PART  87
                                         .I................... rMISS10NS COMPUTED  FROM  TEST CONDITION NO.  5   »».»»».»»»»».»
                                         HYDROCARBONS (HC AS CH4)              .721 L8.  POLLUTANT PER 1000 HP -HR
                                         CARBON MONOXIDE (CO)               20.503 LB   POLLUTANT PER illl HP*!^'
                                         OXIDES OF NITROGEN (NOX AS N02)     4.758 LB.  POLLUTANT PER loSS HP -"5*.
                                                                                                            17 JULY 1973
                      COMBUSTOR TYPEI TANGENTIAL CAN          P/NI  698168-3  SURFACE/VOLUME?   725 SO IN/CU I«
                      ENGINE  TOTAL  SERVICE!     0.0  HR.   TIME SINCE ENGINE OVERHAUL!       0.0 H"
                      ENGINE  ASSEMBLY AND MAINTENANCE INFORMATION!
                      AIRCRAFT  INSTALLATION ••» MFR.I
                                                                                   MODEL  NO.I
                                                                                               FUEL INJ. TYPE<
                                                                                                                          USERl
                                                                                                                   DUAL ORIFICE
GASEOUS EMISSION TEST NO.,     14     D™"";"?''6'1"10?;!^"' "^'"""•^rPttSs"'"^.'^":^
AMBIENT AIR TEMP.I 59.0  DEG.  F         RELATIVE HUMIDITY!  70.00 PERCENT        SPECIFIc'luHIDIT?!
AMBIENT AI« QUALITY    HYDROCARBONS  (HC).  0.0   PPMC    CARBON MONOXIDE  (CO)I o!o        HUMID1TYI
SAMPLE LINE ••• TEMP.I  300.00 OEG.  F.      FIOWRATEI   K..16 LlTERS/MIN.
                                                                                                                          .007500 L8. H20/LB.  DRY  AIR
                                                                                                           PPMV    OXIDES OF NITROGEN (NOXII 0.0    PPHV
                                                                                                    TRANSPORT TIMEI    6.50 SEC.     LENGTH!    50.00 FT.
(D
00
Iv)
  TEST  CONDITION
  PONER SETTING, CORRECTED HP.
  Nl  SPEED,  RPM
  FUEL  FLCW  (MEAS.)  L8./HR.
  ENGINE CORE INLET  AIRFLCMCALC.)  LB./SEC.
  COMPRESSOR INLET TEMP., OEG. F
  COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
  COMPRESSOR DISCHARGE AIR T£MP., DEG. F
  COMPRESSOR BLEED AIRFLOW (MEAS.)  LB./SEC.
  BLEED AIR  PRESSURE,  PSIA
  BLEED AIR  TEMPERATURE,  DEG.  F
  ENGINE EXHAUST GAS TEMP.,  OEG. F
  EMISSION CONCENTRATION, WET  ANALYSIS
       HYDROCARBON (HC AS CH«>, PPMC
       CARBON MONOXIDE (CO), PPMV
       TOTAL  OXIDES  OF NITROGEN (NOX), PPMV
       CARBON DIOXIDE  (C02I. PERCENT BY VOL.
       NITRIC OXIDE  (NO).  PPMV
 EMISSION INDEX.  LB.  POLLUTANT/1000 L8.  FUEL
       HYDROCARBONS  (HC AS CH4)
       CARBON MONOXIDE (CO)
       TOTAL  OXIDES  OF NITROGEN (NOX AS NOZ)
 EMISSION RATE, L3.  POLLUTANT/HR.
      HYDROCARBONS  (HC AS CH4)
      CARBON MONOXIDE (CO)
      TOTAL  OXIDES OF NITROGEN  (NOX AS NOZ)
 ENGINE HORK OUTPUT, MiAS. SHP
 ENGINE MORK OUTPUT, ISENTROPIC AIR HP
 ENGINE WORK OUTPUT, TOTAL HP
COH8USTION  EFFICIENCY, PERCENT (EMISSIONS!
F/A (cfUSSIONSI
                                                                           COMPUTED  EMISSIONS
                                                        206
                                                       0.00
                                                   1.1711). 00
                                                     130.00
                                                       5.1.3
                                                       60.1
                                                      55.73
                                                     381,. 00
                                                       0.00
                                                       0.00
                                                      -0.00
                                                      493.0

                                                   150.000
                                                   271.. 83".
                                                    IS. 000
                                                     1.3*7
                                                    15.000

                                                    13.385
                                                    39.701
                                                     3.559

                                                    1.611
                                                    5.161
                                                     .<>63
                                                      0.00
                                                      0.01
                                                      0.01
                                                     97.90
                                                      .007
     207
   78.99
••151,0.00
  161,. 00
    5.26
    59.0
   5<>. 60
  388.00
    0.00
    0.00
   -0.00
   610.0

 88.500
306.306
 21.300
  1.773
 19.000

  5.611
 33.916
  3.871.

   .919
  5.562
   .635
  68.59
   0.00
  60.59
  90.71
   .009
     Z08
  198.35
41200.00
  228.00
    4.90
    59.0
   53.86
  391,. 08
    0.00
    a. oo
   -0.00
   853.0

 15.600
203.790
 38.200
  2.696
 38.000

   .650
 15.81.1
  4.631

  .150
  3.1.29
  1.056
  172.23
   0.00
 17Z.23
  99.59
   .013
     209
    0.00
41120.00
  242.00
    6.16
    61.0
   48.61
  354.00
    1.99
   47.63
  376.00
   963.0

 19.500
333.664
 45.000
  3.358
 44.000

   .659
 19.741
  4.373

   .160
  4.777
  1.056
   0.00
 213.34
 213.34
  99.40
   .016
      210
    AS.47
 41060.00
   250.00
     6.07
     58.0
    50.43
   355.00
     i-75_

   37&!oo
    963.0

  19.500
 317.124
  44.000
   3.358
  44.000

    .660

   4.356

    .165
   4.693
   1.089
   39.45
  189.42
  228.17
	99.51
    .016
                                                                                                                                                                  JB-
                                                                                                                                                                  fO
-------
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") »•»»»»»•«»•»»••»»»••»»•»•»*»*»»•»»••»••••»»»• JJ(
ENtINE» GTCP«S-9»CK S/H
i RAT SHP» 208. RA E6T.F-
• ' FUEL H/C« 1.9280 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POMER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OEG.F
SHAFT SPEED, Nl , RPH
COMPRESSOR OSCHG. PRES. .PSIA
' COMPRESSOR CSCHG. TEHP.DEG F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOH, LB/SEC
COMPRESSOR HAP FLOM, LB/SEC
FA RATIO BASED ON HAP FLOH
CORRECTED FUEL FLOH , LB/HR
FA RATIO CALC. FROM EMISSION
: EQUIVALENCE 6«TIO
' LOADING H/P»»N/Y/EIT/5i.fll
1 COM3 EFFIC FROM EMISSIONS
CARBON DIOXIDE
) PERCENT BY VOLUME, MET
L3. COZ PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
1 CARBON MONOXIDE
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH. LB./HR.
UNBURNEO HYDROCARBONS* PPH AS
PPM BY VOLUME. HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH. LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NOI - HEIGHTS AS
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
NITROGEN DIOXIDE (NOZ)
PPM BY VOLUME, MET
> L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
« 36179
1150.
.06822
Z06
o.a
0.0
0.0
1.93.0
1,1710.0
55.7
381.. 0
13.61.
0.030
5.Z7
.0069
130.0
.0067
.098
.390
97.9JO



RESEARCH EMISSION. TEST SUMMARY, »»»•»•»•••••••••••••••••»•••»•»••••••••»»••»•
COMB P/IU 698168-3
RAT SPO<
L H »«
207
39.5
79.0
66.6
610.0
1,151,0.0
51.. 6
366.0
13.69
0.000
1..99
.0091
161,. 0
.0087
.127
.381
98.711
U1600.
161,70.
zaa
99. Z
198.1,
172. Z
853. a
1.1200.0
53.9
39i>. 0
13.61
0.000
H.I. 9
.011,1
228.0
.0129
.190
.31.6
TEST DATE
OEM PI,F«
S LN T,F»
209
a. a
0.0
o.a
983.0
1.1120.0
1.6.6
351,. 0
13.61
2.292
5.77
.0178
21.2.0
.0161
.236
.376
99.566 99.1,76
6-19-75 FUEL«AV. KERO. P 8ARO» ZS.98
51. REL -»UIU 78.00 SPEC HUM- .117511
308.8 F4.0,<./H« 11,. 160 SL TIM,S« 6.5088
zta "'""• "
2Z.7
1.5.5
39.1,
963.0
1.1080.0
50.1,
355.8
13.61
2.010
5.78
.0176
250.0
.0161
.236
.368 	 ;
99.501

1.35
3.06
397.5

Z7I..8
39.701
5.161
1.77
3.09
506.0

306.3
33.916
5.562
CARBCN, HEIGHTS AS
150.0
12.365
1.610
.3130
NOZ
15.0
3.559
.1.63

0.0
0.000
0.000
83.5
5.601
.919
.1651

19.0
3.1,56
.567

3.3
.1,18
.069
2.70
3.13
713.3

203.8
15.01,1
3.1.29
CHI.
15.6
.656
.150
.01.38

38.0
*. 607
1.050

.2
.021,
.006
3.36
3. 12
755.3

333.7
19.71,1
*.777

19.5
.659
.160
.0331,

1.1.. 0
1..276
1.035

1.0
.097
.021,
3.36
3.12 	 .. .
760.7

317.1 __
18.770
I,. 693

19.5
.660
.165. 	
.0351

*«,. 8
I..276
1.069

.« - - — -- 	 	
.076
.019 	 ... 	 __
TOTAL OXIDES OF NITROGEN 




                                                                                                                                                                   *>
                      NOTES  1.  ALL EMISSIONS CONCENTRATIONS ARE MET VALUES.                                                              	
                            2.EQUIVALENCE RATIO CALCULATED FROM COZ.CO,AND HC DATA AND FUEL COMPOSITION.
                            3.MASS EMISSIONS OF NO,  N02, AND ;40»NOZ CALCULATED AS NOZ FROM CONCENTRATIONS MITH MOLECULAR HEIGHT OF NOZ (1,6.011.
                            l».COMBUSTION EFFICIENCY  CALCULATED FROM CO,AND UHC AS VAPORIZED ORIGINAL FUEL ON L3/ LB FUEL BASIS.
'S
-------
                                                  S/N=
                                                        J6179
                                                           206
'•••  AI9ESEARCH  EMISSION  TEST  SUMMARY
COM3 P/N= 690168-3  TEST DATE 6-19-75
                                                                     307
                                                                               200
                                                                                         209
                                                                                                   218
  ENGINE^ GTCPS5-98C<
DATA POINT NUMBER
EMISSION RATE L6/HR
    CARBON MONOXIDE
    UN6URNED HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIDE
POWER LEVEL HP
TOTAL CORRECTED HORScPOHcR
BRAKE SPECIFIC EMISSION INDEX LSS1000HP-HR
    CARBON HONOXIOE
    UNBURNEO HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIDE
    NOTE«0. APPEARING IN SRAH-i SPECIFIC EMISSION INDEX COLUMN DENOTES AN IDLE CONDITION
                                             FUEL=AV.  KERO.
                                                               P BARO» Z5.98
5.161
1.610
.463
.1*63
0.00
0.00
'1000HP-
0.000
0.000
0.000
0.000
5.562
.919
.635
.567
68.59
78.99
HR
31.097
13.393
9.263
8.263
3.429
.150
1.056
1.050
172.23
198.35
19.910
.871
6.131
6.090
4.777
.160
1.058
1.035
213.34
2*6.17
22.393
.748
4.960
4.850
4.693
.165
1.089
1.069
228.07
263.41
20.503
.721
4.750
4.673
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                     ENGINE KFR.l AIRESEARCH
                    MODEL NO.I  GTCPIS-98CK

                    FUEL I ASTH 01655-73
 TEST FACILITY< PHX L*CCZ       INSTR. OESCRIP.t   FEDERAL  RE6 VJ8 N1J6    CM.C.
 S/NI  36179          ENGINE TYPE  »CLASS11   APU               CAtC. I.O.t     1
MAX SUP       ZOO. » BLEED AIR EXTRACTION TO    115*. DEt. F E6T
    ATONIC H/C RATIOI    1.928     LHVI      181.70.  8TU/LB.     AOOITIVESt NONE
OATEI  t-lS-TS
                               EXHAUST  EMISSIONS  PER  EPA RATED HORK OUTt-UT »» CODE OF FEDERAL REGULATIONS TIKE  40  PART  87
                              .............................. ^MISSIONS COMPUTED FROM TEST CONDITION NO.  5   »••»••••••••••
                                        HYDROCARBONS  IMC AS CH4)              .596  L8. POLLUTANT PER 1000 HP.-HR.
                                        CARBON  MONOXIDE (COI               16.033  iB. POLLUTANT PER 1000 riP.-HR.
                                        OXIDES  OF  NITROGEN (NOX AS NOZ)     "..93".  LB. POLLUTANT PER 1000 HP.-HR.
                                                                             17 JULY  1973
                    [[[  ENE1N£ DESCRIPTION  «•»»»•••»»•••»••
                    CONBUSTOR TVPEI  TANGENTIAL  CAN          P/N1  698166-3  SURFACE/VOLUMEJ  .725 SO  IN/CO  IN
                    ENGINE TOTAL  SERVICE*     0.0   HR.    TIHE SINCE ENGINE OVERHAULS      0.0 MR.
                    ENGINE ASSEMBLY  AND  MAINTENANCE INFORHATIONI
                    AIRCRAFT INSTALLATION  »»»  NFR.I
                                                                                 MODEL NO.I
                                                                FUEL INJ. TYPE I
                                                                                                                         USERI
                                                                                     DUAL  ORIFICE
f"
ua
(D
u>
en
                    ................................................OPERATIONAL TEST DATA SUMMARY »»»»»»»»•»•»»»»»•«»»*••»«»«»»»»•»»••»»••»»»»•»»»
                    GASEOUS EMISSION TEST NO.«     15     OATEI   6-15-75      TIMEI    13.00      8ARO. PRESS.I   Z8.6ZO  IN.  HGA.
                    AMBIENT AIR TEMP.I  59.0   DEG.  f         RELATIVE HUMIDITY:  70.00 PERCENT       SPECIFIC HUMIOITYI   .007500  LB.  H20/LB.  DRY AIR
                    AMBIENT AIR QUALITY    HYDROCARBONS  (HOI  0.0   PPMC    CARBON MONOXIDE (COX 0.0   PPHV     OXIDES OF  NITROGEN  (NOXIt  0.0   PPNV
                    SAMPLE LINE *•* TEMP.I  300.00 DEC.  F.      FLOMRATEl   14.16 uITERS/MIN.     TRANSPORT TIMEI     6.50 SEC.     LENGTHI    50.00 FT.
TEST CONDITION
PONER SETTING. CORRECTED HP.
Nl SPEED. RPM
FUEL FLOW IMEAS.I LB./HR.
ENGINE CORE INLET AIRFLOHICALC.) LB./SEC.
COMPRESSOR INLET TEMP., DEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP., DEG. F
COMPRESSOR BLEED AIRFLOW IME1S.) LB./SEC.
BLEED AIR PRESSURE. PSIA
BLEED AIR TEMPERATURE. OEG. F
ENGINE EXHAUST GAS TEMP., DEG. F
EMISSION CONCENTRATION, NET ANALYSIS
HYDROCARBON CHC AS CHo) , PPMC
CARBON MONOXIDE (COI , PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPMV
CARBON DIOXIDE CCOZ) , PERCENT BY VOL.
NITRIC OXIDE (NOI. PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CHliI
CARBON MONOXIDE ICOI
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS IMC AS CHI. I
CARBON MONOXIDE ICOt
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
ENGINE WORK OUTPUT, M£AS. SHP
ENGINE MORK OUTPUT, ISENTROPIC AIR HP
ENGINE MORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS)
Zll 212 213
0.00
41610.00
iti.oo
5.91
59.0
60.88
378.00
0.00
0.00
-0.00
490.0

124.500
Z47.mo
16.000
1.347
It. 900

10.319
35.838
3.811

1.455
5.053
.537
0.00
0.00
0.00
98.25
.007
79.12
>»1-.30.0I)
175.00
5.54
59.0
59.90
384. DO
0.00
0.00
-0.00
61Z.O

75.000
277.404
23.200
1.800
21.000

4.689
30.340
4.168

.821
5.310
.729
75.68
0.00
75.68
98.87
.009
198.60
41070.00
244.00
5.14
59.0
58.92
392.00
0.00
0.00
-0.00
462.0

14.400
190.717
41.200
2.752
40.000

.596
13.809
4.900

.145
3.369
1.196
189.97
0.00
189.97
99.62
.013
Z14
0.00
40960.00
261.00
6.66
60.0
53.03
349.00
Z.18
51.65
370.00
1000.0

13.500
267.179
-.9.000
3.389
47.800

.453
15.698
4.7Z9

.118
4.097
1.234
0.00
230.74
230.74
99.59
.016
215
45.61
40900.00
272.00
6.61
58.0
54.99
352.0(
1.95
53.67
373.01
990.*

16.500
285.169
47.500
3.389
47.000 .... _ 	

.554
16.744
4.581

.151
-------
ft)
ENGINE- GTCP85-98CK S/N* 36179
RAT SHP= 200. RA EGT,F= 1150.
FUEL H/C* 1.9280 STOI F/»= .06822
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., DEG.F
SHAFT SPEED, Nl , RPM
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR OSCHG. TEHP.OtG F
EXHAUST GAS PRESS., PSIA
CORRECTED 9LEED FLOH, LB/SEC
COMPRESSOR MAP FLOH, LB/SEC
FA RATIO BASED ON NAP FLOM
CORRECTED FUEL FLOM , LB/HR
FA RATIO CALC. FR9M EMISSION
EQUIVALENCE RATIO
LOADING H/P»»N/V/ECT/540I
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
LB. C02 PER LB. OF FUEL
MEIGHT FLOM, LB./HR.
CARBON MONOXIDE
PPH BY VOLUME, MET
L3. PER 1008 LB. OF FUEL
HEIGHT FLOM, LB./HR.
UNBURNEO HYDROCARBONS- PPH AS
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIOE INOI - HEIGHTS AS
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
NITROIEN DIOXIDE IN02I
PPH BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
TOTAL OXIDES OF NITROGEN INOtN
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED MEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLCM
SMOKE NUMBER
CORRECTED MCIGHT FLCM
SMOKE NUMBER
CORRECTED MEIGHT FLOM
SMOKE NUMBER
SMOKE NUMBER AT MA«0.023
211
1.8
0.0
0.0
490.0
U1610.0
60.9
378.0
13.62
0.000
5.97
.0066
141.0
.0066
.097
.383
98.252

1.35
3.07
432.8

247.1
35.838
5.053
COMB P/N= 698168-3 TEST DATE 6-15-75 FUEL-Atf. KERO. P BARO* 28.62
RAT SPO* 41600. OEM PT,F« 51. REi. HUM 70.80 SPEC HUM» .007511
L H V* 18470. S LN T,F= 301.0 FLO.L/M* 14.160 SL TIM,S= 6.5111
212
39.6
"79,1
75.7
612.0
41430.0
59.9
384.0
13.68
0.000
5.67
.0086
175.0
.0088
.129
.370
98.875

1.80
3.09
541.4

277.4
30.340
5.310
CARBON, HEIGHTS AS
124.5
10.319
1.455
.2879
N02
14.9
3.5*9
.510

1.1
.2«2
.037
02) AS NO2
16.0
3.811
.537

.00695
24.10
.02084
36.10
.03472
44.60
. 04861
49.40
39.00
75.1
4.689
.821
.1545

21.8
3.773
.661

2.2
.395
.069

23.2
4.168
.729

.00695
19.90
.02084
34.90
.03472
43.40
.04860
58.60
37.70
213
99.3
198.6
190.0
862.0
41070.0
58.9
392.1
14.30
0.011
5.18
.0134
244.0
.0132
.193
.336
99.623

2.75
3.13
763.9

190.7
13.809
3.369
CH4
14.4
.596
.145
.0432

41.1
4.757
1.161

1.2
.143
.135

41.2
4.910
1.196

.00694
18.10
.02083
30.10
.03469
39.80
.04856
48.20
34.60
214
0.
0.
0.
1000.
40960.
53.
349.0
13.81
2.284
6.62
.0163
261.0
.0162
.237
.382
99.591
REDUCED
3.39

816.4

267.2
15.698
4.097

13.5
.453
.118
.0289

47.8
4.613
1.204

1.2
.116
.030

49.1
4.729
1.234

.01696
24.11
.02086
39.20
.03475
51.80
. 14032
57.01
41.00
215
22.8
45.6
43.6
998.0
41900.1
55.0
3S2.0
13.80
2.032
6.52
.0165
272.0 _....._.
.0162
.238
.367 " ' "
99.558

3.39
3.13
850.3

285.2
16.744 	
4.554

16.5 - - •-- 	 - - ------- -- -- 	
.554
.151
.0331 """ "" ~

47.1
4.533 " ~
1.233

.5
.048
.013 .._.
•
47.5
4.581
1.246 " 	

.00695
25.30 ~ 	 - .- . __ . _.
.02181
43.41
.03467 	 " 	
51.20
.04853
60.21 	 "- •-- 	 	 " 	 — - - ---••
45.61
                          2.EQUIVALENCE *ATIO CALCULATED FROM C02.CO,AND HC DATA AND FUEL COMPOSITION.                                 	
                          3.MASS EMISSIONS OF HO, HOZ, AW NO+N02 CALCULATED AS K02 FRON CONCENTRATIONS KITH MOLECULAR HEIGHT OF N02 <46.lll.
                          4.COHBUSTIOK EFFICIENCY CAJ.CIH.ATEO FROH CO.AND UNC «S VAPORIZED ORIGINAL FU£t ON L«T18 FUCt MIS.        «*'••»'«
-------

ENGINE' GTCP85-98CIC S/N«
DATA POINT NUMBER
EMISSION RATE LB/HR
CARBON MONOXIDE
UNBURNEO HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIDE
POWER LEVEL HP
TOTAL CORRECTED HORSEPOWER
36179
211

5.053
1.1.55
.537
.500
0.00
0.00
COMB P/N«
212

5.310
.821
.729
.660
75.68
79.12
698168-3
213

3.369
.1<>5
1.196
1.161
1)9.97
198.60
TEST DATE
211,

1..097
.118
1.231.
1.281.
230.71,

6-15-7!
215


.151
1.21.6
1.233
252.57
263.87
BRAKE SPECIFIC EMISSION INDEX L3/UOOMP-HR
CARBON MONOXIDE
UNBURNEO HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIOE
O.ODO
0.000
0.000
0.000
70.156
10.81,2
9.638
8.724
17.737
.765
6.29V
6.111
17.757
.513
5.31,9
5.218
18.033
.596
1..931,
«.862
                                                                                                               FUEL'AV. KERO.
                                                                                                                                 P SARD' 28.62
                           NOTE»«0. APPE»RING  IN  3R4KE SPECIFIC EMISSION INOcX COLUMN  DENOTES AN IDLE CONDITION
0)

M
OJ
                                                                                                                                                                      )
                                                                                                                                                                      )
                                                                                                                                                                      )
                                                                                                                                                                    : CM
-------
(D
OJ
CO
                       ENGINE MFR. I AIRESEARCH
                      MODEL NO.I   GTCP85-98CK

                      FUEL' ASTM 01655-73
«7»
36179
                                                              INSIRl OESCRIP.I  FEDERAL REG  V38 N136
                                                    ENGINE TYPE  ICLASS1 I  APU              CAi r   in,
                              MAX SHP       200. , BLEED AIR EXTRACTION TO    1150. OEG. F EM
                                  ATOMIC H/C RATIO.   1.928    LHV.     18470. BT^J.     ADDITIVES! NONE
CALC. OATEI
   2
                                                                                6-15-75
                                                                                                                                17 JULY 1973
                   OXIDES OF NITROGEN INOX AS N02.
                                                                            1§:SS  ts: --•« -    •  --
                                                                             4.SM  LB. POLLUTANT p" 1000 Hpi-HRl
COH3USTOR TYPEI TANGENTIAL CAN          P/NI  698168-3  SJRFACc/VOLUMEl  .725 SQ IN/CJ IN
ENGINE TOTAL SERVICE!     0.0  HR.   TIME SINCE ENGINE OVERHAu!,      fl., HR
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!

AIRCRAFT INSTALLATION ••• NFR.I
                                                                                                                   FUEL INJ. TYPEI
                                                                                                                                       DUAL ORIFICE
;
HUUEL NO. I
USERI
> GASEOUS EMISSION TEST NO., i5 DmrTM:™1111^:"1 ":^siii"*Rs.;r*MKrr*«"«ri:":^""' 	 • — "
> SS^ttzSv^zS^-^^^tttt
•>
TEST CONDITION
POKER SETTING, CORRECTED HP.
Ml SPEED, RPH
FUEL FLOW IHEAS.I LB./HR.
.' ENGINE CORE INLET AIRFLON ICAuC.I LB./SEC.
COMPRESSOR INLET TEMP., DEE. F
COMPRESSOR DISCHARGE AIR PRESSURE. PSIA
COMPRESSOR DISCHARGE AIR TEMP., OEG. F
COMPRESSOR BLEED AIRFLOK (NEAS.) LB./SEC.
BLEED AIR PRESSURE, PSIA
BLEED AIR TEMPERATURE, OEG. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION, KET ANALYSIS
1 HYDROCARBON IHC AS CH*I . PPMC
CARBON MONOXIDE (CO) , PPMV
TOTAL OXIDES OF NITROScN CNOXI , PPMV
CARBON DIOXIDE (C02> , PERCENT BY VOL.
NITRIC OXIDE (NO), PPHV
EMISSION INDEX, LB. POLLUTANT/1000 L3. FUEL
HYDROCARBONS (HC AS CH4I
CARBON MONOXIDE 
TOTAL OXIDES OF NITROGEN (NOX AS N02I
EMISSION RATE, IB. POLLUTANT/MR.
HYDROCARBONS (HC AS CH4I
CARBON MONOXIDE (CO)
) TOTAL OXIDES OF NITROGEN (NOX AS N02I
ENGINE NORK OUTPUT. MEAS. SHP
ENGINE WORK OUTPUT. ISENTROPIC AIR HP
) ENGINE MORK OUTPUT, TOTAL HP
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS!


216 217 218
0.00 79.04 198.86
41600.00 1,1430.00 41060.00
139.00 176.00 244.00
5.83 5.59 5.14
60.8 60.0 60.0
60.64 59.41 58.67
379.00 3*6.00 394.00
0.00 0.00 n.an
0.00
-0.00
<<93.0
120.000
24*. 671
15.400
1.347
13.300
9.951
35.498
3.670
1.383
4.934
.51*
0.00
0.00
0.00
98.29
.(•7
9.00
-0.00
615.0
75.000
276.375
23.000
1.796
la.aoo
4.700
30.303
4.142
.827
5.333
.729
75.68
t.OO
75.68
9S.«7
.(•9
0.00
-0.00
866.0
15.000
187.476
41.000
2.752
39.000
.621
13.575
4.877
.151
3.312
1.190
190.40
0.00
190.40
99.63
.•13
219
0.00
40930.00
261.00
6.56
60.0
52.78
348.00
51.31
370.00
1007.0
10.500
239.757
50.500
3.463
49.000
.345
13.798
4.774
.•91
3.601
1.246
0.00
229.83
229. 83
99.65
.•17
220
45.54
40880.00
271.00 ~
6.53
- 59.0 .... 	 	 	
54.80
351.0*
53.52 	 I"- 	 	
371.00
997.0
16.500
290.393
47.000
3.432
45.500__ 	

16.835
4.476

4.562
1.213
2(6. 81
250.37
.•16
-------
ifl
0)
co
                 »••»»»••••»»•»»•••••••••»•••»»•»»••»••»•••«••   AIRESEARCH EMISSION  TEST  SimH»Rt
                    EN6INE*  6TW»5-9»«      S/««  J*m     COHB P/H«  b«ib»-J TEST 0»T£  b-15-75
                   MT SHP»    210.    RA E6T.F" 1150.      RAT SPO« *1600.    OEM PT,F«  51.
                  FUEL H/C«  1.9ZBI    STOI F/»« ,»b»ZZ       L H V« 18*70.    S UN T,F» 310.0
                                                                                 ••»••»•••»••••»»•»••»••••••••»••»••••••»•••••
                                                                                      FUEL»»W. KERO.    P i»*0» tt.M
                                                                                 REu HUH-  70.00    SPEC HUM» .II7SQI
                                                                                 FLOtL/H»  I*. 161   SL TIH,S»  6.5MI
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., OtG.F
SHAFT SPEED. Nl, RPM
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR OSCHG. TEMP, DEC F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOH, LB/SEC
COMPRESSOR HAP FLOH, LB/SEC
FA RATIO BASED ON MAP FLOM
CORRECTED FUEL FLOH , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING M/P**N/V/E(T/5*0)
COM3 EFFIC FROH EHISSIOKS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
LB. C02 PER LB. OF FUEL
HEIGHT FLOM, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NO) - HEIGHTS AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE (N02I
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
216
0.0
0.0
0.0
1.93.0
*1600.0
60.6
379.0
13.63
0.000
5.97
.0065
139.0
.0066
.097
.305
98.292

1.35
3.07
*Z6.9

2**. 7
35.498
*.93»
Z17
39.5
79.0
75.7
615.0
*I*JO.D
59.*
386.0
13.68
0.000
5.58
.0088
176.0
.0087
.128
.368
98.875

1.80
3.09
5**. 5

276.*
30.303
5.333
CARSON, HEIGHTS AS
120.0
9.951
1.383
.2803
N02
13.3
3.170
.**!

2.1
.500
.070
75.0
*.700
.827
.1551

18.8
3.386
.596

*.2
.756
.133
211
99.*
190.9
190.*
868.0
1.1060.0
58.7
39*. 0
13.81
0.000
5.08
.013*
2**.0
.0132
.193
.337
99.626

2.75
3.13
76i.. a

187.5
13.575
3.312
CH»
15.0
.621
.151
.0*57

39.0
*.639
1.132

2.0
.238
.058
219
0.0
0.
0.
1007.
40930.
52.
3*8.
13.79
2.275
6.62
.0163
261.0
.0165
.2*2
.386
99.6*5
REDUGEO
3.*6
3.13
817.3

239.0
13.798
3.601

10.5
.3*5
.090
.0250

*9.0
*.632
1.209

1.5
.1*2
.037
ZZI
zz.o
*5.5
*3.6
997.0
*OAlfi.O
5*. 6
351.0
13.00
2. 032
6.5Z
.0165
271.0
.016*
.2*1
.371
99.556

3.*3
3.13 ....... . .
6*7.2

290.* 	 ........
16.835
*.562
	 .. _ — . 	 	 _ ^ — 	 —
16.5
.5*7
.1*0 . ._ __ 	 	 _ — 	 	 - - . - 	
.0325

*5.5 	 _ 	 — 	 - ...
*.333
1.17*

1.5
.1*3
.039 .... . . 	 .. .. . . 	 _......
TOTAL OXIDES OF NITROGEN (NC«N02I AS N02
PPM BY VOLUME, NET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
SMCKE MEASUREMENT DATA
CORRECTED HEIGHT FLOM
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
SMOKE NUMBER AT HA=O.OZ3
15.*
3.670
.510

.00695
17.50
.0208*
3*. 90
.03*72
*2.ZO
.0*858
1.8.20
36. ZO
23.1
*.1*2
.729

.00693
19.30
.02080
33.70
.03*65
*3.*0
.0*851
50.60
37.30
1.1.0
*.077
1.190

.0069*
16.30
.02078
30.10
.03*63
36.10
.0*8*6
**.60
32.30
50.5
*.77*
1.2*6

.0069*
22.30
.02082
1.2.20
.03*69
5Z.*0
.0*853
59.60
**.oo
*7.0
*.*76 - -

1.213

.00693 .... -. . .
26.59
.02079
*2.8fl . .
.03*63
53.01
.0*6** . 	
60. ZO
1.6.30
                                                                                                                                            >
                                                                                                                                            )
                                                                                                                                            )
                                                                                                                                            >

                                                                                                                                            )
                                                                                                                                            )

                                                                                                                                            )
                                                                                                                                            >;.
                                                                                                                                            )
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE HET VALUES.                                                           -
      2.EQUIVALENCE RATIO CALCULATED FROM C02,CO,ANO HC DATA AND FUEL COMPOSITION.
      3.MASS EMISSIONS OF NO, N02,  AND NO»NOZ CALCULATED AS NO2 FROH CONCENTRATIONS HITH MOLECULAR  HEIGHT OF N02
      •..COMBUSTION EFFICIENCY CALCULATED FROM CO,AND UHC AS VAPORIZED ORIGINAL FUEL ON LB/ LB  FUEL  BASIS.
                                                                                                                                    1*6.111.
-------
  ENGINE* GTCPB5-98CK      S/K
DATA POINT NUMBER
EMISSION RATE LB/HR
    CARBON MONOXIDE
    UNBURNEC HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIDE
POWER LEVEL HP
TOTAL CORRECTED HORSEPOWER
BRAKE SPECIFIC EMISSION INDEX
    CARBON MONOXIDE
    UNIURNEO HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIOE
36179
   216
                                                           ••••  AIR£S£ARCH EMISSION TEST SUMMARY
                                                            C013 P/N* 698168-3 TtST DATE  b-15-75
                                                               Z17
                                                                         218
«..93i. 5.33J
1.383 .827
.510 .729
.<><»1 .596
0.01 75.68
1.01 79.0k
B/1000MP-HR
0.000 70. -.78
0.010 10.931
0.008 9.633
0.000 7.870
3. 312
..151
1.191
1.132
190.1.0
198.86

17.397
.796
6.250
5.91.5
                                 219

                               3.601
                                .090

                               l!zi9
                             229.83
                                                                                15.669
                                                                                  .392
                                                                                 5.260
  220

4.562
                                                                                           1.213
                                                                                         250.37
                                                                                         261.74
                                        18.223
                                          .592
                                                                                           
-------
                    ENGINE HFR.I AIRESEARCH
                   NODE). NO. I  GTCP1S-9«CK

                   FUEL! ASTM 01655-73
                               TEST FACILITY I PHX LACCZ       INSJR.  OESCRIP.I   FEDERAL REG V38 HI36    C»LC. DATE I   6-15-7J
                               S/NI   36179         ENGINC  TYPE  (CLASS!I  APU              CALC. I.O.I     3
                              MAX SHP       200.  »  sLEto AIR  EXTRACTION TO    mo. DEC. r EGT
                                  ATOMIC  H/C  RATIOI    1.921    LHVt      181.70.  3TU/LB.      AOOITIVESI NONE
                              EXHAUST  EMISSIONS  PER  EPA  RATED WORK OUTPUT •• CODE OF FEDERAL REGULATIONS TITLE 1,0 PART  87
                             ..,,...»....,..,,.,,.,..,,.... ^MISSIONS COMPUTED FROM TEST CONDITION NO.  5   ••••••»•»••»••
                                       HYDROCARBONS  (HC AS CHto>              .597  LB. POLLUTANT PER 1000 HP.-HR.
                                       CARBON  MONOXIDE (CO)                18.388  LB. POLLUTANT PER 1000 HP.-HR.
                                       OXIDES  OF  NITROGEN (NOX AS NOZ)     to.889  LB. POLLUTANT PER 1000 HP.-HR.

....,...»..,.,..»....,.,...».„...„.,,.„.„.„.......   £N6IME DESCRIPTION  »»•••••»»»»*•»«»
COMBUSTOR TYPEI TANGENTIAL CAN           P/N!    698168-3  SURFACE/VOLUME I  .725 SQ IN/CU IN
ENGINE TOTAL SERVICEI     0.0  HR.    TIME  SINCE ENGINE OVERHAUL!      0.0 HR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                   AIRCRAFT INSTALLATION »•* MFR. 1
                                                                                MODEL NO. 1
                                                                                                                 FUEL  INJ. TYPEI
                                                                                                                       USERI
                                                                                                                                      DUAL  ORIFICE
tu
iQ
(D
                   ».».».»,».»..«...,.„».,..,»..»»»,.,.»».,»»,»,.»»OPERAIIONAL TEST QATA 5UMMARr ...............................................
                   GASEOUS EMISSION TEST NO. I    15    OATEI    6-15-75      TIMEI     1511.7      8SRO. PRESS.!  28.620 IN. HGA.
                   AM8IENT AIR TEMP.I 59.0   OEG. F         RELATIVE  HUMIOITYI   70.00 PERCENT       SPECIFIC HUMIDITYI   .007500 LB. HZO/LB.  DRT  AIR
                   AMBIENT AIR QUALITY    HYDROCARBONS (HOI  0.0    PPMC    CARBON MONOXIDE (CO) I 0.0   PPMV    OXIDES  OF NITROGEN  (NOX)I  0.0    PPMV
                   SAMPLE LINE »•» TEMP.!  300.00 OEG. F.     FLOHRATEI   Ito.16 -ITERS/MIN.     TRANSPORT TIMEI    6.50 SEC.     LENGTH!    50.00 FT.
TEST CONDITION
POWER SETTING, CORRECTED HP.
Nl SPEED, RPH
FUEL FLOW (MEAS.) LB./HR.
ENGINE CORE INLET AIRFLOW (CALC. ) LB./SEC.
COMPRESSOR INLET TEMP., DEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
COMPRESSOR DISCHARGE AIR TEMP., DEG. F
COMPRESSOR BLEED AIRFLOW (MEAS.) LB./SEC.
BLEED AIR PRESSURE, PSIA
> BLEED AIR TEMPERATURE, DEG. F
ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION, NET ANALYSIS
) HYDROCARBON (HC AS CHI.) , PPMC
CARBON MONOXIDE ICOI , PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPMV
; CARBON DIOXIDE ICOZ) , PERCENT BY VOL.
NITRIC OXIDE CNO). PPMV
EMISSION INDEX, L6. POLLUTANT/1000 L3. FUEL
I HYDROCARBONS CHC AS CM*)
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS -5.658
16.000
1.31.7
13.200

9.6Z7
35.61.2
3.813

1.366
-------
ft
0>
M
to
ENGINE* GTCP85-98CK S/N= 36179
RAT SMP* 211. RA ECT.Fc 1150.
FUEL H/C« 1.9281 STOI F/A* .868Z2
DATA POINT NUMBER 221
PERCENT MAX. CORRECTED POMER 8.0
CORRECTED SHAFT HP O.I
MEASURED SHAFT HP 0.8
EXHAUST GAS TEMP., OEG.F 1.92.0
SHAFT SPEED. HI, RPH 41600.0
COMPRESSOR 3SCMG. PRES..PSIA 60.5
COMPRESSOR OSCHG. TEMP.DEG F 380.0
EXHAUST GAS PRtSS.. PSIA 13.63
CORRECTED BLEED FLOM, LB/SEC 0.090
COMPRESSOR MAP FLOM.LB/SEC 5.97
FA RATIO BASED ON MAP FLOH .0065
CORRECTED FUEL FLOM , LB/MR 139.0
FA RATIO CALC. FROM EMISSION .0066
EQUIVALENCE RATIO .097
LOADING H/P»»N/V/E(T/54fl) .385
COMB EFFIC FROM EMISSIONS 98.300
CARBON DIOXIDE
PERCENT BY VOLUME, MET 1.35
LB. CC2 PER LB. OF FUEL 3.07
MEIGHT FLOM, LB./HR. 426. 9
CARBON MONOXIDE
PPM BY VOLUME. MET 245.7
LB. PER 1000 LB. OF FUEL 35.642
RATHSPD*'Nl!i-nn81"~^SI,0*IE _6"15-75 ... FUEL*AV. KERO. P BARO= 28.62
L H 1* 1
222
39.8
79.7
76.1
615.0
41420.0
54.6
38k. 0
13.69
0.000
5.58
.0089
178.1
.0086
.126
.367
8-.7S.
223
99. 8
199. 7
190.8
S68.1
-1050.0
58. 7
393.0
13.82
0.000
5.03
.0135
.0132
.193
.X34
S LN T,F
224

0*
•
0.
1000.
c?
?£.
347.
13.80
2.273
6. 62
.0163
261.1
.0163
.239
. »»7
98.875 99.639 99.596

1.77
3.09
550.6

276.1,
30.756
MEIGHT FtOM, LB./HR. t..95i. 5.475
UNBURNED HYDROCARBONS- PPM AS CAR90N, HEIGHTS AS CM
PPM BY VOLUME. MET 118.5
LB. PER 1000 LB. OF FUEL 9.827
HEIGHT FLOM, LB./HR. 1.366
RATIO L3 HC/LB CO .2757
NITRIC CXIOE (NO) - HEIGHTS AS NOZ
PPM BY VOLUME, MET 13. Z
LB. PER 1000 LB. OF FUEL 3.146
HEIGHT FLOM, LB./HR. .437
NITROGEN DIOXIDE (N02I
PPM BY VOLUME, M£T 2.8
LB. PER 1000 LB. OF FUEL .667
HEIGHT FLOH, LB./HR. .093
TOTAt. OXIDES OF NITROGEN (NO*N02I AS NOZ
PPM BY VOLUME, MET 16.0
LB. PER 1000 LB. OF FUEL 3.813
HEIGHT FLOH, LB./MR. .530
SMOKE MEASUREMENT DATA
CORRECTED MEIGHT FLCM .11693
SMOKE NUMBER 18.10
CORRECTED HEIGHT FLCH .02076
SMOKE NUMBER 34.91
CORRECTED MEIGHT FLOH .03460
SMOKE NUMBER 42. Zl
CORRECTED KEIthT FLOM .0*842
SMOKE NUMBER 51.81
SMOKE NUMBER AT MA»1.823 37.41
NOTES 1. «LL EMISSIONS CONCENTRATIONS ARE
Z. EQUIVALENCE RATIO CALCU.ATEO FROM
• . Mf CC CM TCCTrtUC i%£ Ufl »t*9 AUf* ••*.
72.1
4.580
.815
.1489

18.5
3.382
.602
4.5
.823
.146
23.0
4.204
y t •
• r *> 0
.0069Z
20.50
.02076
36.10
.03459
43.40
.04441
49.40
37.91
MET VALUES
COZ,CO,ANJ
2.75
3.13
764.1

187.5
13.577
i.313
11.4
.472
.115
.0348

39.0
4.639
1.132
2.5
.297
.073
41 • 5
4.937

1*205
.00692
15.70
.02075
28.30
.03457
31.10
.04839

32.51

HC DATA
3 41
3.13
816.5

269.7
15.733
4.106
11*7
.390
.102


47.3
4*532
1.183
1.2
• 115
.131
48
4 647

1*213
.01692
21.51
.02174
41.10
.13455
53.10
.04135
59*61
44.31

AND FUEL
= 300.0 FLO,L/M= 14.160 SL TIH.S* *6.5000
2Z5 —

23.
it* "
998 !
41870.
f.
*>***
352.
13.80
2.036
6.49
.0165
?7B 0
C ' V . N
.0161
• 236
.368 "
99.548

3.37
3.13
843*9

291.4
17.141
4.62!
16.5 	 " ' ...... ...

• 150
.0325 " - - . - - ..._._. 	 	 	

44.5

1.165
2.5 •• ' - 	 	 ._..... _ . . .
• Z4Z
.065
1.7 •
*.« • •
4*557

1.231 '•• 	 	
.11691
24.11
.02174
43.41
.13462
55.41 '
.14144' • '

46 II
* . :
COMPOSITION. . i
                             twmmm
                            . COMBUSTION EFFICIENCY
    *S "°2 F*OH CONCENTRATIONS «fH  «OL£tUl«  HEZ6M OF  MU  (46.I1J.
UHC AS VAPORIZED ORIGINAL FUEL ON It/ LB FUEL  BASIS.
-------
                                                                        AIRESEARCH EMISSION TEST SUMMARY  ••»••»•»•
                        EMISSION RATE  LB/HR
                            CARBON  HONOXIDE
                            UNBURNED HYDROCARBONS
                            2?«tr  ^TNITROGEN
                            NITRIC  OXIDE
                        POWER LEVEL HP
                        TOTAL CORRECTED HORScPOHER
J..95".
1.366
 -530
 .1,37
fl.,0
0.00
                                                           .
                        BRAKE SPECIFIC EHISSION  INDEX  L3/1000HP-H*
                            CARBON HOHOXIDE               0.000
                            UNBURNEO  HYDROCARBONS         0.000
                            OXIDES OF NITROGEN            0.000
                            NITRIC OXIOE                  0.000
5.

                                                                                                                                                                     00
-------
1    ENGINE MFR.I AIRESEARCH
    MODEL NO.I  GTCP85-98CK

"*   FUEL I ASTM 01655-73
                                                      TEST FACILITY! PHX LACC2        INSTR.  OESCRIP.I   FEDcRAL REt V38 N136
                                                      S/NI  36179          ENGINE  TYPE  (CLASS)I   APU               CALC. I.O.I
                                                     HAX SHP       ZOO. » BLEED AIR EXTRACTION TO   1150.  OE6. F EGT
                                                         ATOMIC H/C RATIOI   1.928   LMVI     ie-,70.  BTU/LB.      AOOITIVESI NONE
           CALC. DATE I
              1
                         6-19-75
                                 EXHAUST EMISSIONS  PER EPA RATED WORK OUTPUT •• COOE OF FEDERAL  REGULATIONS TITLE ,0 PART 87
                                .»........,......»....,,.„.». EHISSIONS CONFUTED FROM TEST CONDITION  NO.   5   ..»»»..»»»»..«
                                         HYDROCARBONS  (HC AS CH-I             2.011  LB. POLLUTANT PER  1000  HP.-HR.
                                         CARBON  MONOXIDE £!
(D
, SfflS^rafer^S^^S-'^^^asr^Sf.
TEST CONDITION
POWER SETTING, CORRECTED HP.
Nl SPEED, RPM
FUEL FLOW (HEAS.) LB./HR.
1 ENGINE CORE INLET AIRFLOW (CALC. » LB./SEC.
COMPRESSOR INLET TEMP., OEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
< COMPRESSOR DISCHARGE AIR TEMP., OEG. F
; COMPRESSOR BLEED AIRFLOW (MEAS.I LB./SEC.
i BLEED AIR PRESSURE, PSIA
> BLEED AIR TEMPERATURE, OEG. F
; ENGINE EXHAUST GAS TEMP., OEG. F
EMISSION CONCENTRATION, WET ANALYSIS
) HYDROCARBON (HC AS CH*) , PPHC
CARBON MONOXIDE (COI , PPMV
TOTAL OXIDES OF NITROGEN (NOXI , PPHV
CARBON DIOXIDE (C02) , PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH*)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02I
' EMISSION RATE, L». POLLUTANT/HR.
ttYOKOCAKBOMS (HC ffS CH*)
CARBON MONOXIDE (CO)
• TOTAL OXIDES OF NITROGEN (NOX AS N02)
ENGINE WORK OUTPUT. MtAS. SHP
ENGINE WORK OUTPUT. ISENTROPIC AIR HP
ENGINE WORK OUTPUT, TOTAL HP
COMBUSTION fcFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS!
Z26 227 228
0.00 79.75 198.99
100.00
o.l9
61.0
383.00
0.00
0.00
-0.00
1.90.0
231.000
13.500
1.327
10.500
19.132
51.6*6
3.21S

1.913
5.165
.321
0.00
0.00
O.DO
97.11
»»«7
1.1730.00
123.00
3.93
59.0
»1.78
391.00
0.00
0.00
-0.00
613.0
139.500
ol3.792
20.500
1.765
16.300
8.795
1.5.61.1
3.71*

1.882
5.61*
.1.57
52.1,8
0.00
52.1.8
96.15
.0(9
*1*80.00
170.00
3.69
59.0
Hi. 19
1.01.08
0.00
a. oo
-0.00
857.0
21.900
2*8.625
36.500
2.661
33.000
.935
18.570
V.H78

.159
3.157
.761
130.95
1.06
130.95
99. *0
.•11
229
0.00
Hll.00.00
190.00
*.83
59.0
37.22
356.00
1. 57
36.33
383.00
1005.0
. 15.000
290.393
1,5.000
3.309
1.2.000
.503
17.0*9
*
-•a&
»9W,
3.239
.825
0.61
173.6*
173.0*
99.55
.•16
230
1.6.1*
*1*20.00
190.00
*.7S
59.0 	
39.13
362.00
19*
• CO
38.35 	
386.06
9*7.0
51.000
*99.960
30.000
3.1*8
35.000

1.627
31,336
3.912 	 	 - -


5*95* ""
.7*3
30.36
1*2.22
172.59
99.1*
.615
                                                                                                                                                                   CD
-------
ft)
(D
M
Ul
1 ENGINE' GTCP05-98CK S/N* 36179 COM3 P/N= 698168-3 TEST DATE 6-19-75 FUEL-AV. KERO. P BARO* 19.69
RAT SHP* 200. RA EGT.F* 1150. RAT SPO* *1600.
FUEL H/C= 1.9260 STOI F/A= .06822 L H »= 18*70.
DATA POINT NUMBER 226 ZZ7 228
' PERCENT MAX. CORRECTED POMES 0.0 39.9 99.5
CORRECTED SHAFT HP 0.0 79.7 199.0
MEASURED SHAFT HP 0.0 52.5 131.0
EXHAUST GAS TEMP., OEG.F 1.90.0 613.0 857.0
SHAFT SPEED, Nl, RPM 1,18*0.0 t.1730.0 1.1*80.0
COMPRESSOR OSCHG. FRES. ,PSIA *Z.8 *1.8 *1. Z
) COMPRESSOR OSCHG. TEMP, DEC F 313.0 391.0 ".01.0
: EXHAUST GAS PRESS., PSIA 9.37 9.1,3 9.1.9
CORRECTED BLEED FLOM, LB/SEC 0.000 0.008 0.000
1 COMPRESSOR MAP FLOM, LB/SEC *.00 3.73 3.*1
FA RATIO BASED ON MAP FLOM .0070 .0092 .0139
; CORRECTtO FUEL FiOU , LB/HR 100.0 123.0 170.0
FA RATIO CALC. FROM EMISSION .0066 .0067 .0128
• EQUIVALENCE RATIO .097 .127 .187
LOADING H/P»N/V/EIT/5*OI .1.70 .*51 .*!*
OEM PT.F* 51. REL HUH' 70.10 SPEC HUH* .007500
S <.N T.F- 300.0 FLO.L/M* 1*.160 SL TIN,S» 6. 5001
229
o.g
0.0
0.0
1005.0
1,11.00.0
37.2
356.0
9.*9
2.391
*.**
.016*
190.0
.0162
.238
.*52
• ) COM3 EFFIC FROM EMISSIONS 97. U7 98.155 99.1.81 99.555
CARBON DIOXIDE
) PERCENT BY VOLUME, MET 1.33 1.76 2.66
LB. COZ PER LB. OF FUEL 3.02 3.06 3.12
HEIGHT FLOM, LB./HR. 302.0 376. Z 530.8
) CARBON MONOXIDE
PPM BY VOLUME, MET 356.* *13.8 21.8.6
LB. PER 1000 LB. OF FUEL 51.6*6 1,5.6*1 18.570
> HEIGHT FLOM, LB./HR. 5.165 5.61* 3.157
UNBURNEO HYDROCARBONS- PPM AS CARBON, HEIGHTS AS CH*
PPM BY VOLUME, MET 231.0 139.5 21.9
) LB. PER 1000 LB. OF FUEL 19.132 8.795 .935
MEIGHT FLOH, LB./HR. 1.913 1.082 .159
RATIO LB HC/LB CO .370-, .1927 .0503
) NITRIC OXIDE INO) - HEIGHTS AS NOZ
PPM BY VOLUME. MET 10.5 16.3 33.0
LB. PER 1000 LB. OF FUEL Z.*99 Z.953 *.0*9
) MEIGHT FLOM, LB./HR. .250 .363 .688
NITROGEN DIOXIDE (NOZI
PPM BY VOLUME, MET 3.0 *.Z 3.5
) L3. PER 1000 LB. OF FUEL .71* .761 .*29
MEIGHT FLON, LB./HR. .071 .091, .073
TOTAL OXIDES OF NITROGEN (NC+NOZI AS NOZ
) PPM BY VOLUME, MET 13.5 20.5 36.5
LB. PER 1000 tB. OF FUEL 3.213 3.71* *.*78
MEIGHT FLOM, LB./HR. .321 .*57 .761
SMOKE MEASUREMENT DATA
CORRECTED MEIGHT FLOM .00705 .00707 .00706
SNOKE NUMBER 8.1,0 9.00 *.ZO
< CORRECTED MEIGHT FLOM .02113 .02121 .02119
SMOKE NUMBER 20.50 22.90 1Z.OO
CORRECTED MEIGHT FLOM .03521 .03526 .03532
) SMOKE NUMBER 27.70 26.90 19.90
CORRECTED HEIGHT FLOM . 3*9Z7 .0*936 .0*9**
SMOKE NUMBER 32.50 36.10 25.90
) SMOKE NUMBER AT MA=O.OZ3 22.50 2*.SO 15.70
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE MET VtLUES.
Z. EQUIVALENCE RATIO CALCU.ATED FROM COZ. CO, AND HC DATA
) 3. MASS EMISSIONS OF NO, NOZ, AND NO»N02 CALCULATED AS
*. COMBUSTION EFFICIENCY CALCULATED FROM C3.ANO UHC AS
3.39
3.13
593.9

290.*
17.0*9
3.239
,
15.0
.503
.096
.0295

1.2.0
*.OS*
.770

3.0
.289
.055

i.S.0
*.3*l
.825

.00706
10.20
.02119
27.70
.03532
3*. 90
.0*)**
1.1.60
28.90

AND FUEL
N3Z FROM
VAPORIZED
230
23.1
*6.1
30.*
9*7.0
*1*20.0
39.1
362.0
9.50
1.938
*.32
.•173
190.0
.0152
.223
,*36 . 	 - -
99.103

3.15
3.10
589.0

500.0
31.336
5.95*

51.0
1.827
.3*7
.0583

35.0
3.603
.685

3.i " '"' " 	 " "
.309
.059

36.1
3.912
.7**

.00716
19.30
.02119
32.50 .
.03532
*6.*0
.0*9**
51.80
37.80

COMPOSITION.
CONCENTRATIONS MITH MOLECULAR HEIGHT OF NOZ 1*6.011.
ORIGINAL FUEL ON LB/ LB FUEL BASIS.
                                                                                                                                                                                                         3
                                                                                                                                                                                                        h
                                                                                                                                                                                                         CO
-------

ENGINE* GTCP85-98CK S/N*
DATA POINT NUMBER
EMISSION RATE LBSHR
CARBON MONOXIDE
UNBURNEO HYDROCARBONS
OXIOES OF NITROGEN
NlTRIC OXIOE
POKER LEVEL HP
TOTAL CORRECTED HORSEPOWER

36179
226

5.165
1.913
.321
.250
0.00
0.00
COMB ?/n*
227

5.614
1.082
.457
.363
52.48
79.75
BRAKE SPECIFIC EMISSION INDEX LB/100IHP-HR
CARBON MONOXIDE
UNBURNEO HYDROCARBONS
OXIOES OF NITROGEN
MIT8IC OXIDE
0.000 106.969
0.090
0.0(0
0.0(0
20.612
8.705
6.922
698168-3
228

3.157
.159
.761
.668
130.95
190.99

24.108
1.214
5.814

T£ST DATE
229

3.239
.096
.825
.770
173.84
264.16

18.634
.550
4.743
4.427
6-19-75
230

5.954
.347
.743
.685
172.59
262.25

34. 496
2.011
4.307
3.967
                                                                                                                 FUEl«AV.  KtRO.
                                                                                                                                    P BARD' 19.69
                                      APPEARING  IN  BRAKE  SPECIFIC EMISSION INDEX COLUMN  DENOTES AN IDLE CONDITION
n>
-------
                                                                                                                                              e
  ENGINE NFR.I URESEARCH
 MODEL NO. I  GTCP85-9BCK

 FUELI ASTN 01655-73
 TEST FACILITY! PHX LACCZ       INSTR. OESCRIP.l  FEDERAL REC  V38  N136    CALC.  OATEI
 S/NI  36179          ENGINE TYPE  (CLASS)I  APU              CALC.  I.D.I      2
MAX SHP       ZOO. » BLEED AIR EXTRACTION 10    1158. DtG. F EGT
    ATONIC H/C RATIO!   1.928    LHVI      18470.  BTU/L8.     ADDITIVES! NONE
                                                                                                                      6-19-75
                                                                                                                                              >
            tXHAUST  EMISSIONS PER  EPA RATED WORK OUTPUT *» CODE OF FEDERAL REGULATIONS TITLE 40 PART 87
            »..*,..,.«...,....,......«....  £MiSSioNS COMPUTED FROM TEST CONDITION NO.  5   »»»»»««»••»»•«
                     HYDROCARBONS  (HC  AS  CH4)             1.990  LB. POLLUTANT PER 1000 HP.-HR.
                     CARBON  MONOXIDE  (CO)                33.598  LB. POLLUTANT PER 1000 HP.-HR.
                     OXIDES  OF NITROGEN (NOX AS NOZ)     4.430  LB. POLLUTANT PER 1800 HP.-HR.

[[[   ENGJNE  DESCRIPTION  »•«»»••••»••*•••
COMBUSTOR TYPEI TANGENTIAL CAN          P/NI  698168-3  SURFACE/VOLUNEI   .7Z5  SO IN/CJ  IN
ENGINE TOTAL SERVICE!     0.0  HR.   TIME SINCE  ENGINE OVERHAUL       0.0  HR.
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
 AIRCRAFT INSTALLATION ••• MFR. 1
                                                              MODEL NO. I
                                                                                               FUcL INJ. TYPE!
                                                                                                     USER!
                                                                                                                   DUAL ORIFICE
 ,..,.»....,...,,.»»»,..»,.,»,.,.»,,..,.,..,...••OPERATIONAL  TEST DATA SUMMARY  ••••»••••••••••••••••»•»••••••••«••••••••••••»••
 GASEOUS EMISSION TEST NO.1    16    OATEI   6-19-75       TIME!    18.55       BARO.  PRESS.!  19.690 IN. HGA.
 AMBIENT AIR TEMP.I 59.0  OEG. F         RELATIVE  HUMIDITY!   70.00 PERCENT       SPECIFIC  HUMIDITY!  .007500  LB. HZO/LB. DRY AIR
 AMBIENT AIR QUALITY    HYDROCARBONS (HOI  0.0    PPMC     CARBON  MONOXIDE (CO)!  0.0    PPMV    OXIDES OF NITROGEN (NOX)I 0.0   PPMV
 SAMPLE LINE •»• TEMP.I  300.00 DEG. F.      FLOWRATE«    14.16 LITERS/MIN.    TRANSPORT  TIME!    6.50 SEC.      LENGTH!   50.08 FT.
                                                       COMPUTES  EMISSIONS
 TEST CONDITION                                         231        23Z
 POWER SETTING, CORRECTED HP.                          0.00      79.73
 Nl SPEED, RPM                                     41890.00   41760.00
 FUEL FLOW (MEAS.) LB./HR.                           102.00    1Z4.00
 ENGINE CORE INLET AIRFLOW(CALC.I  LB./SEC.             4.28       3.91
 COMPRESSOR INLET TEMP., OEG. F                        59.0       60.0
 COMPRESSOR DISCHARGE AIR PRESSURE. PSIA              42,47      41.49
 COMPRESSOR DISCHARGE AIR TEMP., DEG. F              387.00    394.00
 COMPRESSOR BLEED AIRFLOW (HEAS.)  L8./SEC.             0.00       0.00
 BLEED AIR PRESSURE, PSIA                              0.00       0.00
 BLEED AIR TEMPERATURE, OEG. F                        -0.00      -0.00
 ENGINE EXHAUST GAS TEMP., OEG. F                      493.0      622.0
 EMISSION CONCENTRATION, WET ANALYSIS
      HYOROSARBON (HC AS CH4), PPMC                232.500    134.400
      CARBON MONOXIDE (CO), PPMV      "             352.389    413.792
      TOTAL OXIDES OF NITROGEN (NOX), PPMV          14.000    20.508
      CARBON DIOXIDE (C02), PERCENT BY VOL.          1.323     1.787
      NITRIC OXIDE (NO), PPNV                        9.800    16.000
 EMISSION INDEX, LB. POLLUTANT/1000 L3.  FUEL
      HYDROCARBONS (HC AS CH4)                      19.317     8.374
      CARBON MONOXIDE (CO)                          51.222    45.104
      TOTAL OXIDES OF NITROGEN (NOX AS NOZ)          3.343     3.671
 EMISSION RATE,  LB.  POLLUTANT/HR.
      HYDROCARBONS INC AS CH4)                       1.978     1.038
      CARBON  MONOXIDE (COI                           5.225     5.593
      TOTAL  OXIDES OF NITROGEN (NOX AS NOZ)           .341       .455
 ENGINE  WORK  OUTPUT, MEAS. SHP                         0.00     52.52
 ENGINE  WORK  OUTPUT, ISENT40PIC AIR HP                 0.00      0.00
 ENGINE  WORK  OUTPUT,  TOTAL HP                          0.00     52.52
 COMBUSTION EFFICIENCY,  PERCENT (EMISSIONS)           97.10     98.20
F/A (EMISSIONS!                                        .007      .009
233
198.89
41500.00
175.00
3.72
60.0
41.15
403.00
0.00
0.00
-0.80
864.0
21.000
244.671
35.500
2.719
32.500
.877
17.886
4.263
.154
3.130
.746
131.02
8.08
131.02
99.50
.013
234
8.00
41400.00
198.80
4.77
59.8
37.22
356.00
1.57
36.33
383.08
1804.8
15.008
298.384
46.808
3.444
44.888
.495
17.229
4.364
.894
3.273
.829
0.00
173.53
173.53
99.55
.016
235
46.18
41428.00
190.08
4.72
58.8
39. IS
361.88
1.28
38.38
385.08
949,8
51.008
492.035 . . 	 .
39.588
3.177
36.508 	 	 	
1.811
30.565
-------
n>
*».
00

RAT SHP. ?«n ». rrr f 7, co C°H3 P/N= "•«•-» TeST DATE 6-19-75 FUELSAII. KFBO. D a.an, .= *„
N*I SHP« 200. RA EGT.FS nso. RAT SPO= *i60o. OEH PT,F
= 51. REL HUMS 7a.fin corr UIIM* *»-rt**
FUEL N/C« 1.9280 STOI F/A= .06822 L H V« 18*70. S .N T,F» 300.0 FLO,L/H- 1*^160 SL~Tlil7s« '".'silt
DATA POINT NUHBER 231 232 233 23*
PERCENT MAX. CORRECTED POHER 0.0 39.9 99 4. „ n
CORRECTED SHAFT HP o.O 7*.T 197*o J'J
MEASURED SHAFT HP 8.B 52 5 131 i J'J
EXHAUST GAS TEMP., DEG.F *93.0 622.0 86*!l 100* 0
SHAFT SPEED, Ml. RPM *1890.0 *1760.0 *1500.0 *l*flj fl
COMPRESSOR DSCHG. PRES..PSIA *2.5 *1.5 *lli 37 I
COMPRESSOR OSCHG. TEMP.OE6 F 387.0 39".. 0 *os!o 356 0
EXHAUST US PHESS., PSIA - 9.37 9.*2 9.51 III
CORRECTED BLEED FLOH. LB/SEC 0.000 0.000 0.000 2 3«7
COMPRESSOR HAP FLOH.LB/SEC 3.93 3.67 3.3* I 39
FA RATIO BASED ON MAP FLOH .0072 .009* .01*6 0187
CORRECTED FUEL FLOH , LB/HR 102.8 124.0 175.0 lit 0
FA RATIO CALC. FROM EMISSION .0066 .0088 .0131 0165
EQUIVALENCE RATIO .0,7 "J, .J,J '"^1
LOADING H/P«N/V/EIT/5*fl» .*65 .**6 !*06 *kS
COMB EFFIC FROM EMISSIONS 97.101 98.20* 99.502 99 551
CARSON DIOXIDE SUMMARY OF RtOU-EO
PERCENT BY VOLUME, MET 1.32 1.79 2.72 3.**
LB. C02 PER LB. OF FUEL 3.02 3.06 s!l2 3 13
CARB^N'MONOXIDE' "•""*• S"'1 3"'5 ^ "*"
PPM BY VOLUME, HET 352.* *13.8 2**.7 298.3
LB. PER 1000 LB. OF FUEL 51.222 ".5.10* 17.886 17.229
HEIGHT FLOH, LB./HR. 5.225 5.593 3 130 3 273
UNBURNEO HYDROCARBONS- PPH AS CARSON, HEIGHTS AS CH*
PPM BY VOLUME, HET 232.5 13*.* 21.0 15.0
LB. PER 1000 LB. OF FUEL 19.317 8.37* .877 .1*1
HEIGHT FLOH, LB./HR. 1.970 1.038 .15* lol*
RATIO LB MC/LB CO .3771 .1857 .0*91 .0207
NITRIC OXIDE INO> - HEIGHTS AS N02
PPM BY VOLUME, HET 9.8 16.0 32.5 **.B
LB. PER 1000 LB. OF FUEL 2.3*0 2.865 3.903 *.17*
HEIGHT FLOH, LB./HR. .239 .355 .603 .793
NITROGEN DIOXIDE IN02I '
PPM BY VOLUME, HEI *.2 ~ it. 5 3.5 2 .
LB. PER 1000 LB. OF FUE". 1.003 .806 .360 .190
HEIGHT FLOH, LB./HR. .102 .101 .063 036
TOTAL OXIDES OF NITROGEN (NO+N02I AS NO2
PPM BY VOLUME, HET n,.o 20.5 35.5 *6 .
LB. PER 1000 LB. OF FUEL 3.3*3 3.671 *.2&J *.36*
HEIGHT FLON. LB./HR. *k< tec »7< iiZ
fc* »fc**i., ko«*nn. .oil «*>9 .7*6 >A2Q
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOH .00706 .00707 .00708 .00789
SMOKE NUMBER 9.60 10.80 *.60 10.20
CORRECTED HEIGHT FLOH .02117 .02121 .0212* .02127
SMOKE NUMBER 18.18 21.70 1J.38 22.90
CORRECTED HEIGHT FLOH .03526 .0353* .03539 .83538
SMOKE NUMBER 25.30 30.18 18.78 33.*8
CORRECTED HEIGHT FLOH .0*939 .0*9*8 .8*955 .0*953
SMOKE NUMBER 32.50 38.00 2*.7i *1.8fl
SMOKE NUHBER AT HA« 0.823 21.60 2S.*8 15.58 27.2i
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE HET VALUES.
2. EQUIVALENCE RATIO CALCULATED FROH C02.CO,AND rtC DATA AND FUEL
3. MASS EMISSIONS OF NO, N02, AND NO»NOZ CALCULATED AS N02 FROM C
(..COMBUSTION EFFICIENCY CALCULATED FROM CO, AND IMC AS VAPORIZED

23.1
*6«2 .
30.* ........
9*9.1
*1*21.0
39.1 	 " - 	 - - 	 • - - -
361.0
9.*9
1.9*0 	
*.31
.017*
190.1 -- - - -
.1153
.225
99 1 122
34 A
.IO
589.2
*>92»0
30.565
5.«07
c i n " " " , . - . __._.„.._
71.4I
l.ftll
*3*»*»
.0592 """ ~ 	 	 	
36.5
3.72IP 	 	 	 	
.718
-_•-_- 	 	 	 	 	 	 -- - - - -— . — , _ . ^ 	
3.B 	 -
» 306
. - ...-.Me 	 	
39«5
*.031
.766 " 	
.11709
18.11
.12132
36.71
.03551
*4.61
.1*972
51.81 '--'""'. • •- - - --.- 	
38.81 .
COMPOSITION. - "
ONCEMTRATIOMS WTM MOLECULAR «MHf OF tHU I46.«il.
ORIGINAL FUEL ON LI/ LB FUEL MSIS.
                                                                                                                                                         >)

                                                                                                                                                         I
                                                                                                                                                          )
-------
  ENGINE' STCP8S-98CK
DATA POINT HUHBER
EMISSION RATE LB/HR
    CARBON MONOXIDE
    UNBURNED HYDROCARBONS
    OXIDES OF NITROGEN
    NITRIC OXIDE
POKER LEVEL HP
TOTAL CORRECTED HORSEPOWER
                                                S/N
36179
   231

 5.225
 1.970
   . 3H
   .239
 0.00
 0.00
                                          »•»»  AIRtSEARCH  EMISSION TEST SUMMARY
                                          COMB P/N*  698168-3 TEST DATE  6-19-75
                                                                                                            FUEL'AV. KERO.
                                                                                                                              P BARO« 19.69
                                                                   23Z
                                                                             233
                                                                                       23<»
                                                                                                 Z35
5.593
1.038
.«*55
.355
52.52
79.73
06.U93
19.770
8.666
6. 76*
3.130
.15k
.71.6
.683
131.02
198.89
23.890
1.172
5.691.
5.213
3. 273
.091.
.829
.793
173.53
263.69
18.86". *
.5«>2
I..778
I..571
5.6*7
.3**
.766
.708
17.2.65
262. <»9
33.598
1.990
It. *30
"4.09".
                     BRAKE SPECIFIC EMISSION INDEX L8/1000HP-HR
                         CARBON MONOXIDE               0.000
                         UNBURNEO HYDROCARBONS         0.000
                         OXIDES OF NITROGEN            0.000
                         NITRIC OXIDE                  0.000
                         NOTE**0. APPEARING IN  BRAKE  SPECIFIC EMISSION INDEX COLUMN DENOTES AN IDLE CONDITION
(D
vo
-------
 13
 fl»
iQ
 (D
MAX SHP
FUELI ASTH 01655-73 ATONIC M/(

HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (COI
OXIDES OF NITROGEN (NOX t
It PHX LACC2
ENGINE
: RATIOt 1.92
IORK OUTPUT •• 1
SSIONS COMFUTtl
1.6-
31.71
S NOZ) 4.4<
COMBUSTOR TYPEt TANGENTIAL CAN P/N, 69816B-3t"sU(
ENGINE TOTAL SERVICEI 0.0 HR. TIME SINCE ENGINE OVE
> ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
AIRCRAFT INSTALLATION »•• MFR.I
) GASEOUS EMISSION TEST NO. « 16 DATE. 6-20-75 Tit
AMBIENT AIR TEMP. 1 59.0 DEG. F RE ATIVE HUMIDITY!
AMBIENT AIR QUALITY HYDROCARBONS IHCMO.O PPMC CA*
) SAMPLE LINE «• TEMP., 300.00 DEG. F. FLOH1ATEI l"l
TEST CONDITION
> POWER SETTING, CORRECTED HP.
Nl SPEED, RPM
FUEL FLOW (MEAS.I LB./MR.
) ENGINE CORE INLET AIRFLOW (CALC. 1 LB./SEC.
COMPRESSOR INLET TEMP., DEG. F
COMPRESSOR DISCHARGE AIR PRESSURE, PSIA
) COMPRESSOR DISCHARGE «IR TEMP., DEG. F
COMPRESSOR BLEED AIRFLOW (MEAS.) LB./SEC.
BLEED AIR PRESSURE, PSIA
) BLEED AIR TEMPERATURE, OEG. F
ENGINE EXHAUST CAS TEMP., OEG. F
EMISSION CONCENTRATION, WET ANALYSIS
; ' HYDROCARBON (HC AS CH4», PPMC
CARBON MONOXIDE (CO) , PPMV
TOTAL OXIDES OF NITROGEN tNOX) , PPHV
' CARBON DIOXIDE (COZ), PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSION INDEX, LB. POLLUTANT/lflflfl LB. FUEL
' HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4I
CARBON MONOXIDE (CO)
) TOTAL OXIDES OF NITROGEN (NOX AS NOZJ
ENGINE WOR< OUTPUT, MEAS. SMP
ENGINE WORK OUTPUT. ISENTROPIC AIR HP
) ENGINE HOIK OUTPUT, TOTAL MP
COMSUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/» (EMISSIONS!
236
0.00
41890.00
101.00
57.0
367.00
0.00
0.00
-0.00
491.0
2Z6.500
339. Z96
14.0PO
1.286
12.000
19.360
50.739
3.439
1.955
5.125
.347
0.00
0.00
0.00
97.11
TYPE (CLAI
IR EXTRACT]
t Lnv i
:OO£ OF FEC
J FROM TES1
>Z i.8. POl
L2 LB. POL
>5 LB. POL
IE OESCRIPT
(FACE/VOLUH
(HAUL 1
MODEL NO.
TEST DATA
El 13.00
70.00 PERC
BON MONOXI
6 LITERS/M
EO EMISSIO
237
79.58
41720.00
124.00
61.0
394!oO
g.oo
0.00
-0.00
618.0
133.500
<.OU.399
20.500
1.729
18.001
8.590
45.527
3.791
1.065
$.645
.470
52.47
0.00
52.47
98.18
.••9
>S)I APU
ON TO
FEDERAL
ERAL REGULATIONS T]
CONDITION NO. 5
LUTANT PER 1000 HP.
LUTANT PER 1800 HP.
LUTANT PER 1000 HP.
REG V38 N136 CALC. OATEI 6-28-75
CALC. I.O.I 3
F EGT
ADDITIVESI NONE

-HR.
-HR.
-MR.
Eo n'7" S° IN/CU IN FU£L INJ* TTPEI OUAL ORIFI«
1 USERt
BARO. PRESS. I 19.690 IN. H6A.
n?Tirn,. nSnECIFIC HUHIOITY« .007500 LB. H20/LB. DRY AIR
OE (CO)I 0.0 PPHV OXIDES OF NITROGEN (NOX)I 0.0 PPHV
IN. TRANSPORT TIMEI 6.50 SEC. LENGTH. 58.00 FT.
238
198.85
41450.00
172.00
3.76
59.0
401.00
0.00
0.00
-0.08
850.0
21.600
38^000
2.645
35.000
.928
18.571
4.690
.161
3.194
.807
130.86
0.00
130.86
99.48
.013
Z39
0.00
41350.00
198.00
4.89
60. •
37.17
363. OB
1.57
' 36.24
389.00
1014.0
16.500
282.571
47.000
3.327
44.000
.564
16.896
4.616
.1B7.
3.210
.877
0.10
176.61
176.61
99.5$
.(It
240 .---.-.
46. OB
41380.00
188.01 	
4.75
	 61. •
39.28 —
364.00
_ 1.Z8
38.38
388.00
949.8 _._....
42.000
460.824
39.500
3.118
37.008 __ 	
1.521
29.194
4.111 	
5.488
.77J
3a,33 	 	
14Z.7*
173.07
.•15 . .- .
                                                                                                                                                                                             £
                                                                                                                                                                                            -CD
-------
tu
«
(D

H1
Ul
ENGINE' GTCP»5-9»« S/N
RAT SHP« 208. RA E6T,F»
FUEL H/C= 1.9288 STOI F/A«
DATA POINT NUMBER
PERCENT MAX. CORRECTED POKER
CORRECTED SHAFT HP
MEASURED SHAFT HP
EXHAUST GAS TEMP., DEG.F
SHAFT SPEED, Nl, RPM
COMPRESSOR OSCHG. PRES. ,PSIA
COMPRESSOR OSCHG. TEMP, DEC F
EXHAUST GAS PRESS., PSIA
CORRECTED BLEED FLOH, L8/SEC
COMPRESSOR MAP FLOH,L8/SEC
FA RATIO BASED ON MAP FLOM
CORRECTED FUEL FLOH , LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P»»N/V/E(T/548)
COM3 £FFIC FROM EMISSIONS
* 36179
1150.
.06822
236
0.0
0.0
8.0
491.0
*1880.0
*2.5
387.0
9.37
0.000
3.99
.0070
101.0
.00 in
.094
.473
97.108
COHB P/M* 696168-1 TEST DATE 6-20-75 FUEL'AV. KERO. P BARO« 19.69 	
RAT SPO* *1680. OEM PT,F« 51. REL HUM' 78.08 SPEC HUM> .887500
L H V* 18478. S UN t,F« 388.0 FLO,L/M« 14.160 Si TIH,S» 6.5000
237 238 239 240 ,
39.8 99.4 0. 23.8
79.6 198.8 1. 46.8
52.5 130.9
618.0 850.0
41720.0 41*50.0
42.1 42.8
394.0 *01.8
9.*2 9.51
0.000 0.000
3.73 3.47
.0092 .0138
124.0 172.0
.0085 .8127
.125 .186
.443 .408
98.175 99.482
CARBON DIOXIDE
PERCENT BY VOLUME, MET 1.29 1.73 2.64
LB. COZ PER -.8. OF FUEL 3.02 3.06 3.12
HEIGHT FLOM, ..B./HR. 305.1 379.3 537.0
CARBON MONOXIDE
PPM BY VOLUME, MET 339.3 1.0*. * 2*7.1
LB. PER 1800 LB. OF FUEL 50.739 *S.527 18.571
HEIGHT FLOH, LB./HR. 5.125 5.645 3.19*
UNBURNED HYDROCARBONS- PPH AS CARBON, HEIGHTS AS CH*
PPM BY VOLUME, NET 226.5 133.5 21.6
LB. PER 1080 LB. OF FUEL 19.368 8.590 .928
HEIGHT FLOM. LB./HR. 1.955 1.065 .168
RATIO LB HC/i.8 CO .3816 .1887 .0580
NITRIC OXIDE (NO) - HEIGHTS AS NOZ
PPM BY VOLUME, HET 12.0 18.8 35.0
LB. PER 1000 LB. OF FUEL 2.9*8 3.329 *.3Z8
HEIGHT FLOH, LB./HR. .298 .413 .743
NITROGEN DIOXIDE (NOZI
PPM BY VOLUME. HET 2.0 2.5 3.0
LB. PER 1800 LB. OF FUEL .491 .46Z .370
HEIGHT FLOH, LB./HR. .850 .057 .064
TOTAL OXIDES OF NITROGEN (NOtNOZI AS N02
PPM BY VOLUME. HET 14.0 28.5 38.8
LB. PER 1080 LB. OF FUEL 3.439 3.791 4.690
HEIGHT FLOH, ..B./HR. .3*7 .470 .807
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLCH .00787 .00705 .80785
SMOKE NUMBER 4.80 9.60 7.80
CORRECTED HEIGHT FLOM .82121 .02116 .82116
SMOKE NUMBER . 17.50 19.90 12.08
CORRECTED HEIGHT FLOM .0353* .03526 .03519
SMOKE NUMBER 24.10 28.90 18.10
CORRECTED NEIGMT FLCM .04945 .04936 .04926
SMOKE NUMBER 28.90 33.70 2*. 10
SMOKE NUMBER AT MA=0.023 19.00 23.30 15.70
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE MET VALUES.
8.
1014.
41350.
37.2
363.8
9.50
2.395
4.39
.0188
190.0
.0159
.233
.448
99.553
REDUCED
3.33
3.13
593.9
282.6
16.896
3.210
16.5
.564
.107
.0334
4*. 8
4.322
.821
3.0
.295
.056
47.0
4.616
.877
.08784
10.88
.82111
24.18
.03525
33.78
.04935
43.40
28.38
30.3
949.8
41388.8 .. . . 	 	 .„
39.3
364.0
9.50
1.949
4.32
.0172 . _ 	 	 	 	 	
188.0
.0158
.221
.431
99.180
3.12
3.10 	 	 	 	 _ 	 _ _...
583.6
29.194.
5.*88
42.8
1.521
.0521
37.0
3.850
.724
2.5 '. ~
.260
.049
39.5
4.111
.773
.00785 _
11.48
.82111
22.98 _ _. . . ..• 	 	
.03518
37.38
.84925
42.20
28.88
                                                                                                                                                               )!
                           Z.EQUIVALENCE RATIO  CALCULATED  FROM COZ,CO,AN3 HC DATA AND FUEL COMPOSITION.
                           3.MASS EMISSIONS  OF  NO,  NOZ.  AND  NO»N02 CALCULATED AS NOZ FROM CONCENTRATIONS MITH MOLECULAR  HEIGHT OF NOZ (46.01).
                           4.COMBUSTION EFFICIENCY  CALCULATED FROM CO,AND UHC AS VAPORIZED ORIGINAL FUEL ON LB/ LB FUEL  BASIS.
'S
-------
ENGINE= GTCP85-98CK S/N = 36179
DATA POINT NUMBER Z36
EHISSIOM RATE LB/HR
CARBON MONOXIDE
UNBURNED HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIDE
POWER LEVEL HP
TOTAL CORRECTED HORSEPONER
BRAKE SPECIFIC EMISSION INDEX
CARBON MONOXIDE
UNBliKNEO HYDROCARBONS
OXIDES OF NITROGEN
NITRIC OXIOE

5.135
1.95S
.3*7
.298
0.00
0.00
COM3 P/N= 698168-3 TtST DATE 6-20-75
237 23* 230 ;>..•

S.6VS
1.065
.8.65

18.175
.607
t.966
•..&<, 9

5,«.e»
.286
.773
.72.*65
t>.182
                                                                                                                FUEL'AV. KERO.
                                                                                                                                   P BARO= 19.69
                            NOTE»»0.  APPEARING IN BRAKE SPECIFIC EMISSION INDEX COtUHN DENOTES  AN  IDLE  CONDITION
p>
vQ
0>
 in
 to
-------
                                                                                                                                                                  i
fD
ai
OJ
                      •»•«..»*.•*»*•••«•*».•*,**••»,«>.(»•»*•*„.,.   MRESEARCH  EMISSION TEST SUMMARY  •••»••»•»•»••»
                      ENG HFG : AIRESEA3CH           TEST FSCIL  I  PHX LACC2   INSTR OESCRIP : FED REG VI8 N136
                      MODEL NO.<     TPE331-5-251M      S/NI    P04001               ENGINE TYPE(CLASS!I  TURBOPROP
                      RATED POMERI     706.0  SHP  AT  SEA  LEVEL STANDARD DAY  CONDITIONS
                      FUEL I ASTM 01655-73            ATOMIC  H/C  RATIO:   1.928     LHVI 18470. BTU/LB     ADDITIVES:
                                                                                                                       NONE
 CALC DATE Hl-S-75
 CALC IDt   1
TEST NOI     1
                       ••»**»»* EXHAUST  EMISSIONS PER EPA CYCLE OF WORK OUTPUT »* CODE OF FED.EFAL REGULATIONS TITLE 40 PART 87  17 JULY
                                           HYDROCARBONS (CH AS CH4)          4.360 -8. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                           CARBON MONOXIDE (CO)             19.665 L3. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                           OXIDES OF NITROGEN (NOX AS N02)    9.202 .8. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                           SMOKE                             IS.8  SMOKE NUMBER, MAXIMUM AT  CRUISE    MODE.  70  PERCENT  RATED  POWER
                       TAXI-IDLE  SETTING!  5.0      PERCENT RATtD TAKEOFF POW£R AT 65.      PERCENT RATED TAKEOFF Nl RPM
                       [[[  ENGINE DESCRIPTION  ••••••»••»••••»••••»••••»»•»••»»•••»•••••••••••••»••
                       COMB  TYPE:  REVERSE  FLOW ANNULAR           P/NI   869082-4           SUR/VOi.: 1.260  FUEL INJ TYPE:   STAGED  SIMPLEX
                       ENGINE  TOTAL  SERVICE'   0.0       HR    TI1E SINCE ENGINE OVERHAUL'  0.0       HR
                       ENGINE  ASSEMBLY  AND MAINTENANCE INFORMATION:
                       AIRCRAFT  INSTALLATION  **** MfR.I                                  MODEL NO.t
                                                  USER:                        ENGINE INSTALLATION POSITION:
                       ..............,.,....................,..........OPE,,ATIONAL r£ST OAIA SUMMARy ..»..»..•».»».»»»»»»»»»»»»»»•»•»«••»»••••••»»»••
                       GASEOUS EMISSION TEST  NO.>     1         DATE! 11-5-75            TIME:                    BARO PRESS.I  28.780  IN.  H6A.
                       AMBIENT AIR TEMP.:   19.00  OEG.  F         RELATIVE HUMIDITY:  1.9.00 PERCENT       SPECIFIC HUMIDITY:   .001000  LB.  H20/LB.  DRY  AIR
                       AMBIENT AIR QUALITY    HYDROCARBONS IHCII  0.0   PPNC     CARBON MONOXIDE (COX 0.0   PPMV    OXIDES  OF NITROGEN  (NCX)I  0.0    PPMV
                       SAMPLE  LINE ***  TEMP.:   300.00  OEG. F.      F.ONRAUI   14.16 LITERS/MIN.     TRANSPORT TINE:    6.50 SEC.     LENGTH:    50.01 FT.
                                        y

                                        y
TEST CONDITION
ACTUAL POWER SETTING, HORSEPOWER
CORR. POHtR SETTING (STO DAY), PERCENT RATED
Nl SPEED, RPM
FUEL FLCW (MEAS.I LB./HR.
CORR. ENGINE CORE AIRFLOW (HEAS). LB/SEC
COMPRESSOR IN.-ET AIR TOTAL TEMP., OEG F
COMPRESSOR INLET AIR TOTAL PRESS.. PSIA
COMPRESSOR DISCHARGE AIR TOTAu PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL TEMP.. D£G F
TURBINE INTERSTAGE GAS TOTAL TEMP., UEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION, WET ANALYSIS
HYDROCARBON «HC AS CH".) , PPMC
CARBON MONOXIDE ICOI , PPMV
TOTAL OXIDES OF NITROGEN INOX), PPMV
CARBON DIOXIDE (C02) , PERCENT BY VOL.
NITRIC OXIDE INO), PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4>
CARBON MONOXIDE ICOI
TOTAL OXIDES OF NITROGEN (NOX AS N02I
EMISSION RATE. LS. POLLUTANT/riP.
HYDROCARBONS IHC AS CM4)
CAP60N MONOXIDE ICO)
TOTAL OXIDES OF NITROGEN (NOX AS NO2)
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS, CALCI
123
33.3
5.11
27510.00
105.0
3.1
18.00
14.14
51.08
296.00
900.0
14.13

93.000
225.166
20.600
1. 840
12.000.

5.700
24.142
3.628

.598
2.535
.381
98.93
.0089
49.1
7.53
27500.00
113.0
3.1
18.00
14.14
51.18
301.00
845.0
14.12

48.600
202.590
25.500
2.023
17.500

2.722
13.853
4.105

.308
2.243
.464
99.29
.0098
65.0
9.98
27540.00
125.0
3.0
17.00
14.14
51.47
301.00
895.0
14.12

39.300
186.904
28.300
2.151
21.300

2.075
17.262
4.293

.259
2.158
.537
99.41
.0104
4
195.8
29.89
41720.00
258.0
8.1
23.00
14.14
140.47
628.00
1032.0
14.01

6.300
65.235
57.500
1.886
42.400

.362
6.919
10.018

.099 "
1.78S
2.585
99.80
.0090
5
455.5
69.60
41760.00
346.0
8.1
22.00
l4.ll.
146.58
638.00
1246.0
14.03

.900
26.732
90.200
2.519
81.000

.041 _.
2.128
11.795

.01",
.736
4.061
99.95
.11120
6
585.7
89.49
41730.00
388.0
6.1
22.00
14.14
152.26
643.00
1347.0
14.06

.901
19.039
99.25*
2.879
90.250

.036
1.327
11.361
_
• 014
.515
4.406
99.97
.0137
7
653.1
100.20
41760.00
415.0
6.1
16.00
14.14
154.72
640.01
14*3.0
14.06

.60*
15.621
109.250
3.066 	 __:
100.5*1 :

	 .022 	 1:
1.035
11.743
•
.009 " ~;
.430
4. 871 	 	 . 	
99.97
.0146
                                                                                                                                                                   >;,
-------
                     ..........................................   EpA CTC_E £NISSIONS  COMPUTATION SUMMARY  •••••••••«
                     ENG MFC I AIRESEARCH           TEST FACIL  I  PMX LACC2   INSTR OESCRIP I  FED REG V38 N136
                     MOOEi. NO.t     TPE331-5-251M     S/NI   P04001               ENGINE TYPE (CLAiS) 1  TURBOPROP
                     RATED POWER I    706.0 SHP AT SEA LEVEL STANDARD DAY CONDITIONS
                     FUEL! ASTM 01655-73            ATOMIC H/C  RATIO!   1.928      LMVI  18470.  BTU/LB     ADDITIVES!
                                                                                                          CALC DATE 111-5-75
                                                                                                          CALC IDI   1
                                                                                                         TEST NOI     1
                                                                                                                      NONE
CD
in
•u
                            "ODE
                                                                          TAXI-IOiE
                                                                             (INI
                                                                       TAXI-IDLE
                                                                         (OUTI
                                                                                                      APPROACH
                                                                                                  CLIMBOUT
                                                  TAKEOFF
                                                             TOTAL PER
                                                              CYCLE
    TIME IN MODE, HINUTES
    RATED POWER. PEUCEHT
    CORRECTED POWER. HORSEPOWER
    HP-NR
    FUEL FLOW, LB/HR
    FUEL MASS, LB

     " HYDROCARBON EMISSION  (HCI »•
    INDEX, LB HC/1000 LB FUEL
    RATE, L8 HC/HR
    MASS, LB HC
    MASS, PERCENT OF TOTAL  CYCLE
    CYCLE, LB HC/1000 HORSEPOMER-HR PER CYCLE

     •• CARBON MONOXIDE EMISSIONS (CO) ••
    INDEX, LB CO/1101 LB FUEL
    RATE. LB CO/HR
    MASS, LB CO
    MASS, PERCENT OF TOTAL  CYCLE
    CYCLE, LB CO/1000 HORSEPONER-HR PER CYCLE

     •• TOTAL OXIDES OF NITROGEN EMISSIONS  (NOXI
    INDEX, LB NOX/1010 LB FUEL
    RATE. LB NOX/HR
    MASS, LB NOX
    MASS, PERCENT OF TOTAL  CYCLE
    CYCLE, LB NOX/1000 HORSEPOWER-HI  PER CYCLE
7.000
5.001
35.300
4. 116
114.751
12.221
19.000
5.000
IS. 300
11.176
194.750
S3. 171
4.500
30.000
211. SOO
15.865
256.585
19.394
2.500
90.000
635. 400
26.475
369.355
16.223
.501
111.011
706.000
5.863
414.561
3.455
33.511


63.541

14.461
                                                                               5.906
                                                                                .619
                                                                                .072
                                                                                26.1
                                                                              24.3«2
                                                                               2.554
                                                                                .296
                                                                                23.6
3.594
 .376
 .044
  7.5
             5.906
              .619
              .196
              71.7
            24.382
             2.554
              .809
3.594
 .376
 .119
 21.4
              .334
              .086
              .006
               2,3
             6.859
             1.774
              .133
              10.5
10.06D
 2.601
  .195
  33.4
               .129
               .050
               .002
                 .6
              1.165
               .461
               .019
                1.5
11.447
 4.457
  .186
  31.6
               .115
               .146
               .111
                 .1
               .934
               .367
               .103
                 .3
 11.797
.  4.691
   .141
    7.1
               3.281
                .496
                .277
               100.0
               4.361
              14.944
               2.261
               1.262
               100.1
              19.165
6.923
1.047
 .515
101.1
9.20Z
)


)


)


)
                                           •• EMISSION  INDEX  LEVELS REQUIRED TO MEET EPA 1979 STANDARDS FOR CLASS P2 ENGINES'"'
                                        EPA LTO-CYCLE
                                 POLLUTANT   LBP/1000 HORSEPOMER-HR-CYCLE '
                                    CO             26.8
                                    HC              4.9
                                 -   NOX            12.9
                                                                                                 REQUIRED EMISSION INDEX, LBP/llOO LB FUEL
                   POLLUTANT (NODE)
                      CO IIDLEI
                      HC (IDLEI
                      NOX ITAKEOFFI
                                                B
                                             34.1
                                              6.7
                                             24.1
                                           A  ASSUMES  PROPORTIONAL REDUCTION OF POLLUTANT EMISSION INDEX AT EACH LTO CYCLE HOOC"

                                           B  ASSUMES  (II  REQUIRED REDUCTION IN CO AND HC OBTAINED BY LOWERING EMISSION INDEX VALUES
                                              AT TAXI-IDLE NODE  ONLY,  CO AND HC EMISSIONS AT OTMcR NODES RiNAIN UNCHANGED. (21 REQUIRED
                                              REDUCTION  IN NOX OBTAINED BY LOkeRING EMISSION INDEX VALUES AT CLIMBOOT AND TAKEOFF HOOES IN
                                             KMH*Wc52«!o" ""SU*£°  "tU£S>  "°X  ""SIONS AT TAXI-iOLE AND APPROACH MOOES  _*___
                                                                                                                                            	 it
                                                                                                                                                                '£
                                                                                                                                                                .JCV
-------
           wiwiwiwnnnnnuunuwuntwniwVwuwuutwiMimnwuniwt
                                                                                    •5
0)
iQ
(D
Ul
(J1

ENGINE* TPE331-5-Z51M S/N* PI4101
RAT SHP= 706. RA EGT,F» 1650.
> FUEL H/C« 1.9260 STOI F/A* .06622
DATA POINT NUMBER 1
' PERCENT MAX. CORRECTED POWER 5.1
CORRECTED SHIFT HP 36.1
MEASURED SHAFT HP 33.3
1 SHAFT SPEED, Nl , RPM 27510.0
COMPRESSOR INLET- TEMP., OEG.F 18.0
COMPRESSOR DSCHG. PRES..PSIA 51.1
> COMPRESSOR DSCHG. TEHP.CEG F 296.0
TURa INTERSTAGE TEMP., DEG.F 600.0
CORR BELMTH FLOW, LB/SEC 3.07
t FA RATIO BASED ON BELLMTH. .0895
MEASURED FUEL FLOH, L6/HR 105.0
FA RATIO CALC. FROM EMISSION .0089
) EQUIVALENCE RATIO .131
LOADING W/P"N/V/ECT/540) .330
COM3 EFFIC FROM EMISSIONS 98.932
CARBON DIOXIDE
PERCENT BY VOLUME, WET 1.84
) LB. COZ PER LB. OF FUEL 3.10
WEIGHT FLOW, LB./HR. 325.5
CARBON MONOXIDE
1 PPM BY VOLUMc, WET 225.2
LB. PER 1000 LB. OF FUEL 24.142
' WEIGHT FLOW, LB./HR. 2.535

COMB
RAT SPD= 41730.
L H V- 16470.
2 3
7.5 10.0
53.2 70.5
49.1 65.0
27500.0 27540.0
18.0 17.0
51. Z 51.5
301.0 301.0
845.0 895.0
3.05 2.96
.0103 .0117
113.0 125.0
.0098 .0104
.143 .152
.324 .312
99.294 99.412

2.02 2.15
3.12 3.12
352.8 390.2

202.6 106.9
19.853 17.262
2.243 2.158



P/N* 869062-4 FUEL* AV. ICERO. TEST NO.* 1
DEW PT,F* 6. REL **M
S LN T,F»
4
29.9
211.1
195.8
41720.0
23.8
140.5
626.8
1032.0
6.06
.0069
258.0
.0090
.132
.080
99.804
REDUCED
1.69
3.14
810.7

65.2
6.919
1.785
300.0 FLO.L/M
5 6
69.6 89.5
491.4 631.8
455.5 585.7
41760.0 41730.8
22.0 22.8
148.6 152.3
636.0 643.0
1246.0 1347.0
8.08 8.08
.0119 .0134
346.0 388.0
.0120 .0137
.176 .201
.071 .067
99.946 99.966

2.52 2.88
3.15 3.15
1090.1 1222.9

26.7 19.0
2.128 1.327
.736 .515
* 49.81 SPEC HUN* .111100
* 14.168 SL TIM.S- 6.5000
7
100. Z
707.4
653.0
41760.0
16.0
154.7
640.0
1403.0
8.11
.0142
415.1
.0146
.214
.066
99.974

3.07 " "
3.15
1308.Z

15.6
1.035 	 	
.430
UNBURrfEO HYDROCARBONS- PPN AS CARBON. WEIGHTS AS CH4
PPM BY VOLUME, WET 93.0
L3. PER 1000 LB. OF FUEL 5.700
> WEIGHT FLOW, LB./HR. .596
RATIO LB HC/LB CO .2361
NITRIC CXIOE (NOI - WEIGHTS AS N02
) PPM BY VOLUME, WET 12.0
LB. PER 1000 LB. OF FUEL 2.113
WEIGHT FLOW, LB./HR. .222
) NITROGEN DIOXIDE INOZ)
PPM BY VOLUME, WET 8.6
LB. PER 1000 LB. OF FUEL 1.515
) WEIGHT FLCW, LB./HR. .159
TOTAL OXIDES OF NITROGEN INO«N02) AS N02
PPH BY VOLUHE, NET 20.6
) LB. PER 1000 LB. OF FUEL 3.626
WEIGHT FLOH, LB./HR. .381
SMOKE MEASUREMENT DATA
) CORRECTED WEIGHT FLOW .00710
SMOKE WUMBER 1.21
CORRECTED WEIGHT FLOW .02130
) SMOKE NUMBER 3.50
CORRECTED WEIGHT FLCW .03557
SHCKE NUMBER 7.10
) CORRECTED WEIGHT FLCW .04979
SMCKE NUMBER 7.10
SMOKE NUMBER AT WA*O.OZ3 4.70
; NOTES 1. Ai.L EMISSIONS CONCENTRATIONS ARE
2. EQUIVALENCE RATIO CALCULATED FROM
48.6 39.3
2.722 2.075
.306 .259
.1371 .1202

17.5 21.3
2.817 3.231
.318 .404

8.1 7.0
1.268 1.062
.146 .133

25.5 26.3
4.105 4.293
.,64 .537

.00710 .00705
2.40 3.50
.02130 .02114
3.50 5.90
.03549 .03523
7.10 5.90
.04969 .04924
6.20 . 4.70
5.30 5.00
WET VALUES.
C02.CO.ANO HC DATA
6.3
.382
.099
.0552

42.4
7.387
1.906

15.1
2.631
.679

57.5
10.018
2.585

.00702
4.70
.02105
6.20
.03508
12.90
.04912
14.10
10.10

AND FUEL
3. MASS EMISSIONS OF NO, N02. AND NO+N02 CALCULATED AS NO2 FROM
J


.9 .9
.041 .036
.014 .014
.0192 .1270

81.0 90.2
10.592 10.331
3.665 4.909

9.2 9.0
1.203 1.130
.416 .1.00

90.2 99.2
11.795 11.361
4.081 4.408

.00702 .00700
3.50 3.50
.02105 .02101
14.10 12.91
.03506 .03501
20.00 18.80
.04912 .04902
24.70 25.98
15.81 15.61

COMPOSITION.
CONCENTRATIONS WITH

.6
.022
.009
,0217 	 	 	 	

108.5
10.883 	 __.... 	 ... 	 . _
4.463

8.8
.941
.398

109.2
11.743
4.873, 	 	

.80699
5.98 	 	 . .. ._.. 	 	 	 ...._
.02896
18.60
.8349* 	 ....... . .
20.80
.04692
22.40 .. _ 	 	 ...... 	
14.91


MOLECULAR WEIGHT OF N02 (46.11). """"•

                                                                                     Y
-------
 f»
«Q
 (D
 ui
 o\
                                            ••""»»•»»•»*»»»•»*»»•»»»..»  AIRESEARCH EMISSION TEST SUMMARY  ......

                            5SS-P Sn . IRESf  CM            TEST F*CIL ' P"X L*6C2  INSTR °"«IP ' '» KS6 V30 NUt
                            HOOcL NO. I     TPE331-5-251H      S/NI    PfelOl              £N5IN£ TYPE (CLASS) •
                            R*TcD FOHERI    706.0 S»*> AT SEA  LE«L  9tMMR0 BAY CONDITIONS          »•"•»••

                            FUELl ASTM 01655-71             ATOH16 «/C *ATlBt   1.92*     LN«f 1ID7I. BtUA-B
                                                                                                                 AODITIWESI  MOME
                                                                                                       C8MLOATE IU-6-75
                                                                                                       CALOttlDi   Z
                                                                                                      TEST NM    1
........ EXHAUST E«SSIO«  J« fJ'J'CVE Of W«K OUTPUT « COOt OF rtO£RAt REiULATlONS  TITLE ^0 PART S7

                    MYOROCARBOHS »CH AS CMMI          «..fl»l LB. POLLUTANT PER 1000  MP.-HR.  PER CYCLE

                    CARBON  MONOXIDE ICO)             30.911 .8. PX.UT»NT PtR 1000  HP.-HR.  PE* CYCLE

                    OXIDES  OF  NITROGEN (NOX AS NO2)   9.290 LB. POLLUTANT PtR 1000  HP.-HR.  PER CYCLE


TAXI-IDLE SETTING, s!?"'    PERCENT ,ATED TAKEOFF PO-E"« £°** ™""     "             "™'  ''
                                                                                                                                       17  JULY 1971
                                                                                                                                                «""
    ~~.......................,...,.•..,...,,..„,....  CNGJNE DESCRIPTION  »*»»»*»»»»»»•»•«.........

COMB TYPEJ REVERSE FLOW ANNULAR            p/Nt   869082-4           SUR/VOtl 1.260  FUEL  INJ  TYPE.
ENGINE TOTAL SERVICE.  0.0        HR    TIME SINCE ENGINE OVERHAUL.  0.0       MR

ENGINE ASSEMBLY AND MAINTENANCE  INFORMATION.

AIRCRAFT INSTALLATION •••• MFR.I                                  MODEL NO.I

„„,                      USERI                        ENGINE INSTALLATION POSITION!
                                                                                                                                  STAGED  SIMPLEX
                            CASEOUS EMISSION TEST NO.I    1

                            AMBItNT AIR T.EHP.I  19.00 3E6. F
                                         OATEI 11-6-75            TIME.                    8ARO  PRESS.!   28.780 IN. HCA.


AMBIENT AIR QUALITY    HYDROCARBONS  IHClf oT Vp^'^'cAR.^^^^'^1 (CO, . ^"ppS*"0""1"'   •001000 "• ""'^ ™ *"<
SAMPLE LINE *»» TEMP..  300.80 OEG.  F.      FLOtHATE.   14.16 IITERS/MIN.     TRANSPORT
      OXIDES OF NITROGEN  INOXII  0.0    PPNV
TIMEl    6.50 SEC.     LENGTH!    58.00 FT.
1 TEST CONDITION
ACTUAL POWER SETTING, HORSEPONER
CORR. POWER SETTING ISTD OAYI , PERCENT RATED
Nl SPEEO. *PN
FUEL F^CH IHEAS.) LB./HR.
CORR. INGINE CORE AIRFLOW IMtASI , LB/SEC
> COMPRESS** INLET AIR TOTAL TtMP. , OEG F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTA. PRESS., PSIA
I COMPRESSOR DISCHARGE AIR TOTAL TEMP., OEG F
TURBINE INTERSTAGE GAS TOTAL TEMP., DEC F
EXHAUST GAS STATIC PRESSURE, PSIA
1 EMISSION CONCENTRATION, WET ANALYSIS
HYDROCARBON IMC AS CM4), PPMC
CARBON rONOXIOE (CO) , PF*V
) TOTAL OXIDES OF NITROGEN (NOX), PPMV
CARBON DIOXIDE (C02I , PERCENT BY VOL.
NITRIC OXIDE (NOI, PPMV
) EHISSIOK INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS IHC AS CH4I
CARBON MONOXIDE ICOI
> TOTAL OXIDES OF NITROGEN (NOX AS NOZI
EMISSION RATE, LB. POLLUTANT/MR.
HYDROCARBONS IHC AS CH4I
CARBON MONOXIDE ICOI
TOTAL OXIDES OF NITROGEN INOX AS NOZI
COMBUSTION EFFICIENCY, PERCENT (EHISSIONSI
F/A (EMISSIONS, CALCI
*

32.7
5.02
27560.00
105.0
3.0
16.00
5l!23
300.00
805.0
14.12
82.500
19.700
1.827
15.100
5.093
25.352
3.495
.535
2.662
.367
98.96
.0089

49.0
7.53
27560.00
11-.. 0
3.0
17.00
5l)47
300.00
860.0
69.600
208. 652
24.100
2.000
17.000
3.938
•20.654
3.919
.449
2.355
99.17
.8097
64.9
9.96
27520.00
125.0
3.0
18.00
14.14
51.33
302.00
921.0
14.12
54.000
198.415
27.800
2.180
23.600
2.810
18.060
4.157
.351
2.258
.520
99.33
.8105


194. 5
29.87
41750.00
264.0
8.0
17.00
140I32
623.00
1071.0
13.99
14.700
66.076
57.000
1.858
44.700
.904
7.106
10.070
.239
1.876
2.658
99.75
.0089


456.9
70.11
41730.00
350.0
£55. Z
18.00
14.14
149.31
632.00
1250.0
14.00
6.900
32.851
86.100
2.566
79.000
.308
2.566
11.049
.108
.898
3.867
99.91
.8122


13
588.9
89.23
41750.00
396.0
8.1
17.08
153!z4
635.00
1345.0
14.04
6.888
27.953
97.250
2.045
91.088
.242
1.970
11.257
.896
.788
4.458
99.93
.8135


14
653,8 ___
108.31
41760.08
420.8 	
8.1
17.08
14.14 	
155.78
639.08
1401.0 	
14.06
6.800
21.057
109.508
3.872
101.580
.22* 	
1.375
11.744
.09*
.577
4.932
99.95
.0146

                                                                                                                                                                         iV
-------
(D

M
(Jl
                       •..I.,..,**.,,.,..**....,*.,........**,...,  £PA C,C,E EMISSIONS COMPUTATION SUMMARY   ••••••••••
                       ENG HFG  I AIRESEARCH           TEST FACIL I PHX LACCZ  INSTR OESCRIP  I  FED  REG  V38 N136
                       MODEL N0.<      TPE331-5-Z51M     S/NI   PQ4001              ENGINE  TYPE(CLASS)!  TURBOPROP
                       RATED POMER!     706.0 SHP AT SEA LEVEL STANDARD DAY CONDITIONS
                       FUELI ASTM  01655-73            ATOMIC H/C RATIO!   1.928     uHVt  18470.  BTU/LB     AODITIVESI
 CALC DATE 111-6-75
 CALC IDI   Z
TEST HOI    1
                                                                                                                         NONE
MODE
TIME IN MODE, MINUTES
RATED POHER, PERCENT
CORRECTED PONER, HORSEPOWER
HP-HR
FUEL FLOW, LB/HR
FUEL MASS, LB
•* HYDROCARBON EMISSIOK (HC) ••
INDEX, LB HC/1000 LB FUEL
RATE, L8 HC/HR .
MASS. LB HC
HASS, PERCENT OF TOTAL CYCLE
CYCLE. LB HC/1000 HORSEPOHER-HR PER CYCLE
•» CARBON MONOXIDE EMISSIONS (CO) »•
INDEX, LB CO/1000 LB FUEL
RATE, LB CO/MR
HASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORSEPOHER-HR PER CYCLE
•» TOTAL OXIDES OF NITROGEN EMISSIONS (NOX) "»»~
INDEX, LB NOX/1000 LB FUEL
RATE, LB NOX/HR
HASS, LB NOX
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB NOX/1000 HORSEPOHER-HR PER CYCLE
TAXI-IO-E 1
(IN)
7.000
5.000
35.300
4.118
104.923
12.241

5.103
.535
.062
24.4


25.413
2.666
.311
23.4

. - .. _ -
3.489
.366
.043
7.2

rAXI-IOLE
(OUT)
19.000
5.000
35.300
11.178
104.923
33.226

5.103
.535
.170
66.2


25.413
2.666
.844
63.5


3.489
.366
.116
19.6

APPROACH
4.500
30.000
211.800
15.885
264.923
19.869

.915
.242
.018
7.1


7.032
1.863
.140
10.5

..
10.114
2.679
.201
34.0

CLIHBOUT
2.500
90.000
635.400
26.475
399.274
16.636

.297
.119
.005
1.9


1.767
.705
.029
2.2

	
11.381
4.544
.189
32.1

TAKEOFF
.500
100.000
706.000
5.883
420.681
3.506

.273
.115
.081
_ .4


1.Z48
.525
.084
.3


11.811
4.968
.041
7.0

TOTAL PER
CTCLE
33.518


63.540

B5.*78 ..

2.996
.459
.256
100.0
4.031

15.5*7
2.388
1.329
101.0
20.915

6.906
1.057 _
.590
100.8
9.290
                                              ••  EMISSION INDEX LiVtLS RE3UHED TO MEET EPA  197S  STAN3ARDS  FOR CLASS P2 ENGINES ••
                                           EPA  LTO-CYCLE
                                   POLLUTANT    LBP/iaOO  HORSEPOHER-HR-CYCLE
                                      CO              26.8
                                      HC               <>.9
                                      NOX             12.9
                                                                                                    REQUIRED EMISSION INDEX, LBP/1000 LB FUEL

POLLUTANT (HODEI
CO IXOkEI
HC (IDLE)
NOX (TAKEOFF)

A
25.4
5.1
11.8

B
33.6
_ . 6.3
23.6
                                              A   ASSUMES PROPORTIONAL REDUCTION OF POLLUTANT  tHISSION  INDEX AT  EACH LTO CYCLE MODE

                                              B   ASSUMES (II 
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 13
 ft)
vQ
 (D
 tn
 oo
)

ENGINE* TPE331-5-Z51N S/N« P0*001 COMB P/N= 6690SZ-* FUEL=
RAT SHP= 706. M EGT,F= 165D. RAT SPO* *1730. OEM PT.F* 8. REL HUM=
FUEL H/C« 1.9380 STOI F/A« .0683Z L H »= 16*70. S LN T.F= 300.0 FLO.L/M*
DATA POINT NUMBER 89 18 11 1Z 13
PERCcNT MAX. CORRECTED POWER 5.0 7.5 10.0 Z9.9 70.1 89. Z
CORRECTED SHAFT HP J5.5 53.2 70.3 Z10.9 *95.0 639.9
MEASURED SHAFT HP 3Z.7 *9. 0 64.9 19*.5 *56.9 580.9
SHAFT SPEED. Nl , RPM Z7S60.0 Z7560.0 37520.0 ".1750.0 1.1730.0 *1750.0
COMPRESSOR INLET TEHP.tDEG.F 16.0 17.0 18.0 17.0 18.0 17.0
COMPRESSOR OSCHG. PRES.,PSIA 51. Z 51. 5 51.3 1*0.3 11.9.3 1S3.2
COMPRESSOR OSCHG. TEHP.OEG F 300.0 300.0 30Z.O 6Z3.0 632.0 635.0
TURB INTERSTAGE TEMP., OEG.F 805.0 860.0 9Z1.0 1071.0 1Z50.0 13*5.0
CORR 3ELMTH FLOM, LB/SEC 3.0<< 3.05 Z.96 8.0Z 255. Z3 8.08
FA RATIO BASED ON BELLHTH. .0096 .0103 .0117 .0091 .000* .0136
MEASURED FUEL FLOW, LB/MP. 105.0 11*. 0 125.0 Z6*.0 350.0 396.0
FA RATIO CALC. FROM EMISSION .0089 .0097 .0105 .0089 .0122 .0135
EQUIVALENCE RATIO .130 .1*2 .15* .131 .179 .198
LOADING H/P"N/V/E O/5*0 > .3Z3 .331 .31Z .080 Z.Z5* .068
COHB EFFIC FROM EMISSIONS 98.957 99.169 99.339 99.75* 99.913 99.93Z
CARBON DIOXIDE
PERCENT BY VOLUME, WET 1.83 3.00 3.18 '1.86 3.57 3.85
) LB. C02 PER LB. OF FUEL 3.10 3.11 3.1Z 3.1* 3.15 3.15
HEIGHT FLON, LB./HR. 335.5 35*. b 389.7 839.1 1103.3 13*7.5
CARBON MONOXIDE
PPM BY VOLUME, NET 23*.7 308. 7 198.* 66.1 3Z.9 38.0
LB. PER 1000 LB. OF FUEL Z5.3S3 Z0.65* 18.06* 7.136 3.566 1.970
HEIGHT FLOH, LB./HR. 2.663 Z.355 3.358 1.876 .898 .780
UNBURNEO HYDROCARBONS- PPM AS CARBON, HEIGHTS AS CHs
PPM BY VOLUME, HET 63.5 69.6 5*.0 1*.7 6.9 6.0
LB. PER 1000 LB. OF FUEL 5.093 3.936 3.810 .90* .306 .Z*2
> HEIGHT FLOH, LB./HR. .535 .-.*9 .351 .339 .108 .096
RATIO LB MC/LB CO .3009 .1907 .1556 .1Z7Z .1Z01 .12Z7
NITRIC OXIDE (NO) - HEIGHTS AS N02
1 PPM BY VOLUME, HET 15.1 17.0 Z3.6 **.7 79.0 91.0
LB. PER 1000 LB. OF FUEL Z.679 3.76* 3.529 7.697 10.136 10.53*
HEIGHT FLOH, LB./HR. .281 .315 .**! 2.085 3.5*8 *.171
NITROGEN DIOXIDE 4N02I
PPM BY VOLUME. HET *.6 7.1 *.Z 1Z.3 7.1 6.S
LB. PER 1000 LB. OF FUEL .816 1.15* .624 2.173 .911 .723
) HEIGHT FLOW, LB./HR. .066 .133 .079 .57* .319 .286
TOTAL OXIDES OF NITROGEN (NC+NOZI AS NOZ
PPM BY VOLUME, HET 19.7 2*.l 27.8 57.0 86.1 97.Z~
IB. PER 1800 LB. OF FUEL 3.*95 3.919 *.1S7 10.070 11.0*9 11.257
HEIGHT FLOH, LB./HR. .367 .**7 . SZO 3.658 3.867 *.*58
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLCH .00735 .00720 .00719 .60716 .00716 .0071*
S.10KE NUMBER 3.50 2.*0 *.70 *.70 5.90 *.70
CORRECTED HEIGHT FLOH .0317* .OZ161 .OZ157 .OZ1*7 .031*7 .031*3
) SMOKE NUMBER 5.90 5.90 *.70 10.60 16.50 1*.10
CORRECTED HEIGHT FLOH .03623 .0360Z .03589 .0357Z .03578 .03571
SMOKE NUMBER 7.10 5.90 5.90 l*.lfl Z1.30 20.00
) CORRECTED HEIGHT FLOM .05062 .050*3 .05035 .05010 .05000 .0*999
SMOKE NUMBER 9.*0 9.*0 8.30 18.80 27.10 25.90
SMOKE NUMBER AT HJU0.023 6.*fl 5.90 5.90 12.10 17.70 16.20
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE MET VALUES.
2. EQUIVALENCE RATIO CALCULATED FROM COZ.CO.ANO HC DATA AND FUEL COMPOSITION.
3. MASS EMISSIONS OF MO, NOZ, AND MO»NOZ CALCULATED AS NOZ FROM CONCENTRATIONS KITH MOL
J

AV. KEW. TEST NO.* 1
*9.00 SPEC HUM' .001000
1*.160 SL TIM.S* 6.5000
1*
100.3
708. Z
653.
1.1760.
17.
155.
639.
1*01.
6.09
.01**
*2«.« . . 	
.01*6
.21*
.066
99.9*8
3.07 ~ -. ' ~
3.15
13Z3.S 	 	 	
21.1
1.375. 	 	 	 	
.577
6.8 	 ... 	
.22*
.09*
.16Z9 	 , 	 	 ..
101.5
10.886. ._
*.572
8.0 	 . . ...
.656
.360
109.5~ ~.
11.7**
*.93Z 	 	
.00713
5.98. 	 . . . _ 	 __ . ..
.02139
1*.10
.0356*
16.80
.0499*
2Z.*«-; _ .... 	 	 	 •_
15. *0
ECULAR HEIGHT OF NOZ 1*6. 111.
                                                                                                                                                                                                   !C



                                                                                                                                                                                                   -'l





                                                                                                                                                                                                   *>
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                    *.....,...,*..,......,...„,....,.,..„......  »IR£SEARCH EMISSION TEST  SUMMARY   ••••••••••»•••
                    ENG MFC « AIRESEARCH      .      TEST FACIi. I PHX LACU2  INSTR DtSCRIP  I FED REG V38 N136
                    MODEL N0.«     TPE331-5-2S1M      S/NI   P04001              ENilNE TYPEICLASS) I   TURBOPROP
                    RATED POttERI     706.0  SHP AT  SEA LEVEL STANDARD DAY CONDITIONS
                    FUELI ASTM 01655-73             ATONIC H/C RATIO!   1.928     LHV» 18470. BTU/LB      ADDITIVESI
                                                                                                                      NONE
                                                                                                       CALC DATE 111-6-75
                                                                                                       CALC 101    3
                                                                                                      TEST NOI    1
........ EXHAUST EMISSIONS  PER  EPA CYCLE OF WORK OUTPUT »• CODE OF FEDERAL  REGULATIONS  TITLE 40 PART 87  17 JULT 1973
                    HYDROCARBONS  (CM AS CHI,)          4.053 LB. POLLUTANT PiR  1000  HP.-HR.  PER CYCLE
                    CARBON  MONOXIDE 
,-~* *w*.i. *».ii*r.w. ...w rt.:\i,c.ni KMitu iMivturr ruw=.K Al O3. KtKlbNI KAIfcD TAKtUrr Ml KPM
COMB TYPE! REVERSE FLOW ANNULAR P/NI 8690S2-4 SUR/VOLI 1.260 FUEL
ENGINE TOTAL SERVICE! 0.0 HR TIME SINCE ENGINE OVERHAULl 0.0 HR
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
AIRCRAFT INSTALLATION •»•• MFR.I MODEL NO.»
USER! ENGINE INSTALLATION POSITION!
INJ TYPE!
STAGED SIMPLEX
GASEOUS EMISSION TEST NO. 1 1 DATE! 11-6-75 TIME! BARO PRESS. I 28.780 IN. HGA.
AMBIENT AIR TEMP.! 19.00 OEG. F RELATIVE HUMIDITY! 1.9.00 PERCENT SPECIFIC HUMIDITY! .001000 LB. H20/LB. DRY AIR
AMBIENT AIR QUALITY HYDROCARBONS (HC)« 0.0 PPMC CAR30N MONOXIDE ICO) 1 0.0 PPMV OXIDES OF NITROGEN INOX) 1 0.0 PPHV
SAMPLE LINE ••• TEMP.! 300.00 OEG. F. FLOHRATEI 14.16 LITERS/HIM. TRANSPORT TIME! 6.50 SEC. LENGTH! 50.00 FT.
TEST CONDITION
ACTUAL POMER SETTING, HORSEPOWER
CORR. POMER SETTING ISTO OAY> , PERCENT RATED
Nl SPEED, RPM
FUEL FLCH IHEAS.I LB./HR.
CCRR. ENGINE CORE AIRFLOW (MEAS), LB/SEC
COMPRESSOR INLET AIR TOTAL TENP., OEG F
COMPRESSOR INLET AIR TOTAt PRESS. , PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS.. PSIA
COMPRESSOR DISCHARGE AIR TOTAL TEMP., DEG F
TURBINE INTERSTAGE GAS TOTAL TEMP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION, NET ANALYSIS
HYDROCARBON IHC AS CH4I , PPMC
CARBON MONOXIDE (CO) , PPMV
TOTAL OXIDES OF NITROGEN INOX), PPMV
CARBON DIOXIDE 
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(£1
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*»•»»••••»»••»»•»»»••»••»••••»»»»»»•»•»»•»  EPA CVC4.E EMISSIONS COMPUTATION SUMMARY  •••••»»»»«
ENG HFG t AIRESEARCM            TEST  FACIL I  PHX LACC2  INSTR OESCRIP I FED REG ¥38 N136
MODEL NO.I     TPE331-5-Z51N      S/NI    P04001              iNGINE TYP£(CLASS)t  TURBOPROP
RATED POWERI    706.9 SHP AT  SEA  i£V£L  STANDARD DAY CONDITIONS
FUE_« ASTM 01655-73             ATOMIC H/C *ATIOI   1.9Z8     LHV« 18»70. BTU/iB     AOOITIVESI
                                                                                                                        HOME
                                                                                                                             C*LC DATE tll-6-75
                                                                                                                             CALC ID*    3
                                                                                                                            TEST NOI    1
MODE
TIME IN MODE, MINUTES
RATED POWER, PERCENT
CORRECTED POWER, HORSEPOWER
HP-HR
FUEL FLCW, LB/HR
FUEL HASS, LB
*• HYDROCARBON EMISSION (HCI **
INDEX, LB HC/1088 LB FUEL
RATE, Lfi HC/HR
MASS. LB HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE. LB HC/1000 HORSEPOWER-HR PER CYCLE
** CARBON HONOXIOE EMISSIONS (COt *•
INDEX, LB CO/1000 LB FUEL
RATE, LB CO/HR
HASS, LB CO
HASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1008 HORSEPOWER-HR PER CYCLE
** TOTAL OXIDES OF NITROGEN EMISSIONS (NOX) »•
INDEX, LB NOX/1000 LB FUEL
RATE, LB NOX/HR
KASS, LB NOX
HASS, PEP.CENT OF TOTAL CYCLE
CrC.E, LB NOX/1000 HORSEPOWER-HR PER CYCLE
T«XI-IOi.£
(INI
7.000
5.000
35.300
4.116
106.367
1Z.409

5.217
.555
.065
25.1


23.641
2.519
.294
23.6


3.591
.382
.345
7.9

TAXI-IOLE
(OUT)
19.000
5.000
3S.300
11.178
106.367
33.683

5.217
.555
.176
68.2


23.681
2.519
.798
64.2


3.591
.382
.121
21.3

APPROACH
4.500
30.000
211.800
15.665
259.936
19.495

.631
.164
.012



0.414
1.667
.125
10.1


9.299
2.417
.181
32. a

CLINBOUT
Z.500
90.000
635.400
26.475
397.765
16.574

.241
.096
.004
1.6


1.354
.539 .
.022
1.8


10.953
4.357
.182
32. •

TAKEOFF 1
.500
loa.ooi
706.000
5.863
410.110
3.416

.219
.090
.001
.3


1.264
.518
.004
.3


11.286
4.629
.039
6.8

roTAL PER
CYCLE
33.500


63.540

85.579

3.009
.461
.258
100.1
4.053

14.528
2.227
1.243
100.8
19.567

6.624)
1.015
.567
100.0
6.92Z
                                             ••  EMISSION INDEX BEVELS REWIRED TO MEET EPA 1979 STANDARDS FOR CLASS  P2  ENGINES ••
                                         EPA  LTO-CrCLE
                                  POLLUTANT   LBP/1000  HORSEPOMER-HR-CYCLE
                                     CO              26.6
                                     HC              4.9
                                     NOX             12.9
                                                                                                  REQUIRED EMISSION  INDEX,  LBP/1000 LB FUEL

POLLUTANT (MODE)
CO (IOLE)
HC (ID..E)
NOX (TAKEOFF)

A '
23.7
5.2
11.3

B
33.7
6.4 	
24.2
                                            A  ASSUMES PROPORTIONAL  REDUCTION OF PO-.CTANT EMISSION INDEX AT EACH LTO CYCiE NODE

                                            6  ASSUMES (II RECcJIREO  REDUCTION IN CO  AND  HC OBTAINED 3Y LOWERING EMISSION INDEX VALUES
                                               AT TAXI-IOLE N00£ ONLY, CO  AND HC EMISSIONS AT OTHER MODES RiNAIN UNCHANGED. (Z) REQUIRED
                                               REDUCTION IN NOX OBTAINED BY LOWERING EMISSION INDEX VALUES AT CLIMdOUT AND, TAKEOFF MOOES IN
                                               SAME PROPORTION AS MEASURED VALUES. NOX EMISSIONS  AT TAXI-ID..E AND APPROACH NODES
                                               REMAIN UNCHANGED
                                                                                                                                                                   .CJ
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 01
ua
 CD
ENGINE^ TPE331-5-251M S/N» P04001
RAT SHF* 706. RA EGT.F* 1650.
' FUEL H/C« 1.9280 STOI F/A* .06822
DATA POINT NUMBER 15
PERCENT MAX. CORRECTED POHER 5.4
CORRECTED SHAFT HP 37.9
MEASURED SHAFT HP 35.0
SHAFT SPEED, Nl, RPM 27540.0
COMPRESSOR INLET TEMP..OEG.F 17.0
COMPRESSOR OSCHG. PRES..PSIA 50.9
' COMPRESSOR OSCHG. TEMP.OEG F 298.0
TURB INTERSTAGE TEMP., DEG.F 795.0
COR'* BELMTM FLOH, LB/SEC 3.06
FA RATIO BASED ON BELLNTH. .0097
MEASURED FUEL FLOH, LB/HR 107.0
FA RATIO CALC. FROM EMISSION .0090
) EQUIVALENCE RATIO .131
LOADING H/P»*N/V/E«T/540> .330
COMB EFFIC FROM EMISSIONS 99.D18
CARBON DIOXIDE
PERCENT BY VOLUME. HET 1.84
) L0. C02 PER LB. OF FUEL 3.10
HEIGHT FLOH, LB./HR. 332.1
CARBON MONOXIDE
' PPM BY VOLUME, HET 217.1
LB. PER 1100 LB. OF FUEL 23.247
' HEIGHT FLOH, LB./HR. Z.487
COMB P/N= 869082-4 FUEL= AV. KERO. TEST NO.- 1
RAT SPO* 41730.
L H V
16
7.7
54.2
50.0
27530.0
17.0
51.2
300.0
857.0
2.98
.0105
113.0
.0097
.142
.318
99.204
= 1S470.
17
10.3
72.4
66.7
27650.0
17.0
51.7
302.0
916.0
2.93
.0117
124.0
.0104
.153
.305
OEM PT,F« 8. REk HUM
S LN T.F
18
30.0
211.9
196.0
41750.0
20.0
140.5
627.0
1067.0
7.99
.0090
260.0
.0091
.134
.079
99.368 99.794

2.00
•3.11
351.7

206.3
20.431
2.309
UNBURtlED HYDROCARBONS- PPM AS CARBON, HEIGHTS AS
PPH BY VOLUME, HET 81.0
L3. PER 1000 LB. OF FUEL 4.958
) HEIGHT FLOH, LB./HR. .530
RATIO LB HC/LB CO .2132
NITRIC OXIDE (NO) - HEIGHTS AS N02
) PPM BY VOLUME, HET 14.0
1.8. PER 1000 LB. OF FUEL 2.462
HEIGHT FLOH, LB./HR. .263
) NITROGEN DIOXIDE (N02I
PPM BY VOLUME, HET 6.4
L3. PER 1000 LB. OF FUEL 1.126
) HEIGHT FLOH, 4.B./HR. .120
TOTAL OXIDES OF NITROGEN INC«N02) AS N02
PPM BY VOLUME, HET 20.4
) L9. PER 1000 LB. OF FUEL 3.588
HEIGHT FLOH. LB./HR. .384
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOH .00710
SMOKE NUMBER 3.50
CORRECTED HEIGHT FLOH .02130
> SHOKE NUMBER 4.70
CORRECTED HEIGHT FLCH .03549
SHOKE NUMBER 8.20
) CORRECTED HEIGHT FLOH .04969
SHOKE NUMBER 8.20
SMOKE NUMBER AT HA*0.023 6.20
) NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE
2. EQUIVALENCE RATIO CALCULATED FROM
63.6
3.601
.407
.1762

18.0
2.928
.331

4.6
.748
.085

22.6
3.676
.415

.00708
1.20
.02125
3.50
.03542
4.70
.04959
8.20
4.50
2.17
3.12
366.9

168.3
17.266
2.141
CH4
49.2
2.579
.320
.1494

22.2
3.344
.415

4.5
.678
.084

26.7
4.022
.499

.00707
2.40
.02121
3.50
.03535
4.70
.04949
5.90
4.10
1.90
3.14
817.0

61.0
6.412
1.667

10.5
.630
.164
.0983

43.8
7.558
1.965

13. 1
1.743
.453

53.9
9.301
2.418

.00706
3.50
.02119
8.20
.03532
12.90
.04945
17.60
10.70
= 300.0 FLO.L/M
19 20
69.7 90.1
492.3 636.0
454.9 587.1
41780.0 41740.0
19.0 18.0
149.3 153.5
634.0 637.0
1253.0 1332.0
8.00 7.95
.0121 .0139
348.0 398.0
.0122 .0137
.179 .201
.070 .066
99.927 99.947

2.57 2.88
3.15 3.15
1096.2 1254.2

26.7 19.4
2.089 1.355
.727 .539

6.0. . 6.0
.268 .239
.093 .095
.1283 .1764

78.0 91.7
10.012 10.501
3.484 4.179

7.6 4.0
.976 .458
.339 .182

85.6 95.7
10.988 10.959
3.824 4.362

.00705 .00704
3.50 4.70
.02116 .02111
16.50 12.90
.03526 .03519
21.20 18.80
.04936 .04926
27.10 23.50
17.30 15.20
* 49.00 SPEC HUH' .101101
- 14.160 SL TIM,S« 6.5000
zi 	 "
100.1
. . 706.5 . . . '
651.5
41740.

155.
639.
1400.
7.89
.014%
410.1
.0147
.216
.06%
99.951

3.10
3.15
1292,1. .._...... . _

19.%
1.260
.517

6.0
.222
.091
.176%

98.8 ',
.10.512 _ . ... . ..... . .
4.310

7.3
.772
.316 ;

106.0
11.28%
4.626

.00704
4.70 	 ,
.02111 '
14.10
•113518. 	 	 ._._ ...... 	 ,.
10.10 ,
.04925 ,
23.50
15. SO
HET VALUES.
C02.CO.
AND HC OAT«
3. MASS EMISSIONS OF NO, N02, AND NO+N02 CALCULATED AS
AND FUEL
N02 FROM
COMPOSITION.
CONCENTRATIONS HITH
t
MOLECULAR HEIGHT OF N02 (46.011. i
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13
0)
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                    cur »rr . .»»P... """•»••***»*»•»•••*«••  AIRESEARCH EMISSION TEST  SUMKARY   •»•»•»••••••»•

                    «nn T Sn ,     rf CH            TEST F*CIt ' PHX L*CCZ  IMSTR OESCRIP  I FED  RES V3»  N136
                    NOOtL NO. <     TPE331-S-251H      S/NI    P8*001              ENGINE TYPEICLASS1I   ruRSOPBOP
                    RATED POWER.    706.0  SHP  AT  SEA  LEVEL  STANDARD DAY CONDITIONS     TYPt«CLASS)l   TURBOPROP

                    FUELI ASTM 01655-73             ATONIS H/C RATIO!   1.928     LHV1 18470. BTU/Lfl      ADDITIVES!
                                                                                                                      NONE
                                                               CALC DATE 111-6-75
                                                               CALC ID!    1
                                                              TEST NOt     2
                                       b
                    ........ EXHAUST EMISSIONS  PER EPA  CfCLE OF WORK OUTPUT *• CODE OF FEDERAL REGULATIONS  TITLE 40  PART 87  17 JULY 1973
                                        HYDROCARBON*  (CH AS CHfcl           5.228 LB. POLLUTANT PER  1008  HP.-HR.  PER CYCLE
                                        CARBON  MONOXIDE (COI             19.695 LB. POLLUTANT PER  1000  HP.-HR.  PER CYCLE    ~             ~
                                        OXIDES  OF  NITROGEN  (NOX AS N02)    8.976 LB. POLLUTANT PER  1000  HP.-HR.  PER CYCLE

                    T... rn r «- ,       SMOKE                              H..7  SMOKE NUMBER, MAXIMUM AT  CRUISE
                    TAXI-IDLE SETTINGI  5.0      PERCENT RATED TAKEOFF POWER AT 65.
                                                                                         PERCENT RATED TAK-OFF  Nl  RPM
                                                          MODE,  78 PERCENT RATED POWER
                    COMB TYPE I REVERSE FLOW ANNULAR
                    ENGINE TOTAL SERVICE!  0.0        HR
                    ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
............  £NGINE DESCRIPTION  .».».»»».»»...»..»..»....

   P/NI   869082-4            SUR/VOLI  1.260   FUEL INJ TYPEt
TIME SINCE ENGINE OVERHAUL!   8.0        HR
STAGED SIMPLEX
1 AIRCRAFT INSTALLATION *»»» NFR. «
MODEL NO.!
ENGINE INSTA.LATION POSITION.
GASEOUS EMISSION TEST NO. t 2 DATE! 11-6-75 TIME! BARO PRESS 1 2g 760 TV MCI
AMBIENT AIR TEMP.. 19.88 OEG. F RELATIVE HUMIOITY. 100.00 PERCENT SPECIFIC HUMIDITY! .002080 LB HZO/"" DRY AIR
AMBItNT AIR QUALITY HYDROCARBONS (HO 1 0.0 PPMC CARBON MONOXIDE ICO) 1 0.0 PPMV OXIDES OF NITROGEN (NOXI 1 0.0 PPMV
SANPLE LINE *•• TEMP.l 300.00 OEG. F. FLOWRATEI K..16 ..ITERS/MIN. TRANSPORT TIME! 6.58 SEC. LENGTHI 58.80 FT.
) TEST CONDITION
ACTUAL POWER SETTING, HORSEPOWER
CORR. POWER SETTING (STO OAYI , PERCENT RATED
1 Nl SPEED, RPM
FUEL FLCH (MEAS.I LB./HR.
: CORR. ENGINE CORE AIRFLOW (MEASI, LB/SEC
) COMPRESSOR INLET AIR TOTAL TEMP. , OEG F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
i COMPRESSOR DISCHARGE AIR TOTA. PRESS., PSIA
) COMPRESSOR DISCHARGE AIR TOTA. TEMP., DEC F
i TURBINE INTERSTAGE GAS TOTAL TEMP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
> EMISSION CONCENTRATION, WET ANALYSIS
HYDROCARBON (HC AS CH4), PPNC
CARBON MONOXIDE (COI, PFMV
' TOTAL OXIDES OF NITROGEN (NOX), PPNV
CARBON DIOXIDE (C02I , PERCENT BY VOL.
NITRIC OXIDE (NO), PPNV
EMISSION INDEX, LB. POLLUTANT/1880 LB. FUEL
HYDROCARBONS (HC AS CH«.)
CARBON MONOXIDE (COI
i TOTAL OXIDES OF NITROGEN (NOX AS N02)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4)
) CARBON MONOXIDE (CO)
TCTAL OXIDES OF NITROGEN (NOX AS N02)
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS!
> F/A (EMISSIONS, CALC)

33.6
5.15
37530.00
106.8
3.1
20.88
58.69
380.00
608.0
14.12
106.500
223.264
H..30H
1.854
13.900
23^752
3.722
.666
2.516
.395
96.87
.0098
49.4
7.58
27520.00
108.0
3.0
19.00
14.13
51.08
296.00
678.0
14.11
60.008
283.528
23.100
Z.047
18.000
3.321
19.707
3.67li
.359
2.128
.397
99.25
.0099
65.9
10.11
27520.00
121.0
3.0
19.80
14.13
51.57
308.80
927.8
14.11
57.000
201.660
27.100
2.238
21.880
2.869
17.683
3.948
.358
2.164
.478
99.33
.8186

194.2
29.83
1.1700.80
256.0
6.8
16.80
14.13
140.72
619.80
1066.0
13.97
12.300
65.235
53.000
1.931
40.988
.. .728
6.754
9.814
.186
1.729
2.388
99.78
.0893

457.0
69.96
41740.00
31.6.0
21.00
14.13
147.94
633.00
1260.0
13.99
6.300
27.953
84.500
2.602
7i>. 750
.277
2.153
18.693
.896
.745
3.780
99.93
.0124

561.8
66.84
41768.80
398.6 .
22.88
- 14.13
152.81
638.80
-1J57.0 .
14.03
6.048
15.621
97.251
2.867
.248
1.107
11.175
.094
.432
4.356
99.95
.8136

26
644.3 	 	
9 A. 94
41770.00
421.8
16.80
14.13 	
154.72
637.80
.. 1395.0
14.05
9.300.
15.420
in. 000
. 3.4131
96.250
_. . .352
1.020
11.303
.146
.430
4.759 	 _
99.95
.0144
                                                                                                                                                                -CU
-------
(D
(Ti
CO
EKC-MEG t A1RESEAKCH TEST FAClL I PHX LACC2 INSTR OESCRIP 1 FED REG V38 N136
MODEL NO.I TPE331-5-Z51M S/Nt P0*'001
ENGINE
TTPEICLfSSIt • TURBOPROP
RATED PCWERI 706.0 SHP AT SEA LEVEL STANDARD DAY CONDITIONS
FUE..1 ASTM 01655-73 ATOMIC H/C RATIO! 1.928 LHVI
H 0 0 E TAXI-ID-E
>
TIME IN NODE, MINUTES
RATED POWER, PERCENT
CORRECTED POWER, HORSEPOWER
HP-HR
' FUEL FLOW, LB/HR
FUEL MASS, LB
" HYDROCARBON EMISSION (HO »•
INDEX, LB HC/1000 LB FUEL
RATE. LB HC/HR
MASS, LB HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORSEPOHER-HR PER CYCLE
)
•• CARBON MONOXIDE EMISSIONS (CO) ••
INDEX, LB CO/1000 LB FUEL
RATE, LB CO/HR
MASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCi.E. LB CO/1000 HORSEPOHER-HR PER CYCLE
*• TOTAL OXIDES OF NITROGEN EMISSIONS (NOX) **
INDEX. LB NOX/1000 LB FUEL
RATE, LB NOX/HR
MASS, LB NOX
) MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB NOX/1000 HORSEPOHER-HR PER CYCLE
*• EMISSION INDEX LEVELS REQUIRED
EPA CTO-CYCLE
POLLUTANT LBP/1000 HORSEPOHER-HR-CYCLE
J CO 26.8
HC *.9
NOX 12.9
)
A ASSUMES PROPORTIONAL REDUCTION
6 ASSUMES (11 REQUIRED REDUCTION
(INI
7.000
5.090
35.300
4.118
106.308
1Z.*03

6.78*
.721
.08*
Z5.3



Z*.093
2.561
.299
23.9


3.735
.397
.0*6
8.1

CALC
CM.C
DATE 111-6-75
U>* . 1

TEST NOI 2
18*70. BTU/LB ADDITIVES! NONE
TAX I -IDLE APPROACH
(OUT)
19.000 *.500
5.000 30.000
35.300 211. 800
11.178 15.885
106.308 Z56.**3
33.66* 19.233

6.78* .615 •
.721 .158
.228 .012
68.7 3.6



2*. 093 6.569^ ~
2.561 1.68*
.811 .126
6*. 8 10.1


3.735 9.065
.397 2.325
.126 .17*
22.0 30.6

TO McET EPA 1979 STANDARDS FOR CLASS




REQUIRED EMISSION
POLLUTANT (MODEI
CO HOLE)
MC HOLE)
NOX (TAKEOFF)
CLINBOUT

2.500
90.000
635. *00
26.*75
369.973
16.2*9

.208
.081
.003
1.0



.*35
.170
.007
.6


11.333
*.*19
.18*
3Z.3


PZ ENGINES ••

TAKEOFF

.500
100.001
706.001
5.183
1.31.68*
3.597

l.Z*2
.536
.01*
... 1.3



2.266
.978
.008
.7


11.0*7
*.769
.0*0
7.1




TOTAL PER
CYCLE
33.500


63.5*0. " ~:

85.1*6

3.912
.595
.332
100.0
5.220


1*.697
2.2*1
1.251
100.0
19.695

6.698
1.021
.570
100.0
0.976


INDEX, LBP/1000 LB FUEL .

A
2*.l

11. if


33.
6.
23.

a
9
3 . 	 . 	
*
OF POLLUTANT EMISSION INDEX AT EACH LTO CYCLE NODE 	 "
IN CO AND HC OBTAINED BY LOWERING EMISSION INDEX VALUES . __ ' 	
                                               AT TAXI-IOLs MODE ON'.Y, CO AND HC  EMISSIONS AT OTHER MODES REMAIN UNCHANGED. (21 REQUIRED
                                               REDUCTION IN NOX OBTAINED BY LOWERING  EMISSION INOi.X VALUES AT CLIM3CUT AND TAKEOFF NODES  IN
                                               SAME PROPORTION AS MEASURED VALUES,  NOX  EMISSIONS AT TAXI-IDLE AND APPROACH MODES
                                               REMAIN UNCHANGED
-------
 (U
vQ
 ro
>

ENGINE- TPE331-5-251M S/N> P04001 COMB P/N* 869082-4
RAT SHP= 706. RA EGT,F= 1650. RAT SPB= 41730. 0£H PT,F= 19.
FUEL H/C= 1.9280 STOI F/A= .06822 L H ^ 18470. S LN T.F* 300.0
DATA POINT NUMBER 22 23 24 25 26
' PERCENT MAX. CORRECTED POHER 5.2 7.6 10.1 29.8 70.0
CORRECTED SHAFT HP 36.4 53.5 71.4 210.6 493^
MEASURED SHAFT HP 33.6 49.4 65.9
SHAFT SPEED, Nl, RPM 27530.0 27520.0 27520.0
COMPRESSOR INLET TEMP. , OEG.F 20.0 19.0 19.0
COMPRESSOR OSCHG. FRES..PSIA 50.7 51.1 51.6
> COMPRESSOR OSCHG. TEMP.CEG F 300.0 298.0 300.0
TUR3 INTERSTAGE TEMP., OEG.F 808.0 474.0 9*7.0
CORR BELNTH FLON, LB/SEC 3.09 2.98 2.98
' FA RATIO BASED ON BELLMTH. .0095 .0101 .0113
MEASURED FUEL FLOH, LB/HR 106.0 108.0 121.0
FA RATIO CALC. FROM EMISSION .0090 .0099 .0108
1 EQUIVALENCE RATIO .132 .145 .158
LOADING H/P»»N/V/EIT/540) .333 .318 .312
COM3 EFFIC FROM EMISSIONS 9S.873 39.245 99.326
CARBON DIOXIDE
PcRCENT BY VOLUME. HET 1.85 Z.05 2.24
> LB. C02 PER LB. OF FUEL 3.10 3.11 3.12
HEIGHT FLOH, LB./HR. 328.5 336.3 377.3
CARSON MONOXIDE
) PPP BY VOLUME, HET 223.3 - 203.5 201.7
LB. PER 1000 LB. OF FUEL 23.752 19.707 17.883
HEIGHT FLOH, LB./HR. 2.518 2.128 2.164
) UNBJKNfO HYDROCARBONS- PPM AS CARBCN, HEIGHTS AS CH4
PPK BY VOLUME, NET 106.5 60.0 57.0
LB. PER 1000 LB. OF FUEL 6.476 3.321 2.889
) HEIGHT FLOH, LB./HR. .686 .359 .350
RATIO LB HC/LB CO .2727 .1685 .1616
NITRIC OXIDE (NOI - HEIGHTS AS N02
) PPM 91 VOLUME. MET 13.9 18.0 21.8
LB. PER 1000 LB. OF FUEL 2.429 2.863 3.176
HEIGHT FLOH, LB./HR. .257 .309 .384
) NITROGEN DIOXIDE IN02I
PPM BY VOLUME, HET 7.4 5.1 5.3
L3. PER 1000 LB. OF FUEL 1.Z93 .811 .772
) HEIGHT FLOH, LB./HR. .137 .088 .093
TOTAL OXIDES OF NITROGEN 
h

)

>

*

^
*



1.93 2.60
3.14 3.15
804.2 1049.9

65.2 28.0
6.754 2.153
1.729 .745

12.3 6.3
.728 .277
.186 .096
.1078 .1288

40.9 74.7
6.956 9.459
1.781 3.273

12.1 9.8
2.058 1.234
.527 .1,27

53.0 84.5
9.014 10.693
2.308 3.780

.00710 .00707
1.20 3.60
.02130 .02122
8.30 11.90
.03557 .03537
10.70 17.90
.04980 .0*962
15.50 25.00
9.00 14.70

2.87
3.15
1229.1

15.8
1.107
.432

6.0
.240
.094
.2168

90.0
,10.342
4.033

7.3
.833
.325

97. if
11.175
4.358

.00701
3.60
.02103
10.70
-.03511
17.90
.04924
21.41
13.60

3.03 -
3.15
1326.8

15.4
1.020
- —•-*•• ._ _ ... — ... _ .. — — 	
.430

9 3
.352 ~
.148
.3447
— .*^^F_ — 	 . 	 	 	 	 	 	
96.3
10.461
4.404

7.7
• * ' - - - 	 	 . . ... .
.842
.355

jgfc'g
11.303
4.759

.00695
3.60. 	
.02084
10.70
.03473.
16.70
.04853
19.00
— *• <*1* - — - • - — 	 - .- 	 	 _.—.._ 	
iz.ao

2. EQUIVALENCE RATIO CALCULATED FROM C02.CO.ANO HC DATA AMD FOB. COMPOSITION.
3. MASS EMISSIONS OF NO, NOZ..AMO NO»NOZ CALCULATED AS



- - . ,





	

.
_ 	
)-
.


.

* •
} i
\
)'~
•
	 — :
. :


)"


^
•*
--— —


H02 FROM CONCENTRATIONS HITH MOLECULAR NEIGHT OF N02 146.011. " — ..
-------
                     .............................................  »IRESEARCH EMISSION  TEST  SUMMARY   ••..•.•....»»»
                     ENG «P« » «r«SCT«tl»-          TES* FACIk. I -PH* 4.ACC2 .INSTR DESC8IP _t_E£D. REG  V38 N136
                     HODEL NO.I     TPE331-5-ZS1H      S/NI   P04001              cNGINE  TYPE«CLASS)I   TURBOPROP
                     RATED POWER!    706.0  SMP AT  SEA LEVEL STANDARD DAT CONDITIONS
                     FUELI ASTM 01655-73             ATONIC H/C RATIOI   1.928     LMVi 18470. 8TU/LB     ADDITIVES I
                                                                                                                       NONE
 CALC DATE Hl-7-75
' CALC IDt ~ t
TEST NOI    Z
                     ........ EXHAUST EMISSIONS  PER  £PA CYCLE OF WORK OUTPUT •• CODE  OF  FEDERAL REGULATIONS TITLE 0 IN. HtA.
                     AMBIENT AIR TEMP.I  19.00 DEG. F         RELATIVE HUMIDITY! 100.00 PERCENT        SPECIFIC HUMIDITY!  .002000 LB. HZO/LB. DRY AIR
                     AMBIENT AIR QUALITY    HYDROCARBONS  (HC11  0.0    PPMC     CARBON MONOXIDE  (CO)l  0.0   PPMV    OXIDES OF NITROGEN INOX)! 0.0   PPH»
                     SAMPLE LINE ••• TEMP.J  300.00 DEG.  F.      FLOHRATEI   H..16 LlTERS/MIN.      TRANSPORT  TIMEI    6.SO SEC.     LENGTHI   50.01 FT.
TEST CONDITION
ACTUAL FOHEfc SETTING, HORSEPOWER
CORR. POKER SETTING ISTD DAYI , PERCENT RATED
Nl SPEED, RPH
FUEL FLCM (HEAS.I LB./HR.
CORR. ENGINE CORE AIRFLCM (MEAS) , LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., DEC F
COMPRESSOR INLET AIR TOTAL PftdSS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL TEMP., OEG F
TURBINE INTERSTASE GAS TOTAL TEMP., OEG F
EXHAUST GAS STATIC PRESSURE. PSIA
EMISSION CONCENTRATION, MET ANALYSIS
HYDROCARBON IHC AS CH4I , PPMC
CARBON MONOXIDE (COI , PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPMV
CARBON DIOXIDE (CO?), PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CM*)
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS HOZI
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS IHC AS CHO)
CARSON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN INOX AS N02)
CON3USTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS. CALC)
29 30 31
33.2
5.07
2756(1. 00
103.0
3.0
19.00
l
-------
 tu
iQ
 (D
• )
ENG MFG « A1RESEARCH TEST FACIL 1 PHX
MODEL NO.: TPE331-5-Z51M S/NI P04001
RATED POHERI 706.0 SHf> AT SEA LEVEL STANDARD
FUELI ASTM D165S-73 ATOMIC H/C RATIO
MODE
TIME IN MODE, MINUTES
' RATED POWER, PERCENT
CORRECTED POWER, HORSEPOWER
HP— HR
"> FUEL FLCH, LB/HR
FUEL NASS, LB
i } •• HYDROCARBON EMISSION (HC) »*
INDEX, LB HC/1000 LB FUEL
RATE, LB HC/HR
1 NASS, LC HC
KASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORSEPOWER-HR PER CYCLE
)
•» CARBON MONOXIDE EMISSIONS (CO) ••
INDEX, LB CO/1010 LB FUEL
1 RATE. LB CO/MR
MASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE. LB CO/1000 HORSEPOWER-HR PER CYCLE

— TOTAL OXIDES OF NITROGEN EMISSIONS (NOX) ••
INDEX, LB NOX/1000 LB FUEL
RATE, LB NOX/HR
MASS, LB NOX
) MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB NOX/1000 HORSEPOHER-HR PER CYCLE




LACC2 INSTR DESCRIP 1 FED REG V38 N136 CALC
ENGINE TYPE (CLASS! 1 TURBOPROP CALC
DAY CONDITIONS TEST ,
1 1.928 LHVt 18470. BTU/LB ADDITIVES! NONE
TAXI-IDLE
(IN)
7.000
5.000
35.300
4.118
102.533
11.96Z

4.052
.415
. 0-.8
24.3


23.887
2.449
.286
23. 7



3.786
.388
.045
8.0
TAXI-IOLE
(OUT)
19.000
5.000
35.300
11.178
102.533
32.469

4.052
.415
.132
65.8


23.887
1 776
•


3.786
.388
.123
21.7
APPROACH
4.500
30.000
211.800
15.885
260.591
19.544

.635
.166
.012
6.2


5.937
1.547
.116
9.6

- 	
9.267
2.415
.181
31.9
CI.IMBOUT
2.500
90.000
635.400
26.475
400.567
16.690

.332
.133
.006
2.8


1.330
.533
.022
1.8

	
10.723
4.295
.179
31.6


DATE Jll-7-75
(01 2
TAKEOFF
.500
100.000
706.000
5.883
424.620
3.539

.522
.221
.002
.9


1.167
.496
.004
.3


10.931
4.642
.039
6.8
TOTAL PER
33.500
63.540
84,204

2.373
.358
.201
. 100.8
3.145

14.295
2.156
1.204
100.*
18.944
. --
6.733
1.015
.567
loo. i

                                             "  EMISSION  INDEX  LEVELS  REQUIRED TO HEET EPA 1979 STANDARDS FOR CLASS P2 ENGINES ••
                                          EPA  LTO-CYCLE
                                  POLLUTANT   LBP/1000 HORSEPOWER-HR-CYCLE
                                     CO             26.8
                                     HC              4.9
                                     NOX            12.9
                                                                                                 REQUIRED EMISSION INDEX,  LBP/1000  LB FUEL
POLLUTANT (MODE)
   CO (IDLE)
   HC (IDLE)
   NOX (TAKEOFF)
   A
23.9
 4.1
10.9
   B
35.1
 6.6
23.6
                                               ASSUMES PROPORTIONAL REDUCTION OF POLLUTANT EMISSION  INDEX  AT EACH LTO CYCLE NODE

                                               ATST*v? ?vrRE,on-RnS, REDUCTION IN C0 »•"> "C OBTAINED  BY COWERING EMISSION INDEX VALUES
                                               £L JJrni r   ~ " °*~*'  " *N° HC EMISS«MS AT  OTHER  MODES  REMAIN UNCHANGED, (21 REQUIRED
                                               REDUCTION IN NOX OBTAINED BY  LOWERING  EMISSION  INDEX  VALUES AT CLIMBCUT AND TAKEOFF HOOES 111
                                               «NAiN*SNC0Ml«EVS "E'SURE° "LOES>  MOX  «ISSIONS "  »«-IOLE AND A#RO«S woes           .
-------
                                                                                                                                                                                                             fc
0)

n>

M
ON
ENGINE: TPE331-5-ZS1M S/Ns P04001 COMB P/N' 669083-4
RAT SHF- 706. RA EGT,F=
) FUEL H/C« 1.9Z60 STOI F/»=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Nl, RPM
COMPRESSOR INLET TEMP., DEG.F
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR OSCHG. TEMP,CEG F
TUR8 INTERSTAGE TEMP., DEG.F
CORK BELMTH FLOW, LB/SEC
FA SATIC BASED ON BELLMTH.
MEASURED FUEL FLOH, LB/HR
FA RATIO CALC. FROM EMISSION
) EQUIVALENCE RATIO
LOADING H/P»»N/V/E(T/540)
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
) L3. COZ PER LB. OF FUEL
HEIGHT FLOW, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, WET
! L3. PER 1000 LB. OF FUEL
WEIGHT FLOH, LB./HR.
UNBURNED HYDROCARBONS- PPM AS
PPM BY VOLUME, WET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
1650.
.06*32
Z9
5.1
35.8
33. Z
27560.0
19.0
50.6
302.0
833.0
3.05
.0094
103. D
.0091
.134
.330
99.094
RAT SPD= 41730.
L H V- 18470.
31
7.4
52.0
48. Z
27550.0
19.0
50.6
300.0
680.0
2.96
.0108
115.0
.0100
.147
.322
99.3ZJ
31
9.9
69.6
64.7
37550.0
19.0
50.6
303.0
956.0
2.91
.0113
1Z5.0
.C113
.165
.311,
OEH PT,F« 19.
S LN T,F* 300.0
32
39.9
211.4
195.9
41740.0
20.0
141.0
622.0
1075.0
8.00
.0090
260.0
.0093
.136
.080
99.398 99.802

1.88
3.11
319.9

225.6
Z3.713
2.442
2.07
3.1Z
358.4

206.3
19.767
Z.273
CARBON, HEIGHTS AS
66.0
3.964
.406
.1672
44.1
2.415
.278
.1222
2.34
3.12
390.1

202.6
17.ZZ4
2.153
CM 4
46.2
Z.Z45
.261
.1303
1.9H
3.14
817.2

57.7
5.961
1.550

11.1
.656
.170
.1100
33
78.3
496.6
459.9
41770.0
19.0
146.6
631.0
1273.0
8.00
.0122
352.0
.0124
.182
.071
99.924
FUEL' AV. KERO. TEST NO.' 2
REL HUH
FLO.L/M
34
69.9
634.8
587.9
41760.
19.
153.
635.
1372.
6.03
.0138
400. 0
.0141
.207
.066
99.936
* 100.00 SPEC HUH* .002000
= 14.160 SL TIH.S* 6.5000
35
99.
704.
651.
41760.
18.
154.
636.
1415. ..
B.03
.0147
426. B
.0149
.216
.066
99.935

2.61
3.15
1108.6

28.0
Z.149
.796

6.6
.290
.102
.1359
2.97
3.15
1260.4

19.8
1.338
.535

9.0
.347
.139
.2592
3.1%
3.15
1342.4

17.6

.466

12.0 _'
.439
.167
	 ,3647 	 	 .. ... „
NITRIC OXIDE (NO) - HEIGHTS AS NOZ
PPM B» VOLUME, HET
LB. PER 1000 LB. OF FUEL
WEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE (NOZ)
PPM BY VOLUME, HET
^8. PER 1000 L6. OF FUEL
' ) HEIGHT FLOH, LB./HR.
14.0
2.417
.249

8.0
1.361
.142
19.0
Z.990
.34*

6.3
.991
.114
Z4.Z
3.360
.422

4.6
.670
.064
42.2
7.163
1.663

12.3
2.068
.543
74.5
9.409
3.312

8.0
1.D11
.356
91.0
10.079
4.032

5. a
.637
.235
90. >
10.374
4.419

5.5
.578
.246
TOTAL OXIDES OF NITROGEN (NOtNOZ) AS NOZ
PPM BY VOLUME, HET
i Ld. PER 1000 LB. OF FUEL
! HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
' CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
, CORRECTED HEIGHT FLOH
SMCKE NUMBER
SMOKE NUMBER AT HA*O.OZ3
22.0
3.798
.391

.00713
Z.40
.02114
4 .80
.03516
6.00
.04923
6.50
5.00
1 NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE
Z. EQUIVALENCE RATIO CALCULATED FROM
3. MASS EMISSIONS OF NO,
25.3
3. 982
.458

.00703
.60
.03110
3.00
.03510
3.60
.04914
6.50
3.ZO
29.0
4.050
.506

.00701
1.20
.02102
3.60
.03504
4.80
.04905
7.10
4.20
54.5
9.251
2.405

.00712
3.60
.02136
6.30
.03560
11.30
.04993
15.50
9.70
62.5
10.419
3.667

.00704
3.60
.02112
13.10
.03521
19.00
. .04936
23.80
15.10
96.7
10.716
4.266

.00705
4.80
.02114
11.90
.03523
20.20
.04932
22.60
15.10
104.2
10.951
4.665 	 	

.00703
10.70 	 	
.02109
13.10
.03522
19.00
.04932
21.40
16.20
HET VALUES.
COZ, CO,
AND HC DATA
NOZ, AND NO»MOZ CALCULATED AS
AND FUEL
NOZ FROM
COMPOSITION
»
CONCENTRATIONS HITM

MOLECULAR HEIGHT OF NOZ (46.01).
-------
01
0>

H1
CO
                                                                                        "
                            W? ASTHMRD1655773"° SHP~"  SE*  [E'V£L S'*"""" "' CONDITIONS51"'  "PE'CL»SS"
                            FUt-« ASTM 01655-73            ATONIC H/C RATIO,   1.928
                                                                                          LHVI 18470. BTU/LB
                                                       TURBOPROP

                                                          ADDITIVES!
                                                                                                                              NONE
            CALC DATE  111-7-75
            CALC ID!   3
           TEST NOI     Z
                                                                                                                                       17 JUL» 1973  •••••»»•
                            T*XI-JDLE SETTING*
                           9.056 LB. POLLUTANT PIR 1000 HP.-HR.  PER CYCLE
                           9.084 LB. POLLUTANT PER 1000 HP.-HR.  PER CYCLE

PERCENT RATED TAKEOFF  POHER  i? 6^°" NU«|cENT*MTEO TlKsS?^"  RPM
                                                OXIDES OF NITROGEN  (NOX AS N02)
                                                SMOKE
                                                                                                                                  t  70 PERCENT RATED POWER
                            COM3  TYPE I  REVERSE FLOH ANNULAR
                            ENGINt  TOTAL SERVICE I  0.0	HR     ,illl.
                            ENGINE  ASSEMBLY AND MAINTENANCE INF03MATION1
                    ....   ENGINE  DESCRIPTION  ••»••«»•»•«»».
           TT-     ,.  B69B8Z-|»            SUR/VOLJ 1.260  FUEL
           TIME SINCE ENGINE OVERHAULI   0.0       HR
INJ TYPE!  STAGED SIMPLEX
US£R!
MODEL NO.I
ENGINE INSTALLATION POSITION!
GASEOUS EMISSION TEST NO. , 2 Dml'Il^";' """• '"'?!«
AMBIENT AIR TEMP., 19.00 DEG. F RELATIVE Hu"oiTYI 100 00 PER
AMBIENT AIR QUALITY HYDROCARBONS (HO, 0.0 PPMC CARBON MONO*
SAMPLE LINE ••» TEMP., 300.00 OEG. F. FLOW»»Tr« ... .^ .r^";.,:.::

TEST CONDITION
ACTUAL POWER SETTING, HORSEPOWER
CORR. POWER SETTING (STO DAY), PERCENT RATED
Nl SPEED, RPM
FUEL FLOW «MEAS.» LG./HR.
CORR. ENGINE CORE AIRFLOW (MEASI, LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., DEG F
COMPRESSOR INLET AIR TOTAL PRESS.. PSIA
COMPRESSOR DISCHARGE AIR TOTA. PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL TEMP., OEG f
TUR3INE INTERSTAGE GAS TOTAL TEMP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
» EMISSION CONCENTRATION, HET ANALYSIS
HYDROCARBON IHC AS CH4), PPMC
CARBON M9NOXIOE ICOI , PPMV
' TOTAL OXIDES OF NITROGEN (HOX) , PPMV
CARBON DIOXIDE (C02» , PERCENT BY VOL.
NITRIC OXIDE (NOI, PPMV
EMISSION INDEX. LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CM4I
CAKBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS N02i
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4I
CARBON MONOXIDE CCCJ
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS, CALC)
)
}
SUMMARY <
1
:ENT
^"Zl
*»J 11. 1 KHn^rUKI 1 J
36 37 38
32.5 46.5 68.8
4.98 7.1,1 10.52
27570.00 27530.00 27520.00
103.0 114.0 129.0
3.0 3.0 2.9
18.00 20.00 19.00
14.11 14.11 14.11
50.59 50.59 50.59
302.00 302. OD 304.00
812.0 878.0 957.0
14.16 14.15 14.15
66.300
220.418
21.700
1.863
13.200
4.022
23.391
3.783
.1.14
2.409
.390
99.10
.0090


51.600
215.693
24. 000
2.042
17.500
2.862
20.929
3.825
.326
2.386
.436
99.26
.0099


36.000
192.874
29.000
2.311
24.300
1.770
16.586
4.096
.228
2.140
.528
99.45
.0111


39
196.3
29.99
41760.00
260.0
8.0
20.00
14.17
140.32
623.00
1074.0
14.01
7.500
63.974
55.400
1.899
42.600
.451
6.737
9.503
.117
1.752
2.492
99.80
.0091


™i{£
Soh;TRoi
ME! 6.50 SEC.
40
458.3
70.10
41740.00
350.0
8.0
19.00
14.17
148.58
630.00
1275.0
14.03
4.500
32.033
85.000
2.555
77.500
.202
Z.513
10.954
.071~
.080
3.034
99.92
.0122


41
588.5
90.11
41750.00
398.0
8.0
10.00
14.17
152.75
634.00
1373.0
14.07
5.400
27.139
97.500
2.929
94.500
ilsso
10.964
.084
.739
4.364
99.94
.0139


B. H20/LB. DRY AIR
.EN (NOXM 0.0 PPNV
LENGTHI 50.00 FT.
42
653.0 	
99.78
41740.00
426.0
8.0
20.00
14.17
154. 7Z
637.00
1419.0
14.09
7.500
22.675
106.750
3.130
100.750
.275
1.453 " :
11.235
_
.117 ,
.619
4.786
99.94
.0149


                                                                                                                                                                         CM
-------
         ,  V
                                                                                                                                                               *
CTi
vo
«..»....»»..•••.....»......,...,......„..  EP)k CYCuE EMISSIONS COMPUTATION  SUMMARY   •••••••»••
ENG MFC I AIRESEARCH           TEST FAClL  I PHX LACC2  INSTR DESCRIP I  FED REG  V36 N136
MODEL NO.I     TPE331-5-251M     S/NI    POU001              ENGINE  TYPE(CLASSII   TURBOPROP
RATED POWER!     706.0 SHP AT SEA _EVEL  STANDARD DAY CONDITIONS
FUE.t ASTM 01655-73            ATOMIC H/C  RATIOI   1.928     LHVI  18470.  BTU/LB     AOOITIVESI
                                                                                                                         CALC  DATE tll-7-75
                                                                                                                         CALC  101   1
                                                                                                                        TEST NOI      2
                                                                                                                   .HOME
MODE TAXI-IDLE
(INI
TIM; IN MODE, MINUTES
RATED POWER, PERCENT
CORRECTED POWER, HORSEPOWER
HP-HR
FUEL FLOW. LB/HR
FUEL MASS, LB _ _
•• HYDROCARBON EMISSIOK (HC) "
INDEX, LB HC/1000 LB FUEL
RATE, LB HC/HR
NASS, LB HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORSEPONER-HR PER CYCLE
»• CARBON MONOXIDE EMISSIONS 
-------
13
0)
iQ
(D
h '



ENGINE* TPE331-5-2S1M S/N. Pl-flOl**" "^^^"p/M^VanL5"1"1*** *""""""*""""«""««•••««•"«•
RAT SHP* 706. RA EGT.F* 1658. RAT SPO- 41730 — — 86908Z-1' FUE«-« *«• *«<>• TEST NO.' 2
FUE;. H/C* 1.9280 STOI F/A* .06822 L H V* 1847o!
DATA POINT NUMBER J6 37 «
utn KI,F« 19. REL HUM»
S LN T.F= 300.0 FLO,L/M=

PERCENT MAX. CORRECTED POHER 5.0 7.i in S *a*« *„*.' **
SS^SHS:?TFTHPHP g:,' »: : «S:! £:J Jtt.
' ^PRE^OR^E-; ?EMP..OEC.F «"£ «» £ «» £ "^ ^j -£'
> SRSS =: KG'; ,S:: .S:s 3 : i : j : £:
ra^SsT 2S a! l-i« "1 J* "Si
EEi^r— ••«>• *& % fH € S
LOADING H/P-N/V/EIT/540, 3Z9 '32? 'if! "J" •"* -2»*
; ss!.;s:s.:s:.s:i5;j^. "•°'? «:'» «''« «:"' 99:5» 99:93!
CARBON DIOXIDE *"»"'*»»SUMMARY OF REDUCED EMISSION DATA*»»»»'*-
) ^ PE^IF F-uL \:ll IX i:ii j-;:'. «-» •«.«
uMS'SS^ffi- tB"H" 319-9 «*•• ««" •»" «fc" iAf5
) PPM BY VOLUME, NET 220. 4 215.7 192 a
LB. PER 1000 LB. OF FUEL 23.391 20.929 16.586
HEIGHT FLON, L8./H1. 2...09 2.386 2 140
' UNBU^e° "YOROCARBONS- PPM AS CARBCN, WEIGHTS AS CH4
PPH BY VOLUME, WET 66.3 51. 6 36.0
LB. PER 1000 LB. OF FUEL 4.022 2.862 1.770
1 HEIGHT FLOW. Lfl./HR. .4,11, S26 228
RATIO LB HC/L8 CO .1719 .1367 1067
NITRIC OXIDE INOI - HEIGHTS AS N02
) PPM BY VOLUME, WET 13.2 17.5 24.3
L3. PER 1000 LB. OF FUEL 2.3H1 2.789 3.433
WEIGHT FLOW, LB./HR. .237 .318 .1.1,3
) NITROGEN DIOXIDE CN02)
PPM BY VOLUME, WET «.S 6.5 ,, ,
L3. PER 1000 LB. OF FUEL 1.482 1.036 .664
) HEIGHT FLOW, LB./HR. .153 .118 .086
TOTAL OXIDES OF NITROGEN (NO+N02I AS N02
PPM BY VOLUME, WET 21.7 24.0 29.0
> LB. PER 1000 LB. OF FUEL 3.783 3.825 *.096
WEIGHT FLON, LB./HR. .390 .436 .528
SMCKE MEASUREMENT DATA
) CORRECTED WEIGHT FLON .00731 .00705 .00706
SMOKE NUMBER 2.»0 2.40 0.00
CORRECTED HEIGHT FLOW .02102 .02114 .02117
) SMOKE NUMBER 1..80 3.60 1.20
CORRECTED WEIGHT FLOM .03510 .03524 .03520
SMOKE NUMBER 8.30 -.88 3.60
} CORRECTED HEIGHT FLOM .04914 .04942 .04940
SMOKE NUMBER 7.10 6.01 "lO
SMOKE NUMBER AT HA*0.023 5.70 4.20 3.00
1 NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE WET VALUES.
64.0 32.0 27.1
6.737 2.513 1.858
1.752 .880 .739

•» 4.5 5.4
.451 .202 .211
.117 .071 .084
.0670 .0803 .1137
42.6 77.5 94.5
7.369 9.987 10.627
1.916 3.495 4.230

"•' '«' ._ 3.0
2.21* .966 .337
.576 .338 ,13fc
55.4 85.0 " 97. S ~
9.583 10.954 10.964
2.492 3.834 4.364
.00712 .00713 .00713'
2.40 4.80 4.00
.02135 .02139 .02139
7.10 13.10 10.71
.03558 .13564 .03564
10.70 20.20 17.90
.04981 .04990 .04990
15.50 25.00 21.40
9.10 15.90 13.01
100.00 SPEC HUM= .002000
14.160 SL TIM.S' 6.5011

42
99.8
704.4
653.
41740.
20.
154. 	 	
637.
1419.
8.11 ~ - - — -- .
.0167
426.1
.0149
.218
.066
99.942
3.13 ' "" '"" "
3.15
1342.3 ... . . ._
22.7
.619

7.5
.275
.117
100.7
10.603 .
4.517 -

6.0 	 	
.631
.269
11.235
4.716
.00713
3.61 . . .. .
.12139
11.90
.03564
15.51 - -
.04990
19.00
12.60
2, EQUIVALENCE RATIO CALCULATED FROM C02.CO, AND HC DATA AND FUEL COMPOSITION.
3.MASS EMISSIONS OF NO, N02. ANO WHN02 CALCULATED AS N02 FROM CONCENTRATIONS "lOTM MOLECULAR NEI6MT O^OZ M.itT.~ 	 ~
                                                                                                                                                                                       S
                                                                                                                                                                                        )

                                                                                                                                                                                        )
                                                                                                                                                                                       OJ
-------
                         .............................................   »IR£SEARCH EMISSION TEST SUMMARY  ••»••»»•»»»••»
                         ENG NFC I A1RESEARCH           TEST FACIL  I  PHX LACCZ   INSTR DESCRIP t FED KEG Y38 N136
                         KOOEL NO.I     TPE331-5-251H     S/Nt    P04001              ENGINE TYPE(CLASS)I  TURBOPROP
                         HATED POWER!    706.0 SHP AT SEA LEVEL  STANDARD DAY  CONDITIONS
                         FUEL! ASTK 01655-73            ATONIC H/C  RATIOI   1.928     LHVI 18471. BTU/LB     ADDITIVES!
 CALC DATE tll-    I TOTAL OXIDES OF NITROGEN (NOX AS N02I
EMISSIOK RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4I
CARBON MONOXIDE (COI
TOTAL OXIDES Of NITROGEN INOX AS N02I
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS, CALCI
J
:>
43 44 45
33.1
5.05
27510.00
107.0
3.1
40.00
14.17
49.36
315.00
841. 0
14. 16

78.000
213.340
22.011
1. 954
14.800

4.513
21.595
3.658

.483
2.311
.391
99.10
.0095


49.9
7.49
27520.00
117.0
2.9
38.11
14.17
49.98
313.11
896.0
14.16

42.001
192.413
25.010
2.103
18.811

2.266
18.162
3.876

.265
2.125
.454
99.37
.0101


69.6
11.44
27540.00
130.0
2.9
38.01
14.17
51.44
315.80
976.0
14.16

32.400
170.536
30.000
2.371
24.501

1.554
14.315
4.136

.202
1.861
.538
99.53
.0114


46
zoo. a
30.10
41750.00
260.0
8.1
38.81
14.17
138.65
640.00
1070.0
14.16

7.200
62.294
57.501
1.913
41.300

.431
6.514
9.876

.112
1.694
2.568
99.81
.0092


47
469.8
70.42
4175B-.00
356.0
8.1
38.01
14.17
146.46
649.00
1270.0
14.17

2.400
29.175
90.500
2.613
83.011

.115

11^407

.137
.797
4.161
99.94
.0124


41
60Z.1
90.26
41750.00
400.1
8.0
38.11
14.17
151.29
655.11
1319.0
14.11

.900
22.675
107.501
2.963
101.501

.135
1.535
11.954

.014
.614
4.782
99.96
.0141


49
668.8
101.16
41721.01
428.1 	 ._.
7.9
41.11
14,17 	
151.52
659.01
1430.1 	 	 _
14.12

1.208
19.846
118.750
3.195^ 	
112.511

.043
-------
(D
to
                  )
                  y

ENG MFC J AIRESEARCH CYCLE EMISSIONS
2l*J^ ««9i,«.«cr!6'0 SHP *T SE* L-"EL ST'""™ BAY
FUEt, ASTM 01655-73 ATOMIC H/C RATIO, 1
MODE
TIME IN MODE, MINUTES
RATED POWER, PERCENT
CORRECTED POWER, HORSEPOWER
HP-MR
FUEL FLCW, LB/MR
FUEL MASS, LB 	 -
•» HYDROCARBON EMISSION IMCI «•
INDEX, LB HC/1000 LB FUEL
RATE. LG HC/HR
NASS. LE HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORSEPOWER-HS PER CYCLE

*• CARBON MONOXIDE EMISSIONS ICO) ••
INDEX, LB CO/1B08 LB FUEL
RATE, LB CO/MR
MASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1001 HORSEPOHER-HR PER CYCLE

« TOTAL OXIDES OF NITROGEN EMISSIONS INOXI ••
INDEX, LB NOX/1000 LB FUEL
RATE, LB NOX/HR
MASS. LB NOX
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB NOX/1000 HORSEPOHER-HR PER CYCLE
C.NU J
TAXI-IDLE
UNI
7.000
5.000
35.300
106.778
12.1.57

4.589
.057
25.7



21.672
2.3H.
.270
23.3

~
3.651
.390
*7.6



'« 18470. BTU/.B
TAXI-IOLE
IOUTI
19.000
5.000
35.300
11.178
106.778
33.813

4.589
.1.90
.155
69* 7


21.672
.733
63.2


3.651
.398
.123
20.5



CALC DATE ,11-4-75
TURBOPROP CALC 1O« 1
TEST NOI 3
ADDITIVES, NONE
APPROACH
-------
(T)
OJ
EMGINE« TPE331-5-Z51M S/N« P04001 COMB P/Nr 86908Z-*
RAT SHP* 706. RA EGT,F=
FUEL H/C« 1.9280 STOI F/A-
OATA POINT NUMBER
PERCENT MAX. CORRECTED POWER
CORRECTED SHAFT HP
MEASURED SHAFT HP
' SHAFT SPEED, Nl, RPH
COMPRESSOR INLET TEMP., DEC. F
COMPRESSOR OSCHG. PRES. ,PSIA
1 COMPRESSOR OSCHG. TEMP.OEG F
TURB INTERSTAGE TEMP., DEG.F
CORR 3ELMTH FLOH, LB/SEC
%' FA RATIO BASED ON BELLHTH.
MEASURED FUEL FLOH, L9/HR
FA RATIO CALC. FROM EMISSION
' EQUIVALENCE RATIO
LOADING H/P*»N/V/EiT/5*0>
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
) LB. COZ PER LB. OF FUEL
HEIGHT FLOM, LB./HR.
CARBON MONOXIDE
> PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUHE, MET
LB. PER 1000 LB. OF FUEL
) MEIGHT FLOM, LB./HR.
RATIO LB HC/LB CO
NITRIC CXIOE (NOI • HEIGHTS AS
PPM BY VOLUME, MET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
NITROGEN DIOXIDE CN02>
PPM BY VOLUHE, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
1650.
.06822
*3
5.1
35.7
33.8
Z7510.0
1.0.0
*9.*
315.0
8*1.0
Z.98
.0101
107.0
.0095
.139
.322
99.096

1.95
3.11
33Z.5

Z13.3
Z1.S95
2.311
RAT SPD
L H V
44
7.5
52.9
49.9
27520.8
38.0
49.9
313.0
896.0
Z.94
.0112
117.0
.0101
.1*9
.313
99.374

Z.10
3.12
365.0

192.*
18.162
2.125
CARBON, HEIGHTS AS
78.0
*.513
.1.83
.2090
NOZ .
1*.8
2.1.61
.263

7.Z
1.197
.128
42.0
2.266
.265
.1248

18.8
Z.915
.3*1

6.2
.961
.11Z
- 41730.
= 18*70.
45
10.*
73.7
69.6
Z7540.0
38.0
50.4
315.0
978.0
Z.90
.0127
130.0
.011*
.167
.302
99.5Z7

2.37
3.13
406.5

170.5
14.315
1.861
CH4
32.4
1.55*
.202
.1086

24.5
3.378
.439

5.5
.758
.099
OEM PT,F= 19.
S LN T,F= 300.0
46
30.1
212.5
ZOO.
•,1750.
38.
138.
640.
1070.
7.99
.0092
260. 0
.0092
.13*
.078
99.809

1.91
3.1*
817.1

62.3
6.51*
1.69*

7.2
.430
.112
.0661

41.3
7.09*
1.8%*

16. Z
Z.783
.723
*7
70.4
497. Z
469.8
41750.0
38.0
146.5
6*9.0
1Z70.0
7.97
.0126
356.0
.0124
.182
.069
99.938
FUEL* AV. HERO. TEST NO.* 3
RE>. HUH'
FLO.L/N*
*•
90.3
637.3
60Z.
41750.
38.
150.
655.
1389.
7.97

400.0
.0141
.206
.065
99.961
40.00 SPEC HUM' .002000
14.160 SL TIH.S* 6.5001
49
100.1
706.4
668.
41720.
*0.
151.
659.
1*30.
7.95
.0152
428.0
.0152
.222
.06*
99.967

2.61
3.15
1121.5

29. Z
2.239
.797

Z.*
.105
.037
.0471

83.0
10.462
3.7Z4

7.5
.9*5
.337
TOTAL OXIDES OF NITROGEN INC+NOZ) AS NOZ
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED MEIGHT FLCH
SMOKE NUMBER
CORRECTED MEIGHT FLOM
1 SMOKE NUMBER
CORRECTED MEIGHT FLCM
SMOKE NUMBER
CORRECTED HEIGHT FLCH
SMOKE NUMBER
SMOKE NUMBER AT NAcO.023
22.0
3.658
.391

.00692
2.1,0
.02075
2.40
.03*58
4.70
.0*841
8.ZO
4.50
Z5.0
3.876
.*54

.00693
1.20
.02078
Z.40
.03470
5.90
.04651
5.99
3.90
30.0
4.136
.538

.00694
Z.40
.02082
Z.40
.03469
3.50
•04657
7.10
3.90
57.5
9.876
Z.568

.00697
5.90
.02091
8.ZO
.03485
12.90
.04887
17.60
11.30
90.5
11.407
4.061

.00703
7.10
.02109
12.90
.03514
ZO.OO
.049ZO
23.50
16.10
2.96
3.15
1260 . 6

22. 7
1.535
.61*

.9
.035
.01*
.0227

101.5
11.287
4.515

6.0
.667
.267

107.5
11.95%
4.782

.0070*
5.90
.02112
11.80
.03527
17.60
.0*938
23.50
14.90
3.19
3.15
1349.1

19.8
1.2*6
.533

1.2
.0*3
.018
. 03*6

112.5

4.966

6.3
.6*5
.276

118.8
12.2*8 -^
5.2*2

.00705
4.70 . .
.02116
10.6*
.03527
17.61
.0*930
2Z.*I
1*.00
                                                                                                                                                                          3
                                                                                                                                                                         i

                                                                                                                                                                         ')
                            NOTES 1. ALL EMISSIONS  CONCENTRATIONS ARE MET VALUES.
                                  Z.EQUIVALENCE  RATIO CALCULATED FROM COZ,CO,AND HC DATA AND FUEL COMPOSITION.
                                  3.MASS EMISSIONS  OF NO,  NOZ, AND NOtNOZ CALCULATED AS NOZ FROM CONCENTRATIONS HITH
                                                                                                                      MOLECULAR MEIGHT OF  NOZ  (<.6.01).
-------
                             NO ,     "
                                                                      AIRESEARCH EMISSION TEST SUMMARY

                                                                                                       TUR:::;L,
                                                                                                       DATE 111-4-75
                                                                                                  CALC IDI    2
                                                                                                        •    3
                                                                                 co,
                                                                                                                          87   17 JULY 1973
                                                s
                       mi-IOLE SETTING, s        P£SCENT  RATED  TAKEOFF ,o«J%S?


                                                                                                    70 PERCENT RATED POKER
(D
COMB TYPE!  REVERSE FLOH ANNULAR        ***P*Nr"»906Z-"ME
l«ci«r  I2«MBSER"CEI  ••"       M"    TINE SINCE ENGINE  OVERHAUL,  ill
ENGINE  ASSEMBLY  AND MAINTENANCE INFORMATION!
AIRCRAFT  INSTALLATION »••• MFR.I
                          useiRjN»o«Tv7iCr°"H^°[!s"~^EH?s"'i;rt?i?"
50 SI SZ
33.3 50.0 66.3
5.00 7.47 9.97
27560.00 27530.00 27550.00
3.1
39.00
14.17
49.61
314.00
639.0
14.15
99.000
225.642
21.600
1.649
13.400
6.036
24.070
3.820
.646
2.575
.409
96.91
.0090
iir.o
2.9
42.00
14.17
49.61
317.00
916.0
14.15
55.500
203.055
26.500
2.103
20.400
2.991
19. ItS
.350
2. 241
.461
99.29
.0102
127.0
Z.9
36.00
14.17
50.54
314.00
963.0
14.15
33.600
160.966
29.900
2.297
24.201
1.663
15.671
4.253
.211
1.990
.540
99.49
.0110
53
202.1
30.32
41770.00
256.0
6.0
38.00
14.17
138.75
641.00
1063.0
14.05
7.501
59.779
59.100
1.886
45.100
.455
6.3V2
10.281
.117
1.636
2.653
99.11
.0091
54
467.2
69.95
41750.00
346.0
8.0
40.01
14.17
145.36
653.10
1290.0
14.15
.901
26.767
69.500
2.608
80.000
.141
2.212
11.315
.114
.770
3.934
99.94
.0124
55
602.9
91.36
417Z1.00
400.0
6.1
39.10
14.17
151.15
657.01
1396.1
14.11
Z.100
19.846
105.800
3.120
102.000
.811
1.318
11.457
.132
.527
4.563
99.96
.1144
56
671.0
100.45
41760.00
42 6.0
6.0
48.01
isilzi
661.10
1475.0 .
14.11
z.iBi : 	
19.442
115.008
3.177
107.588
.8.76
1.2Z1
11.927
.832
.523
5.811. 	 ._
99.96
.0151
                                                                                                                                                              cv
-------
Ul
                        **•»»»«••**»•»»»»»»»»••»»»»•*»•••*»••*•••»  EP(l CYCLE EMISSIONS COMPUTATION SUMMARY   ••••••••••»»»«•»»•••••»•••»•»•••••»•••••••
                        ENG MFC > AIRESEARCH           TEST FACIL  > PHX LACCZ   INSTR  OESCRIP  I  FED REG  V38 N136               CALC DATE 111-4-75
                        MODEL NO.I      TPE331-5-251M      S/NI    P04001              ENGINE  TYPE(CLASS!I   TURBOPROP           CALC 101    Z
                        RATED POWER!     706.0  SHP  AT  SEA  LEVEL  STANDARD DAY  CONDITIONS                                       TEST NOI    3
                        FUELI ASTM  D1655-73            ATOMIC H/C  RATIOI   1.928      LHVI  18470.  BTU/LB     ADDITIVES!  NONE
MODE
TIME IN MODE, MINUTES
RATED POWER. PERCENT
CORRECTED POWER. HORSEPOWER
HP-MR
FUEL FLCW, LB/HR
FUEL MASS, LB
•• HYDROCARBON EMISSION (HC) "
INDEX, LB HC/1000 LB FUEL
RATE, LB HC/HR
MASS, L6 HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORSEPOMER-H9 PER CYCLE
)
« CARBON MONOXIDE EMISSIONS (CO) ••
INDEX, LB CO/1000 LB FUEL
) RATE, LB CO/MR
MASS, LB CO
MASS. PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORSEPOWER-HR PER CYCLE
•• TOTAL OXIDES OF NITROGEN EMISSIONS (NOX) *•
INDEX. LB NOX/1000 LB FUEL
RATE. LB NOX/HR
MASS. LB NOX
> MASS, PERCENT OF TOTAL CYCLE
CYCLE. LB NOX/1000 H9RSEPOWES.-H* PER CYCLE
TAXI-IDLE
(INI
7.000
5.000
35.300
4.118
107.012
12.485

6.031
.645
.075
25. 8



24.062
2.575
.300
23.8

	 	
3.820
.409
.01.8
7.9

TAXI-IDLE
(OUT)
19.000
S.OOO
35.300
11.178
107.012
33.887

6.031
.645
,204
70.1



24.062
2.575
.815
64.5

_„---- - . -
3.820
.409
.129
21.4

APPROACH
4.500
30.000
211.800
15.885
255.456
19.159

.507
.129
.010
3.3



6.396
1.634
.123
9.7

. • _ .
10.176
2.599
.195
32.3

CLIM80UT
2.500
90.000
635.400
26.475
398.043
16.585

.122
.049
.002
.7



1.321
.526
.022
1.7

._
11.409
4.541
.189
31.3

TAKEOFF 1
.500
100.0*0
706.000
5.883
427.414
3.562

.027
.012
.000
.0



1.236
.528
.004
.3


11.984
5.122
.043
7.1

rOTAL PER
CYCLE
33.500


63.540

85.678

3.402
.522
.292
100.1
4.5S8


14.761
2.265
1.265
100.0
19.904

7.051
i.0«2 _
.6B4
100.0
9.506
                                              •• EMISSION INDEX LEVELS REQUIRED TO MEET EPA 1979 STANDARDS FOR CLASS  P2  ENGINES •*


                                           EPA LTO-CYCLE                                           REQUIRED EMISSION  INDEX, LBP/1000 LB FUEL
                                    POLLUTANT   LBP/1000 HORSEPOMER-HR-CYCLE
                                       CO             26.8
                                       HC              4.9
                                       NOX            12.9
POL4UTANT I MODE!
   CO (IDLE)
   HC «IDtEI
   NOX (TAKEOFF)
   A
24.1
 6.1
12.1
   a
33.5
 6.5
23.1
                                              A  ASSUMES PROPORTIONAL REDUCTION OF POLLUTANT EMISSION INDEX AT EACH LTD CYCLE MODE

                                              B  ASSUMES (1) REQUIRED REDUCTION IN CO AND HC OBTAINED BY LOWERING EMISSION INDEX VALUES
                                                 AT TAXI-IDLE NODE ONLY, CO AND HC EMISSIONS AT OTHLR MODES REMAIN UNCHANGED. 121 REQUIRED
                                                 REDUCTION IN NOX OBTAINED BY LOWERING EMISSION INDEX VA-.UES AT CLIM3CUT AND TAKEOFF MOOES IN
                                                 SAME PROPORTION AS MEASURED VALUES, NOX EMISSIONS AT TAXI-IDLE AND APPROACH MOOES      	
                                                 REMAIN UNCHANGED
                                                               .3

                                                               t
-------
0)
iQ
(D
ENGINE' TPE331-5-251M S/N« P04101 COHB f/N- 969082-1.
RAT SHP= 706. RA EGT.F* 1650.
FUEL M/C« 1.9Z80 STOI F/A' .068ZZ
DATA POINT NUMBER
PERCENT MAX. CORRECTED POKER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Nl, RPH
COMPRESSOR INLET TEMP., DEC. F
COMPRESSOR OSCHG. PRES. iPSIA
COMPRESSOR OSCHG. TEMP, DEC F
TORS INTERSTAGE TEMP.. CEG.F
COR* BELHTH FLOH, IB/SEC
FA RATIO BASED ON BEi-LMTH.
MEASURED FUEL FLON, LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P«N/V/E«T/540>
COHB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, NET
LB. COZ PER LB. OF FUEL
HEIGHT FLOH, LB./H3.
CARBON MONOXIDE
PPP BY VOLUME, NET
LB. PER 1001 LB. OF FUEL
HEIGHT FLOH, L8./H*.
UNBURNED HYDROCARBONS- PPM AS
PPH BY VOLUME, NET
LB. PER 1000 LB. OF FUEL
HEIGHT FLON, LB./HH.
RATIO LB HC/LB CO
SO
5.0
35.3
33.3
27560.0
39.0
49.6
314.0
839.0
3.10
.0097
107.0
.0090
.13Z
.333
98.904

1.05
3.10
331.7

ZZS.6
24.070
Z.575
RAT SPO:
L H V*
51
7.5
5Z.7
50.0
27530.0
wZ.l
1,9.6
317.0
918.0
Z.93
.0113
117.0
.0102
. 1*9
.312
99.207

Z.10
3.12
364.5

203.1
19.11.5
Z.Z40
CARBCN, HEIGHTS AS
99.0
6.036
.646
.zsie
NITRIC OXIDE (NOI - HEIGHTS AS NOZ
PPM BY VOLUME, NET 13.4
LB. PER 1000 LB. OF FUEL Z.J48
HEIGHT FLOH, LB./HR. .251
NITROGEN DIOXIDE INOZI
PPM BY VOLUME, WET
LB. PER 1001 LB. OF FUEL
HEIGHT FLOH, LB./HR.

8.4
1.47Z
.157
TOTAL OXIDES OF NITROGEN INC«N02> AS NOZ
PPM BY VOLUME, HET Zl.l
L3. PER 1000 LB. OF FUEL 3.620 '
HEIGHT FLOH, LB./HR. .'•09
SNOKE MEASUREMENT DATA
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLCH
SNOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLCH
SMOKE NUMBER
SNOKE NUMBER AT HA»0.t23
,00701.
Z.40
.02111
3.50
.03519
7.10
.0
-------
                          c«r  «r i    •••"•*""»••••»••*"•••••••••••   AIRESEARCM EMISSION TEST SUMMARY  •»••»••»»••••.
                          ENG  HFC I  AIREStARCH           TEST  FACIL  I  PHX cACC2  INSTR OESCRIP I FED RE6 V36 N136
                          MODEL NO.!     TPE331-5-2S1M     S/NI    P04001              ENGINE TYPE(CLASS)I  TURBOPROP
                          RATED PONER,    786.8 SMP AT SEA LEVEi.  STANDARD DAT CONDITIONS     TYPEICL*SS"  "«BOPRW
                          FUELI ASTH 01655-73            ATOMIC H/C  RATIO!   1.928     LHVI 18470. BTU/LB     ADDITIVES!
                                                                                                                            NOME
 CALC DATE 111-4-75
 CALC IDI      3
TEST N0<    3
                              ••»• EXHAUST EMISSIONS PER EPA  CYCLE OF WORK OUTPUT " CODE OF FEDERAL REGULATIONS TITLE  41  PART  67   17  JULY  1873  •••••••
                                              HYDROCARBONS  (CH  AS CH4I           2.626 LB. POLLUTANT PER 1000 HP.-HR. PtR CYCLE
                                              CARBON HONOXIOE (CO)              17.199 LB. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                              OXIDES OF NITROGEN 1NOX AS N02)    9.1.71 L8. POLLUTANT PtR 1000 HP.-HR. PER CYCLE

                          T.XI-IOLE SETTING, 9T*   PERCENT RATED  TAKEOFF PO«R*AT5 £™ ^Illl^l^ TOSS'S  RPHM°°£'  "  ***** «"" """-
 0)
iQ
 CD
                               T.C.T   '"""""**"•"••*•••**•*"••""•»••'"•  ENGINE DESCRIPTION  »»••••»••••»»»»...»....».»...»»»,»..,..„

                          ENGINr?0ETALRESVlRv!cE^°H.*rULAR  HR     ^'^12^ ^OVERHAUL,  iT"*' '£"  "" -"" "« '  «"« ^^
                          ENGINE  ASSEMBLY AND MAINTENANCE INFORMATION!                                              -                 —.-..--.
                          AIRCRAFT  INSTALLATION •»•• MFR.t                                  MODEL NO.t
                                                     USER»                        ENGINE  INSTALLATION POSITION!
_ _ " •• •-•» - t-nv*n£,Lii^iMLL
.Hijun rui.
II lUFII



GASEOUS EMISSION TEST NO. 1 3 DATE! 11-4-75 TIME! BARO PRESS 1 28 860 IN Hf.A
AMBllUI IlR JUA^TY "'UJnSnrlo!;,, RELATIVE HUMIDITY. 40.00 PERCENT SPECIFIC HUMIDITY! !o02DOO LB. H20/Ls! DRY AIR
SAMPLF Lli? 2"J JPMO , 7«S n* o??S °'° PPMC C ARSON MONOXIDE ICOI 1 0.0 PPMV OXIDES OF NITROGEN (NOXII 0.1 PPMV
SAMPLE LINE •" TEMP., 300.00 DEC. F. FLOHRATEI 14.16 LITERS/MIN. TRANSPORT TIME! 6.50 SEC. LENGTH! 51.01 FT.
TEST CONDITION
ACTUAL FOWtR SETTING, HORSEPOWER
CORR. POWER SETTING (STO DAY), PERCENT SATED
Nl SPEED, RPM
FUEL FLOW (MEAS.) LB./HR.
CORR. ENGINE CORE AIRFLCM (MEAS), LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., DEG f
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL TEMP., DEE F
TURBINE INTERSTAGE GAS TOTAL TEMP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSIOt. CONCENTRATION, WET ANALYSIS
HYDROCARBON (HC AS CH4I , PPMC
CARBON MONOXIDE (CO), PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPMV
CARBON DIOXIDE (C02), PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSION INDEX, LB. POLLUTANT/1010 LB. FUEL
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
EKISSICK RATE, LB. POLLUTANT/HR. 	
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
COMSUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS, CALC)
57 c* eA
34.2
5.11
27540.00
106.0
3.0
40.00
49.12
317.00
846.0
14.16
60.000
200.268
23.000
1.917
16.300
3.542
20.667
3.903
.376
2.193
99.20
.0093
49.5
7.41
27570.00
113.0
2.9
40.00
14.17
49.61
319.00
908.0
14.16
54.000
197.027
25.500
2.127
19.300
2.879
16.378
3.907
.325
2.077
.441
99.32
.0103
w
67.7
10.12
27570.00
125.0
2.9
41.00
14.17
49.95
321.00
985.0
14.16
30.600
174.153
30.200
2.336
24.500
1.490
14.634
4.225
.186
1.854
.528
99.52
.0112

60
206.1
30.84
41760.00
254.0
8.0
40.00
137.77 .
646.00
1094.0
14.06
6.900
61.036
61.500
1.954
48.200
.404
6.249
10.342
.103
1.587
2.627
99.82
.1094

61
465.8
69.69
417fc0.01
34Z.O
7.9
40.00
145.14
655.00
1295.0
14.06
2.700
28.767
92.750
2.639
85.250
.117
2.185
11.574
.048
.747
3.958
99.94
.0126

62
603.3
90.26
41730.00
389.0
7.9
40.00
14 n
i •(. 1 1
146.62
659.01
1419.1
1*. 11
1.510
21.865
111.510
3.063
104.500
. .056
1.422
11.608
.022
.553
4.593
99.96
.1146

61
669.6
100.16
41771.10
. 4.20.0 	
8m
• •
41.11
151.66
664.01
1474.0 	
14.12
1.511
17.831
121.251
3.231
113.751
	 .053
1.107
12.266
A 99
• VC£
(.&£
• "tOS
5.152
99.97
.0153
                                                                                                                                                                       y
                                                                                                                                                                       >

-------
CD

n>

M

CO
ENG MFC I AIRESEARCH
MODEL NO.I     TP£331-S-251N
RATED POWERI     706.0  SHP  AT
FUEL I ASTM D1655-73
                                                         TEST
              EPA  CYCLE  EMISSIONS COMPUTATION SUMMARY  ••
              PHX  LACC2   INSTR OESCRIP I  FED REG V38 N136
                              ENblNE TYPE(CLASS! 1
                  DAY CONDITIONS
ATOMIC H/C RATIO   1.928      LHVJ  18*70.  BTU/LB
                                                                                                               AOOITIVESI  NONE
                                                                                                                                CALC DATE 111-4-75
                                                                                                                                CALC 101      3
                                                                                                                               TEST NO*     3




)
)

)





1
)
NODE
TIME IN MODE, MINUTES
RATED POWER, PERCENT
CORRECTED POWER, HORSEPOWER
HP-HR
FUEL FLOW, LB/HR
FUEL MASS, LB
•• HYDROCARBON EMISSION CHCI ••
INDEX, LB HC/1000 LB FUEL
.RATE. LB HC/HR
MASS. LB HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORSEPOWER-HR PER CYCLE

•• CARBON MONOXIDE EMISSIONS CCO) •»
INDEX, LB CO/1008 LB FUEL
RATE, LB CO/HR
MASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORSEPOWER-HR PER CYCLE


IUIML UAluta or NITROGEN EMISSIONS (NOXI •*
INDEX, LB NOX/1010 LB FUEL
RATE, LB NOX/HR
MASS, LB NOX -
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB NUX/1000 HORSEPOWER-HR PER CYCLE

TAXI-IDLE
(INI
7.000
5.000
35.300
*. 118
105.750
12.338

3.552
.376
.om,
26.3


20.763
2.196
• 256
2J.5 -



3.908
."»13
. 0<*8

TAXI-IOLE
(OUT!
19.000
5.000
35.300
11.178
105.750
33.1.88

3.552
.376
.119
71.3


Z0.7b3
2.196
.695
63.7



3.908
.*13
.131
21.7

APPROACH
*.500
30.000
211.800
15.885
2*9.396
18.705

.187
.01,7
.001.
Z.I


6.113
1.521.
10.5



10.117
2.523
.189
31.1,

CLIMBOUT
2.500
90.000
635.1.00
26.1,75
388.155
16.173

.013
.005
.000
.1


1.373
.533
.022
2.0



11.781
I..573
.191
31.7

TAKEOFF
.500
100.000
706.000
5.883
419.509
3.1.96

.110
.01.6
.000
.2


1.189
.1.99
.001.
.1.



12.279
5.151
.01,3
7.1

TOTAL PER
33.SBI
63.5*0
8*. 199

1.982
.299
.167
100.0
2.626

12.971
1,956
1.09Z
100.0
17.189


7.1*7
1.078
.602
110. (

                                               »• EMISSION INDEX LEVELS REQUIRED  TO  M£Et  EPA  1979 STANDARDS FOR CLASS P2 ENGINES ••
                                            EPA LTO-CYCLE
                                     POLLUTANT   IBP/1009 HORSEPOMER-HR-CYCLE
                                        CO             26.8
                                        HC              (,.9
                                        NOX             12.9
                                                                                                     REQUIRED  EMISSION INDEX, LBP/1000 LB FUEL
                                                                            POLLUTANT I NODEI
                                                                               CO IIDLEI
                                                                               HC IIDLEI
                                                                               NOX CTAKEOFFI
                                                                          A
                                                                       20.«
                                                                        3.6
                                                                       12.3
   a
M.I
 6.7
23.7
                                              A  ASSUMES PROMOTIONAL  REDUCTION OF POLLUTANT EMISSION INDEX AT EACH LTOI CYCLE MODE	


                                              8  IT^TA^ im'-R5^"n2  R£D"CTION I!» co *"" « 08TAINED 6Y LOWERING EMISSION INDEX VALUES
                                                 ?LT.?*I:IOLc M00t ONLY-  "  AND HC EMISSIONS AT OTHER MOOES REMAIN UNCHANGED, «• •*""«••>
-------
n>
 vo
ENGINE* TP&Sn-S-ZSlN S/H- P04I01 CONB ?/N- 8690(Z-«.
RM SHP- 786. «» E6T.F* 1658. WT SPO- W17«0. OEM PT.F- 19.
FUEL H/C- 1.92(0 STOI F/A« .06(22 L H V= 1(470. S LN T,F« 300.0






)










)


)








)


)


)
DATA POINT NUMBER
PERCENT NAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Ml, RPN
COMPRESSOR INLET TEKP..OEG.F
COMPRESSOR OSCHt. PRES..PSIA
COMPRESSOR OSCHC. TEMP, DEC F
TUR9 INTERSTAGE TEMP., OEG.F
CORR 8ELMTH FLOM. LB/SEC
FA RATIO BASED ON SEt-LMTH.
MEASURED FUEL FLOH, LB/HR
FA .RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P»»N/V/EIT/540)
COMB EFFIC FROM EMISSIONS
CAR30N DIOXIDE
PERCENT BY VOLUME, HEI
LB. COZ PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH. LB./HR.
UN3URNEO HYDROCARBONS* PPM AS
PPM BY VOLUME, HET
L3. PER 1000 L8. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NOI - HEIGHTS AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE (NOZ)
PPM BY VOLUME, NET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
57
5.1
36.1
34. Z
275*0.0
40.0
49.1
317.0
846.0
3. BO
.0100
106.0
.0093
.136
.325
99.203

1.92
3.11
329.9

ZOO. 3
20.637
2.193
CARBON. HEI
61.0'
3.542
.376
.171Z
NOZ
16.3
2.766
.293

6.7
1.137
.121
so
52*.3
49.5
27570.0
40.0
49.6
319.0
908.0
Z.93
.0109
113.0
.0103
.150
.311
99.315

Z.13
3.12
352.1

197.0
18.378
2.077
SHTS AS
54.0
Z.679
.325
.1567

19.3
2.957
.334

6.2
.950
.107
59
7lls
67.7
. 27570.
41.
' 50.
321.
985.
2.89
.0123
1Z5.0
.0112
.165
.302
99.520

2.34
3.13
390.8

174. Z
14.834
1.854
CH4
30.6
1.490
.106
.1004

24.5
3.4Z8
.428

5.7
.798
.100
60
30.0
Z17.7
Z06.
41760.
40.
137.
646.
1094.
7.96
.0090
254.0
.0094
.137
.077
99.818
REDUCED
1.95
3.14
79S.4

61.0
6.249
1.587

6.9
.404
.103
.0646

48. Z
8.106
2.359

13.3
2.237
.568
TOTAL OXIDES OF NITROGEN INCtNOZ) AS NOZ




)


)





PPM BY VOLUME, H£T
LB. PER 1000 1.6. OF FUEL
HEIGHT FLON, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLON
SMOKE NUMBER
CORRECTED HEIGHT FLON
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
SMOKE NUMBER AT HAcO.(23
U/1TEC 4 _ All CMT CCTnuC t*>nOJT>C'MT ffl
23.0
3.903
.414

.0069%
3.50
.02095
3.50
.03492
7.10
.04(97
5.90
5.00
tATTniic A *i*r
Z5.5
3.907
.441

.00700
3.50
.02100
3.50
.03500
4.70
.04900
5,90
4.40
UC » Uft I 1
30. Z
4.Z25
.528

.00700
4.70
.02099
5.90
.03499
5.90
.04699
7.10
5.90
ire-
61.5
10.342
2.627

.00700
3.50
.02124
0.20
.03540
12.90
.04956
17.60
10.70
61
69.7
492.0
465.8
41760.0
40.0
145.1
655.0
1295.0
7.94
.0122
342.0
.0126
.184
.069
99.938
FUEL
RCL HUW«
FIO.L/H*
62
90.3
637.3
603.3
41730.
40.
140.
659.
1419.
7.93
.0139
389.0
.0146
.215
.066
99.962
« AV. HERO. TEST MO.* S
40.00 SPEC HUM* .0020(0
14.160 Si. TIIt-S« 6.5000
63
100. Z
707. J
669.6
41770.0
40.0
150.9
664.0
1474.0
7.96
.0149
420.0
.0153
• 225
.06%
99.969

2.64
3.15
1077.4

28.8
2.185
.747

2.7
.117
.040
.0536

85. Z
10.638
3.630

7.5
.936
.320

9Z.7
11.574
3.958

.00708
3.50
.02124
14.10
.03540
10.00
.04956
21.20
14.50
3.00
3.15
1ZZ6.0

21.9
1.422
.553

1.5
.056
.022
..0392

104.5
11.167
4.344

6.0
.6*1
.249

110.5
11.000
4.593

.00700
5.90
.02126
10.60
.03540

.04947
17.60
12.10
3.2J
3.15
13Z3.9 	 ..

17.0
1.107
.465

1.5
.ass 	 	
. ozz
.0401 ' 	

113.7
^11.603.
4.07J

6.5
.663 	 	
.270

120.2 	 ~
12.266

..- — . 	 . — —
.00700
3.50
.02124
9.40
.03540
15.30 - --.- - 	 --
.04956
10.00
11.90
                                1.  ALL  EMISSIONS CONCENTRATIONS A?£ HET VALUES.
                                2.EQUIVALENCE RATIO CALCULATED FRO* COZ,CO,AND HC DATA AND  FUEL  COMPOSITION.
                                3.MASS  EMISSIONS OF NO, NOZ, AMD KO»NOZ CALCULATED AS NOZ FROM CONCENTRATIONS HITH MOLECULAR HEIGHT OF NOZ  146.011.
-------
                                                               AIRESEARCH EMISSION TEST SUMMARY
                                                              X LACCZ  INST-


                                            „ mma ,.„ „
                                             ,„„„ „«„
                                                                                                                                POHER
                                                                             )


                                                                            h


                                                                             )


                                                                             )
 13
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iQ
 fD
CO
o
                    »I8CR»FT INSTALLATION •••• KFR. 1
                                                                                                    INJ TYPE!  STAGED  SIMPLEX
                    GASEOUS EMISSION TEST NO. •
         MODEL  NO.I
ENGINE INSTALLATION POSITIONI
     TEST DATA SUMMARY ......
         TIHEt
     00.00 PERCENT
SAMPL£ LINE ••• TEMP.t 300.00 BEG. F. FLOH
rrni, ufl
iKBON MONO*
^ i TTrocyu
1 T tl T n
0.0 PPMV
OXIOE!
! OF NITROG

TEST CONDITION
ACTUAL FOMER SETTING, HORSEPOMER
CORR. POKER SETTING (STD DAY), PERCENT RATED
Nl SPEED. RPH
FUEL FLCK (MEAS.I LB./HR.
CORR. ENGINE CORE AIRFLCH (MEASI, LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., OES F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTA^ TEMP., OEG F
TURBINE INTERSTAGE GAS TOTAL TEMP., DEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION, MET ANALYSIS
HYDROCARBON IHC AS CH4), PPMC
CARBON MONOXIDE ICO) , PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPMV
CARSON DIOXIDE (C02), PERCENT BY VOL.
NITRIC OXIDE INO), PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX A3 NOZ)
EMISSION RATE. LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4I
C4R30N MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN INOX AS NOZI
COMBUSTION cFFICIENCr, PERCENT (EMISSIONSI
F/A (EMISSIONS, CALO
64 65 66
35.1 50.5 66.9
5.26 7.56 10.03
37530.00 37540.00 37560.01)
106.0 ..—-
3.0
43.00
14.13
48.72
316.00
850.0
14.11
58.500
198.878
2Z.400
1.954
16.800
3.391
20.166
3.731
.359
Z.138
.395
99.23
.0095
lll.U
2Q
. V
43.00
14.13
49.75
316.00
908.0
14.11
55.500
194.717
Z5.500
2.175
19.700
2.895
17.768
3.8Z2
.324
1.998
.428
99.33
.0105
1Z4.0
2.9
41.00
14.13
50.20
316.00
965.0
14.11
33.000
176.420
29.000
3.401
23.900
1.563
14.620
3.948
.194
1.813
.490
99.52
.0115
67
204.1
30.55
41760.00
254.0
8.0
43.00
14.13
137.28
635.00
1089.0
14.00
6.000
56.014
56.900
1.977
44.000
.347
5.670
9.461
.088
1.440
2.403
99.84
.0095
68
69.52
344.0
8.0
14.13
1272.0
14.01
3.100
23.485
85.000
2.634
78.800
.091
1.788
10.631
.031
.615
3.657
99.95
.0125
69
603.1
90.12
41730.00
394.0
8.0
43.00
14.13
148.92
650.00
1388.8
14.05
1.280
19.846
100.000
3.008
95.750
.046
1.323
10.953
.018
.521
4.315
99.96
.0143
JEN (NOX)I 0.0 PPMV
LENGTHI 50.00 FT.
70
666.9
100.12
41760.00
4Z1.0._
8.0
40.00
14.13 	
151.52
649.08
1436.0
14.07
1.200
16.624
109.508
3.237
105.000
.043
1.830
11.149
.018
.434
4.694
99.97
.0154

-------
(U

(D

M
CO
ENG MF6 t AIRESEARCH TEST FACIL 1 PHX LACC2 INSTR Oc SCRIP 1 FED REG V3I N136
MODEL NO.I TPE331-5-251H S/NI P00001
RATED POWER 1 706.0 SHP AT SEA LEVEL STANDARD DAY
FUEL! ASTM 01655-73 ATOMIC H/C RATIOI
MODE

TIME IN MODE, MINUTES
RATED POWER, PERCENT
CORRECTED POWER, HORSEPOWER
HP-HR
FUEL FLCN, LB/HR
FUEL NASS, LB
** HYDROCARBON EMISSION (HC) "
INOEX, LB HC/1000. LB FUEL
RATE, L8 HC/HR
MASS. LB HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORSEPOWER-HR PER CYCLE
»• CARBON MONOXIDE EMISSIONS (CO) »»
INOEX, LB CO/1000 LB FUEL
RATE, LB CO/HR
MASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORSEPOWER-HR PER CYCLE
*• TOTAL OXIDES OF NITROGEN EMISSIONS (NOX) *•
INOEX, LB NOX/1000 LB FUEL
RATE, LB NOX/HR
MASS, LB NOX
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB NOX/1000 HORSEPOWER-HR PER CYCLE
ENGINE
CONDITIONS
1.928 LHVI
TAXI-IDLE
(IN)
7.000
5.000
35.300
4. 113
105.680
12.329

3.372
.356
. OU2
26.2


20 . 366
3.153
.251
33.6


3.715
.393
.01*6
8.1

TYPE (CLASS) 1

18070. BTU/LB
TAXI-IDLE
(OUT)
19.000
5.000
35.300
11.171
105.680
33.065

3.372
.356
.113
71.2


20.366
2.152
.682
6O.O


3.715
.393
.120
22.1

TURBOPROP

CALC
CALC
TEST
DATE ill-«»-rS
IDt 1
HOI 0


ADDITIVESI NONE . .
APPROACH

0.500
30.000
211.800
15.885
251.673
18.876

.178
.005
.003
2« 1


5.651
1.022
.107
10.0


9.271
2.333
.175
31.0

CLINBOUT

2.500
90.000
635.000
26.075
393.791
16.008

.122
.009
.ODD
.2


1.311
.516
.022
2.0


10.930
0.306
.179
31.8

TAKEOFF

.500
100.000
706.000
5.663
020.008
3.503

.092
.039
.000
.2


1.066
.008
..000
.0


11.161
0.701
.039
6.9

TOTAL PER
CYCLE
33.500


63.501

80.581.

1.870
.260
.158
100.1
2.090

13.586
1.917
1.065
100. «
16.750

6.66S
l.fllfl
.560
100.0
8.872
                                                                                                                                                                     )
                                                                                                                                                                    I)
                                              •• EMISSION  INDEX LEVELS RZQUIREO TO MEET EPA 1979 STANDARDS  FOR  CLASS P2 ENGINES **
                                          EPA LtO-CYCLE
                                   POLLUTANT   L8P/1DOO  HORSEPOWiR-HR-CYCLE
                                      CO        ,     26.6
                                      HC               4.9     _
                                      NOX            12.9
                                                                                                   REQUIRED EMISSION INDEX.  LBP/1000 LB FUEL
POLLUTANT (MODE)
   CO (IDLE)
   HC (IDLE)
   NOX (TAKEOFFI
   A
20.0
 3.0
11.2
   -B
30.3
 6.7_
20.3
                                             A  ASSUMES  PROPORTIONAL REDUCTION OF POLLUTANT EMISSION INOEX AT EACH  LTD CYCLE  HOOE

                                             B  ASSUMES  (1)  REQUIRED REDUCTION IN CO AND HC OBTAINED BY LOWERING EMISSION  INOEX  VALUES
                                                AT  TAXI-IDLE MODE ONLY,  CO AND HC EMISSIONS AT OTHtR MOOES REMAIN UNCHANGED,  (2) REQUIRED
                                                REDUCTION  IN NOX OBTAINED BY LOWERING EMISSION INDEX VALUES AT CLIHBOUT AND TAKEOFF  NODES IN
                                                SAME PROPORTION AS MEASURED VALUES, NOX EMISSIONS AT TAXI-IDLE AND  APPROACH NODES
                                                REMAIN UNCHANGED
-------
01
n>
H
CO
ENGINfc* TPE331-5-2S1M S/N= P0*flfll
RAT SHF* 706. RA EGT.F* loSfl.
1 FUEu H/C= 1.9280 sroi F/As .06822
DATA PCINT NUMBER
PERCENT MAX. CORRECTED POHER
MEASURED SHAFT MpP
t dUKLU inArl HP
co p - *-* *PM
COMPRESSOR OSCHG. PREsJ.PSIA
1 COMPRESSOR DSCHG. TEMP.OEG F
CORR BELMTH FLOH, LB/SEC
FA RATIO BASED ON BELLMTH.
MEASURED FUEL FLOH, uB/HR
EQUIVALENCE**! f*OH EHISSION
LOADING W/P»»N/V/EIT/5*0»
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
' LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
1 PPH BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
i LB. PER 1000 LB. OF FUEL
) HEIGHT FLOH, LB./HR.
RATIO .e MC/LB CO
NITRIC CXIDE (NOI - HEIGHTS AS
) PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
) NITROGEN DIOXIDE .70
3.58
AT
Of
30.6
215.7
20* .1
* 1760.0
*3.0
137.3
635.0
8.01
.0090
25*. 0
.0095
*0?9
99.1.36
RcO'UCEO
1.98
3.1*
798.6
56.0
5.670
l.**0
6. 0
.3*7
.088
.0612
**.o
7.316
1.85.
12.9
2.1*5
.5*5
56.9
9.1,61
2.*03
.00703
*.70
.02118
7.08
.03516
H. 00
15.10
18.38

69?5
*9o!.
*6*.5
H750.0
*3.0
1**.6
7.99
.0123
3*4.0

"fl?4*
99!950
FUEL- AV. KERO. TEST NO.c *
REL HUM= 180.08 SPEC HUM* .085000
FLO.L/M= i«.i60 SL TIN.S- 6.5000

69
636.2
602.1

650.0
1388.0
7.98
.01*1
.01*3
.210
99!965

70
100.1
706.9
666.9
*1760.B
48.0
151.5
649.8
1*36.8
8.81
.01*9
1.21*0
.015*
.225
nee
• uo?
99.972

2.63
3.15
1083.9
23.5
1.788
.615
2. 1
.091
.031
.0511
7. .8
9.655
3.390
6.2
.775
.267
65.0
10.631
3.657
.00705
5.80
.0211*
1*.00
.03516
18.68
.0*923
2*.*8
15.98
3.01
3.15
12*1.8
19.8
1.323
.521
Iy
• £
.0*6
.018
.03*6
95.7
10.*87
*.132
4 X
H. 4
.*65
.1.3
100. 0
10.953
4.315
.00705
5,80
.0211*
11.68
.03516
16.38
.0*923
22.18
14.18
3.2*
3.15
1327. 1_
16.6
1.038
.*3*
.
1.2
.0*3 " "~ "
.018
105.8
10.691
4.501 	 "

,*58
.193
.-.....-- 	 	 	
11.1*9
- *.69* 	 	
.0078*
* 78
.82113
9.38
.03522
15.18
.0*922
28.98
12.78 	 "
Z.tCUIMLENCE RATIO CALCULATED FROM C02.CO,AMD HC DATA AND FUEL COMPOSITION.
3.WASS EMISSIONS OF NO. N02,  AND  NO*N02 CALCULATED AS N02 FROM CONCENTRATION
                                                                                            CONCENTRATIONS  WTH MOLECULAR ' MCX6HT"eF~ NOT
                                                                                                                                            . ill.
                                                                                                                                                                   'ft
-------
                      ..........,.......,.,,......,.*.........,....   AIRESEARCH EMISSION TEST SUMMARY  »»»»»»•»»••»»•
                      ENG MFC t AIRESEARCH            TEST FACIL I PHX LACC2   INSTR DESCRIP I FED REG V38 N136
                      MODEL NO.t      TPE331-5-2MM     S/N1   P04001               ENGINE TYPE (CLASS) I  TURBOPROP
                      RATED POKER!     706.0  SHP AT SEA LEVEL STANDARD DAT  CONDITIONS
                      FUEL! ASTH 01655-73             ATOMIC H/C RATIO!    1.926     LHV1 18470. BTU/LB     ADDITIVES!
 CALC DATE 111-5-75
 CALC IDI    2
TEST NO I     <•
                                                                                                                         NONE
                      ........ £XHAUST  EMISSIONS PER EPA CYCLE OF  WORK  OUTPUT  •• CODE OF FEDERAL REGULATIONS TITLE  40  PART  87  17 JULY 1973  ..»»»..
                                           HYDROCARBONS (CH AS CHI,)           4.435 L8. POLLUTANT PER 1000 HP.-MR. PER CYCLE
                                           CARBON MONOXIDE ICO)              19.653 LB. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                           OXIDES OF NITROGEN  (NOX  AS N02)    8.793 .3. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                           SMOKE                              17.6  SMOKE NUMBER, MAXIMUM AT  CRUISE     HOOE.  70 PERCENT RATED POKER
                      TAXI-IDLE SETTING!  5.0      PERCENT RATED TAKEOFF  PONER  AT 65.       PERCENT RATED TAKEOFF Nl  RPM
 SI)
in
 fD
CO
u>
*) COMB TYPE! REVERSE FLOH ANNULAR P/NI 869082-4 SUR/VOLl 1.260 FUEL
ENGINE TOTAL SERVICE! 0.0 HR TIME SINCE ENGINt OVERHAUL' 0.0 HR 	
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
) AIRCRAFT INSTALLATION *••• MF*. 1 MODEL NO.I
US£RI ENGINE INSTALLATION POSITION!
) GASEOUS EMISSION TEST NO.! 4 DATE! 11-5-75 TIME!
AMBIENT AIR TEMP.! 39.00 DEG. F RELATIVE HUMIDITYI 100.00 PERCEKT
AMBIENT AIR QUALITY HYDROCARBONS (HOI 0.0 PPMC CARBON MONOXIDE (CO)I
SPECIFIC
0.0 PPHV
INJ TYPE!
STAGED SIMPLEX
BARO PRESS.! 28.780 IN.' HGA.
HUMIDITY! .005000 LB. H20/LB. DRY AIR
OXIDES OF NITROGEN (NOX)t 0.0 PPHV
) SAMPLE LINE ••• TEMP.! 300.00 DEG. F. FLOMRATEI 1».16 LlTERS/MIN. TRANSPORT TIME1 6.50 SEC.
) TEST CONDITION
ACTUAL POMER SETTING, HORSEPOWER
CCRR. POMER SETTING (STD DAY), PERCENT RATED
) Nl SPEED. RPH
FUEL FLOW (MEAS.t LB./HR.
CORR. ENGINE CORE AIRFLOW (MESS), LB/SEC
) COMPRESSOR INLET AIR TOTAL TEMP., DEG F
COMPRESSOR INuET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS.. PSIA
) COMPRESSOR DISCHARGE AIR TOTAL TEMP., DEG F
TURBINE INTERSTAGE GAS TOTAL TEMP., DEG F
EXHAUST GAS STATIC PRESSURE, PSIA
) EMISSION CONCENTRATION, HET ANALYSIS
HYDROCARBON (HC AS CH4) , PPMC
CARBON MONOXIDE (CO) , PPMV
) TOTAL OXIDES OF NITROGEN (NOX), PPMV
CARBON DIOXIDE (C02I, PERCENT BY VOL. .
NITRIC OXIDE (NO), PPMV
) EMISSION INDEX, LB. POLLUTANT/1000 L3. FUEL
HYDROCARBONS (HC AS CH4 )
CARBON MONOXIDE (CO)
) TOTAL OXIDES OF NITROGEN (NOX AS NO2)
EMISSION RATE, LB. POLLUTAMT/HR.
HYDROCARBONS (HC AS CH4)
) CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS, CALC)
•
J
. )
71 72 73
33.5
5.02
27540.00
106.0
3.0
40.00
14.13
49.85
308.00
820.0
14.12

100.500
233.298
21. GOO
1.954
13. COO

5.802
23.565
3.584

.615
2.498
.380
98.94
.0095



51.5
7.73
27530.00
114.5
3.0
39.00
14.13
50.34
307.00
895.0
14.12

54.300
196.102
23.200
2.141
17.700

2.876
18.171
i.531

.329
2.081
.404
99.32
.0103



67.0
10.06
27540.00
126.0
2.9
39.00
14.13
50.59
309.00
955.0
14.12

40.500
183.703
27.000
2.287
21.300

2.012
15.970
3. 856

.254
2.012
.486
99.45
.0110



74
199.7
29.96
41740.00
258.5
8.0
40.00
14.13
138.26
630.00
1065.0
14.02

9.000
65.235
53.900
1.931
40.500

.533
6.755
9.169

.138
1.746
2.370
99.79
.0093



75
467.6
70.30
41740.00
352.0
8.0
38.00
14.13
144.89
639.00
1132.0
14.03

2.700
30.399
84.300
2.645
78.200

.117
2.305
10.498

.•41
.811
3.695
99.9k
.0126



76
604.1
90.73
41750.00
410.0
0.0
39.00
14.13
150.54
644.00
1348.0
14.06

1.200
23.079
98.750
3.631
93.750

.84*5
1.527
11.733

.016
.611
4.293
99.96
.01*4)



LENGTH! 50.00 FT.
77
669.2 	
100.50
41730.00
425.5 . _
8.0
39.00
14,13
152.26
646.00
1420.0
14.08

.600
22.271
107.000
3.231 . _
101.500

.021 	
1.383
10.911
. ._
.009
.588
*.6fc3
99.97
.0153



-------
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•)
•)






FUEL. AST$ 01655-73* ^TOMC^X'S""^^""""?.™! 18*70. BTU/L8 ADDITIVES. NONE*"* "Ol *
)
)
~l
1
)
)

)


)
1
14 0 0 E
TIME IN MODE, MINUTES
RATED POWER, PERCENT
CORRECTED POKER, HORSEPOWER
HP-HR
FUEL FLCN, LB/HR
FUEL NASS, LB
•* HYDROCARBON EMISSION (HC) ••
INDEX, LB HC/1000 LB FUEL
RATE, LB HC/HR
HASS, LB HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORSEPOWER-H3 PER CYCLE
•• CARBON MONOXIDE EMISSIONS  REQUIRED
                                               S^IiJISnSfJS'.S8!^™ 31f  L01*«If(6  "ISSION INDEX VALUES AT CLIM30UT AND T«EOFF HoolS IN
                                               SANc PROPORTION AS MEASURED VALUES,  NOX  EMISSIONS  AT TAXI-IDLE AND APPROACH NODES
-------
 p)
i£)
 (D
oo
Ui
ENGINE' TPE331-5-Z51M S/N- P0*001 COMB P/N' 869082-1,
RAT SHP= 706. RA EGT.F:
FUEL H/C* 1.9280 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POKER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Nl, RPM
COMPRESSOR INLET TEMP..OEG.F
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR OSCHG. TEMP.DEG F
TUR8 INTERSTAGE TEMP., DEG.F
CORK 3ELMTH FLOH, LB/SEC
FA RATIO BASED ON BELLMTH.
MEASURED FUEL FLOH, LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P»»N/V/EIT/5*0)
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, NET
LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NO) - HEIGHTS AS
PPM BY VOLUME, MET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH. LB./HR.
NITROGEN DIOXIDE IN02J
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
1650.
.06822
71
5.0
35.5
33.5
2751,0.0
1,0.0
1.9.9
308.0
820.0
3.01.
.0099
106.0
.0095
.139
.326
98.937

1.95
3.10
3Z8.7

Z33.3
23.565
2.1.98
RAT SPD
L H V
72
7.7
51.6
51.5
27530.0
39.0
50.3
307.0
895.0
2.98
.0109
111,. 5
.0103
.151
.316
99.320

2.1",
3.12
357.0

196.1
18.171
2.081
CARBON, HEIGHTS AS
100.5
5.802
.615
.21.62
NOZ
13.0
Z.157
.229

8.6
l.<>27
.151
51.. 3
Z.876
.329
.1583

17.7
2.691.
.308

5.5
.837
.096
= 1,1730.
« 16*70.
73
10.1
71.0
67.0
27 51. 0.0
39.0
50.6
309.0
955.0
2.92
.0122
126.1
.0110
.161
.305
99.1.1,8

2.29
3.12
393.6

183.7
15.970
2.012
CHi,
1.0.5
Z.01Z
.251)
.1260

21.3
3.01,2
.383

5.7
.811,
.103
OEH PT,F« 1.0.
S LN T,F= 300.0
71,
30.0
211.6
199.7
1.171.0.0
1,0.0
138.3
630.0
1065.0
8.01
.0092
Z58.5
.0093
.136
.079
99.79*
REDUCED
1.93
3.H.
81Z.2

65. Z
6.755
1. 7*6

9.0
.533
.138
.0789

1.0.5
6.889
1.781

13.*
2.279
.589
75
70.3
1.96.3
*67.6
1.171.0.0
38.0
1**. 9
639.0
1132.0
7.97
.0125
352.0
.0126
.185
.072
FUEL' AV. KERO. TEST NO.' *
REL HUM'
FLO.L/M'
76
90.7
6*0.5
60*. 1
1.1758.0
39.0
150.5
6**.0
13*0.0
1.10
.01*2
1.00.0
.01**
.211
.067
99.936 99.960
100.00 SPEC HUH' .005101
1*.160 SL TIM.S- 6.5010
77
100.5
709.5
669.2
1.1730.1
39.0
152.3
6*6.1
1*20.0
7.99
.0151
1.25.5
.0153
.225
.065
99.966

2.6*
3.15
1108.8

30.*
Z.305
.811

Z.7
.117
.0*1
.0508

78.2
9.738
3.1.28

6.1
.760
.267
3.03
3.15
1260.6

23.1
1.5Z7
.611

1.2
.0*5
.818
.0297

93.8
10.190
*.076

5.0
.5*3
.217
3.23
3.15
13*1.1

22.3
1.383
.588

.6
.021
.009
.015* 	 	 	 	

101.5
10.352 	


5.5
.561
.239
TOTAL OXIDES OF NITROGEN (NC+NOZ) AS NOZ
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
SMOKE NUMBER AT HA*O.OZ3
21.6
3.581.
.380

.00695
2.30
.02081
7.10
.031.68
5.80
.01.856
I..7D
5.00
•^•TTrtkje nor
23.2
3.531
.UOl.

.00690
1.20
.02069
3.50
.031.1.3
5.81
.01.820
7.00
<>.51
uc r if AI
Z7.0
3.856
.1,86

.00697
1.20
.02092
5.80
.031,86
5.80
.01.881
7.00
5.00
lit «•
53.9
9.169
2.370

.0070*
*.70
.02113
10.50
.03521
I*. 00
.0*938
18.60
12.10
8*. 3
10.1.98
3.695

.00706
7.60
.02119
11.. 00
.03531
23.30
.0*9**
25.60
17.60
98.8
10.733
•,.293

.00708
*.70
.02123
11.60
.03538
19.80
.0*953
2*. 1.0
15.30
107.1
10.913


.01707
*.70
.OZ1Z2
10.51
.03537
17. *0
.0*952
20.91
13.51
                       NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE MET VALUES.

                             2.EQUIVALENCE  RATIO  CALCULATED FROM COZ.CO.AND HC  DATA AND FUEL

                             3.MASS EMISSIONS OF  NO,  NOZ, AMD NO»NOZ CALCULATED AS NOZ FROM
 COMPOSITION.

CONCENTRATIONS HITH
                                                                                                                   MOLECULAR  HEIGHT  OF  NOZ (1.6.01).
-------
                       ENS MFG  t  AIRESEARCH
                          ....................  «IRES£ARCH EMIssioN TEST  SUMMARY   »•»•»»

MODEL NO.,^   ™331-S.«»   /^•"p,:.™ L*C"  »»« «««P  . FED  R£6 V30  N1I6

           01655-73            ATOMIC  H/C RATIO!   1.928
                                                                                           18<>70.  BTU/LB
                                                                                                             ADDITIVES!  NONE
                                                                                                                              CALC DATE «ll-5-75
                                                                                                                              CALC ID!    3
                                                                                                                             TEST NO!    *
                                EXHAUST  E««IONS PER EPA CYCLE OF KOR< OUTPUT " CODE  OF  FEDERAL  REGULATIONS TITLE 40 PART 87  17 JULY 1973

                                                                              3'091
                                                                                         P°LLUTAI" PER 1000  HP.-HR.  PER CYCLE
                                            SMOKE
                       T4XI-IOLE SETTINGI  5.0
                                                                       N02,
                                                    PERCENT  *AT£0 TAKEOFF POKER AT 65.
                                                                            ER 1000 HP.-HR. PER
                                                       16.2  SMOKE NUMBER, MAXIMUM AT  CRUISE     MODE,   70  PERCENT RATED POWER
                                                                     PERCENT RATED TAKEOFF Nl RPM
 •fl
 (U
iQ
 0)
CO
                       COMB TYPE I REVERSE  FLOW  ANNULAR
                       ENGINE TOTAL SERVICEI  0.0        HR
                       ENGINc ASSEMBLY AND MAINTENANCE  INFORMATION:
                       AIRCRAFT  INSTALLATION  •••• HFR.I
                                                  USERI
                                        .............  tnGINL DESCRIPTION  »••»»•»»»...»»...»...........»...•...»...

                                        TIME^NCE'EN'GI'NE'WRHAU,,  1%™' ^  FUEL INJ TYPE'   STA6EO  ™™
                                                                  MODEL NO.I
GASEOUS EMISSION TEST NO. 1 4 DATcl 1
TEST CONDITION
ACTUAL POWER SETTING, HORSEPOWER
CORR. PCHER SETTING (STO DAfl , PERCENT RATED
Nl iPlED, RPM
FUEL FLCM (MEAS.) LB./HR.
CORR. EKGINE CORE AIRFLOW (MEAS), LB/SEC
COMPRESSOR IN..ET AIR TOTAL TEMP., OEG F
CCMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAu PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTA^ TEMP., DEC F
TURBINE INTERSTAGE GAS TOTAL TEMP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSIOK CONCENTRATION, MET ANALYSIS
HYDROCARBON (HC AS CH4) , PPMC
CARBON MONOXIDE (CO) , PPMV
TOTAL OXIDES OF NITROGEN (NOXI, PPMV
CARBON DIOXIDE (C02), PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSIOK INDEX, LB. POLLJTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4I
CARSON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS NO2>
EMISSIOK RATE, L3. POLLUTANT/HR.
HYDROCARBONS (HC AS CM4)
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS N02)
CCM3USTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS, CALC)
•OPERATIONAL
E HUMIOITYI
PPMC Cl
TIME
IRBON HONOX
.6 L. IT £ xS/H
i SUMMARY *
1
IDE (COX
78 79 80
33.5 49.6 65.7
5.05 7.45 9.87
27580.00 27530.00 27510.00
103.0 113.0 127.0
3.1 *.n 9 o
37.00
soeioo
826.0
14.12
70.500
216.165
£1.200
1.917
13.300
4.157
22.298
3.592
.428
Z.297
.370
99.11
.0093
39.00
50.59
308.00
887.0
51.300
202.590
24.700
2.099
18.000
2.771
19.148
3.835
.313
Z.164
.433
99.31
.0101
39.00
14.14
50.59
308.00
947.0
14.12
40.500
187.820
28.000
2.311
22.000
1.991
16.152
3.955
.253
2.051
.502
99.45
.0111
0*0 PPMV
ANSPORT TI
81
20D.8
30.18
41750.00
264.0
38.00
14.14
138.76
630.00
1060.0
14.02
7.500
64.39*
56.300
1.949
41.300
.440
6.607
9.488
.116
1.744
2.505
99.81
.0093
MEI 6.5
82
466.8
70.24
41710.00
356.0
37.00
14.14
146.61
637.00
1260.0
14.03
.900
25.107
67.000
2.623
76.200
.039
10.924
.014
.683
3.889
99.95
.0125
OF NITROG
0 SEC.
83
601.4
90.31
41770.00
405.0
8.0
39.00
14.14
150.54
646.00
1336.0
14.07
.600
20.653
99.250
3.031
91.250
.023
1.367
10.760
.009
.554>
4.369
99.97
.0144
10 IN. HGA.
.8. H2G/LB. DRY ATI
.EN (NCXX 0.0 PI
LENGTHI 50.00 1
84
669.3
100.41
41750.00
431.0
8.0
40.00
14.14
152.75
649.00
1431.0
14.00
.600
20.249
106.250
3.225 ...
100.000
.021 -
1.260
10.657
.009
.543
4.679
99.97
.0153
-------
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CO
                         .,..,,..»»..,.».,,,....,...,,,..,,.»»,...»  EpA CYCv_£ EHISSIONS  COMPUTATION SUMMARY  •»»»•»»•••
                         ENS MF6 I  AIRESEARCH           TEST FACIL  « PHX LACC2   INST*  OtSCRIP I  FED RES V38 N136
                         MODEL NO.I     TPE331-5-251M     S/NI   P04001              ENGINE  TYPE(CLASS)I  TURBOPROP
                         RATED FOHERI    706.0 SHP AT SEA LEVEL STANDARD DAY CONDITIONS
                         FUEL! ASTM 01655-73            ATOMIC H/C  RATIO!   1.928      LHVI 18470.  BTU/LB     ADDITIVES!
                                                                               CALC DATE 111-5-75
                                                                               CALC 101    3
                                                                              TEST NOt    4
                                                                                                                          NONE
MODE
TIME IN MODE, MINUTES
RATED POWER, PERCENT
CORRECTED POWER, HORSEPOWER
HP-HR
FUEL FLCH, LB/HR
FUEL MASS, LB—
•» HYDROCARBON EMISSION (HO »»
INDEX. LB HC/1000 LB FUEL
RATE, LE HC/HR
MASS. LS HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORSEPOHER-HR PER CYCLE
•* CARBON MONOXIDE EMISSIONS (CO) ••
INDEX, LB CO/1000 LB FUEL
RATE, L6 CO/HR
MASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE. LB CO/1000 HORSEPOHER-HR PER CYCLE
** TOTAL OXIDES OF NITROGEN EMISSIONS (NOX) *•
INDEX, LB NOX/1000 LB FUEL
RATE, LB NOX/HR
MASS. LB NOX
MASS, PERCENT OF TOTAL CYCLE
CYC.E, LB NOX/1000 HORSEPOWER-HR PER CYCLE
TAXI-IO.E
(IN)
7.000
5.000
35.300
4.118
102.856
12.000

4.191
.431
.050
25.6


22.356
2.299
.268
23.2


3.584
.369
.043
7.6

TAXI-IDLE
(OUT)
19.000
5.000
35.300
11.178
102.856
32.571

4.191
.431
.136
69.5


22.356
2.299
.728
63.1


3.584
.369
.117
20.6

APPROACH
4.500
30.000
211.800
15.885
263.106
19.733

.454
.120
.009
4.6


6.631
1.745
.131
11.3

""" • "~
9.420
2.478
.186
32.8

CLIMBOUT
2.500
90.000
635.400
26.47S
404.271
16.845

.037
.015
.001
.3


1.359
.549
.023
2.0

_. 	 . 	
10.744
4.343
.181
32.0

TAKEOFF
.500
100.000
706.000
5.883
429.690
3.581

.015
.006
.000
.0


1.292
.555
.005
.4

- 	 	
10.965
4.711
.039
6.9

TOTAL PER
CYCLE
33.501


63.541

04.729

2.318
.352
.196
100.0
3.091

13.629
2.068 ~
1.155
100.0
18.175
	 .
6.679
1.013
.566
100.0
8.906
                                               »• EMISSION  INDEX  LEVELS RtUUIREO TO MEET EPA 1979 STANDARDS FOR CLASS P2  ENGINES  ••
                                           EPA LTO-CYCLE
                                                                                                    REQUIRED EMISSION INDEX. L8P/1000  LB FUEL
                                    POLLUTANT
                                       CO
                                       HC
                                       NOX
LBP/1000 HORSEPOHER-HR-CYCLE
      26.0
                                                      12.9

POLLUTANT (MODE)
CO (IDLE)
HC (IDLE)
NOX (TAKEOFF)

A
22.4
*.Z
11.0

B
34.7
• 6.1
23.6
                                                                                                                                                                      y
                                              A  ASSUMES  PROPORTIONAL  REDUCTION  OF  POLLUTANT EMISSION'INDEX AT EACH LTO CYCLE HOOE

                                              B  ASSUMES  (1) REQUIRED  REDUCTION  IN  CO  AND HC OBTAINED BY LOWERING EMISSION INDEX VALUES
                                                 AT TAXI-IDLE  NODE  ONLY,  CO  AND  HC  EMISSIONS AT OTHER MOOES RIMAIN UNCHANGED, (2) REQUIRED
                                                 REDUCTION  IN  NOX OBTAINED BY  LOHE1IN1 EMISSION INDEX VALUES AT CLIMBOUT AND TAKEOFF MOOES  IN
                                                 SANE PROPORTION AS MEASURED VALUES, NOX  EMISSIONS AT TAXI-IOtE AND APPROACH MOOES
                                                 REMAIN UNCHANtED
-------
13
PJ
M BY VOLUME, WET
LS. PER 1000 LB. OF FUEL
WEIGHT FLOW, LB./HR.
RATIO ..B HC/L8 CO


S/N* P04001 COMB P/N= 869082-4 FUEL* AV. KERO. TEST H0.= 4
1650. RAT SP3 = 41730. DEW PT.F* 40. RE.. HUH* 100.00 SPEC HUH* .005000
.06822
78
5.0
35.6
33.5
Z7580.0
37.0
50.4
306.0
826.0
3.07
.0095
103.0
.0093
.1X6
.324
99.111

1.93
3.11
320.1

Z16.2
33.398
Z.297
L H V=
79
7.5
52.
49.
27530.
39.
50.
308.
887.0
2.99
.0107
113.0
.0101
.149
.313
99.306

3.10
3.13
352.1

303.6
19.148
3.16".
CARBON. WEIGHTS AS
70.5
4.157
.428
.1864
51.3
Z.771
.313
.1447
18470. S LN T.Fs 300.0
80
9.9
69.7
65.7
27510.0
39.0
50.6
308.0
91.7.0
2.95
.0122
127.0
.0111
.163
.309
99.445

2.31
3.12
396.6

187.8
16.152
3.051
CH4
40.5
1.991
.253
.1233
81
30. Z
313.1
zoo. a
1.1750.0
38.0
138.8
630.0
1060.0
8.01
.0093
Z64.0
.0093
.137
.079
99.806
REDUCED
1.95
3.14
829.6

64.4
6.607
1.744

7.5
.440
.116
. .0666
83
70. Z
495.9
466.8
41710.0
37.0
146.6
637.0
1260.0
8.01
.0136
356.0
.0135
.183
.071
99.951
EMISSION
3.63
3.15
1121.7

35.1
1.919
.683

.9
.039
.014
.0305
FLO.L/H*
83
90.3
637.6
601.4
41770.0
39.0
150.5
646.0
1336.0
8.02
.0143
405.0
.0144
.211
.067
99.966

3.03
3.15
1276.5

20.7
1.367
.554

.6
.023
.009
.0166
14.160 SL TIH.S* 6.5000
84
100.4
708.9
669.3
41750.
40.
153.
649.
1431.
8.00
.0153
431.1
.0153
.224
.064
99.968

3.ZZ
3.15
1358.5 	 	

30. Z
1.261
.543

.6 .._._..._
.021
.009
.0169 _
NITRIC OXIDE (NO! - WEIGHTS AS NOZ
: i


i


)


i


)


)


j


PPH 3Y VOLUME, WET
11. PER 1000 LB. OF FUEL
WEIGHT FLOW, LB./HR.
NITROGEN DIOXIDE 
-------
00
10
                      •*»•*.•»«*»•»*•»••••*••**»••*•»•»••*•»»•»••  AIRESEARCH EMISSION  TEST  SUMMARY   •••••••••••••«
                      ENG MFG I AIRESEARCH            TEST FACIL I PHX LACC2  INSTR OESCRIP  I FED REG V38 N136 '
                      MODEL NO. I     TPE331-S-251M      S/NJ   P0
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CM4)
i CARBON MONOXIDE (CO)
TCTAL OXIDES OF NITROGEN (NOX AS N02)
COM9U3TION EFFICIENCY, PERCENT (EMISSIONS*
i F/A (EMISSIONS, CALCI
85 86 67
36.0
5.29
27550.00
106.0
2.9
59.80
14.12
lib. 66
337.00
915.0
14.11

",5.000
192.87*.
26.100
2.056
19.500

2.462
18.615
it.138

.266
2.010
.447
99.31,
.0099
".8.8
7.16
275i>0.00
119.0
2.9
59.00
lit. 12
1.7.25
337.00
960.0
14.12

33.000
180.966
30.700
2.238
23.500

1.676
16.080
it. 1.81

.199
1.911.
.533
99.47
.0108
67.9
9.98
27500.00
125.0
2.8
59.00
lit. 12
1.7.25
336.00
1036.0
lit. 13

26.200
161.. 680
31.. 600
2. 514
28.000

1.277
13.051
it. 50*

.160
1.631
.563
99.58
.0121
68
204.0
29.99
41730.00
251.0
7.8
59.00
14.12
130.65
661.00
1111.0
14.04

6.600
60.617
62.600
1.959
46.100

.385
6.192
10.503

.097
1.554
2.636
99.62
.0094
89
475.1
69.86
41730.00
344.0
7.7
59.00
14.12
137.38
677.00
1338.0
14.06

3.001
27.546
100.000
2.714
90.000

.127
2.035
12.136

.044
.700
4.175
99.94
.0129
90
613*4
90.20 '
41730.00
396.0
7.7
59.00
14.12
140.77
682.00
1460.0
14.09

2.700
16.223
122.500
3.154
112.000

.096
1.032
12.601

.039
.409
5.D69
99.97
.0150
LENGTH! 50.0
91
680.3
100.04
41730.01
421.0
7.7
59.00
14.12 	
ll>Z.44
684.00
1516.0
14.10

2.700
16.223
132.750
3.389 . .
122.000

.,.091
.960
12.911

.038
.404
5.435
99.97
.0161
-------
o
vo
o
aury.—ss,.™.   ™F£:» — ^sss^rar-s
RATED PCWERI    706.0 SHP AT  S£A LEVEL STANDARD DAY  	        TYPclCLASSM
FUELI ASTM D 1655-73          ATOMIC H/C RATIOI  1.928
                                                                        LHVI 18*70. BTU/LB
                                                                                             ADDITIVESI  NONE
                                                                                                            CALC DATE  110-26-75
                                                                                                            CALC 101   1
                                                                                                           TEST NOt 5
)
1
1

;
)

)

)
i
NODE
TINE IK MODE. MINUTES
RATED FCMEft, PERCENT
CORRECTED POM£R, HORSEPOWER
HP-MR
FUEL FLOW, LB/HR
FUEL MASS, LB
•• HYDROCARBON EMISSION 
-------
 ftl
iQ
 (D
\

)

1














)

)










ENGINE' TPE331-5-251M
RAT SHP- 706. RA E6T,F*
FUEL H/C= 1.9280 STOI F/A*
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Nl , RPM
COMPRESSOR INLET TEMP..DEG.F
COMPRESSOR OSCHG. PR£S.,PSIA
COMPRESSOR OSCHG. TEMP.OEG F
TURB INTERSTAGE TEMP., BEG.F
CORR 3ELMTH FLOH. LB/SEC
FA RATIO BASED ON BELLMTH.
MEASURED FUEL FLOH, LB/HR
FA RATIO CA.C. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P"N/V/E«T/5*0>
COM3 EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
LB. C02 PER LB. OF FUEL

HEIGHT FLOH» LB»XHR*
CARBON MONOXIDE
PPK BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNED HYDROCARBONS- PPM AS
PPK BY VOLUME, HcT
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
S/N= P8*001
COHB P/N= B69082-* FUEL* AV. KERO. TEST N0.= 5
0. RAT SPD:
.06822
85
5.3
37.*
36.0
L H V:
86
7.2
50.7
1.8.8
27550.0 275*0.0
59.0
*6.7
337.0
915.0
2.89
.0108
108.0
.0099
.1*5
.32*
99.3**

2.06
3.12
336 7

192.9
19.615
2.010
59.0
".7.2
337.0
960.0
2.86
.0128
119.0
.0108
.158
.313
99.*75

2.2*
3.12
371.8

181.0
16.080
1.91*
CARBCN, HEIGHTS AS
*5.0
2.*82
.268
.133*
33.0
1.676
.199
.10*2
= *1730. DEH PT,F=
= 18*70. S
87
10.0
70.5
67.9
27500.0
59.0
"•7.2
336.0
1038.0
2.78
.0130
125.0
.0121
.177
.306
99.581

2.51
3.13
391 .3

16*. 7
13.051
1.631
CH*
28.2
1.277
.160
.0979
LN T,F=
68
30.0
211.8
20H.O
1.1730.0
59.0
130.6
661.0
1111.0
7.82
.0093
251.0
.009*
.138
.079
99.821
REDUCED
1.96
3.1*
789.0

60.6
6.192
1.55*

6.6
.385
.097
.0622
19.
300.0
89
69.9
*93.2
1.75.1
*1730.0
59.8
137.*
677.0
1338.0
7.70
.0129
3*1.. 0
.0129
.189
.070
99.9*1
EMISSION
2.71
3.15
1063.8

27.5
2.035
.700

3.0
.127
.0**
.0623
REL HUM'
FLO,L/M=
90
98.2
636.8
613.*
*1738.0
59.0
1*0.6
682.0
1*60.0
7.67
.01*9
396.0
.8150
.220
.066
99.967

3.15
3.15
12*8.3

16.2
1.032
.*09

_2.7
.098
.039
.0951
NITRIC OXIDE INO) - HEIGHTS AS N02



)

)


.


)


)


)


)
J
PPM BY VOLUME, HET

LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE (N02I
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEi.
HEIGHT FLOH. LB./HR.

PPK BY VOLUME, NET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMCKE MEASUREMENT DATA
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLCH
SMCKE NUMBER
SMOKE NUMBER AT HA=8.023
19.5

1 33*
6t
• D
1.0*6
.113
N02I AS N02
26.1
*.136
.**7

.00701
2.30
.8210*
3.50
.03507
5.69
.0*906
9.30
5.38
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE
2. EQUIVALENCE RATIO CALCULATED FROM
3. MASS EMISSIONS OF NO, N02, AND NO


23.5
3 **30
,*08
7 2
1.051
.125

30.7
*.*81
.533

.00700
2.30
.02100
2.38
.03505
7.00
.0*916
9.30
5.30
28.0
3 6^*5
.1.56
6 6
.859
.107

3*. 6
*.50*
.563

.0071*
2.30
.1121*6
*.70
.93569
*.70
.0*997
7.00
*.70
1.9.1
6.070
2.026
1*.5
2.<.33
.611

62.6
10.503
2.636

.00713
2.30
.021*0
10.50
.03566
11.. 00
.0*991
19.80
11.70
HET VALUES.
C02,CO,AND HC DATA AND FUEL
*N02 CALCULATED AS 1402 FROM



90.0
10.922
3.757
10.0
1.21*
.*17

100.0
12.136
*.17S

.00715
5.80
.021*3
11.60
.03565
17. *0
.0*991
25.60
15.20
112.0
11.70*
It. 635
10.5
1.097
.*35

122.5
12.801
5.069

.0071*
5.80
.021*2
10.58
.03570
1*.00
.05008
22.10
13.10
COMPOSITION.
CONCENTRATIONS MITH


20.00 SPEC HUM* .ODZOII
1*.160 Si. TIH.S* 6.5000
91
100.0
706.3
bSO.3
*1730.0
59.0 	 	
1*2.*
66*. 1
1516.0 . . .
7.67
.0158
*21.l . . .
.0161
.236
.06*
99.969
	 	
3.39
3.15
1327.1 . _ 	

16.2
.968_ .. _ . 	 	 	 	
.*0*

	 2.7 	 ..... 	 — _.. . ._
.091
.038
.0951 	 . 	 	

122.1
11.869 _ . 	
*.99S
10.7 . . 	 ..
1.0*5
.**•

132.7
12.911
._ _5.*35 	 	 	

.00715
5.80 	 . . 	 	 	 	
.02151
10.50
.03583 . . 	 - 	
16.60
.05016
20.90 . . . - -
l*.0fl
MOLECULAR HEIGHT OF N02 1*6.011.

1 ^\

•\
)

-.
'

^
'




..
'

)

•v
•*

..
•*
- -
^


\
j

•*
'

j

)'


)'

-' 	


- - -
)'

. _ , _ - '•
)
' 9
..- .- ...'
* \
: J
)

-------
,.... „,   ..„ „  «•••••»«•••••»••••»•••«•••••  AIRESEARCH EMISSION TEST SUMMARY  .........

MmFr So ,     «?«.  *  ,c.    TEST  FACIL  '  PHX LAC"  INSrR DESCRIP  I FED REG V38 N136
MODEL NO.I     TPE331-5-2S1M      S/NI    P04001              ENGINE TYPEICLASSII TURBOPROP
                706.0  SHP AT  S£A  LEVEL  STANDARD DAY CONDITIONS
RATED POWER!
                         FUEL I ASTM  D16S5-73
                                                         ATOMIC H/C .RATIOJ   1.928
                                                                                        LHVt  18470.  BTU/LB
                                                                                                               ADDITIVES!  NONE
                                                                                                                                CALC DATE 110-27-75
                                                                                                                                CALC IDI  2
                                                                                                                               TEST NOI  5
 )



 )



1)
                                   EXHAUST  £HI
                           -n    ,
                           MONOXIDE  (COI
                    OXIDES OF NITROGEN  (NOX  AS N02I
                                                                        *  °UTPUT     COOE  OF  Feo£RSl-  PECULATIONS  TITLE 40 PART 87  17 JULY 1973
                                                                                Z-Z89 L8>  POLl-UTA''T PL* 1000  HP.-HR.  PER CYCLE
                                                                               16.026 LB.  POLLUTANT PER 1000  HP.-HR.  PER CYCLE
                                                                                9.944 LB.  POLLUTANT P£R 1000  HP.-HR.  PER CYCLE
                          TAXI-IDLE  SETTING,
                                                      PERCENT RATED TAKEOFF
                                                                                                                                  "
                                                                                                                                             """
                                                                                                                               STAGED SIMPLEX
(D
to
[[[  ENGINE DESCRIPTION  »•••»»»».»»»»».»».»»».»»<
COMB TYPE! REVERSE FLOW ANNULAR            P/N»    869082-',           SUR/VOLI 1.260  FUEL INJ TYPEI
ENGINE TOTAL SERVICE*  0.0       HR     TINE  SINCE ENGINE OVERHAOLI  0.0       HR
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION I
AIRCRAFT INSTALLATION •••• MFR. I                                  MODEL NO.t
                           USERI                        ENSINE INSTALLATION POSITIONI


                                                                                           BARO PRESS.I  28.730  IN.  HGA.
                                                                                      FIC HUMIDITY!   .002000 L8. HZO/LB.  DRY  i
                                                                                                                               PPMV
GASEOUS EMISSION TEST NO. 1 5 DATEl 10-27-75 TIMEl BARD PRESS i ?g 7sn TM MC»
AMBIENT AIR TEMP.I 59.00 OEG. F RELATIVE HUMIDITY! 20.00 PERCENT SPECIFIC HUMIDITY! .002000 L8. H20/LB" DRT All
^Mpf^liF «ALTPMP , H™n0£2R^S I"'" °-° PPMC CAR8°N MON°XIOE 
99.30
.0098
51. J.
7.57
27560.00
119.0
2.8
59.00
14.11
<>7.00
338.00
978.0
14.07
29.100
177.782
30.1.00
2.287
2U.100
1.M.7
15.1.67
<>.3l»
13.981.
<>.62<>
.121
1.662
.592
99.61
.0122
95
20V. 0
30.09
4171,0.00
255.0
7.8
59.00
14.11
131.63
661.00
1110.0
14.00
8.700
62.714
61.200
1.959
48.000
.508
6.404
10.266
.129
1.633
2. 618
99.80
.0094
96
475.8
70.19
41750.00
347.0
7.7
59.00
14.11
138.02
672.00
1335.0
14.01
2.700
25.919
99.750
2.677
90.250
.116
1.942
12.276
.(41
.674
4.260
99.94
.0127
97
612.3
90.32
41740.00
396.0
77
. f
59.00
14.11
142.34
680.00
1450.0
14.05
1.800
21.057
110.750
3.095
115. 000
.067
1.365
12.642
.026
.540
5.006
99.96
.0147

96
680.5
100.38
41740.00
425.0
7.7
59.00
14.11
143.07
682.01
1512.0
14.06
2.100
15.821
130.000
3.333 .
123.000
.072
.952
12.852
.031
.405
5.462
99.97
.0158
                                                                                                                                             )

                                                                                                                                             >

                                                                                                                                             )

                                                                                                                                             )

                                                                                                                                             )

                                                                                                                                             )

                                                                                                                                             )•

                                                                                                                                             )

                                                                                                                                             )

                                                                                                                                            ')

-------
                                                                                                                                                                    t-
13
H
vo
00
                      »,*,,.**•.*.>.•**•<>»»»**•*»»••»»••»*»»**»*  EPA CYC.t EMISSIONS COMPUTATION  SUMMARY   •••»'
                      ENG NFG  « AIRESEARCH           TEST  FACIL « PHX LACCZ  INSTR DESCRIP  i  FED REG  V38 MIS&
                      MODEL NO.t      TPE331-5-251N     S/NI   P00001              ENGINE  TYPE«CLASS)I  TURBOPROP
                      RATED POHERa     706.0  SHP  AT SEA  LEVEL STANDARD DAY CONDITIONS
                      FUEL* ASTH  01655-73            »TO«IC H/C RATIOI   1.926     i-rtV» 18070.  BTU/L8
                 CALC DATE 110-27-75
                 CALC IDI  2
                TEST NOt  5
I)
ADDITIVES I  NONE
MODE TAXI-IO-E TAXI-IDLE APPROACH
) (IN) (OUT)
TIME IN MODE, MINUTES
RATED POWER, PERCENT
CORRECTED POKER, HORSEPOHER
HP-HR
7.000 19.000 0.500
5.000 5.000 30.000
35.300 35.300 211.800
H.118 11.178 15.885
FUEL FLOW. LB/HR 106.025 106.025 Z50.090
FUEL MASS. LB 12. «0 33.57, 19.057
•• HYDROCARBON EMISSION (HCI ••
INDEX, LB HC/1000 LB FUEL
RATE, LB HC/HR
1 MASS, LB HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORSEPOHE3-HR PER CYCLE
•• CARBON MONOXIDE EMISSIONS (CO) *•
INDEX, LB CO/1000 LB FUEL
RATE. LB CO/HR
MASS. LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORSEPOWEU-HR PER CYCLE
»» TOTAL OXIDES OF NITROGEN EMISSIONS «NOX) ••
INDEX. LB NOX/1000 LB FUEL
RATE, LB NOX/HR . .._
MASS, LB NOX
MASS, PERCENT OF TOTAL CYCLE
•» EMISSION INDEX LEVELS REQUIRED
EPA LTO-CYCLE
POLLUTANT L3P/1000 HORS£POHER-HR-CYCi.E
) CO 26. 8
HC *«9
NOX 12.9
A ASSUMcS PROPORTIONAL REDUCTION
B ASSUMES (1) REQUIRED REDUCTION
Z.918 2.916
.309 .309
.036 .098
20. 8 67.0

18.9*9 18.909
Z.009 2.009
.230 .636
23.0 6Z.5

3.998 3.998
.020 .OZO
.009 .130
7.8 21.2
TO M£ET EPA 1979 STANDARDS
.517
.131
.010
6.8 .

6.005
1.628
.122
12.0

10.200
2.603
.195
30.9
FOR CLASS
REQUIRED EMISSION
POLLUTANT (MODE)
CO (IOLE1 .
HC
NOX
(IDLE)
(TAKEOFF)
OF POLLUTANT EMISSION INDEX AT EACH
IN CD AND HC OBTAINED BY L
CLIMBOUT TAKEOFF TOTAL PER
CYILE
2.580 .500
90.000 100.000
635.000 706.000
26.075 5.883
393. 66O 027.301
16.003 3.561
.068
.030
.001
l.i

1.329
.523
.022
2.1

12.628
0.971
.207
32.8
>2 ENGINES «
INDEX, LBP/1000
18.9
2.9
12.9
i TO CYCLE NODE
.025
.011
.000
.1

1.076
.060
.000
.0

12.859
5.095
.006
7.2
	
LB FUEL
B
33.8
6.5
22.4

33.500
63.500
80.965
1.712
.268
.105
100.0
2.289
11.985
1.8211
1.018 .
100.0
1 f* fl 9ft
lo •IICB
7.037
1.132 	
.632
lOt. 8
9.90V ..
	

.
	 .. 	 . . . _


OMENING EMISSION INDEX VALUES
c DCMATU iturMAijcrn. (71 RFOUT0FQ
                                                AT  TAXI-IDLE MODE ON.Y, CO AND HC  EMISSIONS  AT  OTHtR MOOES REMAIN
                                                DEDUCTION IN NOX OBTHNtD BY LOWERING  EMISSION  INDEX VALUES AT CLIMBOUT AND TAKEOFF MOOES IN
                                                SAME  PROPCRTION AS MEASURED VALUES, NOX  EMISSIONS AT TAXI-IDLE AND APPROACH MOOES
                                                REMAIN UNCHANGED
-------
pi
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>




.
ENGINE* TPE331-5-2S1M S/N= P04001 COH8 P/N= 869082-4
RAT SHP= 706. RA EGT.F* 1650. RAT SPO= 1.1730. OEH PT,F« 19.
FUE. H/C= 1.9280 STOI F/A= .06822 L H V- 18470. S LN T,F= 300.0
DATA POINT NUMBER
PERCENT MAX. CORRECTED POMER
: CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Nl, RPM
! COMPRESSOR INLET TEMP., DEC. F
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR OSCHG. TEMP.OEG F
TUR3 INTERSTAGE TEMP., DE6.F
CCRR 3ELMTH FLON, LB/SEC
FA RATIC 3ASED ON BELLMTH.
MEASURED FUEL FLOM, LB/HR
FA <*AT10 C»LC. FROH EMISSION
EQUIVALENCE RATIO
LOADING H/P»«N/V/E«T/540I
COM3 £FFIC FROM EMISSIONS
CAR3CN DIOXIDE
PERCENT BY VOLUME. MET
> L3. C02 PER LB. OF FUEL
HEIGHT FLOW, LB./HR.
CAR30N MONOXIDE
1 PPM BY VOLUME, NET
LD. PER 1000 LB. OF FUEL
HEIGHT FLOW, LB./HR.
UNBURNEC HYDROCARBONS- PPM AS
PPM BY VOLUME, MET
L3. PER 1000 LB. OF FUEL
) HEIGHT FLOW, LB./HR.
RATIO LB HC/LB CO
NIIRIC CXIOE (NO) - HEIGHTS AS
) PPH BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
•EIGHT FLOM, LB./HR.
) NITROGEN OIOXIOE (N02I
PPM BY VOLUME, HET
i.3. PER 1000 LB. OF FUEL
) HEIGHT FLOH, LB./HR.
92
5.0
35.3
33.9
27560.0
59.0
1.6.6
336.0
905.0
2.85
.0108
106.0
.0098
.144
.320
99.298

J.04
3.12
3)0.3

19li.7
18.955
2.009
CAR3CN,
52.5
2.921
.310
.151,1
N02
18.1
2.891,
.307

6.9
1.103
.117
93
7.
53.
51.
27560.
59.
i«7.
336.
978.
2.80
.0123
119.0
.0110
.161
.309
99.509

2.29
3.13
372.0

177.8
15.l|67
1.8*1
HEIGHTS AS
29.1
1.447
.172
.9936

24.1
3.444
.1,10

6.3
.900
.107
9*
10.1
71.1
68.3
27530.0
59.0
<.7.2
338.0
10*5.0
3.81.
.0130
128.0
.0122
.178
.311
99.612

Z. 53
3.13
1*00.8

165.1
12.981,
1.662
CHI.
21.0
.98.0
8.052
2.053

13.2
2.211,
.565
96
70.2
1,95.5
1,75.8
1.1750.0
59.0
136.0
672.0
1335.0
7.71
.0130
31,7.0
.0127
.187
.070
99.91.1.


FUEL- 4V. KERO. TEST NO.* 5
REL HUM: 20.00 SPEC HUM: .002001
FLO,L/M= 14.160 SL TIN,S= 6.5000
97
90* 3
637.7
612.3
41740.0
59.0
142.3
680. 0
1450.0
7.72
.0148
396.0
.0147
.216
.065
99.962
98
100.4
708.7
688. S
•41740.1
59.1
143.1
602. fl
1512.0
7.67
.0160
425.1
.0158
.232
.064
99.971

Z.66
3.15
1093.3

25.9
1.91,2
.671,

2.7
.116
. 0*0
.0595

90.2
11.107
3.85".

9.5
1.169
.1.06
3.10
3.15
1248.1

21.1
1.365
.540

1.8
.067
.026
.0489

lis. a
12.243
4.848

3.8
.399
.158
TOTAL OXIDES OF NITROGEN (NC*N02> AS N02
PFH BY VOLUME, HET
) LB. PER 1800 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
> CORRECTED HEIGHT FLOH
SMCKE NUMBER
CORRECTED HEIGHT FLOH
; SMCKE MuraeB
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLCU
SMCKE NUMBER
SMOKE NUMBER AT HA^O.023
25.0
3.998
.".2".

.00722
3.50
.02161
3.50
.03601
7.90
.05033
9.30
5.90
30.1.
4.344
.517

.00720
5.80
.(2156
7.00
.03593
7.00
.05030
8.10
7.00
35.8
«.624t
.592

.00720
4.70
.02152
5.80
.03586
3.50
.05020
7.00
5.1.0
61.2
10.266
2.618

.00715
"..70
.82141.
9.30
.03573
li>. 00
.01.992
18.60
11.70
99.7
12.276
4.260

.00713
5.80
.0211.0
11.60
.03566
. 18.60
.04992
24.40
15.20
118.8
. 12.642
5.006

.00711
4.70
.02132
11.60
.03553
17.41
.04974
22.10
14.10
3.33
3.15
1339.8

15.8
.952
.405

2.1
.072
.031
.0759 . . . 	 	 __

123.0
12.161
5.168

7.0
.692
.294

130.0
12.853
5.462

.00709
5.80
.02128
11.60
.C3S46
16.30
.04965
20.90
13.80
                       NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE HET VALUES.
                             2.EQUIVALENCE RATIO CALCU.ATED FROM COZ,CO,ANO HC DATA AND FUEL COMPOSITION.
                             3.MASS EMISSIONS OF NO, N02, AND NO+N02 CALCULATED AS NO2 FROM COkCENTftATIOMS WITH MOLECULAR HEIGHT OF  N02  116.011.
-------
                      ............,...........,,..,......,.„.,..,,,  »l*ESEARCH  EMISSION  TEST SUHMARY  •»••»«••••»•»•
                      ENG HFC  I  AIRESEARCH            TEST FACIL < PHX LACC2  INSTR OESCRIP I FED KEG V38 N136
                      MODEL NO. I      TPE331-5-251M     S/NI   P84001               ENGINE  TYPE (CLASS! I  TURBOPROP
                      RATED POWER:     roe.o  SHP AT SEA LEVEL STANDARD DAY CONDITIONS
                      FUEL! ASTH  D1655-73            ATOMIC H/C RATIO!   1.928      LHVt  18470. BTU/LB     ADDITIVES»
 CALC DATE 110-27-75
 CALC IDI   3
TEST NOI   5
                                                                                                                        NONE
                      »•••»•»•• EXHAUST  EMISSIONS PER EPA CYCLE OF  WOR<  OUTPUT  »»  CODE  OF FEDERAL REGULATIONS TITLE 40 PART 87  17 JULY  1973   »•••»••
                                           HYDROCARBONS (CH AS CHi.)           2.038 LB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                           CARBON MONOXIDE (COI              14.768 LB.  POLLUTANT PER 1090 HP.-HR. PER CYCLE
                                           OXIDES OF NITROGEN  (NOX  AS N02I    9.898 LB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                           SMOKE                              15.7   SMOKE NUMBER. MAXIMUM AT  CRUISt    HOOE.  70 PERCENT RATED POKER
                      TAXI-IDLE  SETTINGI  5.0      PERCENT RATED TAKEOFF  PONE.R  AT  65.       PERCENT RATED TAKEOFF Nl RPM
Ui
                      [[[  £N6IN£  DESCRIPTION  ••••*••••••••*••••••»••••••••»•«»••••••»•••••••»••••
                      COMB TYPEI REVERSE  FLOM ANNULAR           P/N>    869032-1.            SUR/VOi' 1.260  FUEL INJ TYPE<  STAGED SIMPLEX
                      ENGINE TOTAL SERVICE!   0.0        HR    TIME SINCE ENGINE OVE»HAULI   0.0       HR                  _.  	  _.   .
                      ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                      AIRCRAFT INSTALLATION  »•*»»  MFR. I                                  MODEL  NO.I
                                                  USER:                       ENGINE  INSTALLATION POSITIONI                            .
                      ...................,............»»»»»»»»»»..».».0p£|?4fIoNAL fESI  OATA SUMMARY ••»•••••»••••«••»»»»»»•»••»«•»•••»•»»••••••••»••
                      GASEOUS EMISSION TEST  NO.I    5           DATES 10-27-75            TIME!                     6ARO PRESS.I  21.730  IN.  HGA.
                      AMBIENT AIR TEMP.t   59.00 DEG.  F        RELATIVE HUMIDITY I  20.00 PERCENT       SPECIFIC HUMIDITY!  .082000 LB. H20/LB.  DRY AIR
                      AMBIENT AIR QUALITY    HYDROCARBONS CMC)! 0.0   PPMC     CARBON MONOXIDE (COJI 0.0   PPMV    OXIDES OF NITROGEN INOXII  0.0   PPMV
) SAMPLE LINE »•• TEMP.: 300.00 DEG. F. FLOHRATE: 14.16 LITERS/WIN. TRANSPORT TIME: 6.50 SEC.
> TEST CONDITION
ACTUAL FOHER SETTING, HCRSEPOHER
CORR. POHER SETTING (STD DAYI , PERCENT RATED
Nl SPEED, RPN
FUEL FLCW (MEAS.I L8./HR.
CORR. ENGINE CORE AIRFLOM (MEAS) , LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., DEG F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS., PSIA
' COMPRESSOR DISCHARGE AIR TOTA. TEKP., OEG F
TURBINE INTERSTAGE GAS TOTAL TEMP., BEG F
EXHAUST GAS STATIC PRESSURE, PSIA
i EMISSION CONCENTRATION, NET ANALYSIS
HYDROCARBON ( HC AS CH4I , PPMC
CARBON MONOXIDE (CO) , PPMV
) TOTAL OXIDES OF NITROGEN (NOXJ, PPMV
CARBON DIOXIDE (C02) , PERCENT BY VOL.
NITRIC OXIDE (NOt, PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS N02)
EMISSIOK RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS N02)
COMBUSTION EFFICIENCY. PERCENT (EMISSIONS)
F/A (EMISSIONS, CALC)
99 100 101
33.7
4.97
27560.00
105.0
2.9
59.00
14.11
46.86
337.00
904.0
14.07

1.8.000
178.691
26. 000
2.014
19.200

2.704
17.612
<>.209

• 284
1.849
.442
99.35
.0097
51.1
7.53
27580.00
117.0
2.8
59.00
14.11
47.35
338.00
975.0
14.07

35.400
172.795
30.800
2.272
2*. 200

1.772
15.129
*.429

.207
1.770
.518
99.49
.0109
67.6
9.98
27540.00
128.0
2.7
59.00
14.11
47.40
338.00
1039.0
14.07

21.300
161.538
35.000
2.493
28.600

.973
12.912
4.596

.125
1.653
.568
99.61
.0120
102
203.9
30.08
41720.00
247.0
7.9
59.80
14.11
130.26
663.00
1114.0
14.00

5.100
61.036
62.800
1.945
48.200

.388
6.279
10.612

.074
1.551
2.621
99.83
.0043
103
475.0
70.01
41770.90
343.0
7.7
60.00
14.11
137.28
678.00
1342.0
14.01

1.280
20.653
98.500
2.703
88.750

.051
1.532
12.005

.017
.526
4.118
99.96
.0129
104
613.3
90.46
41720.00
394.0
7.7
59.88
14.11
140.72
680.00
1465.0
14.05

1.800
18.233
116.000
3.207
109.250

.864
1.141
12.125

.825
.449
4.777
99.97
.8152
LENGTHS 50.0
105
679.5
100.23
41710.00
421.0
7.6
59.00
14.11
142.93
682.08
1515.0
14.06

.608
15.821
129.258
3.389 	
119.508

-------
pj
iQ
o>
vo
CTi
                     I....*......,.*..................,..,.,...  EpA CYCLE EHisslONS COMPUTATION  SUMMARY  ••••••••»«
                     ENG MFC I AIRESEARCH            TEST FACIL I  PHX LACC2  INSTR OESC^IP  I FED REG  V3« N136
                     MODEL NO.I      TPE331-5-251M      S/NI    P0<>001              C.NGINE TYP£(CLASSII   TURBOPROP
                     RATED PCNERt     706.0  SHP  AT  SEA  LEVEL  STANDARD DAY CONDITIONS
                     FUELI ASTM 01655-73             ATOMIC H/C RATI01   1.928     LHV« 18it3
.052
8.2

TAXI-IDLE
IOUT)
19.000
5.000
35.300
11. ire
105.159
31.300

2.692
.283
.090
69.6


17.580
1.8<.9
.585
62.lt


<>.21

.291
.072
.005
i>.2


6.278
1.5*7
.116
12.1,


10.585
2.609
.196
31.1

CLIMBOUT
2.500
90.000
635.1,00
26.1.75
391.795
16.325

.036
.01*
.001
.5


1.082
.tz*
.018
1.9

•- 	 • 	 	 -
12.070
<>.729
.197
31.3

TAKEOFF
.500
100.000
706.000
5.883
<>21.302
3.511

.050
.021
.000
.1


1.006
.«*
.oo>>
.<»

- _
12.595
5.306
.0". i,
7.0

TOTAL PER
CYCLE
33.500


63.51.0

83.889

1.536
.231
.129
100.0
2.028

11.185
1.681
.916
100.0
1<>.768
•-- 	 - -
7.197
1.126
.629
100.0
9.898
                                           •• EMISSION  INDEX  LEVELS REQUIRED TO MEET EPA 1979 STANDARDS FOR CLASS  P2  ENGINES •«
                                        £PA LTO-CYCLE
                                                                                                 REQUIRED EMISSION  INDEX,  LBP/1000 LB FUEL
                                 POLLUTANT   LBP/1000 HORSEPOHEft-HR-CYCLE
                                    CO             26.8
                                    HC              
-------
fli
-1 -
ENGINE- TPE331-5-251H
RAT SHP» 786. RA EGT.F'
) FUEL M/C" 1.9280 STOI F/A'
DATA POINT NUMBER
PERCENT NAX. CORRECTED POWER
CORRECTED SHAFT HP
MEASURES SHAFT HP
SHAFT SFEEO. Nl, RPM
COMPRESSOR INLET TEMP. .DEC. F
COMPRESSOR DSCHG. PRE.S..PSIA
1 COMPRESSOR OSCHG. TEMP, DEC F
TUR3 INTERSTAGE TEMP., OEG.F
CORR 3ELMTH FLOW, LB/SEC
• FA RATIO BASED ON BELLMTH.
MEASURED FUEL FLOM, LB/HR
FA RATIO CALC. FROM EMISSION
) EQUIVALENCE RATIO
LOADING M/P«N/V/EIT/500»
COM3 EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
) LB. C02 PER LB. OF FUEL
HEIGHT FLOM, LB./HR.
CARBON MONOXIDE
; PPM BY VOLUME, MET
LB. PER 1081 LB. OF FUEL
HEIGHT FLOM, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
} HEIGHT FLOM, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NO) - WEIGHTS A
) PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
J NITROGEN DIOXIDE 
it
* .

i
-------
srv.—ss^   T.:~^^-™™:S-.». «
sail ss'!,».:!;-' '» •• "M^S-SKS."",:,..
                                                                       LHVI 18470.  BTU/LB
                                                                                         ADDITIVES! NONE
                                                                                                        CALC DATE 110-28-75
                                                                                                        CALC'IOI  1

                                                                                                       TESTNOt   '
                                    OXIDES
                                    SMOKE
                    TAXI-IDLE SETTING!  5.0

                       ««*« RATED TAKEOFF POKER^ ^ "TMES JUS^S RPM""*'
70 PERCENT RATED POKER
(U
iQ
(D
vo
CO
                    COMB TYPE: REVERSE FLO* ANNULAR          P/N.   869082?"       "
                    ENGINE TOTAL SERVICE!  0.0      Hft   TIHE SINCE ENGINE OVERHAUL!   .t
                    ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!           u»t«n«ULl  «.»
                    AIRCRAFT INSTALLATION •••• MFR. 1                            MOOEL „„.,
                                                                »
                                                                MR
                                                                     FUEL  INJ TYPE!  STAGED SIMPLEX
, iiyili^-S'b r??f
' TEST CONDITION
ACTUAi. POWER SETTING, HORSEPOWER
CORR. POWER SETTING (STO DAY), PERCENT RATED
Nl SPEEO. RPM
FUEL FLCK IMEAS.) LB./HR.
CORR. ENGINE CORE AIRFLOW , tB/SEC
COMPRESSOR INLET AIR TOTAL TE1P., DES F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTA^ PR£SS., PSIA
COMPRESSOR DISCHARGE AIR TOTAc TEMP., OEG F
TURBINE INTERSTAGE GAS TOTA,. TEMP., DCG F
EXHAUST GAS STATIC PRESSURE, PSIA
CNISSICN CONCENTRATION, HET ANALYSIS
HYDROCARBON (HC AS CH4), PPMC
CARBON MONOXIDE (CO), PFHV
' TOTAL OXIDES OF NITROGEN INOXI, PPHV
CAS30N DIOXIDE (C02), PERCENT BY VOL.
NITRIC OXIDE 
-------
{a
VO
vo
                         ..........................................   £PA  crCL£  EMISSIONS COMPUTATION SUMMARY  •••••»»•»•
                         ENG MFC I AIRESEARCH           TEST FACIL  I  PHX  LACC2   INSTR DESC3IP I FED REG V38 N136
                         MODEL NO.I     TPE331-5-Z51H     S/Nt    PO-.001               ENGINE TYPEICLASSII  TURBOPROP
                         RATED POHERI    706.0 SHP AT SEA LEVEL  STANDARD  DAY  CONDITIONS
                         FUELI ASTH D1655-73            ATOMIC H/C  RATIOI   1.928     LHVI 18470. BTU/LB     ADDITIVES*
                                                                                                                          NONE
                          CALC DATE 110-28-75
                          CALC IDI   1
                         TEST NOI    «
NODE
TIME IN NODE, MINUTES
RATED POWER, PERCENT
CORRECTED POHER, HORSEPOWER
HP-HR
FUEi. FLOH, LB/HR
FUEL MASS. LB
•• HYDROCARBON EMISSION (HCI »•
INDEX, LB HC/1000 LB FUEL
RATE, LB HC/HR
MASS. LB HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1100 MORSEPOHER-HR PER CYCLE
•• CARBON MONOXIDE EMISSIONS CCOI •*
INDEX, L8 CO/1000 LB FUEL
RATE, LB CO/HR
MASS. LB CO
MASS. PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORSEPOWER-HR PER CYCLE
»» TOTAL OXIDES OF NITROGEN EMISSIONS (NOX)" •»
INDEX, LB NOX/100I LB FUEL
RATE, L8 NOX/HR
MASS, IS NOX
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB NOX/1000 HORSEPONER-HR PER CYCLE
TAXI-IDLE
(IN)
7.000
9.000
35.300
4.U8
105.037
12.251.

3.035
.319
.037
25.6


21.066
2.108
.246
23.5


4.415
.464
.051.
8.5

TAXI-IDLE
(OUT)
19.000
5.000
35.309
11.178
105.037
33.262

3.035
.319
.101
69.4.


20.066
2.108
.667
63.8


'..'.15
.464
.147
22.9

APPROACH
-------
(D
 L9. COZ PE? LB. OF FUEL
HEIGHT FLON, LB./HR.
CARBCN MONOXIDE
PPH BY VOLUME, HET
L9. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
' HEIGHT FLOH, LB./HR.
RATIO L6 HC/LB CO
NITRIC OXIDE (NOI - HEIGHTS AS
) PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH. LB./HR.
) NITROGEN DIOXIDE IN02)
PPM SY VOLUME, HET
L3. PER 1000 LB. OF FUEL
) HEIGHT FLOH, LB./HR.
1650.
.06833
196
5.0
35.2
34.0
2751.0.0
60.0
47.3
330.0
888.0
2.92
.oiOn
105.0
.0096
.1%!
,32k
99.361

1.99
3.11
337.0

201.7
20.076
2.108
RAT SPO=
L H V=
107
7.5
52.8
51.0
27550.0
62.0
1.7.5
33*. 0
950.0
2.86
.0117
116.0
.0107
.156
.311
99.1.30

2.21
3.1Z
362.1

188.1
16.9)0
1.960
CARBON, HEIGHTS AS
53.4
3.039
.319
.1511*
NOZ
30.3
3.330
.31.9

6.7
1.096
.115
40.5
3.078
.241
.1230

23.0
3.391
.393

6.4
.944
.109
1.1730.
181.70.
10*
10.0
70.6
68.3
27570.0
6Z.O
1.7.8
335.0
1030.0
Z.7S
.0130
125.0
.0119
.175
.399
99.536
'SUMMARY OF
3.1.9
3.13
391.0

175.1
11.. 008
1.751
CH-
33.6
1.537
.193
.1097

28.2
3.707
.1.63

7.0
.920
.115
DEH PT.F*
S ..N T,F=
109
30.1
212.7
204.7
1.1770.0
58.0
133.9
695.0
1105.0
7.88
.0092
353.0
.0095
.139
.073
99.838
1.0.
300.0
110
70.1
494.9
47S.8
41750.0
57.0
140.6
659.0
1319.0
7.79
.0129
348.0
.0126
.165
.070
99.941
REDUCED EMISSION
1.99
3.11.
795.5

56.8
5.738
1.1.1.9

5.1.
.311
.079
.0543

1.8.8
8.076
2.01,3

14.9
3.1.66
.631.
TOTAL OXIDES OF NITROGEN INC*N02I AS N03
PPM BY VOLUME, HET
) LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
) CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLCH
) SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
SMOKE NUMBER AT NA*O.OZ3
Z7.0
4.415
.<>6<>

.00697
1.30
.02090
3.50
.03477
7.00
.D<>868
9. JO
5.40
NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE
29.1.
4.335
.503

.00695
3.30
.02086
3. 50
.031.71
5.80
.01,359
8.10
5.00
35.2
4.637
.578

.00691.
1.20
.02083
4.70
.031.71
2.30
.01.859
7.00
3.90
61.7
10.543
2.667

.00697
5.80
.02092
9.30
.03k92
16.30
.04889
16.30
12. IB
3.65
3.15
1096.4

28.0
3.115
.736

Z.4
.104
.036
.0491

82.5
10.254
3.566

7.5
.932
.324

90.0
11.166
3.893

.00710
5.80
.02130
12.80
.03557
20.90
.•4988
26.70
16.71
REL HUM*
FLO,L/M=
111
90.3
637.5
615.2
41730. 0
61.0
143. 7
666.0
1443.0
7.78
.0146
399.0
.0147
.215
.066
99.963

3.09
3.15
1257.6

20.2
1.315
.535

1.8
.067
.027
.0508

102.7
10.960
4.373

9.8
1.040
.415

113.5
12.000
4.760

.00716
8.10
.02149
11.60
.03581
17.40
.05014
23.30
15.11
49.00 SPEC HUME .005000
14.160 SL TIM.S- 6.5000
112
100.7
710.9
664.1
4173B.
56.
146.
669.
1500.
7.81
.0157
426.0
.0158
.331
.064
99.973

3.33
3.15
1342.9. . .. _ 	 	

15.1
.954
.406 	 "

1.5
.052
.022
.0542

110.7
10. 970. _ 	
4.673

6.1
.669
.285

117.5
11*636
4.958.

.00716
5.80
.02149
8.11
.03561
16.30
.05014
28.90
12.60
HET VALUES.
                             2.EQUIVALENCE RATIO CALCULATED FROM CO2.CO.ANO  HC  DATA AND FUEL COMPOSITION.

                             3.MASS EMISSIONS OF NO, N02, AND N3+N02 CALCULATED AS  NOZ FROM CONCENTRATIONS WITH MOLECULAR HEIGHT OF NOZ  (46.011.
-------
n>
N>
O
                       .............................................   »I^ES£»RCM EMISSION TEST SUMMARY  ••••••••••••••
                       ENG  HFG I  AIRESEARCH           TEST FACIL  I  PHX LACCZ  INSTR OESCRIP 1 FED REG V36 N136
                       MODEL NO.»     TPE331-5-251H     S/NI    P04801              ENSINE TYPE(CLASS)I  TURBOPROP
                       RATED POMERt    706.0 SHP AT SEA LEVEL  STANDARD DAY CONDITIONS
                       FUEL I ASTM 01655-73            ATOMIC H/C  SATIOI   1.928     LHV> 18470. 8TU/LB     ADDITIVES I
                                                                                                                         NONE
 CALC DATE 110-28-75
 CALC 101   Z
TEST NOt    6
                       ........ ExHAUST EMISSIONS PL* £PA CYCLE  OF  WORK OUTPUT •• COD£ OF FEDERAL REGULATIONS TITLE  40  PART 67  17  JULY 1973  •»»»»••
                                           HYDROCARBONS  ICH  AS CHi.)           2.356 1.3. POLLUTANT PER 1000 HP.-MR.  PER CYCLE
                                           CARBOK MCNOXIOE  (COI              16.440 L3. POLLUTANT PER 1000 HP.-HI.  PER CYCLE
                                           OXIDES OF NITROGEN  (NOX  AS N03)    9.5b2 .3. POLLUTANT Pfc* 1000 HP.-HR.  PER CYCLE
                                           SMOKE     %                        16. •»  SMOKE NUMBER, MAXIMUM AT  CRUISE     NODE,  70 PERCENT RATED POKER
                       TAXI-IDLE SETTINGS 5.0      PERCENT RATIO TAKEOFF POKER AT 65.      PERCENT RATED TAKEOFF Nl  RPM
                       [[[  £NG1NE DESCRIPTION  •»»»••••••••••»»»»»»«».»...»».»»»»»»«»»»»»»»...»»»..
                       COMB  TYPE I  REVERSE FLOH ANNULAR            P/NI    869082-4           SUR/VOLI 1.260  FUEL INJ TYPEI   STAGED  SIMPLEX
                       ENGINE  TOTAL SERVICE*  0.0       HR     TIME  SINCE ENGINE OVERHAUL!  0.0       HR
                       ENGINE  ASSEMBLY AND MAINTENANCE INFORMATION I
                       AIRCRAFT INSTALLATION »»»• HFR.I                                  MODEL NO.I
                                                  USERJ                        ENGINE INSTALLATION POSITIONI
                       I........*........*..,.......,........»«»».»».»»0pERATIONAL TEST DATA SUMMARY »••••»••••»»•»•••»••»»••••»••»••••••»»••••••'•»••
                       GASEOJS EMISSION TEST NO.t    6         DATtl 10-28-75           TIME!                    BARO PRESS.I  28.820  IN. H6A.
                       AMBIENT AIR TEMP.I  59.00  DEC. F        RcLATIVE  MUHIDITYI   49.00 PERCENT       SPECIFIC HUMIOITYI   .005000  LB. H20/LB. DRY AIR
                       AMBIENT AIR QUALITY    HY030C4330NS  (MC)I  0.0   PPMC     CARBON MONOXI3E (C0»X 0.0   PPMV    OXIDES  OF  NITROGEN (NOX)I  0.0   PPM*
                       SAMPLE  LINE »»• TEMP.I  300.00 DEC. F.     Fi_3HRATE«   14.16 .ITERS/MIN.     TRANSPORT TIME!    6.50 SEC.     LENGTH!   50.00 FT.
TEST CONDITION
ACTUAL POWER SETTING, HORSEPOMER
CORR. PONE* SETTING (STD OAtl, PERCENT 94 TED
Nl SPEED, RPM
FUEL FLCW IHEAS.) L8./HR.
CORR.' ENGINE CORE AIRFLOW IHEASI, LB/SEC
COMPRESSOR INLET AIR TOTAL TEHP., OEG F
COMPRESSOR INLET AIR TOTAL PRcSS. , PSIA
COMPRESSOR DISCHARGE AIR TOTA_ PRESS., PSIA
COMPRESSOR OISCHARGE AIR TOTA. TEMP., OEG F
TURBINE INTERSTASE GAS TOTAc TENP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION, MET ANALYSIS
HYCROCAR30N (MC AS CN4I , PPNC
CARBON MONOXIDE ICOI , PPHV
TOTAL OXIDES OF NITROGEN INOX), PPMV
CARSON DIOXIDE (COZI , PERCENT BY VOL.
NITRIC OXIDE INO). PPM*
EMISSION INDEX, LB. POLLUTANT/1000 L9. FUEL
HYDROCARBONS IHC AS CH4I
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
EMISSIOK RATE, LB. POLLUTANT /MR.
HYDROCARBONS IHC AS CM»»
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN IMOX AS NOZ)
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS. CALCI
113 11". 115
33.9
4.99
27510.00
105.0
3.0
60.00
14.16
1.7. 45
326.00
856.0
14. 1Z

31.. 900
200.732
23.800
2.009
17.100

3.095
19.801
3.856

.325
2.079
.<>05
99.26
.0097
53.9
7.1.8
27510.00
115.0
2.9
60.00
14.16
45.92
3Z7.00
949.0
I3.500
192.<.13
27.700
2.Z46
Z1.100

2.198
17.007
4.022

.253
1.956
.V63
99.<.1
.0108
67.9
9.97
27530.00
126.0
2.8
61.00
14.16
-.8.38
326.10
1001.. 0
Ki.lZ

30.300
169.633
31.800
Z.<«11
Z5.400

1.430
14.005
4.313

.iao
1.765
.543
59.55
.0116
116
199. Z
29.29
1.1730.00
253.0
7.9
59.00
14.16
13Z.37
648.00
1095.0
l

6.300
56.941
58.500
1.945
45.500

.370
6.064
9.886

.094
1.534
2.501
99.82
.0093
117
473. Z
69.51
41760.00
348.0
7.8
60.00
14.16
140.23
660.00
1318.0
14.05

1.800
25.107
92.500
2.671
84.750

.077
1.885
11.407

.027
.656
3.970
99.95
.0127
118
614.7
90.30
41710.00
400.0
7.6
60.00
14.16
11.1.26
666.00
1439.0
14.09

1.600
Z0.249
110.500
3.101
102.500

.067
1.310
11.742

.027
.5Z4
4.697
99.96
.0147
119
660.3
99.94
41730.00
426.0
7.8
60.08
14.16
143.22
670.00
1497.8
14.10

1.508
19.039
121.008
3.348
112.500

-------
                      ENGIFG  i  AIRESEARCH
13
to
o
                         ,».,.......,...,.   £pft  crCl_E  EMISSJONS COMPUTATION SUMMARY  ....»»»...

„„„..                           fEST FACI.  I  PHX  LACC2   INSTR DESCRIP I  FED REG V38 N136
MODEL NO.I     TPE331-5-251N     S/NI   P04001               £NGIN= TYPE(CLASS)I  TURBOPROP
RATED PONERI    706.li SMP AT SEA LEVEL STANDARD  DAY CONDITIONS      TYPE
-------
fl)
O
OJ

ENGINE^ TPE331-5-251M S/N= P04001 COM3 P/N= 86908Z-4
RAT SHP= 706. RA EGT,F=
FUEL H/C* 1.9280 STOI F/»=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Nl, RPM
COMPRESSOR INLET TEMP., DEC. F
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR DSCHG. TEMP, DEC F
TURS INTERSTAGE TEMP., DEG.F
CORR 3ELMTH FLOH, LB/SEC
FA RATIC BASED ON 9ELLMTH.
MEASURED FUEL FLOH, LB/HR
FA RATIO CAtC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P»»N/V/E«T/540I
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
L3. COZ PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARSON MONOXIDE
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNED HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LE HC/LB CO
NITRIC OXIDE (NOI - HEIGHTS AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE CN02)
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
1650.
.06822
113
5.0
35.2
33.9
27510.0
60.0
47.4
326.0
886.0
3.00
.0101
105.0
.0097
.142
.334
99.263

2.01
3.11
327.0

200.7
19.901
2.079
RAT SPD=
L H V=
114
7.5
52.8
50.9
27510.0
60.0
45.9
327.9
949.0
2.92
.0114
115.0
.0108
.159
.343
99.407

2.25
3.12
358.9

192.4
17.007
1.956
41730.
18470.
115
10.0
70.4
67.9
27530.0
61.0
48.4
326.0
1004.0
2.85
.0128
126.0
.0116
.170
.306
93.545
'SUMMARY OF
2.41
3.13
394.1

169.6
14.005
1.765
D£H PT.F* 40.
S _N T,F=
116
29.3
206.8
199.2
41730.0
59.0
132.-.
648.0
1095.0
7.85
.0093
253.0
.0093
.137
.080
99.825
REDUCED
1.94
3.14
795.3

58.9
6.064
1.534
= 300.0
117
69.5
490.7
473.2
41760. D
60.0
140.2
660.0
1318.0
7.79
.0129
348.0
.0127
.186
.070
99.949
FUEL:
REi. HUM*
FLO,L/M=
118
90.3
637.5
614.7
41710. •
60.0
141.3
666.0
1439.0
7.80
.0148
400.0
.0147
.216
.068
99.963
' AV. KERO. TEST NO.' 6
49.00 SPEC HUH* .005000
14.160 SL TIN.S* 6.5000
119
99.9
705.6
680.3
41730.0
60.0
143.2
670.0
1497.0
7.7«
.0158
426.0
.0158
.232
.066
99.969

2.67
3.15
1096.5

25.1
1.885
.656
3.10
3.15
1260.7

20.2
1.310
.524
3.34
3.15
1342.8

19.0
1.144
.487
Jr
•v

t
1)

}


)


)


y


y




j


y


CARBCN. HEIGHTS AS CH4 . )
54.9
3.095
.325
.1563
N02
17.1
2.771
.291

6.7
1.086
.114
43.5
2.198
.253
.1292

21.1
3.063
.352

6.6
.958
.110
30.3
1.430
.180
.1021

25.4
3. 445
.434

6.4
.868
.109
6.3
.370
.094
.0611

45.5
7.689
1.945

13.0
2.197
.556
1.8
.077
.027
.0410

84.7
10.451
3.637

7.8
.956
.333
1.8
.067
.027
.0508

102.5
10.892
4.357

8.0
.850
.340
_ 1.5 	 	
.052
.022
.0450. 	 _ 	 .

112.5
11.101
4.729

8.5
.839
.357


y


) :


y


y .
TOTAL OXIDES OF NITROGEN INC-.N02I AS N02
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLCH
SMOKE NUMBER
SMOKE NUMBER AT MA-0.023
23.8
3.856
.405

.00717
4.70
.02152
5.80
.03587
8.10
.05022
8.10
6.70
27.7
1>.022
.463

.00719
1.20
.02156
5.80
.03594
8.11
.05031
8.10
5.81
31.8
4.313
.543

.00712
2.30
.02156
4.70
.03594
5.80
.05031
8.10
5.20
58.5
9.886
2.501

.00718
4.70
.02153
11.60
.03588
15.10
.05023
18.60
12.50
92.5
11.407
3.970

.00711,
7.00
.02141
14. GO
.03561
19.80
.04977
24.40
16.40
110.5
11.742
4.697

.00707
7.00
.02121
12.80
.03528
19.80
.04939
22.10
15.58
121.0
11.940
5.086. 	

.00703
5.80 .. 	 _ ....
.02109
11.60
.03515
17.40
.04921
18.40
13.50

J-


y '•

"~"n
" y

,
t y

t
                      NOTES 1. ALL  EMISSIONS CONCENTRATIONS  ARE  HET VALUES.
                            2.EQUIVALENCE RATIO CALCULATED FROM  CC2.CO.ANO HC DATA AND FUEL
                            3.MASS  EMISSIONS OF NO, N02,  A*O NO+N02 CALCULATED AS N02 FROM
 COMPOSITION.
CONCENTRATIONS HITH
                                                                                                                  MOLECULAR HEIGHT OF  N02  ('•6.811.
-------
                      cur  -cr  .
                      loDfL  HC
                      MODEL  NC.
                      RATED  POWER.
                      FUELI  ASTM D1655-73
AIRESEARCH
              •Z51H      S/NI    P04001
      706.0 SHP AT SEA  LEVEL  STANDARD DAY CONDITIONS
                     ATONIC H/C RATIO,   1.928     LHV,  18470.  BTU/LB
AIKESEARCH EMISSION TEST  SUMMARY   »»*..»..».
        INSTR OESCRIP  I FED  SEG V38  N136
             ENGINE TYPE(CLASS),   TURBOPROP
                                                                                                            ADDITIVES,  NONE
                                                                                                        CALC  DATE  110-28-75
                                                                                                        CALC  IDI    3
                                                                                                       TEST NOI     6
........ EXHAUST EHISSIONS PER  EPA CYCLE OF WORK OUTPUT  ••  CODE  OF FEOERA. REGULATIONS TITLE 40  PART  87

                    CARBON SoSSxiDE ICO,             i2'"" ^'  POLI-UTSNT P£R *<">» HP.-HR. ?EK CYCLE
                    CARBON MONOXIDE (CO)             16.198 ^B.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                    SMOKED °F NITR°G£N 'NOX *S N02'   9'1*55 LS-  POLLUTANT PER 1000 Hpl-HRJ P|R CYCLE
TAXI-IDLE SETTING. 5.0      PERCENT RATED TAKEOFF POWE^A?  65?°^  ""PERCENT'""!!" TAKEOFF^! R
                                                                                                                                 17 JULY 1975
                                                                                                                                  '"*"" '"" ""«
 (U
vQ
 CD
 to
 o
                     COMB  TYPE.  REVERSE FLOW ANNULAR           P/NI
                     ENGINE  TOTAL  SERVICE,  0.0       HR    TIME  SINCE  ENGINt  OVERHAUL!
                     ENGINE  ASSEMBLY  AND MAINTENANCE INFORMATION,
                     AIRCRAFT  INSTALLATION •••• MFR.t                                  HODEL NO. 1
                                                 USER.
                                                  •**  ENGINE DESCRIPTION  .........................................
                                                  869082-*            SUR/VOL.  1.260  FUEL INJ TYPE!  STAGED  SIMPLEX
                                                                      0.0        HR
GASEOUS'E^ION'TEST'NO""**; 	 ""oATEr;;0.^;11"^ T£ST ?I*HE,SUMMAM ——•"••
AMBIENT AIR TEMP.I 59.00 OEG. F RELATIVE HUMILITY, 49.00 PERCENT SPECIFIC
AMBIENT AIR OUALITV HYDROCARBONS (HOI 0.0 PPMC CARSON MONOXIDE (CO) 1 0 0 PPMV
SAMPLE LINE ••• TEMP., JOO.OO OEG. F. FLOWRATEI 14.16 .ITERS/MIN. TRANSPORT TI
TEST CONDITION
ACTUAL POWER SETTING, HORSEPOWER
CORR. POWER SETTING (STO DAY), PERCENT RATED
Nl SPEED, RPM
FUEL FLOW (MEAS.) LB./HR.
CORR. ENGINE CORE AIRFLOW (NEAS), LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP. , DEG F
COMPRESSOR INLET AIR TOTAL PRESS. , PSIA
COMPRESSOR DISCHARGE AIR TOTA. PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL TEMP., OEG F
TURBINE INTERSTAGE GAS TOTAL TEMP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
ENISSIOK CONCENTRATION, MET ANALYSIS
HYDROCARBON (HC AS CH4) , PPMC
CARBON MONOXIDE (CO), PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPMV
CARBON DIOXIDE (C02), PERCENT 31 VOL.
NITRIC OXIDE (NO). PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4>
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4)
CARBON noNoxioe (CO)
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/« (EMISSIONS, CALC)
120 121 122
37.5 51.4 68.1
5.51 7.58 10.03
27530.00 27520.00 27520.00
107.0 116.0 127.0
2.9 ?.a y-K
59.00
47.79
325.00
895.0
14.12
52.500
194.717
£5.000
2.051
17.700
2.901
18.827
3.971
.310
*4Z5
99.30
.0099
57.00
14.16
48.23
324.00
9*2.0
14.12
45.000
187.820
28.000
2.233
21.000
2.299
16.711
4.092
.265
1.938
.475
99.41
.0108
57.00
14.16
48.48
325.00
1014.0
14.12
36.900
179.145
32.100
2.462
26.000
1.705
14.478
4.261
.216
1.839
.541
99.51
.0118
123
207.0
30.41
41730.00
257.0
7.9
60.00
133!lO
651.00
1103.0
14.04
6.300
62.714
60.100
1.972
46.700
.365
6.360
10.012
1.635
2.573
99.82
.0094
BARO PRESS., 28.820 IN. HGA.
HUMIDITY, .005000 LB. H20/LB. DRV AIR
OXIDES OF NITROGEN (NOX), 0.0 PPHV
ME, 6.50 SEC. LENGTH, 50.00 FT.
12*
470.3
69.22
41750.00
342.0
7n
• 0
58.00
14.16
140.47
660.00
1314.0
14.0*
1.800
28.767
89.750
2.687
82.500
.077
2.147
11.000
.026
.73*
3.762
99.9*
.0128
125
61*. 9
90.42
41760.00
405.0
ra
• 6
59.00
14.16
1*4.65
666.00
1*36.0
14.09
1.510
21.865
107.750
3.101
102.000
.055
1.414
11.449
.022
.573
4.637
99.96
.01*7
126
680.3
100.03
41710.00
427.0
7.8
59.00
143.76
668.01
1492.0
14.10
1.500 .
15.821
119.750
3.303
112.500
.052
.961
11.9*8
.022
5.102
99.97
.0157
-------
fa
                    ..........................................  Ep, CYC_£ EMISSIONS COMPUTATION SUMMARY  ••••»••••«
                    ENG MFC  :  AIRESEARCH           TEST FACU I PHX uACCZ  INSTR DESCRIP  t  FED REG V36 N136
                    MODEL NO.I      TPE331-5-251N     S/NI   P04001              £NGINE  TYPE(CLASS)I  TURBOPROP
                    RATED POMERI     706.0 SHP AT SEA LEVEL STANDARD DAY CONDITIONS
                    FUELI ASTM 01655-73            ATOMIC H/C RATIOt   1.928     LHVI 181.70.  BTU/L8     ADDITIVESI
                                                                                           CALC DATE I14I-2S-75
                                                                                           CALC IDI    3
                                                                                           TEST NOI     6
                                                                                                                      NONE
MODE
TIME IN MODE. MINUTES
RATED POKER. PERCENT
CORRECTED POWER, HORSEPOWER
HP-HR
FUEL FLOW, LB/HR
FUEL MASS. LB
** HYDROCARBON EMISSION (riCI **
INDEX, LB HC/lOOt LB FUEL
RATE, LB HC/HR
MASS, L8 HC
KASS, PERCENT OF TOT At. CYCLE
CYCLE. LB HC/1000 HORSEPOHER-H9 PER CYCLE
•• CARBON MONOXIDE EMISSIONS (CO) •»
INDEX, LB CO/1BOO LB FUEL
RATE. LB CO/HR
NASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 MORSEFOKcR-HR PER CYCLE
»» TOTAL OXIDES OF NITROGEN EMISSIONS (NOX) •»
INDEX. LB NOX/1000 LB FUEL
RATE, LB NOX/HR
NASS, LB NOX
KASS, PERCENT OF TOTAL CYCLE
CYCLE, LB NOX/1000 H01SEPOMER-HR PER CYCLE
TAXI-IDLE
(IN)
7.000
5.000
35.300
4.118
101.. 770
12.223

3.072
.322
.038
25.5


19.388
2.031
.237
23.0

. _
3.930
.1.12
.046
8.0

TAXI-IOLE
(OUT)
19.000
5.000
35.300
11.178
10i>. 770
33.177

3.072
.322
.102
69.1


19.386
2.031
.6<>3
62.5


3.930
.1.12
.130
21.7

APPROACH
4.500
30.000
211.800
15.885
2 51.. 107
19.058

.363
.092
.007
"•.7


6.1.05
1.628
.122
11.9

_ . . .
9.89k
2.511.
.189
31.1.

CLIMBOUT
2.500
90.000
635.1,00
26.1.75
1.02.627
16.784

.050
.020
.001
.6


1.399
.563
.023
2.3

- - 	 -
11.396
-------
*t>
CD

to
O
ENGINE* TPES31-5-251M
RAT SHP= 706. RA EGT.F'
FUEL H/C« 1.9281 STOI F/A
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED. Ml. RPM
COMPRESSOR INLET TEMP., DEC. F
COMPRESSOR OSCH6. PRES..PSIA
COMPRESSOR OSCHG. TEMP. DEC F
TUR8 INTERSTAGE TEMP., OEG.F
COR? 8ELMTH FLOH, LB/SEC
FA RATIO BASED ON BELLMTH.
M.EASURLO FUEL FLOM, L3/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P*»N/V/E(T/5401
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
S/Mi PBUDOl COMB P/N* 869082-4 FUEL' AV. KERO. TEST NO.* 6
= 1650.
* .06622
120
5.5
38.9
37.5
27530.0
59.0
47.8
325.0
495. 0
2.94
.0105
107.0
.0099
.1,5
.323
99.303

2.05
3.12
333.5

194. 7
ia.627
2.014
RAT SPO=
L H V*
1Z1
7.6
53.5
51.4
27520.0
57.0
48.2
324.1
942.6
2.92
.0114
116.0
.010)
.158
.317
99.406

2.23
3.12
362.1

187.8
16.711
1.936
UNBURNEO HYDROCARBONS- PPM AS CARBCN, HEIGHTS AS
PPH BY VOLUKE, MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
RATIO L8 HC/LB CO
NITRIC OXIDE INO) - HEIGHTS
PPM BY VOLUME. MET
L3. PER 1300 LB. OF FUEL
HEIGHT FLOM. LB./HR.
NITROGEN DIOXIDE IHO2>
PPH BY VOLUME, NET
LB. PER 10GO LB. OF FUEL
HEIGHT FLOM, LB./HR.
TOTAL OXIDES OF NITROGEN INC
PPM BY VOLUME. NET
LB. PER 1303 LB. OF FUEL
MEIGHT FLOM, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED MEIGHT FLO*
SMOKE NUMBER
CORRECTED MEIGHT FLOW
SMOKE NUM3C.B
CORRECTED MEIGHT FLCK
SMOKE NUMBER
CORRECTED MEIGHT FLOM
SMOKE NUMBER
SMOKE NUMBER AT MA*O.OZ3
52.5
2.901
.310
.15*1
AS N02
17.7
3.811
.301

7.3
1.159
.124
+N02I AS NOZ
25.0
3.971
.425

.80703
4.70
.02110
3.50
.03516
5.80
.04922
9.30
5.90
45.0
2.289
.265
.1369

21.0
3.069
.356

7.8
1.023
.119

28.0
4.092
.475

.00703
3.50
.82110
4.70
.03522
7.00
.04931
7.01
5.60
41730.
18470.
122
10.0
70.8
68.1
Z7520.0
57.0
46.5
325.0
1014.0
2.63
.0129
127.0
.0116
.173
.304
99.510

2.46
3.13
397.1

179.1
14.478
1.839
CH4
36.9
1.705
.216
.1177

26.0
3.452
.438

6.1
.610
.103

32.1
4.261
.541

.00704
3.50
.02113
4.70
.03522
4.70
.04931
7.00
5.00
OEM PT,F=
S i-H J,F=
123
30.4
214.7
207.0
41730.0
60.0
133.1
651.0
1103.0
7.65
.0094
257.0
.0094
.136
.079
99.618
OF REDUCED
1.97
3.14
607.6

62.7
6.360
1.635

6.3
.365
.094
.0574

46.7
7.780
1.999

13.4
2.232
.574

60.1
10.012
2.573

.00704
2.30
.02113
9.30
.03522
12.80
.04940
17.40
10,60
40.
300.0
124
69.2
466.7
470.3
41750.0
56.0
140.5
660.0
1314.0
7.83
.0126
342.0
.0126
.186
.070
99.943
EMISSION
2.69
3.15
1077.5

26.8
2.147
.734

1.6
.077
.026
.0356

62.5
10.112
3.458

7.3
.869
.304

89.7
11.000
3.762

.00704
7.00
.02117
16.30
.03529
16.60
.04940
26.70
17.30
RE_ HUMs
FLO,L/M=
125
90.4
636.4
614.9
41760.0
59.8
144.6
666.6
1436.0
7.81
.0150
405.0
.0147
.216
.066
99.962

3.10
3.15
1276.4

21.9
1.414
.573

1.5
.055
.022
.0392

102.0
10.636
4.390

5.8
.611
.247

107.7
11.449
4.637

.00704
8.10
.02117
11.61
.03535
18.60
.04949
23.30
15.50
49.00 SPEC HUH* .005010
14.160 SL TIN,S» 6.5000
126
100.0
706.2
660.3
41710.0
59.0
143.8
666.0
1492.0
7.79
.0156
427.0
.0157
.230
.066
99.973

3.30 ~
3.15
1346,!L_ . ._. 	

15.8
.961 _ ...
.410

.. .1.5 	 .... 	 	
.052
.022
.854Z . _ _ . _ 	

112.5
11.225 	 _. 	 	 _.
4.793

7»S __
.723
.309

119.7
11.946
5.10Z. 	 ._. 	 _...

.00706
4.70 	 	 	 	 _ _ .
.02117
14.10
. .03521 	
18.60
.04940
Z0.9fl.__ 	 .__ 	 	 ... .
14.70
                   MOTES 1. ALL EMISSIONS CONCENTRATIONS ARE MET VALUES.
                         2.EQUIVALENCE RATIO CALCULATED FROM C02.CJ.ANO HC OAT* AND FUEL
                         3.MASS EMISSIONS OF NO. N02, MO NO*N02 CALCULATED *S HOZ FROM
 COMPOSITION.
CONCENTRATIONS WITH
MOLECULAR HEIGHT OF N02 (46.111.
-------
                    „....,..*...........,..........,,.,...,,..„.   AIRESEARCH EMISSION TEST SUMMARY  »•••••••»•»»••
                    ENG MFC I AIRESEARCH           TEST FACIL  I  PHX LACC2   INSTR DESCRIP I FED REG V38 N136
                    MODEL NO.I     TPE331-5-2S1H     S/NI    PO 1.001              ENGINE TYPE (CLASS) <  TURBOPROP
                    RATED PONERI    706.0 SHP AT SEA LEVEL  STANDARD DAY  CONDITIONS
                    FUELI ASTH 01655-73            ATOMIC H/C  RATIOI   1.928     LHVI 18470. BTU/LB     ADDITIVES!
 CALC DATE 111-28-75
 CALC 101   1
TEST NOI  7
                                                                                                                     NONE
                    »••»*»•• EXHAUST EMISSIONS PER EPA  CYCLE  OF WORK OUTPUT •• CODE OF FEDERAL REGULATIONS TITLE «.• PART 87  17 JULY 1973  •»»»»»»
                                        HYDROCARBONS  (CH  AS CH4)           3.0H
FUEL FLCH INEAS.t LB./HR.
CORR. ENGINE. CORE AIRFLOW (HEASI, LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., OEG F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL. TEMP., DEG F
TURBINE INTERSTAGE GAS TOTAL TEMP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION, WET ANALYSIS
HYDROCARBON IHC AS CM), PPMC
CARBON MONOXIDE ICOI, PPNV
TOTAL OXIDES OF NITROGEN (NOXI, PPHV
CARBON DIOXIDE (COZI , PERCENT BY VOL.
NITRIC OXIDE INOI. PPHV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS IHC AS CH4I
CARBON MONOXIDE ICOI
TOTAL OXIDES OF NITROGEN INOX AS N02)
EMISSION RATE, LB. POLLUTANT/MR.
HYDROCARBONS IHC AS CH<»I
CARBON MONOXIDE ICOI
TOTAL OXIDES OF NITROGEN INOX AS NOZ)
COMBUSTION EFFICIENCY, PERCENT IEKISSIONSI
F/A IEMISSIONS.CALC)
1Z7 12* 129
31,. 3
5.0%
27560.00
106.0
3.0
59.00
1<>.17
1.8.28
318.00
868.0
11.. 12

67.590
210.993
22.1.00
1.991
15.200

3.837
20.981
3.659

.<>07
2.Z2*
.388
99.17
.0096
52.5
7.70
27530.09
119. t
2.9
59.00
lS1
99.37
.0187
67.8
9.96
27530.00
130.0
2.9
58.00
l16
22.800

2. l
15.790
3.781,

.279
2.053
.<>92
99.
.0116
130
203. >t
29.86
1.1710.00
260.0
7.9
59.00
H.. 17
133.50
639.00
1097.0
11.. 86

6.601
69.41.6
55.803
1.977
VI. 300

.382
7.021.
9.271

.099
1.826
2.".11
99. tO
.0095
131
1.76.2
69.87
M720.00
355.0
7.8
60.00
I*. 17
11(0.96
650.00
1315.0
K..07

2.700
32.851
66.500
2.71*
79.800

.111.
2.1.27
10.1.95

.01.0
.861
3.726
99.93
.0129
132
633.0
93.01.
1.1720.00
417.0
7.9
58.00
li>.17
H.5.1.5
655. 00
1*1.2.0
It. 11

2.400
23.190
102.750
3.159
9*. 750

.187
1.517
11.715

.035
.617
4.361
99.96
.0150
133
683.0
100.38
1.1690.00
W36.0
7.8
58.00
11.. 17
H.7.35
656.00
11.87.0
lit. 12

1.500
21.057
110.000
3.327
10*. 500

-------
0)
to
o
CD
                    CNC HFC I AtBf^c.oru     •••••••»••«»•»••»•   EPA  CYCcE EMISSIONS COMPUTATION SUMMARY  »»»•»
                    m^r £n .     ?««, e  «.      ESI  F*CIL  '  PHX  L*CCZ  INSTR OESCRIP • FED REG V38 N136
                    MODEL NO.f     TPE331-S-Z51H      S/NI    POV001               ENGINE TYPEICLASSIl  TiiPBnBDnD
                    RATED PCWERi    706.0 SHP  AT  SEA  LEVEL  STANDARD  DAY  CONDITIONS     TYP£ICL»SS"  TURBOPROP
                    FUEL1 ASTM D1655-73            ATOKIC H/C RATIO!    1.928     LHV1 18*70. BTU/LB
                                                                                                         ADDITIVES!  NONE
 CALC DATE 110-28-75
 CALC IDI   t
TEST NOI  7

> "ODE TAXI-IOLE TAXI-IOLE APPROACH
TIME IN MODE. MINUTES
> RATED POWER. PERCENT
CORRECTED POWER. HORSEPCNER
HP-HR
' FUEL FLCW. LB/HR
FUEL MASS. LB
< . *» HYDROCARBON EMISSION (HC) ••
INDEX. LB HC/1800 LB FUEL
RATE. LB HC/HR
MASS, L8 HC
MASS. PERCENT OF TOTAL CYCLE
CYCLE. LB HC/1000 HORSEPOWER-HR PER CYCLE
•• CARBON MONOXIDE EMISSIONS (CO) ••
INDEX, LB CO/ 1000 LB FUEL
I RATE, LB CO/HR
MASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE. LB CO/1000 HORSEPOWER-HR PER CYCcE
*• TOTAL OXIDES OF NITROGEN EMISSIONS (NOX) ••
INDEX, LB NOX/1000 LB FUEL
RATE. LB NOX/HR
HASS. LB NOX
MASS, PERCENT OF TOTAL CYCLE
CYCLE. LB NOX/1000 HORSEPOWER-HR PER CYCLE
) ' "•"""•"••" 	 	
•• EMISSION INDEX LEVELS REQUIRED
EPA LTO-CYCLE
POLLUTANT LBP/1011 HORSEPOWcR-HR-CYCLE
: CO 26.1
HC fc 9
NOX 12^9
)
7.000
5.030
15.300
"i.llB
105.782
12.3*1

3.876
.'o«,8
2*. 7

21.1*9
2.227
.260
22.9

3.653
.386
.0*5
8.1

TO HEcT EPA




19.000 *.500
5.000 30.000
35.300 211.800
11.178 15.885
105.7(2 261.006
33.*98 19.575

3.876 .3*8
•»10 .091
.130 .007
67.2 3.5

21.1*9 6.981
2.227 1.822
.705 .137
62.1 1Z.O

3.653 9.320
.386 Z.*3Z
.122 .182
22. 0 32.7

1979 STANDARDS FOR CLASS
REQUIRED EMISSION
POLLUTANT (MODE)
*CO (IDLE)
HC (IDLE)
NOX (TAKEOFF)
CLIHBOUT
2.500
90.000
635. «01
26.*75
391.399
16.308

.53*
.209
.009
*.5

1.757
.688
.029
2.5

11.277
*.02Z
.168
30.1

P2 ENGINES •»
TAKEOFF TOTAL PER
.510
111.100
706.011
5.883
»35.3**
3.628

.019
.008
.000
.0

1.261
.5*8
.115
.*

10.9*6
«.765
.0*0
7.1


33.500
63.5*0
85.351

2.26«
.3*6
.193
100.1
3.8*1

13.295
2.132
1.135
100.0
17.859

6.SZ8
.991
.557
101.1


INDEX. LBP/1011 LB FUEL
A
21.0
3.9
11.9
|
33.*
6.5
Z*.8



                                            ASSUMES PROPORTIONAL REDUCTION OF POLLUTANT EMISSION  INDEX AT EACH  LTD CYCLE NODE

                                            ASSUMES (1) REQUIRED REDUCTION IN CO AND HC OBTAINED  BY LOWERING EMISSION INDEX HALUTS

                                            «JOUCA?^«0r5 :^En«?i,*' " *M" W £"«IO"S " O^ER  MOOES SM« SSSSSeSr^W  SSSw. •
                                            REDUCTION II NOX OBTAINED BY LOWERING EMISSION INDEX  VALUES AT CLIMOUT AND TAKEOFF  MOOES IN
                                                        ION AS MEASURED VALUES.  NOX EMISSIONS AT  TAXI-IOLE AND APPROACH	
-------
(D

NJ
O
ENGINE' TPE331-S-Z51H S/N« P04001 COMB P/N= 869082-4
RAT SHP- 706. RA EGT,F=
FUEL H/C« 1.9280 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POWER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SFEED, Ml, RPM
COMPRESSOR INLET TEMP., DEE. F
COMPRESSOR OSCHG. PRES..PSIA
COMPRESSOR OSCHG. TEHP.OEG F
TURB INTERSTAGE TEMP.. OEG.F
CORR BELMTH FLON, LB/SEC
FA RATIO BASED ON BELLNTH.
MEASURED FUEL FLON, LB/HR
Ft RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING W/P"N/V/E«T/540>
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME. MET
LB. COZ PER LB. OF FUEL
HEIGHT FLOW, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, WET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
UNBURNEO HYDROCARBONS- FPN AS
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
RATIO LB HC/LB CO
NITRIC CXIDE CNOI - HEIGHTS AS
FPM BY VOLUME, MET
LB. PER 1080 LB. OF FUEL
HEIGHT FLOM, LB./HR.
NITROGEN DIOXIDE CN02I
PPM BY VOLUME, MET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
1650.
.06822
1Z7
5.0
35.6
34.3
Z7560.0
59.0
4S.3
318.0
868.0
2.98
.0103
106.0
.0096
.141
.326
99.170

1.99
3.11
3Z9.7

211.0
Z0.981
2.224
RAT SPO
L H ».
1Z8
7.7
54.4
52.5
27530.0
59.0
48.6
318.0
939.0
Z.94
.0117
119.0
.0107
.157
.318
99.372

2.23
3.12
371. Z

198.4
17.682
2.104
CARSON, WEIGHTS AS
67.5
3.837
.407
.1829
NOZ
15.2
2.483
.263

7.Z
1.176
.125
47.4
2.41-
.287
.1365

20.0
2.9ZJ
.348

5.9
.864
.103
= 41730.
= 18470.
129
10.0
70.3
67.8
27530.0
58.0
49.1
314.0
987.0
2.91
.0129
130.0
.0116
.170
.312
99.440

2.42
3.12
406.0

19Z.O
15.790
2.053
CH4
45.6
2.144
.279
.1358

2Z.8
3.081
.401

5.2
.703
.091
DEM PT,F=
S LN T.F*
130
Z9.9
210.8
203.4
41710.0
59.0
133.5
639.0
1097.0
7.88
.0095
260.8
.0095
.139
.080
99.801
REDUCED
1.98
3.14
816.9

69.4
7.024
1.626

6.6
.382
.099
.0543

41.3
6.862
1.784

14.5
2.409
.626
51.
300.0
131
69.9
493.3
476. Z
41720.0
60.0
141.0
650.8
1315.0
7.83
.0131
355.0
.0129
.189
.071
FUEL
REL HUM-
FLO, L/M=
132
93.0
656.9
633.0
41720.0
58.8
145.5
655.0
1442.0
7.86
.0149
487.0
.0150
.220
.067
99.933 99.957
= AV. KERO. TEST NO.* 7
78.80 SPEC HUH« .007908
14.160 SL TIH.S* 6.5000
133
108.
718.
683.
41698.
58.
147.
656.
1487.
7.84
.0160
436.1
.0158
.231
.065
99.966

2.71
3.15
1118. Z

32.9
2. 427
.861

Z.7
.114
.040
.0470

79.8
9.682
3.437

6.7
.813
.289
3.16
3.15
1282.6

23.9
1.517
.617

2.4
.087
.035
.0574

94.7
9.880
4.021

8.0
.834
.340
3.33
3.15
1374.2

21.1
1.278
.554

1.5
.052
.023
.0487

184.5
10.349
4.512

5.5
.545
.237
TOTAL OXIDES OF NITROGEN (NC+NOZI AS NOZ
PPM BY VOLUME, MET
LB. PER 1080 LB. OF FUEL
WEIGHT FLOW, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLCM
SMOKE NUMBER
CORRECTED HEIGHT FLON
SMOKE NUMBER
CORRECTED HEIGHT FLON
SMOKE NUMBER
CORRECTED WEIGHT FLCH
SMOKE NUMBER
SMOKE NUMBER AT MA=0.023
22.4
3.659
.388

.81718
3.50
.12124
5.88
.13546
9.38
.14973
18.50
7.38
25.3
3.791
.451

.01713
4.70
.02139
4.70
.03572
5.80
.05001
8.10
5.88
28.0
3.784
.492

.00715
4.70
.02144
5.88
.03573
4.70
.05011
7.00
5.50
55.8
9.271
2.411

.00715
5.80
.02144
10.51
. 0 3573
16.38
. 05DOZ
18.60
12.80
86.5
10.495
3. 726

.00716
5.80
.02148
17.40
.03579
22.10
.05011
26.70
18.10
102.7
10.715
4.361

.01716
8.18
.02148
14.00
.03586
18.60
.05021
24.40
16.38
111.8
10.894
4.750

.11717
7.08
.02152
14.00
.03586
19.81
.05021
28.98
15.41
                                                                                                                                                                   1

                                                                                                                                                                   3
                       NOTES  1.  »LL  EMISSIONS CONCENTRATIONS ARE MET VALUES.
                             Z.EQUIVALENCE RATIO CALCULATED FROM COZ,CO.AND HC DATA AND FUEL COMPOSITION.
                             3.MASS  EMISSIONS CF NO, NOZ, AND NO»N02 CALCULATED AS NOZ FROM CONCENTRATIONS WITH MOLECULAR HEIGHT OF NOZ (46.111.
-------
pj
(D
ro
(-•
o
                                                                                                                                                                CO
                         •••••••••••••»•••••••••••••••••»..••»•»  AIRESEARCH EMISSION  TEST  SUMMARY   ••••••»»•»...«
                   ENG MFC I AIRESEARCH           TEST FACIL I PHX LACCZ  INSTR DESCRIP  I FED RE6 V3* N136
                   2?5fn 25*'     TPE331-5-2S1*     S/NI   P04001              ENGINE  TYPE(CLASS)•   TURBOPROP
                   RATED POWERI    706.0 SHP AT SEA LEVEL STANDARD DAY CONDITIONS
                   FUELI «STM 01655-73            ATOMIC H/C RATIOI   1.928     LHVI 10470. BTU/L8     ADDITIVES!
                                                                                                                   NONE
                 CALC DATE 110-28-75
                 CALC 101   2
                TEST MOI  7
                            EXHAUST EMISSIONS PER EPA CYCLE OF WORK OUTPUT •• CODE OF FEDERAL REGULATIONS TITLE 40 PART 87  17 JULY 197J
                                       HYDROCARBONS (CH AS CH4I          2.816 LB. POLLUTANT PER 1000 HP.-HR.PcR CYCLE
                                       CARBON KONOXIDE (COI             18.986 L8. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                       OXIDES OF NITROGEN (NOX AS N02)   9.0SO LB. POLLUTANT PER 1000 HP.-HR. PER CYCLE

                             SETTI«,  5?rE   P^CENT ,AT£0 TAKEOFF POW^'.T
FUEL INJ T»P£i  STArpn
                                                                                DESCRIPTION  »••••"••
                   CCM8 TYPEI  REVERSE  FLOW ANNULAR            P/NI   659082-4           SU3/VOLI 1.260
                   ENGINE TOTAL  SERVICEI   O.I       HR    TIME SINCE ENGINE OVERHAUL!  0.0       MR
                   ENGINE ASSEMBLY  AND MAINTENANCE  INFORNATIONI
                   AIRCRAFT  INSTALLATION  •••• HFR. I                                  HOOEL N0.«
                                              USER"                        ENGINE INSTALLATION POSITIONI
                                                                                                        •••••••*••»•••••••*•••••••*•••»•»»...»»
                                                                                                             BARO PRESS I  28 160 TM  MCI
                                                                                                        FIC HUMIOITYI   007500 L8. H20*S* DRY
                                                                                                                                         '      PPNV
GASEOUS EMISSION TEST NO. 1 7 OATE1 10-28-75 TIMEI BARO PRESS 1 28 160 TM MCI
AMBIENT AIR TENP.t 59.00 DEG. F RELATIVE HUMIDITY. 70.00 PERCENT SPECIFIC HUMIDITY. 007500 L8. H20*S* DRY AI
AMBIENT AIR QUALITY MYOROCAR30NS (HOI 0.0 PPMC CARBON MONOXIDE (CO) 1 0.0 PPMV OXIDES OF NITROGEN (NOXll'o 0 P
) SAMPLE LINE «• TEMP.. 300.00 OEG. F. FLOWRATE. 14.16 LITERS/HIN. TRANSPORT TINE. l.lo SEC. ?ENG?H. sS.OO
•> TEST CONDITION
ACTUAL POWER SETTING. HORSEPOWER
CORR. POWER SETTING (STO DAY), PERCENT RATED
Nl SPEED, RPN
FUEL FLCH INEAS.I LB./H8.
CORR. ENGINE CORE AIRFLCN IMEAS) . LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., DEC F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS., PSIA
> COMPRESSOR DISCHARGE AIR TOTAL TEMP.. OEG F
TUR3INE INTERSTAGE GAS TOTAL TEMP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
) EMISSION CONCENTRATION, WET ANALYSIS
HYDROCARBON (HC AS CH4) , PPMC
CARBON MONOXIDE (CO), PPHV
) TOTAL OXIDES OF NITROGEN (NOX), PPHV
CARBON DIOXIDE (C02I , PERCENT BY VOL.
NITRIC OXIOE (NO), PPMV
EMISSION INDEX, LB. POLLUTANT/ 10 80 LB. FUEL
HYDROCARBONS (HC AS CH4I
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS NO2I
EHISSIC* RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CM4I
CARBON MONOXIDE 
-------
tt>
                                                                            EMISSIONS CORPUTATION SUMMARY  •••••••«••
                     £N6 MFG I AIRESEARCH           TEST  FACIL  I  PHX LACC2  IMSTR DESCR1P I FED REG V38 N136
                     MODEL NO.t     TPE331-5-251M      S/NI    P0*001              tNGINE TYPE(CLASS)I  TURBOPROP
                     RATED PONERI    7B6.0 SHP AT SEA  LEVEL  STANDARD DAY CONDITIONS
                     FUEL1 ASTM 01655-73            ATONIC H/C  RATIO!   1.928     LHVI 18*70. BTU/LB     AOOITIVESI
                          CALC DATE 110-21-75
                          CALC IDI   2
                         TEST NOI  7
                                                                                                                      NONE
H 0 0 E
TIME IN HOOEt MINUTES
RATED POWER. PERCENT
CORRECTED POWER, HOftSEPOMER
HP-HR
FUEL FLOW, LB/HR
FUEL MASS, LB
•• HYDROCARBON EMISSION 


21.958
2.365
.276
22.9


3.58A
.387
.01.5
7.8

TAXI-IDLE
IOUT)
19. got
5.000
35.310
11.178
107.719
3*. Ill

3.612
.389
.123
68.9


21.958
2.36$
.71(9
62.1


3.588
.387
.122
21.3

APPROACH
*.510
30.001
211.800
15.885
266.778
20.008

.1.61
.123
.009
5.2


7.1.65
1.991
.11.9
12. <»


9.207
2.»56
.181,
32.0

CLIMBOUT
2.500
90.000
635.100
26.l>75
1.09.726
17.072

.053
.022
.801
.5


1.582
.61.6
.027
2.2


10.758
*.*08
.181,
31.9

TAKEOFF
.500
1(0.000
706.800
5.883
".36.0*9
3.63<>

.ll»*
.019
.010
.1


1.387
.605
.005
.*


11.918
-------
                                                                                                                                                             CO
CD
ENGINE* TPE331-S-Z51H S/N« P04001
RAT SHP« 706. RA EGT,F« 1650.
FUEL M/C» 1.9280 STOI F/A= .0682Z
DATA POINT NUMBER
PERCENT MAX. CORRECTED PONES
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Nl, RPM
COMPRESSOR INLET TEMP.,OEG.F
COMPRESSOR DSCHG. PRES. >PSIA
COMPRESSOR DSCHG. TENP.DEG F
TURB INTERSTAGE TEMP., OEG.F
CORR BELMTH FLOH, LB/SEC
FA RATIO BASED ON BELLMTH.
MEASURED FUEL FLOH, LB/HR
FA RATIO CA1.C. FROM EMISSION
EQUIVALENCE RATIO
LCAOING H/P»»N/V/£«T/5*OI
COMB EFFIC FROM EMISSIOKS
CARBON DIOXIDE
PERCENT BY VOLUME. NET
) LB. COZ PER LB. OF FUEL
NEIGHT FLOM, LB./HR.
CARBON MONOXIDE
) PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
NEIGHT FLOH, LB./HR.
UNBURNED HYDROCARBONS- PPM AS
FPH BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
RATIO LB HC/LB CO
NITRIC CXIOE INOI - HEIGHTS AS
PPK BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLON, LB./HR.
) NITROGEN DIOXIDE (NOZI
PPM BY VOLUME, NET
LB. PER 1000 LB. Of FUEL
HEIGHT FLON, LB./HR.
13*
5.1
35.8
3*. 5
27550.8
59.0
48.1
320.0
860.0
2.98
.0104
100.0
.0099
.1*5
.327
99.171

Z.O*
3.11
335.9

225.2
21.874
2,362
COHB P/N= 059002-*
<*AT SPO* 41730. OEH PT,F» 51.
L H V= 18*70. S IN T,F» 300.0
135
7.5
53.1
51.2
27550.0
58.0
48.6
318.0
931.0
2.93
.0117
119.0
.0107
.156
.318
99.342

2.21
3.1Z
371.0

206.3
18.497
2.201
136
9.9
70.1
67.7
27550.0
- 60.0
48.9
322.0
1000.0
2.88
.0131
131.0
.0118
.173
.306
'SUMMARY OF
2.46
3.13
409.5

186.9
15.131
1.982
CARBON. HEIGHTS AS CH4
6*. 5 .
3.582
.387
.1637
NOZ
16.0
Z.553
.276

6.5
1.937
.112
49.5
2.537
.392
.1371
19.0
2. 798
.333

6.1
.89*
.107
36.9
1.708
.1120
23.8
3.165
.415

5.7
.758
.099
137
29.3
207. 0
199.*
41730.0
50.0
134.1
639.0
1094.0
7.89
.0095
262.0
.0096
I 080
99.790
REDUCED
2.00
3.14
823. 6

73.Z
7.339
1.923

7.5
.430
.113
.0585
41.1
6.764
1.772

13.8
Z.Z71
.595
130
69.9
493.3
475.3
41730.0
50.0
141.7
6*8.0
1311.0
7.85
.0130
356.0
.0129
FUEL
REL HUH*
FLO,t/M»
139
90.1
635.8
612.7
41750.0
58.9
145.5
655.9
1429.0
7.85
.9159
410.9
.0148
.189 • £*•*
.071 .067
99.932 99.958

2.71
3.15
1121.3

34.1
2.5ZZ
.096

Z.*
.102
.036
.0*03
77.0
9.361
3.332

7.5
.912
.325
TOTAL OXIDES OF NITROGEN INC+NOZ) AS NOZ
PPM BY VOLUME, HET
LB. PER 1000 L8. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED NEIGHT FLCH
SHOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
COKRECTEV WIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLCH
SHOKE NUMBER
SHOKE NUMBER AT H«»«.»Z3
22.5
3.599
.3S8
i
.99719
3.50
.02156
5.99
.03593
5.90
.05021
9.30
6.18
25.1
3.696
.4*0
»
.00717
1.20
.02156
5.09
.03506
7.00
.05021
7.00
5.29
29.5
3.923
.514

.00717
3.50
.02152
3.50
.03506
7.09
.05039
0.10
5.50
54.9
9.035
2.367

.08719
5.09
.02156
12.60
. 0 3593
15.10
.C5030
20.90
13.70
»4.5
19.273
3.657

.00719
7.99
.02160
15.10
.93599
Z4.40
.05039
27.90
18.60
3.11
3.15
1292.1

2*. 7
1.595
.65*

1.5
.955
.923
.03*7
95. Z
10.101
*.1*2

6.3
.663
.272

101.5
10.76*
4.413

.00720
9.19
.9216*
1*. 09
.03606
20.90
.050*9
23.30
16.51
= AV. KERO. TEST NO.' 7
70.00 SPEC HUM* .007599
14.160 SL TIN.S* 6.5000
1*8
100.0
706.3
660.
41730.
58.
1*7.
657.
1462.
7.0*
.0160
436.0
.0158
.231
.065
99.964

3.3Z
3.15
137*. Z

22.7
1.369
.597

1.2
.0*1
.918
.9392
19*. 2
10.3*3
*.509

5.9
.570
.2*9

110.0
10.913
4.758

.00721
7.90
.0216*
11.60
.03696
19.00
.059*9
25.40
16.00
                  NOTES  1.  ALL EMISSIONS  CONCENTRATIONS ARE HET VALUES.
                        Z.EQUIVALENCE  RATIO CALCULATED  FRCH COZ,CO,AND MC DATA AND FUEL  COMPOSITION.                  „_„... ». „„, ...  .,,
                        3.KASS EMISSIONS  OF NO. NOZ.  AND NO*NOZ CALCULATED AS NOZ  FROM CONCENTRATIONS  HIM  MOLECULAR HEIGHT OF NOZ (46.011.
-------
                                                                               EMISSION TEST SUMMARY  ••»••»••««»•••
                    ENG MFG I AIRESEARCM            TEST  FACIL < PHX LACC2  INSTR OESCRIP I FED REG V38  N136
                    MODEL NO.I     TPE331-5-251M      S/NI    P04001              ENGINE TYPE(CLASS!I  TURBOPROP
                 )   RATED POWER I     706.0  SHP  AT  SEA  LEVEL STANDARD DAY CONDITIONS
                    FUELI ASTM 01655-73             ATOMIC  H/C RATIO!   1.928     LHVI 18470. BTU/LB      ADDITIVES!
 CALC DATE 110-29-75
 CALC IDI   3
TEST NO!    7
                                                                                                                      NONE
                    ••«••»•• EXHAUST  EMISSIONS  PER EPA CYCLE OF WORK OUTPUT •• CODE OF FEDERAL REGULATIONS  TITLE 40 PART 87  17 JULY 1973  «••»*•»
                                         HYDROCARBONS  ICH AS CH4)           2.673 LB. POLLUTANT PER  1000  HP.-HR.  PER CYCLE
                                         CARBOK  KONOXIOE (CO)             17.634 LB. POLLUTANT PER  1000  HP.-HR.  PER CYCLE
                                         OXIDES  OF  NITROGEN (NOX AS NOZ)   8.899 LB. POcLUTANT PER  1000  HP.-HR.  PER CYCLE
                                         SMOKE                              18.9  SMOKE NUMBER, MAXIMUM AT  CRUISE    MODE,  70 PERCENT RATED POWER
                    TAXI-IDLE  SETTING!  5.0       PERCENT SATED TAKEOFF POW£R AT 65.      PERCENT RATED TAKEOFF  Nl RPM
 ••a
 JD
LQ
 (D

 NJ
 I—'
 CO
                    ,,.,.,.,............„..............,.»..,..„......,  ENSINE DESCRIPTION   ••»»*•»••••»»»••»•»»»•»••»»»•»»»»»»•••»•»»»••«•»»•••
                    COM3 TYPE! REVERSE  FLOW ANNULAR            P/N«   86908Z-4           SUR/VOi.!  1.260   FUEL  INJ TYPEI  STAGED SIMPLES
                    ENGINE TOTAL SERVICEI  0.0        HR     11 Me. SINCE ENGINE OVERHAULI  0.0        HR
                    ENGINE ASSEMBLY AND MAINTENANCE  INFORMATION!
                    AIRCRAFT INSTALLATION "•* HFR.I                                  MODEL NO.I
                                               USER!                        ENGINE INSTALLATION POSITION!
                    ••»»»•»»»»»*••»»»•»»»»»•»•»»»•*»«»»»»»»*»»»»»»»»OPERAT10NAL TtST DATA SUMMARY  •••••»••»••••••»»•«•••••••»»«»••»»•••«••••*•••»»
                    GASEOUS EMISSION TEST NC.I    7          DATE!  10-29-75           TIME!                     BARO PRESS.!   28.980 IN. HGA.
                    AMBIENT AIR TEMP.I  59.00 OEG. F         RELATIVE HUMIDITY!  70.00 PERCENT       SPECIFIC  HUMIDITY!  .007500 LB. H20/LB. DRY AIR
                    AMBIENT AIR QUALITY   HYDROCARBONS  (HC)I  0.0    PPMC     CARBON MONOXIDE 
99.21
.0095
50.6
7.1.2
27520.00
117.0
2.9
57.00
14.23
4».8£
317.00
932.0
l39
99.39
.0105
70.0
10.26
2751(0.00
132.0
2.9
56.00
14.23
49.51
318.00
1000. 1
14.20

36.000
178.691
28.900
2.<>88
22.900

1.646
It. 295
3.798

.217
1.887
.501
99.52
.0119
I".*.
208. 4
30.5*
41760.00
259.0
7.8
57.00
14.23
134.66
653.00
1103.0
14.11

6.600
61.036
56.000
2.000
42.500

.377
6.115
9.201

.098
1.581
2.383
99.82
.0096
145
476.1
69.82
41750.00
356.0
7.9
56.00
14.23
142.44
648.00
1306.0
14.13

2.700
27.546
82.500
2.747
75.000

.113
2.011
9.894

.040
.716
3.522
99.94
.0131
146
613.1
89.40
41740.00
405.0
7.8
62.00
14.23
145. Z*
658.00
1435.0
14.17

1.500
19.846
100.250
3.089
95.000

.056
1.289
10.693

.023
.522
4.331
99.96
.0147
147
679.4
99.45
41720.00
431.0
7.8
58.00
14. 23
147.99
657.00
1478.0
14.18

1.200
19.442
107.500
3.267
102.500

.042
1.194
10.844

.018
.515
4.674
99.97
.0155
                                         3

                                         3

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                                         3

                                         3

                                         3

                                         3

                                         3

                                         3

                                        3
                                                                                                                                                                  £.
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ENG MFC 1 AIRESEARCH TEST FACIL 1 PHX
fOOEL NO.I TPE331-5-251N S/Nt P04001
RATED POHERI 706.0 SHP AT SEA LEVEL STANDARD
FUEL I ASTH 01655-73 ATOMIC H/C RATIOS
NODE

TIME IN MODE, MINUTES
) RATED POKER, PERCENT
CORRECTED POKER, HORSEPOWER
HP -MR
1 FUEL FLCM, LB/HR
FUEL MASS. LB
•• HYDROCARBON EMISSION (HCI ••
INDEX, LB MC/1011 LB FUEL
RATE, LB HC/HR
MASS, L6 HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1100 HORSEPOHER-HR PER CYCLE
)
•* CARBON HONOXIDE EMISSIONS (CDI »»
INDEX, LB CO/1001 LB FUEL
> RATE, LB CO/HR
MASS. LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1001 HORSEPOHER-HR PER CYCLE
•• TOTAL OXIDES OF NITROGEN EMISSIONS (NOXI ••
.' INDEX. LB NOX/1010 LB FUEL
RATE. LB NOX/HR
MASS. LB NOX
MASS. PERCENT OF TOTAL CYCLE
CYCLE, LB NOX/1010 HORSEPONER-HR PER CYCLE


LACC2 INSTR OESCRIP 1 FED REG V38 N136
cNGINE TYPEICLASSM TURBOPROP
DAY CONDITIONS
1.928 LHVI
TAXI-IDLE
(INI
7.100
5.001
35.300
4.118
108.043
12.605

3.432
.371
.043
25.5



20.839
2.252
.263
23.4


3.647
.394
.046
•.1

CALC
CALC
DATE 110-29-75
IO« S
TEST NOI 7
18471. BTU/LB
TAXI-IDLE
IOUTI
19.000
5.000
35.300
11.178
108.043
34.214

1.432
.371
.117
69.1



20.839
2.252
.713
63.6


3.647
.394
.125
22.1

ADO ITI VESI NONE
APPROACH

4.500
30.001
211.811
15.885
256.424
19.232

.445
.114
.009
5.0



6.177
1.584
.119
10.6


9.013
2.311
.173
30.7

CLIMBOUT

2.500
90.000
635.400
26.475
406.501
16.938

.012
.005
.000
.1



1.286
.523
.ozz
1.9


10.797
4.389
.183
32. 3

TAKEOFF

.500
110.100
716.111
5.883
432.607
3.605

.125
.054
.000
.3



1.179
.511
.004
.4


10.678
4.619
.138
6.8

TOTAL PER
CYCLE
33.511


63.541

•6.591

1.962
.314
.171
110.1
2.673


12.948
2.817
1.1ZI
110. 1
17.634

6.531
1.113
.565
111.1
• .199
                                          ••  EMISSION  INDEX  LEVELS REQUIRED TO MEET EPA 1S79 STANDARDS FOR CLASS PZ ENGINES ••
                                                                                               REQUIRED EMISSION INDEX,  LBP/KOD LB FUEi
POLLUTANT (HOOEI
CO (IDLE!
HC (IDLE!
NOX (TAKEOFFI
A
20.8
3.4
11.7
B
33.3
6.5
22.9
                                      EPA  LTO-CYCLE
POLLUTANT   LBP/10QO HORSEPOHER-HR-CYCLE
   CO             26.8
   HC              4.9
   NOX            12.9
          A  ASSUMES  PROPORTIONAL REDUCTION OF POLLUTANT EMISSION INDEX  AT  EACH  LTD CYCLE  MODE

          B  ASSUMES  (II REQUIRED REDUCTION IN CO AND HC OBTAINED BY  LOWERING EMISSION INDEX VALUES
             AT  TAXI-IDLE NODE  ONLY,  CO  AND HC EMISSIONS AT OTHER MODES  REMAIN UNCHANGED,  (21 REQUIRED
             REDUCTION IN NOX OBTAINED BY LOWERING EMISSION INDEX VALUES AT CLIMBOUT AND TAKEOFF MODES IN
             SAME PROPORTION AS MEASURED VALUES.  NOX  EMISSIONS AT TAXI-IDLE AND  APPROACH NODES
             REMAIN UNCMAN6EO
                                                                                                                                                               >

                                                                                                                                                               )

                                                                                                                                                               >
-------
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ENGINE* TPE331-S-ZS1M S/N« P04001 COMB P/N* 869082-4
RAT SHPa 706. RA EGT.F*
FUEL H/C* 1.9280 STOI F/A=
OATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Nl, RPM
COMPRESSOR INLET TEMP..OEG.F
COMPRESSOR DSCHG. PRES. .PSIA
• COMPRESSOR DSCHG. TEMP, EEC F
TURB INTERSTAGE TEMP., OEG.F
CORR BELMTH FLOH, LB/SEC
FA RATIO BASED ON BELLMTH.
MEASURED FUEL FLOH, L8/HR
FA RATIC CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P»»N/V/EIT/540I
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
) LB. COZ PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
) PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBUPNED HYDROCARBONS- PPM AS
PPP BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC CXIOE (NOI - HEIGHTS AS
PPM BY VOLUME, HET
LB. PER 100D LB. OF FUEL
HEIGHT FLOH, LB./HR.
) NITROGEN DIOXIDE CNOZi
FPM BY VOLUME, NET
LB. PER 1000 LB. OF FUEL
) HEIGHT FLOH, LB./HR.
1650.
.06622
141
5.0
35.2
34.
27540.
56.
48.
317.
873.
2.97
.0104
108.0
.0095
.139
.325
99.207

1.96
3.11
336.1

206.8
20.861
2.253
RAT SPO
= 41730.
L H If 18470.
142
7.4
52.4
50.6
27520.0
57.0
46.8
317.0
932.0
2.90
.0116
117.0
.0105
.154
.314
99.392

2.17
3.12
365.1

192.4
17.570
2.056
CARBCN, HEIGHTS AS
59.7
3.442
.372
.1650
N02
15.2
2.519
.272

6.8
1.127
.122
42.6
2.223
.260
.1265

16.5
2.775
.325

6.5
.975
.114
143
10.3
72. 5
70.0
Z7540.0
56.0
49.5
316.0
1000.0
2.86
.0132
132.0
.0119
.175
.302
99.519

2.49
3.13
412.8

176.7
l*r. 295
1.887
CHi.
36.0
1.646
.217
.1152

22.9
3.009
.397

6.0
.788
.104
DEN PT.F* 51.
S 4.N T,F* 300.0
144
30.5
Z15.6
Z08.4
41760.0
57.0
134.7
653.0
1103.0
7.84
.0095
259.0
.0096
.140
.077
99.833
REDUCED
2.00
3.14
814.1

61.0
b.105
1.581

6.6
.377
.098
.0618

42.5
6.983
1.809

13.5
2. 218
.574
145
69.
493.
476.
41750.
56.
142.
648.
1306.0
7.87
.0129
356.0
.0131
.192
.071
99.943
FUEL
REL HUM*
FLO.L/M*
146
•9.
631.
613.
41740.
62.
145.2
658.0
1435.6
7.84
.0149
405.0
.0147
.215
.067
99.965
= AV. KERO. TEST NO.* 7
70.00 SPEC HUH* .007500
14.160 SL TIM.S* 6.5000
147
99.
70Z.
679.
41720.
58.
148.
657.
1476.
7.63
.0158
431.0
.0155
.227
.065
99.968

2.75
3.15
1121.6

Z7.5
2.011
.716

2.7
.113
.040
.0560

75.0
8.994
3.202

7.5
.699
.320
3.19
3.15
1276.5

19.6
1.289 '
.522

1.5
.056
.023
.0 AS N02
PPH BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DAT*
CORRECTED HEIGHT FLCN
SMOKE NUMBER
CORRECTED HEIGHT FLOH
; SMOKE NUMBER
CORRECTED HEIGHT FLCH
SMOKE NUMBER
) CORRECTED HEIGHT FLON
SMOKE NUMBER
SMOKE NUMBER AT HA-O.OZ3
22.1
3.646
.394

.00726
k.TO
.02179
7.00
.03632
8.10
.05065
9.30
7.20
Z5.0
3.750
.439

.00724
4.70
.02171
5.80
.03619
8.18
.05066
7.00
6.40
28.9
3.798
.501

.00721
3.50
.82163
4.70
.03605
5.60
.05038
5.60
4.90
56.8
9.Z01
Z.383

.00717
7.00
.02152
14.00
.03586
19.80
.05021
2Z.10
15.70
62.5
9.694
3.522

.00716
8.10
.02148
15.10
.03579
23.30
.05011
29.10
16.90
100.2
10.693
4.331

.01715
6.10
.02144
15.10
.03573
18.60
.05002
24.40
16.60
107.5
10.644
4.676

.01711
8.10
.02140
14.00
.03566
19.80
.04993
Z3.3I
. 16.30
                      NOTES 1.  ALL EMISSIONS CONCENTRATIONS ARE HET VALUES.
                            2.EQUIVALENCE RATIO CALCULATED FROM COZ.CO.ANO HC DATA AND FUEL COMPOSITION.
                            3.MASS EMISSIONS OF NO, NOZ. AND NO»NOZ CALCULATED AS N02 FROM CONCENTRATIONS HITH MOLECULAR HEIGHT OF N02  146.011.
-------
rur -cr .    ""*"•"****•*""•*""••*•»"   AI^ESEARCH  EMISSION  TEST SUMMARY  »..»».»»»
ENG MFC I AIRESEARCH            TEST FACIL  I PMX  _iCC2   INSTR  OESCRIP :  FED REG V38 N136
2??'!; ™'*      TPE331-S-2S1M     S/NI   P9U001              tNGINE  TYPE (CLASS) I  TURBOPROP
RATtO POWER!     706.0  SHP  AT SEA LEVEL STANDARD  DAY CONDITIONS
FUELt ASTM 01655-73             ATOMIC H/C RATIOI   1.9Z8      LHVI 18*7*.  8TU/LB
                                EXHAUST
                      TAXI-IDLE  SETTING
                                                                                      ADDITIVES!  NONE

                     «vns-,r.olLlP\CrCLE °F "°R< OUIf>UI "  COOE  OF  FEDERAL  REGULATIONS TITLE «,0 PART 87
                     HYOROCAReONS (CH AS CHl.»          2.711, LB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                     CASBON  MONOXIDE (CO)             17.726 LB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                     OXIDES  OF  NITROGEN (NOX AS N02)   8.*77 LB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                                       17.6
                             PERCENT RATED TAKEOFF POWER AT
                                                                                                                              CALC DATE I1I-Z9-7S
                                                                                                                              MLCTBl   1
                                                                                                                              CAL C 101   1
                                                                                                                                  17 JULY 1973
                                                                                                                                '°
                                                                                                                                           «"" «"
Ot
Id
ft)
NJ
                              -..•............»»..,».,,.................,„  ENGINE DESCRIPTION  •»»»•••••»••••••••••»»••«
                      COMB TYPEI  REVERSE  FLO*  ANNULAR           P/NI    S69082-*            SUR/VOLI 1.260  FUEL INJ  TYPEI
                      ENGINE TOTAL  SERVICE!  0.0        HR    TIME SINCE ENGINE OVERHAUL!   0.0       MR
                      ENGINE ASSEMBLY  AND MAINTENANCE INFORMATION!
                      AIRCRAFT INSTALLATION  ••••  MF*.I                                   HOOEL NO.I
                                                  USERl                        ENGINE  INSTALLATION POSITION!

                                                                                                                  BARO PRESS.!   28.980 IN.  HG».
                                                                                                             FIC HUMIOITYI   .010000  LB. H20/LB. DRY
                                                                                                                                                      PPMV
GASEOUS EMISSION TEST NO. 1 8 DATE! 10-29-75 TIME!
AMBIENT AIR TEMP.I 59.00 OEG. F RELATIVE HUMIOITYI 95.00 PERCENT
AMBIENT AIR DUALITY HT030CARBONS (HCII 0.0 PPMC CARBON MONOXIDE (CO)!
SPECIFIC
0.0 PPMV
BARO PRESS.! 28.980 IN. HG».
HUMIOITYI .010000 LB. H20/LB. DRY All
OXIDES OF NITROGEN (NCX)I 0.0 PI
SAMPLE LINE ••• TEMP.I 300.00 DEG. F. FLOWSJTEl 1*.16 LITERS/NIN. TRANSPORT TIMEl 6.50 SEC.
TEST CONDITION
ACTUAL POWER SETTING, HORSEPOWER
CORR. POWER SETTING (STD OAYI , PERCENT RATED
HI SPEED, RPM
FUEL FLCW (MEAS.) LB./HR.
CORK. ENGINE CORE AIRFLOW (NEAS), LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., OEG F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL TEMP., OEG F
TUR9IME INTERSTAGE GAS TOTAL TcMP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION. NET ANALYSIS
HYDROCARBON (HC AS CH») , PPMC
CARBON MONOXIDE (COI , PFMV
TOTAL OXIDES OF NITROGEN (NOX), PPMV
CARBON DIOXIDE (C02) , PERCENT BY VOL.
NITRIC OXIDE (NOI, PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH*t
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
EMISSICK RATE, LB. POLLUTANT /MR.
HYDROCARBONS IHC AS CH*)
CARBON MONOXIDE ICO)
TOTAL OXIDES OT NITROGEN (NOX AS N021
COMBUSTION EFFICIENCY, PEftCcNT (EMISSIONS)
»/A (EMISSIONS, CALC)
1*8 1*9 150
3*.l 50.5 68.3
•..97 7.39 9.98
27520.00 27530.00 27530.00
108.0 117.0 130.0
3.0 3.0 >.a
58.00
*«.77
311.00
857.0
14.20
61.500
211.931
21.000
2.009
13.000
3.1.65
20.888
3.1.00
.37*
2.256
.367
99.20
.0197
57.00
1.9.36
310.00
919.0
1*.20
5*. 000
206.316
23.000
2.19*
16.000-
2.791
18.655
3.*16
.327
2.183
.*08
99.32
.0116
60.01
*9.71
310.00
1000.0
1*.2D
39.000
168.279
27.600
2.*27
21.100
1.827
15.1.31
3.716
.238
2.886
.*«
99. *8
.0117
151
202.1
29.61
".1760.00
261.0
7.9
57.10
l*t. 23
135.17
631.00
1090.0
6.600
61.036
53.100
2.105
<.o.ooo
.376
6.191
8.70*
.098
1.590
2.272
99.82
.8096
152
*75.7
69.50
1.1720.00
3S-..0
7 A
f . D
60.00
1 /. y\
X H •£«
1*1.70
6*1.00
1310.0
11.. 12
2.1.01
29.583
79.750
2.709
72.100
.102
2.190
9.697
.036
.775
3.1.33
99.9*
.0129
153
613.*
89.71
1.1730.01
1.05.9
rQ
• V
59.11
1*6.37
6*7.00
1*25.0
1*.17.
2.*IO
20.653
95.250
3.12*
89.00*
.114
1.326
10.0*6
.036
.537
*.06I
99.96
.01*1
LENGTH! 50.00 1
15*
680.2
99.56
1.1728.00
*31.l.
7.9
58.00
1*9.17 "
6*8.11
1*72.1.
1*.18
1.211 	
23.079
100.750
3.327
95.000
.1*1 _
1.391
9.977
.011
.601
*.300
99.96
.1151
                                                                                                                                                                     J
                                                                                                                                                                     )
                                                                                                                                                                     i;
-------
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 (I)
                         ..........................................  EpA CTCLE EMISSIONS  COMPUTATION SUMMARY  »••»»•••«•
                         ENG MFC I AIRESEARCH            TEST FACIL < PHX LACC2  INSTR DESC11P  I  FED REG V38 N136.
                         MODEL NO.I     TPE331-5-251M     S/N»   POnOOl              ENGINE  TYPEICLASSII  TURBOPROP
                         RATED POKE*:    706.0  SHP  AT SEA LEVEL STANDARD DAY CONDITIONS
                         FUELI ASTM 01655-73             ATOMIC H/C RATIO!   1.928     LHVI 18470.  BTU/tB     ADDITIVES!
                          CALC DATE  110-29-75
                          CALC 101    1
                         TEST NOI    8
                                                                                                                           NONE
M 0 0 E

TIME IN MODE. MINUTES
RATED POWER. PERCENT
CORRECTED POWER. HORSEPOWER
HP-HR
FUEL FLCW. LB/HR
FUEL MASS, LB
*» HYDROCARBON EMISSION IHCI *»
INDEX. LB HC/1000 LB FUEL
RATE, LB HC/HR
MASS, LB HC
MASS. PERCENT OF TOTAL CVCLE
CYCLE. LB HC/1000 HORSEPOHER-HR~ PER CYCLE
»» CARBON MONOXIDE EMISSIONS ICOI ••
INDEX, LB CO/1008 LB FUEL
RATE, LB CO/HR
MASS, L8 CO
MASS, PERCENT OF TOTAL CYCLE
CVCLE. LB CO/1000 HORSEPOMEft-HR PER CYCLE
« TOTAL OXIDES OF NITROSEN EMISSIONS JNOX) •»
INDEX. LB NOX/1000 LB FUEL
RATE, LB NOX/HR
MASS, LB NOX
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB NOX/1000 HORSEPOWER-HS PER CYCLE
TAXI-IO..E
(INI
7.000
5.000
35.300
"..116
108.085
12.610

3. 460
.374,
.out,
25.3


20.871
2.256
.263
23.1,

3.398
.367
.01.3
8.0

TAXI-IDLE
IOUT)
19.000
5.000
35.300
11.178
108.085
34.22?

3.<>60
.371,
.118
68.7


20.871
2.256
.711.
63. 
.17".
32.2

CLIMBOUT

2.500
90.000
635.1.00
26.1,75
405.968
16.915

.112
.046
.002
1.1


1.377
.559
.023
2.1

10.066
4.086
.170
31.6

TAKEOFF

.500
100.008
706.000
5.883
431.592
3.597 .

.039
.017
.080
.1


1.236
.533
.004
.4

9.911
4.278
.036
6.6

TOTAL PER
CYCLE
33.5)0


63.541

87.093

1.980
.3(9
.172
100.1
2.714

12.932
2.017
1.126
100.0
17.726
6.184
.965
.539
100.0
8.477
                                               " EMISSION INDEX LEVELS REQUIRED  TO MEET EPA 1979 STANDARDS FOR CLASS P2 ENGINES «*
                                            EPA LTO-CYCLE
                                     POLLUTANT   LBP/1000 HORSEPOHER-HR-CYCLE
                                        CO             26.8
                                        HC              4.9
                                        NOX            12.9
                                                                                                     REQUIRED EMISSION INDEX,  LBP/1000 LB FUEL
POLLUTANT IMOOEI
   CO HOLE)
   HC (IDLE)
   NOX ITAKEOFFJ
   A
20.9
 3.5
 9.9
   B
33.2
 6.4
23.4
                                               A  ASSUMES PROPORTIONAL REDUCTION  OF  POLLUTANT EMISSION INDEX AT EACH LTO CYCLE HOOE

                                               B  ASSUMES (II REQUIRED REDUCTION  IN  CO  AND HC OBTAINED Br LOWERING EMISSION  INDEX  VALUES
                                                  AT TAXI-IDLE MOO- ONLY, CO AND  HC  EMISSIONS AT OTHtR MOOES REMAIN UNCHANGED. 121 REQUIRED
                                                  REDUCTION IN NOX OBTAINED 3V LOWERING EMISSION INDEX VALUES AT CLIM80UT AND TAKEOFF  MODES IN
                                                  SAME PROPORTION AS MEASURED VALUES, NOX EMISSIONS AT TAXI-IDLE AND APPROACH NODES
                                                  REHAIN UNCHANGED
-------
0)
^
(D
to
^-•
CO
                          XYXYXtXYXYXYXVXYXYXYXYXtXYXVXVXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXr
                          XYXYXVXYXYXYXVXYXYXYXYkrXYXYXYXYXYXrXYXVXYXYXVXYXrxYXYXYXYXYXYXYXVXYXYXYXYXYXYXYXYXYXY
ENGINE: TPE331-5-ZS1H i/N= P04101 COHB P/N= 8690S2-1. FUEL
RAT SUP* T06. RA EGT,F=
FUE.. H/C* 1.9280 STOI F/A-
OATA POINT NUMBER
PERCENT MAX. CORRECTED POWER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED t Nl, RPM
COMPRESSOR INLET TEMP..OEG.F
COMPRESSOR DSCHG. PRES.tPSIA
COMPRESSOR BSCHC, TENP.OES F
TURB IMTERSTA3E TEHP., DEG.F
CORR BELMTH FLOH. L8/SEC
FA RATIO BASED ON BELLHTH.
MEASURED FUEL FLOW, L8/MR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING W/P"N/V/E«T/540)
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, NET
L3. C02 PER LB. OF FUEL
WEIGHT FLOH, L6./HR.
CARBON MONOXIDE
PPM BY VOLUME, MET
L3. PER 1000 LB. OF FUEL
WEIGHT FLOM, LB./HR.
UNBURNED HYDROCARBONS- PPH AS
PPM BY VOLUME, NET
La. PER loan LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NOI - HEIGHTS AS
PPM BY VOLUME, WET
LB. PER 1000 LB. OF FUEL
WEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE IN02I
PPM BY VOLUME. HET
LB. PER 100! LB. OF FUEL
WEIGHT FLOH, LB./HR.
1650.
.OoSZZ
146
5.
35.
34.
Z7520.
58.
48.
311.
857.0
3.00
.0103
108.0
.0097
.142
.329
99.205

2.01
3.11
336.1

211.9
30.888
2.256
RAT SPO= 41730.
L H V
149
7.1,
52.2
50.5
27S30.0
57. 0
49.4
310.0
919.3
2.98
.0112
117.0
.0106
.155
.321
99.316

2.19
3.12
36».7

206.3
18.655
2.183
CARBON, HEIGHTS AS
61.5
3.465
.371,
.1659
N02
13.0
2.105
.227

8.0
1.295
.11(0
5k. 0
2.791
.327
.11,96

16.0
2.376
.278

7.0
1.0*0
.122
= ia47fl.
ISO
10.0
70.1.
68.3
27530. H
60.0
1.9.7
310.0
1000.0
2.89
.0129
130.0
.0117
.171
.306
99.W7T

2.1,3
3.12
1.06.2

ISA. 3
15.1.31
2.006
CHU
39.0
1.827
.238
.1181,

21.1
2.81,1
.369

6.5
.875
.111.
DEW PT,F*
S LN T,F=
151
29.6
209.1
202.1
1,1760.0
57.0
135.2
631.0
1090.0
7.89
.0095
261.0
.0096
.141
.080
99.821,
REDUCED
2.00
3.14
820.4

61.0
6.091
1.590

6.6
.376
.098
.1618

40.0
6.557
1.711

13.1
2.147
.560
57.
308. 0
152
69.5
490.7
475.7
417ZO.O
60.0
141.7
641.0
1310.0
7.83
.0130
354.0
.0129
.189
.072
99.948
EMISSION
2.71
3.15
1115.2

29.6
2.190
.775

2.4
.102
.036
.0464

72.0
8.754
3.099

7.8
.942
.334
REL HUH'
FLO..VM*
153
89.7
633.3
613.4
41730.0
59.0
146.4
647.0
1425.0
7.88
.0147
405.0
.0148
.218
.068
S9.961

3.12
3.15
1276.5

20.7
1.326
.537

2.4
.086
.036
.0664

89.0
9.386
3.802

6.3
.659
.267
> AV. KERO. TEST NO.* 6
95.00 SPEC HUH* .018000
14.160 SL TIM.S* 6.5000
154
99.6
702.9
680.2
41720.1
58.1
149.2
648.0
1472.0
7.68
.0157
431.0
.0158
.231
.065
99.964

3.33
3.15
1358.4

23.1
1.391
.600

1.2 	 	 . .. . .
.041
.118
.0297 . . . ... .

95.1
9.416 . . .
4.055

5.7
.569
.245
TOTAL OXIDES OF NITROGEN (NC»N02I AS N02
PPH BY VOLUME. WET
LB. PER 1000 LB. OF FUEL
WEIGHT FLOH. LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLCW
SMOKE NUMBER
CORRECTED HEIGHT FLOW
SHOW NUMBER
CORSECrttJ HETCWr FLOW
SMOKE NUMBER
CORRECTED WEIGHT FLCW
SMOKE NUMBER
SMOKE NUMBER AT WA*0.023
21.0
3.400
.367

.00713
g.oo
.02134
4./0
.0356<>
5.90
.0<,989
7.10
i>. <>0
23.0
3.1,16
.1.00

.00710
l.ZO
.02129
2.40
.0351,8
5.90
.04967
5.90
3.91
27.6
3.716
.1,83

.00709
2.1.0
.02126
3.50
.0351,3
3.50
.01,961
7.10
It. 10
93.1
6.704
2.272

.00706
4.70
.02119
10.60
.03532
16.50
.04945
21.20
13.40
79.7
9.697
3.433

.00703
5.90
.02110
15.30
.03517
22.40
.04924
25.90
17.60
95.2
10.04,6
4.068

.00702
5.90
.02107
11.80
.03511
17.61
.04916
24.70
15.21
100.7
9.977
4.310 	 	 	

.00701
3.59
.02111
11.68
.03499 	
16.50
.14699
22.41 	
13.51
                        NOTES 1. A.L EMISSIONS  CONCENTRATIONS ARE HET VALUES.
                              2.EQUIVALENCE  RATIO  CALCULATED FROM C02.CO.ANO HC DATA AND  FUEL COMPOSITION.
                              3.MASS EMISSIONS  OF  NO,  N02.  AND NO»N02 CALCULATED AS N02 FROM CONCENTRATIONS HITH HOLECUwAR WEIGHT OF  NO2  «.6.1U,
-------
                      ••»•••..».*»•.»»..•»•»-•.».-••..-».»...*.•»,.  AIRESEARCH EMISSION  TEST  SUMMARY   »••••••••»••••
                      ENG MFC > AIRESEARCH            TEST FACIL > PHX ..ACCZ  INSTR OESCRIP  t FC.O  REG  vss Ni36
                      MODEL NO.I     TPE331-5-251M      S/NI   P04001              ENGINE  TYPE(CLASS)I   TURBOPROP
                      RATED POMERI     706.0  SHP  AT  SEA LEVEL STANDARD DAY CONDITIONS
                      FUE.t ASTM 01655-73             ATOMIC H/C RATIO!   1.928     LHVI 18470. BTU/LB     AODITIVESI
 CALC DATE 110-29*75
 CALC ID!   Z
TEST NOI    8
                                                                                                                        NONE
                      "»"*»* EXHAUST  EMISSIONS  Pt* £PA C^CL£ OF HOR< OUTPUT •» C00£  OF  FEOERA;. REGULATIONS  TITLE «.fl PART 87  17 JULY 1973   •••»••»
                                           HYDROCARBONS (CH AS CH«)          2.787 ^B.  POLLUTANT  PER 1000 HP.-HR. PER CYCLE
                                           CARBON  MONOXIDE (CO)             17.108 LB.  POLLUTANT  PER 1000 HP.-HR. PER CYCLE
                                           OXIDES  OF  tUTROGEN (NOX AS N03)   8.276 LB.  POLLUTANT  PER 1000 HP.-HR. PER CYCLE
                                           SMOKE                              17.9  SMOKE NUMBER.  MAXIMUM AT CRUISE    MODE.  70 PERCENT RATED POHER
                      TAXI-IDLE SETTINGI  5.0       PtSCENT RATED TAKEOFF POHER AT 65.       PERCENT RATED TAKEOFF Nl RPM
(D

N)
                      .......,.,..,.,...»..,..,.,..,..»»...,.....„........  tHGIN£ DESCRIPTION   •••»»•-••-•••»»•»••»-«»»»»•»••-»--»»••»•»••-»•--»•••
                      COMB TYPEI REVERSE FLOH ANNULAR            P/NI   869082-4            SUR/VOL<  1.260   FUEL INJ TYPEI  STAGED SIMPLES
                      ENGINE TOTAL SERVICE 1  0.0        HR    TIMS. SINCE ENGINE OVERHAUL*   0.0        MR
                      ENGINE ASSEMBLY AND MAINTENANCE  INFORMATION!
                      AIRCRAFT INSTALLATION •••• MFR.I                                  MODEL NO.I
                                                 USE"?»                        ENGINE INSTALLATION POSITIONI
                      ..........I.................,,.....,.„....,....ap£^ATIOSAL T£ST QAT4 SUMHARY  ................................................
                      GASEOUS EMISSION TEST NO.>     8          OATE> 10-29-75           TIME!                     6ARO PRESS.I  28.900 IN. HGA.
                      AMBIENT AIR TEMP.!  59.00 OEG. F         RELATIVE HUMIDITY!  95.00 PERCENT        SPECIFIC HUMIDITYI  .010000 LB. H20/LB.  DRY  AIR
                      AMBIENT AIR QUALITY    HYDROCARBONS (HC>!  0.0   PPMC     CARBON MONOXIDE  (CO)!  0.0    PPHV    OXIDES OF NITROGEN (NOX)I 0.0    PPMV
                      SAMPLE LINE ••• TEMP.I  300.00 DEG. F.      FLOWRArE!   14.16 tlTE^S/MIN.     TRANSPORT  TIMEt    6.50 SEC.     LENGTH!    50.00 FT.

TEST CONDITION
ACTUAL POHER SETTING, HORSEPOWER
CORR. POHER SETTING (STO DAY), PERCENT RATED
Nl SPEED, RPM
FUEL FLOW (MEAS.) LB./HR.
CCRR. ENGINE CORE AIRFLOH (MEAS), L8/SEC
COMPRESSOR INLET AIR TOTAL TEMP., OEG F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS.. PSIA
COMPRESSOR DISCHARGE AIR TOTAL TEMP., DEG F
TURBINE INTERSTAGE GAS TOTAL TEMP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION, NET ANALYSIS
HYDROCARBON (HC AS CH4), PPMC
CARBON MONOXIDE (CO), PPMV
TOTAL OXIDES OF NITROSEN (NOX), PPMV
CARBON DIOXIDE (C02) , PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4I
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02I
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS, CALC)
155
34.0
4.97
275LO'.00
107.0
3.0
61.00
14.19
48.13
320.00
879.0
14.16

04.500
208.652
20.000
2.009
13.100

3.634
20.965
3.238

.389
2.200
.346
99.20
.0097
156
50.8
7.44
27520.00
119.0
2.9
60.00
14.19
49.02
312.00
934.0
14.16

48.000
197.027
23.500
2.213
17.200

2.461
17.673
3.462

.293
2.103
.412
99.37
.0107
157
67.2
9.83
27550.00
127.0
2.9
61.00
14.19
54.27
314.00
997.0
14.16

39.000
166.41.6
26.200
2.437
iZ. ICO

1.820
15.218
3.761

• 231
1.933
.480
99.48
.0117
158
204.2
30.00
41770.00
263.0
7.9
57.00
14.19
135.07
632.00
1094.0
14.08

6.600
56.014
54.000
2.028
41.500

.37?
5.527
8.753

.098
1.454
2.302
99.84
.0097
159
476.0
69.66
1,1740.00
352.0
7.8
61.00
14.19
11.1.65
643.00
1315.0
14.09

1.200
26.325
80.000
2.752
73.750

.050
1.918
9.576

.018
.675
3.371
99.95
.0131
160
616.0
98.50
41730.00
407.0
7.9
57.00
14.19
146.46
643.00
1421.0
14.13

2.400
21.057
95.000
3.159
88.500

.087
1.337
9.907

.035
.5%%
H.032
99.96
.0150
161
680.1
99.53
41730.00
431.0
7.8
61.00
1H.19 ...
147.50
652.00
1482.0
14.14

1.600
18.233
105. ooa
3.376 	
100.000

.061 _
1.083
10.249

.026
.467
4.417
99.97
.0161
-------
(D
to
to
o
                     ........................................  £M CYCLE EMISSIONS COMPUTATION SUMMARY  ••»•••••••
                     EN6 MFC  I  AIRESEARCH           TEST FACIL : PHX _ACC2  INSTR DESMIP  I  FED REG V38 N136
                     MODEL NC.t      TPE331-5-251M     S/NI   P04001              ENGINE TYPE(CLASS)I  TURBOPROP
                     RATED PCHERI     706.0 SHP AT SEA LEVEL STANDARD DAY CONDITIONS
                     FUE^I ASTM  01655-73            ATOMIC H/C RATIO:   1.928     LHVI 18470. BTU/LB     ADDITIVES'
                          CALC DATE 110-29-75
                          CALC IDt   2
                         TEST NOI     8
                                                                                                                       NONE
MODE
TIN£ IN NODE. MINUTES
RATED POWER, PERCENT
CORRECTED POMER, HORSEPOWER
HP-MR
FUEL FLON, LB/HR
FUEL HASS, LB
•• HYDROCARBON EMISSION IHCI •*
INDEX, LB HC/1000 LB FUEL
RATE, LB HC/HR
HASS, L6 HC
HASS, PERCENT OF TOTAL CVCLE
CYCLE, LB HC/1000 HORSEPOHER-HR PER CYCLE
•• CARBON MONOXIDE EMISSIONS «COI ••
INDEX, LB CO/1000 LB FUEL
RATE, LB CO/HR
HASS, LB CO
HASS, PERCENT OF TOTAL CYCLE
CYCLE. LB CO/1000 HORSEPCHER-HR PER CYCLE
•• TOTAL OXIDES OF NITROGEN EMISSIONS (NOX) **
INDEX. LB NOX/1000 LB FUEL
RATE. L6 NOX/HR
HASS. L8 NOX
MASS, PERCENT OF TOTAL CYCLE
CYC.E, LB NOX/1000 HORSEPOHER-HR PER CYCLE
TAXI-IDcE
(IN)
7.000
$.000
35.300
4.116
107. 158
12.502

3.617
.388
.01,5
25.5


20.SJ1
a. 200
.257
23.6


3.240
.31,7
.Obi
r.T

TAXI-IDLE
(OUTI
19.000
5.000
J5.300
11.176
107. ISA
33.333

3.617
.388
.123
69.3


20.531
2.200
.697
6<>.l


3.240
.3<>7
.111
20.9

APPROACH
-------
 OJ
i£!
 n>

 to
 to
ENGINE- TPE331-5-2S1M S/N* P0*001 COMB P/N- 869082-1.
RAT SHP= 706. RA EGT.F*
J FUEL H/C* 1.9280 ST01 F/A-
OATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SFEEO. Nl , RPH
COMPRESSOR INLET TEMP., DEC. F
COMPRESSOR OSCHG. PRES. ,PSIA
COMPRESSOR DSCHG. TEMP.OEG F
TUR3 INTERSTAGE TEMP., OEC.F
j CORR 3ELHTH FLOM, LB/SEC
1 FA RATIO BASED ON BELLMTH.
MEASURED FUEL FLOH, ,-B/HR
FA RATIO CALC. FROM EMISSION
} EQUIVALENCE RATIO
LOADING H/P»»N/V/£IT/5*OI
COM3 EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
) L3. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
) PPH BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PP* BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
> HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC CXIDE (NOI - HEIGHTS AS
' PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
) NITROSEN DIOXIDE (N02I
PPK BY VOLUME, MET
i.3. PER 1000 LB. OF FUEL
) HEIGHT FLOH, LB./HR.
1650.
.06822
155
5.0
35.1
31.. 0
275*0.0
61.0
1.8.1
320.0
879.0
2.95
.0101.
107.0
.0097
.11.2
.321.
99.198

2.01
3.11
333.0

208.7
20.565
2.200
RAT SPO-
L H V=
156
7.1,
52.5
50.8
27520.0
60.0
1.9.0
312.0
93U. 0
2.9*
.0116
119.0
.0107
.156
.318
99.368

2.21
3.12
371.2

197.0
17.673
2.103
1.1730.
18*70.
157
9.8
69.*
67.2
27550.0
61.0
5*. 3
314.0
997.0
2.92
.0125
127.0
.0117
.172
.263
99.*B2
'SUMMARY OF
2.**
3.13
396.9

186.*
15.218
1.933
DEH PT,F=
S LN T,F=
158
30.0
211.8
20*. 2
*1770.0
57.0
135.1
632.0
109*. 0
7.92
.0095
263.0
.0097
.1*2
.080
94.837
57.
300.0
159
69.7
*91.8
1,70.0
1.171.0.0
61.0
1*1.7
6*3.0
1315.0
7.8*
.0129
352.0
.0131
.192
.072
99.950
FUEL
REL HUM=
FLO,L/M=
161
90.5
638.9
616.1
*1738. 0
57.0
1*6.5
6*3.0
1*21 . 0
7.86
.01*9
*07.0
.0150
.220
.068
99.961
« AV. KERO. TEST NO.* 8
95.00 SPEC HUM. .010000
14.160 SL TIM, S* 6.5000
161
99.5
702.7
680.1
1.1730.1
61.1 _ .
1*7.5
652.1
1*82.0
7.82
.0159
*31.0
.0160
.235
.065 _ . 	
99.969

2.03
•3.1*
827.0

56.0
5.527
l.*5*
2.75
3.15
1109.1

26.3
1.918
.675
3.16
3.15
1282.8

21.1
1.337
.5**
3.38
3.15
1358.6 _..

18.2
1.083 __. 	 	 _ _..
.*67
CARBON. HEIGHTS AS CHI.
61.. 5
3.631.
.389
.1767
N02
13.1
2.121
.227

6.9
1.117
.120
1.8.0
2.1.61
.293
.1392

17.2
2.531.
.302

6.3
.928
.110
39.0
1.820
.231
.1196

22.1
2.963
.376

6.1
.818
.10*
6.6
.372
.098
.0673

*1.5
6.727
1.769

12.5
2.026
.533
1.2
.050
.018
.0261

73.8
8.828
3.107

6.3
.7*8
.263
2.* .
.087
.035
.0651

88.5
9.229
3.756

6.5
.678
.276
1.9-
.061
.026
.056* . ._. _ .. 	 	

100.0
9.761 . _ . _
*.207

5.9 .. . __ . 	 	 	
.*88
.210
TOTAL OXIDES OF NITROGEN (NC*N02) AS N02 ......_._.._.......
PPM BY VOLUME, MET
) L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
; CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
) SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
) CORRECTED HEIGHT FLOH
SMOKE NUMBER
SMOKE NUMBER AT MA*0.023
20.0
3.238
.31,6

.00711.
1.20
.02H.2
3.50
.03570
. 8.20
.0«998
8.20
5.30
23.5
3.1.62
1.12

.00711
2.1.0
.02131.
3.50
.03557
*.7fl
.0*980
5.90
*.10
28.2
3.781
.480

.00710
1.20
.02130
3.50
.03551
5.90
.0*971
*.70
3.80
5*.0
8.753
2.302

.00708
1.20
.02123
11.80
.03532
17.60
.0*9*5
18.80
12.50
80.0
9.576
3.371

.00705
5.90
.02115
1*.10
.03526
23.50
.0*936
27.10
17.90
95.0
9.907
*.032

.00709
7.10
.02127
12.90
.035*5
20.00
.0*963
22. *0
15.70
105.8
10.2*9
*.*17

.00711
3.50 .. _ _ .. .
. 02131
9.*0
.03552
17.60
.0*972
22. *0
13.30
                   NOTES 1. ALL EMISSIONS  CONCENTRATIONS ARE HET VALUES.
                         2.EQUIVALENCE  RATIO CALCULATED FROM CO2,CO,ANO HC  DATA  AND FUEL COMPOSITION.

                         3.MASS EMISSIONS  OF NO,  N02, AND NO*N02 CALCULATED  AS N02 FROM CONCENTRATIONS HUH MOLECULAR HEIGHT OF  N02  1*6.011.
-------
                      _Mr  M_,   ..„ ..   „   •••••••»••»»•••••••»•»•  AIREiEARCH EMISSION TEST SUMMARY  •••••••••

                      »nnr  Sn ,   £ l~«  *        IEST F*CIL '  PHX  L*C"  INSIR °£SCRIP I FED  RES V38 N136
                      HOOEi. NO.I     TPE331-5-251M     S/NI   POltOOl             -NuINE TYPE(CLASS)!  TURaapBOP
                      RATED PONERI    706.0 SHP AT SE»  LEVEL STANDARD  DAY CONDITIONS     TrPE. 33
632.00
1095.0
11*. 08

8.100
61.036
53.000
2.000
1.1.000
.163
6.105
8.707
.119
1.569
2.238
99.82
.0096
166
1.71.. 9
69.61.
•.1760.00
350.0
7Q
. if
59.00
11.. 19
11.1.91.
61,3.00
1310.0

3.300
27.953
80.000
2.725
7*. 501
.139
2.057
9.670
.0^9
.720
3.38V
99. 9*
.0130
167
610.9
89.50
1.1730.00
1.05.0
7m
»O
61.00
Ht. 19
1<,5.63
6*8.00
K.Z7.0
1%. 13
1.500
19.81.6
95.500
3.089
90.000
. .056
1.289
10.187
• 023
.522
».126
99.96
.014)7
168
679.8
99.79
1.1730.00
1.26.0
7*1
58.60
Ik. 19
14.8.58
61.8.00
1<|72.Q
1 *»•!**
2.100
19. 81.6
102.500
. 3.315
97.500
.073 . ...
1.201
10.180
A*.
. U01
Ki y
. yjLC
99.97 ~
.1157
                                                                                                                                                     --TO
-------
 fa
iQ
 (D
NJ
U)
                      *»*•*••*•»«***•••»*»»***••*•*»»*»*»».•>.»  EPA CYCLE EMISSIONS COMPUTATION SUMMARY  •»»••»•••«
                      ENG MFC I AIRESEARCH            TEST FACIL I PHX LACC2  INSTR OESCRIP I FED KEG V38 N136
                      MODEL NO.l     TPE331-S-Z51M      S/N<   P01.001              ENGINE TYPEICLASSX   TURBOPROP
                      RATED FOHERI     706.0 SHP  AT  SEA LEVEL STANDARD DAY CONDITIONS
                      FUEL I ASTM 01655-73             ATOMIC H/C RATIOI   1,928     LHVI 18V70.  BTU/LB      ADDITIVES!
                                                                                           CALC DATE •16-29-75
                                                                                           CALC 101    ]
                                                                                          TEST NOI    •

                                                                                                                        NONE
'MODE
TIME IN MODE, MINUTES
RATED POHER, PERCENT
CORRECTED POKER, HORSEPOHES
HP-HR
FUEL FLCW, LB/HR
FUEL MASS, LB
•» HYDROCARBON EMISSION (MCI «»
INDEX, LB HC/1000 LB FUEL
RATE, LB HC/HR
MASS, LB HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE, L6 HC/1000 HORSEPOMER-HR PER CYCLE
»• CARBON MONOXIDE EMISSIONS (CO) ••
INOEX, LB CO/1000 LB FUEL
RATE, LB CO/HR
MASS. LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORSEPOMER-HR PER CYCLE
»» TOTAL OXIDES OF NITROGEN EMISSIONS (NOX) »»
INDEX, LB NOX/1000 LB FUEL
RATE, LB NOX/HR
MASS, LB NOX
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB NOX/1000 HORSEPOHEP-HR PER CYCLE
TAXI-IO-t
(INI
7.000
5.000
35.300
4.118
105.156
12.268

3.386
.356
.042
24.9


20.492
2.155
.251
23.3


3.260
.31.3
.0^0
7.6

TAX I -IDLE
(OUT)
19.000
5.000
35.300
11.178
105.156
33.299

3.386
.356
.113
67.6


20.492
2.155
.682
63.2


3.260
.343
.109
20.5

APPROACH
"..500
30.000
211.800
15.885
260.076
19.506

.524
.136
.010
6.1


6.114
1.590
.119
11.0


0.755
2.277
.171
32.3

CLINBOUT
2.500
90.000
635.400
26.475
409.075
17.01.5

.132
.054
.002
1.3


1.385
.567
.024
2.2


10.202
4. 174
.174
32.9

TAKEOFF
.500
100.000
706.000
5.083
423.622
3.538

.002
.001
.0*0
.0


1.102
.467
.004
.1.


11.177
4.311
.036
6.8

TOTAL PER
CYCLE
33.500


63.540

85.61.8

1.947
.299
.167
100.0
2.625

12.616
1.935
1.081
100.0
17.005

6.170
. .940
.529
100.0
8.327
                                            •• EMISSION  INOEX LEVELS REOUIREO TO H££T EPA 1979 STANDARDS FOR CLASS  P2  ENGINES •»
                                         EPA LTO-CYCLE
                                                                                                  REQUIRED EMISSION  INOEX.  LBP/1000 LB FUEL
POLLUTANT
   CO
   HC
   NOX
                                              LBP/1000  HORSEPOMER-HR-CYCLE.
                                                    26.8
                                                      <>.9
                                                    12.9
POLLUTANT I MODE)
   CO HOLE)
   HC (ID.EI
   NOX (TAKEOFF)
   *
20.5
 3.4
10.Z
   a
34.1
 6.6
24. 3
                                            A  ASSUMES  PROPORTIONAL REDUCTION OF POLLUTANT EMISSION INDEX AT EACH  LTD CYCLE  MODE

                                            B  ASSUMES  (II  REQUIRED REDUCTION I* CO AND HC OBTAINED 3Y  LOMERINS  EMISSION INOEX VALUES
                                               AT TAXI-IDLE MODE ONLY, CO AND HC EMISSIONS AT OTHt.* H03£S REMAIN UNCHANGED.  (21 REQUIRED
                                               REDUCTION IN NOX OBTAINED 3Y LOMERIIb EMISSION INDEX VALUES  AT  CLIMBOUT AND TAKEOFF MODES IN
                                               SAME P-iOPORTION AS NEASU3E3 VALUES, NOX EMISSIONS  AT TAXI-I3cE  AND  APPROACH NODES
                                               REMAIN UNCHANGED
-------
P>
N)
ENGINES TPE331-5-251M S/N= P04001 COHB P/N= 86908Z-4 FUEL= AV KERO TEST NO > 8
RAT SHP= 706. RA EGT,F= 1650. RAT SPO* 41738. DEW PT,F= 57. REL HUH* 95 00 SPEC HUM. tt 0,1,
FUEL H/C« 1.9280 STOI F/As .06822 L H V= 18470. S LN T!F= 300.0 FLO,!I/M= ll.llt llllH."l '""S!
OATA POINT NUMBER 162 163 164 165 166 167 166
PERCENT MAX. CORRECTED POWER 5.0 7.5 9. Z9.7 69 6 «9 S oa »
CORRECTED SHAFT HP 35.1 52.7 69. 209.8 49ll? Jit 70!'?














;


)


1


i


)


)


)
MEASURED SHAFT HP
SHAFT SFEEO, Nl, RPM
COMPRESSOR INLET TEMP..OEG.F
COMPRESSOR OSCHG. PRES..PSIA
COMPRESSOR OSCHG. TEMP, DEC F
TURB INTERSTAGE TEMP., DEG.F
CORR BELMTH FLOW, LB/SEC
FA RATIO BASED ON BELLMTH.
MEASURED FUEL FLOW, LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING W/P»»N/V/E


PPM BY VOLUME, WET
LB. PER 1000 LB. OF FUEL
WEIGHT FLOW, LB./HR.
S10KE MEASUREMENT OATA
CORRECTED WEIGHT FLCW
SMOKE NUMBER
CORRECTED WEIGHT FLCW
SMOKE NUMBER
CORRECTED H£I6MT FLCW
SMOKE NUMBER
CORRECTED WEIGHT FLCW
SMOKE NUMBER
SMOKE NUMBER AT WA-0.023
20.4
3.256
.342

.00712
1.20
.02135
3.50
.03552
5.90
.04963
7.10
4.40
23.0
3.366
.393

.00710
2.40
.02131
2.40
.03552
5.90
.04972
4.70
3.68
26. 1
3.566
.441

.00710
1.20
.02131
1.20
.03552
5.90
.04961
5.90
3.60
53.0
6.707
Z.236

.00710
4.70
.02131
2.40
.03552
15.30
.04972
20.00
12.40
474.9
41760.0
59.0
141.9
643.0
1310.0
7.85
.0128
350.0
.0130
.190
.072
99.939
EMISSION
2.72
3.15
1102.7

26.0
2.057
.720

3.3
.139
.049
.0675

74.5
9.005
3.152

5.5
.665
.233

60.0
9.670
3.384

.00712
3.50
.02135
17.60
.03556
21.20
.04901
27.10
17.50
610.
41730.
60.
145.
648.
1427.0
7.84
.0149
405.0
.0147
.215
.066
99.965

3.09
3.15
1276.5

19.8
1.289
.522

1.5
.056
.023
.0432

90.0
9.600
3.868

5.5
.567
.238

95.5
10.107
4. 126

.00712
5.90
.02135
11.00
.03558
16.60
.04901
27.10
16.00
679.6
41730.0
58.0
146.6
646.0
1472.0
7.04
.0156
426.0
.0157
.231
.065
99.965

3. u
3.15
1342.7
-*u^*-* '- - . - -- -- . _ 	
19.8
1.201
.512

2.1

.031
.0605

97.5
9.691
4.129

5.0
- •" 	 --.....
.497 " " "
.212

10Z.5 -- - -
10.100
4.340
-I.WT* 	 	 	
.00712
3.50 '
.02135
11.60
.03550
16.50 " 	 ~~ "" 	 "••" -
.04990
22.41
13.61
                                                                                                                                                              h
                   NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE NET VALUES.
                         2.EQUIVALENCE RATIO CALCULATED FROM C02,CO,AND HC DATA AND FUEL COMPOSITION.
                         3.MASS EMISSIONS OF NO,  N02,  AND NO+N02 CALCULATED AS N02 FROM CONCEMTMTIOHS  MTH MOLcCULA* HEICHT OF  N02  1*6 111

                                                                                                                                                              rz
-------
                    »•**«*••••••»••»••••••••*•**»**••••»•»•*»••»»  AIRESEARCh EMISSION  TEST SUMMARY  ••»••••••••••«
                    ENG MFC I AIRESEARCH            TEST FACIi- I PHX LACC2  INSTR OESCRIP  I  FED REG V3« N136
                    MODEL NO.I    TPE331-5-251M       S/Nl  P04001               ENGINE  TYPEICLASS1I  TURBOPROP
                    RATED POWER I    706.0  SHP  AT  SEA LEVEL STANDARD DAY CONDITIONS
                    FUELI ASTM 01655-73             ATOMIC H/C RATIO!   1.928     LHVI 18470. BTU/LB     AODITIVESI
 CALC DATE 110-29-75
 CALC IDI  1
TEST NOI   9
h
                                                                                                                      NONE
                    •»»••••» EXHAUST EMISSIONS  PL* EPA CYCLE OF WORK OUTPUT ••  CODE  OF  FEDERAL REGULATIONS TITLE 40 PART 87   17 JULY  1973  »»•*•»•
                                        HYDROCARBONS (CH AS CH-.)          2. OSS LB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                        CARBON  MONOXIDE (CO)             15.219 LB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                        OXIDES  OF  NITROGEN (NOX AS N02I   8.934 LB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                        SMOKE                              14.6  SMOKE NUMBER, MAXIMUM AT  CRUISE    MODE,  70 PERCENT RATED POKER
                    TAXI-IOLE SETTINGl  5.0       PERCENT RATED TAKEOFF POHcR AT  65.       PERCENT RATED TAKEOFF Nl RPM
 P)
iQ
 fl>
 ro
 M
 ui
                    ,„................,............,»....,..,..,....,*..  ENGINE DESCRIPTION  »•»•»••••»••»••••*••»»»•••••»••••••»••••••••••»•••»•
                    COMB TYPEI REVERSE FLOW ANNULAR           P/NI   S69082-4            SUS/VOLI  1.260  FUEL INJ TYPE1  STAGED  SIMPLEX
                    ENGINE TOTAL SERVICEI  0.0        HR    TIME SINCE ENGINE OVtRHAULI   0.0       MR
                    ENGINE ASSEMBLY AND MAINTENANCE INFORMATION*
                    AIRCRAFT INSTALLATION •••• MFR.I                                  MODEL  NO.«
                                               USER!                        ENGINE  INSTALLATION POSITIONS
                    »»»..»»»»»»»»»•»»»*»»»»»»».»*»»»»»»»»»•»»»»»»..»0PER»TIONAL TEST DATA  SUMMARY »••••»»••••••»»•••••••»••••••••••»»»»»••»•»•••••
                    GASEOUS EMISSION TEST NO.t    9           DATE! 10-29-75           TIME!                     BARO PRESS.I  28.820  IN.  H6A.
                    AMBIENT AIR TEMP.I  91.00 OEG.  F         R£LATIVE HUMIDITY!  32.00 PERCENT        SPECIFIC HUHIDITYI  .010000 LB.  H20/LB.  DRY AIR
                    AMBIENT AIR QUALITY    HYDROCARBONS (HC)I 0.0   PPMC     CARSON MONOXIDE (COM  0.0   PPMV    OXIDES OF NITROGEN (NOX)I  0.0   PPMV
                    SAMPLE LINE ••• TdMP.l  300.00  DEG. F.      FLOWRATE>   14.16 LITERS/MIN.      TRANSPORT TIMEI    6.50 SEC.     LENGTH!    50.00 FT.
TEST CONDITION
ACTUAL POWER SETTING, HORSEPOWER
CORR. POWER SETTING (STD DAY), PERCENT RATED
Nl SPEED, RPM
FUEL FLCH 
-------
CD
                      ,„,•""•**"  EPA CTC^E EMISSIONS  COMPUTATION  SUMMARY  •••••••••«
                      ENG  MFC t  AIRESEARCM           TEST FACIL  « PHX LACC2   INSTR  OESCRIP »  FED REG  V3» N136
                      MODEL  NO. I    TPE331-5-2S1M      S/NI  POi.001               ENGINE  TYPE (CLASS) I   TURBOPROP
                      RATED  PCNERI    706.0 SHP AT SEA LEVEL STANDARD DAY CONDITIONS
                      FUELI  ASTM 01655-73            ATOMIC H/C RATIO!   1.9ZS      LHV1 1*1,70.  BTU/L8      AODITIVESt
                                                                                                                       NONE
                                                                                                           CALC DATE  110-29-75
                                                                                                           CALC IDI   1
                                                                                                          TEST NOI    9
)
•)
•v
)
)
)

)

)
)
MODE
TIME IN HOOE, MINUTES
RATED POKER, PERCENT
CORRECTED POMER, HORSEPOWER
FUEi. FLCN, LB/HR
FUEL MASS, LB
•• HYDROCARBON EMISSION (HC) ••
INDEX, L8 HC/1000 LB FUEL
RATE, LB HC/HR
HASS. LB HC
HASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORSEPOHER-HR PER CYCLE
•• CARBON MONOXIDE EMISSIONS (CO) ••
INDEX, LB CO/1000 LB FUEL
RATE, LB CO/HR
MASS, LB CO
MASS, PERCENT OF TOTAt CYCLE
CYCLE, LB CO/1000 HORSEPOHER-HR PER CYCLE
•• TOTAL OXIDES OF NITROGEN EMISSIONS (NOXI *•
INDEX, LB NOX/1088 LB FUEL
RATE, LB NOX/Hft
MASS, LB NOX
HASS, PERCENT OF TOTAL CYCLE
CYCLE, L8 NOX/1000 HORSEPOHER-HR PER CYCLE
TAXI-IDLE
7.000
5.000
35.300
4.111
107.534
12.546

2.663
.286
.033
25.6

18.01.4
1.940
.226
23.4

3.434
.369
.043
7.6
TAXI-IDLE
(OUT)
19.000
5.000
39.300
11.174
107.534
34.052

2.663
.266
.091
69.4

1.940
.614
63.5

3.434
.369
.117
20.7
APPROACH
4.500
30.000
211.600
is. ess
254.273
19.070

.315
.080
.006
4.6

1.351
.101
10.5

9.459
2.405
.188
31.9
CLIM80UT
2.500
90.000
635.408
26.475
412.248
17.177

.027
.811
.008
.1

1.251
.516
.021
2.2
	 	
10.767
4.439
.185
32.7
TAKEOFF TOTAL PER
CYCLE
.500
100.008
706.008
5.883
437.227
3.644

.009
.804
.088
.8

.919
.482
.003
.3
_.
11.095
4.8S1
.040
7.1
33.508
03.540
86.489

1.518
.234
.131
100.8
2.855

11.181
1.732
.967
100.8
15.219 ...
- - . -
6.541
1.013
.566
100.0
)
)
)
)
                                              EMISSION  INDEX  LEVELS REQUIRED TO MiET EPA 1979 STANDARDS FOR CLASS P2 ENGINES »•
                                        EPA LTO-CYCLE
                                 POLLUTANT   LBP/1000 HORSEPOMER-HR-CYCLE
                                    CO             26.8
                                    HC              4.9
                                    NOX            12.9
                                                                                                 REQUIRED EMISSION INDEX, LBP/1000 Lg FUEL
POLLUTANT (MODE)
   CO (IDLE)
   HC (IDLE)
   NOX (TAKEOFF)
   A
18.0
 2.7
11.1
33.8
 6.5
23.6
                                              ASSUMES PROPORTIONAL REDUCTION OF POLLUTANT EMISSION  INDEX  AT  EACH LTD CYCLE NODE     .

                                              ASSUMES (1) REQUIRED REDUCTION IN CO AND HC OBTAINED  BY  LOWERING  EMISSION INDEX VALUES
                                              AT  TAXI-IDLE MODE ONLY, CO AND HC EMISSIONS AT OTHER  MOOES  REMAIN UNCHANGED, (21  REQUIRED
                                              5fSi*I»«" IN NOX OBTAINED 9Y kO«£RING EMISSION INDEX  VALUES AT CLIHBOUT AND  TAKEOFF IWDES IN
                                              SAME PROPORTION AS MEASURED VALUES,  NOX EMISSIONS AT  TAXI-IDLE AND  APPROACH  MOOES
                                                                                                                                                  )

                                                                                                                                                '  -53
-------
ENGINE- TPE331-5-Z51N S/N= P04101
RAT SHP= 706. RA EGT,F=
FUEL H/C* 1.9280 STOI F/»=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POWER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Nl , RPH
COMPRESSOR INLET TEMP..DEG.F
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR DSCHG. TEHP.CEG F
TUR3 INTERSTAGE TEMP., CEG.F
CORR 3ELMTH FLOH, LB/SEC
FA RATIO BASED ON BELLKTH.
MEASURED FUEL FLOH, LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING W/P»»N/V/E
-------
                                                                  ..  AIRESEARCH EMISSION  TEST SUMMARY  •»•••••••

                                                                .,.H"* L*C"  INSTR  0£SC*IP «  FED REG V38 N136
                                                        S/NI    POItOOl              PNG1NF  TYPFfriACCl.  TimnnBnnn
                      RATED POWER 1    706.0 SHP AT SEA  LEVEL  STANDARD DAY CONDITIONS      TTP£«CLASSM  TURBOPROP

                      FUEL! ASTH D165S-73            ATOMIC H/C RATIO.   1.928
ENG HFG t

MODEL NO.
AIRESEARCH

     TPE331-5-
                                                                                     LHVI  181.70.  BTU/LB
                               "HAUST
««-IOL£ SETTtNC,  S..
PERCENT R.TED  TAKEOFF POHER^T
                                                                                                            ADDITIVES I  HONE
                                                                           CALC DATE .10-29-75
                                                                           CALC 101   2
                                                                          TEST NOI   9
                                                                                                          TA^""'*!
                                                                                                                               "
 PJ
l£)
 (D

 to
 ro
 oo
                      COMB  TYPE! REVERSE FLOW ANNULAR            P,N.    869082-"

                      ENGINE  TOTAL SER«C£I  0.0       HR     TINE  SINSE EM6INE OVERMAULI
                      ENGINE  ASSEMBLY AND MAINTENANCE INFORMATIONI              «»«n.UL

                      AIRCRAFT INSTALLATION •••• MFR. «                                  NOOEL  NO. 1
                                                          FUEL  INJ TYPE!  STAGED SIMPLEX
CASEOUS EMISSION TEST NO.. 9 DATE! 1
AMBIENT AM TcMP. 1 91. BO DEC. F RELATIV
AMBIENT AIR QUALITY HYDROCARBONS (HC) .00
SAMPLE LINE ••» TEMP.I 310.00 DEC. F. FLOW
TEST CONDITION
ACTUAL POWER SETTING, HORSEPOWER
CORR. POWER SETTING (STO DAY), PERCENT RATED
Nl SPEED. RPM
FUEL FLOW (MEAS.t LB./HR.
CORR. ENGINE CORE AIRFLOW (NEAS), LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., DEG F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTA,. PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL TEMP., OEG F
TURBINE INTERSTAGE GAS TOTAL TEMP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION, WCT ANALYSIS
HYDROCARBON (HC AS CH4), PPMC
CARBON MONOXIDE (CO), PPMV
TOTAL OXIDES OF NITROGEN (NOX) , PPMV
CARSON DIOXIDE (C02), PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4)
CA«aON MONOXIDE (CO)
TCTAL OXIDES OF NITROGEN (NOX AS N02)
EMISSION RATE, LB. POS.LUTANT/HR.
HYDROCARBONS (HC AS CH41
CARBON HOMOKIOE ICO*
TOTAL OXIDES OF NITROGEN (NOX AS N02I
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS, CALC)
0-29-75
TIME
i SUMMARY *
:.
'.Ci.Hl


!S!oioooo8i

WTE' ^Ar.i^r^: """^1^"^ """i"^""^^?!;.' 0;,.o.%T
176 177 178
36.0 51.8 71.4
5.13 7.40 10.20
27550.00 27550.00 27560.00
108.0 119.0 130.0
2.8 2.8 2.8
93.00 90.00 89.00
14.16 14.16 14.16
46.07 46.81 47.30
345.00 341.00 343.00
954.0 1065.0 1087.0
40.500
187.820
24.500
2.184
19.000
2.105
17.081
3.660
.227
.395
99.41
.0105
33.600
184.159
27.100
2.381
21.700
1.604
15.384
3.705
.191
1.831
.441
99.50
.0114
24.900
166.479
32.000
2.671
27.500
1.062
12.422
3.922
1.615
.510
99.61
.0128
179
216.1
29.45
41760.00
256.0
7.6
90.00
14.16
128.68
668.00
1144.0
Ik. ItS
5.700
56.850
61.800
2.051
48.500
.318
5.546
9.903
.081
1.420
2.535
99.84
.0098
180
1.85.8
69.33
41720.00
352.0
7.6
91.00
14.16
135.95
675.00
1382.0
14.05
1.800
25.919
93.000
2.890
87.500
.871
1.799
10.602
.125
.633
3.732
99.95
.1137
181
629.1
89.78
41730.00
405.0
7.5
91.00
14.16
139.49
683.00
1508.0
14.09
1.210
23.890
112.500
3.389
10*. 750
.141
1.414
10.939
.016
.573
4.431
99.96
.0161
182
700.1
99.99
41730.01
436.1
7.5
90.00
14.16 .._.._... .._
141.60
685.01
1569.0
14.11
1.501
15.821
122.501
117.501 "
.048
.880
11.188
.121
.314
4.171
99.9*
.0171
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                    ...,,,...........,.,.,.,.,..,....,.,......  £PA CYC^E EMISSIONS  COMPUTATION SUMMARY  »»••»•••»«
                    ENG  NFC  I  AIRESEARCH           TEST FACIL  I PHX LACC2   INSTR DtSCRIP I  FED REG V38 N136
                    MODEL  N0.«      TPE331-5-251H     S/NI   P0".001               ENGIN£  TYPE(CLASS) I   TURBOPROP
                    RATED  PCHERI     706.0 SHP AT SEA LEVEL STANDARD DAY CONDITIONS
                    FUEL!  ASTM  01655-73            ATOMIC H/C  RATIO:   1.928      LHVI 18*70.  BTU/L8      ADDITIVES"
                                                                                           CALC DATE 110-29-75
                                                                                           CALC 101   2
                                                                                          TEST NO!   9
                                                                                                                      NONE
MODE
TIME IN HOOEi MINUTES
RATEO POHER, PERCENT
CORRECTED POHER, HORSEPOWER
HP-HR
FUEL FLON, LB/HR
FUEL MASSi LB
•• HYDROCARBON EMISSION (HO •»
INDEX, LB HC/1000 LB FUEL
RATE, LB HC/HR
MASS, LB HC
HASS. PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1880 HORSEPOWER-Hf PER CYCLE
•• CARBON MONOXIDE EMISSIONS ICOI **
INDEX, LB CO/1000 LB FUEL
RATE, LB CO/HR
MASS, LS CO
MASS, PERCENT OF TOTAL CYC..E
CYCLE, LB CO/1000 H03SEPOMER-HR PER CYCLE
*• TOTAL OXIDES OF NITROGEN EMISSIONS INOXI •»
INDEX. LB NOX/1000 LB FUEL
RATE, LB NOX/HR
MASS, LB NOX
HASS, PERCENT OF TOTAL CYCLE
CYCLE, LB NOX/1000 HORSEPOMER-HR PER CYCLE
TAXI-IOuE
(IN)
7.000
5.000
35.300
•..its
107.386
13.517

Z.135
.229
.027
25.0


17.1H1.
1.839
.215
22.9


3.658
.392
.01,6
7.7

TAXI-IDLE
(OUT)
19.000
5.000
35.300
11.178
107.286
33.97I>

2.135
.229
.073
67.8


17. II*
1.839
.582
62.2


3.658
.392
.12".
21.0

APPROACH
.l>55
.186
31.3

TAKEOFF
.500
100.000
706.000
5.883
435. 9*9
3.633

.01,7
.021
.000
.2


.873
.380
.003
.3

- •- 	 	
11.187
4.877
.0*1
6.9

TOTAL PER
CYCLE
33.500


63.51.0

86.6.9
                                                   12.9
POLLUTANT I MODE»
   CO (IDLE)
   HC (IDLE)
   NOX (TAKEOFF)
   A
17.1
 2.1
11.2
   a
33.6
 6.5
22.*
                                          A   ASSUMES PROPORTIONAL REDUCTION  OF  POLLUTANT  EMISSION INDEX AT EACH LTD CYCLE NODE

                                          B   ASSUMES ID REQUIRED REDUCTION  IN  CO  4NO HC  OBTAINED BY LOWERING EMISSION INDEX VALUES
                                              AT  TAXI-IDLE MOOt  ONLY,  CO  AND  HC  EMISSIONS  AT OTHER NODES REMAIN UNCHANGED, (2)  REQUIRED
                                              REDUCTION IN NOX OBTAINED 3Y  LOWERING EMISSION INDEX VALUES AT CLIM30UT AND TAKEOFF NODES IN
                                              SAME  PROPORTION AS  MEASURED VALUES, NOX EMISSIONS AT TAXI-IDLE AND APPROACH MOOES
                                              R£KAIN UNCHANGED
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)

ENGINE' TPE331-5-251N S/N> P00001 COMB P/N* 869082-0 FUEL
RAT SHP= 706. RA EGT.F= 1650. RAT SPD* O1730. OEM PT,F= 57. REL HUM=
FUEL M/C« 1.9Z80 STOI F/A= .06022 L H t= 18O70. S LN T,F* 300.0 FLO.L/M*
DATA POINT NUMBER 176 177 178 179 180 181
PERCENT MAX. CORRECTED POMER 5.1 7.o 10.2 29.0 69.3 89.
CORRECTED SHAFT HP 36.2 52.3 72.0 207.9 069.5 633.
MEASURED SHAFT HP 36.0 51.8 71.0 206.1 015.8 629.
SHAFT SPEED, Nl, RPM 27550.0 27550.0 27560.0 01760.0 O1720.0 1.1730.
COMPRESSOR INLET TEMP..OEG.F
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR DSCHG. TEMP.DEG F
TURd INTERSTAGE TEMP., OEG.F
CORR 3ELMTH FLOH, LB/SEC
FA RATIO BASED ON BELLMTH.
MEASURED FUEL FLOH, LB/HR
FA RATIO CALC. FROH EMISSION
EQUIVALENCE RATIO
ITOAOING H/P*»N/V/ECT/5*0»
COMB EFFIC FROM EMISSIONS
CARBON OIOXIOE
PERCENT BY VOLUME, NET
LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, NET
LB. PER 1000 4.B. Of FUEL
HEIGHT FLOH, LB./HR.
UNBURMEO HYDROCARBONS- P»H AS (
PPH BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC CXIOE INO) - HEIGHTS AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLO*. LB./HR.
NITROGEN DIOXIDE IN02I
PPH BY VOLUME, HET
L9. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
vnYAi nvrncc nt u TTancckJ f ki (*•*«!
93.0
46.1
3*5.0
950.0
2.80
.0113
108.0
.0105
.150
.311
99.010

2.18
3.12
337.1

187.8
17.081
1.805
;ARBON, MEI
00.5
2.105
.227
.1233
N02
19.0
2.838
.307

5.5
.822
.889
191 AC MA?
PPM BY VOLUME, MET 2o.5



)


)


)


LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECtfcO WEIGHT FLOM
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECT £0 HEIGHT FLOM
SMOKE NUMBER
SMOKE NUMBER AT MA«0.023
3.668
.395

.00702
1.10
.02186
3.00
.03518
6.90
.0*905
9.20
5.38
90.0
06.8
3*1.0
1005. 0
2.79
.0127
119.0
.0110
.168
.300
99.097

2.38
3.13
371.9

180.2
15.380
1.831
GHTS AS
33.6
1.600
.191
.1003

21.7
2.978
.354

5.3
.T27
.087

27.0
3.705
.001

.03697
1.10
.02090
5.78
.03083
6.90
.C0968
9.20
5.98
89.0
07.3
303.0
1087.0
2.76
.0100
130.0
.0128
.188
.291
99.615

2.67
3.13
007.1

166.5
12.022
1.615
CHO
20.9
1.062
.138
.0855

27.5
3.371
.038

*. 5
.552
.072

32.0
3.922
.510

.0069*
3.00
.02082
5.70
.03*78
3.08
.10858
0.60
0.30
90.0
128.7
668.0
1100.0
7.63
.0100
256.0
.0098
.100
.076
99.802
REDUCED
2.05
3.1o
885.0

56.8
5.506
1.020

5.7
.318
.081
.0573

08.5
7.772
1.990

13.3
2.131
.506

61.8
9.903
2.535

.00692
2.30
.02877
11.50
.03061
16.10
.0*805
18.00
12.00
91.0
136.0
675.0
1362.0
7.56
.0138
352.0
.0137
.201
.068
99.951
EMISSION OATA
2.89
3.15
1119.2

25.9
1.799
.633

1.8
.071
.025
.0397

87,5
9.975
3.511

5.5
.627
.221

93.0
10.602
3.732
*
.00693
2.30
.02080
11.50
.03067
20.70
.0*852
26.00
15.78
91.
139.5
683.0
1508.0
7.50
.0160
005.0
.0161
.236
.060
99.963

3.39
3.15
1276.5

23.9
1.1.10
.573

1.2
.001
.016
.0287

106. 7
10.380
0.20*

5.8
.559
.226

112.5
10.939
0.1,30

.0869*
5.70
.02083
11.58
.83*72
19.58
.8*868
21.88
10.90
= AV. KERO. TEST NO.' 9
32.00 SPEC HUM' .010088
10.160 SL TIM.S- 6.5000
182
100.8
705.9
780.8
01730.0
• 90.8
1*1.6
685.8
1569.8
7.52
.0172
. 036.0 ......
.0171
.251
.062 .'._.....
99.975

3.61
3.15
1370.5 ... .

is. o
.888 .
.38*

1.5 _ ....
.000
.021
.05*2. 	 	

117.5
18.731.. 	 	
A.679

5.8 . ._ _ . .... . . .... '.. .
.057
.199

122.5
11.188
*.078 	 	 	 	 	 	 	 ....._ .

.8869*
6.98 ... 	
.02083
11.50
.03*72 . . . .._. 	
18.08
.0*868
20.18 	 	
15.58
                     NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE HET VALUES.
                           2.EQUIVALENCE RATIO CAiCU.ATEO FROM ;02.CO,ANO HC DATA MO FUEL COMPOSITION.                               ..
                           J.MASS EMISSIONS OF *C, N02, AMD »0«MD2 CAtCU.»T£0 AS M02 FROM CONCENTRATIONS (HIM MOLECULAR HEIGHT OF H02  (06.011.
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                                                                                                                           CALC DATE  110-29-75
                                                                                                                           CALC IDI    3
                                                                                                                           TEST NOI    9
,..,.,»,*.*»,..»...»••.»•***«•.»*»»•••»»*•**•  AIRESEARCH EMISSION TEST SUMKARY  ••»»»•»•»•«»»•
ENG MFG I AIRESEARCH            TtST FACIL I PHX LACCZ  INSTR DESCRIP  I FcO REG V38  M136
HOOEL NO.I     TPE331-5-251M      S/NI   P01.001              ENGINE TYPECCLASSH  TURBOPROP
RATED POHERI    706.0 SHP  AT  SEA  LEVEL STANDARD DAY CONDITIONS
FUEL1 ASTM 01655-73             ATOMIC H/C RATIO:   1.928     LHV: 18*70. BTU/LB      AOOITIVESI  NONE

........ EXHAUST ^MISSIONS PER EPA CYCLE OF HORK OUTPUT •• CODE OF FEDERAL REGULATIONS TITLE «.0 PART 87  17 JULY 1973  ••»•••»
                    HYDROCARBONS  ICH AS CH4)          J.240 LB. POLLUTANT PER  1000  HP.-HR. PER CYCLE ...
                    CftRBOH MONQXIOE ICO»             15.6Z<. -B. POLLUTANT PER  100»  HP.-HR. PER CYCLE
                    OXIDES OF NITROGEN INOX AS NOZ)   9.366 uB. POLLUTANT PER  1000  HP.-HR. PER CYCLE
                    SMOKE                              17.1  SMOKE NUMBER, MAXIMUM AT CRUISE    MODE,  7» PERCENT RATED POKER
TAXI-IDLE SETTING: s.o      PERCENT RATED TAKEOFF PONER AT 65.      PERCENT RATED TAKEOFF NI RPM
                                                                                                          FUEL  INJ  TYPEI   STAGED  SIMPLEX
..............».»..«..*»...••*..*..»..+.•»«•....»»•«  ENGINE DESCRIPTION »»»»»•»»•
CCMB TYPE: REVERSE FLOW  ANNULAR            P/Nt   869082-fc            SUR/VOL: 1.260
ENGINE TOTAL SERVICE!  0.0        HR    TIME SINCE ENGINE OVERHAUL!   0.0        MR
ENGINE ASSEMBLY AND MAINTENANCE  INFORMATION:
AIRCRAFT INSTALLATION »»•»  MFR.1                                  MODEL NO.l
                            USER:                        ENGINE INSTALLATION POSITION!
                                  ............»».0p£R«TIONAL TEST DATA SUMMARY  ••»••»••»•»»•»•«•«»•"«•-"•—-'----——'-•'-
                                         DATE! 10-29-75           TIME!                     BARO PRESS.I  Z8.8*0 IN. HGA.
                                         0^1 amir miMTnlTYi  .77.nn PFRCFNT       SPECIFIC HUMIOITYI  .010000 LB. H20/LB. DRY
                                                                                                                               PPMV
GASEOUS EMISSION TEST NO.: 9 ' DATE! 10-29-75 TIME!
AMBIENT AIR TEMP.: 91.00 DEG. F R£LATIVE HUMIDITY: 32.00 PERCENT
AMBIENT AIR QUALITY HYDROCARBONS IHCM 0.0 PPMC CARBON MONOXIDE ICOl:
SPECIFIC
0.0 PPMV
BARO PRESS. 1 28.840 IN. HGA.
HUMIOITYI .010000 LB. H20/LB. DRY All
CXIOES OF NITROGEN INOX)! 0.0 Pi
SAMPLE LINE *•* TEMF.: 300.00 OEG. F. FLOWRATE 1 14.16 LITERS/HIN. TRANSPORT TIME: 6.50 SEC.
TEST CONDITION
ACTUAL POHER SETTING, HORSEPOWER
CORR. POHER SETTING ISTO DAY), "ERCENT RATED
Nl SPcEO, P.PH
FUEL FLCN IHEAS.) L6./HR.
CORR. ENGINE CORE AIRFLON (MEAS), LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., 3EG F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAi. PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL TEMP., DEG F
TURBINE INTERSTAGE GAS TOTAL TEMP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION, MET ANALYSIS
HYDROCARBON IHC AS CH4) , PPMC
CARBON MONOXIDE ICOl , PPMV
TOTAL OXIDES OF NITROGEN INOXI, PPMV
CARBON DIOXIDE IC02) , PERCENT BY VOL.
NITRIC OXIDE INO), PPMV
EMISSION INDEX, LB. POLLUTANT/1080 LB. FUEL
HYDROCARBONS IHC AS CH4)
CARBON MONOXIDE ICO)
TOTAL OXIDES OF NITROGEN INOX AS NOZ)
EMISSION RAU, LB. POLLUTANT/MR.
HYDROCARBONS (HC AS CM4)
CARBON MONOXIDE ICO)
TOTAL OXIDES OF NITROGEN INOX AS N02I
COMBUSTION EFFICIENCY, PERCENT IEMISSIONS)
F/A IEMISSIONS, CALC)
183 184 185
34.7
4.95
27540.08
108.0
2.9
90.00
14.17
46.51
339.00
938.0
14.12
55.500
198.878
24.500
2.165
18. ZOO
2.907
18.221.
3.688
.314
1.968
.398
99.32
.0104
52.9
7.54
27560.00
122.0
2.8
90.00
14.17
46.91
341.00
1013.0
14.14
36.000
185.531
29.000
2.427
23.000
1.687
• 15.209
3.905
.206
1.855
.476.
99.49
.0117
72.6
10.37
27540.00
135.0
2.7
90.00
14.17
47.30
342.00
1109.0
14.14
29.500
165.129
33.800
Z.752
29.000
1.056
11.962
4.022
.143
1.615
99.63
.8132
186
209.1
29.82
41740.00
259.0
7.6
91.00
14.17
129.03
664.00
1141.8
14.06
6.300
61.036
61.700
2.884
48.808
.346
5.859
9.729
.090
1.518
2.520
99.83
.8100
187
488.7
69.70
41730.08
354.0
7.5
91.00
14.17
135.98
677.08
1386.8
14.86
1.800
28.360
93.500
2.873
86.500
.872
1.988
10.728
.025
.701
3.795
99.95
.0137
188
628.8
89.68
41730.00
410.8
7*5
91.00
14.17
139.3*
683.08
1509.0
14. 10
1.500
19.946
1,13.250
3.389
107.588
.051
1.175
11.813
.021

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                  •)   ...
                            r     ••»••••••••«»••••••••••••••»••  £p» CYC.E EMISSIONS  COMPUTATION SUMMARY  »»•••

                             o't     ?S?«i 5 «,«   TE*LF*CIin' PHX U*C"   INSTR  OESC*IP  '  ^D REG  V38 N136
                            NO. I     TPc331-5-251H     S/NI   P0»001              ENGINE  TVPFICLAS^Il   TnsanDano
                      RATED POMERI    706.0 SHP AT SEA LEVEL STANDARD DAY CONDITIONS      ITPECCLASS>'   TURBOPROP

                      FUELt ASTM 01655-73            ATONIC H/C RATIOI   1.928      LHVI 18470.  BTU/LB
                                                                                                          AOOITIVESI   NONE
 CALC DATE 110-29-75
 CALC 101   I
TEST HOI   9
1 MODE TAXI-IOLE TAXI-IOLE
TIME IN MODE, MINUTES 7 «ao
' RATED PONER. PERCENT 5.000
CORRECTED POHER, HORSEPOWER 35.300
FUEL FLOW. LB/HR 118*325
FUEL HASS, LB 12.638
: •• HYDROCARBON EMISSION «HC> ••

INOEX. LB HC/1001 LB FUEL 2.872
RATE, L8 HC/HR ,311
HASS, L8 HC .,36
HASS, PERCENT OF TOTAi. CYCLE 25.5
CYCLE, LB HC/1000 HORSEPOHER-HR PER CYC..E
•• CARBON MONOXIDE EMISSIONS ICOI ••
INOEX, LB CO/1100 LB FUEL ' 18
> RATE, LB CO/HR i
HASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1BOO HORSEPOMER-MR PER CYCLE
•• TOTAL OXIDES OF NITROGEN EMISSIONS  REDUCTION IN NOX OBTAINED BY LOHERIN6 EMISSION INOEX
SAItt PROPORTION AS MEASURED VALUES, NOX EMISSIONS AT
REMAIN UNCHANGED
CO (IDLE)
HC (IOLEI
NOX (TAKEOFF!
INOEX AT EACH LTD
.- „
18.2
2.9
11.2
CYCLE MODE

.038
.017
.001
.1

.963
.420
.004
.4
- 	 . 	 	
11.196
4.182
.141
6.8
	 	
LB FUEL
.. , 	 	
33.3
6.S
22.1

33.500
63.540
87.273

1.631
.255
.142
100.0
2.240

11.375
1.771
.993
110.0
15.624
. _ .. 	 .
6.819
1.166
.595
100.0

	 —
. 	 	




BY LOMERINC EMISSION INOEX VALUES
MODES REMAIN UNCHANGED, (21 REQUIRED
VALUES AT CLIM30UT AND TAKEOFF MOOES IM
TAXI-IDLE AMD APPROACH MOOES
                                                                                                                                                                '£.
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ENGINE- TPE331-5-251M 3/N* P04001 COMB P/N= 869062-4 ' FUEL
RAT SHP= 706. RA EGT ,F=
FUEL H/C* 1.9280 STOI F/A-
OATA POINT NUMBER
PERCENT MAX. CORRECTED POKER
CORRECTED SHAFT HP
MEASURED SHAFT HP
1 SHAFT SPEED, Nl, RPH
COMPRESSOR INLET TEHP..OEG.F
COMPRESSOR OSCHG. PReS. ,PSIA
COMPRESSOR OSCHG. TEHP.CEG F
TURB INTERSTAGE TEMP., DEG.F
CORR 3ELMTH FLOH, LB/SEC
: FA RATIO BASED ON BELLMTH.
MEASURED FUEL FLON, LB/HR
FA RATIO CALC. FROM EMISSION
i EQUIVALENCE RATIO
LOADING H/P"N/V/E«T/540I
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
) LB. C02 PER LB. OF FUEL
HEIGHT FLOH. LB./HR.
CARBON MONOXIDE
) PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEi.
HEIGHT FLOH, LB./HR.
UNBURNED HYDROCARBONS- PPM AS
FPH BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXI9E (NO) - HEIGHTS AS
FPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, 1.8. /HR.
NITROGEN DIOXIDE IN02I
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
' HEIGHT FLOH, LB./HR.
1650.
.06822
183
4.9
34.9
34.7
27540.0
90.0
46.5
339.0
938.0
2.85
.0112
106.0
.0104
.153
.312
99.316

2.17
3.12
336.7

198.9
18.224
1.968
SAT SPD* 41730.
L H V-
184
7.5
53.3
52.9
27560.0
30.0
46.9
341.0
1013.0
2.82
.0129
122.0
.3117
.171
.302
99.494

2.43
3.13
361.3

135.5
15.209
1.355
CARBON, HEIGHTS AS
55.5
2.907
.314
.1595
N02
18.2
2.739
.296

6.3
.948
.102
36.0
1.667
.206
.1109

23.0
3.097
.378

6.1
.808
.099
= 16470.
185
10.4
73.2
72.6
27540.0
90.0
47.3
342.0
1109.0
2.74
.0146
135.0
.0132
.193
.289
99.626

2.75
3.13
422.9

165.1
11.962
1.615
CH4
25.5
1.056
.143
.0883

29.1
3.451
.466

4.6
.571
.077
OEH PI.F*
S cN T,F=
186
29.8
210.5
209.1
41740.0
91.0
129.0
664.0
1141.0
7.6*
.0101
259.0
.0100
.146
.077
99.832
OF REDUCED
2.06
3.14
814.3

61.0
5.859
1.516

6.3
.346
.090
.0590

46.0
7.569
1.960

13.7
2.160
.560
57.
300.0
167
69.7
492.1
468.7
41730.0
91.0
135.9
677.0
1366.0
7.55
.0139
354.0
.0137
.200
.067
99.947
EMISSION
2.87
3.15
1115.4

26.4
1.980
.701

1.6
.072
.025
.0363

86.5
9.916
3.511

7.8
.803
.264
REL HUH*
FLO.L/M*
188
69.
633.
626.
41731.
91.
139.3
683.0
1509.0
7.52
.0162
410.1
.1161
.236
.064
99.966

3.39
3.15
1292.4

19.8
1.175
.482

1.5
.051
.121
.0432

187.5
10.45*
4.286

5.7
.559
.229
TOTAL OXIDES OF NITROGEN (NC+N02) AS N02 . 	
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
) SMOKE NUMBER
CORRECTED HEIGHT FLCH
SMOKE NUMBER
i CORRECTED HEIGHT FLOH
SMOKE NUMBER
SMOKE NUMBER AT HA*8.023
24.5
3.686
• 396

.11706
4.60
.02125
6.90
.03541
8.00
.04957
9.20
7.20
29.0
3.905
• 476

.00707
2.30
.02121
•..60
.03535
8.00
.04949
9.20
6.10
33.6
4.022
• 543

.00707
3.40
.02121
4.60
.03535
8.00
.04958
8.00
6.10
61.7
9.729
2.520

.10709
5.70
.02126
11.50
.03547
16.10
.04957
20.70
13.60
93.5
11.720
3.795

.00709
8.00
.02126
13.61
.03553
20.70
.0497*
25.30
17.11
113.2
11.013
4.51S

.01711
6.90
.02131
12.68
.03552
17.20
.0*973
21.80
14.70
= AV. KERO. TEST NO.* 9
32.00 SPEC HUM' .010011
14.161 SL TIM.S* 6.5001
169
110.
706. •
701.
41710.
91. . .
141.
666.
1577.
7.49
.0173
436.1 _ . ... .
.0172
.252
.062
99.97*

3.63
3.15
1374.5 . ._. _.. .

17.*
.96* 	
.420

1*2
.038
.017
.839* . 	 	 	

117.5
10.67* 	 	 	
4.65*

_ 5,7. _ ' .. . .._ 	
.522
.221
__ 	 	 	 	 . . . - 	 .. 1 —
123.2
11.196
4.862

.01710
4.60
. 12131
11.58
.03551.
18.41
.0*971
21.61 . _ 	 _
14.20
                    NOTES  1.  ALL EMISSIONS CONCENTRATIONS  ARE HET  VALUES.
                           2.EQUIVALENCE RATIO CALCU.ATEO FROM C02.CO.ANO HC  DATA AND FUEL
                           3.MASS EMISSIONS OF NO, N02,  AND NO»NC2  CALCULATED AS N02 FRQH
 COMPOSITION.
CONCENTRATIONS WITH
                    MOLECULAR HEIGHT OF  N02  146.11).
-------
                           .............................................  «IR£SE»RCH EMISSION  TEST SUMMARY   »••»••»»..••..
                           ENG KF6 I  AIRESEARCH           TEST FACIL I PHX LACCZ  INSTR OESCRIP  I FED REG V38 N136
                           MODEL  NO.I     TPE331-5-251H     S/NI   P04001              ENGINE  TYPEICLASSM   TURBOPROP
                           RATED  POMERI    706.0 ShP AT SEA LEVEL STANDARD DAY CONDITIONS
                           FUELI  ASTM 01655-73            ATOMIC H/C RATIOI   1.928     LHVI 18470. BTU/LB      ADDITIVES!
                                                                                                                            NONE
                                                                                                      CALC DATE 118-29-75
                                                                                                      CALC IDI   1
                                                                                                     TEST N0<  18
                                                                                                                                     17  JULY 1973
........ EXHAUST EMISSIONS PER EPA CYCLE  OF  HORK  OUTPUT •* CODE OF FEDERAL REGULATIONS TITLE 48 PART 87
                    HYDROCARBONS  (CH AS CH4I           2.407 LB. POLLUTANT  PER 1000 HP.-HR. PER CYCLE
                    CAREON MONOXIDE (CO)              16.949 LB. POLLUTANT  PER 1008 HP.-HR. PER CYCLE
                    OXIDES OF NITROGEN  (NOX  AS  N02)    8.195 LB. POLLUTANT  PER 1000 HP.-HR. PER CYCLE
     	            SMOKE   .                          18.2  SMOKE NUMBER,  MAXIMUM AT  CRUISE    MODE,  78 PERCENT RATED POHER
»AXI-IBti. SCT.TU4CA 5.8      PERCENT RATED TAKEOFF PONER AT 65.       PERCENT RATED TAKEOFF Nl RPM
                                                                                                                                STAGED  SIMPLEX
.17
47.74
326.01
994.0
14.14

l>0.508
197.027
25.300
2.1.11
20.000

1.908
16.21.1
3.1.26

.235
1.998
.4Z1
99. 4$
.0116
73.5
10.1.9
271.80.00
135.0
2.8
90.00
14.17
1.8.01.
327.00
1081.. 0
11.. 15

33.808
176.1.20
30.308
2.71.1
25.800

1.371
12.82Z
3.617

.185
1.731
.1,86
99.58
.8131
193
209.1.
Z9.89
1.1750.00
262.0
7.7
90.00
Hi. 17
129.96
6m.OO
1132.0
IV. 05

6.608
61.. 811.
53.800
2.132
1.0.000

.351.
6.883
8.171

.893
1.594
2.11.1
99.83
.0102
194
491.3
70.12
41750.08
364.0
7.6
98.08
14.17
137.67
654.08
1373.8
14.86

2.400
27.953
80.700
2.912
75.508

.894
1.925
9.128

.834
.701
3.323
99.95
.8139
195
631.2
89.93
41700.08
417.8
7.6
92.08
14.17
148.72
668.88
1495.8
14.18

1.280
22.270
97.588
3.487
93.758

.848
1.311
9.438

.817
.547
1.932
99.97
.8162
LENGTHI 50.08
196
700.6
99.92
41720.00
446.8
7.6
91.08
14.17
142.83
674.08
1556.8
14.11

1.588
15.821
188.758
3.609
103.758

-------
fa
iQ
(D

to
U)
U1
                     .,*.„»..,....,,.,»..,,..,..»,,..,.....,..   EPA ctCLE EMISSIONS COMPUTATION SUMMARY  •»•••»»•»«
                     ENG  HFG  I AIRESEARCH            TEST  FACIL  t  PHX LACC2  INSTR DESCRIP I FED REC ¥38 N136
                     MODEL NO.I      TPE331-5-251M      S/NI    P0*001              ENGINE TYPEICLASSM  TURBOPROP
                     RATED PONERI     706.0  SHP  AT  SEA  LEVEL  STANDARD DAY CONDITIONS
                     FUELI ASTM D1655-73             ATONIC  H/C  RATIOI   1.928     LHVI 10*70. BTU/LB     ADDITIVESI
                                                                                          CALC DATE 110-29-75
                                                                                          CALC IDI   1
                                                                                         TEST NOI  10
                                                                                                                      NONE
MODE
TIME IN MODE, MINUTES
RATED POWER, PERCENT
CORRECTED POWER, HORSEPOWER
HP-HR
FUEL FLCW, LB/HR
FUEL MASS, LB
•• HYDROCARBON EMISSION (HC) ••
INDEX, LB HC/1000 LB FUEL
RATE, LB HC/HR
MASS, L8 HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE. LB HC/1000 HORSEPOMER-HR PER CYCLE
•• CARBON MONOXIDE EMISSIONS (CO) **
INDEX, LB CO/1000 LB FUEL
RATE, LB CO/HR
NASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORSEPOWER-HR PER CYCLE
»• TOTAL OXIDES OF NITROGEN EMISSIONS (NOX) **
INDEX. LB NOX/1000 LB FUEL
RATE, LB NOX/HR
MASS, LB NOX
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB NOX/1000 HORSEPOWER-HR PER CYCLE
TAXI-IDLE
(IN)
7.000
5.000
35.300
*.118
110.157
12.852

3.0*5
.335
.039
25.6


19.1.96
2.1*8
.251
23.3


3.311
.365
.0*3
1.2

TAXI-IDLE
(OUT)
19.000
5.000
35.300
11.178
110.157
3*.8«3

3.0*5
.335
.106
69.*


19.1.96
2.1*8
.6(0
63.2


3.311
.365
.115
22.2

APPROACH
*.SOO
30.000
211.800
15.885
263.115
19.73*

.3*2
.090
.007
*.*


6.009
1.602
.120
11.2


0.193
2.156
.162
31.0

CLIHBOUT
2.500
90.000
635. *00
26.*7S
*17.527
17.397

.036
.015
.001
.*


1.321
.552
.023
2.1


9.1.3*
3.939
.16*
31.5

TAKEOFF
.500
100.000
706.000
5.883
**5.*13
3.712

.050
.026
.000
.1


.0**
.376
.003
.3


9.93*
*.*Z5
.037
7.1

TOTAL PER
CYCLE
33.500


63.5*0

88.577

1.727
.27*
.153
100.0
Z.*07

12.158
1.929
1.077
100.0
16.9*9

5.878
.933
.521
100.0
0.195
                                                                                                                                 >
                                                                                                                                 >
                                           •» EMISSION INDEX LEVELS REQUIRED TO MEET EPA  1979  STANDARDS  FDR  CLASS P2 ENGINES »•


                                        EPA LTO-CYCLE                                           REQUIRED EMISSION INDEX,  LBP/1000 LB FUEL
POLLUTANT
   CO
   HC
   NOX
                                             l.BP/1000 HORSEPOMER-HR-CYCLE
                                                   26. B
                                                   12.9
POLLUTANT IMODEI
   CO (IDLEI
   HC (IDLEI
   NOX (TAKEOFF)
   A
19.5
 3.0
 9.9
   B
32.6
 6.*
2*. 7
                                           A  ASSUMES PROPORTIONAL REDUCTION OF POLLUTANT EMISSION  INDEX  AT  EACH LTO CYCLE NODE

                                           B  ASSUMES (1) REQUIRED REDUCTION IN CO AND HC OBTAINED  BY  LOWERING EMISSION  INDEX  VALUES
                                              AT TAXI-IDLE MODE ONLY, CO AND HC EMISSIONS AT OTHER  MOOES  REMAIN UNCHANGED, (21 REQUIRED
                                              REDUCTION  IN NOX OBTAINED BY LONERING  EMISSION INDEX  VALUES AT CLIHBOUT AND TAKEOFF  MOOES  IN
                                              SAME PROPORTION AS MEASURED VALUES, NOX EMISSIONS  AT  TAXI-IDLE AND APPROACH MOOES
                                              REMAIN UNCHANGED
                                                                                                                                 >


                                                                                                                                 )


                                                                                                                                 >
-------
 fa
iQ
 rt>
 N)
0

ENGINE* TPE331-5-251N S/N« PO*B01 COMB P/N= 869082-*
RAT SHP= 706. RA EGT.F* 1650. RAT SPO« *1730. OEH PT,F« 68.
) FUEL H/C- 1.9280 STOI F/A« .06822 L H Y« 18*70. S LN T,F= 300.0
DATA POINT NUMBER
> PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
1 SHAFT SPEED, Nl. RPN
COMPRESSOR INLET TEMP..CEG.F
COMPRESSOR OSCHG. PRES. ,PSIA
1 COMPRESSOR DSCHG. TEMP, DEC F
TURB INTERSTAGE TEMP., OEG.F
CORR BELNTH FLOH, LB/SEC
1 FA RATIO BASED ON BELLMTH.
MEASURED FUEL FLOH, LB/HR
FA RATIC CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING M/P**N/tf/E IT/SOI
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, NET
) LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
) PPM BY VOLUME, HET
La. PER 10BO LB. OF FUEL
HEIGHT FLOH, LB./HR.
1 UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, MET
LB. PER 18BB LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIOE INOI - HEIGHTS AS
> PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
NITROGEN DIOXIDE (N02>
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
190
5.
35.
3*.
27550.
89.
*7.
32*.
92*.
2.91
.0112
110.0
.0105
.153
.317
99.272

2.17
3.11
3*2.6

213.3
19.51*
2.1*9
191
7.*
51.9
51.5
27550.0
90. t
*7.7
326.0
99".. 0
2.86
.0128
123.0
.0116
.170
.306
99.1.51

2.*1
3.12
38*. 2

197.0
16.2*1
1.998
CARBON, HEIGHTS AS
58.5
3.B62
.337
.1567
N02.
18.0
2.707
.298

*.B
.602
.066
*0.5
1.908
.235
.1175

20.0
2.708
.333

5.3
.718
.088
192
10.5
7*.B
73.5
27*88.
90.
*8.
327.
108*.
2.79
.01**
135.0
.0131
.193
.29*
99.578

2.7*
3.13
*22.6

176.*
1Z.822
1.731
CH*
33.0
1.371
.185
.1069

25. B
2.985
.*03

5.3
.633
.085
TOTAL OXIDES OF NITROGEN 
 >
 )
 >
 1
 )

>
*
                  NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE HET VALUES.
                        2.EQUIVALENCE RATIO CALCULATED FRON C02.CO.ANO HC DATA AND FUEL COMPOSITION.
                        3.KISS EMISSIONS OF NO, N02, AND NO*N02 CALCULATED AS N02 FROM CONCENTRATIONS HITH MOLECULAR HEIGHT OF NOZ 1*6.111.
-------
                       ••*»•••*»*••••••».••*•••.•••••••••»»*»»•••»•»   AIRESEARCH EMISSION TEST SUMMARY  ••»»»•••»»•»»•
                       ENG MFC  I AIRESEARCH            TEST  FACIL I  PHX LACCZ  INSTR 0£SCRIP I FED REG V38 N136
                       MODEL NO.t     TPE331-5-251M      S/NI    P04001               ENGINE TYPE(CLASS)I  TURBOPROP
                       RATED FOHERI     706.0 SHP  AT SEA  LEVEL  STANDARD DAY  CONDITIONS
                       FUEi.1 ASTM 01655-73             ATOMIC H/C RATIOS   1.928     LHVI 18470. BTU/LB     ADOITIVESI
     CALC DATE 110-30-75
     CALC 101    2
    TEST NOI   II
NONE
                       •»•*•»«. EXHAUST EHISSICNS PER EPA  CYCLE  OF HORK  OUTPUT '» CODE OF FEDERAL REGULATIONS TITLE 40 PART 87  17 JULY 1973  •••••••
                                           HYDROCARBONS  (CH  AS CH4)           Z.564 L3. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                           CARSON MONOXIDE (CO)              16.625' -B. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                           OXICES OF NITROGEN  (NOX AS  N02)    6.055 LB. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                           SMOKE                              19.1  SMOKE NUMBER. MAXIMUM AT  CRUISE    MODE,  78 PERCENT RATED PONER
                       TAXI-IDLE SETTINGI 5.0      PERCENT RATED TAKEOFF POWER AT 65.       PERCENT RATED TAKEOFF Nl RPM
0)
to
OJ
                       .........,.......,.............,,..,..*.........,...   EN6IN£ DESCRIPTION  »«»»••»»»••»»•»•»•••«••»»»*•»•»»••»•*••»••»•••»»•••
                       COMB TYPE I REVERSE FLOM ANNULAR            P/Nt    869082-4           SUR/VOLI  1.260  FUEL INJ TYPEI  STAGED SIMPLEX
                       ENGINE TOTAL SERVICE*  0.0       HR     TIME  SINCE  ENGINE OVERHAUL!  0.0       HR
                       ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                       AIRCRAFT INSTALLATION •••• MFR.I                                  MODEL NO.I
                                                  USER!                        ENGINE INSTALLATION  POSITION!
                                                                                                             L*«**»»•»»»»•»»•»»»•••»•»»*»»»»»»»»»••»»»•
                                                                                                                  BARO PRESET I  28.760 IN. HGA.
                                                                                                             FIC HUMIOITYI  .015000 LB. H20/LB. DRY AIR
                                                                                                                                                     PPMV
' GASEOUS EMISSION TEST NC. 1 10 DATE! 10-30-75 TIME!
AMBIENT AIR TEMP. 1 91.00 OEG. F RcLATIVE HUMIOITYI 41.00 PERCENT
AMBIENT AIR QUALITY HYDROCARBONS (HC) t 0.0 PPHC CARBON MONOXIDE (CO) 1
SPECIFIC
0.0 PPMV
BARO PRESS; 1 28.760 IN. HGA.
HUMIOITYI .015000 LB. H20/LB. DRY
OXIDES OF NITROGEN (NOX)I 0.0
) SAMPLE LINE ••» TEMP.I 300.00 OEG. F. FLOH3ATEI 14.16 LITERS/HIM. TRANSPORT TIMEl 6.50 SEC.
) TEST CONDITION
ACTUAL POHER SETTING, HORSEPOWER
CORR. PONER SETTING (STC OAYI, PERCENT RATED
Nl SPEED, RPM
FUEL FLCN (MEAS.) LB./HR.
CORR. ENGINE CORE AIRFLCH (MEAS). LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., OEG F
COMPRESSOR INLET AIR TOTAL PRESS.. PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS.. PSIA
COMPRESSOR DISCHARGE AIR TOTAL TEMP., DEG F
: TURBINE INTERSTAGE GAS TOTAL TEMP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
> EMISSION CONCENTRATION, WET ANALYSIS
HYDROCARBON (HC AS CH4), PPMC
CARBON MONOXIDE (CO) , PPMV
) TOTAL OXIDES OF NITROGEN (NOX), PPMV
CARBON DIOXIDE (C02) . PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
, EMISSION INDEX. LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
EMISSION RATE. LB. POLLUTANT/MR.
HYDROCARBONS IMC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
) F/A (EMISSIONS, CALC)
19? 198 199
35.0
5.01
Z7540.00
110.0
2.9
90.00
14.13
47.35
323.00
922.0
14.10

60.300
208.652
20.000
2.156
14.600

3.170
19.191
3.022

.349
2.111
.332
99.27
.0104
52.4
7.48
27510.00
122.0
2.9
93.00
14.13
47.79
327.00
1000.0
14.10

40.500
191.493
24.600
2.411
19.000

1.909
15.789
3.332

.233
1.926
.406
99.46
.0116
70.4
10.09
Z7570.00
135.0
2.8
88.00
14.13
48.13
327.00
1067.0
14.10

35.700
175.513
28.500
2.645
23.000

1.537
13.217
3.525

.207
1.784
.476
99.55
.0127
200
209.9
30.13
41760.00
263.0
7.7
87.00
14.13
130.26
640.00
1130.0
14.01

9.000
62.714
53.200
2.084
41.500

.494
6.019
8. 38 7

.131
1.583
2.206
99.82
.0100
201
484.8
69.33
41740.00
358.0
7.7
91.00
14.13
136.39
655.00
1366.0
14.03

5.180
25.919
78.750
2.862
71.751

.204
1.816
9.064

.073
.650
3.245
99.94
.0136
202
631.3
90.19
41740.00
415.0
7.6
92.00
14.13
140.86
669.00
1501.0
14. B7

1.500
17.831
98.000
3.321
92.750

.052
1.077
9.724

.•21
.447
4.035
99.97
.015*
LENGTHI 50.0
203
699.1
99.89
41750. OS
446.0
7.6
92.00
14.13
142.19
673.00
1558.0
14.08

.900
19.442
107.250
3.602
100.250

.029
1.083
9.812

.013
.483
4.376
99.97
.0171
-------
to
iS
n>

to
(_o
CO
                      ..........................................  £P4 CYCLE EMISSIONS COMPUTATION SUMMARY  »....»....
                      ENG NFC t AIRESEARCH           TEST FACIL I PHX LACC2  INSTR OESCRIP I FED REG V38 N136
                      MODEL NO.I     TPE331-5-251H     S/NI    P0*001              ENGINE TYPE (CLASS)I  TURBOPROP
                      RATED POWER!    706.0 SHP AT SEA LEVEL STANDARD DAY CONDITIONS
                      FUELI ASTM 01655-73            ATOMIC  H/C RATIOI   1.928     LHVI 18*78. BTU/LB     ADDITIVES!
                         CALC DATE 110-30-75
                         CALC 101    2
                        TEST NO I   18
                                                                                                                                                                   n
                                                                                                                                                                   •
                                                                                                                                                                  I
                                                                                                                      NOME
MODE
TIM£ IN MODE* MINUTES
RATED POWER, PERCCKT
CORRECTED PONER, HORSEPOWER
HP-HR
FUEL FLOW, LB/HR
FUEL MASS, LB
*» HYDROCARBON EMISSION CHCI **
INDEX. LB HC/100B LB FUEL
RATE, LB HC/HR
MASS, LB HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE. LB HC/1000 HORSEPOHER-HR PER CYCLE
•• CARSON MONOXIDE EMISSIONS (COI *•
INDEX. L8 CO/1000 LB FUEL
RATE. LB CO/MR
MASS. LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, L8 CO/ 1000 HORSEPOMER-HR PER CYCLE
»• TOTAL OXIDES OF NITROGEN EMISSIONS (NOXt •*
INDEX, LB NOX/1000 LB FUEL
RATE. LB NOX/HR
MASS. LB NOX
MASS, PERCENT OF TOTAL CYCLE
CYCLE. LB NOX/1000 HORSEPOMER-HR PER CYCLE
TAXI-IDLE
(INI
7.000
5.000
35.300
4.118
109.962
12.829

3.176
.3*9
.0*1
ZS.O


19.20*
2.112
.2*6
23.3


3.020
.332
.039
7.6

TAXI-IDLE
(OUTI
19.000
5.000
35.300
11.170
109.962
3*.8Z1

3.176
.3*9
.111
67.9


19.20*
2.112
.669
63.3


3.82D
.332
.105
20.5

APPROACH
*.500
30.000
211.800
15.885
262.113
19.b58

.515
.135
.010
6.Z


6.039
1.503
.119
11. Z


8.351
2.189
.16*
32.1

CLIMBOUT
2.500
90.000
635. *0fl
Z6.*75
*1*.053
17.252

.072
.030
.001
.0


1.076
.**6
.019
1.8


9.780
*.D16
.167
32.7

TAKEOFF
.580
100.000
706.000
5.803
-------
03
ENGINE* TPE331-5-251M S/N= P0*001 COMB P/N* 869082-1.
RAT SHP» 706. RA EGT,F' 1650. RAT SPD> *1730. OEM PT,F« 68.
1 FUEL H/C= 1.9280 STOI F/A- .06022
DATA POINT NUMBER 197
; PERCENT MAX. CORRECTED POMER 5.0
CORRECTED SHAFT HP 35.*
MEASURED SHAFT HP 35.0
•> SHAFT SPEED. Nl, RPM 275*0.0
COMPRESSOR INLET TEMP.. OEG. f 90.0
COMPRESSOR DSCHG. PRES..PSIA 1.7.3
) COMPRESSOR OSCMG. TEMP, DEC F 323.0
TUR3 INTERSTAGE TEMP., DEG.F 922.0
CORR BELMTH FLOH, LB/SEC 2.92
' FA RATIO BASED ON BELLHTH. .0112
MEASURED FUEL FLOM, L8/HR 110.0
FA RATIO CALC. FROM EMISSION .010*
| EQUIVALENCE RATIO .153
I LOADING H/P»»N/V/EIT/S*OI .317
COMB EFFIC FROM EMISSIONS 99.270
CARBON DIOXIDE
PERCENT BY VOLUME. MET 2.16
- LB. C02 PER LB. OF FUEL 3.12
HEIGHT FLOH, LB./HR. 3*2.7
CARBON MONOXIDE
1 PPM BY VOLUME. MET 218. 7
LB. PER 1000 LB. OF FUEL 19.191
HEIGHT FLOH, LB./HR. 2.111
L H V = 18*70. S LN T.F* 300.0
198
7.5
52.8
52.1.
27510.0
93.0
1.7.8
327.0
1000.0
2.87
.0127
122.0
.0116
.170
.30*
99.1.61

2.1.1
3.12
381.1

191.5
15.789
1.926
UNBURNEO HYDROCARBONS- PPM AS CARBON, HEIGHTS AS
PPM BY VOLUME, MET 60.3
LB. PER 1000 LB. OF FUEL 3.170
) HEIGHT FLOH, LB./HR. .3*9
RATIO LB HC/LB CO .1652
NITRIC OXIDE (NO) - HEIGHTS AS N02
PPM BY VOLUME, MET I*. 6
L9. PER 1000 LB. OF FUEL 2.206
HEIGHT FLOM. LB./HR. .2*3
) NITROGEN DIOXIDE (N02I
PPM BY VOLUME. MET 5.*
LB. PER 1000 LB. OF FUEL .816
) HEIGHT FLOM, LB./HR. .090
TOTAL OXIDES OF NITROGEN INO»N02» AS NO2
PPM BY VOLUME, MET 20.0
i > LB. PER 1000 LB. OF FUEL 3.022
HEIGHT FLOM, LB./HR. .332
SMOKE MEASUREMENT DATA
1 CORRECTED HEIGHT FLCM .1071*
SMOKE NUMBER *.70
CORRECTED HEIGHT FLCH .021*2
; SHOKC NUMBER *.7Q
CORRECTED HEIGHT FLCM .03571
SHOKE NUMBER 5.80
) CORRECTED HEIGHT FLCM .0*989
SMOKE NUMBER 9.30
SMOKE NUMBER AT MA*0.023 6.11
1 NOTES 1. ALL EMISSIONS CONCENTRATIONS A«
nwibw — - 	 __..—_ .. * v*« /» •< out • T*rn con
1,0.5
1.909
.233
.1209

19.0
2.573
.31*

5.6
.758
.093

2*. 6
3.332
.1.06
.00711
2.30
.0213*
3.50
.035*9
5.80
.0*969
8.10
5.00
199
10.1
71.3
70.*
27570.0
88.0
1.8.1
327.0
1067.0
2.80
.01*3
135.0
.0127
.186
.29*
99.55*
•SUMMARY OF
2.61.
3.13
*22.*

175.5
13.217
1.78*
CH*
35.7
1.537
.207
.1163

23.0
2.8*5
.38*

5.5
.680
.092

28.5
3.525
.1.76
.00709
*.70
.02126
5.80
.035*3
5.80
.4*960
8.10
6.10
211
30.1
212.7
209.9
1.1760.1
87.0
130.3
6*0.0
1130.0
7.73
.0101
263.1
.0100
.1*6
.080
99.815
REDUCED
2.08
3.1*
826.7

62.7
6.019
1.583

9.0
.1.9*
.130
.0820

1.0.5
6.385
1.679

12.7
2.012
.527

53.2
8.387
2.206
.00707
7.00
.02120
11.60
.03533
18.60
.0*9*7
20.90
1*.70
211
69.3
1.89.5
*8*.
1.171,0.
91.
136.
655.
1366.
7.70
.0138
358.0
.0136
.200
.071
FUEL' AV. KERO. TEST NO.' 11
1EL HUH' 1,8.00 SPEC HUM. .015080
FLO.L/M*
212
90.2
636.8
631.3
* 171,0.0
92.0
1*0.9
669.1
1510.0
7.61
.0162
*15.0
.0150
.231
.065
99.939 99.970

2.66
3.15
1127.9

25.9
1.816
.650

5.1
.20*
.073
.1125

71.7
8.258
2.956

7.0
.806
.288

78.7
9.06*
3.2*5
.0070*
8.10
.02111
16.30
.03519
22.10
.0*926
29.10
19.11
3.32
3.15
1308.2

17.1
1.077
.**7

1.5
.052
.021
.1*11

92.7
9.203
3.819

5.3
.521
.216

90.1
9.72*
*.035
.11712
7.11
.02105
1*.00
.13509
16.30
.0*912
23.31
15.30
1*.16I SL TIM.S' 6.5001
213
99.9
705.2
699.1
*1758.0
92.1
1*2.2
673.1
1550.1
7.63
.117*
**6.0
.0171
.250
.063
99.972

3.60
3.15
1*05.9

19.*
1.003
.1.83

.9
.029
.013
.0265

100.2
9.171
*.09I

7.1
.6*1
.286

117.2
9. 812
*.376
. 01710
8.11
.12111
15.11
.13502
19.00
. 0*913
22.11
16.51
E MET VALUES.
M rn9.rn.ANn MC nATA AND FUFL roMpncTTTmi. . '
                                                                                                                    MOLECULAR HEIGHT OF N02  (*6.11I.
                L
-------
                                                                                                                                                                    8
                     •rvr ..rr """"*••"••**""••••"•"•"*"•  AIRESEARCH EMISSION  TEST  SUMMARY   »	••	
                     ENG NF6 I AIRESEARCH            TEST F»CIL I PHX LACCZ  INSTR DESCRIP  t FED REG V38  N136
                     ROOELNO.I     TPE331-S-251H      S/NI    P84001              ENGINE  TYPE(CLASSII  TURBOPROP
                     RATED POWER,    706.0 SHP AT SEA  LEVEL STANDARD DAT CONDITIONS      TYf>E«CLASS»   TURBOPROP
                     FUEL! ASTH 01655-73             ATOMIC  H/C RATIOt   1.9Z8     LHVI 16470. BTU/LB      AOOITIVESi
                                                                                                                       NONE
 CALC DATE 110-30-75
 CALC IDI   3
TEST NOI   10
                              EXHAUST EMISSIONS PER EPA  CYCLE OF MORK OUTPUT •• CODE OF FEDERAL  REGULATIONS  TITLE -.0 PART 87  17 JULY 1973

                                         C«BON MWOXIOEH|COI  *'           -'"7 LB' POLLUTANr P£R 1DO°  Hf.-H*. «« CYCLE
                                                                           15.Z96 LB. POLLUTANT PER 1000  HP.-MR. PER CYCLE
                                         OXIDES OF NITROGEN  (NOX AS NOZ)   7.94Z LB. POLLUTANT PER 1000  HP.-HR. PER CYCLE
                     T.VT in. c »TT..U.  _SMOKE                              17.3  SMOKE NUMBER, MAXIMUM AT   CRUISE    MODE
                     TAXI-IDLE SETTINCI 5.0      PERCENT RATED TAKEOFF POHER AT 65.      PERCENT RATED TAKEOFF  Nl RPH
   70 PERCENT RATED POKER
(D

to
iU
o
COMB TYPEI REVERSE FLOW ANNULAR P/Nt 66908Z-4 S JS/ VOL « 1.Z60 FUEL
ENGINE TOTAL SERVICEl 0.0 HR TIME SINCE ENGINE OVERHAUL. 0.0 HR
ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
AIRCRAFT INSTALLATION ••»• NFR. 1 MODEL NO.I
........I.......,, US£I" ENGINE INSTALLATION POSITION!
CASEOUS EMISSION TEST HO.,"".""" 	 ol^".^""10"*1 '"' S^,8"""*1" *
AMBIENT AIR TEMP.I 91.00 DEC. F RELATIVE HUMIDITY! -.8.00 PERCENT
SAMPLE LINE ••» TEMP.I 308.00 DEG. F. FLOM
TEST CONDITION
ACTUAL POWER SETTING. HORSEPOWER
CCRR. POWER SETTING (STD DAT), PERCENT RATED
Nl SPEED, RPM
FUEL FLOW (MEAS.) LB./HR.
CCRR. ENGINE CORE AIRFLOW (HEAS) . LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., OEG F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL TEMP.. DEG F
TURBINE INTERSTAGE GAS TOTAL TEMP., DEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION, NET ANALYSIS
HYDROCARBON (HC AS CH4) , PPNC
CARBON MONOXIDE (CO) , PPMV
TOTAL OXIDES OF NITROGEN (NOX). PPMV
CARBON DIOXIDE (C02I, PERCENT BY VOL.
NITRIC OXIDE (NO). PPMV
EMISSION INDEX. LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
ENISSIOK RATE. LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CN4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS, CALC)
SPECIFIC
INJ TYPE.
STAGED SIMPLEX
8ARO PRESS.. 28.770 IN. HGA.'
HUMIDITY. .015000 LB. HZO/LB. DRY AIR
PPMC CARBON MONOXIDE (CO) 1 0.0 PPMV OXIDES OF NITROGEN INGXM 0.0 PPMV
IRATE! 14.16 LITERS/MIN. TRANSPORT TIMEI 6.50 SEC. LENGTH1 50.00 FT.
264 305 206
35.0 5Z.4 73.3
5.01 7.50 10.48
27560.00 27520.00 27530.00
108.0 119.0 135.0
2.9 2.9 ».«
91.00
14.13
47.30
324.00
927.0
14.09
57.600
197.469
20.700
2.151
15.000
3.037
18.216
3.136
.328
1.967
.339
99.31
.0104
90.00
14.13
47.54
325.00
993.0
14.10
45.801
182.334
25.000
2.391
19.400
2.139
15.162
3.415
.255
1.604
.416
99.46
.0115
91.10
14.13
46.0<>
328.00
1085.0
14.10
33.000
163. 33Z
21.000
Z.671
23.600
1.407
12.185
3.431
.190
1.645
.463
99.59
.01Z8
207
212.2
30.41
41750.00
261.0
7. 7
81.00
14.13
129.67
640.00
1136.0
14.02
5.700
53.926
54.100
2.103
41.701
.311
5.13Z
8.458
.881
1.340
Z.Z07
99.85
.1111
206
491.9
70.26
41700.00
358.0
i*«>6
92.00
14.13
136.54
660.00
1377.8
14.04
1.508
19.846
77.750
2.662
72.600
.060
1.391
8. 952
.022
.496
3.ZOS
99.96
.0136
209
631.4
90.10
41750.00
41Z.O
rfL
• D
93.08
14.13
140.47
667.66
1500.8
14.07
.300
16.223
97.510
3.369
91.510
.110
.961
9.481
.884
.396
3.907
99.98
.1161
210
699.3
100.06
41730.06
436.8
7.6
90.08
14.13
14Z.76
669.81
1553.1
14.00
.300
11.617
105.088
3.673
98.750
.889
fi4f»
. D1O
9.423
• I0f»
?A4
• COl
4.108
49.98
.0174
-------
                 ..................*.....,.....,.......*...  EPA CYCLE EMISSIONS COMPUTATION SUMMARY  ••«•»»•»••
                 ENG  MFC  I  AIRESEARCH           TEST FACIL I PHX LACC2  INSTR DESCRIP I FED REG V38 N136
                 HOOEL  NO.I     TPE331-5-251H      S/NI    P0*001              ENGINE TYPE(CLASS)I TURBOPROP
                 RATED  POHERI     786.0  SHP AT  SEA LEVEL STANDARD DAY CONDITIONS
                 FUEL!  ASTH 01655-73            ATONIC  H/C RATIOI   1.928     LHVI 18*70. BTU/LB     AODITIVESa
                                                                                                                 HONE
                                                                                                      CALC DATE 110-31-75
                                                                                                      CALC 101   3
                                                                                                     TEST N0«   l«
                        MODE
n>
NJ
                                                                      TAXI-IDLE
                                                                        (INI
                                                                   TAXI-IDLE
                                                                     (OUT)
                                                                                                 APPROACH
                                                                                                              CLINBOUT
                                                                                                                             TAKEOFF
                                                               TOTAL PER
                                                                CYCLE
TINE IN MODE, MINUTES
RATED POWER, PERCENT
CORRECTED POWER. HORSEPOWER
HP-HR
FUEL FLON, LB/HR
FUEL MASS. LB

 " HYDROCARBON EMISSIOK  (HC1 "
INDEX, LB HC/liOO LB FUEL
RATE. LB HC/HR
MASS. LB HC
NASS, PERCENT OF TOTAL CYCLE
CYCLE. LB HC/1001 HORSEPOWER-MR PER CYCLE

 »• CARBON MONOXIDE EMISSIONS (CO) •»
INDEX, LB CO/1000 LB FUEL
RATE, LB CO/MR
BASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/10BB HORSEFOHES-HR PER CYCLE
                                                        (NOXI
                 ** TOTAL OXIDES OF NITROGEN EMISSIONS
                INDEX, LB NOX/IOBO LB FUEL
                RATE. L8 NOX/HR
                NASS, LB NOX
                HASS, PERCENT OF TOTAL CYCLE
                CYCLE, LB NOX/1DOO HORSEPOUER-HR PER CYCLE
                                                                          7.000
                                                                          5.000
                                                                         35.300
                                                                          4.118
                                                                        107.980
                                                                         1Z.598
                                                                          3.039
                                                                           .328
                                                                           .038
                                                                           Z5.8
18.2Z2
 1.961
  .230
  23.6
                                                         3.135
                                                           .339
                                                           .039
                                                           7.8
             19.110
              5.001
             3S.300
             11.178
            107.980
             3*.19*
              3.039
               .326
               .10*
               70.0
                                                                                      18.222
                                                                                       1.968
                                                                                        .623
              3.135
               .339
               .107
               21.2
  d.500
 30.009
211.800
 15.885
258.753
 19.1,06
   .312
   .081
   .006
  5.175
  1.339
   .100
   10.3
  8.309
  2.158
   .161
   32.8
  2.500
 90.000
635.*00
 26.1,75
-------
                                                                                                                                                                     CO
(D

to
£*
to
ENGINE' TPE331-5-251M S/N« P0*001 COMB P/N« 8690B2-*
RAT SHP' 706. RA EGT.F' 1650. RAT SPO« *1730. DEH PT,F= 68.
FUEL H/C= 1.9280 STOI F/A= .06822 L H V« 18*70. S LN T.F' 300.0
DATA POINT NUMBER
PERCENT MAX. CORRECTED POKER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Nl, RPM
COMPRESSOR INLET TEMP..DEG.F
COMPRESSOR OSCHG. PRES. ,PSIA
COMPRESSOR OSCHG. TENP.OEG F
TURB INTERSTAGE TEMP., OEG.F
CORR BELMTH FLOH, LB/SEC
FA RATIO BASED ON BELLNTH.
MEASURED FUEL FLOH, LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P»»N/V/E«T/5*fl>
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, kET
LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME. HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOK, LB./HR.
UNBURMEO HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NO) - HEIGHTS AS
PPH BY VOLUME, MET
LB. PER 1100 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE IN02)
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
5.0
35.3
35.0
27560.0
91.0
*7.3
32*. 0
927.0
2.91
.0110
108.0
.0101.
.152
.316
99.305

2.15
3.12
336,6

197.5
18.216
1.967
205
7.5
53.0
52.*
27520.0
90.0
1.7.5
325.0
993.0
2.87
.0123
119.0
.0115
.169
.309
99.U56

2.39
3.12
371.8

182.3
15.162
1 .80*
CARBON, HEIGHTS AS
57.6
3.037
.328
.1667
N02
15.0
2.273
.2*5

5.7
.86*
.093
1.5.0
2.139
.255
• 1*11

19.*
2.650
.315

5.6
.765
.091
206
10.5
7*.0
73.3
27530.0
91.0
1.8.0
328.0
1085.0
2.82
.01*2
135.0
.0128
.188
.296
99.590

2.67
3.13
*22.7

163.3
12.185
1.6*5
CM*
33.0
1.1.07
.190
.1155

23.6
2.892
.390

*.*
.539
.073
207
30.*
21*. 7
212.2
1.1750.0
88.0
129.7
6*0.0
1136.0
7.73
.0100
261.0
.0101
.1*7
.080
99.852
REDUCED
2.10
3.15
820.9

53.9
5.132
1.3*0

5.7
.310
.081
.060*

*1.7
6.519
1.701

12.*
1.939
.506
TOTAL OXIDES OF NITROGEN (NO*N02> AS N02
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NtJttflCft
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLCH
SMOKE NUMBER
SMOKE NUMBER AT NA'0.023
20.7
3.136
.339

.00708
3.50
.0212*
7.00
.035*0
9.30
.0*956
9.30
7.30
25.0
3.1.15
.1.06

.00702
5.80
.02105
5.80
.03508
7.00
.0*911
7.00
6.*0
28.0
3.1,31
.*63

.00707
5.80
.12120
5.80
.035*7
7.00
.0*98*
8.10
6.70
5*.l
e.*58
2.207

.00718
8.10
.0215*
11.60
.03590
17.1.0
.05027
22.10
1*.80
208
70.3
1.96.0
1.91.9
1.1700.0
92.0
136.5
660.0
1377.0
7.6*
.01*0
358.0
.0136
.200
.079
99.962
FUEL' AV. KERO. TEST NO.' 10
REL HUM- 1.8.80 SPEC HUM* .015000
FLO.L/H' 1*.160 SL TIM.S* 6.5000
209
90.
636.
631.
1.1750.
93.
1*0.
667.
1500.
7.62
.0161
1.12.0
.0161
.236
.065
99.977
210
100.1
706.*
699.3
1.1730.0
90. 0
1*2.8
669.0
1553.0
7.6*
.0170
*36.0
.017*
9CC
. £79
• 06*
99.98*

2.86
3.15
1128.3

19.8
1.391
.*98

1.5
.060
.022
.0*32

72.0
8.290
2.968

5.8
.662
.237

77.7
8.952
3.205

.00707
7.00
.02121
15.10
.03528
20.90
.0*9*0
25.60
17.30
3.39
3.15
1298.8

16.2
.961
.396

.3
.010
.00*
.0106

91.5
8.899
3.667

6.0
.58*
.2*0

97.5
9.*83
3.907

.00690
9.30
.0209*
12.80
.13*90
19.00
.0*806
2*.*«
16.00
3.67
3.15
137*. 7

11.8
.6*6
.281

.3
.009
.00*
.01*5

98.8
8.862
3.86*

6.3
.561
.2*5

105.0
9.1.23
*.110

.0069*
7.00
.02002
11.60
.03*71
17. *0
.0*062
19.80
1*.20
                       NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE NET VALUES.
                             2.EQUIVALENCE RATIO CALCU.ATEO FROM C02.CO.ANO MC DATA AND FUEL COMPOSITION.
                             3.MASS EMISSIONS OF NO. N02. AND NO+N02 CALCULATED AS N02 FROM CONCENTRATIONS HITH MOLECULAR HEIGHT OF N02  1*6.011.
-------
                       .........I.....................................  AIRESEARCH EMISSION TEST SUMMARY  »•»••»*••'
                       ENG MFC t  AIRESEARCH           TEST FACIL « PHX LACCZ  INSTR OESCRIP  I FED REG V38 N136
                       MODEL NO.!     TPE331-5-251M     S/NI   P04001              ENGINE TYPtlCLASSM  TURBOPROP
                       RATED POWER!    706.0 SHP AT SEA LEVEL STANDARD DAY CONDITIONS
                       FUEL! ASTM D1655-73            ATOHIC H/C RATIO!   1.9Z6     LHVl 18470. BTu/LB
                 CALC DATE 110-31-75
                 CALC 101    1
                TEST N0«   11
ADDITIVES!  NONE
                       ,„..».., EXHAUST EMISSIONS PL* EPA CYCLE OF WOR< OUTPUT »• CODE OF FEDERAL REGULATIONS  TITLE  40  PART  87   17  JULY  1973   »•»••»»
                                           HYDROCARBONS (CH AS CH4)          3.306 LB. POLLUTANT PER 1000 HP.-HR.  PER CYCLE
                                           CARBON MONOXIDE (CO)             17.647 L3. POLLUTANT PER 1000 HP.-HR.  PER CYCLE
                                           OXIDES OF NITROGEN  (NOX AS NOZ)   7.Z10 ..3. POLLUTANT PER 1000 HP.-HR.  PER CYCLE
                                           SMOKE                             16.1  SHOKE NUMBER, MAXIMUM AT  CRUISE     MODE, 70 PERCENT RATED POWER
                       TAXI-IDLE SETTING! 5.0      PERCENT RATED TAKEOFF POWER AT 65.      PERCENT RATED TAKEOFF Ml  RPN
 T)
 0>
iQ
 (T)

 NJ
 £>.
 U)
                       .......».........,».».»...,..............»......*...  ENGINE DESCRIPTION  ••••»••••••••*•••••»•••••••••••»••••••••••••»»»•••••
                       COMB TYPE! REVERSE FLOW ANNULAR           P/NI   869082-4           SUR/VOLI 1.260  FUEL  INJ  TYPEI   STAGED  SIMPLEX
                       ENGINE TOTAL SERVICE!  0.0       HR    TIME SINCE ENGINE OVERHAUL!  0.1       HR                              . .    _  .
                       ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                       AIRCRAFT  INSTALLATION ***• MFR.1                                 MODEL NO.I
                                                  USER!                       ENGINE INSTALLATION POSITION!
                       .»...».....,.,.,.........»..»»».»»».»»»»»»,».»,.OP£R4IIONAL TESI OATA SUMMARY ••«»••••«»••»«»•»••••»»•»••»••»••••»«•»•••••••••
                       GASEOUS EMISSION TEST NO.I   11         DATE! 10-30-75           TIME!                    BARO PRESS.I   28.700 IN.  HGA.
                       AMBIENT AIR TEMP.I  91.00 OEG.  F        RELATIVE HUMIDITY!  65.00 PERCENT       SPECIFIC  HUMIDITY!   .020000  LB.  H2O/LB.  DRY AIR
                       AMBIENT AIR QUALITY    HYDROCARBONS (HOI 0.0   PPMC     CARBON MONOXIDE CCO) I 0.0   PPMV     OXIDES  OF NITROGEN  (NOX) I  0.0    PPMV
                       SAMPLE LINE ••• TEMP.I  300.00  DEG. F.     FLOWRATE8   14.16 LITERS/HIM.     TRANSPORT  TIME!     6.50 SEC.     LENGTHI    50.01 FT.
TEST CONDITION
ACTUAL POWER SETTING, HORSEPOWER
CORf. POWER SETTING (STO DAY), PERCENT RATED
XI SPEED, RPM
FUEL FLOW IMEAS.I LB./HR.
CORR. ENGINE CORE AIRFLOW (MEAS), LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., OEG F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAi. PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL TEMP., DES F
TURBINE INTERSTAGE GAS TOTAL TEMP., BEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION. WET ANALYSIS
HYDROCARBON (HC AS CHI,), PPMC
CARBON MONOXIDE (CO), PPMV
TOTAu OXIDES OF NITROGEN (NOXI, PPMV
CARBON DIOXIDE (C02) , PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSION INDEX, LB. POLLUTANT/1000 L8. FUEL
HYDROCARBONS (HC AS CH4)
CARSON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH4I
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS N02)
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS, CALC)
211 212 213
34. >
4.99
275ZO.OO
113.0
3.0
90.00
14.10
48.04
310.00
918.0
14.06

78.000
Z23.264
18.500
2.204
13.000

4.006
20.063
2.790

.453
Z.Z67
.315
99.19
.0107
50.5
7.22
27550.00
124.0
2.9
93.00
14.10
48. Z3
313.00
982.0
14.06

60.300
Z09.119
zz.ooo
2.386
16.400

Z.867
17.396
3.006

.356
2.157
.373
99.34
.0115
70.4
10.11
27570.00
133.0
2.9
88.00
14.10
49.02
310.00
1040.0
14.06

53.700
196.564
24.800
2.613
20.100

2.336
14.959
3.100

.311
1.989
.412
99.44
.0126
214
210.1
30.20
41750.00
266.0
7.8
88.00
14.10
130.75
618.00
1118.0
13.99

12.300
61.036
49.200
2.117
36.400

.664
S.766
7.635

.177
1.534
2.031
99.81
.0101
215
489.0
70.20
41750.00
362.0
7.7
89.00
14.10
138.75
622.00
1360.0
14.01

3.300
23.890
70.000
2.873
63.000

.132
1.668
8.027

.048
.604
2.906
99.95
.0137
216
629.1
90.07
41730.00
416.0
7.7
92.00
14.10
141.80
629.00
1510.0
14.03

.601
19.846
84.000
3.413
79.751

.021
1.166
8.111

.118
.485
3.374
99.97
.0162
217
698. Z
100.05
41740.01
443.0 	 	 . . ._
7.7
91.00
14.11 ___.....
143.57
630.00
1600.0 . . . . ._.. .
14.05

.301
19.846
91.251
3.609
87.001

.010 .... _... 	 _
1.103
8.331

.004
.4)89
3.692
99.97
.1171
-------
n>
•£N6 MFC I AIRESEARCM            TEST
 MODEL NO.I     TPE331-5-2S1H     S/NI
 RATED FOWERI    706.0  SHP  AT SEA LEVEL
 FUEL. ASTM 01655-73             ATOMIC H/C RATIOI
   EMISSIONS COMPUTATION SUMMARY  •»••»»»»»«
    INSTR DE5C3IP  I  FED REG  V38 N136

 CONDITION""**  T">EIC14SS"   TURBOPROP
1.928     LHV« 18*70. BTU/LB     ADDITIVES.
                                                                                                                          NONE
                                                                                                                               CALC DATE 110-30-75
                                                                                                                               CALC 101     1
                                                                                                                              TEST  NOI    11

MODE
TIME IN K03E, HINUTES
RATED POKER. PERCENT
CORRECTED POWER, HORSEPOWER
HP-MR
FUEL FLCK, LB/HR
FUEL MASS, LB

*• HYDROCARBON EMISSION INC) *•
INDEX, LB HC/1000 LB FUEL
RATE. LB HC/HR
MASS, LB HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORStPOWER-HR PER CYCLE

•• CARBON MONOXIDE EMISSIONS (CO) ••
INDEX, LB CO/1000 LB FUEL
RATE, LB CO/HR
MASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORS£POWER-HR PER CYCLE

•• TOTAL OXIDES OF NITROSEN EMISSIONS CNOXI »»
INDEX, LB NOX/1000 LB FUEL
RATE, LB NOX/NR
BASS, LB NOX
NASS, PERCENT OF TOTAL CYCLE
CYCLE, LB NOX/1000 HORSEPOWER-HR PER CYCLE


TAXI-IOLE
(INI

5 . 000
35.300
113.057
13.190

3.999
.',52
-25.1


20.0.0
                                                   8.3
   B
31.9
 6.1
26.0
                                                ASSUMES  PROPORTIONAL REDUCTION OF POLLUTANT EMISSION INDEX AT EACH  LTD CYCLE MODE
-------
                                                                                                                                                                        fc
 13
 fa
iQ
 CD
ENGINE' TPE3St-5-Z51H S/N* P04001 COM3 P/N= •69083-'. FUEL- AV. KERO. TEST N0.« 11
RAT SHP- 706. RA E6T,F= 1650. RAT SPO= ".1730. OEM PT.F* 77. ML MUM« 65.00 SPEC HUM- .OZ8000
FUEL H/C- 1.9240 STOI F/A=
OATA POINT NUMBER
PERCENT NAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED. Nl, RPN
COMPRESSOR IN.ET TEMP., DEC. F
COMPRESSOR OSCHG. PRES..PSIA
COMPRESSOR DSCHG. TEMP.CEG F
TURB INTEP.STAGE TEMP., OES.F
CORR 3ELMTH FLOH, LB/SEC
FA RATIO BASED ON BELLHTH.
MCACiiDcn FIICI Ft nu i R./MC
ncldUKtU r UcL r I»U** « IDr n?c
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING M/F"N/V/£«T/540»
COHB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
L3. C02 PER LB. OF FUEL
MEIGHT FLOM, LB./HR.
CARBCN MONOXIDE
PPM BY VOLUME. NET

LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
UN8URNEO HYDROCARBONS- PPM AS
PPH BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOW, LB./HR.
RATIO LB HC/LB CO
NITRIC CXIDE (NOI - MEIGHTS AS
PPH 3Y VOLUHE. MET
L3. PER 1010 LB. OF FUE..
MEIGHT FLOM, LB./HR.
NITROGEN DIOXIDE INOZI
PPM BY VOLUME. WET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOH, LB./HR.
.06822
211
5.0
35.2
34.8
27520.0
90.0
1.8.0
310.0
918.0
2.96
.0111.
113.0
.0107
.156
.321
99.177

2.20
3.11
351.6

223.3
9 n flfk ^
£ 11. UO<>
2.267
L H V=
212
7.2
51.0
50.5
27550.0
93.0
1.8.2
313.0
982. 0
2.92
.0127
124.0
.0115
.169
.312
99.339

2.39
3.12
386.7

209.1
1 7 1Q6
i 1 • J9O
2.157
CARBON. MEIGHTS AS
78.0
1
.278

5.6
.765
.095
161.70.
213
10.1
71.1.
70.1.
27570.0
88.0
1.9.0
310.0
10^.0,0
2.92
.0136
133.0
.0126
.181.
.306
99.1.1.3

2.61
3.12
1.15.5

196.6
!*»• 959
1.989
CHI.
53. r
2.336
.311
. 1562
20.1
2.513
.331.

4.7
.508
.078
S LN T.F*
21<.
30.2
213.2
210.1
1.1750.0
88.0
130.7
618.0
1118.0
7.78
.0182
266.0
.0101
.11.9
.083
99.806
OF REDUCED
2.12
3.14
836.1

61.0
5. 766
1.531.

12.3
.661.
.177
1 4 C9
• 1X9£
36.4
5.6*9
1.503

12.8
1.9B6
.520
300.0
215
70.2
495.6
469.0
41750.
89.
138.
622.
1360.
7.74
.0139
362.0
.0137
.280
.074
99.949
EMISSION
2.87
3.15
1140.7

23.9
1.668
.604

3.3
.132
.048
. 0790

63.0
7.224
z.eis

7.0
.8(3
.291
TOTAL OXIDES OF NITROGEN  AS NOZ . .
• PPC. BY VOLUME. MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM. LB./HR.
SMOKE MEASUREMENT OATA
CORRECTED HEIGHT FLCM
SMOKE NUHBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED MEIGHT FLON
SMOKE NUMBER
CORRECTED MEIGHT FLOH
SMOKE NUMBER
SMOKE NUMBER AT HAM. 023
18.9
2.790
»* c
• Jl?
.00713
'•.00
.•2139
Z.40
.03579
3.60
.05010
.l
3.100
1*1 9
*Hl£
.00711
0.00
.0215k
1.20
.03590
1.20
.05027
3.60
1.50
1.9.2
7.635
2n Yf
. UOl
.00717
4.00
.02152
10.70
.03586
15.50
.05021
21. 40
13.10
70.0
8.027
2.906

.00716
6.00
.82147
15.50
.03579
20.20
.05008
22.60
16.11
FLO,L/M=
216
90.1
635.9
629.1
41730.
92.
141.
629.
1510.
7.78
.0161
416. •
.•162
.237
.069
99.971

3.41
3.15
1311.3

19.8
1.166
.485

.6
.020
.008
.8173

79. 7
7.700
3.2D3

4.3
.410
.171
. 	 _.
84.0
8.110
3.374

.••715
6.0*
.02146
11.30
.03577
16.78
.05017
21.40
13.90
. 14.160 SL TIN, 5* 6.500*
217
108.1
706.4
698.2
41741.*
91.1 	 .... - - .......
143.6
630.1
1600.0 	 	 _. . ......
7.78
.0172
443.1
.0171
.251
.068 . .. . 	 	
99.973
_ 	 	 ... 	 	 -
3.61
3.15
1396.5 . _ 	 .. . ... - - -

19.8
1.103 . . 	 	 	 _.
.489

.3. ....... . 	 	 -
.018
.014
.0086

87.1
7.945 	 	 . 	 	
3.521

_ . 4.3 	 	 	 _.. .. 	 -
.388
.172
. . .. . — — .. 	 - . ^ . . ~. 	 — 	 •
91.3
8.333
3.692 . ...

.••719
4.81.. 	 . . ._ 	 	 	
.02146
11.9*
.03514 _ _ 	 	 .. .
16.71 '
.85015
22.61 ..._.... ... 	
14. ••
                       NOTES 1. ALL  EMISSIONS CONCENTRATIONS ARE MET VALUES.
                             2 EQUIVALENCE RATIO CALCULATED FROM COZ.CO.ANO HC  DATA AND FUEL COMPOSITION.
                             3.MASS  EMISSIONS OF NO.  N02. AND NO+N02 CALCULATED AS NOZ FROM CONCENTRATIONS  MITH
MOLECULAR MEICHT OF  NOZ K.6.81).
-------
.............................................  AIRESEARCH EMISSION  TEST  SUMMARY   »•••«»»»«•«•»•
ENG MFG I AIRESEARCH            TEST FACIL I PHX LACCZ  INSTR DESCRIP  t FED REG V38  N136
MODEL NO.S     TPE331-5-251M      S/NI    P04001              ENGINE  TYPE(CLASS)!   TURBOPROP
RATED POWERS     706.0  SHP  AT  SEA  LEVEL STANDARD DAY CONDITIONS
FUELS ASTM 01655-73             ATOMIC  H/C RATIO!   1.928     LHVS 18470.  BTU/LB      ADDITIVES!
                                                                                                                               CALC DATE 110-30-75
                                                                                                                               CALC IDI   2
                                                                                                                              TEST NOI  11
                                                                                                                          NONE
                        ........ EXHAUST  EMISSIONS PER EPA CYCLE OF WORK OUTPUT ••  CODE  OF  FEDERAL  REGULATIONS TITLE 40 PART 87  17 JULY 1973  »•••»•*
                                             HYDROCARBONS ICH AS CH4)          2.887 LB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                             CARBON MONOXIDE ICO)             17.253 ..B.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                             OXIOES OF NITROGEN (NOX AS N02)   7.077 LB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                             SMOKE                              14.7   SMOKE  NUMBER, MAXIMUM AT  CRUISE    HOOE,  70 PERCENT RATED POWER
                        TAXI-IDLE  SETTINGS  5.8      PERCENT RATED TAKEOFF POWER AT  65.       PERCENT RATED TAKEOFF Nl RPM
 0)
05
 (I)
                         [[[  tN6iNE  DESCRIPTION  »•••••»»•••»•••»•••»•••••«••••»•»•••••••••••••••••»•
                         COMB  TYPE!  REVERSE FLOW ANNULAR           P/NS    869082-4            SUR/VOLS  1.260  FUEL INJ TYPE!  STAGED SIMPLEX
                         ENGINE  TOTAL  SERVICE!   0.0       HR    TINE SINCE ENGINE OVERHAUL!   0.0       MR
                         ENGINE  ASSEMBLY AND MAINTENANCE INFORMATION!
                         AIRCRAFT  INSTALLATION  »••• MFR.S                                   MODEL  NO.t
                                                    UStRt                        ENGINE  INSTALLATION POSITION!
                         ........................................»»«».».»QPERATIONAL TEST  DATA SUMMARY »»»•»»»»»•»»»•«»»»»•••»»»»»»»•»»•»»•»»»•»»•»»»•»
                         GASEOUS EMISSION TEST  NO.I  11          OATEI 10-30-75            TIME!                     BARO PRESS.!  28.700 IN. HGA.
                         AMBIENT AIR TEMP.I  91.00 DEG. F         RELATIVE  HUMIOITYS  65.00 PERCENT       SPECIFIC HUMIDITYI  .020000 LB. H20/LB. DRY  AIR
                         AMBIENT AIR QUALITY    HYDROCARBONS (HOI 0.0   PPMt     CARBON MONOXIDE (CO)! 0.0   PPMV    OXIOES OF NITROGEN (NOX)I 0.0    PPMV
                         SAMPLE  LINE *** TEMP.S  300.00 OEG. F.     FLOWRATEI   14.16  LITERS/MIN.     TRANSPORT TIME!    6.50 SEC.     LENGTH!   50.00 FT.
) TEST CONDITION
ACTUAL POWER SETTING, HORSEPOWER
CORR. POWER SETTING ISTD DAY), PERCENT RATED
) Nl SPEED, RPH
FUEL FLOW IMEAS.) LB./HR.
CORR. ENGINE CORE AIRFLOW IMEAS), LB/SEC
) COMPRESSOR INLET AIR TOTAL TEMP., OEG F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS., PSIA
) COMPRESSOR DISCHARGE AIR TOTAL TEMP., DEG F
TURBINE INTERSTAGE GAS TOTAL TEMP., 3EG F
EXHAUST GAS STATIC PRESSURE, PSIA
) EMISSION CONCENTRATION, NET ANALYSIS
HYDROCARBON (HC AS CHI.) , PPMC
CARBON MONOXIDE (CO), PPMV
) TOTAL OXIOES OF NITROGEN (NOX), PPMV
CARBON DIOXIDE IC02) , PERCENT BY VOL.
NITRIC OXIDE INO) , PPMV
) EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
) TOTAL OXIOES OF NITROGEN (NOX AS NOZ)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CH«I
) CARBON MONOXIDE ICO)
TOTAL OXIOES OF NITROGEN INOX AS NOZ)
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
1 F/A (EMISSIONS, CALC)
218 Z19 220
35.0
5.00
27550.00
112.0
2.9
95.00
14.10
47.50
313.00
907.0
14.07

67.500
220.418
19.200
2.194
14.000

3.484
19.905
2.848

.390
2.229
.319
99.23
.0106
53.6
7.68
27500.00
125.0
2.9
90.00
14.10
48.04
312.00
968.0
14.06

59.700
206.782
22.200
2.411
16.400

2.810
17.025
3.002

.351 .
2.128
.375
99.35
.0116
73.3
10.52
27520.00
136.0
2.9
89.00
14.10
48.82
311.00
1064.0
14.06

48.600
192.413
25.300
2.752
20.900

2.009
13.914
3.005

.273
1.892
.409
99.50
.0132
221
210.9
30.30
41750.00
263.0
7.7
88.00
14.10
130.80
616.00
1121.0
13.99

12.000
61.036
46.000
2.099
34.800

.654
5.818
7.203

.172
1.530
1.894
99.81
.0100
222
488.2
70.29
41710.00
362.0
7.7
86.00
14.10
138.75
620.00
1360.0
14.00

1.500
27.546
68.750
2.884
62.750

.060
1.915
7.852

.022
.693
2.843
99.95
.0137
223
641.7
91.87
41760.00
421.0
7.7
92.00
14.10
142.29
629.00
1488.0
14.03

.600
19.039
87.750
3.426
80.750

.020
1.115
6.442

.008
.469
3.554
99.97
.0162
22*
70Z.2
100.54
41740.00
446.0 	 .._. 	
7.7
92.00
14.10 .. . . .
143.91
631.00
.1541. •__ 	 ...'_. __•
14.05

.308
17.428
91.250
3.609
87.759

	 .010 	 	
. 969
8.334

.00% • 	
.432
3.717 . 	 	 .
99.98
.0171
-------
(0
                    *.».....».•»•••.•.»•.*.••».*..*•••.»•»..**  EPA CYCtE EMISSIONS COMPUTATION  SUMMARY  «•••••••»«
                    EN6  NFG  t  AIRESEARCH           TEST FACIL  I PHX LACC2   INSTR OESCSIP  >  FED REG  V38 N136
                    MODEL  NO.I     TPE331-5-251M     S/N1   P04001              ENGINE  TYPE(CLASS)!   TURBOPROP
                    RATED  POWER I     706.0 SHP AT SEA LEVEL STANDARD DAY CONDITIONS
                    FUELt  ASTM 01655-73            ATOMIC H/C  RATIOI   1.928     LHVt 18470.  BTU/LB     ADDITIVES!
                          CALC DATE HO-30-75
                          CALC 101    2
                         TEST  NOI   11
                     NONE
NODE
TIME IN NODE, MINUTES
RATED POWER, PERCENT
CORRECTED POWER, HORSEPOWER
HP-HR
FUEL FLCN, LB/HR
FUEL MASS. LB
•• HYDROCARBON EMISSION IHC) **
INDEX, LB HC/1801 LB FUEL
RATE, LS HC/HR
MASS, LB HC
MASS, PERCENT OF TOTAL CYCLE
CrCLE, LB HC/1000 HORSEPOMER-HR PER CYCLE
»• CARBON MONOXIDE EMISSIONS ICOI •*
INDEX. LB CO/1000 LB FUEL
RATE, LB CO/HR
MASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/ 1001 HORSEPOHER-HR PER CYCLE
•• TOTAL OXIDES OF NITROGEN EMISSIONS INOXI •»
INDEX, LB NOX/10IO LB FUEL
RATE. LB NOX/HR
MASS. L8 NOX
MASS, PERCENT OF TOTAL CYCLE
CYCLE. LB NOX/1000 HORSEPOHER-HR PER CYCLE
TAXI-IDLt 1
(INI
7.000
5.000
35.300
"..116
112.011.
13.068

3.484
.390
.0*6
24.8


19.902
2.229
.260
23. 7

- - - 	
2.8*8
.319
.037
6.3

rAXI-IOLE
IOUTI
19.000
5.000
35.300
11.17*
112.011,
35.471

3.1.61.
.390
.124
67.4


19.902
2.229
.706
Ed.*

-...---- _ -
2.848
.319
.101
22.5

APPROACH
4.500
30.000
211.800
15.885
260.309
19.523

.630
.164
.012
6.7


5.706
1.516
.113
10.3

.
7.129
1.656
.139
31.0

CLIMBOUT
2.500
90.000
635.400
26.475
408.744
17.131

.106
.043
.002
1.0


.762
.311
.013
1.2

" ~ 	 "
8.268
3.380
.141
31.3

TAKEOFF
.500
100.000
706.000
5.883
447.783
3.732

.068
.131
.000
.1


1.155
.517
.004
.4

......
8.421
3.771
.031
7.0

TOTAL PER
CYCLE
33.501


63.541

88.82$

2.065
.329
.183
100,0
2.887

12.342
1.963
1.096
100.0
17.253
	
5.062
.805 	
.451
100.8
7.077
                                                                                                                                                                 3:

                                                                                                                                                                 y
                                          »•  EHISSION INDEX LEVELS REQUIRED TO MEET EPA 1979 STANDARDS FOR CLASS P2 ENGINES
                                       EPA  LTO-CYCLE
                                                                                               REQUIRED EMISSION  INDEX,  LBP/1000  L8 FUEL
                               POLLUTANT    LBP/1000  HORSEPOHCT-HR-CYCLE
                                  CO              26.8
                                  HC               4.9
                                  NOX             12.9
POLLUTANT (MODE)
   CO IIDLE I
   HC HOLE)
   NOX (TAKEOFF)
   A
19.9
 3.5
 8.4
   8
32.4
 6.1
26.5
                                          A   ASSUMES PROPORTIONAL REDUCTION OF PCL.UTANT EMISSION INDEX AT EACH LTO CYCLE MODE

                                          B   ASSUMES (II REQUIRED REDUCTION IN CO AND HC OBTAINED BY LOWERING EMISSION  INDEX VALUES
                                             AT  TAXI-IDLE MOOE ONLY, CO AND HC EMISSIONS AT OTHER MOOES %£MAIN UNCHANGED, (21 REQUIRED
                                             REDUCTION IN NOX OBTAINED 3Y LOWERING EMISSION INDEX VALUES AT CLIMSOUT  AND TAKEOFF  MODES  IN
                                             SAME  PROPORTION AS MEASURED VALUES, NOX EMISSIONS AT TAXI-IDLE AND APPROACH MODES
                                             REMAIN UNCHANGED
-------
 ta
iQ
 ID

 to
 *»
 CO
1



ENGINE- TPE331-5-Z51M S/N= POI.001 COM3 P/N= 869083-1. FUEL* AV. KERO. TEST N0.« 11
RAT SHP= 706. RA EGT,F=
1 FUEL H/C* 1.9Z8D STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED. Nl, RPM
COMPRESSOR INLET TEMP. .OEG.F
COMPRESSOR OSCHG. PRES..PSIA
COMPRESSOR OSCHG. TEHP.DEG F
TURB INTERSTAGE TEMP., CEG.F
CORR BELMTH FLOH, LB/SEC
FA RATIC BASED ON BELLMTH.
MEASURED FUEL FLOH, LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING N/P"N/V/E«T/5%0)
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
) LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
) PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNED HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
> HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NOI - HEIGHTS AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
i HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE . 0
210.9
1,1750.0
88.0
130.8
616.0
1121.0
7.74
.0101
263.0
.0100
.11,7
.083
39.806
OF REDUCED
2.10
3.H,
826.6

61.0
5.818
1.530

•12.0
.651.
.172
.1121,

3 it. 8
5.1,1,9
1.1,33

11.2
1.751,
.1,61
77.
300.0
222
70.3
1,96.2
1.88.2
1.1710.0
80.0
138.8
630.0
1360.0
7.71.
.0139
362.0
.0137
.201
.071.
99.950
EMISSION
2.88
3.15
1140.6

27.5
1.915
.693

1.5
.060
.022
.0311

62.7
7.167
2.59%

6.0
.685
.2%8
RE.. HUM*
FLO, L/ MI
223
91.9
61,8.6
61.1.7
1,1760.0
92. 1
11.3.3
629.0
11.88.0
7.69
.0163
1,21.0
.0162
.238
.069
99.972

3.1,3
3.15
1327.1

19.0
1.115
.1,69

.6
.028
.008
.0180

81.7
7.768
3.271

7.1
.673
.28%
65.00 SPEC HUM' .020001
11.. 160 SL TIH,S« 6.5101
Z2%
100.5
709.8
702.2
fcl 740. C
92.1
11.3.9
631.1
151.1.0
7.69
.0173
1.1,6.1
.1171
.251
.167
99.976

3.61
3.15
11,06.1

17.%
.969
.1.32

.3
.111
.00%
.1098 	 	 	 	

87.7
8.01% . . . . . _
3.57%

3.5 	 	
.321
.11.3
TOTAL OXIDES OF NITROGEN (NCtNOZI AS NOZ
PPM BY VOLUME, HET
' LB. PER 1000 L8. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MtASUREMENT DATA
) CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
> SHONE MMtBEK
CORRECTED HEIGHT FLCN
SMOKE NUMBER
' CORRECTED HEIGHT FLC*
SMOKE NUMBER
SMOKE NUMBER AT HA'0.023
19. Z
2.81.8
.319

.00711,
0.00
.0311.1
1.21
.03568
2.1.0
.01.995
3.60
1.80
22. Z
3.002
.375

.00713
1.21
.02139
2.1.0
.03565
3.60
.01,989
3.60
2.71
25.3
3.005
.1(09

.00712
0.00
.02135
2.1.0
.03559
2.1.0
.01.983
3.60
2.11
1,6.0
7.283
1.89%
•
.00711
3.61
.02132
10.70
.03553
16.70
.01,981,
20.20
12.91
68.8
7.852
2.81.3

.00710
%.ll
.02131
13.10
.03552
19.00
.01.983
21. %0
11.. 70
87.7
8.1,1,2
3.55%

.01709
%.80
.02127
11.90
.13551
1%.91
.01,972
Zl.%0
13.31
91.3
8.33%
3.717 	

.10711
3.61
.02131
11.91
.13551
16.71
.01.972
20.11
13.11
                                                                                                                                                                     K
                         NOTtS 1.  ALL EMISSIONS CONCENTRATIONS ARE HET VALUES.
                               2.EQUIVALENCE  RATIO CALCULATED FROM C02.CO.ANO HC DATA AND FUEL COMPOSITION.
                               3.MASS EMISSIONS OF NO, N02, AND MO*NOZ CALCULATED AS NOZ FROM CONCENTRATIONS HITH MOLECULAR HEIGHT OF NOZ  (1.6.111.
                                                                                                                                                                     S
                                                                                                                                                                     .CTi
-------
 0>
iQ
 ro
 NJ
                                                                                                                                 CALC DATE 110-31-75
                                                                                                                                 CALC ID!   3
                                                                                                                                TEST NOI     11
                                                                                                                ADDITIVES!  NONE
•»••»»..».»»»»•»•»•»».»•••»••••»••••••»»•••••   AIRESEARCH EMISSION TEST SUMMARY  ••»•»••••
ENG MFG I AIRtSEARCH           TEST FACIL  I  PHX LACC2   INSTR OESCRIP I FED REG V38 N136
MODEL NO.I     TPE331-5-251M     S/NI    P0*001               ENGINE TYPE(CLASS)I  TURBOPROP
RATED POHtRI    706.0 SHP AT SE« LEVEL  STANDARD DAY  CONDITIONS
FUEL! ASTM 01655-73            ATOMIC H/C  RATIO!   1.928      LHVI 18*70. BTU/LB

........ EXHAUST EMISSIONS PE-* £PA C/CLE OF  WORK OUTPUT •• CODE OF FEDERAL REGULATIONS TITLE UO PART 87   17  JULY  1973  ••••»»•
                    HYDROCARBONS (CH AS CHI.)           3.605 L3. POLLUTANT PER 1COO HP.-HR. PER CYCLE
                    CARBON MONOXIDE  (CO)             18.513 LB. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                    OXIDES OF NITROGEN  (NJX  AS  N02)    7.558 LB. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                    SMOKE                              16.8  SMOKE NUMBER, MAXIMUM AT  CRUISE    MODE,  70  PERCENT RATED POME*
TAXI-IDLE SETTING! 5.0      P£xCENT  RATED  TAKcOFF POKER AT 65.      PERCENT RATED TAKtOFF Nl RPM

..,.......,..,,,,........*...............»*•••••»•»   ENGINE DESCRIPTION  »•"""<
CCMB TYPEI REVERSE FLOM ANNULAR            P'NI    869082-*           SUR/VOLI 1.360
ENGINE TOTAL SERVICE!  0.0        HR     TIME  SINCE ENGINE  OVERHAUL!  0.0       MR                  _            	
ENGINE ASSEMBLY AND MAINTENANCE  INFORMATION!
AIRCRAFT INSTALLATION •••• MFR.I                                  MODEL NO.I
                           USER»                        ENGINE INSTALLATION POSITION!                                        .   .  ..
•».»»»••»».»»»»••"•"""»"""""*"" """OPERATIONAL TEST DATA SUMMARY "»•»»»»••*•»»"•""••"""»••"*«"•»•*«»»»
GASEOUS EMISSION TEST NO.I     11        DATE!  10-31-75            TIME!                    BARO PRESS.!  28.600 IN.  HGA.
AMBIENT A" TEHP.I  91.00 DEG. F         RELATIVE  HUMIDITY.   65.00 PERCENT       SPECIFIC HUMIDITY!   .019286  LB.  H20/LB.  DRY AIR
AMBIENT AIR QUALITY    HYDROCARBONS  (HCII  0.0   PPMC      CARBON MONOXIDE (CO)I 0.0   PPMV     OXIDES  OF  NITROGEN (NOX)l  0.0   PPHV
SAMPLE LINE «• TEMP.I  300.00 DEG.  F.     FLOKWTEl    l*.lb LITERS/MIN.     TRANSPORT TIME!    6.50 SEC.      LENGTH!    50.00 FT.
                                                                                                                FUEL INJ TYPEI  STAGED SIMPLEX
TEST CONDITION
ACTUAL FONER SETTING. HORSEPOWER
CORR. POKER SETTING (STD DAY), PERCENT RATED
Nl SPEED, RPH
FUEL FLCM (MEAS.) LB./HR.
CORR. ENGINE CORE AIRF'.OK (MEAS), LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., OEG F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOT*. PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTA. TEMP., OEG F
TURBINE INTERSTAGE GAS TOTAL T£HP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION, KET ANALYSIS
HYDROCARBON IHC AS CH<.I, PPMC
CARBON MONOXIDE (CO), PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPMV
CARBON DIOXIDE (C02) , PERCENT BY VOL.
NITRIC OXIOE (NO), PPM¥
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS IHC AS CN*I
CARBON MONOXIOE (CO)
TOTAL OXIDES OF NITROGEN (HOX AS N02)
EMISSION RATE, L8. POLLUTANT/MR.
HYDROCARBONS (MC »S CM*»
CARBON MONOXIOE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS, CALC)
225 Z26 227
36.5
5.2*
27560.00
117.0
3.0
90.00
1*.10
1.8.01.
310.00
920.0
11.. 06
79.500
228.028
20.300
2.175
l*.*0fl
1..136
20.75*
3.035
.*8*
2.1.28
.355
99.15
.0105
52.1
7.*7
27520.00
127.0
2.9
91.00
1*.10
1.8.53
310.00
980.0
1*.06
66.600
221.365
23.300
2.336
17.900
3.231
18.789
3.2*9
,*10
2.386
.*13
. 99.27
.0113
70.5
10.13
Z7S50.00
136.0
Z.9
89.00
11.. 10
*9.36
310.00
101.6.0
1*.06
1.8.300
195.179
26.900
2.698
21.800
2.036
1*.392
3.258
.277
1.957
.1.1.3
99.1.8
.0129
228
209.9
30.07
1.1750.00
270.0
7.6
92.00
1*.10
130.26
618.00
1127.0
13.97
13.500
63.97*
1.9.200
2.132
37.000
.72*
6.002
7.583
.195
1.6Z1
2.01.7
99.80
.0102
229
*B7.*
69.8*
1.1750.00
369.0
7.7
92.00
14. 10
137.67
622.00
1360.0
13.99
1.200
29.583
72.750
2.918
67.500
.0*7
2.033
8.213
.017
.750
3.031
99.95
.0139
230
636.3
91.25
*17*0.00
1.25.0
7.7
91.00
1*.10
1*1.70
627.00
1*79.0
li.. 03
1.210
19.039
88.250
3.1.19
8*.7SO
.0*0
1.117
8.585
.017
3^615
99.97
.0162
231
70Z.5
100.83
*1770.00
*52.fl 	 ......
7.7
90.00
1*,10 ...... 	
l**.*l
631.00
1529.0 . _ ......
1*.05
.600
17.026
93.000
3.6*1 __. . . ....
91.000
.019 	 	
• .938
8.*19
	 .009 ~ ~
.*2*
3.005
99.90
.0172
-------
(D

to
Ul
o
cur -cr    .,     «•«••»»•••••••••••••»*••  Ep«  CYC^E  EMISSIONS COMPUTATION SUMMARY  •••»»•

NME? So  I      ?««   *   c     TEST F*CIL  ' PHX  LK"   INSTR DESCRIP • FED REG V38 N136
MODEL NO. I      TPE331-5-251M     S/NJ   P04001               ENGINE TYPE(CLASS)t  TURBOPROP
RATED POWER.     706.0  SHP AT SEA LEVEL STANDARD  DAY CONDITIONS     TYPE CYCLE, LB CO/1000 HORSEPOWER-HR PER CYCLE
•• TOTAL OXIDES OF NITROGEN EMISSIONS INOXJ ••
1 INDEX. LB NOX/1000 LB FUEL
SATE, LB NOX/HR
NASS, 16 NOX
1 "ASS, PERCENT OF TOTAL CYCLE
: CYCLE, LB NOX/1000 HORSEPOKER-H9 PER CYCLE

•» EMISSION INDEX LEVELS RE1UIREO
EPA LTO-CYCLE
POLLUTANT LBP/1000 HORSEPOMER-HR-CYCLE
-1 CO 26.9
HC i», 9
NOX 1Z.9
A ASSUMES PROPORTIONAL REDUCTION
UNI
7.000
5.000
35.300
1..118
115.709
13.499

.9

za.ezz
Z.409
.ZBl
23.9

2.989
.346
.040
«.<•

TO M£ET EPA
IOUT)
19.000
5.000
35.300
11.174
115.709
36.641

4.2Z3
.469
.165
67.6

20.622
2.»09
.763
64.9

2.969
.346
.110
22.8

APPROACH
CLIMBOUT
TAKEOFF TOTAL PER
CYCLE
4.500
30.000
211.800
15.885
269.280
20.196

.712
.192
.014
6.3

5.946
1.601
.120
10.2

7.565
2.037
.153
31.8

1979 STANDARDS FOR CLASS
REQUIRED EMISSION
POLLUTANT IHOOEI



OF POLLUTANT



EMISSION
8 ASSUMES 111 REQUIRED REDUCTION IN CO AMD HC OBTAINED
AT TAXI- IDLE MODE ONLY, CO AND HC EMISSIONS AT OTHER
' REDUCTION IN NOX OBTAINED BY LOWERING EMISSION INDEX
SAKE PROPORTION AS MEASURED VALUES, NOX EMISSIONS AT
REMAIN UNCHANGED
CO (IDLE)
HC IIDLEI
NOX (TAKEOFF!
2.500
90.000
635.400
26.475
415.387
17.308

.125
.052
.002
.9

.394
.122
.005
.4

8.379
3.481
.145
38.2

PZ ENGINES »•
.500
110.000
706.000
5.883
456.760
3.806

.199
.091
.001
.3

1.866
.852
.007
.6
- . -
8.565
3.91Z
.033
6.8

.._...
33.509
63.540
91.451

2.504
.411
.229
100.0
3.605

12.863 ~
2.107
1.176
100.0
18.513

5.251
.860
.480
100.0

- - - -
INDEX, LBP/100B LB FUEL

*
20. 8
4.2
8.6

B
31.3
$.9
24.9
	



INDEX AT EACH LTO CrCLE^NOOE
BY LOWERING EMISSION INDEX VALUES
MOOES R£MAIN UNCHANGED, (Zl REQUIRED
VALUES AT CLIMBOUT AND TAKEOFF NODES IN
TAXI-IOLE AND APPROACH HOUES- .. _ 	
                                                                                                                                                                        fO
-------
0>

NJ
Ul















)


)






ENGINE* TPE331-5-2S1M
RAT SHP= 706. RA EGT,F=
FUEL H/C= 1.9280 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Nl. RPM
COMPRESSOR INLET TEHP..DEG.F
COMPRESSOR OSCHG. PRES..PSIA
COMPRESSOR DSCHG. TEMP.DEG F
TURB INTERSTAGE TEMP., OEG.F
CORR 3ELMTH FLOH, LB/SEC
FA RATIO BASED ON BELLMTH.
MEASURED FUEL FLOH, LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING N/P"N/V/E«T/540>
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, MET
LB. PER 1000 LB. Of FUEL
HEIGHT FLOH, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPH BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
S/N* P04001 COMB P/N= 869082-4
1650. RAT SPO= 41730. OEH PT.F* 77.
.06822 L H V* 18470. S LN T,F= 300.0
225
5.2
37.0
36.5
27560.0
90.0
48.0
310.0
920.0
3.00
.0116
117.0
.0105
.15*
.325
99.1*9

2.17
3.11
363.9

228.0
20.754
2.428
226
7.5
52.8
52.1
27520.0
91.0
48.5
310.0
980.0
2.94
.0129
127.0
.0113
.165
.312
99.275

2.34
3.12
395.7

221.4
18.789
2.386
CARBON, HEIGHTS AS
79.5
4.136
.1993
66.6
3.231
.410
.1720
227
10.1
71.5
70.5
27550.0
89.0
49.4
310.0
1046.0
2.92
.0139
136.0
.0129
.190
.302
99.483

2.70
3.13
425.1

195.2
1*.392
1.957
CH4
48.3
2.036
.277
.1414
NITRIC CXIOE «NO) - HEIGHTS AS N02






)


)
)
PPH BY VOLUME, WET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE 
-------
 0)
iQ
 (D

 to
 Ul
 N)
                   TOOEL So i     rreS
                   nuutL NU.I     TPE33
                   RATED POKER!     706
                   FUEL! ASTM 01655-73
                        •*   AIRESEARCH  EMISSION TEST SUMMARY  •••••••••»••»«
                         PHX  LACC2   INSTR OESCRIP I FED REG V38 N136
1-5-351M     S/NI    P04001               ENGINE TYPE (CLASS)I  TURBOPROP
0 SHP AT SEA LEVEL STANDARD  DAY CONDITIONS

           ATOMIC H/C RATIO!    1.928      LHVI  18470. BTU/LB     ADDITIVES!
                                                                                                                     NONE
                                                                                                            °*TE •«
                                                                                                       r«i I-  rn.    «
                                                                                                      TEST NO?   12
         EXHAUST EMISSIONS p£;j EpA  cfCLE OF WORK OUTPUT •» CODE OF FEDERAL REGULATIONS TITLE  40  PART  87   17  JULY  1973
                    HYDROCARBONS  (CH AS  CH4)           5.384 LB. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                    CARBON MONOXIDE (COI             33.046 _B. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                    OXIDES OF NITROGEN  (NOX AS N03)    6.980 L3. POLLUTANT PER 1000 HP.-HR. PER CYCLE
..... „ ,           SMOKE          '                   19.8  SMOKE NUMBER, MAXIMUM AT  CRUISE
TAXI-IDLE SETTING! 5.0      PERCENT RATED TAKEOFF POHER AT 65.       PERCENT RATED TAKEOFF Nl  RPM
                                                                                                                     MODE,   70  PERCENT RATED POHER
COMB TYPE! REVERSE FLOW ANNULAR P/NI 869082-I. SUR/VOLI 1.260 FJEL
ENGINE TOTAL SERVICE! 0.0 HR TIME SINCE ENGINE OVERHAUL! 0.0 HR
. ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
1 AIRCRAFT INSTALLATION •»•• MFR. 1 MODEL NO.I
USER! ENGINE INSTALLATION POSITION!
INJ TYPE!
STAGED SIMPLEX
M»EN? A«S?r2p IESI,M2;'«?2 * 2*TE> "•'•" UMEI BARO P*ESS-« "•••• I"' HGA.
.USJf ,1 .5 TEMPlt 91t0° OEG- f RELATIVE HUMIOITTI 79.00 PERCENT SPECIFIC HUMIDITYI .035000 LB. H20/LB. DRY AIR
AMBIENT AIR QUALITY HYDROCARBONS IHCM 0.0 PPMC CARSON MONOXIDE (COI « 0. 0 PPMV OXIDES OF NITROGEN INOXM 0.0 PPMV
1 SAMPLE LINE »• TEMP.l 300.00 OEG. F. FLOWRATE' 14.16 LITERS/NIN. TRANSPORT TIME! 6.50 SEC. .LENGTH I 50.00 FT?
) TEST CONDITION
ACTUAL POKER SETTING, HORSEPOWER
CORR. POWER SETTING (STD DAY) , PERCENT RATED
) Nl SPEED, RPh
FUEL FLOW IMEAS.) LB./HR.
CORR. ENGINE CORE AIRFLOW (MEAS), LB/SEC
> COMPRESSOR INLET AIR TOTAL TEMP., OEG F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS., PSIA
) COMPRESSOR DISCHARGE AIR TOTA. TEMP., DEG F
TURBINE INTERSTAGE GAS TOTAL TEMP., DEG F
EXHAUST GAS STATIC PRESSURE, PSIA
' EMISSION CONCENTRATION, WET ANALYSIS
HYDROCARBON (HC AS CH4I , PPHC
CARBON MONOXIDE (CO) , PPMV
' TOTAL OXIDES OF NITROGEN (NOXI , PPMV
CARBON DIOXIDE (C02) , PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
1 EMISSION INDEX, LB. POLLUTANT/1000 L3. FUEL
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE ItXI
) TOTAL OXIDES OF NITROGEN INOX AS N02I
EMISSION RATE, LB. POLLUTANT/HR,
HYDROCARBONS (HC AS CH4I
) CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN (NOX AS NO2I
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A {EMISSIONS, CALC)
)
)
232 233 234
34.1 52.1 73.1
4.86 7.45 10.37
37500.00 27530.00 27580.00
117.0 132.0 141.0
3.0 3.0 7.9
90.00
14.19
46.77
300.00
863.0
14.18
136.000
3o4.643
17.600
2.160
13.800

6.573
34.153
3.639

.769
2.826
.309
98.86
.0105


87.00
14.19
49.61
389.00
954.0
14.18
87.000
233.778
20.300
2.386
15.300

4.138
19.405
3.768

.545
2.562
.365
99.18
.0115


90.00
14.19
50.05
294.00
1030.0
14.18
ts.ooo
2 Ob. 782
24.300
2.655
19.000

2.695
15.476
2.987

.380
2.182
.421
99.40
.0128


Z35
204.7
29.13
41770.00
278.0
7. 8
91.00
14.19
132.37
601.00
1110.0
14.08
12.600
70.712
42.400
3.141
31.500

.673
6.603
6.504

.187
1.836
1.808
99.79
.0103


236
487.3
69.42
41740.00
381.0
7.8
90.00
14.19
140.57
603.00
1335.0
14.09
3.300
34.080
62.000
2.939
59.750

.129
2.333
6.971

.049
.889
2.656
99.93
.0139


237
629.4
89.83
41750.00
438.0
7m
• o
88.00
14.19
146.17
600.00
1412.0
14.14
1.500
27.546
75.350
3.364
73.508

.051
1 .642
7.178

.022
.719
3.228
99.96
.0160


238
70".. 3
100.42
41730.00
467.0
7m
• 0
89.00
14.19
148.08
601.00
1520.0
14.15
1.200
17.831
84.750
3.673
79.758

. 037
• ""*• . 	 _ 	
. 974
7.604

.017
.455
3. 551
* ^** -_-..._
99.97
.0174


-------
                                                                                                                                                                   f-
(D
...I..*....**.**............*.......*.*...  EPA CYCLE EMISSIONS  COMPUTATION SUMMARY  •»••••
ENG MFC « AIRESEARCH            TEST FACIL t PHX LACC2  INSTR OESCRIP I  FED REG V38 N136
MODEL NO.I     TPE331-5-251M     S/NI   P04001               ENGINE TYPE«CLASS»I  TURBOPROP
RATED POWERI     706.0  SHP  AT SEA LEVEL STANDARD DAY CONDITIONS
FUEL! ASTM 01655-73             ATOMIC H/C RATIO!   1.928      uHV: 18478. BTU/LB
                                                                                                                            CALC DATE 111-3-75

                                                                                                                                  ?  «*
                                                                                                          .„„„«««•   your
                                                                                                          AODITIVESI   HOME
MODE
TIME IN MODE, MINUTES
RATED POWER, PERCENT
CORRECTED POWER, HORSEPOWER 	
MP-HR
FUEL FLCH, LB/HR
FUEL MASS, LB 	 	
». HYDROCARBON EMISSION IHCI •*
INDEX, LB HC/1000 LB FUEi.
RATE. LB HC/HR
NASS. Lfi HC
NASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORSEPOWER-HR PER CYCLE
»• CARBON MONOXIDE EMISSIONS ICOI _»• . 	
INDEX, LB CO/1888 LB FUEL
RATE. LB CO/HR
MASS. LB CO .
HASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORSEPOWER-HR PER CYCLE
»» TOTAL OXIDES OF NITROGEN EMISSIONS 
-------
0)
NJ
Ul
ENGINE= TPE331-5-251M S/N= P04001 COMB P/N= 869082-4
RAT ShP= 706. RA EGT,F= 1650. RAT SPO= 41730. OEH PT.F* 84
' FUEL H/C= 1.9280 STOI F/A= .06822 L H V= 18470. S LN T^F= SOflio
DATA POINT NUMBER
> PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
1 SHAFT SPEED, Nl, RPM
COMPRESSOR INLET TEMP., DEC. F
COMPRESSOR OSCHG. PRES..PSIA
COMPRESSOR OSCHG. TEMP.OEG F
TURB INTERSTAGE TEMP., DEG.F
CORR 8ELMTH FLOH, L3/SEC
FA RATIO BASED ON 8ELLMTH.
MEASURED FUEL FLOH, L3/HR
i FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/F»*N/V/EIT/540)
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
> LB. C02 PER LB. OF FUE-
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
) PPM 3Y VOLUME, NET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC CXIDE (NO) - HEIGHTS AS
) PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
) NITRCGEK DIOXIDE IN02)
PPM BY VOLUME, NET
LB. PER 1000 LB. OF FUEL
232
4.9
34.3
34.1
Z7500.0
90.0
48.8
300.0
883.0
Z.98
.0116
117.0
.0105
.154
.323
98.855

2.16
3.10
362.5
264.6
24.153
233
7.".
52.
52.
27530.
87.
-.9.
289.
954.
3.01
.0129
132.0
.0115
.169
99ll81

2.39
3.11
410.8
233.8
19.405
2. 826 2.562
CARBON, NEIGHTS AS
126.0
6.573
.769
.2721
N02
12.8
1.919
.225
4.8
.720
i HEIGHT FLON, LB./HR. .084
TOTAL OXIDES OF NITROGEN (NO«N02I AS N02
PPM HY tfni IIMF UPT t -m r
r~n oi vuLuntf NCI '
I L3. PER 1000 LB. OF FUEL
HEIGHT FLOH. LB./HR.
SNOKE MEASUREMENT DATA
.) CORRECTED HEIGHT FLCN
SNCKE NUMBER
CORRECTED HEIGHT FLOH
) SMCKE NUB8ER
CORRECTED HEIGHT FLON
SNOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
SNOKE NUMBER AT HA=0.023
; NOTES 1. ALL EMISSIONS CONCENTR
LI .O
2.639
.309
.00710
.30
. 02130
3.80
.03543
6.10
.04961
7.30
4.40
AT IONS ARF
87.0
4.128
.545
.2127
15.3
2.086
.275
5.0
.682
.090
20.3
2.768
.365
.00710
1.50
.02130
2.70
.03550
5.00
.04979
5.00
3.60
y^r WAI i
234
10.3
72.5
72.1
27580.0
90.0
50.0
294. 0
1030.0
2.93
.0143
141.0
.0128
.187
.306
99.400

2.66
3.12
440.2
206.8
15.476
2.182
CH4
61.0
2.695
.380
.1741
19.0
2.336
.329
5.3
.652
.092
24.3
2.987
.421
.00711
2.70
.02134
2.70
.03557
3.80
.04979
7.30
4.10
KC
235
29.1
205.6
204.7
41770.0
91.0
132.4
601.0
1110.0
7.79
.0106
278.0
.0103
.150
.084
99.786
REDUCED
2.14
3.14
873.4
70.7
6.603
1.836
12.6
.673
.187
.1018
31.5
4.832
1.343
10.9
1.672
.465
42.4
6.504
1.808
.00713
6.10
.02140
14.30
.03567
20.00
.04992
25.80
16.60
Z36
69.4
490.1
487.3
41740.0
90.0
140.6
602.0
1335.0
7.70
.0145
381.0
.0139
.204
.076
99.934
FUEL= AV. KERO. TEST N0.= 12
REL HUM' 79.00 SPEC HUM= .025000
FLO,L/M= i4.ieo SL TIM,S- 6.5000
237
89.8
634.1
629.4
41750.0
88.0
146.2
600.0
1412.0
7. 80
.0166
438.0
.0160
.234
.071
99.957
236
100.4
709.0
704.3
41730.0
89.0
148.1
601.0
1520.0
7.70
.0177
467.0
.0174
.255
.069
99.974

2.93
3.15
1200.2
34.1
2.333
.889
3.3
.129
.049
.0553
59.7
6.718
2.560
2.3
.253
.096
62.0
6.971
2.656
.00713
7.30
.02139
16.60
.0357?
24.71
.05001
30.50
19.80
3. 36
3.15
1380.3
27.5
1.642
.719
1.5
'.051
.022
.0311
72.5
7.100
3.110
2.0
.269
.118
75.2
7.370
3.228
.00714
8.50
.02143
15.40
.03571
23.50
.05000
28.20
10.90
3.67
3.15
1472.2 	
17.8
.974
.455

.037
.017
..0305 . , ._ _ 	
79.7
7.156
3.342

.449
.210
84.7
7.604
3.551. 	 	 	 	 __ .; 	
.00714
6.10
. 02143
13.10
.03571 ..-__._
10.90
.05000
2»-5«
19.51
                       ' • » "fcfc. h. "«..«•»* wn^  wivw^i* • "•»* • A wn« f*r\b P»C I  THLUKd*
                        2.EQUIVALENCE RATIO  CALCULATED FROM C02,CO,ANO HC OATA AND FUEL COMPOSITION.
                        3.MASS EMISSIONS  OF  NO, NOZ, AND NO»N02 CALCULATED AS NOZ FROM CONCENTRATIONS  «TH
                                                                                                              MOLECULAR HEIGHT OF  NOZ  146.011.
-------
                 - y
                                                                                                                              CM.C  DATE H1-3-7S
                                                                                                                              CU.C  IDI   2
                                                                                                                             TEST NOl  12
»»»»»••»»»»»•»»•»••»»»»•»»»•••••»••»»»»•••»•»  AIRESEARCH EMISSION  TEST SUMMARY  •»»»•••«•»•••»
EN6 MFC » AIRESEARCH            TEST FACIL I PHX LACCZ  INSTR OESCRIP  :  FED REG V3» N136
MODEL NO. »     TPE331-S-2S1N     S/N1   PO-.001              ENGINE  TYPEICLASSM  TURBOPROP
RATED FONERI    706.0  SHP AT SEA LEVEL STANDARD DAY CONDITIONS
FUEt« ASTM 01655-73             ATONIC H/C RATIO!   1.928     LriVt  18470. BTU/LB     ADDITIVES!  NONE                   . .  .

........  E)iHAUST EMISSIONS PtS EPA CYCLE OF HORK OUTPUT ••  CODE  OF  FEDERAL REGULATIONS TITLE 40 PART 87  17 JULY  1973   ••••»••
                    HYDROCARBONS (CM AS CH»1          4.8Z2 Lo.  POLLUTANT PER 100« HP.-MR. PER CYCLE
                    CARBON MONOXIDE CCO)             20.879 cB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                    OXIDES OF NITROGEN (NOX AS NOZ)   fc.709 LB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                    SMOKE                             18-1  SMOKE  NUMBER, MAXIMUM AT  CRUISE    MOOEt  711 PERCENT RATED POKE*
TAXI-IDLE SETTINGI 5.0       PERCENT RATcO TAKEOFF POHER AT  65.      PERCENT RATED TAKEOFF Nl RPH
ro
en
                      ».»»».»»»»»»».*.»»»»»».»»»••••»•»»»•»»»»••»*»»»»•»*•   ENGINE DESCRIPTION  ••••••••••»••••••••»••••••••••••»•••••••••••»••»•••»
                      COMB  TYPEI  REVERSE FLON ANNULAR           P/NI   869082-1.            S'JR/VOL* 1.260  FUEL  INJ  TYPEt   STAGED SIMPLEX
                      ENGINE  TOTAL  SERVICE I   0.0       HR    TIME  SINCE  ENGINE OVERHAULI  0.0       MR  ..         ._   	
                      ENGINE  ASSEMBLY AND MAINTENANCE INFORMATION!
                      AIRCRAFT  INSTALLATION  *•»* MFR.»                                  HODEL NO.I
                                                  USER!                        ENGINE INSTALLATION POSITIONI.
                      .,..»...,..,....................................OPERATIONAL TEST DATA SUMMARY • »»»*••»»••»»•»•••••»»«•»»•••»»»»»"»«•»"••»•••
                      CASEOUS EMISSION TEST  NO.I  1Z          DATE! 11-3-75             TINE«                     BAUD PRESS.<  Z8.900 IN. HGA.
                      AMBIENT AIR TEMP.I  91.00 OEG. F        RELATIVE HUMIDITY!   79.00 PERCENT       SPECIFIC  HUMIDITY*   .025000 LB. H2C/LB. DRY AIR
                      AMBIENT AIR QUALITY    HYDROCARBONS  (HCII 0.0    PPMC      CAR3QN MONOXIDE  (CO)I 0.0   PPMV    OXIDES OF NITROGEN INOXM 0.0   PPHV
                      SAMPLE  LINE »•» TEMP.I  300.00 DEC. F.     FLOM^ATEI    1V.16 LlTERS/MIN.     TRANSPO*! TIMEl     6.50 SEC.      LENGTH!   50.00 FT.
TEST CONDITION
ACTUAL POHER SETTING, HORSEPOWER
CORR. POHER SETTING (STD DAY), PERCENT RATED
Nl SPEED, RPM
FUEL FLCM (MEAS.) LB./HR.
CORR. ENGINE CORE AIRFLOH (M£AS>. LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., OEG F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTA^ PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAi. TEMP., OEG F
TURBINE INTERSTAGE GAS TOTAL TEMP., OEC F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION, NET ANALYSIS
HYDROCARBON (HC AS CH4), PPMC
CARBON MONOXIDE (CO) , PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPMV
CARBON DIOXIDE (C02) , PERCENT BY VOL.
NITRIC OXIDE INO), PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH4)
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS HOZ)
EMISSION RATE, LB. POLLUTANT/HR. _
HYDROCARBONS IHC AS CH4I
CARBON MONOXIDE 
-------
                      ..........................................  EPt CYCi-E EMISSIONS COMPUTATION SUMMARY  »»»»»•»•»•
                      ENG  HFG  «  AIRtSEARCH           TEST FACIL « PHX LACC2  INSTR OESCRIP  « FED REG »38 N136
                      MODEL  NO.t      TPE331-S-Z51H     S/NI   P04001              ENGINE  TYPEICLASSII  TURBOPROP
                      RATED  POHER<     706.9 SHP AT SEA LEVEL STANDARD DAY CONDITIONS
                      FUEL!  ASTM 01655-73            ATOMIC H/C RATIO"   1.928     LHVI 18470. BTU/LB     AODITIVESI
                                                                                                      CALC DATE tll-3-75.
                                                                                                      CALC 101   2
                                                                                                     TEST NOI   12
                                                                                                 NONE
(D

to
Ul
                             MODE
                                                     TAXI-IOLE
                                                        (INI
TAXI-IOLE
  (OUTI
                                                                                                      APPROACH
                                                                                                                    CLIHBOUT
                                                                                                                                  TAKEOFF
                                   TOTAL PER
                                    CYCLE
TIME IN MODE. MINUTES
RATED POMER. PERCENT
CORRECTED POMER, HORScPOMER
MP-NR
FUEL FLOV!, LB/HR
FUEL MASS, LB

 •• HYDROCARBON EMISSION (HCI "
INDEX, LB HC/1BOO LB FUEL
RATE. LB HC/HR
MASS, LB HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE. LB HC/1000 HORSEPOMER-HR PER CYCLE

 »• CARBON MONOXIDE EMISSIONS (CO)  "
INDEX, LB CO/1000 LB FUEL
RATE, LB CO/HR
MASS. LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORSEPOHER-HR PER CYCLE

 *• TOTAL OXIDES OF NITROGEN EMISSIONS (NOX)
INDEX, LB NOX/1000 LB FUEL
RATE, LB NOX/HR
MASS. LB NOX
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB NOX/iOOO HORSEPOHER-HR  PER CYCLE
7.010
5.000
35. 300
4.118
117.139
13.606
19.000
5.000
35.300
11.178
117.139
37.091.
4.500
30.000
311.600
15.885
278.611
30.896
2. 500
90.000
635. fcOO
26.1.75
1.38.808
18.28*
.500
100.000
706.000
5.883
470. 4zi
3.9ZD
13.500


63.540

93.060
                                                                               5.839
                                                                                 .68*
                                                                                 .180
                                                                                 26.0
                                                                              2Z.7D9
                                                                                2.660
                                                                                 .311
                                                                                 23.1.
                                                                                2.56Z
                                                                                 .300
                                                                                 .135
                                                                                  6.Z
    5.839
     .684
     .217
     70.7
   ZZ.709
    2.660
     .842
     63.5
    Z.562
     .300
     .095
     Z2.3
 .1.58
 .128
 .010
  3.1
6.752
1.881
 .141
 10.6
6.510
1.816
 .136
 32.0
 .014
 .006
 .000
   .1
1.487
 .652
 .027
  2.0
7.16S
3.144
 .131
 30.7
 .048
 .023
 .001
   .1
1.448
 .6*1
 .006
   .4
7.411
3.486
 .029
  6.8
 3.264
  .549
  .306
 101.*
 4.822
14.114
 2.376
 1.327
 100.0
20.S79
 4.542
  .764
  .426
 100.0
 6.709
                                            *» EMISSION  INDEX LEVELS  REQUIRED  TO  Mitt  EP« 1S79 STANDARDS FOR CLASS P2 ENGINES ••
                                         EPA LTO-CYCLE
                                  POLLUTANT   LBP/1000 HORSEPOMER-HR-CYCLE
                                     CO             26.8
                                     HC              4.9
                                     NOX            12.9
                                                                                                  REQUIfU.0 EMISSION INDEX, LBP/1««« L8 FUEL
                                                                             POLLUTANT (MODE!
                                                                                CO IIDLE I
                                                                                HC HOLE)
                                                                                NOX (TAKEOFF!
                                       A
                                    22.7
                                     5.8
                                     7.4
                                   B
                                30.1
                                . 5.9
                                25.6
                                            A  ASSUMES PROPORTIONAL REDUCTION OF POLLUTANT  EMISSION  INDEX AT  EACH LTD CYCLE MODE .

                                            B  ASSUMES 111 9E3UIREO REDUCTION IN CO »NO MC  OBTAIMID  BY  LOHERIN6  EMISSION INDEX VALUES
                                               AT TAXI-IOLE M03£ ONLY, CO AND HC EMISSIONS  AT OTHER  MOOES REMAIN UNCHANGED, (Zl  REWIRED
                                               REDUCTION IN NOX OBTAINED BT COHERING EMISSION INDEX  VAiUES AT CLIM80UT AMO TAKEOFF  MOOES IN
                                               SANE PROPORTION AS MEASURED VALUES, NOX EMISSIONS AT  TAXI-IDLE AHO APPROACH NODES      	
                                               REMAIN UNCHANGED
                                                                                                                                                                 .  rr
-------
to
en
\ ^

ENGINE* TPE331-5-251M S/N* P04001 COMB P/N= 869082-1,
RAT SHP= 706. RA EGT,F=
1 FUEL H/C= 1.9280 STOI F/A=
DATA POINT NUMBER
1 PERCENT MAX. CORRECTED POWER
CORRECTED SHAFT HP
MEASURED SHAFT HP
) SHAFT SPEED, Nl, RPM
COMPRESSOR INLET TEMP., DEC. F
COMPRESSOR OSCHG. PRES..PSIA
1 COMPRESSOR OSCHG. TEMP, DEC F
TURB INTERSTAGE TEMP., OEG.F
CORR 8ELMTH FLOH, LB/SEC
FA RATIO BASED ON BELLHTH.
MEASURED FUEL FLOW, LB/HR
FA RATIO CALC. FROM EMISSION
' EQUIVALENCE RATIO
LOADING H/P»»N/V/E(T/5*0)
COMB if fit FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
1 LB. C02 PER LB. OF FUEt.
WEIGHT FLOW, LB./HR.
CARBON MONOXIDE
) PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
WEIGHT FLOW, LB./HR.
> UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, WET
LB. PER 1000 LB. OF FUEL
) WEIGHT FLOH, LB./HR.
RATIO LB MC/L9 CO
NITRIC OXIDE (NO) - WEIGHTS AS
FPM BY VOLUME, WET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE (N02I
PPM BY VOLUME, WET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
TOTAL OXIDES OF NITROGEN (NC»N
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
: SMOKE MEASUREMENT DATA
CORRECTED WEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
; CORRECTED HEIGHT FLOH
SMOKE NUMBER
SMOKE NUMBER AT HA=0.023
1650.
.06622
239
5.0
35.2
35.0
275*0.0
90.0
49.2
289.0
87*. 0
3.05
.011*
117.0
.0105
.15*
.332
98.951

2.17
3.10
363.0

2*9.3
22.73*
2.660
RAT SPO= 1,1730.
L H V= 16470.
2*0
7.3
51.9
51.7
27560.0
92.0
*9.7
294.0
956.0
2.98
.0131
132.0
.0116
.169
.316
99.233

2.*0
3.11
411. 0

23*. 3
19.37*
2.557
CARBON, HEIGHTS AS
112.5
5.66*
.686
.2579
N02
12.0
1.797
.210

5.1
.76*
.089
021 AS N02
17.1
2.561
.390

.0071*
3.90
.021*2
5.00
.03570
6.10
.0*996
9.60
6.20
75.0
3.5*5
.468
.1830

15.0
2.038
.269

4.3
.584
.077

19.3
2.622
.3*6

.0071«
2.70
.021*2
5.00
.03570
7.30
.0*998
7.30
5.60
2*1
10.0
70.6
70.3
275*0.0
92.0
50.0
29*. 0
1030.0
2.95
.01*2
1*1.0
.0126
.185
.309
99.400

2.62
3.12
440.2

206.7
15.80*
2.228
CH*
60.0
2.598
.366
.16**

19.1
2.376
.335

3.3
.411
.056

22.*
2.787
.393

.0071*
3.60
.021*2
5.00
.03570
5.00
.0*998
6.10
5.00
DEN PT,F=
S LN T,F=
2*2
30.0
211.5
209.9
41750.0
88.0
133.8
597.0
1116.0
7.61
.0105
276.0
.0105
.15*
.06*
8*.
300.0
2*3
69.7
491.8
486.6
41740.0
69.0
1*1.6
681.0
1331.0
7.80
.01**
381.0
.01*3
.209
.075
FUEL
REL HUM'
FLO,L/M=
2**
89.7
633.5
626.7
41740.
88.
1*6.
601.
1*35.
7.61
.0165
436.0
.816*
.2*0
.071
99.600 99.9*1 99.966
« AV. KERO. TEST N0.= 12
79.00 SPEC HUMs .025808
14.160 SL TIN.S* 6.5008
2*5
100.3
707.9 .
782.6
41780.0
•8.8 ....
1*8.1
603.8
1515.0
7.62
.0177
467.8
.017*
.255
.069
99.969

2.20
3.1*
873.5

74.1
6.738
1.673

9.0
.468
.130
.069*

31.6
*.7S1
1.321

11.6
1.763
.490

43.6
6.513
1.611

.00713
7.30
.021*0
13.10
.03567
17.70
.0*993
29.30
16.90
3.08
3.15
1200.3

34.1
2.276
.867

1.5
.057
.022
.0252

57.5
6.307
2.403

6.8
.7*0
.262

6*. 2
7.0*7
2.665

.08713
9.60
.021*0
15.40
.03567
21.20
.0*993
25.88
18.10
3.45
3.15
137*. 2

23.9
1.389
.606

.6
.028
.009
.81**

70.2
6.708
2.925

4.8
.454
.198

75.0
7.162
3.123

.08713
5.80
.021*0
15. *»
.03567
20.00
.0*993
2*. 70
16. *0
3.67
3.15
1*72,8 	 	 	

22.7
1.238 	 _ 	 	
.578

.6
.019
.889
.0151

79.7
7.1SS


3.8
.269
.126

82.7
7.*2*
. 3.*67 	

.80712
6.18
.82136
13.10
.03567 	 	 	 .
21.28
.0*993
23.58 	 . .._. 	 	
16.10
"' f
^
t
h

3


}


)


}


)

•»
J

)


)


")


)


'j •


y


)


)


) •

n
" y
„
,
. )
,
,
                  NOTES 1. ALL  EMISSIONS CONCENTRATIONS ARE WET VALUES.
                        2.EQUIVALENCE  RATIO CALCULATED FROM C02.CO.ANJ HC DATA AND FUEL

                        3.MASS  EMISSIONS OF NO, N02, AND NO»N02 CALCULATED AS MO2 FROM
 COMPOSITION.

CONCENTRATIONS WITH
                                                                                                             MOLECULAR HEIGHT OF N02 (46.011.
-------
fu
iQ
(D

NJ
U1
00
' )
)
)
)
)
>
)
>
)
)
'
FUEL. ASTM 01655-73 ATONIC H/C RAT
AIRE SEARCH
HX LACC2 IN!
L
<0 DAY CONDI 1
[0. 1.928
EMISSION TEST SUMMAR
riONS
LHV. 18470. BTU/L




V38 N136 CALC DATE 111-3-75
TEST NOt 12
B ADDITIVES. NONE
* 	 "HAUST EMIHSYO°ScARloNr?CH'«ECH0[,1'OR< """"I I™"06 °F FE°ERftL ^"ULATIONS TITLE 40 PART 87 17
CARBON MONOXIDE ICOI ~*' POLUJIANT P£R 10I)(1 HP.-HR. PER CYCLE
SMOKE5 °F NI™OG£N 
-------
                                                                                                                                                                       §
 pj
iQ
 n>
 to
 Ln
                         ....,.,....,...,,..,,.,..*....,,.,....„,.  £ps CrCL£ EMISSIONS COMPUTATION SUMMARY   ••••»••»•«
                         ENG MFG  I  AIRESEARCM            TEST FACIL I PHX LACCZ  INSTR OtSCRIP  I FED REG V38 N136
                         MODEL NO.I      TPE331-5-251M     S/NI   PObOOl              ENGINE TYPE(CLASS)I   TURBOPROP
                         RATED POWER!     706.0  SHP AT SES LEVEL STANDARD DAY CONDITIONS
                         FUEL I ASTM  01655-73             ATONIC H/C RATIO!   1.92*     LHVI 18<,7«.  BTU/LB      AOOITIVESI
                                                                                                                           NONE
                                                                                           CALC DATE <11-3-75
                                                                                           CALC 101   3
                                                                                          TEST NOI   1Z
n'o o E
TIHE IN MODE. MINUTES
RATED PCMER, PERCENT
CORRECTED POWER, HORSEPOWER
HP-HR
FUEL FLON, L8/HR
FUEL HASS, LB
•• HYDROCARBON EMISSION IHCI •*
INDEX, LB HC/1001 L8 FUEL
RATE. LB HC/Hft
NASSi LC HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORSEPOWER-HR PER CYCLE
" CARBON MONOXIDE EMISSIONS ICOI »•
INDEX, LB CO/1101 LB FUEL
RATE, LB CO/HR
MASS, LB CO
HASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORSEPOWER-HR PER CYCLE
•• TOTAL OXIDES OF NITROGEN EMISSIONS CNOXI <
INDEX, L8 NOX/1080 LB FUEL
RATE, LB NOX/HR
NASS, LB NOX
NASS, PERCENT OF TOTAL CYCLE
CYCLE, LB NOX/1000 HORSEPOMER-HR PER CYCLE
TAXI-IOcE
UNI
7.000
5.000
35.300
4.118
117.3'.'.
13.690

6.173
.72*
.885
25. 9


32.888
2.679
.313
23.8

M>
2.1.27
.285
.133
8.0

TAXI-IDLE
(OUTI
19.000
5.000
35.300
11.17*
117. 3M»
37.159

6.173
.721,
.229
70.3


zz.sza
2.679
.81.8
61.. 6


2.«.27
.285
.090
Z1.8

APPROACH
k.500
30.000
211.800
15.885
27<>.583
28.59'.

.<<99
.137
.010
3.2


5.918~
1.625
.122
9.3


6.282
1.725
.129
31.3

CLIMBOUT
2.500
90.008
635.1.00
26.1.75
1,31,. 954
18.123

.099
.01.3
.002
	 .5


1.1.89
.61,8
.027
2.1


7.277
3.165
.132
31.9

TAKEOFF
.500
100.000
706.000
5.883
1.56.755
3.806

.077
.035
.000
. ... . .1 .


.681"
.311
.003
.Z


7.579
3.1.62
.029
7.0

TOTAL PER
CYCLE
33.500


63.5*0

93.372

3.M* _.
.SB*
.326
_ ._._WO.I 	
5.135

" 11.705% ~
2.350
	 1.31Z 	 . _...
100.0
20.652
•
*.*Z9
	 .7**
.41*
101.0
6.508 	
                                               »» EMISSION  INDEX  LEKELS  REQUIRED TO HEET EPA 1979 STANDARDS FOR  CLASS P2 ENGINES'••
                                            EPA LTO-CYCLE
                                                                                                     REQUIRED EMISSION INDEX,  LBP/1000 LB FUEL
                 i.
POLLUTANT
   CO
   HC
   NOX
                                                 L8P/1000  HORStPOMER-HR-CYCLE
                                                        26.8
                                                        12.9
POLLUTANT I MODE)
   CO (IDLE)
   HC HOLE)
   NOX (TAKEOFF)
   A
22.8
 5.9
 7.6
   a
30.5
 5.9
26.7
          A  ASSUMES  PROPORTIONAL REDUCTION OF POLLUTANT EMISSION INDEX AT  EACH  LTO  CYCLE  MODE

          B  ASSUMES  (1)  REQUIRED REDUCTION IN CO AND HC OBTAINED BY LOWERING  EMISSION  INDEX VALUES
             AT TAXI-IDLE MODE ONLY, CO AND HC EMISSIONS AT OTHER MOOES REMAIN UNCHANGED,  121  REQUIRED
             REDUCTION IN NOX OBTAINED BY LOWERING EMISSION INOtX VALUES AT  CLIMBOUT AND TAKEOFF MOOES IN
             SAME  PROPORTION AS MEASURED VALUES, NOX EMISSIONS AT TAXI-IDLE  AND  APPROACH MOOES
             REMAIN UNCHANGED
-------
 (1)
^Q
 
-------
                  OCOOVf ' '
flj
cr>
                         .............................................   AIRESEAPCH EMISSION TEST SUMMARY  •••••••••••••«
                         ENG KFG  t  AIRESEARCH           TEST  FACIL  I  PHX  LACCZ   INSTR OESCRIP I FED REG V38 N13b
                         MODEL  NO.J      TPE331-5-251M     S/NI   PB»301               ENGIN£ TYPE(C-ASS)I  TURBOPROP
                         RATED  PONERI     706.0 SHP AT Sri -EVEL  STANDARD  DAY  CONDITIONS
                         FUEL:  ASTr  C16S5-7J            ATOMIC H/C  RATIO!   1.928     LHV1 181.70. BTU/LB     ADDITIVES!
                                                                                                                            NONE
                                                 CALC DATE 111*7-75
                                                 CALC 101  1
                                                TEST NOI  13
                                   EXHAUST EMISSIONS PE* JPA CYCLE  OF  HOS<  OUTPUT  •* CODE OF FEDERAL REGULATIONS  TITLE  «.«  PART 87  17 JULY 1973
                                              HYCRCCS3BJNS ICH AS CHi»l
                                              CARBON MONOXIDE  (CO)
                                              OXICES OF NITROGEN  (NO*  AS  N02)
                                              SMOKE
                         TAXI-IDLE  SETTING!  5.0
                                                      P-RCENT RATCD TAKEOFF POHcR  AT  65.
 6.",55 ^a. POLLUTANT  PER  1000  HP.-HR. PER CYCLE
19.11,2 LB. POLLUTANT  PtR  1000  HP.-HR. PER CYCLE
 b.837 .3. POLLUTANT  PER  1000  HP.-HR. PER CYCLE
 11.9  SMOKE NUMBER.  MAXIMUM AT  CRUISE    HOOE.
                                                                                               PcRCENT RATED TAKEOFF Nl  FPM
                                                                                                                                   70  PERCENT RATED POKER
                         .».....,..»,.........„.».,...,.,».,.......,,..,».,.,   E(J6INE DESCRIPTION  •»•••»•••»•»•••••••»•»»••••••••»••••»••••
                         COMB TYPE!  REVERSE  FLOW  ANNULAR           P/Nt    8690S2-1.            SUR/VOLl l.ZbO  FUE. INJ  TYPEI   STAGED  SIMPLEX
                         ENGINE TOTAL SERVICE!   0.0        HR    TI1E SINCE EMGINE OVERHAUL!  0.0       HR
                         ENGINE ASSEhBl.>  AND MAINTENANCE INFORMATION I
                         AIRCRAFT  INSTALLATION  »**»  MF^.I                                  MODEL NO.:
                                                     US£RI                       ENGINE INSTALLATION POSITIONI
                         GASEOUS EMISSION  TEST  NO. <   U          DATE: 11-7-75             TIMEI                    8ARC  PRESS. I   33.830 IN.  HGA.
                         AMBIENT AIR TEMP. I   59.00 DtG. F        RELATIVE HUMIDITY I   70.00 PERCENT       SPECIFIC HUMIDITY!   .007500  LB. H30/LB. DRY AIR
                         AMBIENT c:^ QUALITY     HYOROCA330NS (HC)> 0.0   P°NC     CARB3N  MONOXIDE (C0» 0.0   PPMV    CXIOES  OF  NITROGEN INCXI1 0.0   PPMV
                         SAfPLE wINE »•• TECF.l   380.00 OES. F.     FLOMRATEI   1"..16 LITERS/MIN.     TRANSPORT TI«£J     6.50 SEC.      LENGTH!   50.00 FT.
                                                                                        3

                                                                                        3
)


1


1





)


)





,1


)


)
)
)
TEST CONDITION
ACTJAL POWER SETTING, HCRSEPOHER
CORR. POWER SETTING . 63
319.00
933.0
11. £1

210.000
398.916
31.1.00
Z.117
16.300

11.107
28.565
3.253

.911
3.31.1.
.167
48.35
.0101,


1.1.3
7.66
27560.00
89.0
2.7
57.00
11.21
35.61
318.00
995.0
11.20

94. 508
261.651
35.000
Z.376
31.800

<>.!>96
Z1.778
3.1,16

.1,00
1.938
.301,
99.09
.0115


53.3
9.93
27550.00
95.0
3.6
56.00
11. 21
35.61
318.00
1070.0
11.21

60.000
231.378
28.200
3.557
26.100

2.621
17.6t>6
3. 5*1

*2'»9
1.680
.336
S9.35
.0125


158.1
29.35
1,1750.00
211..0
7.7
59.00
11.21
106. 2*
6«3.00
1122.0
11.09

20.700
106.312
54. 100
2.056
36.800

1.11.8
10.509
9.632

.Zi,6
2.2i>9
1.845
99.65
.0099


257
377.3
69.98
1,1750.00
290.0
7.7
60.00
11.21
113.62
656.00
131,6.0
11.10

lt.200
1,0.657
82.500
Z.812
78.000

.171
2.898
9.656

.050
.8hO
2.801
99.92
.0131,


256
<>79.5
88.92
1,1760.00
329.0
7.7
60.00
11.21
115.06
662.00
11,55.0
11.13

2.700
25.513
99.250
3.21,3
97.500

.095
1.576
10.081.

.031
.519
3.317
99.95
.0151,


259
Si.5.9
101.21,
1,171.0.00
353.0
7.6
60.00
'11.21
116.55
666.00
151.3.0
11.11,

2.100
23.079
111.250
3.532
109.000

.068
1.311
10.376

.03",
.1,63
3.663
99.96
.0167


                                                                                                                                                                       3

                                                                                                                                                                       3

                                                                                                                                                                       3
-------
J1J
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0)
to
                         ...».,»....»„»»»..»»..».».»,.»,,,..»„,..   £pA  CYC^E  [MISSIONS COMPUTATION SUMMiivY  •••»»••*••
                         ENG MFC  I  A1RESEARCH           TEST  FACIL  I  PHX  LACC2   1NSTR DESC^IP I FED SEG V33 N136
                         MODEL NO.I      TPE331-5-251M     S/NI   P0«.001               ENGINE TVPE(CLASS)!  TURBOPROP
                         RATED POHERI     706.0 SHP AT SEA LE»£-  STANDARD  DAY  JONDITIONS
                         FUELt ASTM  01655-73            ATOMIC H/C RATI01   1.926      uMVJ 18*70. BTU/LB     ADDITIKESI
                                                                               CALC DATE 111-7-75
                                                                               CALC 101  1
                                                                              TEST NOI  13
MODE
TIM- IN NODE, MINUTES
RATED FOMER, PERCENT
CORRECTED POWER, HORSEPOWER
HP-HR
FUEL FLOW, LB/HR
FUEL MASS, L3
*» HYDROCARBON EMISSION (HC) •«•
INDEX, LB HC/1000 LE FUEu
RATE. LB HC/HP
MASS. LB HC
MASS, PtRCENT OF TOTAL CYC.E
CYCLE, LB HC/1000 HORSEPOHEx-rtP, PER CYCLE
»• CARBON MONOXIDE EMISSIONS (GDI •»
INDEX, LB CO/1000 LB FUEL
RATE, LB CO/HR
MASS. LB CO
MASS, PERCENT OF TOTAu CYC.E
CYCLE, LB CO/1000 HORSEPCKER-HR PER CYC.E
•• TOTAL OXIDES OF NITROGEN EMISSIONS (NOXI ••
INDEX, LB NOX/1000 13 FUEL
RATE, LB NOX/HR
MASS, LB NOX
MASS, PERCENT OF TOTAL CYCLE
CYCLE, Lb NOX/1000 HORSEPOWER-HS PER CYC..E
TAXI-ID. E
UN)
7.000
5.030
35.300
<.. 118
82.125
9.581

10.9*0
.898
.105
25.6


2a.*5o
2.336
.273
22.*


3.258
.268
.031
7.2

TAXI-IflLE
(OUT)
19.000
5.000
35.300
11.178
62.125
26.006

10.9*0
.898
.285
69.*


28.1.50
2.336
.7*0
60.8


3.258
.268
.065
19.5

APPROACH
*.500
33.000
211.800
15.885
219. *72
16.1.60

.858
.186
.01*
3.*


10.5*2
2.31*
.17*
1*.3


a. 77*
1.926
.1**
33.2

CLIHBOUT
2.500
90.000
635.1.00
26.1.75
335.1.5*
13.977

.296
.099
.00*
1.0


1.771
.59*
.025
2.0


10.190
3.1.18
.1*2
32.6

TAKEOFF
.500
100.000
706,000
5.883
361.020
3.008

.836
.302
.003
.6


1.8*5
.666
.006
.5


10.525
3.800
.032
7.3

TOTAL PER
CYCLE
33.500


63.5*0

69.03%

5.9*1
.735
.*10
100.0
6.*55

17.619
2.176
1.216
100.0


6.293
.776
.*3*
100.0
6.637
                                                ••  EHIS3ION INDEX
                                                                         REQUIRED TO MEET  EPA  1979  STANDARDS F3S CLASS F2 ENGINES ••
                                            EPA  LTO-CYCLE
                                                                                                       EQUIRED  EMISSION INDEX, LBP/1000 LB FUEL
                                     POLLUTANT
                                        CO
                                        HC
                                        NOX
L8P/1050 HORSEPOKER-HR-CYCLE
      26.6
                                                        12.9
POLLUTANT (MODE)
CO (IDLE)
HC II3LE1
NOX (TAKEOFF)
A
28. 5
8.3
10. 5
B
*Z.l
6.2
33.8
                                               A  ASSUMES  PROPORTIONAL REDUCTION CF POLLUTANT EMISSION INDEX AT  EACH  LTD CYCLE NODE

                                               B  ASSUMES  11)  REQUIRED REDUCTION IN CO AND HC OBTAINED 8f COHERING  EMISSION INDEX VALUES
                                                  AT T»XI-I3L£ MODE  ON^Y,  CO AND HC EMISSIONS AT OTHER MODES REMAIN UNCHANGED, (21  REQUIRED
                                                  REDUCTION  IN NOX OBTAINED 3Y  .OHERING EMISSION INDEX VA.UES AT CLIM30UT AND TAKEOFF MOOES IN
                                                  SAME ?*OPDPTION AS  MEASURED VALUES,  NOX EMISSIONS AT TAXI-IDLE AND  APPROACH MODES
                                                  REMAIN UNCHANGED
                 OCCOTh
-------
So
iQ
(D

N)
YX1XYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXY
CNSINE* TFE331-5-251M 3/N= P9-.001 COM3 P/N- 869082-* FUEL: AV. HERO. TEST N0.= 13
RAT SHP= 706. RA EGT,F- loSO. RAT S°3= ".1730. DEN PT,F= 51. REt HUM= 70.00 SPEC HUH- .007500
FUEL H/C* 1.9280 STOI F/A= .06822
! DATA POINT NUMBER 253
PERCENT MAX. CORRECTED POHER 5.0
; CORRECTED SHAFT HP 35.0
MEASURED SHAFT HP 26.7
' SHAFT SFEEO, Ml, RPM 275SO.O
COMPRESSOR IN-ET TEMP., DEC. F 59.0
COMPRESSOR OSCHS. PF.ES..FSIA 3*. 6
> COMPRESSOR DSCHG. TE.1P.OEG F 319.0
TUR3 INTERSTAGE TEMP., GEG.F 923.0
1 CO*R 3ELKTH FLOH, LB/SEC 2. SO
FA RATIO BASED ON BtLLMTH. .010?
MEASURED FUEL FLOH, LB/HR 82.0
FA 4ATIO CAuC. FROM EMISSION .010*
EQUIVALENCE RATIO .152
LOWING H/P*«N/V/E .*3*
COM3 EFFIC FROM EMISSIONS 93.353
CARBON DIOXIDE
PERCENT BY VOLUME, HET 2.12
> LB. C02 FER LB. OF FUEL 1. OS
i HEIGHT FLOH, LB./HR. 252.*
CARBON MONOXIDE
I PPM 3t VOLUME, KET 308.9
LB. PER 1000 LB. OF FUE- 25.5S3
HEIGHT FLOH, LB./HR. 2.3**
UNBURNEO HYDROCARBONS- PFM AS CARBON, HEI
PPC BY VOLUME, HET 210.0
L3. PER 1000 LB. OF FUEL 11.107
HEIGHT FLOH, LB./HR. .911
RATIO LB hC/LB CO .3886
NITRIC OXIDE (NO) - HEIGHTS AS N02
i I PPM BY VOLUME, HET 16.3
Lfl. PER 1000 LB. OF FUEL 2.551.
HEIGHT FLOH, LB./HR. .Z09
> NITROGEN DIOXIDE 
PPK 8Y VOLUME, HET *.6
L3. PER 1000 -B. OF FUEL .699
> HEIGHT FLOH, LB./HR. .057
TOTAL OXIDES OF NITROGEN (NC»W021 AS N02
PPM BY VOLUME, HET 21.*
LJ. PER 1000 LB. OF FJE- 3.253
HEIGHT FLOH, LB./HR. .267
SMOKE MEASUREMENT DATA
; CORRECTED HEIGHT FLCH .00716
S.10KE NUMBER *.1B
CORRECTED HEIGHT FLCH .021*7
) SMOKE NUMBER 7.10
CORRECTED HEIGHT FLOH .03577
SUCKS NUMBER 7. 10
CORRECTED HEIGHT FLCH .0*999
SMOKE NUHBES 9.«0
SMOKE NUMBER AT HAcO.323 6.90
NOTrS 1. ALL EMISSIONS CONCENTRATIONS ARE
2. EQUIVALENCE RATIO CA.CU.ATEO FROM
3. MASS EMISSIONS CF SO, N02, AND -iO
L H V =
25*
7.7
5H.1
<*1.2
27503. J
57.0
35.6
315.0
995.5
2.o7
.0121
d9.0
.S115
.loS
.596
99.533

2.38
3.11
276.6

2=1.7
Z1.T7S
l.?36
SHTS AS
9—5
V.-96
..00
.206*

21.9
Z.533
.265

3.2
.L»6
.033

25.0
3.LH
.30-.

.OD'l*
3.50
.321.2
3.50
.03571
6.;a
.3*999
4.20
5.50
HET V1L
C02.C3,
»NC2 CAL
ie»7o.
255
9.9
70.1
53.3
£7i50. 0
56.0
35.6
jia.o
1070.0
2.6*
.0130
95.0
.0125
.183
.392
93.35*
*SJMMARY OF
2.60
3.12
296.3

231.*
17.686
1.680
CH*»
bO.O
2.621
.2*9
.1*82

26.1
3.277
.311

2.1
.26*
.025

28.2
3.5*1
.336

.0071*
3.50
.021*2
2.1.0
.03571
3.50
.0*999
8.20
*.*0
UcS.
1NO HC DATA
CJ.ATEO AS
a LN T,F=
256
29.3
207.2
158.1
*1?50.0
59.0
106.2
6*3.0
1122.0
7.69
.0101
21-. 0
.0099
.1*5
.092
99.oS2
RECUCEJ
2.06
3.13
670. a

103.3
10.509
.. 2.2»9

20.7
1.1*3
.2*6
.1092

3b.8
5.965
1.255

17.3
2.757
.590

5*.l
£.622
. 1.8*5

.00703
2.*0
.02109
7.10
.03515
9.20
.0*921
11.20
7.30

AND FUEL
402 FROM
300.0 FLO.L/M
257
70.0
*9*.0
377.3
i}750.0 *
60.0
112. b
656.0
13*6.0
7.68
.0138
290.0
.013*
.196
.081
99.917
EMISSION OATA
2.81
3.15
913.2

*0.7
2.896
.8*0

*.2
.171
.050
.0590

76.0
9.132
2.6*8

*.5
.527
.153

82.5
9.658
2.801

.0070*
•..70
.02113
9.*0
.03521
1*.10
.0*930
18.80
11.90

COMPOSITION.
258
88.
627.
*79.
1760.
60.
115.
662.
1*55.
7.66
.0156
329.0
.015*
.226
.077
99.955

3.2*
3.15
1036.8

25.5
1.578
.519

2.7
.095
.031
.0605

97.5
9.906
3.259

1.8
.178
.058

99.2
10.08*
3.317

.1)0703
*.7fl
.02110
9.*0
.03517
1*.10
.0*92*
17.60
11.60


CONCENTRATIONS HITH
= 1-..160 SL TIM,S= 6.5000
259
101.2
71*. 8
5*5.9
1,17*0.0
60.0
116.6
666.0
15*2.0
7.63
.0169
353.0
.0167
.2*5
.07*
99.963

3.53
3.15
1112.6

23.1
1.311
.*63

2.1
.068
.02*
.0520

109.0
10.168
3.589

2.3
.210
.07*

111.2
10.378
3.663

.00703
*.70
.02110
7. IB
.03517
1*.10
.0*92*
16.50
10.70


MOLECULAR HEIGHT OF N02 U6.01I.
-------
                                                                                                                           CALC DATE 111-7-75
                                                                                                                           CALC 101  2
                                                                                                                          TEST NOI  IS
                                                                                                         AOOITIVES:   NOME
.•».»•»».»».»»»»»»..»....».»...»».».•»».•»»»«   AIRtSEAKCH EMISSION TEST SUMMARY  ..»»...•»
ENG MFG : AIRES'ARCH            TEST FAClL  I  PHX  LACC2  INSTR OESCRIP : FED REG ¥38 N136
MODEL Nil.:      TPE331-5-251M     S/N:   POkOOl               ENGINE TYPE(C.ASS):  TURBOPROP
RATED POWER:     706.0 SHP AT SEA _£VEL STANDARD  DAY  CONDITIONS
FUEL: ASTM 01655-73             ATOMIC H/C  RATIO:    1.-J28     uHV« 181.70. BTU/LB

........ EXHAUST EMISSIONS PE-< EPA CYCLE OF  WORK OUTPUT »* CODE OF FEOERA-. REGULATIONS TIT^E *0 PART 87  17 JULY 1973  »••••••
                     HYDROCARBONS (CH SS CH*)           6.21.1 ,.6. POL-UTANT PtS 1000 HP.-HR.  PER CYCLE
                     CARBON MONOXIDE (COI              18.313 LB. POLLUTANT PER 1000 HP.-HR.  PER CYCLE
                     OXIDES OF NITROGEN (NOX  AS  NOZ)    6.509 LB. POLLUTANT PfcR 1000 HP.-HR.  PER CYCLE      _._„.„. _.....  ona.a
                     SMOKE                              13.<  SMOKE NUMBER, MAXIMUM AT  CRUISE    MODE,  70 PERCENT RATED  POWER
TAXI-IDLE SETTING:  5.0      PERCENT RATED  TAKEOFF POWER AT 65.      PERCENT RATED TAKEOFF NI RPM
                                                                                                          FJEL  INJ TYFE»  STAGED SIMPLEX
CD
to
CTi
....I,.....,,..,..,...............*...*.**...*..**"  ENGINE DESCRIPTION  ••»»•»»•«
COMB  TYPE:  REVERSE FLOW ANNULAR            F/NJ    869082-1.           SUR/VOL: 1.260
ENGINE  TOTAL SLRVICt.1  0.0       MR     TIME  SINCE ENGINE OVERHAUL:  0.0        HR
ENGINE  ASSEMBLY AND MAINTENANCE INFORMATION:
AIRCkAFT  INSTALLATION »»»• MFR.:                                  MODEL NO.:
                            USERI                        EN5INE INSTALLATION POSITION:
..................................•..•."..•..•»OPc^AT10N4. TEST DATA SUMMARY  •»•»»*»*••*»«••»•»•»•»••••»•»•••••»*••»•••••••••
r««eon< ?*T^CTnu Tr^T up t  1J           DATE:  11-7-75            TIME:                     BARO PRESS.:  22.830  IN.  HGA.
"S"« 5« ?EH?.I  H"OO DE" F         RELATIVE HUMIDITY,  70.00 PERCENT        SPECIFIC HUHIOITY,  .007500 L6.  H20/LB.  DRY AIR
AMBIENT A'R QUALITY    HYDROCARBONS  (HC):  0.0    PPMC     CARSON MONOXIDE  (CO)1  0.0    PPMV    OXIDES OF NITROGEN (NOX):  0.0    PPMV
SAMPLE  LINE ••• TEMP.:  300.00 OEG.  F.      FLOWRATEI   1*.16 LITERS/MIN.      TRANSPORT TIME*    6.50 SEC.
                                                                                                                                     LENGTHI    50.00 FT.
TEST CONDITION
ACTUAL POWER SETTING, HORSEPOWER
CORX. POWER SETTING (STO DAY), PERCENT RATED
Nl liP£EO, RFM
FJEL FLOW (MEAS.) LB./HR.
CORR. ENGINE COKE AIRFLOW (MEASI, LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., OEG F
COMPRESSOR INLET AIR TOTAL PRiSS. , PSIA
COMPRESSOR DISCHARGE AIR TOTA;. PRESS., »SIA
COMPRESSOR DISCHARGE AIR TOTA. TEMP., DEG F
TURBINE INTERSTAGE GAS TOTA,. TEHF., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION, WET ANA.YSIS
HYOR3CAR30N (HC AS CM*), PPMC
CARSON MONOXIDE (CO, PrMV
TOTAL OXIDES OF NITROGEN (NOX), PPMV
CARBON OIOXIDE (C02), PERCENT BY VOL.
NITRIC OXIDE INO) , PPMV
EMISSION INDEX, L8. POLLUTANT/1000 L3. FUEL
HYDROCARBONS (HC AS CHI.)
CARBON MONOXIDE ICO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
EMISSION RATE, LB. POLLUTANT/MR.
HYDROCARBONS «HC *S CH*)
CARBON M3NOXIOE (CO)
TCTA' OXIDES OF NITROGEN (NOX AS N02)
COMBUSTION EFFICIENCY. PERCENT (EMISSIONS)
F/A ^MISSIONS, CALC)
260 261 262
26.7 111. 7 53.9
t.97 7.76 10.05
27570.00 2751.0.00 27590.00
82.0
2.8
55.03
11.21
35.12
317.00
913.0
11.21
198.000
29*. 719
20.600
2.108
17.000
10.531
27.W25
3.179
.864
2.2*9
.261
*8.<*3
.0103
90.0
2.6
55.00
11.21
35.51
316.00
996.0
11.21
93.000
269.152
2>>.900
2.366
22.200
<«.<<<<2
22. 
-------
                  OCUOVf
to
01
en
                         ....,...„...,.„„...,......,».».•»•..••••»•   EPJ CYC-i EMISSIONS COMPUTATION  SUMMARY  •»•»••»»»«
                         ENG MFC  «  AIRESEARCH           TEST  FACIc  «  DMX LACC2  1NSTR JESCRIP  J FED FEG  V38 N136
                         MODEL NO. I      TPE331-5-251M     S/Nt    PJi.001               ENI.INE TYPE (CtASSJ I   TURBOPROP
                         RATtO PCHERI     706.3  SHP AT SEA LEVE.  STANOARD DAY  CONDITIONS
                         FUE..I ASTM  D1655-73            ATOMIC H/C  RATIOI   1.928     LHVI 18".70. BTU/..B      ADDITIVES!
                                                                                            C»LC DATE  Jll-7-75
                                                                                            CALC 101   Z
                                                                                           TEST NOI  13
                                                                                       NONE
K 0 0 E
TIME IN MUOEt MINUTES
RATED POWER, PERCENT
CORRECTED POHER. HORSiPOHER
HP- MR
FUEL FLOM, LB/MR
FUEL »»SS, LB
•• H/CROCARSON EHISSION CHCJ »*
INDEX, LB HC71006 LB FUEL
RATE, LB HC/HR
MASS, LB HC
MASS, PERCENT OF TOTAL CYCLE
CYC.i, LB MC/1000 MORS£POH£*-Hi? Ptl CYCLE
*» CARSON MONOXIDE EMISSIONS ICOI »•
INDEX, LB CO/1000 LB FUEi.
RATE. LB CO/HR
MASS, LB CO
HASS, PtRCENT OF TOT A. CYCLE
CYCLE, L3 CO/1008 HORSEPOHER-HR PER CYC^E
•• TOTAL OXIDES OF NITROGEN £1ISSIONS CNOX) »»
INDEX, L3 NOX/1000 LB FUEL
RATE, LB NOX/HR
MASS, LB NOX
MASS, PERCENT OF TOTAL CYCLE
CYCLE, L3 NOX/iOaO HOP.SEPOMER-H* PER CYCLE
TAXI-ID. E
(INI
7.000
5.000
3S.300
«.118
8Z.OS9
9.577

10.1.37
.857
.100
Z5.Z


Z7.38S
2.21.8
.262
23.5


3.182
.261
.030
7.»

TAXI-IO^E
(OUT)
19.000
5.000
35.300
11.178
82.089
25. 995

ID. 437
.857
.271
68. <»


27.385
2.21.8
.712
61.2


3.182
.261
.083
20.0

APPROACH
"..500
30.000
211.800
15. 885
209. Z55
15.09".

1.1.89
.312
.023
5.9


9.939
2.080
.156
13. <.


S.tOl
1.758
.132
31.9

CLIM30UT
2.500
90.000
635. "tOO
26.<.75
331.030
13.793

.129
.01.3
.002
.".


2.07".
.687
.029
2.5


10.0".7
3.326
.139
33.5

TAKEOFF
.500
100.000
706.000
5.883
353.029
2.9".2

.058
.020
.000
.0


1.663
.587
.005
.">


10.182
3.59
-------
tl
en
ENGINE= TPE331-5-251M S/N= P0.001 COMB P/N= 869082-4 FUEL= AV. KERO. TEST NO.* 13
RAT SHP= 706. «A £GT,F* liSO.
FUEL H/C= 1.9280 STOI F/A = .06822
DATA POINT NUMBER 250
PERCENT MAX. CORRECTED POHER s.o
CORRECTED SHAFT HP 35.1
MEASURED SHAFT HP 26.7
SHAFT SPEED, Nl, RPM 27570. C
COMPRESSOR IX. ET TEMP..OEG.F 55.0
COMPRESSOR OSCHG. PRES. ,PSIA 35.1
COMPRESSOR DSCHS. TEMP.OEG F 317.0
TUR3 INTERSTAGE TEMP., CEG.F 913.3
CORR BELMTH FLOH, LB/SEC 2.81
FA RATIO BAStO ON EELLMTH. .0106
MEASURED FUEL FLOW, LB/HR 82.0
FA RATIO CALC. FROM EMISSION .01C2
EQUIVALENCE RATIO .151
LOADING H/(-»»N/V/E
-------
               uouo nr
•)    ,,.»...,..,,,,,..,.,.,,...,....,»,»,,,,,.,,,.  AISESEARCh EMISSION  TEST  SUMMARY  •»•••••••»•••«
     ENG MFC I AIRESEARCM            IEST FACIL I ' PrlX LACt2  INSTR OESCRIP  I FED  REG V38 N136
     MODE- NO.t     TPE331-5-c51M      S/NI   PD-031              ENGINE  TYFt(CLASS)1  TUR3SPROF
 1    RATED POWER!    706.G SHP AT  SEA  LEVE- STiNOA=>0 DAY CONDITIONS
     FUEi.» ASTM O1655-73             ATOMIC H/C RSTIOI    1.326     I.HVI 181.70.  6TU/LB     AODITIVESI
                                                                                                                         NONE
                                                                                                                              CALC DATE 111-6-75
                                                                                                                              CALC 101  3
                                                                                                                             TEST NOI  13
                               EXHAUST  EMISSIONS  PL-? iPA CYCLt. OF XORK OUTPJT  "  CODE  OF FEDERAL REGULATIONS  TITLE  <-0  PART  87  17 JULY 1973
                                  (CH SS CHn)
                    CiS33N  MONOXIDE ICO)
                    OnICiS  OF  NITROGEN 37 .3. POLLUTANT  PER 1000 HP.-HR. PER CYCLE
                                                            6.6.5 -3. POLLUTANT  PER 1000 HP.-HR. PER CYCLE
                                                            1-..5  3HOKE NUMBER.  MAXIMUM AT  CRUISE    MODE,
                                                          H£.K AT 63.      PERCENT  RATED TAKEOFF NI RPC
                                                                                                                                70  PERCENT RATED POWER
n>
NJ
CTi
COMB TYPE! -.EYERSE F.OW INNULAR P/NI 85SOB2-4 SUR/VOLI 1.260 FJEL
ENGiHE TOTA. SERVICE1 0.0 HR TIM= SINCE ENGINE OVtWAUul 0.0 HR
ENGINE ASSEMBLY AND M4IN7ENANCE INFOR1ATIONI
AIRCRAFT INSTALLATION »»•» MF3. t MODEL NO. 1
USrSt iNGINi INSTALLATION FOSITIONI
GASECUS EMISSION TEST NO. » 13 3ATEI 1
AMBIENT AH TE1P.S 6B.OO 3£G. F Ri.ATIV
AMBIENT AIR QUALITY Hra^OC-BSONS (nC) s 0.0
* Jrt-
-------
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to
.001              ENGINE TrPE(CLASS)!  TURBOPROP
                     RATED POHERI    706.0 SHP AT iEA  ..EVEL  STANDARD DAY CONDITIONS
                     FJE..1 ASTM 01655-73             ATOMIC H/C  RATIO!    1.928     LHVI 18".7fl. BTU/LB     AOOITIVESI
                                                                                                                       NONE
 CALC DATE 111-8-75
 CALC IDI  3
TEST N0<  13
MODE
TIME IN MODE, MINUTES
RATED PCMER, PERCENT
CORRECTED POHER, HORSEPOHER
HP-HR
FUEL FLCH, LB/HR
FUE. MASS, LB
*• HYDROCARBON EMISSIOK (HC) »»
INDEX, LB HC/1000 LB FUEL
RATE. LB HC/HR
MASS, LB HC
MASS, PERCENT OF TOTAL CYCLE
CYC.E. LB HC/1000 HORSEPOKSR-rtR PER CYCLE
*• CARBON MONOXIDE EMISSIONS (CO) ••
INDEX, LB CO/1800 LB FUEL
RATE, LB CO/HR
MASS, LB CO
MASS. PERCENT OF TOTAL CYCt_E
CYC.E. LB CO/1000 HORSEPOHER-HR P£R CYCLE
•• TOTAL OXIDES OF NITROGEN EMISSIONS (NOX) ••
INDEX, LB NOX/1000 LB FUEL
RATE, LB NOX/HR
MASS, LB NOX
MASS, PERCENT OF TOTAL CYCLE
CYC.E, LB NOX/1000 HORSEPOMER-HR ?£R CYCLE
TAXI-IDLE
(IN)
7.000
5.000
35.300
*».118
82.082
9.576

10.617
.872
.102
25.7


29.1.13
2.«li»
.Z8Z
22. B


'3.1.1',
.280
.033
7.7

TAXI-IDLE
(OUT)
19.000
5.000
35.300
11.178
32.082
25.993

10.617
.872
.276
69.6


29.U13
2.1.11.
.765
61.3


3.1.11.
.280
.089
21.0

APPROACH
t.500
30.000
211. SOO
15.885
209.822 '
15.737

1.161
.21.1,
.018
I..6


11.177
2.31.5
.176
1U.1


8.601
1.805
.135
32.1

CLIMBOUT
3.500
yn.ooo
635.1.00
26.1.75
330.291.
U.762

.011
.00
-------
               Cicuot*
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ENGINE- TPE331-5-251M S/N= POwflOl COM6 P/N= 869082-4
RAT SHP= 706. RA EGT.Fs
FUEL H/C= 1.9260 STOI F/As
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHSR
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Nl, RPM
COMPRESSOR INLET TEHP.,O£G.F
COMPRESSOR OSCHG. PRES. ,PSIA
COMPRESSOR OSCHG. T£MP,D£G F
TUfcB INTERSTAGE TEMP., OLG.F
CORR 3ELMTH FLOM, LB/SEC
FA RATIO BASED ON BELLMTH.
MEASURED FUEL FLOW, LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/?»«N/V/EIT/540I
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
LB. C02 PER LB. OF FUEL
HEIGHT FLOM, uB./HR.
CARBON MONOXIDE
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM. LB./HR.
UN6URNEO HYDROCAR30KS- FPM AS
PPH Bf VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIOE INO) - HEIGHTS AS
PPM BY VOLUME, MET
L3. PER 1300 LB. OF FU£L
HEIGHT FLOM, LB./HR.
NITROGEN DIOXIDE (NOZI
PPM BY VOLUME, MET
L3. PC.* 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
1650.
.06822
267
5.0
35.1
26.7
27570.0
55.0
35.5
315.0
915.0
2.63
.0113
82.0
.0102
.150
;395
93.362

2.09
3.08
252.4

315.9
29.553
2.423
RAT SPD
L H V
268
7.6
53.8
1.1.0
27560.0
57.0
35.t
317.0
993.0
2.68
.0120
89.0
.0115
.168
.403
99.162

2.38
3.11
276. «

255.2
21.259
1.89Z
CARBON, HEIGHTS AS
201.0
10.749
.881
.3637
NOZ
17.9
2.751
.226

4.3
.661
.054
81.0
3.857
.343
.1814

22.3
5.051
.272

3.7
.506
.045
- 41730.
= 18470.
269
10.0
70.5
s3.8
27540.0
59.0
35.4
321.0
1073.0
2.64
.0132
96.8
.0126
.185
.393
99.369

2.62
3.12
299.4

237. Z
17.961
1.726
CH4
57.0
2.470
.237
.1374

27.5
3.425
.329

2.5
.311
.030
OEM PT.Fi
S ..N T.Fs
270
30.2
213.0
162.8
41730.0
60.0
106.3
650.0
1075.0
7.70
.8100
211.0
.0100
.146
.091
99.648
RdOUCEJ
2.07
3.13
661.2

115.2
11.078
2.337

18.9
1.038
.219
.0937

36.6
5.779
1.219

18.1
2.658
.603
TOTAL OXIDES OF NITROGEN «NO+N02I AS N02
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOM
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOM
SHOKE NUM3ER
CORRECTED HEISHT FLOM
SMOKE NUMBER
SMOKE NLIM3ER AT WA=0.023
22. 2
3.412
.280

.00706
3.50
.02119
4.70
.03531
8.20
.04944
9.40
6.50
•OAT rntic A o
26.0
3.558
.317

.00705
2.40
.02115
4.70
.03525
5.90
5.90
4.70
~ US T tl A
30.0
3.736
.359

.00704
1.20
.02111
4.70
.03518
4.70
.01.925
6.50
4.30
1 IICC -
Sfc. 7
6.637
1.822

.00711
4.70
.0213»
5.90
.03556
11.20
.04979
14.10
9.00
51.
300.0
271
69.8
493.0
376.9
41730.0
60.0
112.0
056.0
1335.0
7.62
.0137
286.0
.0136
.199
.091
FUEL
SEL HUN=
Fi_0,l/M=
27Z
• 9.8
634.2
*64.8
41740.0
68.8
115.4
663.8
1465.0
7.63
.8157
329.5
.8155
.ZZ7
.076
99.916 99.956
= AV. KERO. TEST N0.= 13
70.00 SPEC HUM* .007508
14.168 SL UM,S= 6.5888
273
100.1
787.8
540.5
41/38.8
60. »
116.7
666.8
1523.8
7.63
.0167
350.8
.8166
.244
.074
99.968

2.86
3.15
900.6

44.4
3.113
.890

3.0
.120
.034
.8386

74.0
8.529
2.439

7.5
.864
.247

81.5
9.393
Z.666

.00711
6.20
.02134
11.60
.03556
16.50
.04979
21.20
14.50
3.27
3.15
1036.4

Z6.3
1.616
.533

Z.I
.074
.024
.0456

94.2
9.505
3.132

3.3
.326
.186

97.5
9.633
3.248

.88718
8.20
.82138
11.60
.83558
17.18
.84969
28.80
14.38
3.51
3.15
1183.1

25.5
1.459
.511

Z.I
.069
.024
.0478

186.3
9.96Z
3.494

2.5
.235
.082

188.7
18.217
3.576

.08789
4.78
.02126
18.88
.83543
14.18
.04968
17.68
11.78
                     NOTtS 1. ALL EMISSIONS  CONCENTRATIONS AR£ MET VALUES.
                           2.EQUIVALENCE  RATIO CALCUtaTED FROM C02.CO.ANO HC  DATA
                           3.MASS EMISSIONS  OF NO, N02, ANC NO»N02 CALCULATED AS
 AND FUEL COMPOSITION.
N02 FROM COKCtNTftATIONS WITH
                             MOLECULAR HEIGHT OF N02  146.811.
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 13
 ft>
ifl
 (D
                         ....».»..,....,.»»»,„..,,„»,.,,...,.„»»„.»..   AIRESEARCH  EMISSION TEST  SUMMARY   •••»•••••»»•»«

                         ENG MFC  I  AIRESEAOCH           TEST FACIi. 1 PH» .ACC2   IN3TR  OESCRIP  I FED  REG  V38  N136

                         HOOEL  NO.I      TPE331-5-251K     S/Nt   P3»001              ENGINE TYPEtCLASSM   TURBOPROP
                         RATED  POHERi     706.0 SHP AT SEA LEVEL STANDARD DAY CONOITIOMS

                         FUELI  AST1  Dlb55-73            ATOMII H/C RATIOS   1.928      LHVI  18470.  6TU/LB      ADDITIVES:
                                                                                                      CALC  DATE  111-6-75

                                                                                                      CALC  101   1
                                                                                                      TEST NOI   14
                                                                                                                           NONE
                         ********  EXHAUST EMISSIONS P£* EPA CYCLE OF WORK. 3UTPUT »•  C30E  OF  FcDEFA.  REGULATIONS  TITLE -0 PART 87  17 JULY 1973  •»•••••
                                              HYOR.CAR6.TJS (CH AS Cl»)          3.114 .6.  POLLUTANT PER  1000  MP.-HR.  PER CYCLE
                                              CARBON HOM3XIOE (CO)             15.491 LB.  POnUTAKT PER  1000  HP.-HR.  PER CYCLE
                                              OXIDES OF NITROGEN  (NOX AS N02)   S.038 .8.  POL.UTANT PER  1000  hP.-HR.  PER CYCLE
                                              SMOKE                             17.9   SMOKE NJMtEK, MAXIMUM AT  CRUISE    MODE,  70 PERCENT RATED POWER
                         TAXI-IDLE SETTING:  5.0       P.RCENT RATED TAKEOFF POWER AT  65.      PERCENT  RATED TAKEOFF NI RPM
....».»»..,.,»........»,,,».......,.»»»,.,,,..,,,,..  LNGINt DESCRIPTION  ••»»••••••••»•»•»»•••»»••

COM3 TYPEI REVERSE FLOW  ANNULAR            P/N:    869082-4           SUR/VOL! 1.260  FUEL INJ  TYFEI

ENGINE TOTAL SERVICEl  0.0        HR     TIME  SINCE EHSlhc. OVERHAUL"  0.0       HR
ENGINE ASSEMBLY AND MAINTENANCE  INFORMATION:

AIRCRAFT INSTALLATION »*»* MFR. «                                  MODEL NO. I

                           JS£RI                        ENGINE INSTA.LATION POSITIONI
                                                                                                                               STAGED SIMPLEX
                         GASEOUS  EMISSION TEST  NO.:   !••          01Tt« 11-6-75             TIME:         •            6«RC PRESS. 1   25.960 IN. hGA.
                         AMBItNT  AIR  TEMP. I   59.00  DiG. F        <£LiTII/E HUMIOITY:  70.00 PERCENT        SPECIFIC  HUMIDITY:  .007500 LB. H20/LB. DRY AIR

                         AMBIENT  AIR  DUALITY     "YOR3CAR30NS IHC)« 0.0   PPMC     CARBON MONOXIOc  (C0)l 0.0    PPMV    OXIOES OF  NITROGEN (NOX)I 0.0   PPMV

                         SAMPLE LINE  *•»  TEMF.l   300. OJ OEG. F.     FuiW.RATEl   14.16 LITE*S/MIN.      TRANSPORT  TIME:     6.50 SEC.      LENGTH!   50.00 FT.
TEST CONDITION
ACTUA. POKER SETTING, HORSEPOWER
COS*. POME* SETTING ISTC OJY), "ESCENT RATED
Nl SPEED, RPN
FUEv FLOW (MEAS.I L6./HF.
COR*. ENGINE CORE AIRFLOW (MEASI , ,.6/SEC
COMPRESSOR INLET AIR TOTAL TEMP., OEG f
COMPRESSOR INLET «IR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAk PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL TEMP., 0£S F
TUR3INE INTLRSTAGE GAS TOTA.. TEMP., OEG F
EXHAUST GAS STATIC PRESSURE . PSIt
EMISSION CONCENTRATION, MET ANALYSIS
HYDROCARBON (HC AS CHI.), PPMC
CAR30N MONOXIDE (CO), PPMV
TOTAL CXIOCS CF NITROGEN (N3X) , PPMV
CARBON OIOXICE (C02), °ERC£NT BY VOL.
NITRIC OXIOE (NO), PPMV
EMISSION INDEX, LE. POLLUTANT/1003 L3. FUEL
HYOROCAPBONS IHC AS CH4I
CAR83N MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN INOX AS N02)
EMISSION RATE, L3. POLLUTANT/HR.
HYDROCARBONS (HC 'AS Cri4)
CARBON MiN OXIOE ICO)
TOTAL OXIOES OF NITROGEN (NOX AS N02)
COM3U3TION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS, CALC)
27", 275 276
31.6
5.15
27510.00
96.0
2. 9
60. DO
12.76
.3.71
326.00
91^.0
12.75

78.900
206.782
i3.50fl
3.106
14.61)0

4.237
U.-.28
3.627

.1,07
1.865
.346
99.17
.0102
-.5.7
7.45
27580. 00
105.0
2.9
60.00
12.76
".4.06
322.00
"36, .0
12.75

5*. 630
164.655
Z6.900
2.267
23.200

2.731,
16.614
3.871

.287
1.7-.4
.406
99.37
.8109
62.0
10.11
37530.00
116.0
2.8
59.00
12.76
44.35
323.00
1033.0
12.74

33.000
172.795
31.500
2.524
27.508

1.488
13.632
4.08Z

.173
1.581
.47%
99.55
.0121
277
179.3
29.22
H17-.0.00
234.0
7.7
eO.Ofl
12.76
121.32
6 -.1.00
1075.0
12.63

15.000
82.579
52.800
1.959
40.000

.874
8.422
8.845

.205
1.971
2.070
99.73
.0094
278
431.0
70.23
41710.00
321.0
7.8
60.00
12.76
129.91
652.00
1274.0
12.64

2.400
32.033
65.000
2.725
78.500

.101
2.357
10.273

.032
.757
3.296
99.94
.0130
279
554.1
90.39
41710.00
369.0
7.6
59.00
12.76
133.25
657.00
1371.0
12.66

1.800
18.233
103.750
3.146
97.500

.066
1.162
10.662

.024
.429
4.008
99.97
.0149
£80
610. 5
99.66
41700.00
390.0
7.7
56.00
12.76
133.45
660.00
1421.0
12.69

2.700
16.636
105.750
3.358
102.500

.092
1.11J
10.376

.036
.••34
4.047
99.97
.0159
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 to
.»•»••»•»•*•»»•»*»•••»»»•»»•»»»»••»»•»•»••«  EFA C»C-E  EMISSIONS COMPUTATION SUMMARY  •»••»»»»»«
ENG MFC « AIRESEARCH            TEST FACIi. I PHX LACC2   INST* OESCKIP I FED REG 1/38 N136
MODEL NO.:     TPE331-5-251N     S/NJ   POvDOl               ENGINE TYPE(CLASS)I  TURSOPROP
RATED POWER!    706.0 SHF  AT SEA ^EYiL STANDARD DAY CONDITIONS
FUE-I ASTM 01655-73             AT01IC H/0 RtTIOl   1.928 .    urtVl 131.70. 3TU/i.a     AOOITIVES'
                                                                                                                              CALC DATE Ul-6-75
                                                                                                                              CALC IDt  1
                                                                                                                             TEST NOI  1".
                                                                                                                         NONE
MODE
TIME IN MODE, MINUTES
RATED POMES, PERCENT
CORRECTED POKES, HORSEPOWER
HP-MR
FUEL FLCH, LB/HR
FUEL MASS. LB
•• HYDROCARBON ENISSION (MCI »•
INOEX, LB HC/1090 LB FUEL
RATE, LB HC/HR
MASS, LB HC
MASS, PERCENT OF TOTAL CYCLE
CYC.E. LB HC/lOaO HORSEPOHSR-H? PER CYC^E
•» CARBON MONOXIDE EMISSIONS (COI »•
INOEX, LB CO/1000 LB FUE-
RATE, Lfc CO/HR
MASS, LB CO
MASS, PERCENT OF TOTAL CYC..E
CYCLE, LB CO/1000 HORS£POHER-HR PtR CYC..E
»• TOTAL OXIDES CF N1TROSEN EMISSIONS A 1979 STANDARDS FOR CLASS  F2  ENGINES "
                                         EPA  LTO-CYCLE
                                                                                                   REQUIRED ENISSION  INOEX,  LBP/1000 LB FUEL
                                  POLLUTANT
                                     CO
                                     HC
                                     NOX
                         LBP/1003 rtORSEPOHER-HR-CYCLE
                               26.8
                                                     12.9
POLLUTANT  (MODEI
   CO  (IDLE)
   HC  (IO..E>
   NOX  (TAKEOFF)
   A
19.6
 *.%
10.3
37.0
 7.1
26.3
                                            A   ASSUMES PROPORTIONAL REOJCTION  OF  PO^^UTANT EMISSION INDEX AT  EACH  LTO CYCLE  NODE

                                            3   ASSUMES (1) 9£JUIS£0 REDUCTION  IN  CO AND HC 03TAINE.O BY LOHE'.ING  EHISSIOM INOEX VALUES
                                                AT  TSXI-IOLE H03E ON-Y,  CO  AND  HC  EMISSIONS AT OTHtR MOOES REMAIN UNCHANGED,  I2»  REQUIRED
                                                R=OU;TION IN NOX OBTAINED 3Y  -.CWERINS EMISSION INCEX YA'.UES  AT CLIMJOUT AND TAKEOFF MODES IN
                                                SAME PROPORTION AS MEASURED YALUES, NOX EMISSIONS 11 TAXI-IDLE AND  APPROACH MOOES
                                                REMAIN UNCHANGED
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                 j.
ENGINE* TPE331-E-251M S/N= P34001 COM3 P/N= 669082-4 FUEL- Atf. KERO. TEST NO.' 14
RAT SHP= 706. RA EuT,F= 1650. RAT SPO- 41730.
FUEL H/C- 1.9280 STOI F/A= .06822 L H V= 16470.
DATA POINT NUMBER 274 275 276
PERCENT MiX. CORRECTED POHER 5.2 7.4 10.1
CORRECTED SHAFT HP 36.4 52.6 71.3
MEASURED SHAFT HP 31.6 45.7 62.0
SHAFT SPEED, Nl , RPM 27510.0 27580.0 27530.0
COMPRESSOR INLET TEMP..DEG.F 60.0 60.0 59.0
COMPRESSOR CSCHG. PRES..PSIA 43.7 44.1 44.4
COMPRESSOR OSCHG. TE1P.OEG F 326.0 322.0 323.0
TURS INTERSTAGE TEMP., 3EG.F 914.0 964.0 1033.0
CORR BELMTH FLOH, LB/SEC 2.90 2.92 2.81
FA RATIO BASED ON 3E.Lt.MTH. .0106 .0115 .0132
MEASURED FUEL FuOH, LB/HR 96.0 105.0 116.0
FA RATIO CAi.C. FROM EMISSION .0102 .0109 .0121
EQUIVALENCE RATIO .149 .160 .178
LOADING */P»*N/V/ECT/S'.OI .335 .335 .319
•COM5EFFIC FROM EMISSIONS 99.171 99.369 99.J49
OcH PT,F=
S LN T,F:
277
29.2
206.3
179.3
41740.0
60.0
121.3
641.0
1075.0
7.70
.11097
234.0
.0094
.138
.083
99.725
CARBON DIOXIDE
PERCENT BY VOLUME, HET 2.11 2.27 2.52
LB. C02 PE4 LS. OF FUEL 3.11 3.12 3.13
HEIGHT FLOH, .B./HR. 298.7 327.6 36t.9
CARBON MONOXIDE
PPK BY VOLUME, HET 206.8 189.7 172.6
LB. PER 1000 LB. OF FUEL 19.428 16. 61- 13.632
HEIGHT FLOH, .B./HR. 1.865 1.744 1.581
UNBURNEU HY3ROCAR30NS- fPH AS CARBON, HEIGHTS AS CH4
PPM BY VOLUME, HET 78.9 54.6 33.0
L3. PER 1000 LB. OF FUEL 4.Z37 2.734 1.488
HEIGHT FLOH, .B./HR. .407 .287 .173
RATIO LB HC/LB CO .2181 .Ib46 .1092
NITRIC OXIDE (NO) - HEIGHTS AS N02
PPH BY VOLUME, HET 18.8 23.2 27.5
LB. PER 1000 .8. OF FUEL 2.901 3.338 3.564
HEIGHT FLOH, LS./HR. .279 .351 .413
NITROGEN DIOXIDE IN02)
PPM BY VOLUME, HET 4.7 3.7 4.0
L3. PER 1000 LB. OF FUEL .725 .532 .518
HEIGHT FLOH, L6./HR. .070 .056 .060
TOTAi. OXIDES OF NITROGEN (,40+NOZ) AS NO2
PPM BY VOLUME, HET 23.5 26.9 31.5
LB. PER 1000 LB. OF FUE- 3.627 3.971 4.062
H€IGHT FLOH, LS./HR. .348 .406 .474
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOW .00698 .00698 .00696
SMOKE NUMBER 4.70 2.43 1.20
CORRECTED HEIGHT FLOH .02033 .02093 .02089
SMCKE NUMBER 4.70 5.90 4.70
CORRECTED HEIGHT FLCH .034*9 .03469 .03482
SMCKE NUMBER 3.20 7.10 8.20
CORRECTED HEIGHT FLCH .04884 .04«d* .04875
SMOKE NUMBER 11. SO 8.60 8.20
SMCKE NUMdER AT HA-0.023 7.40 6.10 5.70
MOTES 1. ALL EMISSIONS CONCENTRATIONS ARE MET VALUES.
2. EQUIVALENCE RATIO CALCULATED FRO* C02,CO,ANO HC DATA
3. MASS EMISSIONS OF NO, NDZ, ANJ NO+N02 CALCULATED AS
1.96
3.14
734.1,

82.6
S.-22
1.371

15.0
.874
.205
.1036

40.0
6.701
1.566

12.6
2.144
.502

52.8
8.845
2.070

. 00705
4.70
.02115
9.40
.03525
10.60
.04935
12.90
9.50

AND FUEL
N02 FROM
= 51. *EL HUM=
= 300.0 FLO,./M=
278 279
70.2 90.4
495.8 638.1
431.0 554.1
41710.0 41710.0
60.0 59.0
129.9 133.3
652.0 657.0
1274.0 1371.0
7.75 7.78
.0133 .0152
321.0 369.0
.0130 .0149
.190 .219
.073 .069
99.936 99.967

2.72 3.15
3.15 3.15
1011.2 1163.1

32.0 18.2
2.357 1.162
.757 .429

2.4 1.8
.101 .066
.032 .024
.0428 .0564

78.5 97. S
9.487 10.207
3.045 3.766

6.5 6.3
.786 .654
.252 .241

85.0 103.7
10.273 10.862
3.298 4.008

.00717 .00717
11.60 9.40
.02151 .02150
15.30 14.10
.03591 .03583
20.00 18.50
.05027 .05017
24.70 24.70
17.90 16.60

COMPOSITION.
70.00 SPEC HUM' .007500
14.160 SL TIM.S' 6.5001
280
99.7
703.7
610.5
41700.0
58.0
133.4
660.0
1421.0
7.67
.0163
390.0
.0159
.23<>
.066
99.966

3.36
3.15
1229.3

16.6
1.113
.434

2.7
.092
.036
.0626

102.5
10.059
3.923

3.2
.319
.124

105.7
10.378
4.0I>7

.00717
9.20
.02150
11.81
.03563
17.61
.05017
23.50
15.30


CONCENTRATIONS HITH MOLECULAR HEIGHT OF NDZ 146.111.
-------
ro
to
^j
CO
                       .....,......,.,....„..,....«•..•»*•.»..».«»..  AISEScuRCH  EMISSION TEST SUMMARY  •»»»»•»»••••»•
                       ENG MFC I AI9ESEA9CH            TEST FACU  : PHX L»C^I   INSTR DESCRIP I  F£3 REG ¥38 N136
                       MODEL NC.»     TPE331-5-251M     S/NI   P04001               ENGINE T»P£ ICi-ASSI J  TURdOPROP
                       RATEO PCHES1     706.0  SHP  AT SEA LEVEL STANDARD DA» CONDITIONS
                       FUELI ASTM 01655-73             ATOMIC H/C  RATIOI   1.936      ^HVI  18.70. BTU/-8     AOOITIVESI
                                                 CALC DATE 111-6-75
                                                 CALC IDI  2
                                                TEST NOI  I*
                                            NONE
                                tXKAUST EMISSIONS  P£< £P« CYCLE OF HORK OUTPUT ••  COOE OF F-OERAL  REoUuATIONS TITLE <-0 PART 87   17  JULY 1973
                                            HYDROCARBONS 
                                            CARdON MOMOXIOE ICO)
                                            OXIDES OF  NITROGEN  INOX AS N02)
                                            SMOKE
 3.035 LB. POLLUTANT PER 1000  H?.-HR.  PER CYCCE
16.401 i_B. POLLUTJM PER 1000  HP.-HR.  PER CYCLE
 7.932 LB. POLLUTANT FtR 1800  HP.-HR.  Ftfi CYCLE
 li.6  3HOK.E NUMBER, MAXIMUM AT   CRUISE    MODE,
70 PERCENT RATEO  POKER
                       TAXI-IDLE SETTING! 5.0
                                                            RATEO TAX-OFF POWER AT  65.
                                                                                             PERCENT RATEO TAKEOFF Nl KPM
                       »»....,.........,.»».....».».».»»...»»..».........»«  tMGINE  DESCRIPTION  »»»»»»»»»..»»»».»»».»»»»•»»»»»•••»••»••••
                       COMB TYPEI REVERSE FLOM  ANNULAR           P/NI   S6908Z-1.            SUR/VC-I  1.260  FUEL INJ TTFEI   STAGED  SIMPLEX
                       ENGINE TOTAL SERVICE!  0.0        HR    TIME SINCE ENGINE OVERMAULI   ».»       HR
                       ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                       AIRCRAFT INSTALLATION »•»•  MF<.I                                   MODEL  NO.I
                                                   USERI                        ENGINE INSTALLATION  POSITIONI
                                                                             '
GASEOUS EMISSION TEST NC.J 14 DATES 11-6-75 TIME!
AMBIENT AIR TEHF.I 59.00 DEG. F RiLATIVi HUMIDITY: 70.08 PERCENT
AMBIENT AIR QUALITY HYDROCARBONS (HCM 0.0 PPNC CAR93N HONOXIOE (C0)«
SPECIFIC
0.0 PPMV
BASo fRESS.I 25.980 IN. HGA.
HUMIDITY! .007500 LB. H20/LB. DRY AIR
C-XIOES OF NITROGEN INOX)I 0.0 PPM¥
SAMPLE LINE ••• TEHP.I 300. CJ OEG. F. FLCHSATEJ 14.16 .ITERS/MIN. TRANSPORT TIME! 6. 50. SEC.
TEST CONDITION
ACTUAL FOHER SETTING, HORSEPOWER
CORR. FOMER SETTING (STD DAYI, PERCENT RATEO
Nl SPEED. RPM
FUEL FLCN (MEAS.I LB./HR.
CORR. ENGINE CORE AIRFLCM MEAS) , LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., OEG F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTA. PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTA- TEMP., OEG F
TURBINE INTERSTAGE GAS TOTAL TEMP., OFG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION, MET ANALYSIS
HYDROCARBON IMC AS CH4) , PPMC
CARBON MONOXIDE (CO) , PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPNY
CARBON DIOXIDE IC02), PERCENT BY VO...
NITRIC OXIDE INO), PPMV
EMISSION INDEX, LB. POLLUTANT/1808 L3. FUEL
HYDROCARBONS «HC AS CHfcl
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN INOX A3 N02)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS IHC AS CH<»)
CARBON MONOXIDE (CO)
TOTA' OXIOES OF NITROGEN INOX AS N02) .
conausTiON EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS. CALC)
281 282 283
30.0
4.90
2756i).00
96.0
3.0
59.00
12.76
43.47
320.00
917.0
12.75

81.000
219.944
22.-.00
2.0*7
16.900

4.4.75
21.259
3.556

.4JO
2.841
.341
99.11
.0099
46.6
7.61
27530.00
106.0
2.9
59.00
12.76
43.86
320.00
972.0
12.75

52.500
195.179
27.300
2.277
22.900

2.617
17.022
3.911

.277
1.804
.415
99.37
.0110
61.9
10.10
27520.00
115.3
2.8
59.00
12.76
44.20
321.00
1037.0
12.74

33.000
175.966
52.000
2.514
27.500

1.494
13.937
4.1fa3

.172
1.603
.479
99.54
.0121
284
1*4.3
30.13
41740.00
236.0
7.7
57.00
12.76
119.84
642.00
1123.0
12.62

12.000
80.028
55.300
2.051
41.000

.658
7.796
S.8-,9

.158
1.840
2.098
99.76
.0098
285
1-27.8
b9.85
41720.00
325.0
7.7
58.00
12.76
128.59
652.00
1335.0
12.64

2.400
37.775
82.500
2.785
77.500

.099
2.719
9.755

.032
.884
3.170
99.93
.0133
2«6
551.1
89.98
41730.00
373.0
7.8
58.00
12.76
132.22
658.00
1458.0
12.68

1.800
21.865
103.250
3.207
99.500

.064
1.368
•10.609

.024
.510
3.957
99.96
.0152
LENGTHI 50.80 FT.
287
609.9
99.30
41730.00
397.0
7.7
61.00
12.76
133.45
661.01
1511.0
12.69

i.eoe
19.442
110.000
3.457 '
108.750

.060
1.128
10.486

.021,
.448
4.163
99.97
.0161,
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to
      ..........................................   cpu  CYC_E EMISSIONS COMPUTATION SUMMARY  •••»•»»••«
      ENG MFC I AIRESEARCH           TEST  FACIL  I  PMK  LACCI  IN3TR OESCAIP I FED REG V38 N136
      MODEL NO. I     TPE341-5-251M     S/NI    P0<>001               £NGIN£ TYPE(CLASS»  TUR33PROP
      RATED POWER!    706.0 SHP AT SEA LEVEL  STANDARD  DAY  CONDITIONS
      FUEL< ASTM Dlb55-73            ATOMIC H/0 RATIO!    1.92d     LHVI 181.70. oTU/^6     AODITIVESI
                                                                                                                                CALC DATE 111-6-75
                                                                                                                                CALC IDt   2
                                                                                                                               TEST  NOI   14
                                                                                                                           NONE
NODE
TIME IN MODE, MINUTES
RATED FOWER, PERCENT
CORRECTED POWER, HCRStPONES
HP-HR
FUE- FLOW, LB/HR
FUE. MASS, LB
•• HYDROCARBON EMSSION (nCI »•
INDEX. LB HC/1001) LB FUEL
RATE. LB hC/HR
MASS. LB HC * ,
MASS, FERCEMT OF TOTAL CYCLE
CYCLE. LB HC/1000 HCRSEPCKER-HR PER CYC^E
•• CARBON MONOXIDE EMISSIONS CCOI •»
INDEX. LB CO/1000 LB FUEL
RATE. IB CO/HR
MASS. LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE. L3 CO/1000 HORSEPOHER-HR PER CYCLE
»• TOTAL OXIDES OF NITROGEN EMISSIONS 
-------
            oouov*
-j
ui
ENGINE^ IPt331-5-251N S/N= PO-.OC1
RAT SHP- 706. RA EGT.F- 1654.
FUEL H/C= 1.9280 STOI F/A= .06422
DATA POINT NUMBER - 281
PERCENT MAX. CORRECTED PCHER *.9
CORRECTED SHAFT HP 3».6
MEASURED SHAFT HP 30.0
SHAFT SPEED, Nl. RFH 37560.0
COMPRESSOR INLET TEHP.,OLG.F 59.0
COMPRESSOR DSCHG. PF.ES..PSIA -.3.5
COMPRESSOR DSCMG. TEMP, BEG F 320. C
TUR3 INTERSTAGE TEMP., 0£G.F 917.0
COR* SEtNTri FLOH, LB/SEC 2.99
FA RATIO EASED ON BcLLMTH. .0103
MEASURED FUEL FLOH, LB/HR 96.0
FA SATIO CALC. FRCM EMISSION .0099
EQUIVALENCE RATIO .1*5
LOADING H/F»»N/V/£(T/5*0) .353
COM3 EFFIC FROM EMISSIONS 99.107
CARBON DIOXIDE
PERCENT BY VOLUME, HET 2.05
L3. CCZ PER iB. OF FUEL 3.11
HEIGHT FLOH, LB./HR. 295.1.
CARBON MONOXIDE
PPIl BY VOLUME, HET 219.9
L3. PER 1000 LB. OF FUEL 21.259
HEIGHT FLOH, LB./HR. 2.0
-------
0)
iQ
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to
                        •.»>..».*............,.,......,.,,....,.....,  AIRE3EARCH EMISSION  TEST  SUMMARY  »•»•••»•••»»•«
                        ENG MFC I AIRESEARCH            TEST FACI.. 1 P^X LACC2  IN3TR OESCfJIP  I FED  KEG  V3S N136
                        MODEL NO. I     TPc331-5-25in      S/Nt   PO-.001              ENGINE  TYPE (CLASS) I  TURBOPROP
                        RATED POWERS     706.0 SHP  AT  St.A  LEVEL STANDARD DAY CONDITIONS
                        FUELS ASTN 01655-73             ATOMIC H/C RATIOI   1.939     LHVI 181.70.  6TU/LB     ADOITIVESI
 CALC DATE 111*6-75
 CALC 101  3
TEST NOt  14
                                                                                                                          NONE
                        •*«»»»»» EXHAUST EMISSIONS PER  £PA CYCLE OF WORK OUTPUT •• CODE OF FEDERAL  REGULATIONS TITLE 40 PART 67  17  JULY  1973   •»»»»•»
                                            HYDROCARBONS  (CH AS CH4I          3.005 .3. POLLUTANT PER 1000  HP.-HR. PER CYCLE
                                            CARBON MONOXIDE (GDI             16.477 L3. FOLUUTANT PER 1000  HP.-HR. PER CYCLE
                                            OXIDES OF NIT90GEN  (N3X AS N02)   8.244 LB. POLLUTANT PER 1000  HP.-HR. PER CYCLE
                                            SMOKE                              16.0  SMOKE NUMBER, MAXIMUM AT  CRUISE    MODE,  70 PERCENT  RATEO POWER
                        TAXI-IDLE SETTINGS 5.0      PERCENT RST-:0 TAKEOFF PUHER AT 6i.      PERCENT RATED TAK-OFF Nl RPM
                        .*...........,.......,..,......,..„...,......•..,,,.  ENGIN£ DESCRIPTION  »»»*••«••*»»»••»»••••»•••«•»••••»••»»•«.»•»•••••••••»
                        COMB TYPEI REVERSE FLOW ANNULAR            P/NS   869082-4            SUR/VOLS  1.260   FJEL INJ TYPES . STAGED  SIMPLEX
                        ENGINE TOTAL SERVICES  0.0        HR    TIME SINCE ENGINE OVERHAULS   0.0        HR
                        ENGINE ASSEMBLY AND MAINTENANCE  INFORMATION!
                        AIRCRAFT INSTALLATION »»•• MFR.I                                  MODEL NO. S
                                                   USERI                        ^NGINE  INSTALLATION POSITIONS
                        „.»».»..,.,.,..,.,,...,...,,.,,.,»».,,..,..,,,,3PER4rlONftL T£S7 OATA  SUMHARV ..I,*.*..*.......*....................*...........
                        GASEOUS EMISSION TEST HO. I   In           DATES 11-6-75            TIMES                     8ARO PRESS.S  25.980  IN.  HGA.
                        AMBIENT AIR TEMP.I  59.00 OEG. F         R-LtTIVE HUMIDITY:  70.00 PERCENT        SPECIFIC HUMIOITYS  .007500  LB.  H20/I.B. DRT AIR
                        AMBIENT AIR QUALITY    HYDROCARBONS 1HCI1 0.0   PPHC     CAR30N HONOXIOE (CO):  0.0    PPMV    OXIDES OF NITROGEN  (NOX)I 0.0   PPMV
                        SAMPLE LINE ••» TEMF.S  300.00 DEC. F.     FLOWRATE:   14.16 ^ITEKS/MIN.     TRANSPORT TIME:    6.50  SEC.     LENGTHS   50.00 FT.
TEST CONDITION
ACTUAL POME? SETTING, HORSEPOWER
CORR. POWER SETTING (ST3 OAYt , PERCENT RATED
Nl SPEED, RPH
FJEt. FLCW (MEAS.) LB./HR.
CORR. ENGINE CORE AIRFLOW (MEAS), LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., OEG F
COMPRESSOR. INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTA. PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTA. TEMP., OEG F
TURBINE INTctSTAGE GAS TOTAL TEMP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION, WET ANA.YSIS
HYDROCARBON ( HC AS CH-,) . PPMC
CARBON HONOXIOE ICC) , PFKV
TOTAL OXIDES OF NITROGEN  , FPKV
CARBON DIOXIDE (C02), PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSION INOEX, L8. POLLUTANT/1000 LB. FUEL
HYDROCARBONS IHC AS CH4I
CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (MOX AS N02)
EMISSION RATE, 1.8. PCLLUTANT/HR.
HYDROCARBONS IHC AS CH4.1
CARBON MONOXIDE (CO)
TOTAL OX13ES OF NITROGEN (NOX AS N02)
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS, CALCI
288 289 290
31.1
5.07
27500.00
96.0
2.9
59.00
12.76
»3.37
319.00
902. 0
12.75

75.000
216.636
23.900
2.019
19.100

4.202
21.235
3.848

.<>03
2.039
.369
99.13
.0098
46.7
7.61
27560.00
108.0
2.9
59.00
12.76
44.11
32G.OO
974.0
12.75

47.100
191.033
28.500
2.287
24.200

2.339
16.597
4.067

.253
1.792
.439
99.40
.0110
62.6
10.21
27500.00
119.0
2.8
58.00
12.76
'44.70
322.00
1032.0
12.75

31.8GC
174.153
32.200
2.488
27.600

1.455
13.937
4.233

.173
1.658
.504
•99.54
.0119
291
185.6
30.33
41740.00
236. 0
7.7
57.00
12.76
119.84
6*3. 00
1115. 0
12.63

13.500
80.028
58.100
2.070
43.700

.745
7.725
9.213

.176
1.823
2.174
99.75
.0099
292
433.8
70.83
41740.00
322.0
7.8
58.00
12.76
128.54
651.00
1352.0
12.63

1.500
35.310
83.250
2.752
74.250

.062
2.572
9.962

.020
.828
3.208
99.93
.0131
293
546.9
89.21
41720.00
372.0
7.7
59.00
12.76
132.51
658.00
1447.0
12.66

.600
22.270
105.500
3.237
102.250

.021
1.380
10.740

.008
.513
3.995
99.97
.0150
" *"«" *"
609.0
99.53
41770.00
393.0
7.7
57.00
12.76
133.10
659.00
1507.0
12.68

.900
11.817
113.250
3.419
112.500

.030
.693
10.917

.012
.273
0.290
99.98
.0162
                                        >


                                        )


                                        >


                                        )


                                       . >


                                        )


                                        )
                                                                                                                                                                      >


                                                                                                                                                                      >
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                         w»"~
(D
                          ..........................................  EPA CYCw£ ^MISSIONS  COMPUTATION  SUMMARY  ••••»•••»«
                          CNG MF6 I AIRESEARCH            TEST FACI* « PHX LACC2  INSTR  OESCUP  «  f £0 RE&  V38. N136
                          MODEL NO.S     TPE331-5-2S1H      S/NJ   P04001              ENGIN;  TYPcfCLASSII   TURBOPROP
                          RATED PCWERI    706.0 SM? AT  SEA  i.EI/E_ STANDARD ClAY CONDITIONS
                          FUEL I ASTN D1655-73             ATOMIC H/C RATIO:   1.928      tHUI 18*70.  BTU/LB      AOOITIVESI
                          C»LC DATE 111-6-75
                          CALC 101  3
                         TEST NO!  It
                                                                                                                            NONE
MODE
TIHt IN H03f, MINUTES
RATED POWER, PERCENT
CORRECTED PCHEK, HORSEPOWER
HP-HR
FUEL FLCN. LB/HR
FUE. MASS. LB
•• HYOKOCA43JN EMISSION IHCI •»
INDEX. L3 HC/1BOO LB FUEL
RATE, LB HC/MR
MASSt LB MC
HASSt PERCEMT OF TOTAL CYCLE
CYCLE, L3 HC/10CO HO<{S£POMc«-H% PER CYCLE
»» CARbON MONOXIDE EMISSIONS (COI »•
INDEX, L8 CO/1000 LB FUEi.
RATE. LB CO/HR
MASS, LB CO
MASS, PtRCEM OF TOTAL CYCLE
CYC^E, LB CO/1000 MORSEPC14HR-HR PER CYCLE
•» TOTAL OXIDES OF NITSO&tN EMISSIONS «NOX1 »•
INDEX, LB NOX/1000 LB FUEL
RATE, LB NOX/HR
NASS. L6 NOX
MASS, PERCENT OF TOTAL CYCcE
CCCi-t, LB NCX/1000 HOftSEPOHER-HR PER CYCLE
TAXI-UI.E
(IN)
7.000
$.000
35.300
1..11S
95.613
11.155

••.279
.«,09
.01.8
25. 0


21.»18
Z.0>>8
.239
22. e


3.636
.367
.043
8.2

TAXI-IO.E
IOUT)
19.000
s. aoo
35.300
11.176
95.613
30.278

V.279
.1,09
.130
67.9


21.-.18
2.01,6
.61,6
61.9


3.838
.367
.116
22.2

APPROACH
H.500
30.000
211.600
15.885
233.666
17.525

.763
.178
.013
7.0


7.900
1.823
.137
13.1


9.129
2.133
.160
30.5

CLIMBOUT-
2.500
40.000
635. i. 00
Z6.I.75
375.895
15.662

.003
.101
.000
.0


1.316
.<.95
.021
2.0


10.821
"..068
.169
32. *

TAKEOFF
.500
100.000
706.000
5.863
390.99".
3.258

.065
.025
.000
.1


.677
.265
.002
.2


10.8*2
i.. 239
.035
6.7

TOTAL PER
CYCLE
33.911


63.5*1

77.878

2.452
.342
.191
110. 1
3.015

13.t<>3
1.875
1.01.7
1«0.0
16.1.77

6.72S
.938
.52)1
101. 1
8.2^
                                                »• EMISSION INOEX LEV£.S  lEQUI^EO  TO MEcT EPA 197S STANDARDS FO? CLASS  P2  ENGINES ••


                                             EPA LTO-CYCLE                                            REQUIRED EMISSION  INDEX,  LBP/1000 LB FUEL
                                     POLLUTANT    LBP/1JOO HORS£POWiR-HS-CYCL£
                                        CO              Z6.8
                                        HC               4.9
                                        NOX             12.9
POLLUTANT (MODE)
   CO CID..EI
   HC 1IO-E)
   NOX  ITAKEOFF)
 1..3
10.8
   B
37.2
 7.2
26.5
                                                A   ASSUHES PAOPORTI3NA,. REUUCIION  OF PO-LUTANT EMISSION INDEX AT  EACH LTD  CYCLE  NODE

                                                B   ASSUHES (1) 3E3UKEO REDUCTION  IN CO AND HC OSTAINtO BY LOWERING EMISSION  INDEX  VALUES
                                                   AT TAXI-ia^c M00£ CM.Y, CO  AND  HC EMISSIONS AT OTHER MOOES REMAIN UNCHANGED,  12)  REQUIRED
                                                   REDUCTION IN NJX OuTOINED bY  -OHL^I.-JG EMISSION INOiX VALUES AT CLIKBOUT  AND TAKEOFF MODES IN
                                                   SAME PROPORTION AS  .liiSJKEJ VALUES, NOX EMISSIONS AT TAXI-IOLE AND APPROACH MOOES
                                                   %£HAIN UNCHANGED
-------
13
Pi
KJ
>J
CO
ENGINE- TPE331-5-251M
RAT SHP= 706. RA FGT,r=
FUEI. H/C- 1.9260 STOI f/t=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POME*
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEE3, Nl. RPM
COMPRESSOR INLET TEBP..OEG.F.
COMPRcSSO* CSCrii. PR£S. .FSIA
COMPRESSOR DSCHG. TE^P.DLG F
TURd INTERSTA5E TtMP. , CCG.F
COR* StLMTH FLOH, L6/SEC
FA RATIO 54SEO ON BF.LMTH.
MEASURED FUEL FLOH, L3/HR
FA P.ATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P**N/V/E(T/5i.O»
COMB EFFIC FROM EMISSIONS
CARBON OIOXIOE
PERCENT BY VOLUME, HET
LB. C02 PER ..9. Of FUEu
HEIGHT FLOH, L8./HR.
CARBON MONOXIDE
PPH BY VOLUVE, MET
LB. PER lOOa LB. CF FUE-
HEIGHT FLOH, LB./HR.
UNBUKNEO HYOHOC«R30NS-- PFN AS
PPf BY VOLUME, MET
L3. PtR 1000 LB. OF FUEL
HEIGHT Ft.OH. LB./HR.
RATIO LB HC/LB CO
j/H= FO-.
1650.
.06822
238
5.1
35. i
31.1
27590.0
' 59.0
1.3.1.
319.0
902.0
2.9*
.310<
96.0
.0095
.11.3
.353
99.132

2.02
3.11
295.5

216.6
21.235
2.039
CARSON.
75. J
1..202
• **03
.1979
001
RAT SPD=
L H V-
264
7.6
53.8
*o. 7
27560.0
59.0
1-. 1
320.0
97L. 0
2.93
.0118
103.0
.0110
.161
.338
49.10*

2.29
3.12
337.1

191.0
16.597
1.79Z
HEI3HTS AS
1.7. 1
2.339
.253
. 1L09
COMB P/N= 869062-1. FUEL= AV. KERO. TEST NO.* 1*
1.1730.
161.70.
290
1C. 2
72.1
6Z . 6
27500.0
58.0
•»-. 7
122.0
1032.0
2.81.
. 013>.
119.0
.0119
.175
.319
99.S<»5
•SUMMARY
2.1.9
3.13
372.3

17n. Z
13.937
1.656
CHI.
31.8
1.1.S5
.173
.10'.'.
OEM PT.F-
S LK T,F=
291
30.3
21W.1
165.6
-.17-.J.O
57.0
119. S
£1.3.0
1115.0
7.68
.0099
Z3fc.O
.0093
.115
. CSS
99.753
OF REOUCEO
2.07
3.1i
7.1.0

83.0
7.7Z5
1.923

13.5
.71.5
.176
.0961.
51.
300. a
292
70.8
500.1
1.33.8
1.1710.0
58.0
128.5
651.0
1352.0
7.76
.0132
322.0
.0131
.192
.075
99.93k
EMISSION
2.75
3.15
101». 3

35.3
2.572
.626

1.5
.062
.020
.021.3
RE- HUM=
FLO,^/M=
293
89.2
629.9
5*6.9
1.1720.0
59.0
132.5
659.0
lit 47.0
7.72
.0151.
372.0
.0151.
.225
.069
99.966

3.21
3.15
1172.5

ZZ.3
1.360
.513

.6
.021
.006
.0151.
70.00 SPEC HUH= .007500
11.160 SL TIN.Ss 6.5000
291.
99.5
702.7
609.0
1.1770.0
57.0
133.1
659.0
1507.0
7.73
.0162
393.0
.0162
.236
.069
99.961

3.12
3.15
1239.1

11.6
.693
.273

.9
.030
.012
.0135
NITRIC OXIDE INOI - HEIGHTS A3 N02
PPM BY VOLUME, MET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH. LB./HR.
NITROGEN DIOXIDE IN02I
PPM BY VOLUME, MET
L3. FER 1000 .B. OF FUEL
HEIGHT FLOH, .B./HR.
TOTAL OXIDES OF NITROGEN INC*
PPM BY VOLUME, MET
IB. PER 1000 LB. OF FUEL
HEIGHT FLOM, LB./HR.
SMOKE MfASUREMENf DATA
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLCM
SMOKE NUMBER
C3RRECTCG HEIGHT FLO
SMOKE NUMBER
CORRECTED HEIGHT FLCM
SROKE NUMBER
SriOKE NUMBER AT H4-0.023
19.1
3.075
.295

1.8
.773
.07-.
2i.. 2
3.*5i»
.373

-.3
.alU
.056
27.6
3. 628
.1.32

1..6
.605
.072
1.3.7
6.529
1.635

li.l
2.263
.539
71..2
8.665
2.661

9.0
1.077
.3*7
102.2
10.409
3.672

3.3
.331
.123
112. S
10.81.1,
<..26Z

.7
.072
.026
N02> «3 NOZ
23.9
3. 8*6
.369

.03696
.60
.02088
7.10
.03l>91
).20
.01.873
10.60
6.80
29.5
1.067
.•.39

.00696
2.1.3
.02088
5.90
.03U81
7.19
.01873
9.1.0
6.39
32. Z
1.233
.501,

.00696
2.1.0
.92086
5.30
.031.81
5.90
.01073
7.11
5.20
59.1
9.213
3.171.

.00695
b.70
.02066
8.80
.03,77
12.10
.01-368
16.20
11. ZO
63.2
9.962
3.208

.00708
7.10
.02123
li.lO
.03536
18.60
.01,953
23.50
16.01
105.5
10.71.0
3.995

.00710
5.90
.02131
11.80
.03551
17.60
.01572
21.20
It.ZO
113. Z
10.917
<..29I

.00713
5.91
.02136
9.1.0
.03563
15.30
.01.S89
20.00
12.70
                    NOTtS 1. ALL  EMISSIONS  CONCENTRATIONS ARE  MET  VALUES.
                          2.£UU:V«LtNCE  WTIO CALCJ-ATED FROM  COZ.CO.ANO MC DATA
                          3.MASS  EMISSIONS  CF MO, N02, AND N3»N02  CAwCU^ATE3 AS
 AND FUEL COMPOSITION.
'102 F=.OK CONCENTRATIONS HITH
MOLECU.AR HEIGHT OF  NOZ C.6.011.
-------
•••••••••••••••••••••••••••••••••••••••••••I*  AIRESEARCH EMISSION  TEST  SUMMARY   ••••»••••••••«
ENG MFC t AIRESEARCH            TEST FACIL > PHX LACCZ  INSTR OESCRIP  I FED   REG  V38 N136
MODEL NO.S      TPE331-5-251N     S/NI    P04001              ENGINE  TYPE(CLASS)S   TURBOPROP
RATED POWERS     706.0  SHP  AT SEA LEVE.. STANDARD DAY CONDITIONS
FUELS ASTM 01655-73             ATOMIC  H/C RATIOS   1.928     LHVI 18470.  BTU/LB      AOOITIVESS
                                                                                                                     NONE
                                                                                                                          CALC DATE  111-3-75
                                                                                                                          CALC IDI     1
                                                                                                                         TEST NOI     15
                   »»»»••»»  EXHAUST EMISSIONS PER EPA CYCLE OF WORK OUTPUT •»  CODE  OF FEDERAL REGULATIONS TITLE 40 PART 87  17 JULY  1973   ••*»••»•
                                        HYDROCARBONS (CH AS CH4)          3.770  ,.8.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                        CARBON MONOXIDE (CO)             19.454  LB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                        OXIDES OF NITROGEN  (NOX AS N02I   9.060  LB.  POLLUTANT PER 1000 HP.-HR. PtR CYCLE
                                        SMOKE                             15.8   SMOKE  NUMBER, MAXIMUM AT  CRUISE    MODE.  70 PERCENT RATED POWER
                   TAXI-IDLE  SETTINGS  5.0      PERCENT RAT£0 TAKEOFF POWER AT  65.       PERCENT RATED TAKEOFF Nl RPH
(D
                   ..,•..,.».»».»„.„.„„.„„»„».„„»„»...„...»,,  £NGINE DESCRIPTION  •••»•»••••••••••••••••••••»•••••••••»•••••••••••••••
                   COMB TYPES  REVERSE  FLOW ANNULAR           P/NI   869082-4            SUR/VOLS  1.260  FUEL INJ TYPES  STAGED SIMPLEX
                   ENGINE TOTAL  SERVICES   0.0       HR    TIME SINCE ENGINE OVERHAULS   0.0        HR
                   ENGINE ASSEMBLY  AND MAINTENANCE INFORMATION!
                   AIRCRAFT INSTALLATION  •••• HF3.I                                  MODEL  NO.S
                                               USERS                       ENGINE  INSTALLATION POSITIONS
                   •••••'••••••••••••••••••••••••••••••••••••••••••OPERATIONAL TEST  DATA  SUMMARY •••»•••••••••••••••••••••••••••••••»•»••••••••••
                   GASEOUS EMISSION TEST  NO. s    15        OATEl  11-3-75            TIMES                     BARO PRESS.s  20.960 IN. HGA.
                   AMBIENT AIR TEMP.I   59.00  OEG.  F        RELATIVE HUHIOITYS  70.00 PERCENT       SPECIFIC HUMIOITYS  .007500 LU. H2O/LB. ORV AIR
                   AMBIENT AIR QUALITY    HYDROCARBONS (HO I 0.0   PPHC     CARBON MONOXIDE (CO) I  0.0   PPMV    OXIDES OF NITROGEN INOXM 0.0    PPHV
                   SAMPLE LINE »•»  TEMP.S   300.00  OEG. F.     FLOWRATES   14.16 LlTERS/MIN.     TRANSPORT TINES    6.50 SEC.     LENGTHS   50.00 FT.
TEST CONDITION
ACTUAL POWER SETTING, HORSEPOWER
CORR. POWER SETTING (STO 0«Y), PERCENT RATED
Nl SPEED, RPH
FUEL FLOW (MEAS.) LB./HR.
CORR. ENGINE CORE AIRFLOW (MEAS). LB/SEC
COMPRESSOR INLET AIR TOTAL TE1P. . DEG F
COMPRESSOR INLET AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS.. PSIA
COMPRESSOR DISCHARGE AIR TOTAL TEMP., OEG F
TURBINE INTERSTAGE GAS TOTAL TEMP.. BEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION, WET ANALYSIS
HYDROCARBON (HC AS CH4), PPMC
CARBON MONOXIDE (CO) , PPHV
TOTAL OXIDES OF NITROGEN (NOX), PPHV
CARBON DIOXIDE (C02). PERCENT BY VOL.
NITRIC OXIDE INO), PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS CMC AS CH4)
CASBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS CMC AS CH4)
CARBON MONOXIDE ICO)
TOTAL OXIDES OF NITROGEN (NOX AS NOZ)
COHBUSTION EFFICIENCY, PERCENT (EMISSIONS)
F/A (EMISSIONS, CALC)
Z95 296 297
34.7
5.08
27570.00
116.0
3.0
58.00
14. 22
49. Zl
321.00
865.0
14. Zl

78.000
216.636
21.000
1.963
14.000

4.491
21.824
3.475

.521
2.532
.403
99.09
.0095
50.3
7.38
27520.00
119.0
2.9
56.00
14.22
49.36
319.00
929.0
14.21

48.000
190.114
23.400
Z.170
18.100

2.510
17.396
3.517

.299
2.070
.419
99.37
.0105
70.6
10.32
27540.00
132.0
2. »
61.00
14.22
49.36
326.00
1018.0
14.21

31.500
165.129
26.800
2.467
23.300

1.453
13.328
3.818

.192
1.759
.504
99.56
.0118
298
ZOZ.O
29.56
41740.00
256.8
7.9
59.00
14.22
135.41
643.00
1093.0
14.10

7.800
56.850
56.000
1.977
41.700

.451
5.754
9.310

.116
1.484
2.402
99.03
.0095
299
475.6
69.39
41750.01
350.0
7.9
62.00
14.22
142.53
654.00
1300.9
14.12

3.900
20.249
65.250
Z.690
76.000

.166
1.505
10.410

.058
.527
3.643
99.95
.0128
300
611.9
89.37
41730.00
400.0
7.9
61.00
14.22
147.10
659.00
1404.0
14.16

3.300
17.026
101.000
3.124
93.000

.121
1.093
10.653

.048
.437
4.261
99.96
.0148
301
680.3 . . 	
99.27
41730.00
. 431.0 	 	
7.8
62.00
14.22 _____
140.82
663.00
1480.0
14.17

3.300
13.416 " ."
107.500
3.364
102.500

.111
.000
10.532

.040
.345
4.539 	 .....
99.97
.0160
-------
 (U
Ifl
 n>
 00
 o
..........................................   £pA CYC^E EMISSIONS COMPUTATION SUMMARY  •••»»••»••
ENG MFC I AIRESEARCH            TEST  FACIi.  I  PHX LACC2  INSTR OESCRIP I  FED  REG  V38 N136
MODEL NO.I     TPE331-5-251M      S/Nt    P04001               ENGINE TYPE«CLASS»«   TURBOPROP
RATED POWER!    706.0 SHP AT  SEA  LEVEL  STANDARD DAY CONDITIONS
FUEL« ASTM 01655-73             ATOMIC H/C  RATIOI    1.926     -HV1 16470. BTU/LB      ADDITIVES!
                                                                                                                         CALC DATE  111-3-75
                                                                                                                         CALC IDI    1
                                                                                                                         TEST NO!    15
                                                                                                                     NONE
MODE
TIME IN MODE, MINUTES
RATED POME*, PERCENT
CORRECTED POWER, HORSEPOWER
HP-HR
FUEL FLOW, LB/HR
FUEL MASS. LB
•• HYDROCARBON EMISSION IHC» ••
INDEX, LB HC/1000 LB FUEL
RATE, LB HC/HR
MASS, LB HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORSEPOHER-HR PER CYClE
•• CARBON MONOXIDE EMISSIONS ICOI ••
INDEX. LB CO/1000 LB FUEL
RATE, LB CO/HR
MASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE. LB CO/1000 HORSEPOHER-HR PER CYCLE
•• TOTAL OXIDES OF NITROGEN EMISSIONS INOXI »•
INDEX, LB NOX/10BO LB FUEL
RATE, LB NOX/HR . . . _ .
MASS, LB NOX
MASS. PERCENT OF TOTAL CYCLE
CYCi.E. LB NOX/1000 HOSSEPOHER-HR PER CYCLE
TAXI-IDLE
(INI
7.000
5.000
35.300
4.118
116.039
13.536

4.583
.532
.062
25. 9


21.995
2.552
.296
24.1


3.476
.403
.047
6.2

TAXI-IDLE
(OUTI
19.000
5.000
35.300
11.176
116.039
36.746

4.583
.532
.166
70.3


21.995
2.552
.608
65.4


3.476
.403
.126
22.2

APPROACH
4.500
30.000
211.800
15.885
259.844
19.488

.375
.097
.007
3.0


5.635
1.464
.110
8.9


9.448
2.455
.164
32.0

CLIMBOUT
2.500
90.000
635.400
26.475
401.095
16.712

.042
.017
.001
.3


1.011
.405
.017
1.4


10.728
4.303
.179
31.1

TAKEOFF
.500
lao.ooo
706.000
5.863
435.449
3.629

.299
.13*
.001
.5


.941
.410
.003
.3


10.336
4.501
.038
6.5

TOTAL PER
CYCLE
33.510


63.540

90.113

2. 658
.429
.240
100.0
3.771

13.717
2.214
1.236
100.0
19.454

6.389
. l.I31_
.576
100.0
9.060
                                          •• EMISSION  INOEX  LEVELS  REQUIRED  TO MEET  EPA 1979 STANDARDS FOR CLASS P2 ENGINES •*
                                       EPA LTO-CYCLE
                                                                                                REQUIRED EMISSION INDEX,' LBP/1000 LB FUEL
                                POLLUTANT   L3P/1000 HORStPOW£R-HR-CYCLE
                                   CO             26.6
                                   HC          _ .   4.9
                                   NOX            12.9
                                                                             POLLUTANT 
-------
                       XYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYXYxYXYXYXYXVXYXYXYXYXYXYXYXYXYXYXVXrXY
                       XVXYXYXYXYXVXYXYXYXYXYXYXYXYXYXYXYXYXYXYXVXrXVXYXYXYXYXYXYXVXYXYXYXYXYXYXYXYXYXYXYXYXY
 {a
iQ
 (D

 to
 CO
ENGINE^ TPE331-5-Z51H S/N= P04001 COMB P/N= 869082-4
RAT SHP* 706. RA EGT.F-
FUEL H/C= 1.9Z80 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POKER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Ml. RPM
COMPRESSOR INLET TEMP., OEG.F
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR DSCHG. TENP.DEG F
TURB INTERSTAGE TEMP., OEG.F
CORK BELNTH FLOH, LB/SEC
FA RATIO BASED ON BELLNTH.
MEASURED FUEL FLON, LB/HS
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P*»N/V/E«T/540I
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
LB. COZ PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NO) - HEIGHTS AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE (N02)
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
TOTAL OXIDES OF NITROGEN (NO»N
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
SMOKE NUMBER AT HA*0.023
1650.
.06822
295
5.1
35.9
34.7
27570.0
58.0
49.2
321.0
865.0
2.97
.0112
116.0
.0095
.139
.31*
99.093

1.96
3.11
360.5

216.6
21.824
2.532
RAT SPO= 41730.
L H V
Z96
7.4
52.1
50.3
^7520.0
56.0
*9.4
319.0
929.0
2.92
.0117
119.0
.0105
.153
.309
99.371

Z.17
3.12
371.3

190.1
17.396
2.070
CARBON, HEIGHTS AS
78.0
4.491
.521
.2058
N02
14.0
2.317
.269

7.0
1.158
.134
021 AS N02
21.0
3.475
.433

.00797
1.20
.02121
7.00
.03535
7.00
.049*9
1. 10
S.»0
48.0
2.510
.299
.1*43

18.1
2.720
.324

5.3
.797
.095

23.4
3.517
.419

.00707
2.30
.02121
3.50
.03535
4.78
.04949
5.80
4.10
= 18470.
297
10.3
72.8
70.6
27540.0
61.0
49.4
326.0
1018.0
2.81
.0135
132.0
.0118
. 1?*
.292
9».55s
SUMMARY 0
2.^7
3.13
413.0

165.1
13.3Z8
1.759
CH4
31.5
1.453
• 192
.1090

23.3
3.069
• 418

5.5
• 729
• 096

28.8
3.818
.504

•00706
2.30

3.50
.03528
4.70
.0*9*0
7.00
4.40
DEM PT.F=
51.
S I.N T,F= 300.0
298
29.6
208.7
202.0
-.1740.0
59.0
135.*
643.0
1093.0
7.89
.009*
258.0
.0095
.139
.078
99.825
f REDUCED
1.98
3.14
811.1

56.8
5.754
1.48*

7.8
.451
.116
.078*

41.7
6.932
1.789

14.3
2.377
.613

56.0
9.310
2.402

.00704
3.50
.02112
10.50
.03519
16.30
.04918
18.60
12.40
299
69.4
489.9
475.6
41750.0
62.0
142.5
654.0
1300.0
7.86
.0128
350.0
.0128
.188
.070
99.950
FUEL* AV. KERO. TEST NO.' 15
REL HUM=
FLO.L/HI
300
89.4
631.
611.
41730.
61.
147.
659.
1404.
7.85
.0146
400.0
.1148
.218
.065
99.964
70.00 SPEC HUN= .007500
14.160 SL TIM,S» 6.5000
311
99.3
708.9
680.3
41730.0
62.0
148.8
663.0
1480.0
7.82
.0159
431.1
.0161
.234
.063
99.971

2.70
3.15
1102.9

20.2
1.505
.527

3.9
.166
.058
.1101

76.0
9.280
3.248

9.3
1.130
.395

85.2
10.410
3.643

.00705
7.00
.02115
12.80
.03531
19.80
.04944
23.30
15.80
3.12
3.15
1260.8

17.0
1.093
.437

3.3
.121

.1108

93.0
9.809
3.924

8.0
.844
.338

101.0
10.653
4.261

.01709
4.70
.02126
11.60
.03544
16.30
.04962
20.90
13.50
3.36
3.15
1358.7 	 	 	

13.4
.800
.345

3.3
.113
.048


102.5
10.042
4.320

5.0
.490
.211

1B7.5""
10.532


.00710
7.00
.02131
11.60
.03557 . 	
16.30
.04981
18.60 . .. . .
13.40
                     NOTES 1. ALL  EMISSIONS CONCENTRATIONS ASE  HET VALUES.
                           2.EQUIVALENCE RATIO CALCULATED  FROM  C02,CO,ANO HC DATA AND FUEL
                           3.MASS  EMISSIONS OF NO, N02.  AND NO»N02 CALCULATED AS N02 FROM
 COMPOSITION.
CONCENTRATIONS HITH
                                                                                                                 MOLECULAR HEIGHT OF N02 «*6.01>.
-------
13
(D

N)
00
NO
                   .............................................   AIRESEARCH  EMISSION TEST SUMMARY  ••••••»•»•••••
                   ENG HFG  I  AIRESEARCH           TEST FACIL  I PHX  LACC2   INSTR OESCRIP I  FED REG V38 N136
                   MODEL NO. I      TPE331-5-251M     S/NI   P04001               ENGINE TYPEICLASSM  TURBOPROP
                   RATED POHERt     706.0  SHP AT SEA LEVEL STANDARD  DAY CONDITIONS
                   FUEL I ASTM  D1655-73            ATOMIC H/C  RATIOI    1.928      LHVI  18470. BTU/L8     ADDITIVES!
 CALC DATE 111-3-75
 CALC IDI    2
TEST HOI    15
                                                                                                                     NONE
                    ........  EXHAUST EMISSIONS PER EPA CYCLE OF  WORK  OUTPUT  *»  CODE  OF  FEDERAL REGULATIONS TITLE 40 PART 87  17 JULY 1973   »»••••»
                                        HYDROCARBONS (CH AS CH4)           3.762 LB.  POLLUTANT PtR 1000 HP.-HR. PER CYCLE
                                        CARBON MONOXIDE ICO)             19.025 LB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                        OXICES OF NITROGEN  (NOX  AS N02)    8.794 LB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                        SMOKE                              18.5   SMOKE NUMBER, MAXIMUM AT  CRUISE    MODE,  70 PERCENT RATED POWER
                    TAXI-IDLE SETTING. 5.0      PERCENT RATED TAKEOFF POWER  AT  65.       PERCENT RATED TAKEOFF Nl RPM
                    ......................,......,T.....................  ENGINE  DESCRIPTION  ••»•••••••»»•••••••»••••»••••••»•••••»»•••••••••»•••
                    COM3  TYPEI  REVERSE FLOW ANNULAR           P/N<    869082-4            SUR/VOLI 1.Z60  FUEL INJ TYPE.  STAGED SIMPLEX
                    ENGINE  TOTAL SERVICE!  0.0       HR    TIME SINCE ENGINE OVERHAUL!   0.0       HR                   .       	   	  ._ .
                    ENGINE  ASSEMBLY AND MAINTENANCE INFORMATION!
                    AIRCRAFT  INSTALLATION «*• MFR.I                                  MODEL NO.t
                                               USER:                        ENGIN£ INSTALLATION POSITION!
                    ...............................,................Qpt^ATIONAL  T£ST DATA SUMMARY »»»»»»»»»••»»»•»••»»»»»»•»»••»•»••»•»»»•»»•»»»»»
                    GASEOUS EMISSION TEST NO. I    15        DATE! 11-3-75       .     TIME!                    BARO PRESS.!  Z8.660  IN.  HGA.
                    AMBIENT AIR TEMP.!  59.00 DEC. F        RELATIVE  HUMIDITY:   70.00 PERCENT       SPECIFIC HUMIDITY:  .007500 LB.  HZO/LB.  DRY »IR
                    AMBIENT AIR QUALITY    HYDROCARBONS  IHCII 0.0   PPMC     CARBON MONOXIDE (CO): 0.0   PPMV    OXIDES OF NITROGEN (NOX)I  D.O    PPMV
                    SAMPLE  LINE '" TEMP.I  300.00 DEC.  F.     FLOHRATE:    14.16  LITERS/HIM.     TRANSPORT TIME!    6.50  SEC.     LENGTH!    50.00 FT.
tESt CONDITION
ACTUAL POWER SETTING, HORSEPOWER
CORR. PCHE1 SETTING ISTO DAYI , PERCENT RATED
Nl SPEED, RPM
FUEL FLCW INEAS.) LB./HR.
CORR. ENGINE CORE AIRFLOW (MEAS) , IB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., OES F
COMPRESSOR INLET AIR TOTAL PRESS*, PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTAL TEMP., OEG F
TURBINE INTERSTAGE GAS TOTAL TEHP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EKISSICN CONCENTRATION, WET ANALYSIS
HYDROCARBON IHC AS CH4) , PPMC
CARBON MONOXIDE ICOI , PPMV
TOTAL OXIDES OF NITROGEN (NOXI, PPMV
CARBON DIOXIDE (COZ) , PERCENT BY VOL.
NITRIC OXIDE (NO), PPMV
EMISSION INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS IHC AS CH4)
CARBON MONOXIDE (COI
TOTAL OXIDES OF NITROGEN CNOX AS NOZI
EMISSION RATE. LB. POLLUTANT/HR.
HYDROCARBONS IHC AS CH4I
CARBON MONOXIDE {COI
TOTAL OXIDES OF NITROGEN IMOX AS NOZI
COMBUSTION EFFICIENCY. PERCENT (EMISSIONS)
F/A IEMISSIONS.CALC)
30Z 303 301,
33.6
4.94
27520.00
116.0
3.0
57.00
14. 14
46.47
319.00
175.0
11,. 17

81.000
215.693
21.000
Z.OOO
14.700

4.579
21.331
3.411

.531
Z.l. 7*
.396
99.10
.0097
50.8
7.44
2751.0.00
116.0
Z.9
61.00
14.18
46.87
324.00
9<>I.O
11,. 17

1,3.500
187.620
25.000
2.218
19.100

2.227
16.621
3.676

.258
1.951
.4Z7
99.1,1
.0107
67.1
9.60
27510.00
130.0
z.a
63.00
It. 18
1.9.56
325.00
1011.0
Id. 17

31.. 501
176.1.20
27.800
2.1.1.7
22.500

1.601.
14.349
3.711.

.209
1.665
.1,83
99.52
.0116
305
207.2
30.1.6
1.1760.00
260.0
7.9
57.00
I*. 18
136.05
639.00
1098.0
11.. 07

6.000
58.91.1
53.800
2.000
1,1.000

.3V3
5.896
8.81.1

.069
1.533
2.299
99.63
.0096
306
<.77.6
70.15
1.1770.00
352.0
7.9
58.00
14.18
11.3.1.2
651.00
1318.0
14.08

.600
23.690
85.000
2.696
77.500

.025
1.776
10.379

.009
.625
3.653
99.96
, .0126
307
610.5
89.1,1
1,1700.00
40Z.O
7.6
61.00
14.16
146.37
657.00
1369.0
14. 1Z

.601
19.446
102.500
3.177
96.000

.022
1.253
11.631

.009
.504
4.Z74
99.97
.0151
30 •
679.4 	 	 	 	
99.41
41750.00
_ 4Z5.5 	 	 	 .
7.B
62.00
14. IB
147.64
661. Ot
1450.0 _ ._ 	 __
14.13

.*••
19.442
114.500
3.426 	
106.251

.. .020 -_. . 	 	
1.139
11.015
_ 	 	 .-
.009
.484
4.667 ......
99.97
.0162
                                                                                                                                                                  y
               J
-------
 TJ
 JU
iQ
 (D
00
CO
                      ..........................................   £P4  crCuE EMISSIONS COMPUTATION SUMMARY  •••»••»»••
                      ENG MFG I AIRESEARCH           TEST  FACIL  I  PHX  LACC2  INSTR DESCRIP I FED REG V38 N136
                      MODEL NO.I     TPE331-5-251H     S/NI    P04001              ENGINE TYPE(CLASS)!  TURBOPROP
                      RATED POMERt    706.0 SHP AT SEA LEVEL  STANDARD  DAY  CONDI IIONS
                      FUEL I ASTM 01655-73            ATOMIC H/C  RATIOI   1.928     LHVI 181,70. BTU/LB     ADDITIVES!
                                                                                      NONE
                                                                                           CALC DATE 111-3-75
                                                                                           CALC IDI    2
                                                                                          TEST HOI    IS
H 0 0 E
TIME IN HODE, HIMUTES
RATED POWER. PERCENT
CORRtCTEO POWER. HORSEPONER
HP-HR
FUEL FLCNt LB/HR
FUEL MASS. LB
•• HYDROCARBON EMISSION (HC) «•
INDEX, LB HC/1000 LB FUEL
RATE. L8 HC/HR
NASS, LB HC
MASS. PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HCRSEPOKER-HR PER CYCLE
" CARBON MONOXIDE EMISSIONS ICO) ••
INDEX, LB CO/1008 LB FUEL
RATE, L8 CO/HR
MASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORSEPOHER-MR PER CYCLE
«» TOTAL OXIDES OF NITROGEN EMISSIONS CMOKl"*
INDEX, LB NOX/1000 LB FUEL
RATE, LB NOX/HR
MASS, LB NOX
MASS, PERCENT OF TOTAL CYCLE
CYC-E. LB NOX/1000 HORSEPOMER-HR PER CYCLE
TAXI-IDLE
(IN)
7.000
5.000
35.300
».118
115.775
13.507

».5fl6
.522
.061
25.5


21 . 215
2.456
.287
£3.7

»
3.»22
.396
.01,6
8.3

TAXI-IDLE
(OUT)
19.000
5.000
35.300
11.170
115.775
36.662

<>. 506
.522
.165
69.1


21.215
3.456
.77»
6<>.3


3.422
.396
.125
22.5

APPROACH
<>.500
30.000
211. aoo
15.885
260.<,51
19.531,

.511
.133
.010
4.2


6.2**
1.626
.122
10.1

. . .
8.619
2.21,5
.168
30.1

CLIMBOUT
2.500
90.801
635.i>00
26.475
1,00.260
16.677

.115
.0<>6
.002
.8


".986
.395
.016
1.1,

.._
10.785
<>.317
.180
32.2.

TAKEOFF
.500
100.001
706.000
5.883
1,31,. 122
3.618

.30%
.132
.001
.5


1.67*
.727
.006
.5


10.752
4.660
.039
7.0

TOTAL PER
CYCLE
33.500


63.5*0

•9.99*

2.656
.*28
.239
100.0
3.762

13.02
2.165
1.209
100.1
19.02$

6.209
1.001
.559
101. 1
•.79* _
                                            " EMISSION INDEX LEVELS REQUIRED TO MEET EPA 1979 STANDARDS FOR CLASS P2  ENGINES •*
                                         EPA LTO-CYCLE
                                                                                                  REQUIRED EMISSION  INDEX,  LBP/1000  LB FUEL
POLLUTANT
   CO
   NC
   NOX
                                              L8P/100B  HORSEPOHER-HR-CYCLE
                                                     26. 8
POLLUTANT (MODE)
   CO (IDLE)
   HC (IDLE)
   NOX (TAKEOFF!
   A
21.2
 4.5
10.8
   B
31.1
 5.9
23.6
                                            A  ASSUMES  PROPORTIONAL REDUCTION OF  POLLUTANT EMISSION INDEX AT EACH LTD CYCLE NODE

                                            B  ASSUMES  (II  REQUIRED REDUCTION IN  CO  AND HC OBTAINED BY LOWERING EMISSION  INDEX  VALUES
                                               AT TAXI-IDLE MODE ONLY, CO AND HC  EMISSIONS AT OTHER NODES REMAIN UNCHANGED, (21 REQUIRED
                                               REDUCTION IN NOX OBTAINED BY LONctlNG EMISSION INDEX VALUES AT CLIMBOUT  AND TAKEOFF  MOOES IN
                                               SAMc. PROPORTION AS MEASURED VALUES, NOX EMISSIONS AT TAXI-IDLE AND APPROACH MODES
                                               REMAIN UNCHANGED
-------
(D

10
00
•:> 	
?
ENGINE' TPE331-5-Z51M 3/N= P04001
RAT SHP= 706. RA EGT,F=
FUEL H/C* 1.9280 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POWER
CORRECTED SHAFT HP
MEASURED SHAFT HP
1 SHAFT SFEED. Nl , RPM
COMPRESSOR INLET TEMP., OEG.F
COMPRESSOR OSCHG. PRES..PSIA
) COMPRESSOR OSCHG. TEHP.OEG F
TURB INTERSTAGE TEMP., OEG.F
CORR BELHTH FLOH, LB/SEC
FA RATIO BASED ON BEcLMTH.
MEASURED FUEL FLOM, L3/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOA3ING H/P»»N/V/E(T/54D)
COMB EFFIC FROM EMISSIONS
PAP RDM nTOX TI1F
(« AKOUfl UXUAXUC.
PERCENT BY VOLUME, MET
: LB. COZ PER L8. OF FUEL
MEIGHT FLOH, LB./HR.
CARBON MONOXIDE
i PPH BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNEO HYDROCARBONS- PPH AS

ri*n OT vuLunt, wti
LB. PER 1000 L3. OF FUEL
HEIGHT FLOM, LB./HR.
RATIO LB HC/LB CO
1650.
.06822
302
4.9
34.9
33.6
27520.0
57.0
48.4
319.0
8TS.O
Z.97
.011Z
116.0
.0097
.142
.319
99.097
COM3 P/N= 869082-4
RAT SPO=
L H V=
303
7.4
52. S
50.8
27540.0
61.0
48.9
324.0
9".3.0
Z.90
.0115
116.0
.0107
.157
.307
99.409
41730.
18470.
304
9.8
69. Z
67.1
27510.0
63.0
19.6
325.0
1011.0
2.85
.0132
130.0
.0118
.172
.294
99.522
DEW PT.F* 51.
S LN T.F*
305
30.5
215.0
207.2
-.1760.0
57.0
136.1
639.0
1099.0
7.92
.0094
260.0
.0096
.140
.078
99.831

2.00
3.11
360.5

215.7
21.331
2.474
2.22
3.12
362.1

187. S
16.821
1.951
CARBON, HEIGHTS AS
HI II
91. u
4.579
.531
91 J.&
NITRIC OXIDE INOI - HEIGHTS AS NOZ
PPH BY VOLUME, MET

LB« PER 1000 LB* OF FUEL
HEIGHT FLOM, LB./HR.
/ NITROGEN DIOXIDE (N02I
PPM BY VOLUME. MET
LB. PER 1000 LB. OF FUEL
) HEIGHT FLOH, LB./HR.
TOTAL OX IDES OF NITROGEN IN C+
PPH BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
i CORRECTED MEIGHT FLOH
SMOKE NUMBER
CORRECTED MEIGHT FLOM
) SMOKE NUMBER
CORRECTED MEIGHT FLOH
SMOKE NUMBER
) CORRECTED HEIGHT FLOM
SMOKE NUMBER
SMOKE NUMBER AT HA«0. 023
14.7
2 388


6.3
1.023
.119
21.0
3.411
.396

.01705
4.70
.02114
4.70
.03529
7.00
. 04941
9.30
6.48
) NOTES 1. ALL EMISSIONS CONCENTRATIONS ARE
43. 5
2.227
.258
.1324

19.1
2 .810
.326

5.9
.868
.101
25.0
3.678
.427

.00710
2.30
.02129
5.80
.'03548
7.00
,04967
9.30
6.10
2.45
3.13
406.5

176.4
14.349
1.865
CH4
34.5
1.604
.209
.1118

22.5
3.006
.391

5.3
.708
.092
27.8
3.714
.483

.00707
5.80
.02121
7.00
.03542
5.80
.04959
8.10
6.70
2.00
3.14
817.4

58.9
5.896
1.533

6.0
.343
.089
.0582

41.0
6.737
1.752

12.8
2.103
.547
53.8
8.841
2. 299

.00708
7.00
.OZ124
10.50
.03539
17.40
.04955
22.10
14.40
300.0
306
70.1
495. Z
477.6
1.1770.0
58.0
143.4
651.0
1318.0
7.87
.0129
352.0
.0128
.188
.069
FU£L= AV. KERO. TEST N0.= 15 A
REL HUMS
FLO,L/M=
307
89.4
631.2
610.5
41700.0
61.0
146.4
657.0
1389.0
7.84
.0148
402.0
.0151
.221
.066
99.956 99.969
70.00 SPEC HUM' .OflrSQI 1
14.160 SL TIM.S* 6.5000 1
308
99.4
701.8
679.4
41750.0
62.8 .
147.8
661.0
1450.0 .
7.81
.0157
425.5 	
.0162
.238
.064
99.971
^




.


•\
1

..
'




1

2.70
3.15
1109. Z

Z3.9
1.776
.625

.6
.825
.009
.0144

77.S
9.463
3.331

7.5
.916
.322
85.0
10.379
3.653

.00708
8.10
.02124
15.10
.03539
23.30
.04955
26.70
18.50
3.16
3.15
1267.1

19.8
1.253
.504

.6
.822
.009
.0173

96.0
9.957
4.003

6.5
.674
.271
102.5"
10.631
4.274

.00708
8.10
.02124
15.10
.03539
19.88
.04955
23.38
16.78
3.43
3.15
1341.3 	 _... ... 	 ......

19.4
1.139 . ......... 	
.484


.020
.009
.8176 . .'__ ._ 	 . .. 	 	 :

186.3
10.221 , .......
4.349

8.2. 	 	 . 	 .. — _ - 	 -
.794
.338
114.5
11.015
4.687 	 . ___. 	 	

.00708
8.18. ._ 	 	
.02124
11.68
.03539 ... ..
16.38
.04955
22.18 . 	 .. 	 - - ...
14.68
A
J

•^
'

»
*




\
f '.


' ;

)'
..
\ :
) -

\
J

\
J

\


\
MET VALUES. '
2.EQUIWALENCE RATIO CALCULATED FROM C02.CO.ANO HC DAT*
3. MASS EMISSIONS OF NO, NOZ, A NO NO'NOZ CALCULATED AS
J



AND FUEL COMPOSITION.
HOZ FROM CONCENTRATIONS MITH



MOLECULAR HEIGHT OF NO2 (46.01).


-^
-------
  .
tt>

NJ
00
Ul
                      ....,......*..........,,,....................  AIRESEARCH EMISSION  TEST SUMMARY  •»»»»••••»•••«
                      ENS MFC I AIRLSEARCH            TEST FACIL I PHX LACCZ  INSTR  OESCRIP  I  FED REG V38 N136
                      MODEL NO.I     TPE331-5-251M      S/NI   POV001              ENGINE  TYPEICLASS)I  TURBOPROP
                      RATED FCMERI    706.0  SHP  AT  SEA LEVEL STANDARD DAY CONDITIONS
                      FUEL! ASTM 01655-73             ATOMIC H/C RATIOI   1.928      LHY1 1BV70. BTU/LB     ADDITIVESI
 C*LC DATE «ll-*-75
 CALC IDI    3
TEST NOI   15
K
                                                                                                                        NONE
                      »»•»•••» EXHAUST EMISSIONS  PER EPA CYCLE OF HOR« OUTPUT •*  CODE  OF  FEDERAL REGULATIONS TITLE «.fl PART »7  17 JULY  1973   •••»»••
                                          HYDROCARBONS CCH AS CH-,1          3.338 '-8.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                          CARBON  MONOXIDE ICO)             18.105 LB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                          OXIDES  OF  NITROGEN (NOX AS N02)   9.Z9V LB.  POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                          SMOKE                              17.9  SMOKE NUMBER, MAXIMUM AT  CRUISE    MODE,  70 PERCENT  RATED POWER
                      TAXI-IDLE SETTIN61 5.0       PERCENT RATED TAKEOFF POKER AT  65.       PERCENT  RATED TAK50FF Nl RPM
                      ....,.,,......,..»„.„......,.....,....,...•........  ENGINE  DESCRIPTION  »•••••»•»•»••••»»•••••»••••••••••••••••»»••••»••••••
                      COM3 TYPEJ REVERSE FLOW ANNULAR           P/N1   869083-1.            SUR/VOLt  1.260  FUEL INJ TYPEI  STAGED SIMPLEX
                      ENGINE TOTAL SERVICE!  0.0        HR    TIME SINCE ENGINE OVERHAULI   0.0        MR              	,...  ......_._
                      ENGINE ASSEMBLY AND MAINTENANCE INFORMATION!
                      AIRCRAFT INSTALLATION •••• MFR.«                                   MODEL NO.I
                                                 USERI                        ENGINE INSTALLATION POSITIONI                            .            	
                      .........,..............,..,...............»».»»OPERATIONAL TEST  DATA  SUMMARY ••••»•••»••••*•»••••••»•••••»*•••»»«••»••••«»•••
                      GASEOUS EMISSION TEST NO. »    15         OATE4 ll-V-75             TIMfl                     BAHO PRESS. I  28.8VO IN. HGA.
                      AMBIENT AIR TEMP.I  59.00 OEG.  F         RELATIVE HUMIOITYI  70.00 PERCENT       SPECIFIC HUMIDITY!  .007500 L8. HZO/LB. DRY AIR .
                      AMBIENT AIR QUALITY    HYDROCARBONS CHCI I 0.0   PPNC     CARBJN MONOXIDE (COI I 0.0   PPMV    OXIDES OF NITROGEN INOXII 091   PPMV
                      SAMPLE LINE •»• TEMP.I  300.00  OEG. F.     FLOHRATEI   1W.16  LITERS/MIN.     TRANSPORT TIME!    6.50 SEC.     LENGTH!   50.01 FT.
TEST CONDITION
ACTUAL POWER SETTING, HORSEPOWER
CORR. POWER SETTING >
CARBON MONOXIDE ICOI
TOTAL OXIDES OF NITROGEN INOX AS NOZ)
COMBUSTION EFFICIENCY, PERCENT IEMISSIONSI
F/A (EMISSIONS, CALO
309 310 311
31.7
It. (,3
Z75i)0.00
108.0
3.1
61.00
11.. 17
1.8.87
322.00
865.0
It. 15

83.100
Z15.Z2Z
23.200
1.968
17.100

",.773
21.626
3.830

.515
2.336
.1.11,
99.07
.0095
50.3
7.1.0
Z7530.00
119.0
2.9
58.00
11,. 17
1.9.12
320.00
938.0
li.. 15

1.5.000
190.111.
25.200
2.170
19.700

2.351.
17.396
3.786

.280
2.070
.1.51
99.38
.0105
70.0
10.31
Z7570.00
131.0
2.9
57.00
IV. 17
1,9.71
321.00
1012.0
li». 15

3i>. 500
170.967
29.500
Z.i, 1,7
21.. 1.00

1.601,
13.910
3.91.2

.210
1.822
.516
99.53
.0118
312
Z02.Z
Z9.77
1,1730.00
262.5
7.9
57.00
I*. 17
135.81
61.0.00
1066.0
1">.05

6. tOO
63.131.
5k. 500
1.963
1.0.900

.31.9
6.1,33
9.122

.092
1.689
2.391.
99.82
.0091,
313
1.76.1
70.03
1,1730.00
358.5
7.9
58.00
IV. 17
Ifc3.17
650.00
1260.0
IV. 06

.600
30.399
82.500
2.687
79.000

.026
2.268
10.112

.009
.613
3.625
99.9%
.0128
311.
606.0
89.1.3
1.171.0.00
1.05.0
7.9
58.00
IV. 17
1V7.35
655.00
1350.0
1V.09

.690
19.8V6
102.750
3.060
98.7SO

.022
1.301
11.061,

.009
.527
V.V81
99.97
.01V5
315
678.6
99.81
1.1730.00
1,31.0
7.9
58.00
I*. I/
1 V9. 31
657.00
1380.0
IV. 11

.600
15.821
110.000
3.356
102.500

.020
.9V5
10.797

.019
.V07
(,.653
99.98 .
.1159
-------
00
en
                  •»»•»»«»»»»»»»•••»•••»«»«•»»••»»»»»»»»»»,.  £PA CYCLE EMISSIONS COMPUTATION SUMMARY  »••»»»»»•«
                  ENG MFC I AIRESEARCH            TEST FACIL « PHX LACC2  INSTR OESCRIP  « FED REG V38 N136
                  MODEL NO.I     TPE331-5-251M     S/NI    POtOOl              ENGINE TYPE(CLASS) I  TURBOPROP
                  RATED POWER I     706.0 SHP  AT SEA  LEVEL STANDARD DAY CONDITIONS
                  FUEL* ASTM D16S5-73             ATOMIC  H/C RATIOI   1.928     LHVI 181.70. BTU/LB     ADDITIVES!
                                                                                           CALC  DATE lll-i»-75
                                                                                           CALC  101     3
                                                                                          TEST NO!    15
                                                                                                                    NONE
MODE
TINE IN NODE, MINUTES
RATED POWER, PERCENT
CORRECTED POWER, HORSEPOWER
HP-HR
FUEL FLCW, LB/HR
FUEL MASS, LB
•• HYDROCARBON EMISSION IHCI ••
INDEX, LB HC/1000 LB FUEL
RATE, LB HC/HR
HASS, LB HC
NASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORSEPOHER-HR PER CYCLE
" CARBON MONOXIDE EMISSIONS (CO) »•
INDEX, LB CO/100 > LB FUEL
RATE, LB CO/MR
MASS, LB CO
HASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORSEPOHER-HR PER CYCLE
•» TOTAL OXIDES OF NITROGEN EMISSIONS INOX) »•
INDEX, LB NOX/1000 LB FUEL
RATE, LB NOX/HR
NASS, LB NOX
NASS, PERCENT OF TOTAL CYCLE
CYCuE, LB NOX/1000 HORSEPOHER-HR PER CYCLE
TAXI-IDLE
(INI
7.000
s.ooo
35.300
14.118
109.'. if 5
12.769

k.321
.1*73
.055
26.0 _


21.026
2.301
.268
23.3

	 — -
3.821
.<,!»
.049
8.3

TAXI-IDLE
(OUT)
19.000
5.000
35.300
11.178
109.1,1,5
3<>.65«

18
.132
22. *

APPROACH
<>.SOO
30.000
211.800
15.185
26li.358
19.827

.302
.080
.006
2,8


6.26
.182
30.8

CLIHBOUT
2.500
90.000
635. tOO
26.1,75
-------
0)

to
CO
-J
ENGINE^ TPE331-5-251M S/N* Pll.001
RAT SHP= 706. RA EGT,F=
FUEL H/C» 1.92(0 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POKER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Nl, RPM
COMPRESSOR INLET TEMP., DEC. F
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR DSCHG. TEMP,OEG F
TUR3 INTERSTAGE TEMP., CE6.F
CORR BELMTH FLOH, LB/SEC
FA RATIO BASED ON 8ELLMTH.
MEASURED FUEL FLOH, LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING W/P»»N/V/EIT/5dfl)
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
LB. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME. HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH. LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIOE (NO) - HEIGHTS AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE (N02)
PPM BY VOLUME. HET
LB. PER lOOt LB. OF FUEL
HEIGHT FLOH, LB./HR.
1650.
.06822
309
d.6
32.6
31.7
27580.0
61.0
1,8.9
322.0
865.0
3. 96
.0102
108.0
.0095
.mo
.325
99.073

1.97
3.11
335.6

215.2
21.628
2.336
[RESEARCH EMISSION TEST SUMMARY
COMB P/N* 869082-1,
RAT SPO= 1,1730.
L H V= 18U70.
310
7.1,
52.2
50.3
27530.0
58.0
H9.1
320.0
938.0
2.92
.0117
119.0
.0105
.153
.310
99.381,

2.17
3.12
371.3

190.1
17.398
2.070
CARBON, HEIGHTS AS
83.1
l». 773
.515
.2207
N02
17.1
2.823
.305

6.1
1.007
.109
1,5.0
2.351,
.280
.1353

19.7
2.961
.352

5.5
.827
.098
311
10.3
72.8
70.0
27570.0
57.0
1.9.7
321.0
1012.0
2.86
.0132
131.0
.0118
.172
.297
99.532

2.1,5
3.13
1,09.7

171.0
13.910
1.822
CHd
3d. 5
1.601,
.210
.1153

21,.!,
3.261
.1,27

5.1
.682
.089
DEM PT,F=
= 51.
S LN 1,f* 300.0
312
29. 8
210.2
202.2
1,1730.0
57.0
135.6
fc 1.0.0
1066.0
7.90
.0096
262.5
.0091.
.138
.078
49.818
RcDUCcO
1.96
3.11.
825.0

63.1
6.1,33
1.689

6.0
.31.9
.092
.051.3

1,0.6
6.795
1.781,

13.9
2.327
.611
313
70.0
d9i,.d
1.76.1
1.1730.0
58.0
11.3.3
650.0
1260.0
7.90
.0131
358.5
.0126
.168
.070
99.9dd
FUEL' AV. KERO. TEST NO.= 15
REi. HUN=
FLO,L/M=
31d
69. d
631. d
606.0
dl7dO.O
58.0
11.7.3
655.0
1350.0
7.67
.011.8
1.05.0
.011.5
.213
.066
99.967
70.00 SPEC HUM* .007501
Id. 160 SL TIH,S= 6.5000
315
99.6
70i>. 7
676.6
d!730.«
56.1
Id9.3
657.1
1360. B
7.67
.0156
1.31.0
.0159
.23d
.06d
99.976

2.69
3.15
1129. d

30. d
2.266
.613

.6
.026
.009
.0113

79.0
9.683
3.1.71

3.5
.1.29
.15d
3.06
3.15
1276.5

19.6
. 1.311
.527

.6
.022
.009
.0171

96.8
10.633
i>. 306

d.O
.1,31

TOTAL OXIOES OF NITROGEN INO+N02I AS N02
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLCH
SMOKE NUMBER
CORRECTED HEIGHT FLCH
SMOKE NUMBER
SMOKE NUMBER AT HA=0.023
23.2
3.830
.did

.00720
5.80
.02160
8.10
.03593
8.10
.05030
9.30
7.80
25.2
3.788
.1.51

.00717
3.50
.02152
7.00
.03586
7.00
.05021
9.30
6.70
29.5
3.91,2
.516

.00717
5.60
.02152
8.10
.03586
5.80
.05021
9.30
7.30
Sd.5
9.122
Z.39d

.00713
5.80
.02136
12.80
.03570
16.30
.01,996
19.80
13.70
82.5
10.112
3.625

.00715
8.10
.021d6
12.80
.03577
22.10
.05007
27.90
17.80
102.7
11.061.
d.d81

.00701
6.10
.02101
Id. 10
.03501
20.90
.Od901
2d.dO
17.10
3.36
3.15
1358.7

15.6
.9d5
.1,07

.6
.121
.009
.0217 . 	

102.5
10.061
d.336

7.5
.736
.317

" 110.8
10.797
d.6SJ _... 	

.00691,
6.10
.02062
Id. 01
.031.70
18.60
.01.858
19.80
15.30
                                                                                                                                                                     1)
                        NOTES  1.  ALL EMISSIONS CONCENTRATIONS  ARE HET VALUES.
                              2.EQUIVALENCE RATIO CALCULATED FROM C02,CO,ANO HC DATA AND FUEL COMPOSITION.

                              3.MASS EMISSIONS OF NO. NO2,  AND  NO+N02 CALCU-ATEO AS N02 FROM CONCENTRATIONS HITH
                                                                                                                  MOLECULAR HEIGHT OF N02 (1,6.011.
-------
                                                                                                                                                                           f?
                              -«.   .T „„   """"«•••"•••"•»••••••  AIRESEARCH EMISSION  TEST  SUMMARY  •••••••••
                              MF6 I AIRESEARCH           TEST  FACIL » PHX LACCZ  INSTR OESCRIP  I FED  REG VSt N136
                              n  S'r=    TPE331-S-ZS1H     S/N«    POfcOOl              ENGINE  TYPE(CLASSII  TUR80PROP
                          RATED POMERI     7D6.0  SHP AT SEA LEVEL  STANDARD DAY CONDITIONS
                          FUELI ASTM D16SS-73             ATONIC H/C RATIO!   1.928     LHVI 18<,70.  BTU/LB
                                                                                                                 ADOITIVESI  NONE
                                                                                                         CALC DATE 111-8-75
                                                                                                         CALC IDI  1
                                                                                                        TEST NOI  16
                                   EXHAUST  EMISSIONS PER EPA CYCLc OF HORK OUTPUT *» CODE OF  FEDERAL  REGULATIONS TITLE 1,0 PART  87   17  JULY 1973  "••»»»
                                               HYDROCARBONS CCH AS  CHI.I           5.19". L8. POLLUTANT PER 1000 HP.-HR. P£R CYCLE
                                               CARBON MONOXIDE «CO)              19.01.9 LB. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                               OXIDES OF NITROGEN  (NOX AS NOZI    5.173 LB. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                          TAXT-inir <:crTTT«c> EH"*    o-o,.,- T ,.»^               15tZ  SHOKE NUMBER« MAXIMUM AT  CRUISE    MODE.  7>, PPMC
CARBON MONOXIDE (CO), PPMV
TOTAL OXIDES OF NITROGEN (NOX), PPMV
CARBON DIOXIDE (COZ), PERCENT BY VOL.
NITRIC OXIDE (NOI, PPMV
EMISSIOK INDEX, LB. POLLUTANT/1000 LB. FUEL
HYDROCARBONS (HC AS CH<>>
CAKBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
EMISSION RATE, LB. POLLUTANT/HR.
HYDROCARBONS (HC AS CHI.)
) CARBON MONOXIDE (CO)
TOTAL OXIDES OF NITROGEN (NOX AS N02)
COMBUSTION EFFICIENCY, PERCENT (EMISSIONS)
) F/A (EMISSIONS, CALC)
11-8-75 . TIMEI
HUMIDITY! .on7s;nn in. w?n/in. no» >TO
IRATEI H..16 LITERS/MIN. TRANSPORT TIME! 6. 50 SEC.
316 317 318
23.2 31.. 3 1,6.5
1..99 7.36 9.99
27560.90
74.. 0
3.0
58.00
9.67
33.61,
315.00
911.. 0
-0.10
171.. 000
3Z0.163
18.200
Z.056
13.800
9.1,82
30.521)
2.850
.702
2.259
.211
98.1.5
.0100
27550.00
2.8
63.00
9.67
33.61.
322.00
995.0
9.67
117.000
Z84.38*
22.600
2.376
18.700
5.556
23.626
3.084,
.1.67
1.985
.259
98.96
.0115
27550.00
90.0
2.8
60.00
9.67
33.89
322.00
1060.0
9.67
90.000
2*. 600
2.602
21.700
3.918
18.616
3.070
.353
1.675
.277
99.22
.0125
319
11.0.1
30.18
1.171,0.00
187.0
7. 7
58.00
9.67
92.31,
61,3.00
1120. 0
9.56
3Z.700
153. 9»0
i>9.500
Z.117
29.500
1.756
11,. 1,66
7.61.1
.328
2.705
1.1,29
99.51
.0102
320
325.1
69.93
1.1720.00
•251.0
7.6
59.00
9.67
96.76
656.00
1225.0
9.59
5.1.00
67.339
77.000
2.862
65.500
.216
0.050
.054)
1.183
2.221
99.87
.0136
321
1.18.1.
90.01
<»17i,0.00
286.0
7C
• O
59.00
9.67
99.1.6
663.00
1320.0
9.61
3.000
36.952
90.000
3.297
8*. 250

2 .21, 7
0.990
.030
.61.3
2.571
.0157
LENGTH! 50.00 FT
322
1.61.. 9
100.00
1.171.0.00
315.0
7t
• D
59.00
9.67
100.93
668.00
9.61
2.1.08
31.216
98.750
3.513
96.250
fl 7ft
_*•"•
1.702
9.259

1 561
2.917
99*95
.0167
                                                                                                                                                                          y-
-------
0)
iQ
(D

N)
00
                      ...,........*.,....*......,..,............   £PA CYC_E  EMISSIONS  COMPUTATION SUMMARY  •»•»»«»••«
                      ENG NFG t  AIRESEARCH           TEST FACIL  I  PHX LACC2   INSTR OESC3IP I  FED REG  V38 N136
                      MODEL NO.J     TPE331-5-251M     S/N<   P04001               ENGINE  TYPE(CLASS)»  TURBOPROP
                      RATED POWER I     706.0 SHP AT SEA LEVEL  STANDARD OAT CONDITIONS
                      FUEL* ASTN 01655-73            ATOMIC H/C  RATIO:   1.938      _HV1  18470.  BTU/LB     ADDITIVES!
                          CALC DATE lll-B-75
                          CALC IDI  1
                         TEST NOI  16
                                      1)
                                                                                                                       NONE
MODE
TIME IN MODE, MINUTES
RATED POWER, PERCENT
CORRECTED POWER, HORSEPOWER
HP-HR
FUEL FLOW, LB/HR
FUEL MASS, LB
•» HYDROCARBON EMISSION (MCI "
INDEX, LB HC/1000 L8 FUEL
RATE, LB HC/HR
MASS, LB HC
NASS, PERCENT OF TOTAL CYCLE
CYC^E, LB HC/1000 HORSEPOWER-HR PER CYCLE
*» CARBON MONOXIDE EMISSIONS «CO> •» ' . . . .
INDEX, LB CO/1000 LB FUEL
RATE, LB CO/HR
NASS, L6 CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORSEPOWER-MR PER CYCLE
" TOTAL OXIDES OF NITROGEN EMISSIONS INOX) ••
INDEX, LB NOX/1000 LB FUEL
RATE, L6 NOX/HR
MASS, LB NOX
NASS, PERCENT OF TOTAL CYCLE
CYC..E, LB NOX/1000 HORSEPOHER-HR PER CYCLE
TAXI-IDuE
UN)
7.000
5.000
35.300
4.118
74.036
8.640

9.457
.700
.082
24. 6


30.487
Z.Z58
.263
21.8


2.85Z
.211
.025
7.5

TAXI-IDLE
(OUTI
19.000
5.000
35.300
11.178
74.056
23.451

9.457
.700
.222
67.2


30.487
2.258
.715
59.1


2.852
.211
.067
20.4

APPROACH
4.500
30.000
211.800
15.885
185.484
13.911

1.802
.334
.025
7,6


14.418
2.674
.201
16.6


7.601
1.410
.106
32.2

CLIHBOUT
2.500
90.000
635.400
26.475
265.957
11.915

.105
.030
.001
.4


Z.245
.642
.027
2.2

• • - - - - -
8.990
2.571
.107
32.6

TAKEOFF TOTAL PER
CYCLE
.500
100.000
706.000
5.883^
315.005
2.625

.078
.025
.000
.1


1.782
.561
.005
.4


9.259
2.917
.024
7.4

33.500


63.540

60.542

5.4S1
.591
.330
100.1
5.194

19.992 ~
2. 168
1.210
100.0
19.049
. -— .- - _
5.429
.589
.329
100.0
5.173
                                           *•  EMISSION INDEX LEVELS REQUIRED TO MEET EPA  1979 STANDARDS  FOR  CLASS P2 ENGINES  **
                                        EPA LTO-CYCLE
                                 POLLUTANT   L9P/1000  HORSEPOHER-HR-CYCLE
                                    CO              26.8
                                    HC               4.9
                                    NOX             12.9
                                                                                                 REQUIRED EMISSION INDEX,  LBP/1000  LS FUEL
POLLUTANT IMOOE»
   CO HOLE)
   HC (IDLE)
   NOX (TAKEOFF)
   A
30.5
 8.9
 9.3
   B
45.8
 8.9
43.9
                                           A  ASSUMES.PROPORTIONAL REDUCTION OF POLLUTANT EMISSION INDEX AT  EACH LTO CYCLE MODE

                                           B  ASSUMES  (II REQUIRED REDUCTION IN CO AND HC OBTAINED BY LOWERING EMISSION  INDEX  VALUES
                                              AT  TAXI-IDLE MODE ONLY, CO AND HC EMISSIONS AT OIHtR MOOES REMAIN UNCHANGED, 121 REQUIRED
                                              REDUCTION IN NOX OBTAINED BY LOWERING EMISSION INDEX VALUES AT CLIMBOUT AND TAKEOFF  MOOES  IN
                                              SAME  PROPORTION AS MEASURED VALUES, NOX EMISSIONS AT TAXI-IDLE AND APPROACH MOOES   _ ..    	
                                              REMAIN UNCHANGED
-------
(D
VO
O
ENGINE^ TPE331-5-Z51M S/N= P04001 COMB P/N« 86908Z-4 FUEL* AV. KERO. TEST N0.« 16
RAT SHP= 706. RA £GT,F=
FUEL H/C= 1.9280 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POWER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Nl, RPM
COMPRESSOR INLET TEMP., DEC. F
COMPRESSOR DSCHG. PRES..PSIA
COMPRESSOR DSCHG. TEMP,DEG F
TURB INTERSTAGE TEMP., OEG.F
CORR BELMTH FLOM, LB/SEC
FA RATIO BASED CN 6ELLMTH.
MEASURED FUEL FLOW, LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING M/P"N/V/E(T/540I
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, MET
LB. COZ PER LB. OF FUEL
HEIGHT FLOM, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
MEIGHT FLOM, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NO) - MEIGHTS AS
PPM BY VOLUME, NET
L3. PER 1000 LB. OF FUEL
MEIGHT FLON, LB./HR.
NITROGEN DIOXIDE (NOZ)
PPM BY VOLUME, MET
LB. PER 1080 LB. OF FUEL
MEIGHT FLON, LB./HR.
1650.
.06822
316
5.0
35. Z
23.2
27560.0
58. 0
33.6
315.0
914.0
3.04
.0103
74.0
.0100
.147
.431
98.450

2.06
3.08
227. 9

320.2
30.524
2.259
RAT SPD= 41730.
L H V=
317
7.4
51.9
34.3
27550.0
63.0
33.6
322.0
995.0
2.82
.0126
84.0
.0115
.169
.392
98.957

2.38
3.10
260. 5

28H.4
23.626
1.985
CARBON, HEIGHTS AS
174.0
9.482
.702
.3196
N02
13.8
2.161
.160

4.4
.689
.051
117.0
5.556
.467
.2352

18.7
2.552
.214

3.9
.532
.045
18470.
319
10.0
70.6
46.5
27550.0
60.0
33.9
322.0
1060.0
2.76
.0138
90.0
.0125
.184
.381
99.218

2.60
3.11
280.3

Z44.4
18.616
1.675
CH4
90.0
3.918
.353
.2105

Z1.7
2.715
.244

2.9
.363
.033
OEM PT.Fs 51.
S LN T,F
319
30.2
213. 0
140.1
41740.0
58.0
92. 3
643.0
1120.0
7.69
.0102
187.0
.0102
.149
.101
99.506
OF REDUCED
2. 12
3.13
584.7

153.9
14.466
2.705

3Z.7
1.756
.328
.1214

Z9.5
4.554
.852

21.8
3.087
.577
= 300.0
320
69.9
493.7
325.1
41720.0
59.0
96.8
656.0
1225.0
7.63
.0139
251.0
.0136
.200
.090
99.870
EMISSION
2.86
3.15
789.7

67.3
4.711
1.183

5.4
.216
.054
.0458

65.5
7. 528
1.889

11.5
1.3ZZ
.332
RE. HUM*
FLO,L/M=
321
90.0
635.5
418.4
41740.0
59.0
99.5
663.1
1320.0
7.64
.0158
286.8
.0157
.229
.085
99.938

3.30 "
3.15
901.0

37.0
2.247
.643

3,0
.184
.031
.0464 ...

84.2
8.416
2.487

5.8
.574
.164
70.00 SPEC HUM' .007511
14.160 SL TIH.S* 6.5000
322
100.1
716.0 	
464.
41741.
59. ... __ ... .. . 	
100.
668.
1524.
7.63
.0174
315.1 	
.0167
.244
.082
99.951

3.51 " 	 " ' " " " 	 ~ "."
3.15
99Z.6 	 __. . 	 . ._

31. Z
1.782 	
.561

2.4
.078
.025
. .0439 	 1 	

96.3
9.025
2.843

._. 2.5. 	 - 	 	
.234
.074
TOTAL OXIDES OF NITROGEN INO+NOZI AS NOZ
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLON, LB./HR.
S10KE MEASUREMENT DATA
CORRECTED MEIGHT FLOM
SMOKE NUMBER
CORRECTED MEIGHT FLOM
SMOKE NUMBER
CORRECTED HEIGHT FLOM
SMOKE NUMBER
CORRECTED MEIGHT FLOM
SMOKE NUMBER
SMOKE NUMBER AT MA=0.023
18.2
2.850
.211

.00705
3.50
.02116
5.80
.03527
7.10
.04938
9.30
6.41
22.6
3.084
.259

.00703
3.50
.02109
4.70
.03515
5.80
.04920
8.10
5.61
24.6
3.078
.277

.00700
3.50
.02102
3.50
.03503
5.20
.04895
5.20
4.40
49.5
7.641
1.429

.00709
5.20
.02123
8.10
.03546
9.30
.04964
12.20
8.80
77.0
0.850
Z.221

.08719
9.30
.02128
12.80
.03546
16.30
.04964
22.11
15.21
91.1
8.991
Z.S71

.10719
8.10
.02128
11.00
.03546
18.61
.14974
21.31
14.60
98.8
9.259
Z.917 	

.01711
8.11 . ... . _ 	
.12132
16.31
.03553
16.91
.04974
19.21 	 ... 	 ... _.. 	 - ...
15.21
                   NOTES 1. ALL EMISSIONS CONCENTRATIONS  ARE NET VALUES.
                         2.EQUIVALENCE RATIO CALCULATED FROM COZ,CO,AND HC DATA AND FUEL COMPOSITION.
                         3.MASS EMISSIONS OF NO, NOZ,  AND NO*NOZ CALCUuATEO AS NOZ FROM CONCENTRATIONS HITH MOLECULAR MEIGHT OF NOZ  146.011.

-------
                     .............................................  AIRcSEARCH EMISSION  TEST  SUMMARY   •••••••••••••«
                     ENG MFC I AIRESEARCH            TEST FAClL I PHX LACCZ  INSTR DESCRIP  I FED REG V3»  N136
                     MODEL NO.I     TPE331-5-251M      S/NI   P0   111.16 LITERS/MIN.     TRANSPORT  TIME!    6.50 SEC.      LENGTH!   50.00 FT.
TEST CONDITION
ACTUAL POWER SETTING, HORSEPOWER
CORR. POWER SETTING «STD DAY), PERCENT RATED
Nl SPEED, RPH
FUEL FLCH IMEAS.t LB./HR.
CORR. ENGINE CORE AIRFLOW (HEASIt LB/SEC
COMPRESSOR INLET AIR TOTAL TEHP., OEG F
COMPRESSOR INLET AIR TOTAL PRESS. , PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTA, TEMP., DEC F
TURBINE INTERSTAGE GAS TOTAL TEMP., OEG F
EXHAUST GAS STATIC PRESSURE, PSIA
EMISSION CONCENTRATION, MET ANALYSIS
HYDROCARBON (HC AS CH"») , PPNC
CARBON MONOXIDE (COI . PPMV
TOTAL OXIDES OF NITROGEN (NOXI, PPHV
CARBON DIOXIDE  3Z5
23.0
5.01
27590.00
76.0
2.9
62.00
9.67
33.15
316.00
932.0
9.67

129.000
3111.21.9
21.000
2.117
16.800

6.61,7
39.180
3.203

.520
2.218
.21.3
98.71
.0103
36.3
9.98
27550.00
92.0
2.8
58.08
9.67
33.61.
321.00
1052.0
9.67

9 ",.500
259.167
28.100
2.581
26.500

"..I".*
19.882
3.51.1

.381
1.829
.326
99.17
.0125
3Z6
139.1
29.46
i>1720.00
185.0
7.7
61.00
9.67
91.60
61,7.00
1070.0
9.57

33.300
150.379
50.500
2.091,
29.101

1.809
11,. 292
7.881,

.335
2.61,1,
1.1,59
99.51
.0101
3Z7
325.0
69.91
1,171,0.00
252.5
7.6
59.00
9.67
96.51
659.00
1235.0
9.59

<>.200
67.339
76.500
2.863
65.500

.168
fc.712
0.792

.01,2
1.190
2.220
99.87
.0136
aze
1,17.1,
89.79
1.171.0.00
286.0
7.6
59.00
9.67
99.21
665.00
US'.. 6
9.60

2.700
37.775
08.750
3.267
8*. 500

.095
2.31S
a.91.7

.027
.661
2.559
99.91.
.0155
329
l»65.1^
100.15
1,171.0.01)
30<«.5
7.7
58.80
9.67 	
100.93
666.00
1520. « 	
9.62

1.80D
29.991
96.250
3.1.63
92.501

-------
to
vo
to
                     .........................................  Ep, CKCLE EMISSIONS COMPUTATION SUMMARY  »•»•»»»•»«
                     EN6 MFC  I  AIRESEARCH           TEST FACIt. I PHX LACt2  ISSTR OcSCRIP  I FED REG  V38 N136
                     MODEL NO.t      TPE331-S-251M     S/NJ   P0<»001              ENGINE  TYPE(CLASS) I   TURBOPROP
                     RATED POWER!     706.0  SHP AT SEA L£V£i. STANDARD DAY CONDITIONS
                     FUEL I ASTH  01655-73            ATOMIC H/C RATIOI   1.926     LHVI 18*70. BTU/LB     ADDITIVES!
                                                                                          CALC DATE  111-8-75
                                                                                          CALC IDt   2
                                                                                         TEST NOI  16
                                                                                                                       NONE
n o o E
»
TIME IN MODE, MINUTES
RATED POWER, PERCENT
CORRECTED POWER, HORSEPOWER
HP-HR
FUEL FLOW, LB/HR
FUEL MASS, LB
•• HYDROCARBON EMISSION IHCI »•
INDEX, LB HC/1000 LB FUEL
RATE, LB HC/HR
MASS, LB HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE. LB HC/1000 HORSEPOMER-HR PER CYCLE
•* CARBON MONOXIDE EMISSIONS (COI •*
INDEX, LB CO/1000 LB FUEL
RATE, LB CO/MR
MASS, LB CO
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORSEPOWER-MR PER CYCLE
»• TOTAL OXIDES OF NITROSEN EMISSIONS CNOXI •»
INDEX, LB NOX/1000 LB FUEL
RATE, LB NOX/HR
MASS, LB NOX
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB NOX/1000 HORSEPOMER-HR PER CYCLE
TAXI-IOLE
I IN)
7.000
5.000
35.300
"..118
73.968
3.363

6. SSI
.523
.061
Z0
2.662
.200
16.7


7.331
1.1,72
.110
31.9

CLIMBOUT
2.500
90.000
635.1,00
26.<»75
266.561,
11.91.0

.125
.036
.001
.6


2.373
.66*
.026
2.1,


8.979
2.573
.107
31.0

TAKEOFF TOTAL PER
CYCLE
.500
100.000
716.000
5.683
30

. . _ -
9.195
2.608
.023
6.7

33.500


63.5*0

*1.321

I..123
.V53
.253
100.0
3.979

19.1.72
2.139
1.19*
too. e
11.792
~~
5.61.8
.621
.31,6
100.1
5.1.50
                                            ••  EMISSION INOEX LEVELS REOUIRED TO MEET EPA 1979 STANDARDS  FOR  CLASS PZ ENGINES ••
                                        EPA  LTO-CYCLE
                                                                                                 REQUIRED EMISSION INOEX, LBP/100B LB FUEL
POLLUTANT
   CO
   HC
   MOX
                                              L3P/1000 HORS£POM£R-HR-CYCLE
                                                    26. 8
                                                    12.9
POLLUTANT (MODE!
   CO (IDLE!
   HC 
   NOX ITAKEOFFI
   A
29.2
 6.9
 9.2
                                                                                                                                          -.I..7
                                                                                                                                           6.6
                                           A   ASSUMES  PROPORTIONAL REDUCTION OF POLLUTANT EMISSION INOEX AT EACH  LTD CYCLE MODE

                                           B   ASSUMES  (11  REQUIRED REDUCTION IN CO AND HC OBTAINED BY LOWERING EMISSION INOEX VALUES
                                               AT TAXI-IDLc MODE ONLY,  CO AND HC EMISSIONS AT OTHtR MOOES REMAIN UNCHANGED, 121  REQUIRED
                                               REDUCTION  IN NOX OBTAINED BY l.CH£
-------
NJ
ENGINE* TPE331-5-251M S/N= P04001 COMB P/N- 869082-4
RAT SHP= 706. RA EGT,F=
FUEL H/C= 1.9280 STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Nl, RPN
COMPRESSOR INLET TEMP., OEG.F
COMPRESSOR DSCHG. PRES. ,PSIA
COMPRESSOR OSCHG. TEMP.tEG F
TURB INTERSTAGE TEMP., OEG.F
CORR BELHTH FLOH, LB/SEC
FA RATIO BASED ON BELLMTH.
MEASURED FUEL FLOH, LB/HR
FA RATIO CALC. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P"N/V/£(T/540»
COMB EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT BY VOLUME, HET
i.3. C02 PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
UNBURNEO HYDROCARBONS- PPM AS
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/LB CO
NITRIC OXIDE (NO) - HEIGHTS AS
PPM BY VOLUME, MET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE ;
                                                                                                                                                                    )!
                                                                                                                                                                    y
                                                                                                                                                                  i
                                                                                                                                                                  !)
                                                                                                                                                                  ')
-------
                                                                                                                                                                   V
0)
iQ
(D

N>
VO
                     .............................................   AIRESEARCH EMISSION TEST SUMMARY  •••»•»•••••••«
                     ENG MFC I AIRESEARCH           TEST  FACIL  I  PHX LACC2   INSTR OESCRIP I FED REG V38 N136
                     MODEL NO.:     TPE331-5-251M      S/N:    P04001               ENGINE TYPE(CLASS)!  TURBOPROP
                     RATED POWER:    706.0 SHP AT S£A  LEVEL  STANDARD DAY  CONDITIONS
                     FUEL: ASTH 01655-73            ATONIC H/C  RATIO:    1.929      LHVt 18470. BTU/LB     ADDITIVES!
 CALC DATE :il-fl-75
 CALC 101  3
TEST NO I  16
                                                                                                                       NONE
                     »»*•»»•» EXHAUST EMISSIONS PER EPA  CYCLE  OF  WORK OUTPUT »» CODE OF FEDEPAL REGULATIONS TITLE  40  PART  87   17  JULY  1973  ••»•»••
                                         HYDROCARBONS  (CH  AS CH.I           4.090 LB. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                         CARBON MONOXIDE (COI              18.436 -B. POLLUTANT PER 1000 HP.-HR. PER CYCLE
                                         OXIDES OF NITROGEN  .6  SMOKE NUMBER. MAXIMUM AT  TAKE-OFF   MODE,  100 PERCENT RATED POWER
                     TAXI-IDLE SETTING: s.o      PERCENT RATED TAKEOFF POWER AT f>*.      PERCENT RATED TAKEOFF NI  RPM
                     •»•*•.•»•••••»**••»»•••*•••**•••»»»•»•*•••*•»••••»••   ENGINE DESCRIPTION  »•»•»«»•»•»»••»•••»•»»••••••••••»••••••»••••••»••••
                     COH3 TYPE: REVERSE FLOW ANNULAR            P/N:    869082-4           SUR/VOL: 1.260  FUEL  INJ  TYPEI   STAGED  SIMPLEX
                     ENGINE TOTAL SERVICE:  fl.fl        HR     TIME  SINCE ENGINE OVERHAUL:  0.0       HR.  _    .
                     ENGINE ASSEMBLY AND MAINTENANCE INFORMATION:
                     AIRCRAFT INSTALLATION •»•• MFR. I                                  MODEL NO.I
                                                USER:                        ENGINE INSTALLATION POSITION:                                       _	  .
                     ,.....«..,„.,.......•........,......«>»»«»««»»»»OP£RATIONAL TEST DATA SUMMARY •»»»•»»»•«»»«••»•«•«•»»«»•••»»»»«•»•«»•••••»•»
                     GASEOUS EMISSION TEST NO.:  16           OATEt  11-8-75            TIME:                     BARO PRESS.I   19.700 IN. HGA.
                     AMBIENT AIR TE*P.:  59.00 DEG. f         RELATIVE HUMIDITY:  70.00 PERCENT       SPECIFIC  HUMIDITY:   .007500 LB. H2O/LB. DRY AIR
                     AMBIENT AIR QUALITY    HYDROCARBONS  (HC»:  0.0    PPKC      CAR30N HONOXIOE  (CO): 0.0   PPMV    OXIDES OF  NITROGEN (NOXII 0.0   PPMtf
                     SAMPLE LINE "• TEMP.:  300.00 OEG.  F.      FLOWRATE1    14.16 LITERS/MIN.     TRANSPORT TIMEI     6.50 SEC.      LENGTHI   50.00 FT.
TEST CONDITION
ACTUAL POWER SETTING, HORSEPOWER
CORR. POWER SETTING (STO OAY1 , PERCENT RATED
Nl SPEED. RPM
FUEL FLOM IMEAS.I L6./MR.
CORR. ENGINE CORE AIRFLCW IMEAS) , LB/SEC
COMPRESSOR INLET AIR TOTAL TEMP., DEG F
COMPRESSOR INLET AIR TOTAL PRESS* » PSIA
COMPRESSOR DISCHARGE AIR TOTAL PRESS., PSIA
COMPRESSOR DISCHARGE AIR TOTA. TEMP., OEG F
TURBINE INTERSTAGE GAS TOTAL TEMP., OEG F
EXHAUST GAS STATIC PRESSURE, PSI*
EMISSION CONCENTRATION, WET ANALYSIS
HYDROCARBON 
-------
(D
Ul
)

•)

)

>

)
..........................................  EPA CYCLE EMISSIONS COMPUTATION  SUMMARY  »•»•«•»••«
ENG MFC  I AIRESEARCH            TEST FACI. I PHX LACCZ   INSTR OESCRIP  I  FED REG  V38 N136
NOOEL NO.t     TPE331-5-251M     S/NI   POi.001              ENGINE  TYPE (CLASS) I   TURBOPROP
RATED POHER"     706.0  SHP  AT SEA LEVEL STANDARD DAY CONDITIONS
FUE..J ASTM D1655-73             ATOMIC H/C RATIOI   1.9Z8     LHV« 181.70.  BTU/LB      ADDITIVES!
                                                                                                                           CALC DATE »ll-8-75
                                                                                                                           CALC IDI  3
                                                                                                                          TEST NOI   16
                                                                                                                       I)
                                                                                                                      NONE
MODE
TINE IN MODE, MINUTES
RATED POHER, PERCENT
CORRECTED POHER. HORSEPOWER
HP-HR
FUEL FLCM, LB/HR
FUEL MASS, LB
»• HYDROCARBON EMISSION IHC) »•
INDEX. LB HC/1800 LB FUEL
RATE, LB HC/HR
MASS, LB HC
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HC/1000 HORSEPOHER-HR PER CYCLE
»* CARBON MONOXIDE EMISSIONS (CO) •»
INDEX, LB CO/1000 LB FUEL
RATE, LB CO/HR
MASS, LB CO .
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB CO/1000 HORSEPOHER-HR PER CYCLE
•• TOTAL OXIDES OF NITROGEN EMISSIONS INOXI »»
INDEX, LB NOX/1000 LB FUEL
RATE, LB NOX/HR
NASS, LB NOX
MASS, PERCENT OF TOTAL CYCLE
CYCLE, LB HOX/1000 HORSEPOWER-HR PER CYCLt
TAXI-IO..E TAXI-IDLE
(IN) IOUT)
7.000
5.000
35.300
l».118
75.977
8.861.

7.093
.539
.063
Z4.Z


28.529
2.168
.253
21.6


3.077
.Z3<>
.027
8.2

19.000
5.000
35.380
11.178
75.977
21.. 059

7.093
.539
.171
tS.7


28.529
2.168
.686
58.6


3.077
.23*
.07<>
22.3

APPROACH
*.5flO
30.000
211.800
15.885
189.9**
H«. 2*6

1.71.9
.332
.025
9.6


I*. 213
2.780
.ZOZ
17.3


7.%65
1.1.18
.186
32.0

CLIHBOUT
2.500
90.000
635.1.00
Z6.*75
Z«*.6*0
11.868

.102
.029
.001
.5


Z7076
.591
.029
Z.I
.

8.618
2.1,51
.102
30.7

TAKEOFF
.580
100.088
706.888
S.883
389.635
2.588

.098
.030
.000
.1 .


1.96Z
.607
.005 .
.*


8.859
Z.7*3
.023
6.9

TOTAL PER
CYCLE
33.580


63.5*8

61.618

	 *.Z18
«*65
.260
100.0 .
*.098

19.01*
2.D98
1.171
100.0
18.1.36

5.399
.596
.333
100.8
5.Z35 _.
                                          »* EMISSION INDEX LEVELS REQUIRED TO HEET EPA 1979 STANDARDS FOR  CLASS P2  ENGINES •*
                                       EPA LTO-CYCLE
                                                                                                REQUIRED EMISSION  INDEX, LBP/1000  LB FUEL
                                POLLUTANT
                                   CO
                                   HC
                                   NOX
  LBP/i«aO  HORSEPOWER-HR-CYCLE
        26.8
         ».*-
        1Z.9
                                                                                  POLLUTANT (MODE)
                                                                                     CO HOLE)
                                                                                     HC UDLEI
                                                                                     NOX CTAKEOFF)
                                                                                                           A
                                                                                                        Z8.5
                                                                                                         7.1
                                                                                                         8.9
 **.7
. 8.7
 *3.*
                )



               J
A  ASSUMES  PROPORTIONAL REDUCTION OF POu-UTANT EMISSION INOEX AT  EACH  LTD CYCLE MODE

B  ASSUMES  (II  REQUIRED REDUCTION IN CO AND HC OBTAINED BY LOWERING EMISSION  INOEX  VALUES
   AT TAXI-IDLE MODE ONLY, CO AND HC EMISSIONS AT OTHER MODES REMAIN UNCHANGED, IZ) REQUIRED
   REDUCTION IN NOX OBTAINED dY LOHERING EMISSION INOEX VALUES  AT  CLIHBOUT  AND TAKEOFF  NODES IN
   SAME PROPORTION AS MEASURED VALUES, NOX EMISSIONS AT TAXI-IDLE  AND  APPROACH NODES    .__ 	
   REMAIN UNCHANGED
                                                                                                                        r
-------
13
NJ
ENGINE^ TPE331-S-251M S/N= P0»001 COM3 P/H- 869082-* FUEL
RAT SHF= 706. Ht EGT,F=
FUEL H/C= 1.9ZBO STOI F/A=
DATA POINT NUMBER
PERCENT MAX. CORRECTED POHER
CORRECTED SHAFT HP
MEASURED SHAFT HP
SHAFT SPEED, Nl, RPM
COMPRESSOR INtET TEMP. , DEC. F
COMPRESSOR OSCHG. PRES. ,PSIA
COMPRESSOR OSCHG. TEMP, DEC F
TURB INTERSTAGE TEMP., CEG.F
CORR BE..MTH FLOH, LB/SEC-
FA RATIO BASED ON BELlMTH.
MEASURED FUEL FLOH, LB/HR
FA RATIO CA.C. FROM EMISSION
EQUIVALENCE RATIO
LOADING H/P**N/V/E(T/5*0>
COM3 EFFIC FROM EMISSIONS
CARBON DIOXIDE
PERCENT 3Y VOLUME, HET
L.B. COZ PER LB. OF FUEL
HEIGHT FLOH, LB./HR.
CARBON MONOXIDE
PPK BY VOLUME. HET
L3. PER 1000 LB. OF FU£L
HEIGHT FLOH, LB./HR.
UNBURNED HYDROCARBONS- PPM AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
RATIO LB HC/L9 CO
NITRIC OXIDE INO) - HEIGHTS AS
PPM BY VOLUME, HET
LB. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
NITROGEN DIOXIDE (N02I
PPM BY VOLUME, HET
LB. PER 1010 LB. OF FUEL
HEIGHT FLOH, LB./HR.
1650.
.06822
330
5.0
35.*
Z3.3
27570.0
62.0
33.2
323.0
9ZZ.C
Z.90
.0111
76.0
.010*
.153
.1.13
99. 70S

Z.I*
3.09
23*. 8

310.5
29.516
Z.167
RAT SPD-
L H V=
331
7.3
51.8
3*.. 2
27560.0
61.0
33.6
322.0
982.0
2.83
.0122
82.0
.011*
.168
.395
98.92*

2.36
3.10
2S..2

297.8
2*. 885
2.0*1
CARBON. HEIGHTS AS
135.0
7.086
.539
.2*85
NOZ
15.7
2.368
.180

*.7
.709
.05*
117.0
5.587
.1.58
.22*5

19.2
2.635
.216

3.8
.522
.0*3
1.1730.
18*70.
332
10.0
70.5
1.6.5
27560.0
61.0
33.8
323.0
1063.0
2.75
.0137
89.0
.0126
.185
.380
99.122

2.61
3.11
276.7

27*. Z
20.809
1.852
CH*
102.0
*.*Z»
.39*
.2126

Z*.*
3.01.2
.271

3.1
.386
.03*
OEH PT,F=
S LN T,F=
333
30. Z
213.0
1*0.1.
1.1730.0
60.0
91.8
6*6.0
1060.0
7.68
.0105
191.0
.0102
.1*9
.101
99.512
OF REDUCED
2.12
3.13
597.2

151.7
1*.Z59
Z.7Z3

3Z.*
1.7*1
.332
.1221

29.5
*.55*
.870

19.0
2.933
.560
51.
300.0
33*
69.9
1.93.*
321.. 2
1.17*0.0
' 57.0
9*. 6
65*. 0
1325.0
7.68
.0138
252. 5
.0136
.199
.095
99.867
EMISSION
2.85
3.15
79*. 3

69.0
*.e*s
1.Z2*

5.*
.217
.055
.0**7

63.*
7.31*
1.8*7

11.8
1.361
.3**
REL HUH:
FLO.L/M*
335
90.3
637.6
*19.*
1.17*0.
58.
99.
661.
1*50.
7.6*
.0158
286.0
.0157
.229
.085
99.91,0

3.30
3.15
. 901.0

35.7
2.172
.621

3.0
.10*
.030
.0*80

82.5
8.2*1
2.357

3.8
.375
.107
- AV.KERO. TEST N0.= 16
70.00 SPEC HUM* .007500
11.. 160 SL TIN,S» 6.5000
336
100.5
709.5
1.67.1
4.17*0.0
59.0
101.2
66*. 0
1*86.0
7.66
.0170
308.5
.0165
.2*2
.083 _ ...
99.955

3.1.8 "
3.15
97Z.Z 	 	

27.5
1.587
.*90

2.7
.089
.027
.0560

90.2
. ».5*fl 	 .... .._ . _
2.63*

3.5 . .._ . ...
.331
.102

t
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TOTAc OXIOES OF NITROGEN (NC*NOZ» AS NOZ ........ . 	 .... . ._.._.
PPM BY VOLUME, HET
L3. PER 1000 LB. OF FUEL
HEIGHT FLOH, LB./HR.
SMOKE MEASUREMENT DATA
CORRECTED HEIGHT FLOU
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOH
SMOKE NUMBER
CORRECTED HEIGHT FLOM
SMOKE NUMBER
SMOKE NUMBER AT MA«0.023
20.*
3.077
.23*

.00695
Z.30
.0209*
5.80
.03*73
8.10
.0*863
9.30
6.50
23.0
3.157
.259

.00693
2.30
.02080
5.80
.03*67
5.10
.01.85-.
9.30
5.90
27.5
3.*28
.305

.00693
3.50
.02080
3.50
.03*67
5.60
.0*85*
7.00
5.00
*8.5
7.*87
1.1.38

.00717
*.70
.02151
6.1.0
.03585
10.50
.05019
12.80
8.60
75. Z
8.676
2.191

.00716
7.00
.021*7
9.30
.03578
1*.00
.05009
20.90
12.80
86.3
8.616
2.*6*

.00716
8.10
.021*7
10.51
.03578
13.*0
.05009
19.80
13.00
93.0
8.871
2.737

.80716
7.60
.021*7
12.80
.03578
15.70
.05009
22.10 ,
l*.6fl

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X
                        NOTtS 1. ALL EMISSIONS CONCENTRATIONS ARE HET VALUES.
                              Z.EQUIVALENCE RATIO CALCU.ATEO FROM CC2,CO,ANO HC DATA AND FUEL COMPOSITION.                .           -         	
                              3.MASS EMISSIONS OF NO, NOZ,  AW .10»N02 CALCULATED AS NOZ FROM CONCENTRATIONS  HITH  MOLECULAR HEIGHT  OF NOZ <*6.01I.
-------
                             TECHNICAL REPORT DATA
                       (I'leasc read Instructions on Hie reverse be/
i. PEPOH r NO.
 EPA 460/3-76-009-b
4. TIT L? AND SUB TITLE
 Determination of the Effects  of Ambient
 Conditions on Aircraft Engine Emissions
 Engine Testing - GTCP85 APU,  TPE331 Turboprop
                                                 3. RECIPIENT'S ACCESSION NO.
           5. REPORT DATE
           _Jjficemb.e r  19.  1SL26	
           6. PERFORMING ORGANIZATION CODE
7 AUTHORIS)
 G. A.  Slogar
 R. C.  Holder
           8. PERFORMING ORGANIZATION REPORT NO

            75-311636
:-i PERFOI1MINGOR-ANIZATION NAME AND ADDRESS
 AiResearch Manufacturing Company of Arizona
 A Division of the Garrett Corporation
 402  South 36th Street
 Phoenix,  AZ  85034
12. SPONSORING AGENCY NAME AND ADDRESS
U.S. Environmental Protection  Agency
Office  of Air .and Water Programs
Office  of Mobile Source Air  Pollution Control
Emission Control Tech. Div.,Ann Arbor,MI 48105
                                                 10. PROGRAM ELEMENT NO.
           11. CONTRACT/GRANT NO.


            68-03-2156
           13. TVPF. OF REPORT AND PERIOD COVERED
            Final  Dec 1974-Dec 1975
           14. SPONSORING AGENCY CODE
15. SUPPLEMENTARY NOTES
I G. AUSTR ACT
 Under Environmental Protection Agency contract number 58-03-2156,
 AiResearch Manufacturing  Company of Arizona,  a Division of the
 Garrett Corporation, conducted full scale engine  tests on a
 GTCP85-98CK Auxiliary Power Unit and a TPE331-5-251M Turboprop
 engine.   The purpose of this program was to measure exhaust
 emission of HC, CO, C02»  N^x'  anc^ smoke at controlled (temperature,
 humidity,  and pressure) engine inlet conditions.   This data along
 with  other available data will provide the data  base for the
 determination of the effects of ambient conditions on gas turbine
 engines.
                          KEY WORDS AND DOCUMENT ANALYSIS
               DESCRIPTORS
  Air Pollution
  Aircraft
  Turbines
  Emission Measurement  Procedures
                                      I'.IDENTIFIERS/OPEN ENDED TERMS
                        1C
                        2 IE
                        7
 . DIS'RIBUTI ON STATEMENT


  Release unlimited
19. SECURITY CLASS (1'lii.t Keportl
  Unclassified 	
20. SECURITY CLASS /Thispagr)

  Unclassified
21. NO. OF CAGES
  296
  Form'2220-1 (9-73)
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