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
-------
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
-------
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
-------
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
-------
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
-------
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
-------
(D
I-1
O
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
pj
iQ
(D
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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(D
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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>
>
>
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
0)
(D
M
CO
................................................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
-------
o
P)
} ^
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. . .
*
J
-
\
9
' \
S
. _. . _. _
..
_'
. . <
'^>
-------
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>
(D
to
O
-------
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
(D
to
...».....»»..*.»...»»..*.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
-------
fl
tu
to
to
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
CO
-------
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
(D
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
-------
tJ
0)
U)
)
)
)
)
\
)
)
>
;
)
)
)
)
;
)
)
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.
-------
pi
U3
(D
U)
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)
iQ
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
(D
-------
PJ
vQ
(D
iU
oo
' 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
)
)
)
)
t
)
)
.\
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?
(D
iu
10
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. _ _
-------
to
\Q
n>
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
-------
fa
VQ
(0
Ui
NJ
-)
)
f
]
)
)
)
1
)
)
)
)
)
)
)
1
)
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
-------
pj
VQ
n>
en
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
-------
T-I
0)
VQ
(D
(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
n>
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
CO
;
)
)
)
)
)
)
)
i
;
J
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
-------
ns
fu
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to
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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
n>
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
!)
)
>
>
)
>
*
>
>;
):
);
)i
)
J
)
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
"0
0)
U3
(D
CO
-------
> 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 ,
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CO
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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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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.
)
)
)
)
J
).
)
}
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
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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
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*
-------
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$
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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
to
ua
(D
vo
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.
-------
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
(U
tQ
0>
vo
00
-------
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
(D
VO
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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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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
)
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) 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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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"" ~ ~ ~~" " '"
)
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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
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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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Ul
......................................... 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
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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
uq
(D
O
00
...,.............................».»»..........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§
X3
(U
03
(D
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
'
>
j.
I «yh
£
. ,*?
-------
(U
i-3
(D
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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)
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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
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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 ,
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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
.
^
'
_ _ . -
.. _
^
; '
,. _ _
;
.. .. _ __ _^ . .. . _j
^
*
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
}
)
b
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)
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)
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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
-------
0)
iQ
LJ
>
") »»»»»»«»»»»»»»»»»*»*»»»»»»»» 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
)
t)
0)
vQ
n>
oo
-------
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
'£
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wiwiwiwnnnnnuunuwuntwniwVwuwuutwiMimnwuniwt
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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
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""»»»»»*»»»»*»»»»»..» 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
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..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
-------
13
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vQ
(D
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)
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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(D
*.....,...,*..,......,...,....,.,........ »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
-------
D)
(£1
(D
*»»»»»»»»»»»»»»»»»»»»»» 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
-------
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
-------
13
0)
iQ
(D
ro
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
0)
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
-------
(U
(D
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CO
)
)
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
-------
(D
H
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
-------
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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
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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 ^\
\
)
-.
'
^
'
..
'
)
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*
..
*
- -
^
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*
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)'
-'
- - -
)'
. _ , _ - '
)
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..- .- ...'
* \
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,.... , .. «»«»»« 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 , Hn0£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
)
>
)
)
)
)
)
)
)
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-------
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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
(D
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IO
>
.
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
)
3
3
3
3
3
3
3
£.
-------
(D
}
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
>
)
>
-------
0)
i£|
05
to
M
Ul
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;
-------
TJ
PJ
i£!
(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
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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
-------
fll
N)
...,,,...........,.,.,.,.,..,....,.,...... £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
-------
(D
NJ
CO
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V
1
1
>
)
)
1
)
)
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.
-------
CD
tv>
co
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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iQ
(D
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to
) ...
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
'£.
-------
13
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CD
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1
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
-------
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.,*.»..,....,,.,»..,,..,..»,,..,.....,.. 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
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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
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.........,.......,.............,,..,..*.........,... 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
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)
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)
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)
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)
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)
)
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,
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,
,
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.
-------
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' )
)
)
)
)
>
)
>
)
)
'
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 NIOG£N
-------
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pj
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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
-------
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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 LEȣ- 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
95
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-
-------
(TJ
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*
(D
NJ
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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....».»..,....,.»»»,..,,»,.,,...,.»».».. 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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.»»»»*»»»*»»»»»»»»»»»»»»« 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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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
HIGHT 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.
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.....,......,.,......,....«..»*.»..».«».. 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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.......................................... 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
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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
(D
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
>
)
>
)
. >
)
)
>
>
-------
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
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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
!)
')
-------
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............................................. 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
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.......................................... 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
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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
h .
)
)
)
3
)
3
3
3
3
3
3
3
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
3
3:
i,
)
^}
. . . _.. ....
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.
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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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