11/15/01
MANUFACTURER BOEING BOEING BOEING BOEING
RAYTHEON BAE SYSTEMS (BAe) BOEING BOEING BOEING BOEING BOEING AIRBUS AIRBUS
RAYTHEON
RAYTHEON
MCDONNELL DOUGLAS BAE SYSTEMS (BAe) BAE SYSTEMS (BAe) AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL B-737-700 MTOW 1000#
154.50 MLW 1000#
129.20
ENGINE MODEL CFM56-7B20
AP FLAPS 40 AP NOISE LEVEL (EPNdB)
95.9 NOTES B-737-700 154.50 129.20 CFM56-7B26 40 95.9 B-737-700 154.50 129.20 CFM56-7B22 40 95.9 B-737-700 154.50 129.20 CFM56-7B24 40 95.9 C-29A 28.00 23.35 TFE731-5R-1H 45 95.8 146-200A 93.00 81.00 ALF502R-5 33 95.8 B-737-200 (NORDAM;STC ST00131SE) B-737-200 (NORDAM;STC ST00131SE) B-737-600 B-737-600
119.50
119.50
143.50
143.50
103.00
103.00
120.50
120.50 JT8D-15 w/LGW-L
HUSHKIT JT8D-15 w/LGW HUSHKIT CFM56-7B/2 DAC (B18 derate) CFM56-7B20/2 DAC 30 30 40 40
95.8
95.8
95.8
95.8 37 37 50 50 B-737-600 143.50 120.50 CFM56-7B22/2 DAC 40 95.8 50 A320-214 182.80 150.00 CFM56-5B4/P 35 95.8 A321-231 205.02 171.51 V2533A5 25 95.8 HAWKER 125- 3A/RA 23.60 20.00 TFE731-3-1H 45 95.7 HAWKER 125- 400A 23.60 20.00 TFE731-3-1H 45 95.7 DC-09-20 (ABS;STC SA1613GL) 100.00 93.40 JT8D-9/9A 40 95.7 146-100A 84.00 77.50 ALF502R-5 33 95.6 146-200A 89.50 77.50 ALF502R-3 33 95.6 Page 26
11/15/01
MANUFACTURER BAE SYSTEMS (BAe) BAE SYSTEMS (BAe)
MCDONNELL DOUGLAS BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING BOEING
LEARJET
LEARJET
LEARJET
LEARJET
DASSAULT
DASSAULT AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES
89.50 77.50 ALF502R-3A 33 146-300A 95.6 146-200A 95.6
97.50 84.50 ALF502R-5 33 DC-09-10 (AIRWELD STC 108.00 99.00 JT8D-9A 40 95.6 12
ST00934LA)
B-737-600 143.50 120.50 CFM56-7B22 40 95.5 B-737-600 143.50 120.50 CFM56-7B20 40 95.5 B-737-600 143.50 120.50 CFM56-7B18 40 95.5 B727-100 RE (ROHR STC 174.50 142.50 JT8D-217C/JT8D-9 30 95.4 23
SA4363NM)
B727-100 RE (ROHR STC 174.50 142.50 JT8D-219/JT8D-7B 30 95.4 23
SA4363NM)
B727-100 RE (ROHR STC 174.50 142.50 JT8D-219/JT8D-9 30 95.4 23
SA4363NM)
B-757-300 95.4 58275.00 224.00 RB211-535E4-B 30 B-757-300 95.4 58275.00 224.00 RB211-535-E4 30 B-757-300 95.4 58275.00 224.00 RB211-535E4-C 30 24F-A 95.312.50 11.90 CJ610-6 40 24E 95.312.90 11.90 CJ610-6 40 24F 95.313.50 11.90 CJ610-6 40 25D/25F 15.00 13.30 CJ610-6/8A 40 95.2 FALCON 10 95.219.30 17.64 TFE731-2-1C 52 FALCON 50 (M2193) 40.79 35.72 TFE731-40-1 48 95.2 Page 27
11/15/01
MANUFACTURER
DASSAULT BAE SYSTEMS (BAe) BOEING BOEING BOEING BOEING BAE SYSTEMS (BAe)
MCDONNELL DOUGLAS BOEING BOEING BOEING AIRBUS AIRBUS AIRBUS AIRBUS
DASSAULT CESSNA CESSNA AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL FALCON 50 ( M1810) MTOW 1000#
40.79 MLW 1000#
35.72
ENGINE MODEL TFE731-40-1
AP FLAPS 48 AP NOISE LEVEL (EPNdB)
95.2 NOTES 146-100A 82.25 73.35 ALF502R-3A 33 95.2 B-757-200 255.50 210.00 RB211-535E4-B 30 95.2 58 B-757-200 255.50 210.00 RB211-535E4-B 30 95.2 B-757-200 255.50 210.00 RB211-535-E4 30 95.2 58 B-757-200 255.50 210.00 RB211-535-E4 30 95.2 146-100A 76.00 72.35 ALF502R-3 33 95.1 DC-09-10 (ABS) 90.70 81.70 JT8D-7/7A/7B 40 95.0 6 B-737-200 (AVAERO;STC ST223CH) B-737-200 ADV(AVAERO;STC ST223CH) B-737-200 ADV(AVAERO;STC ST223CH) A319-113
128.10
128.10
128.10
158.73
107.00
107.00
107.00
149.91 JT8D-17 JT8D-17 JT8D-15 CFM56-5A4 30 30 30 40
94.8
94.8
94.8
94.8 27 27 27,42 A319-114 163.14 149.91 CFM56-5A5 40 94.8 A319-131 158.73 149.91 V2522-A5 40 94.5 A319-112 166.44 149.91 CFM56-5B6/P 40 94.4 FALCON 200 (M5634) 32.00 28.88 ATF3-6A-4C 40 94.2 650 CITATION III 22.00 20.00 TFE731-3B-100S 37 93.8 22 650 CITATION VI 22.45 20.00 TFE731-3C-100S 40 93.8 Page 28
11/15/01
MANUFACTURER
AIRBUS UK
MCDONNELL DOUGLAS
MCDONNELL DOUGLAS
MCDONNELL DOUGLAS
LEARJET
MCDONNELL DOUGLAS
MCDONNELL DOUGLAS
MCDONNELL DOUGLAS
LEARJET CESSNA
DASSAULT
ISRAEL AIRCRAFT FOKKER
MCDONNELL DOUGLAS
MCDONNELL DOUGLAS
ISRAEL AIRCRAFT
GULFSTREAM
ISRAEL AIRCRAFT AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES 1-11 400 (QTV STC: ST02167AT) 81.90 78.00 SPEY511-14/14W 26 93.8 MD-80 160.00 150.00 JT8D-217A 40 93.7 10 MD-80 160.00 150.00 JT8D-217C 40 93.7 10 MD-80 160.00 150.00 JT8D-219 40 93.7 10 45 20.50 19.20 TFE731-20R-1B or (-20AR 40 93.4 1B) MD-87 149.50 130.00 JT8D-217A 40 93.3 10 MD-87 149.50 130.00 JT8D-217C 40 93.3 10 MD-87 149.50 130.00 JT8D-219 40 93.3 10 31A 17.00 16.00 TFE731-2-3B 40 93.1 560XL EXCEL 20.00 18.70 PW545A 35 93.1 FALCON 2000 36.50 33.00 CFE738-1-1B 40 93.1 1124 WESTWIND 22.90 19.00 TFE731-3-1G 40 93.0 F100 98.00 88.00 TAY MK650-15 42 93.0 MD-80 149.50 130.00 JT8D-209 40 92.9 10 MD-80 149.50 130.00 JT8D-217 40 92.9 10 1124A WESTWIND 2 23.50 19.00 TFE731-3-1G 40 92.8 * G200 34.85 28.00 PW306A 40 92.7 46 Galaxy 34.85 28.00 PW306A 40 92.7 Page 29
APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES
16.50 15.30 TFE731-2-3B 40LEARJET 31 92.6 *
45.41 41.22 AE3007A 45EMBRAER EMB-145ER 92.6 EMBRAER EMB-145EP 46.29 41.22 AE3007A 45 92.6 * BOMBARDIER CL-600-2C10 (CRJ700) 75.00 66.90 CF34-8C1 45 92.6 EMBRAER EMB-145LR 48.50 42.54 AE3007A1/1 45 92.5 LEARJET 55C 21.50 17.00 TFE731-3AR-3B 40 92.4 * LEARJET 55C 21.50 18.00 TFE731-3AR-2B 40 92.4 * ISRAEL AIRCRAFT 1125 ASTRA SPX 24.65 20.70 TFE731-40R 40 92.3
EMBRAER EMB-135LR 44.09 40.78 AE3007A1/3 45 92.3
DASSAULT FALCON 900EX (M3000) 49.00 44.50 TFE731-60-1 40 92.3
LEARJET 35/36 18.00 14.30 TFE731-2-2B 40 92.2 *
10.40 9.70 FJ44-1A 35CESSNA 525 CESSNA JET 92.1
34.52 31.72 PW306B 32FAIRCHILD DORNIER DORNIER 328-300 Mod 10 92.1 BOMBARDIER CL-600-2B19 (CRJ) 53.00 47.00 CF-34-3A1 45 92.1 BOMBARDIER CL-600-2B19 (CRJ) 53.00 47.00 CF-34-3B1 45 92.1 BOEING B-717-200 121.00 110.00 BR700-715C1-30 (MP) 40 92.1 49 BOEING B-717-200 121.00 110.00 BR700-715A1-30 (MP) 40 92.1 49
12.50 11.60 FJ44-2A 30RAYTHEON 390 PREMIER 92.0 Page 30
11/15/01
MANUFACTURER
RAYTHEON
GULFSTREAM
GULFSTREAM
MCDONNELL DOUGLAS
MCDONNELL DOUGLAS
DASSAULT
DASSAULT
DASSAULT
BOMBARDIER
BOMBARDIER
BOMBARDIER BOEING BOEING CESSNA BEECH
MITSUBISHI
LEARJET
LEARJET AC 36-1H APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES
35.50 28.50 PW305 25HAWKER 125-1000 92.0 G-IV GULFSTREAM w/ASC 190 74.60 66.00 TAY 611-8 39 92.0 G100 24.65 20.70 TFE731-40R-200G 40 91.9 MD-90-30 166.00 142.00 V2525-D5 40 91.9 MD-90-30 166.00 142.00 V2528-D5 40 91.9 FALCON 900 45.50 42.00 TFE731-5AR-1C 40 91.7 FALCON 900 (M1196) 46.50 42.00 TFE731-5AR-1C 40 91.7 FALCON 900B (M1200) 46.50 42.00 TFE731-5BR-1C 40 91.7 CL-600 40.40 36.00 ALF 502L/L-2/L-2C 45 91.6 * CL-600 41.25 36.00 ALF-502L/L-2/L-2C 45 91.6 * CL-600 (WINGLETS) 41.25 36.00 ALF-502L/L-2/L-2C 45 91.6
121.00 110.00 BR700-715A1-30 40B-717-200 91.6 48
121.00 110.00 BR700-715C1-30 40B-717-200 91.6 48 525A CITATION JET II (CJ-2) 12.37 11.50 FJ44-2C 35 91.4 BEECHJET 400 91.4 *15.78 14.22 JT15D-5 30 MU-300-10 (DIAM. II) 15.78 14.22 JT15D-5 30 91.4 * 35A/36A 18.30 15.30 TFE731-2-2B 40 91.4
18.30 15.30 TFE731-2-2B 4036A 91.4 * Page 31
APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES
18.00 14.30 TFE731-2-2B 40 CESSNA 550 CITATION Bravo 91.2 LEARJET 35A 91.3 *
14.80 13.50 PW530A 40 BOMBARDIER CL-600 36.00 33.00 ALF-502 45 91.2 * FAIRCHILD DORNIER DORNIER 328-300 33.51 31.06 PW306B 32 91.1 LEARJET 55B 21.50 18.00 TFE731-3A-2B 40 91.0 * GULFSTREAM G-IV 73.20 58.50 TAY 611-8 39 91.0 GULFSTREAM G200 34.85 28.00 PW306A 40 90.9 47 CESSNA 650 CITATION VII 23.00 20.00 TFE731-4R-3S 40 90.8 GULFSTREAM G-V 90.50 75.30 BR700-710A1-10 39 90.8 DASSAULT FALCON 20-C5/D5/E5 (M3500) 29.10 27.73 TFE731-5AR-2C 40 90.7 DASSAULT FALCON 20-C5/D5/E5 (M3530) 29.10 27.73 TFE-731-5BR-2C 40 90.7 LEARJET 55 90.6 *21.00 17.00 TFE731-3A-2B 40 SABRELINER SABRELINER 65 90.6 *24.00 21.80 TFE731-3R DASSAULT FALCON 20-C5/D5/E5 (M3547) 30.50 28.88 TFE731-5BR-2C 40 90.6
CESSNA 551 CITATION II 90.5 *
12.50 12.00 JT15D-4 40 CESSNA 550 CITATION II 90.514.10 13.50 JT15D-4 40 CESSNA 560 ENCORE 90.516.63 15.20 PW535A 35 DASSAULT FALCON 20-F5 (M3547) 30.50 28.88 TFE731-5BR-2C 40 90.3 Page 32
APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES
48.20 38.00 GE CF34-3B 45BOMBARDIER CL-604 90.3 *
35.70 31.80 AE3007C 35CESSNA 750 CITATION X 90.2 BOMBARDIER CL-601-1A 45.10 36.00 CF-34-1A 45 90.1 * BOMBARDIER CL-601-3A 45.10 36.00 CF-34-3A/-3A2 45 90.1 * BOMBARDIER CL-601-3R 45.10 36.00 CF-34-3A1 45 90.1 * AEROSPATIALE SN601 CORVETTE 14.60 13.20 JT15D-4 35 90.0 DASSAULT FALCON 20-F5 (M3500) 29.10 27.73 TFE731-5AR-2C 40 90.0 DASSAULT FALCON 20-F5 (M3530) 29.10 27.73 TFE-731-5BR-2C 40 90.0 ISRAEL AIRCRAFT 1125 ASTRA 24.70 20.70 TFE731-3A-200G 40 89.8 BOMBARDIER BD-700-1A10 (Global Express) 96.00 78.50 BR700-710-A2-20 30 89.8 BOMBARDIER BD700-1A10 (Global Express) 75.00 75.00 Rolls Royce/ BR700-710- 30 89.7 (Learjet STC: SA8184NM-D) A2-20 BOMBARDIER CL-601 89.4 *43.00 36.00 CF34-1A 45
43.10 36.00 CF-34-3A 45BOMBARDIER CL-601-3A 89.4 *
16.30 15.20 JT15D-5A 35CESSNA 560 CITATION V 88.9
15.50 14.30 JT15D-5 35CESSNA 552 88.5 * FOKKER F70 92.00 81.00 TAY MK620-15 42 CESSNA 500/501 CITATION I 11.80 11.30 JT15D-1/-1A 40 87.9 * CESSNA 500 CITATION 87.7 *10.30 9.90 JT15D-1 40 Page 33
88.3
APPENDIX 5 AIRCRAFT NOISE CERTIFICATION LEVELS IN DESCENDING EPNdB FOR U.S. CERTIFICATED TURBOJET POWERED AIRPLANES ***APPROACH*** MANUFACTURER MODEL MTOW 1000# MLW 1000# ENGINE MODEL AP FLAPS AP NOISE LEVEL (EPNdB) NOTES LEARJET 60 23.10 19.50 PW305A 40 87.7 LEARJET 60 23.50 19.50 PW305A 40 87.7 CESSNA S550 CITATION S/II 15.10 14.40 JT15D-4B 35 86.2 MITSUBISHI MU-300 (DIAMOND I) 14.10 13.20 JT15D-4 30 85.8 * MITSUBISHI MU-300 (DIAMOND I) 15.50 13.20 JT15D-4D 30 85.8 CESSNA 560 CITATION Ultra 16.30 15.20 JT15D-5D 35 85.7 Refer to Appendix 1 for Note Explanations Page 34
APPENDIX 6 MODEL
MANUFACTURER
AEROSPATIALE ATR42-200 MTOW MLW 1000#
34.70
34.20
MFR, MODEL
ENGINE DATA SHPNO.
AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN
AIRPLANES IN THE TRANSPORT CATEGORY
RPM MFR, MODEL
PROPELLER BLADESDIAM (IN) PITCH PW 120 2 2000 1200 HAMILTON STD 14SF-1 156 4 V
PRATT&WHITNEY TO AP FLAPS 15 30
TO SL AP STAGE NOISE LEVEL (EPNdB)
82.1 83.8 96.8 3 NOTES
AEROSPATIALE ATR42-300
35.60
35.30 PW 120 PRATT&WHITNEY 2 2000 1200 HAMILTON STD 14SF-5 156 4 V 15 30 82.6 83.8 96.8 3
AEROSPATIALE ATR42-300
37.30
36.20 PW 120 PRATT&WHITNEY 2 2000 1200 HAMILTON STD 14SF-5 156 4 V 15 30 83.3 83.7 96.7 3
AEROSPATIALE ATR42-320
35.60
35.30 PW 121 PRATT&WHITNEY 2 2100 1200 HAMILTON STD 14SF-5 156 4 V 15 30 82.2 83.9 96.8 3
AEROSPATIALE ATR42-320
37.30
36.20 PW 121 PRATT&WHITNEY 2 2100 1200 HAMILTON STD 14SF-5 156 4 V 15 30 83.0 83.9 96.7 3
AEROSPATIALE ATR42-400
39.50
38.80 PW 121A PRATT&WHITNEY 2 2200 1200 HAMILTON STD 568F 155 6 V 15 35 77.2 80.9 93.1 3
AEROSPATIALE ATR42-400
40.10
39.50 PW 121A PRATT&WHITNEY 2 2200 1200 HAMILTON STD 568F 155 6 V 15 35 77.6 80.9 93.0 3
AEROSPATIALE ATR42-500
41.00
40.30 PW 127E PRATT&WHITNEY 2 2400 1200 HAMILTON STD 568F 155 6 V 15 35 76.6 80.7 92.4 3
AEROSPATIALE ATR42-500
44.05
42.95 PW 127E PRATT&WHITNEY 2 2400 1200 HAMILTON STD 568F 155 6 V 15 35 78.5 80.7 92.2 3
AEROSPATIALE ATR72-100
44.10
43.90 PW 124 PRATT&WHITNEY 2 2400 1200 HAMILTON STD 14SF11 156 4 V 15 30 85.2 84.8 94.1 3
AEROSPATIALE ATR72-200
48.50
47.10 PW 124 PRATT&WHITNEY 2 2400 1200 HAMILTON STD 14SF11 156 4 V 15 30 86.9 84.7 91.1 3
AEROSPATIALE ATR72-200
47.40
47.10 PW 124 PRATT&WHITNEY 2 2400 1200 HAMILTON STD 14SF11 156 4 V 15 30 86.5 84.7 94.1 3
AEROSPATIALE ATR72-210
47.40
47.10 PW 127 PRATT&WHITNEY 2 2450 1200 HAMILTON STD 247F 156 4 V 15 33 80.2 84.8 92.7 3
AEROSPATIALE ATR72-210
47.40
47.10 PW 127 PRATT&WHITNEY 2 2450 1200 HAMILTON STD 14SF11 156 4 V 15 33 86.1 86.1 94.2 3 Page 1
APPENDIX 6 MODEL
MANUFACTURER
AEROSPATIALE ATR72-210 MTOW MLW 1000#
48.50
48.20
MFR, MODEL
ENGINE DATA SHPNO.
AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN
AIRPLANES IN THE TRANSPORT CATEGORY
RPM MFR, MODEL
PROPELLER BLADESDIAM (IN) PITCH PW 127 2 2450 1200 HAMILTON STD 14SF11 156 4 V
PRATT&WHITNEY TO AP FLAPS 15 33
TO SL AP STAGE NOISE LEVEL (EPNdB)
86.5 86.0 94.2 3 NOTES
AEROSPATIALE ATR72-210
50.66
49.56 PW127 PRATT&WHITNEY 2 1200 HAMILTON STD.
247F 156 4 V 15 33 82.2 84.7 92.4 3 BAE SYSTEMS (BAe) 748-2A
44.50
43.00 DART 532-2 ROLLS-ROYCE 2 2470 1394 DOWTY ROTOL CR212/4-30-4/22 144 4 V 15 28 92.5 96.8 103.8 2 BAE SYSTEMS (BAe) 748-2B
46.00
43.00 DART 535-2 ROLLS ROYCE 2 2470 1394 DOWTY ROTOL CR212/4-30-4/22 144 4 V 15 28 92.5 96.8 103.4 2 BAE SYSTEMS (BAe) 748-2B
46.00
43.00 DART 536-2 ROLLS ROYCE 2 2470 1394 DOWTY ROTOL CR212/4-30-4/22 144 4 V 8 28 88.7 93.3 92.8 3 1 BAE SYSTEMS (BAe) ATP
50.55
49.05 PW124A PRATT&WHITNEY 2 2160 1200 HAMILTON STD.
6/5500/F 165 6 V 7 22 80.7 82.1 96.5 3 BAE SYSTEMS (BAe) ATP
50.55
49.05 PW126A PRATT&WHITNEY 2 2396 1200 HAMILTON STANDARD 6/5500/F 165 6 V 7 20 79.5 82.7 97.0 3 BAE SYSTEMS (BAe) ATP
50.55
49.05 PW126A PRATT&WHITNEY 2 2396 1200 HAMILTON STD.
6/5500/F.1 165 6 V 7 15 79.5 82.7 97.9 3
BAE SYSTEMS (JETSTREAM) JETSTREAM 4100
23.00
22.30 TPE-331-14G(H)R-801 ALLIEDSIGNAL 2 1500 1552 MCCAULEY B/C5JFR36C1101/2L114G 114 5 V 9 15 85.8 83.5 87.8 3 *
BAE SYSTEMS (JETSTREAM) JETSTREAM 4100
24.00
23.30 TPE-331-14G(H)R-801 ALLIEDSIGNAL 2 1500 1552 MCCAULEY B/C5JFR36C1101/2L114G 114 5 V 9 15 86.4 83.4 87.8 3 *
BAE SYSTEMS (JETSTREAM) JETSTREAM 4100
24.00
23.30 TPE-331-14G(H)R-805 ALLIEDSIGNAL 2 1650 1552 MCCAULEY B/C5JFR36C1103/4L114H 114 5 V 9 15 86.5 84.3 87.8 3 *
BAE SYSTEMS (JETSTREAM) JETSTREAM 4100
24.00
23.30 TPE-331-14G(H)R-901 ALLIEDSIGNAL 2 1650 1552 MCCAULEY B/C5JFR36C1103/4L114H 114 5 V 9 15 86.7 84.3 87.9 3 *
BOMBARDIER DHC-7-101
43.00
41.01 PT6A-50 PRATT&WHITNEY 4 1017 1210 HAMILTON STD.
24PF-305 135 4 V 25 25 80.1 83.3 91.6 3 *
BOMBARDIER DHC-7-103
44.00
42.00 PT6A-50 PRATT&WHITNEY 4 1120 1210 HAMILTON STD.
24PF-305 135 4 V 25 25 80.5 84.0 91.4 3 * Page 2
APPENDIX 6 MODEL
MANUFACTURER
BOMBARDIER DHC-8 MTOW MLW 1000#
33.00
32.40
MFR, MODEL
ENGINE DATA SHPNO.
AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN
AIRPLANES IN THE TRANSPORT CATEGORY
RPM MFR, MODEL
PROPELLER BLADESDIAM (IN) PITCH PW 120 2 1800 HAMILTON STD.
14SF-1 156 4 V
PRATT&WHITNEY TO AP FLAPS 15 35
TO SL AP STAGE NOISE LEVEL (EPNdB)
80.7 86.3 95.1 3 NOTES
BOMBARDIER DHC-8-102
34.50
33.90 PW 120 PRATT&WHITNEY 2 1800 1150 HAMILTON STD 14SF-7 156 4 V 15 35 80.8 86.3 90.7 3
BOMBARDIER DHC-8-102
34.50
33.90 PW 120 PRATT&WHITNEY 2 1800 1200 HAMILTON STD 14SF-7 156 4 V 15 35 80.8 86.3 94.8 3
BOMBARDIER DHC-8-103
34.50
33.90 PW 121 PRATT&WHITNEY 2 1945 1150 HAMILTON STD 14SF-7 156 4 V 15 35 79.8 85.3 90.7 3
BOMBARDIER DHC-8-103
34.50
33.90 PW 121 PRATT&WHITNEY 2 1945 1200 HAMILTON STD 14SF-7 156 4 V 15 35 79.8 86.1 94.8 3
BOMBARDIER DHC-8-103
34.50
33.90 PW 121 PRATT&WHITNEY 2 1945 1100 HAMILTON STD 14SF-7 156 4 V 15 35 77.8 82.9 91.0 3
BOMBARDIER DHC-8-106
36.30
33.90 PW 121 PRATT&WHITNEY 2 1945 1100 HAMILTON STD 14SF-7 156 4 V 15 35 79.9 84.0 94.8 3
BOMBARDIER DHC-8-106
36.30
33.90 PW 121 PRATT&WHITNEY 2 1945 1200 HAMILTON STD 14SF-7 156 4 V 15 35 80.5 85.6 94.8 3
BOMBARDIER DHC-8-201
36.30
33.90 PW 123 PRATT&WHITNEY 2 1945 1100 HAMILTON STD 14SF-7 156 4 V 15 35 79.9 84.0 94.8 3
BOMBARDIER DHC-8-201
36.30
33.90 PW 123 PRATT&WHITNEY 2 1945 1200 HAMILTON STD 14SF-7 156 4 V 15 35 80.5 85.6 94.8 3
BOMBARDIER DHC-8-202
36.30
33.90 PW 123 PRATT&WHITNEY 2 1945 1100 HAMILTON STD 14SF-7 156 4 V 15 35 79.9 84.0 94.8 3
BOMBARDIER DHC-8-202
36.30
33.90 PW 123 PRATT&WHITNEY 2 1945 1200 HAMILTON STD 14SF-7 156 4 V 15 35 80.5 85.6 94.8 3
BOMBARDIER DHC-8-300
41.10
40.00 PW123 PRATT&WHITNEY 2 1200 HAMILTON STD.
14SF-15 156 4 V 5 15 84.3 87.4 98.9 3
BOMBARDIER DHC-8-311
41.10
40.00 PW123 PRATT&WHITNEY 2 2142 HAMILTON STANDARD 14SF-15 156 4 V 5 35 79.5 87.0 93.3 3 Page 3