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
APPENDIX 6 MODEL
MANUFACTURER
BOMBARDIER DHC-8-311 MTOW MLW 1000#
43.00
42.00
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 123 2 2142 1200 HAMILTON STD 14SF-15 156 4 V
PRATT&WHITNEY TO AP FLAPS 5 35
TO SL AP STAGE NOISE LEVEL (EPNdB)
80.0 86.8 93.3 3 NOTES
BOMBARDIER DHC-8-314
41.10
40.00 PW123 PRATT&WHITNEY 2 2249 1200 HAMILTON STANDARD 14SF-15 156 4 V 5 35 79.9 87.3 93.3 3
BOMBARDIER DHC-8-314
41.10
40.00 PW123 PRATT&WHITNEY 2 2249 1100 HAMILTON STANDARD 14SF-15 156 4 V 5 35 80.7 84.7 93.3 3
BOMBARDIER DHC-8-314
43.00
42.00 PW123 PRATT&WHITNEY 2 2249 1200 HAMILTON STANDARD 14SF-15 156 4 V 5 35 80.7 87.2 93.3 3
BOMBARDIER DHC-8-314
43.00
42.00 PW123 PRATT&WHITNEY 2 2249 1100 HAMILTON STANDARD 14SF-15 156 4 V 5 35 81.7 84.6 93.2 3
BOMBARDIER DHC-8-315
41.10
40.00 PW123E PRATT&WHITNEY 2 2142 1200 HAMILTON STANDARD 14SF-15 156 4 V 5 35 79.5 87.0 93.3 3
BOMBARDIER DHC-8-315
43.00
42.00 PW123E PRATT&WHITNEY 2 2142 1200 HAMILTON STANDARD 14SF-15 156 4 V 5 35 80.0 86.9 93.3 3
BOMBARDIER DHC-8-400 (Q400)
61.70
60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 77.1 84.1 94.9 3
BOMBARDIER DHC-8-400 (Q400)
61.70
60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 35 77.1 84.1 93.0 3 3
BOMBARDIER DHC-8-400 (Q400)
65.20
62.00 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 35 78.6 84.0 93.1 3 3
BOMBARDIER DHC-8-400 (Q400)
65.20
62.00 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 78.6 84.0 94.8 3
BOMBARDIER DHC-8-401 (Q400)
61.70
60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 35 77.1 84.1 93.0 3 3
BOMBARDIER DHC-8-401 (Q400)
61.70
60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 77.1 84.1 94.9 3
BOMBARDIER DHC-8-401 (Q400)
65.20
62.00 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 78.6 84.0 94.8 3 Page 4
APPENDIX 6 MODEL
MANUFACTURER
BOMBARDIER DHC-8-401 (Q400) MTOW MLW 1000#
65.20
62.00
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 PWC 150A 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V
PRATT&WHITNEY TO AP FLAPS 5 35
TO SL AP STAGE NOISE LEVEL (EPNdB)
78.6 84.0 93.1 3 NOTES 3
BOMBARDIER DHC-8-402 (Q400)
61.70
60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 77.1 84.1 94.9 3
BOMBARDIER DHC-8-402 (Q400)
61.70
60.50 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 35 77.1 84.1 93.0 3 3
BOMBARDIER DHC-8-402 (Q400)
65.20
62.00 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 35 78.6 84.0 93.1 3 3
BOMBARDIER DHC-8-402 (Q400)
65.20
62.00 PWC 150A PRATT&WHITNEY 2 5070 1020 DOWTY R408/6-123-F/17 162 6 V 5 15 78.6 84.0 94.8 3 CASA C-212-CB
14.33
13.80 TPE 331-5-251C ALLIEDSIGNAL 2 750 1591 HARTZELL HC-B4TN-5CL/LT10282H 107 4 V 10 20 87.3 84.0 91.2 3 * CASA C-212-CC
16.98
16.42 TPE 331-10/10R-501C/ ALLIEDSIGNAL 2 900 1591 HARTZELL HC-B4MN-5AL 110 4 V 10 15 85.9 85.1 90.9 3 * CASA C-212-CD/CE
16.98
16.42 TPE331-10R-502C/512 ALLIEDSIGNAL 2 900 1591 DOWTY-ROTOL (C)R.334/4-82-F/13 110 4 V 10 40 82.9 83.0 93.2 3 * CASA C-212-CF
16.98
16.42 TPE 331-10R-501C/511 ALLIEDSIGNAL 2 900 1591 HARTZELL HC-B4MN-5AL 110 4 V 10 15 85.9 85.1 90.9 3 * CASA C-212-DE
16.98
16.42 PT6A-65B PRATT&WHITNEY 2 1000 1700 MCCAULEY 4HFR34C756 106 4 V 10 40 84.1 84.7 88.0 3 * CASA C-212-DF
16.98
16.42 TPE331-10R-502C/512 ALLIEDSIGNAL 2 900 1591 DOWTY-ROTOL (C)R.334/4-82-F/13 110 4 V 10 40 82.9 83.0 93.2 3 * CASA C-295
46.30
45.63 PW127-G PRATT&WHITNEY 2 2645 1200 HAMILTON STANDARD HS E568F 155 6 V 10 15 87.1 88.2 93.9 3 * CASA CN-235
31.75
31.30 CT7-7A GENERAL ELECTRIC 2 1700 1384 HAMILTON STD.
14RF-21 132 4 V 8 23 84.5 86.5 87.2 3 * CASA CN-235-100
31.75
31.30 CT7-9C GENERAL ELECTRIC 2 1750 1384 HAMILTON STANDARD 14RF-21 132 4 V 10 23 84.8 86.7 87.2 3 * Page 5
APPENDIX 6 MODEL
MANUFACTURER CASA CN-235-100 MTOW MLW 1000#
33.29
32.85
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 CT7-9C 2 1750 1384 HAMILTON STANDARD 14RF-21 132 4 V
GENERAL ELECTRIC TO AP FLAPS 10 23
TO SL AP STAGE NOISE LEVEL (EPNdB)
85.3 87.8 87.2 3 NOTES * CASA CN-235-200
34.83
34.39 CT7-9C GENERAL ELECTRIC 2 1750 1384 HAMILTON STANDARD 14RF-21 132 4 V 10 23 80.5 87.4 92.4 3 * CASA CN-235-300
34.83
34.39 CT7-9C3 GENERAL ELECTRIC 2 1750 1384 HAMILTON STANDARD 14RF-37 144 4 V 10 15 85.0 87.8 93.3 3 *
CONVAIR 580 (Aeroprod.)
58.16
52.00 501-D13H ALLISON 2 3460 1020 AEROPRODUCTS A6441FN-606A 162 4 V 10 28 87.4 91.1 98.3 3
DORNIER 328-100/MOD 10
30.84
29.17 PW119B PRATT&WHITNEY 2 2180 1300 HARTZELL HD-E6C-3B 142 6 V 12 12 82.1 83.8 94.8 3 2,*
DORNIER 328-100/MOD 20
30.84
29.17 PW119C PRATT&WHITNEY 2 2180 1300 HARTZELL HD-E6C-3B 142 6 V 12 12 82.7 83.8 94.8 3 2,*
DORNIER 328-100/MOD 30
30.84
29.17 PW119C PRATT&WHITNEY 2 2180 1300 HARTZELL HD-E6C-3B 142 6 V 12 12 82.7 83.8 94.8 3 2,*
EMBRAER EMB-120
21.17
21.17 PW 115 PRATT&WHITNEY 2 1500 HAMILTON STD.
14RF-9 126 4 V 15 25 76.6 81.6 92.5 3
EMBRAER EMB-120
25.40
24.80 PW118 PRATT&WHITNEY 2 HAMILTON STD.
14RF-9 126 4 V 15 25 81.2 83.5 92.3 3 * FOKKER 50
45.86
41.83 125B PRATT&WHITNEY 2 V 8 26 81.0 85.0 96.8 3 FOKKER F27 MK500
45.00
42.00 DART 7/MK535-7R ROLLS ROYCE 2 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 90.6 92.2 100.3 2 FOKKER F27 MK500
45.00
43.50 DART 7/MK535-7 ROLLS ROYCE 2 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 86.9 90.1 94.3 3 1 FOKKER F27 MK500
45.00
43.50 DART 7/MK535-7R ROLLS ROYCE 2 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 87.4 89.8 94.3 3 1 FOKKER F27 MK500
45.90
43.50 DART 7/MK551-7R ROLLS ROYCE 2 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 87.6 89.8 94.3 3 1 Page 6
APPENDIX 6 MODEL
MANUFACTURER FOKKER F27 MK500/600 MTOW MLW 1000#
45.00
41.00
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 DART 7/MK552-7R 2 2307 DOWTY ROTOL R193-4-30-4 138 4 V
ROLLS ROYCE TO AP FLAPS 0 40
TO SL AP STAGE NOISE LEVEL (EPNdB)
87.4 89.8 94.1 3 NOTES 1 FOKKER F27 MK500/600
45.90
43.50 DART 7/MK552-7R ROLLS ROYCE 2 2307 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 87.6 89.8 94.3 3 1 FOKKER F27 MK600
45.00
42.00 DART7 MK532-7R ROLLS ROYCE 2 DOWTY ROTOL R193-4-30-4 138 4 V 0 40 90.6 92.2 100.3 2
LOCKHEED L382G
155.00
135.00 501-D22A ALLISON 4 4050 1020 HAMILTON STD.
54H60 162 4 V 18 35 94.8 96.7 98.1 3 *
MCDONNELL DOUGLAS DC3C (BTC STC)
28.75
28.75 PT6A-67R PRATT&WHITNEY 2 HARTZELL HC-B5MA-3/M11276 115 5 V 0 45 82.4 84.4 91.9 3 SAAB 2000(w/PECS mod)
50.20
48.50 AE2100A ALLISON 2 DOWTY ROTOL R381/6-123-F/5 15 35 78.4 87.5 87.9 3 SAAB 340B
28.50
28.00 CT7-9B GENERAL ELECTRIC 2 1384 DOWTY ROTOL R354/4-123-F/13/20 132 4 V 15 20 78.0 85.9 91.6 3 SAAB 340B
28.50
28.00 CT7-9B GENERAL ELECTRIC 2 1384 HAMILTON STD.
14RF-19 132 4 V 15 20 77.7 86.1 90.1 3 SAAB 340B
28.50
28.00 CT7-9B GENERAL ELECTRIC 2 1384 DOWTY ROTOL R375/4-123-F/21 132 4 V 15 20 78.0 85.9 91.6 3 SAAB SF340A
28.00
27.20 CT7-5A2 GENERAL ELECTRIC 2 1384 DOWTY ROTOL R375/4-123-F/21 132 4 V 15 20 78.2 85.8 84.4 3 SAAB SF340A
28.00
27.20 CT7-5A2 GENERAL ELECTRIC 2 1384 DOWTY ROTOL R354/4-123-F/13/20 132 4 V 15 20 78.2 85.8 84.4 3
SAAB FAIRCHILD 340
27.00
26.50 CT7-5A GENERAL ELECTRIC 2 1210 DOWTY ROTOL R320/4-123-F/1 126 4 V 15 35 79.3 87.6 89.6 3
SAAB FAIRCHILD 340
27.00
26.50 CT7-7E GENERAL ELECTRIC 2 1210 DOWTY ROTOL R320/4-123-F/1 126 4 V 15 35 79.5 87.4 89.6 3
SAAB-SCANIA 340A W/APU
27.28
26.50 CT7-5A2 GENERAL ELECTRIC 2 1735 DOWTY ROTOL R354/4-123-F13 132 4 V 35 77.5 86.2 86.3 3 Page 7
APPENDIX 6 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN
AIRPLANES IN THE TRANSPORT CATEGORY MTOW MODEL
MANUFACTURER MLW 1000# MFR, MODEL
ENGINE DATA NO. SHP RPM MFR, MODEL
PROPELLER DIAM (IN) BLADES
PITCH TO AP FLAPS
TO SL AP STAGE NOISE LEVEL (EPNdB) NOTES SHORT BROS. 22.00 PRATT&WHITNEY 2 1120 1675 HARTZELL 111 5 8 35 88.5 83.9 92.8 3 * SD3-30 21.61 PT6A-45 HC-35MP-34/M10282B-6 V SHORT BROS. 26.00 PRATT&WHITNEY 2 1327 HARTZELL 111 5 5 30 84.4 83.7 89.9 3 ** SD3-60 25.70 PT6A-65R HC-B5MP-3C/M10876K V SHORT BROS. 27.10 PRATT&WHITNEY 2 1700 HARTZELL 108 6 15 15 80.0 82.7 94.3 3 SD3-60-300 25.70 PT6A-67R HC-A6A-3/A1046E V Page 8