APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH***
MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES BOEING B-757-200 RB211-535E4 198.00 84.5 25* 8,15,35 BOEING B-757-200 RB211-535E4 198.00 84.5 25* 8,15,36 BOEING B-757-200 RB211-535E4B 198.00 84.5 25* 8,15,35 BOEING B-757-200 RB211-535E4B 198.00 84.5 25* 8,15,36 DASSAULT FALCON 50 ( M1810) TFE731-40-1 35.72 84.5 48 8,15 DASSAULT FALCON 50 (M2193) TFE731-40-1 35.72 84.5 48 8,15 AIRBUS A-320-211 CFM56-5A1 142.20 84.4 20* 8,15 BOEING B-737-700W CFM56-7B20 128.00 84.4 30* 8,15,56 BOEING B-737-700W CFM56-7B22 128.00 84.4 30* 8,15,56 BOEING B-737-700W CFM56-7B24 128.00 84.4 30* 8,15,56 BOEING B-737-700W CFM56-7B26 128.00 84.4 30* 8,15,56 AIRBUS A319-111 CFM56-5B5/P; Mod No. 149.91 84.3 20* 8,15 27772 AIRBUS A319-112/P CFM56-5B6/P 149.91 84.3 20* 8,15 AIRBUS A321-231 V2533-A5 143.29 84.3 21* 8,15 MCDONNELL DOUG. MD-87 JT8D-217A 130.00 84.3 40 8,15 MCDONNELL DOUG. MD-87 JT8D-217C 130.00 84.3 40 8,15 MCDONNELL DOUG. MD-87 JT8D-219 130.00 84.3 40 8,15 AIRBUS A320-214/P CFM56-5B4/P 127.86 84.2 20* 8,15 IAI 1124A WESTWIND II TFE731-3-1G 19.00 84.2 40 MCDONNELL DOUG. MD-87 JT8D-219 128.00 84.2 40 8,15 AIRBUS A319-111 CFM56-5B5/P; Mod No. 121.25 84.1 20* 8,15 27772 AIRBUS A319-112/P CFM56-5B6/P 121.25 84.1 20* 8,15 AIRBUS A320-214/P CFM56-5B4/P 149.91 84.1 20* 8,15 BOEING B-737-600 CFM56-7B18 120.50 84.1 30* 8,15 BOEING B-737-600 CFM56-7B20 120.50 84.1 30* 8,15 BOEING B-737-600 CFM56-7B22 120.50 84.1 30* 8,15 DASSAULT FALCON 20-G (M2500) ATF3-6-2C 27.56 84.1 40 8,15 PAGE 35A 15
AC36-3H 4/5/2012 APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH*** MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES DASSAULT FALCON 200 ATF3-6A-4C 27.60 84.1 40 8,15 BOMBARDIER DHC-7 PT6A-50 42.00 84.0 25 15 DASSAULT FALCON 7X (SFI) PW307A 62.40 84.0 40 DOUGLAS DC-3 R-1830-90C 24.40 84.0 - 5 GENERAL DYNAMICS CV-440 R-2800 47.20 84.0 - 5 IAI 1124 WESTWIND TFE731-3-1G 19.00 84.0 40 8,15 IAI 1124IW WESTWIND IW TFE731-3-1G 19.00 84.0 40 15 SHORTS SD3-60-300 PT6A-67R 26.50 84.0 30 13 GULFSTREAM GULFSTREAM II SPEY MK511-8 58.50 83.9 20* 8,15 GULFSTREAM GULFSTREAM II SPEY MK511-8 58.50 83.9 20* 8,15,16 MCDONNELL DOUG. MD-80 JT8D-209 130.00 83.9 40 8,15 MCDONNELL DOUG. MD-80 JT8D-217 130.00 83.9 40 8,15 MCDONNELL DOUG. MD-80 JT8D-217A 150.00 83.9 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-217C 150.00 83.9 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-219 150.00 83.9 28* 8,15 DASSAULT FALCON 2000 CFE738-1-1B 33.00 83.8 40 8,15 MCDONNELL DOUG. MD-80 JT8D-209 128.00 83.8 40 8,15 MCDONNELL DOUG. MD-80 JT8D-217 128.00 83.8 40 8,15 MCDONNELL DOUG. MD-80 JT8D-217A 128.00 83.8 40 8,15 MCDONNELL DOUG. MD-80 JT8D-217C 128.00 83.8 40 8,15 MCDONNELL DOUG. MD-80 JT8D-219 128.00 83.8 40 8,15 MCDONNELL DOUG. MD-87 JT8D-217A 120.00 83.7 40 8,15 MCDONNELL DOUG. MD-87 JT8D-217C 120.00 83.7 40 8,15 MCDONNELL DOUG. MD-87 JT8D-217A 130.00 83.6 28* 8,15 MCDONNELL DOUG. MD-87 JT8D-217C 130.00 83.6 28* 8,15 MCDONNELL DOUG. MD-87 JT8D-219 130.00 83.6 28* 8,15 RAYTHEON HAWKER 125- 600A TFE731-3-1H 22.00 83.6 25* 8,15 PAGE 36A
APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH***
MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES RAYTHEON HAWKER 125- 700A TFE731-3-1H 22.00 83.6 25* 8,15,26 AIRBUS A319-131 V2522A5 149.91 83.5 40 8,15 AIRBUS A319-132 V2524-A5 149.91 83.5 40 8,15 AIRBUS A320-232 V2527-A5 123.45 83.5 40 8,15 AIRBUS A320-232 V2527-A5 149.91 83.5 40 8,15 MCDONNELL DOUG. MD-80 JT8D-209 128.00 83.5 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-209 130.00 83.5 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-217 130.00 83.5 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-217 128.00 83.5 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-217A 128.00 83.5 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-217C 128.00 83.5 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-219 128.00 83.5 28* 8,15 MCDONNELL DOUG. MD-87 JT8D-219 128.00 83.5 28* 8,15 RAYTHEON HAWKER 125- 3A TFE731-3-1H 20.00 83.5 25* 8,15 RAYTHEON HAWKER 125- 700A TFE731-3R-1H 22.00 83.5 25* 8,15,20,26 BOMBARDIER DHC-8-400 (Q400) PWC 150A 60.50 83.4 15 8,15 BOMBARDIER DHC-8-401 (Q400) PWC 150A 60.50 83.4 15 8,15 BOMBARDIER DHC-8-402 (Q400) PWC 150A 60.50 83.4 15 8,15 BOMBARDIER DHC-8-400 (Q400) PWC 150A 62.00 83.3 15 8,15 BOMBARDIER DHC-8-401 (Q400) PWC 150A 62.00 83.3 15 8,15 BOMBARDIER DHC-8-402 (Q400) PWC 150A 62.00 83.3 15 8,15 FOKKER F100 RR TAY MK620-15 88.00 83.3 42 8,15 MCDONNELL DOUG. MD-87 JT8D-217A 120.00 83.3 28* 8,15 MCDONNELL DOUG. MD-87 JT8D-217C 120.00 83.3 28* 8,15 MCDONNELL DOUG. MD-90-30 V2525-D5 142.00 83.3 40 8,15 MCDONNELL DOUG. MD-90-30 V2528-D5 142.00 83.3 40 8,15 RAYTHEON HAWKER 125- 1A TFE731-3-1H 19.55 83.3 25* 8,15 PAGE 37A
AC36-3H 4/5/2012 APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH*** MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES BOMBARDIER BD-700-1A10 (Global Express) BR700-710-A2-20 78.50 83.2 30 8,15 BOMBARDIER BD-700-1A10 (Global Express) BR700-710-A2-20 78.50 83.2 30 8,15 AIRBUS A-320-231 V2500.A1 142.20 83.1 20* 8,15 AIRBUS A320-231 V2500-A1; Mod No. 23408 142.20 83.1 20* 8,15 AIRBUS A320-231 V2500-A1; Mod No. 23408 142.20 83.1 20* 8,15 GULFSTREAM G200 PW306A 28.00 83.1 40 8,15,44 LEARJET LEARJET 35 TFE731-2 14.30 83.1 40 4 LEARJET LEARJET 36 TFE731-2 14.30 83.1 40 4 BEECH BEECHJET 400 JT15D-5 14.20 83.0 - 15 CESSNA CITATION ENCORE (560) PW535A 15.20 83.0 35 8,15 FAIRCHILD DORNIER 328-100 Mod 10 PW 119B 29.17 83.0 12 15,38 FAIRCHILD DORNIER 328-100 Mod 20 PW 119C 29.17 83.0 12 15,38 MITSUBISHI MU300-10 DIAMOND II JT15D-5 14.20 83.0 - 15 RAYTHEON HAWKER 125- 3A/RA TFE731-3-1H 20.00 83.0 25* 8,15 RAYTHEON HAWKER 125- 400A TFE731-3-1H 20.00 83.0 25* 8,15 AIRBUS A319-131 V2522A5 121.25 82.9 40 8,15 AIRBUS A319-132 V2524-A5 121.25 82.9 40 8,15 BOEING B-717-200 BR700-715A1-30 (MP) 110.00 82.9 40 8,15,53 DASSAULT FALCON 900EX (M3000) TFE731-60-1 44.50 82.9 40 8,15 EMBRAER EMB-145ER AE3007A 41.22 82.9 45 8,15 LEARJET LEARJET 31 TFE731-2-3B 15.30 82.9 40 13,15 RAYTHEON HAWKER 125-1000A PW305 25.00 82.9 45 8,15 FOKKER F100 RR TAY MK650-15 88.00 82.8 42 8,15 AEROSPATIALE ATR72-200 PW124/HS 14SF11 43.87 82.7 30 15 DASSAULT FALCON 900 TFE731-5AR-1C 42.00 82.6 40 8,15 DASSAULT FALCON 900 (M1196) TFE731-5AR-1C 42.00 82.6 40 8,15 DASSAULT FALCON 900B (M1200) TFE731-5BR-1C 42.00 82.6 40 8,15 PAGE 38A
APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH***
MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES FOKKER F-27-100 RR DART6 MK514 37.50 82.6 - 11 RAYTHEON HAWKER 125- 800XP TFE731-5BR-1H 23.35 82.6 45 8,15 BOMBARDIER CL-600-2C10 (CRJ700) CF34-8C1 66.90 82.5 45 8,15 DASSAULT FALCON 900DX (M4000, M3755, TFE731-60(-1C) 42.20 82.5 40 M3758) DASSAULT FALCON 900LX (M5281) TFE731-60(-1C) 44.50 82.5 40 EMBRAER EMB-145LR AE3007A1/1 42.54 82.5 45 8,15 GULFSTREAM GULFSTREAM IIB/GIII SPEY MK511-8 58.50 82.5 20* 8,15,16 RAYTHEON HAWKER 125- 800A TFE731-5R-1H 23.35 82.5 25* 8,15 RAYTHEON HAWKER 125- 800A TFE731-5R-1H 23.35 82.5 25* 8,15,20 AEROSPATIALE ATR72-200 PW124/HS 14SF11 47.07 82.4 30 15 BOEING B-717-200 BR700-715A1-30 110.00 82.4 40 8,15,52 BOEING B-717-200 BR700-715C1-30 110.00 82.4 40 8,15,52 CESSNA CITATION BRAVO (550) PW530A 13.50 82.3 40 8,15 AEROSPATIALE ATR72-210 PW127/HS 14SF11 47.07 82.2 33 15 DASSAULT FALCON 20-C5/D5/E5 (M3547) TFE731-5BR-2C 28.88 82.2 40 8,15 RAYTHEON HAWKER 125-1000A PW305 25.00 82.2 25* 8,15 FOKKER F100 RR TAY MK650-15 88.00 82.1 25* 8,15 DASSAULT FALCON 50 TFE731-3-1C 35.70 82.0 20* 8,15 DASSAULT FALCON 50 (M1230) TFE731-3-1C 35.71 82.0 20* 8,15 GULFSTREAM G-V BR700-710A1-10 75.30 82.0 39 8,15 SAAB SF340A (Dowty props) GE CT7-5A2 27.20 82.0 20 8,15 SAAB SF340B (Dowty props) GE CT7-9B 28.50 82.0 20 8,15 LEARJET LEARJET 55B TFE731-3A-2B 18.00 81.9 40 BOEING B-717-200 BR700-715A1-30 98.00 81.8 40 8,15,52 DASSAULT FALCON 10 TFE731-2 17.64 81.8 30* 8,15 DASSAULT FALCON 20-C5/D5/E5 (M3500) TFE731-5AR-2C 27.73 81.8 40 8,15 DASSAULT FALCON 20-C5/D5/E5 (M3530) TFE-731-5BR-2C 27.73 81.8 40 8,15 PAGE 39A
AC36-3H 4/5/2012 APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH*** MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES EMBRAER EMB-120 BRASILIA PW115 21.20 81.8 45 12 SHORTS 3-30 PT6A-45A 22.10 81.8 - 8,15 BOEING B-717-200 BR700-715A1-30 (MP) 98.00 81.7 40 8,15,53 BOMBARDIER DHC-8-400 (Q400) PWC 150A 62.00 81.7 35 8,15,42 BOMBARDIER DHC-8-401 (Q400) PWC 150A 62.00 81.7 35 8,15,42 BOMBARDIER DHC-8-402 (Q400) PWC 150A 62.00 81.7 35 8,15,42 CANADAIR CHALLENGER CL-600 ALF-502L 36.00 81.7 45 12 CANADAIR CHALLENGER CL-600 ALF-502L 36.00 81.7 45 15 CESSNA CITATION JET (525) FJ44-1A 9.70 81.7 35 8,15 LEARJET LEARJET 35A TFE731-2 15.30 81.7 40 15 LEARJET LEARJET 35A/36A TFE731-2 15.30 81.7 40 8,15 LEARJET LEARJET 36A TFE731-2 15.30 81.7 40 15 SABRELINER CORP. SABRE 65 TFE731-3R-1D 21.80 81.7 - 8,12 BOMBARDIER DHC-8-400 (Q400) PWC 150A 60.50 81.6 35 8,15,42 BOMBARDIER DHC-8-401 (Q400) PWC 150A 60.50 81.6 35 8,15,42 BOMBARDIER DHC-8-402 (Q400) PWC 150A 60.50 81.6 35 8,15,42 CASA AIRCRAFT C-295 PW 127 GM 45.63 81.6 15 15 CESSNA CITATION VII (650) TFE731-4C-3S 20.00 81.6 40 8,15 CESSNA CITATION VII (650) TFE731-4R-3S 20.00 81.6 40 8,15 DASSAULT FALCON 2000EX (M1826) PW308C 39.30 81.6 40 DASSAULT FALCON 2000EX (M1842) PW308C 39.30 81.6 40 LEARJET LEARJET 35 W/CENTURY III TFE731-2 14.30 81.6 40 8,15 LEARJET LEARJET 36 W/CENTURY III TFE731-2 14.30 81.6 40 8,15 LEARJET LEARJET 45 TFE731-20R-1B 19.20 81.5 40 8,15 LEARJET LEARJET 55 TFE731-3B 17.00 81.5 40 15 CANADAIR RJ (CL-600-2B19) CF34-3A1 44.70 81.4 45 15 CANADAIR RJ (CL-600-2B19) CF34-3A1 47.00 81.4 45 15 PAGE 40A
APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH***
MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES CESSNA CITATION III (650) TFE731-3B-100S 20.00 81.4 20* 7,8,15 GULFSTREAM G200 PW306A 28.00 81.4 40 8,15,45 DASSAULT FALCON 20-F5 (M3547) TFE731-5BR-2C 28.88 81.3 40 8,15 GULFSTREAM GULFSTREAM IV - SP RR TAY 611-8 66.00 81.3 39 8,15 BOMBARDIER DHC-8 102 PW120 33.90 81.2 35 15 BOMBARDIER DHC-8 103 PW121 33.90 81.2 35 15 BOMBARDIER DHC-8 106 PW121 33.90 81.2 35 15 BOMBARDIER DHC-8 201/202 PW123 33.90 81.2 35 15 GULFSTREAM G100 TFE731-40R-200G 20.70 81.2 40 8,15 CESSNA CITATION III (650) TFE731-3B-100S 19.00 81.1 20* 8,15 AEROSPATIALE ATR72-210 PW127/HS 247F 47.07 81.0 33 8,15 DASSAULT FALCON 20-F5 (M3500) TFE731-5AR-2C 27.73 81.0 40 8,15 DASSAULT FALCON 20-F5 (M3530) TFE-731-5BR-2C 27.73 81.0 40 8,15 DASSAULT FALCON 900 TFE731-5AR-1C 42.00 81.0 20* 8,15 CASA AIRCRAFT CN-235-100 CT7-9C 32.85 80.8 23 15 BOMBARDIER DHC-8 311 PW123 42.00 80.7 35 8,15 GULFSTREAM GULFSTREAM IV RR TAY 611-8 58.50 80.7 39 8,15 BOMBARDIER DHC-8 314 PW123 42.00 80.6 35 8,15 CASA AIRCRAFT C-212-CD TPE 331-10R-512C/502C 16.42 80.5 40 15 CASA AIRCRAFT C-212-CE TPE 331-10R-512C/502C 16.42 80.5 40 15 CASA AIRCRAFT C-212-DF TPE 331-10R- 16.42 80.5 40 15 502C/512C/513C CESSNA 560 JT15D-5A 15.20 80.5 35 8,15 CESSNA CITATION V (560) JT15D-5A 15.20 80.5 35 8,15 CANADAIR CHALLENGER CL-601 CF34-1A 36.00 80.4 45 15 CANADAIR CHALLENGER CL-601 CF34-1A 36.00 80.4 - 15 CANADAIR CHALLENGER CL-601 CF34-3A/A1/A2 36.00 80.4 45 15 IAI 1125 ASTRA TFE731-3A-200G 20.70 80.4 40 8,15 PAGE 41A
AC36-3H 4/5/2012 APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH*** MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES CESSNA CITATION JET II (525A) FJ44-2C 11.50 80.3 35 8,15 FAIRCHILD DORNIER 328-300 Mod 10 PW306B 31.72 80.3 32 8,15 CASA AIRCRAFT CN-235-300 CT7-9C3 34.39 80.2 15 15 SHORTS 3-60 PT6A-65R 26.10 80.1 30 8,15 BAE SYSTEMS (BAe) BAe-748 SERIES 2B RR-DART MK535- 43.00 80.0 27 8,15
W/HUSHKIT BEECH B60 TI0-541-E1C4 6.80 80.0 - 10,11 SAAB FAIRCHILD SF340 GE CT7-5A2 26.50 80.0 35 12 CASA AIRCRAFT CN-235-200 CT7-9C 34.39 79.9 40 15 CESSNA CITATION II (550) JT15D-4 13.50 79.8 40 8,15 CASA AIRCRAFT C-212-CC TPE 331-10/10R-501C/511C 16.42 79.7 40 15 CASA AIRCRAFT C-212-CF TPE 331-10R-501C/511C 16.42 79.7 40 15 CESSNA S550 (SII) JT15D-4B 14.40 79.6 35 8,15 FAIRCHILD DORNIER 328-300 PW306B 31.06 79.5 32 8,15 DASSAULT FALCON 20-F5 TFE731-5AR-2C 27.76 79.4 25* 8,15 FOKKER F-27 MK500/600 MK552-7R 43.50 79.4 40 15,16 CESSNA CITATION II (550) JT15D-4 12.70 79.3 40 8,15 AEROSPATIALE SN601 CORVETTE JT15D-4 12.40 79.1 35 4 FOKKER F-27 MK500/600 MK552-7R 41.00 79.1 40 15,16 FOKKER F70 RR TAY MK620-15 81.00 79.0 42 8,15 SAAB 2000 AE2100A 47.40 78.9 20 8,15 SAAB SF340B (HS14RF-19 props) GE CT7-9B 28.50 78.8 20 8,15 SAAB SF340B (HS14RF-19 props) GE CT7-9B 28.00 78.8 20 8,15 FOKKER F70 RR TAY MK620-15 75.00 78.6 42 8,15 FAIRCHILD DORNIER SA226-AC METRO III TPE-331-11U 14.00 78.5 - 10,11 FAIRCHILD DORNIER SA226-T(B) MERLIN IIIB TPE-331-10U 12.50 78.5 - 5,11 FAIRCHILD DORNIER SA227-AT MERLIN III C TPE-331-10U 13.20 78.5 - 5,11 FAIRCHILD DORNIER SA227-AT MERLIN IV C TPE-331-11U 14.00 78.5 - 10,11 PAGE 42A
APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH***
MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES PIPER CHEYENNE 400LS TPE-331-14 11.10 78.5 - 11 BOMBARDIER DHC-6 PT6A-27 12.50 78.0 4 CESSNA CITATION ULTRA (560) JT15D-5D 15.20 78.0 35 8,15 CESSNA CITATION VII (650) TFE731-4C-3S 20.00 78.0 20* 8,15 GULFSTREAM 695A COMMANDER 1000 TPE-331-10 10.60 77.9 - 5,11 BEECH SUPER KINGAIR 200 PT6A-41 12.50 77.8 - 11 BEECH SUPER KINGAIR B200 PT6A-41 12.50 77.8 - 10,11 BEECH SUPER KINGAIR B200T/CT PT6A-42 12.50 77.8 - 5,11 CESSNA 500 JT15D-1 10.90 77.7 40 15 CESSNA CITATION I JT15D-1A 11.40 77.7 40 8,15 GULFSTREAM 690C COMMANDER 840 TPE-331-5 9.70 77.4 - 5,11 GULFSTREAM 690D COMMANDER 900 TPE-331-5 10.60 77.4 - 10 GULFSTREAM 695 TPE-331-10 9.70 77.4 - 5,15 GULFSTREAM 695 COMMANDER 980 TPE-331-10 9.70 77.4 - 5,11 LEARJET LEARJET 60 PW305A 19.50 77.4 40 8,15 BEECH F90 KINGAIR PT6A-135 10.90 77.3 - 5,11 SHORTS SKYVAN TPE-331-201 12.50 77.3 46 MITSUBISHI MU300 DIAMOND I JT15D-4 13.20 77.2 30 12 BEECH B100 KINGAIR TPE-331-6 11.20 77.1 - 11 BEECH C99 AIRLINER PT6A-34 11.30 77.1 - 5,11 PIPER PA-42 CHEYENNE PT6A-41 9.40 77.1 - 10,11 BEECH 1900/1900C PT6A-65B 16.10 77.0 - 10 BEECH 58P TSIO-520WB 6.20 77.0 - 10,11 BEECH 58TC TSIO-520-WB 6.20 77.0 - 10,11 GULFSTREAM 500S IO-540-E1B5 6.80 77.0 - 10 CASA AIRCRAFT C-212-DE PT6A-5B 16.42 76.9 40 15 BEECH B200/T/CT/C;C-12F(4 BLD) PT6A-42 12.50 76.6 - PAGE 43A
AC36-3H 4/5/2012 APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH*** MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES CESSNA CONQUEST II TPE-331-8 9.80 76.5 - 5,11 BAE SYSTEMS (JETSTREAM) JETSTREAM 4100 TPE331-14-801H/802H 22.30 76.4 15 12,15 BAE SYSTEMS (JETSTREAM) JETSTREAM 4100 TPE331-14-801H/802H/805H 23.30 76.3 15 12,15 EMBRAER EMB 110-P2 PT6A-34 12.50 76.0 - 4 FAIRCHILD DORNIER SA226-AT TPE-331-3U-303G 12.50 76.0 - 4 FAIRCHILD DORNIER SA226-T TPE-331-3U-303G 12.50 76.0 - 4 FAIRCHILD DORNIER SA226-TC METRO II TPE-331-3UW-303G 12.50 76.0 - 4 GULFSTREAM 690B TPE-331-5-251K 9.70 76.0 - 10 MITSUBISHI MU-2B-26A TPE-331-5-252M 10.00 76.0 - 4 MITSUBISHI MU-2B-36A TPE-331-5-252M 10.20 76.0 - 4 BEECH 300/300C KING AIR PT6A-60A 14.00 75.9 - SAAB SF340A (Dowty props) GE CT7-5A2 26.50 75.8 20 8,15 BEECH C90 PT6A-21 9.70 75.0 - 10 BEECH H18 R-985AN-14B 9.50 75.0 - 11 CESSNA CONQUEST I PT6A-112 8.20 75.0 - 10,11 BAE SYSTEMS (JETSTREAM) JETSTREAM 31 TPE331-10U-501H 14.60 74.7 - 15 FAIRCHILD DORNIER DORNIER 228 TPE-331-5-252D 12.60 74.7 - BEECH 99A PT6A-27 10.40 74.0 - 4 BEECH A100 PT6A-28 11.20 74.0 - 4 BEECH B80 IGS0-540-A1D 8.80 74.0 - 11 BEECH E55 (2 BLD) I0-520-C 5.30 74.0 - 11 BEECH E55 (3BLD) IO-520-C 5.30 74.0 - 11 CESSNA 402C TSIO-520-VB 6.90 74.0 - 11 CESSNA 404 GTSIO-520-M 8.40 74.0 - 11 CESSNA 421C GTSIO-520-L 7.50 74.0 - 11 GULFSTREAM 680FL IGSO-540-B1A 8.00 74.0 - 11 PIPER PA-31-325 TIO-540-F2BD 6.50 74.0 - 11 PAGE 44A
APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH***
MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES PIPER PA-31-350 TI0-540-J2BD 7.00 74.0 - 11 PIPER PA-31T PT6A-28 9.00 74.0 - 4 BEECH 65 QUEENAIR IGSO-480-A1B6 7.40 73.8 - 11 CESSNA 310Q I0-470-V0 5.20 73.7 - 10,11 BEECH 58/58A BARON (3 BLD) IO-550-C 5.40 73.3 - 11 BEECH 58 (2BLD) I0-520-C 5.40 73.0 - 11 BEECH 58 (3BLD) IO-520-C 5.40 73.0 - 11 BEECH B55 IO-470-L 5.10 73.0 - 11 BEECH B55(3BLD) IO-470-L 5.10 73.0 - 11 BRITTEN-NORMAN ISLANDER BN-2B O-540-E4C5 6.20 73.0 - 11 CESSNA 310R TSIO-520-BB 5.50 73.0 - 11 CESSNA 320C TSI0-470-D 5.20 73.0 - 11 CESSNA 340A TSIO-520-MB 6.00 73.0 - 11 CESSNA 401 TSIO-520-E 6.30 73.0 - 11 CESSNA 414A TSIO-520-N 6.80 73.0 - 11 CESSNA CARAVAN I PT6A-114 7.30 73.0 - GULFSTREAM 560E GO-480-C1B6 6.50 73.0 - 11 PIPER 601P IO-540-S1A5 6.00 73.0 - 11 PIPER PA-23-250 IO-540-C4B5 4.94 73.0 - 11 PIPER PA-31-310 TI0-540-A2C 6.50 73.0 - 11 PIPER PA-602P IO-540-AA1A5 6.00 73.0 - 11 PIPER PA-60-600 IO-540-K1J5 5.50 73.0 - 11 CESSNA 337H IO-360-G 4.60 72.0 - 11 GULFSTREAM GA-7 O-320-D1D 3.80 72.0 - 4 PIPER PA-34-200T TSI0-360-E 4.50 72.0 - 11 PIPER PA-34-220T TSIO-360-KB 4.50 72.0 - 11 BEECH D95A TRAVELAIR IO-320-B1B 4.20 71.1 - 11 PAGE 45A
AC36-3H 4/5/2012 APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH*** MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES BEECH 76 I0-360-A1G6D 3.90 71.0 - 11 PIPER PA-44-180 O-360-E1A6D 3.80 71.0 - 11 PIPER PA-44-180T(2BLD) TO-360-E1A6D 3.90 71.0 - 11 PIPER PA-44-180T(3BLD) TO-360-E1A6D 3.90 71.0 - 11 PIPER PA-30 TWIN COMANCHE IO-320-B 3.60 70.6 - 11 BEECH 35-B33 I0-470-K 3.00 68.0 - 10,11 CESSNA 210 IO-520-L 3.80 67.1 - 10,11 BEECH 35-C33A I0-520-B 3.30 64.0 - 11 BEECH A36 IO-520-BA 3.60 64.0 - 11 BEECH A36 BONANZA IO-550-B 3.65 64.0 - 11 BEECH B36TC BONANZA TSIO-520U 3.85 64.0 - 11 BEECH F33A I0-520-B 3.40 64.0 - 11 BEECH V35B (3BLD) I0-520-B 3.40 64.0 - 11 BELLANCA 17-30A I0-540-T4B5D 3.30 64.0 - 4 CESSNA 185F I0-520-D 3.40 64.0 - 11 CESSNA T210L TSI0-520-R 3.80 64.0 - 11 CESSNA T210M TSI0-520-R 3.80 64.0 - 11 CESSNA TU206G TSI0-520-M 3.60 64.0 - 11 EXTRA FLUGZEUGBAU EA 400 TSIOL-550-A 4.41 64.0 - 11,21 PIPER PA-32-300 IO-540-K1G5D 3.40 64.0 - PIPER PA-32R-300 IO-540-K1G5D 3.60 64.0 - 11 PIPER PA-32R-301 IO-540-K1G5D 3.60 64.0 - 11 PIPER PA-32R-301T TIO-540-S1AD 3.60 64.0 - 11 PIPER PA-32RT-300 IO-540-K1A5D 3.60 64.0 - 11 PIPER PA-46-31P MALIBU TSIO-520-BE 4.10 63.9 - 11 CESSNA 207 IO-520-F 3.80 63.8 - 11 CESSNA T206H TIO-540-AJIA 3.60 63.8 - 11,21 PAGE 46A