AC36-3H 4/5/2012 APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***TAKEOFF*** TOGW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES BEECH B200/T/CT/C;C-12F(4 BLD) PT6A-42 12.50 66.1 - BEECH 58P TSIO-520WB 6.20 66.0 - 10,11 BEECH 99A PT6A-27 10.40 66.0 - 4 BEECH B80 IGS0-540-A1D 8.80 66.0 - 11 CESSNA 185F I0-520-D 3.40 66.0 - 11 CESSNA 340A TSIO-520-MB 6.00 66.0 - 11 GULFSTREAM 690B TPE-331-5-251K 10.30 66.0 - 10 MITSUBISHI MU-2B-36A TPE-331-5-252M 11.00 66.0 - 4 PIPER PA-602P IO-540-AA1A5 6.00 66.0 - 11 PIPER PA-60-600 IO-540-K1J5 5.50 66.0 - 11 AIRBUS A319-111 CFM56-5B5/P; Mod No. 123.45 65.9 8,15 27772 AIRBUS A319-111 CFM56-5B5/P; Mod No. 123.45 65.9 8,15 27772 BEECH 65 QUEENAIR IGSO-480-A1B6 7.70 65.9 - 11 EMBRAER EMB-145ER AE3007A 45.41 65.9 9 8,15 BOEING B-737-700W CFM56-7B26 133.00 65.8 1 8,15,56 AIRBUS A319-131 V2522A5 123.45 65.7 10 8,15 BOMBARDIER DHC-8 103 PW121 34.50 65.7 15 CASA AIRCRAFT C-212-CC TPE 331-10/10R-501C/511C 16.98 65.7 10 15 CASA AIRCRAFT C-212-CF TPE 331-10R-501C/511C 16.98 65.7 10 15 CESSNA CITATION VII (650) TFE731-4C-3S 23.00 65.7 7 8,15 BOEING B-737-700W CFM56-7B26/2 DAC 133.00 65.6 1 8,15,54,56 CESSNA T206H TIO-540-AJIA 3.60 65.6 - 11,21 LEARJET LEARJET 35 W/CENTURY III TFE731-2 17.00 65.6 - 8,15 LEARJET LEARJET 36 W/CENTURY III TFE731-2 17.00 65.6 - 8,15 AIRBUS A320-231 V2500-A1; Mod No. 23408 127.86 65.5 8,15 AIRBUS A320-231 V2500-A1; Mod No. 23408 127.86 65.5 8,15 BOMBARDIER DHC-8 311 PW123 43.00 65.4 8,15 PAGE 32T
APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***TAKEOFF***
TOGW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES CESSNA CITATION VII (650) TFE731-4R-3S 22.45 65.4 8,15 FOKKER F70 RR TAY MK620-15 81.00 65.4 8,15 SAAB FAIRCHILD SF340 GE CT7-5A2 27.30 65.3 15 12 AIRBUS A320-214/P CFM56-5B4/P 132.27 65.2 10 8,15 BOEING B-717-200 BR700-715C1-30 (MP) 104.50 65.2 5 8,15,53 BEECH 58/58A BARON (3 BLD) IO-550-C 5.50 65.1 - 11 LEARJET LEARJET 35A/36A TFE731-2 18.30 65.1 8 8,15 BEECH A24R I0-360-A1B6 2.80 65.0 - 11 BELLANCA 17-30A I0-540-T4B5D 3.30 65.0 - 4 CESSNA 177RG I0-360-A1B6 2.80 65.0 - 11 CESSNA 310R TSIO-520-BB 5.50 65.0 - 11 MOONEY M20C 0-360-A1D 2.60 65.0 - 11 PIPER PA-24-260 IO-540-B1A5 3.20 65.0 - 11 AIRBUS A319-112/P CFM56-5B6/P 123.45 64.9 10 8,15 CESSNA CARAVAN I PT6A-114 7.30 64.9 10 GULFSTREAM GULFSTREAM IV - SP RR TAY 611-8 74.60 64.9 20 8,15 CESSNA S550 (SII) JT15D-4B 15.10 64.8 7 8,15 MOONEY M20M TIO-540-AF1A 3.37 64.8 11,21 BEECH 300/300C KING AIR PT6A-60A 14.00 64.7 - BOEING B-717-200 BR700-715C1-30 104.50 64.7 5 8,15,52 CASA AIRCRAFT C-212-CD TPE 331-10R-512C/502C 16.98 64.7 10 15 CASA AIRCRAFT C-212-CE TPE 331-10R-512C/502C 16.98 64.7 10 15 CASA AIRCRAFT C-212-DF TPE 331-10R- 16.98 64.7 10 15 502C/512C/513C AIRBUS A319-114 CFM56-5A5 123.45 64.6 10 8,15 AIRBUS A319-132 V2524-A5 123.45 64.3 8,15 GULFSTREAM GULFSTREAM IV RR TAY 611-8 73.20 64.2 10 8,15 SAAB SF340B (HS14RF-19 props) GE CT7-9B 29.00 64.2 15 8,15 PAGE 33T
AC36-3H 4/5/2012 APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***TAKEOFF*** TOGW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES SAAB SF340B (Dowty props) GE CT7-9B 29.00 64.1 15 8,15 DASSAULT FALCON 2000 CFE738-1-1B 36.50 64.0 20 8,15 GULFSTREAM 680FL IGSO-540-B1A 8.50 64.0 - 11 MITSUBISHI MU-2B-26A TPE-331-5-252M 10.00 64.0 - 4 PIPER PA-34-200T TSI0-360-E 4.80 64.0 - 11 PIPER PA-34-220T TSIO-360-KB 4.75 64.0 - 11 MOONEY M20M TIO-540-AF1A 3.20 63.9 11,21 AEROSPATIALE SN601 CORVETTE JT15D-4 13.90 63.8 15 4 BAE SYSTEMS (JETSTREAM) JETSTREAM 31 TPE331-10U-501H 15.20 63.7 - 15 SAAB 2000 AE2100A 49.60 63.5 15 8,15 SAAB SF340B (HS14RF-19 props) GE CT7-9B 28.50 63.5 15 8,15 SAAB SF340B (Dowty props) GE CT7-9B 28.50 63.4 15 8,15 EMBRAER EMB-120 BRASILIA PW115 21.20 63.2 15 12 MAULE MX7-235 0540-JIA5D 2.50 63.2 - 11 BEECH 58 (3BLD) IO-520-C 5.40 63.0 - 11 BEECH B60 TI0-541-E1C4 6.80 63.0 - 10,11 BEECH C24R IO-360-A1B6 2.80 63.0 - 11 BEECH E55 (3BLD) IO-520-C 5.30 63.0 - 11 CESSNA 172N 0-320-H2AD 2.30 63.0 - 10 CESSNA CONQUEST I PT6A-112 8.20 63.0 - 10,11 CESSNA CONQUEST II TPE-331-8 9.80 63.0 - 5,11 GULFSTREAM 112 IO-360-C1D6 2.70 63.0 - 11 GULFSTREAM GA-7 O-320-D1D 3.80 63.0 - 4 PIPER PA-28-200 I0-360-C1C 2.70 63.0 - SAAB SF340A (Dowty props) GE CT7-5A2 28.00 62.9 15 8,15 CANADAIR RJ (CL-600-2B19) CF34-3A1 47.50 62.7 20 15 CESSNA CITATION JET II (525A) FJ44-2C 12.38 62.7 15 8,15 PAGE 34T
APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***TAKEOFF***
TOGW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES FAIRCHILD DORNIER 328-300 Mod 10 PW306B 34.52 62.7 12 8,15 SAAB SF340A (Dowty props) GE CT7-5A2 27.27 62.7 15 8,15 CESSNA CITATION II (550) JT15D-4 13.30 62.6 15 8,15 BOMBARDIER DHC-8-400 (Q400) PWC 150A 65.20 62.5 5 8,15 BOMBARDIER DHC-8-400 (Q400) PWC 150A 65.20 62.5 5 8,15,42 BOMBARDIER DHC-8-401 (Q400) PWC 150A 65.20 62.5 5 8,15,42 BOMBARDIER DHC-8-401 (Q400) PWC 150A 65.20 62.5 5 8,15 BOMBARDIER DHC-8-402 (Q400) PWC 150A 65.20 62.5 5 8,15,42 BOMBARDIER DHC-8-402 (Q400) PWC 150A 65.20 62.5 5 8,15 FAIRCHILD DORNIER 328-300 PW306B 33.51 62.2 12 8,15 BEECH 76 I0-360-A1G6D 3.90 62.0 - 11 BEECH A100 PT6A-28 11.50 62.0 - 4 BEECH F90 KINGAIR PT6A-135 10.90 62.0 - 5,11 GULFSTREAM 695 TPE-331-10 10.30 62.0 - 5,15 GULFSTREAM 695 COMMANDER 980 TPE-331-10 10.30 62.0 - 5,11 PIPER PA-31T PT6A-28 9.00 62.0 - 4 PIPER PA-44-180 O-360-E1A6D 3.80 62.0 - 11 PIPER PA-44-180T(2BLD) TO-360-E1A6D 3.90 62.0 - 11 GULFSTREAM 690D COMMANDER 900 TPE-331-5 10.70 61.7 - 10 GULFSTREAM 695A COMMANDER 1000 TPE-331-10 11.20 61.6 - 5,11 BEECH B100 KINGAIR TPE-331-6 11.80 61.5 - 11 CESSNA CITATION BRAVO (550) PW530A 14.80 61.3 15 8,15 GULFSTREAM 690C COMMANDER 840 TPE-331-5 10.30 61.3 - 5,11 BOMBARDIER DHC-8-400 (Q400) PWC 150A 61.70 61.0 5 8,15 BOMBARDIER DHC-8-400 (Q400) PWC 150A 61.70 61.0 5 8,15,42 BOMBARDIER DHC-8-401 (Q400) PWC 150A 61.70 61.0 5 8,15 BOMBARDIER DHC-8-401 (Q400) PWC 150A 61.70 61.0 5 8,15,42 PAGE 35T
AC36-3H 4/5/2012 APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***TAKEOFF*** TOGW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES BOMBARDIER DHC-8-402 (Q400) PWC 150A 61.70 61.0 5 8,15,42 BOMBARDIER DHC-8-402 (Q400) PWC 150A 61.70 61.0 5 8,15 CESSNA 172 O-320-E2D 2.30 61.0 - 11 CESSNA 404 GTSIO-520-M 8.40 61.0 - 11 CESSNA 421C GTSIO-520-L 7.50 61.0 - 11 OSTMECKLENBURGISCHE OMF-100-160 O-320-D2A 1.96 61.0 - 11,21
FLUGZEUGBAU LEARJET LEARJET 60 PW305A 23.50 60.9 8 8,15 LEARJET LEARJET 60 PW305A 23.10 60.9 8,15 LEARJET LEARJET 45 TFE731-20R-1B 20.50 60.7 8 8,15 CESSNA CITATION EXCEL (560XL) PW545 20.00 60.6 7 8,15 CESSNA CITATION JET (525) FJ44-1A 10.40 60.3 15 8,15 GULFSTREAM AA-5A O-320-E2G 2.20 60.0 - 11 PIPER PA-28-140 O-320-E3D 2.20 60.0 - 11 PIPER PA-28-151 O-320-E3D 2.20 60.0 - 11 PIPER PA-28-181 O-360-A4M 2.55 60.0 - 11 PIPER PA-44-180T(3BLD) TO-360-E1A6D 3.90 60.0 - 11 BEECH C23 0-360-A4K 2.50 59.0 - 11 GULFSTREAM 560E GO-480-C1B6 6.50 59.0 - 11 PIPER PA-28-161 O-320-D3G 2.40 59.0 - 11 CESSNA CITATION ENCORE (560) PW535A 16.63 58.3 7 8,15 BEECH A-23 IO-360-A 2.40 58.0 - 11 BEECH D95A TRAVELAIR IO-320-B1B 4.20 58.0 - 11 BELLANCA 8GCBC 0-360-C2E 2.20 58.0 - 11 MOONEY M20J I0-360-A1B6D 2.70 58.0 - 4 CLASSIC AIRCRAFT WACO CLASSIC F-5 R-755-B2 2.70 57.8 - 11 GULFSTREAM AA-5B TIGER O-360-A4K 2.20 57.4 - 10,11 GULFSTREAM AA-1B O-235 1.60 57.1 - 11 PAGE 36T
APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***TAKEOFF***
TOGW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES PIPER CHEYENNE 400LS TPE-331-14 12.05 57.0 - 11 BEECH 77 O-235-L2C 1.70 56.0 - 11 CESSNA 150 0-200-A 1.60 56.0 - 11 PIPER PA-30 TWIN COMANCHE IO-320-B 3.60 56.0 - 11 PIPER PA-38-112 O-235-L2C 1.70 56.0 - 11 CESSNA 150M O-200-A 1.60 55.0 - 11 CESSNA 152 0-235-L2C 1.70 55.0 - 11 PIPER PA-18-150 0-320-A2B 1.80 53.0 - 11 BELLANCA 7GCAA 0-320-A2B 1.70 51.0 - 4 PAGE 37T
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 CONCORDE CONCORDE O-593/M-602 109.5 - 4,8 LOCKHEED 1329 JETSTAR JT12A-8 35.00 101.0 50 8,13 IAI 1121 COMMODORE CJ610-5 18.50 100.0 - 4 IAI 1123 WESTWIND CJ610-9 19.00 99.0 - 4 MESSERSCHMITT HFB-320 HANSA CJ610-9 19.40 99.0 - 13 RAYTHEON HAWKER 125- 3A/R VIPER-522 20.00 98.7 50 8,15 RAYTHEON HAWKER 125- 3A/RA VIPER-522 20.00 98.7 45 8,15 RAYTHEON HAWKER 125- 400A VIPER-522 20.00 98.7 45 8,15 AIRBUS UK 1-11-500 SPEY-MK512 87.00 98.6 45 4 RAYTHEON HAWKER 125- 1A VIPER-522 19.60 98.5 50 8,15 BOEING B-707-300B/C (COMTRAN QN) JT3D-3B 247.00 98.4 25 8 BOEING B-747-100 JT9D-7F 585.00 97.8 30 4,6 BOEING B-747-100 JT9D-7FWET 585.00 97.8 30 4,6 BOEING B-747-100 JT9D-7WET 585.00 97.3 30 4,6 MCDONNELL DOUG. DC-10-30 CF6-50C1 411.00 97.3 50 15 BOEING B-747-100 JT9D-7 564.00 97.2 30 4,6 BOEING B-747-200 JT9D-7FWET 630.00 97.2 30 4,6 BOEING B-747-200 RB211-524B 630.00 97.2 30 4 MCDONNELL DOUG. DC-10-30 CF6-50C1 403.00 97.1 50 15 MCDONNELL DOUG. DC-10-40 JT9D-59A 403.00 97.1 50 15 BOEING B-747-200/300 RB211-524C2 585.00 96.8 30 15 BOEING B-747-200 JT9D-7WET 630.00 96.7 30 4,6 BOEING B-747-200 JT9D-7F 564.00 96.6 30 4,6 BOEING B-747-200/300 RB211-524C2 564.00 96.5 30 15 MCDONNELL DOUG. DC-10-30 CF6-50CA 424.00 96.3 50 15 AIRBUS UK 1-11-400 SPEY-MK511 78.00 96.2 45 8,15 MCDONNELL DOUG. DC-10-30 CF6-50C 411.00 96.2 50 15 PAGE 1A
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 BOEING B-747-200 JT9D-3AWET 585.00 96.1 30 4,6 BOEING B-747-200 JT9D-7 564.00 96.1 30 4,6 BOEING B-747-SR JT9D-7A 564.00 96.1 30 4,6 BOEING B-727-100 JT8D-9FCD 137.50 96.0 40 3,8,15 MCDONNELL DOUG. DC-08-63 (ADC QN) JT3D-3B 245.00 96.0 50 8,15 MCDONNELL DOUG. DC-09-30 JT8D-7 99.00 96.0 50 8,15 MCDONNELL DOUG. DC-10-30 CF6-50A 403.00 96.0 50 15 RAYTHEON HAWKER 125- 600A VIPER 601-22 22.00 96.0 45 8,15,16 BOEING B-747-200 JT9D-3A 564.00 95.9 30 4,6 BOEING B-747-200/300 RB211-524C2 666.00 95.9 25 15 MCDONNELL DOUG. DC-08-63F (ADC QN) JT3D-7 245.00 95.9 50 8,15 MCDONNELL DOUG. DC-09-10 JT8D-7 81.70 95.7 50 8,15 MCDONNELL DOUG. DC-10-10 CF6-6D 363.50 95.7 50 15 MCDONNELL DOUG. DC-10-10 CF6-6D1 363.50 95.7 50 15 BOEING B-747-SR JT9D-7A 564.00 95.6 30 4,6 MCDONNELL DOUG. DC-08-63 (TNC QN) JT3D-3B 250.00 95.4 50 8,15 SABRELINER CORP. SABRE 60A JT12A-8 20.60 95.4 - 8,12 BOEING B-747-200/300 RB211-524C2 564.00 95.3 25* 15 BOEING B-747-200 JT9D-70A 630.00 95.2 30 4 MCDONNELL DOUG. DC-08-63 (TNC QN) JT3D-7 275.00 95.2 35 8,15 MCDONNELL DOUG. DC-10-10 CF6-6D 363.50 95.1 50 15 MCDONNELL DOUG. DC-10-30 CF6-50C2 411.00 95.1 50 8,15 MCDONNELL DOUG. DC-10-30 CF6-50C2B 411.00 95.1 50 8,15 BOEING B-747-200/300 CF6-80C2B1F 666.00 95.0 30 8,15 MCDONNELL DOUG. DC-10-40 JT9D-20 403.00 94.9 50 15 MCDONNELL DOUG. DC-10-40 JT9D-59A 403.00 94.9 35* 15 BOEING B-747-200/300 CF6-50E 630.00 94.8 30 8,15 PAGE 2A
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-28 MK1000 SPEY MK555-15 59.00 94.7 42 4 LEARJET LEARJET 24D CJ610-6 11.90 94.7 40 4,8,17 MCDONNELL DOUG. DC-10-10 CF6-6D1 363.50 94.7 50 15 BOEING B-727-100 JT8D-7FCD 137.50 94.5 40 3,8,14,15 MCDONNELL DOUG. DC-08-50 (QNC QN) JT3D-3B 240.00 94.5 - 8,12 MCDONNELL DOUG. DC-08-61 (QNC QN) JT3D-3B 240.00 94.5 - 8,12 MCDONNELL DOUG. DC-10-40 JT9D-20 403.00 94.5 50 15 BOEING B-747-200/300 CF6-50E 564.00 94.4 30 8,15 BOEING B-747-400F PW4056 PKG A (FB2T) 666.00 94.4 30 8,15 AIRBUS UK 1-11-200 SPEY-MK506 71.00 94.3 45 15 BOEING B-747-400 PW4056 PKG A (FB2T) 652.00 94.3 30 8,15 BOEING B-747-400F CF6-80C2B1F 666.00 94.3 30 8,15 BOEING B-747-400F CF6-80C2B1F W/N1 MOD 666.00 94.3 30 8,15 BOEING B-747-200/300 CF6-50E2 630.00 94.2 30 8,15 BOEING B-747-400 CF6-80C2B1F 652.00 94.2 30 8,15 BOEING B-747-400 CF6-80C2B1F W/N1 MOD 652.00 94.2 30 8,15 BOEING B-747-400D CF6-80C2B1F 630.00 94.2 30 8,15 BOEING B-747-400D CF6-80C2B1F W/N1 MOD 630.00 94.2 30 8,15 MCDONNELL DOUG. DC-10-30 CF6-50C2 403.00 94.2 50 8,15 MCDONNELL DOUG. DC-10-30 CF6-50C2B 424.00 94.2 50 8,15 MCDONNELL DOUG. DC-10-30 CF6-6K 403.00 94.2 50 15 BOEING B-747-200/300 RB211-524D4 666.00 94.1 30 8,15 BOEING B-747-400 PW4056 PKG A (FB2T) 564.00 94.1 25* 8,15 BOEING B-747-400F PW4056 PKG A (FB2T) 630.00 94.1 25* 8,15 BOEING B-747-400F PW4056 PKG A (FB2T) 630.00 94.1 30 8,15 FOKKER F-28 MK1000 SPEY MK555-15 59.00 94.1 42 4 BOEING B-747-400 PW4056 PKG A (FB2T) 652.00 94.0 25* 8,15 PAGE 3A
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 BOEING B-747-400F PW4056 PKG A (FB2T) 666.00 94.0 25* 8,15 BOEING B-747-100 CF6-45A2 605.00 93.9 30 8,15 BOEING B-747-100 CF6-50E2 605.00 93.9 30 8,15 BOEING B-747-400 PW4056 PHASE 1/PKG B 652.00 93.9 30 8,15 BOEING B-747-400 PW4056 PKG A (FB2T) 564.00 93.9 30 8,15 BOEING B-747-400D CF6-80C2B1F 564.00 93.9 30 8,15 BOEING B-747-400D CF6-80C2B1F W/N1 MOD 564.00 93.9 30 8,15 BOEING B-747-400F CF6-80C2B1F 630.00 93.9 30 8,15 BOEING B-747-400F CF6-80C2B1F W/N1 MOD 630.00 93.9 30 8,15 BOEING B-747-200/300 CF6-50E 666.00 93.8 25 8,15 BOEING B-747-400 PW4056 PHASE 3 (FB2B) 652.00 93.8 30 8,15 LEARJET LEARJET 25B/C CJ610-6 13.30 93.8 40 4,8,18 MCDONNELL DOUG. DC-09-30 JT8D-9 99.00 93.8 50 8,15 SABRELINER CORP. SABRE 70 JT12A-8 18.50 93.8 - 8,12 BOEING B-747-200/300 CF6-80C2B1F 564.00 93.7 30 8,15 BOEING B-747-200/300 RB211-524D4 666.00 93.5 25* 8,15 BOEING B-747-200/300 RB211-524D4 564.00 93.5 30 8,15 BOEING B-747-200/300 RB211-524D4 564.00 93.5 25* 8,15 BOEING B-747-400 PW4056 PHASE 3 (FB2C) 652.00 93.5 30 8,15 BOEING B-747-SP JT9D-7FWET 475.00 93.5 30 4,6 MCDONNELL DOUG. DC-08-63 (BAC/BACII) JT3D-7 275.00 93.5 35 8,15,16 MCDONNELL DOUG. DC-08-63 (BAC/R1) JT3D-7 275.00 93.5 35 8,15,16 MCDONNELL DOUG. DC-10-30 CF6-50C1 421.00 93.5 35* 15 BOEING B-747-100 CF6-45A2 564.00 93.4 30 8,15 BOEING B-747-100 CF6-50E2 564.00 93.4 30 8,15 BOEING B-747-200/300 CF6-50E2 564.00 93.4 30 8,15 BOEING B-747-400 PW4056 PHASE 1/PKG B 564.00 93.4 30 8,15 PAGE 4A
15 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 MCDONNELL DOUG. DC-10-30 CF6-50A 403.00 93.4 35* BOEING B-747-200/300 CF6-80C2B1F 666.00 93.3 25* 8,15 BOEING B-747-400 CF6-80C2B1F 564.00 93.3 30 8,15 BOEING B-747-400 CF6-80C2B1F W/N1 MOD 564.00 93.3 30 8,15 BOEING B-747-400 PW4056 PHASE 3 (FB2B) 564.00 93.3 30 8,15 BOEING B-747-400 PW4056 PHASE 1/PKG B 652.00 93.2 25* 8,15 MCDONNELL DOUG. DC-08-63 (BAC/BACII) JT3D-7 258.00 93.2 35 8,15,16 BOEING B-747-400 PW4056 PHASE 1/PKG B 564.00 93.1 25* 8,15 BOEING B-747-400 PW4056 PHASE 3 (FB2B) 652.00 93.1 25* 8,15 BOEING B-747-400 PW4056 PHASE 3 (FB2C) 564.00 93.1 30 8,15 BOEING B-747-400F RB211-524G 666.00 93.1 30 8,15 BOEING B-747-400F RB211-524H 666.00 93.1 30 8,15 BOEING B-747-SP JT9D-7A 450.00 93.1 30 4,6 BOEING B-747-SP JT9D-7F 475.00 93.1 30 4,6 MCDONNELL DOUG. DC-08-62 (BAC/BACII) JT3D-7 250.00 93.1 35 8,15,16 MCDONNELL DOUG. DC-08-62 (BAC/R1) JT3D-7 250.00 93.1 35 8,15,16 BOEING B-747-200/300 CF6-50E2 666.00 93.0 25 8,15 BOEING B-747-400 PW4056 PHASE 3 (FB2B) 564.00 93.0 25* 8,15 BOEING B-747-400 PW4056 PHASE 3 (FB2C) 652.00 93.0 25* 8,15 BOEING B-747-400 PW4056 PHASE 3 (FB2C) 564.00 93.0 25* 8,15 BOEING B-747-400 RB211-524G 652.00 93.0 30 8,15 BOEING B-747-400 RB211-524H 652.00 93.0 30 8,15 BOEING B-747-400D CF6-80C2B1F 630.00 93.0 25* 8,15 BOEING B-747-400D CF6-80C2B1F W/N1 MOD 630.00 93.0 25* 8,15 BOEING B-747-400F CF6-80C2B1F 666.00 93.0 25* 8,15 BOEING B-747-400F CF6-80C2B1F W/N1 MOD 666.00 93.0 25* 8,15 BOEING B-747-400F PW4056 FB2B/2C 666.00 93.0 30 8,15 PAGE 5A
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 MCDONNELL DOUG. DC-08-62 (BAC/BACII) JT3D-7 240.00 93.0 35 8,15,16 MCDONNELL DOUG. DC-10-30 CF6-50A 403.00 93.0 35* 15 BOEING B-747-200/300 CF6-50E 564.00 92.9 25* 8,15 BOEING B-747-400 CF6-80C2B1F 652.00 92.9 25* 8,15 BOEING B-747-400 CF6-80C2B1F W/N1 MOD 652.00 92.9 25* 8,15 BOEING B-747-400 RB211-524G 585.00 92.8 25 8,15 BOEING B-747-400 RB211-524H 585.00 92.8 25 8,15 BOEING B-747-400F CF6-80C2B1F 630.00 92.8 25* 8,15 BOEING B-747-400F CF6-80C2B1F W/N1 MOD 630.00 92.8 25* 8,15 BOEING B-747-400F PW4056 FB2B/2C 630.00 92.8 30 8,15 BOEING B-747-400F RB211-524G 630.00 92.8 30 8,15 BOEING B-747-400F RB211-524H 630.00 92.8 30 8,15 BOEING B-747-SP JT9D-7A 450.00 92.8 30 4,6 BOEING B-747-200/300 CF6-80C2B1F 564.00 92.7 25* 8,15 LOCKHEED L-1011-1 RB211-22C 358.00 92.7 42 BOEING B-747-100 CF6-45A2 605.00 92.6 25* 8,15 BOEING B-747-100 CF6-50E2 605.00 92.6 25* 8,15 BOEING B-747-400D CF6-80C2B1F 564.00 92.6 25* 8,15 BOEING B-747-400D CF6-80C2B1F W/N1 MOD 564.00 92.6 25* 8,15 BOEING B-747-400F RB211-524G 630.00 92.6 25* 8,15 BOEING B-747-400F RB211-524H 630.00 92.6 25* 8,15 AIRBUS UK 1-11-400 MK511-W/HUSHKIT 78.00 92.5 45 15 BOEING B-747-400 CF6-80C2B1F 564.00 92.5 25* 8,15 BOEING B-747-400 CF6-80C2B1F W/N1 MOD 564.00 92.5 25* 8,15 BOEING B-747-400 PW4056 PHASE 3 (FB2C) 652.00 92.5 30 8,15,23 BOEING B-747-400 RB211-524G 652.00 92.5 25* 8,15 BOEING B-747-400 RB211-524H 652.00 92.5 25* 8,15 PAGE 6A