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
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 RB211-524G 666.00 92.5 25* 8,15 BOEING B-747-400F RB211-524H 666.00 92.5 25* 8,15 BOEING B-747-400 RB211-524G 564.00 92.4 30 8,15 BOEING B-747-400 RB211-524H 564.00 92.4 30 8,15 BOEING B-747-100 CF6-45A2 564.00 92.3 25* 8,15 BOEING B-747-100 CF6-50E2 564.00 92.3 25* 8,15 BOEING B-747-200/300 CF6-50E2 564.00 92.3 25* 8,15 BOEING B-747-400F PW4056 FB2B/2C 666.00 92.3 25* 8,15 BOEING B-767-300 JT9D-7R4D(B) 320.00 92.3 30 8,15 BOEING B-767-300 JT9D-7R4E 320.00 92.3 30 8,15 MCDONNELL DOUG. DC-09-50 JT8D-17 110.00 92.3 50 1,8,15 BOEING B-727-100 JT8D-9FCD 137.50 92.2 30* 3,8,15 BOEING B-747-400F PW4056 FB2B/2C 630.00 92.2 25* 8,15 MCDONNELL DOUG. DC-09-30 JT8D-17 101.00 92.2 50 1,8,15 BOEING B-737-200 JT8D-15QN 101.00 92.1 40 2,8,15 LOCKHEED L-1011 RB211-22B 358.00 92.1 42 4,5 BOEING B-737-200 JT8D-9QN 101.70 92.0 40 2,8,14,15 BOEING B-747-400 PW4056 PHASE 3 (FB2C) 564.00 92.0 30 8,15,23 LEARJET LEARJET 24B/D W/RAISBECK CJ610-6 11.90 92.0 40 8,13 LEARJET LEARJET 25 B/C/D/F XR CJ610-6/8A 13.30 92.0 40 8,13 MCDONNELL DOUG. DC-09-50 JT8D-15 110.00 92.0 50 1,8,15 SABRELINER CORP. SABRE 40A JT12A-8 17.50 92.0 - 8,12 SABRELINER CORP. SABRE 60 JT12A-8 17.50 92.0 24 8,12 BOEING B-737-200 JT8D-15QN 101.00 91.9 40 2,8,15 BOEING B-737-200 JT8D-9QN 103.00 91.9 40 2,8,14,15 BOEING B-747-400 PW4056 PHASE 3 (FB2C) 652.00 91.9 25* 8,15,23 BOEING B-747-400 PW4056 PHASE 3 (FB2C) 564.00 91.8 25* 8,15,23 PAGE 7A
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 AIRBUS A-310-324 PW4152 271.16 91.6 40 8,15 BOEING B-737-200 JT8D-17QN 101.00 91.6 40 2,8,14,15 AIRBUS A-300B4-2C CF6-50C 293.30 91.5 25 4,8,9 MORANE-SAULNIER MS 760B (PARIS II) MARBORE VI C2 6.96 91.5 55 19 AIRBUS A-300B1 CF6-50A 269.00 91.4 25 4,8,9 AIRBUS A-300B2-1A CF6-50A 281.10 91.4 15* 4,8,9 LOCKHEED L-1011-1 RB211-22C 358.00 91.4 33* AIRBUS A-300B2-K-3C CF6-50C 286.70 91.3 25 4,8,9 BOEING B-767-200 JT9D-7R4E 300.00 91.3 30 8,15 LOCKHEED L-1011 RB211-22B 358.00 91.3 33* 4,5 BOEING B-767-300 JT9D-7R4D(B) 280.00 91.2 30 8,15 BOEING B-767-300 JT9D-7R4E 280.00 91.2 30 8,15 MCDONNELL DOUG. DC-08-61 (BAC/BAC II) JT3D-3B 240.00 91.2 35 8,15,16 MCDONNELL DOUG. DC-10-10 CF6-6D 363.50 91.1 35* 15 BOEING B-737-200 JT8D-17QN 103.50 91.0 40 2,8,14,15 BOEING B-777-300 PW4098 524.00 91.0 30 8,15 SABRELINER CORP. SABRE 80A CF700-2D-2 22.00 91.0 - 12 AIRBUS A-300B CF6-50A 269.00 90.9 25 4,8 AIRBUS A-300B2-1A CF6-50A 286.70 90.9 25 4,8,9 AIRBUS A-300B2-1C CF6-50C 286.70 90.9 25 4,8,9 MCDONNELL DOUG. DC-09-30 JT8D-15 101.00 90.9 50 1,8,15 MCDONNELL DOUG. DC-09-40 JT8D-11 102.00 90.9 50 1,8,15 MCDONNELL DOUG. DC-09-40 JT8D-15 102.00 90.9 50 1,8,15 BOEING B-737-200 JT8D-9QN 95.00 90.8 40 2,8,14,15 BOEING B-767-300 JT9D-7R4D(B) 320.00 90.8 25* 8,15 BOEING B-767-300 JT9D-7R4E 320.00 90.8 25* 8,15 LOCKHEED L-1011-1 RB211-22C 358.00 90.8 33* 8 PAGE 8A
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-09-30 JT8D-9 99.00 90.8 50 1,8,15 AIRBUS A-300B1 CF6-50A 269.00 90.7 15* 4,8,9 AIRBUS A-300B2-1A CF6-50A 281.10 90.7 25 4,8,9 AIRBUS A-300B2-1C CF6-50C 281.10 90.7 25 4,8,9 AIRBUS A-300B2-K-3C CF6-50C 286.70 90.7 15* 4,8,9 BOEING B-737-400 CFM56-3B-2 124.00 90.7 40 8,15 BOEING B-737-400 CFM56-3C-1 124.00 90.7 40 8,15 BOEING B-777-300 RR TRENT 884 524.00 90.7 30 8,15 BOEING B-777-300 RR TRENT 892 524.00 90.7 30 8,15 GULFSTREAM GULFSTREAM II SPEY MK511-8 58.50 90.7 39 8,15,16 BOEING B-727-200 JT8D-7QN 142.50 90.6 40 2,8,15 BOEING B-727-200 RE (ROHR STC JT8D-217C/JT8D-17A 164.00 90.6 30 8,15,37 SA4363NM) GULFSTREAM GULFSTREAM II SPEY MK511-8 58.50 90.6 39 8,15 MCDONNELL DOUG. DC-09-30 JT8D-9 99.00 90.6 50 1,8,15 BOEING B-767-300/300ER PW4056 320.00 90.5 30 8,15 BOEING B-767-300/300ER PW4060 320.00 90.5 30 8,15 AIRBUS A-300B2-1A CF6-50A 286.70 90.4 15* 4,8,9 AIRBUS A-300B2-1C CF6-50C 281.10 90.4 15* 4,8,9 AIRBUS A-300B2-1C CF6-50C 286.70 90.4 15* 4,8,9 BOEING B-727-200 RE (ROHR STC JT8D-217C/JT8D-15 164.00 90.4 30 8,15,37,47 SA4363NM) BOEING B-737-300 CFM56-3-B1 121.00 90.4 40 8,15 BOEING B-737-300 CFM56-3B-2 121.00 90.4 40 8,15 BOEING B-737-400 CFM56-3-B1 121.00 90.4 40 8,15 BOEING B-737-400 CFM56-3B-2 121.00 90.4 40 8,15 BOEING B-737-400 CFM56-3C-1 121.00 90.4 40 8,15 BOEING B-767-200 JT9D-7R4D 257.00 90.4 30 8,15 AIRBUS UK 1-11-200 MK506-W/HUSHKIT 71.00 90.3 45 PAGE 9A 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***
MANUFACTURER AIRPLANE ENGINE MLW 1000 LBS EST dBA FLAPS NOTES BOEING B-727-100 (Fed Ex) JT8D-7 142.50 90.3 30 8,15,16,28 BOEING B-727-200 (Fed Ex) JT8D-7 150.00 90.3 30 8,15,24,29 BOEING B-767-300/300ER CF6-80C2B7F 340.00 90.3 30 8,15 DASSAULT FALCON 20-Basic/D/E CF700-2D-2 27.32 90.3 40 8,15 MCDONNELL DOUG. DC-10-10 CF6-6D 363.50 90.3 35* 15 SABRELINER CORP. SABRE 75A CF700-2D-2 22.00 90.3 25 4 SABRELINER CORP. SABRE 80 CF700-2D-2 22.00 90.3 25 12 BOEING BOEING BOEING BOEING BOEING BOEING B-727-200 RE (ROHR STC SA4363NM) B-727-200 RE (ROHR STC SA4363NM) B-727-200 RE (ROHR STC SA4363NM) B-727-200 RE (ROHR STC SA4363NM) B-727-200 RE (ROHR STC SA4363NM) B-767-300/300ER JT8D-217C/JT8D-17 JT8D-217C/JT8D-9 JT8D-219/JT8D-15 JT8D-219/JT8D-9 JT8D-219/JT8D-9 PW4056
162.00
162.00
162.00
162.00
162.00
280.00
90.2
90.2
90.2
90.2
90.2
90.2 30 30 30 30 30 30 8,15,37,48 8,15,37,46 8,15,37,50 ,51 8,15,37,49 ,51 8,15,37,46 8,15 BOEING B-767-300/300ER PW4056 320.00 90.2 25* 8,15 BOEING B-767-300/300ER PW4060 280.00 90.2 30 8,15 BOEING B-767-300/300ER PW4060 320.00 90.2 25* 8,15 BOEING B-777-300 PW4090 524.00 90.2 30 8,15,59 MCDONNELL DOUG. DC-10-40 JT9D-20 403.00 90.2 35* 15 AIRBUS A-310-322 JT9D-7R4E1 271.16 90.1 40 8,15 BOEING BOEING BOEING BOEING B-727-200 RE (ROHR STC SA4363NM) B-727-200 RE (ROHR STC SA4363NM) B-727-200 RE (ROHR STC SA4363NM) B-737-200 ADV (AVAERO) JT8D-217C/JT8D-17 JT8D-219/JT8D-15 JT8D-219/JT8D-17 JT8D-9
159.00
159.00
162.00
88.00
90.1
90.1
90.1
90.1 30 30 30 40 8,15,37,48 8,15,37,50 ,51 8,15,37 8,15,30 BOEING B-777-300 PW4098 524.00 90.1 25* 8,15 DASSAULT FALCON 20 CF700-2D-2 27.30 90.1 25* 8,15 AIRBUS A-300B4-2C CF6-50C 293.30 90.0 15* 4,8,9 BOEING B-727-100 (Fed Ex) JT8D-7 137.50 90.0 30 8,15,16,28 PAGE 10A