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-767-300/300ER RB211-524G 280.00 88.7 30 8,15 BOEING B-767-300/300ER RB211-524H 280.00 88.7 30 8,15 BOEING B-767-300/300ER RB211-524H 280.00 88.7 25* 8,15 BOEING B-767-300/300ER RB211-524H 320.00 88.7 25* 8,15 BOEING B-777-200 GE90-76B 460.00 88.7 30 8,15,57 BOEING B-777-200 GE90-77B 460.00 88.7 30 8,15,57 BOEING B-777-200 GE90-85B 460.00 88.7 30 8,15,57 BOEING B-777-200 GE90-90B 460.00 88.7 30 8,15,57 BOEING B-777-200 PW4074 440.90 88.7 25* 8,15 BOEING B-777-200 PW4074 445.00 88.7 25* 8,15 BOEING B-777-200 PW4077 445.00 88.7 25* 8,15 BOEING B-777-200 PW4077 440.90 88.7 25* 8,15 MCDONNELL DOUG. DC-10-30 CF6-6K 403.00 88.7 35* 8,15 BOEING B-737-800W CFM56-7B24/2 DAC 144.00 88.6 40 8,15,54,56 BOEING B-737-800W CFM56-7B26/2 DAC 144.00 88.6 40 8,15,54,56 BOEING B-737-800W CFM56-7B27/2 DAC 144.00 88.6 40 8,15,54,56 BOEING B-737-800W CFM56-7B27/2B1 DAC 144.00 88.6 40 8,15,54,56 BOEING B-767-300/300ER CF6-80C2B2F 280.00 88.6 30 8,15 BOEING B-767-300/300ER CF6-80C2B4F W/N1 MOD 280.00 88.6 30 8,15 BOEING B-767-300/300ER CF6-80C2B6F 280.00 88.6 30 8,15 BOEING B-767-300/300ER CF6-80C2B6F W/N1 MOD 280.00 88.6 30 8,15 BOEING B-777-200 RR TRENT 875 445.00 88.6 25* 8,15 BOEING B-777-200 RR TRENT 877 445.00 88.6 25* 8,15 BOEING B-777-200 RR TRENT 884 445.00 88.6 25* 8,15 BOEING B-777-200 RR TRENT 892 445.00 88.6 25* 8,15 BOEING B-777-200 RR TRENT 895 445.00 88.6 25* 8,15 MCDONNELL DOUG. DC-08-72 CFM56-2-C1 245.00 88.6 46 PAGE 17A
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-08-73 CFM56-2-C1 245.00 88.6 46 BOEING B-737-400 CFM56-3B-2 124.00 88.5 30* 8,15 BOEING B-737-400 CFM56-3C-1 124.00 88.5 30* 8,15 BOEING B-767-300/300ER CF6-80C2B4 320.00 88.5 25* 8,15 BOEING B-767-300/300ER CF6-80C2B4 280.00 88.5 30 8,15 BOEING B-767-300/300ER CF6-80C2B4F W/N1 MOD 320.00 88.5 25* 8,15 BOEING B-767-300/300ER CF6-80C2B6 280.00 88.5 30 8,15 BOEING B-767-300/300ER CF6-80C2B6 320.00 88.5 25* 8,15 BOEING B-767-300/300ER CF6-80C2B6F 320.00 88.5 25* 8,15 BOEING B-767-300/300ER CF6-80C2B6F W/N1 MOD 320.00 88.5 25* 8,15 BOEING B-767-300/300ER CF6-80C2B7F 320.00 88.5 25* 8,15 BOEING B-777-200 GE90-76B 445.00 88.5 30 8,15,57 BOEING B-777-200 GE90-76B(BLK IV) 445.00 88.5 30 8,15,58 BOEING B-777-200 GE90-77B 445.00 88.5 30 8,15,57 BOEING B-777-200 GE90-77B(BLK IV) 445.00 88.5 30 8,15,58 BOEING B-777-200 GE90-85B 445.00 88.5 30 8,15,57 BOEING B-777-200 GE90-85B(BLK IV) 445.00 88.5 30 8,15,58 BOEING B-777-200 GE90-90B 445.00 88.5 30 8,15,57 BOEING B-777-200 GE90-90B(BLK IV) 445.00 88.5 30 8,15,58 BOEING B-777-200 GE90-94B(BLK IV) 445.00 88.5 30 8,15,58 BOEING B-777-200 PW4090 445.00 88.5 25* 8,15,59 BOEING B-777-200 PW4090 at PW4074 rating 445.00 88.5 25* 8,15,59 BOEING B-777-200 PW4090 at PW4077 rating 445.00 88.5 25* 8,15,59 BOEING B-767-200/200ER CF6-80C2B2 300.00 88.4 30 8,15 BOEING B-767-200/200ER CF6-80C2B2 270.00 88.4 30 8,15 BOEING B-767-200/200ER CF6-80C2B4 270.00 88.4 30 8,15 BOEING B-767-200/200ER CF6-80C2B4 300.00 88.4 30 8,15 PAGE 18A
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-767-200/200ER PW4056 PHASE 3 (FB2C) 300.00 88.4 30 8,15,23 BOEING B-767-300/300ER CF6-80C2B2F 280.00 88.4 25* 8,15 BOEING B-767-300/300ER CF6-80C2B4 280.00 88.4 25* 8,15 BOEING B-767-300/300ER CF6-80C2B4F W/N1 MOD 280.00 88.4 25* 8,15 BOEING B-767-300/300ER CF6-80C2B6 280.00 88.4 25* 8,15 BOEING B-767-300/300ER CF6-80C2B6F 280.00 88.4 25* 8,15 BOEING B-767-300/300ER CF6-80C2B6F W/N1 MOD 280.00 88.4 25* 8,15 BOEING B-777-300 RR TRENT 884 445.00 88.4 25* 8,15 BOEING B-777-300 RR TRENT 892 445.00 88.4 25* 8,15 BOEING B-737-200 JT8D-15QN 101.00 88.3 30* 2,8,15 BOEING B-737-200 JT8D-17QN 103.50 88.3 30* 2,8,14,15 BOEING B-737-400 CFM56-3-B1 121.00 88.3 30* 8,15 BOEING B-737-400 CFM56-3B-2 121.00 88.3 30* 8,15 BOEING B-737-400 CFM56-3C-1 121.00 88.3 30* 8,15 BOEING B-737-700C/-700ER CFM56-7B20/2 DAC 134.00 88.3 40 8,15,54,55 BOEING B-737-700C/-700ER CFM56-7B22/2 DAC 134.00 88.3 40 8,15,54,55 BOEING B-737-700C/-700ER CFM56-7B24/2 DAC 134.00 88.3 40 8,15,54,55 BOEING B-737-700C/-700ER CFM56-7B26/2 DAC 134.00 88.3 40 8,15,54,55 BOEING B-737-700C/-700ER CFM56-7B27/2 DAC 134.00 88.3 40 8,15,54,55 LEARJET LEARJET 24E CJ610-6 11.90 88.3 40 4,8 LEARJET LEARJET 24F CJ610-6 11.90 88.3 40 4,8 LOCKHEED 1329-23 JETSTAR w/STAR 3 TFE731-3 36.00 88.3 59 8,15,33 LOCKHEED 1329-25 JETSTAR TFE731-3-IE 36.00 88.3 50 LOCKHEED 1329-25 JETSTAR w/STAR 3 TFE731-3 36.00 88.3 59 8,15,34 BOEING B-737-300 CFM56-3-B1 121.00 88.2 30* 8,15 BOEING B-737-300 CFM56-3B-2 121.00 88.2 30* 8,15 BOEING B-737-700C/-700ER W CFM56-7B20/2 DAC 134.00 88.2 40 8,15,54,55 ,56 PAGE 19A 4
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-737-700C/-700ER W CFM56-7B22/2 DAC 134.00 88.2 40 8,15,54,55 ,56 BOEING B-737-700C/-700ER W CFM56-7B24/2 DAC 134.00 88.2 40 8,15,54,55 ,56 BOEING B-737-700C/-700ER W CFM56-7B26/2 DAC 134.00 88.2 40 8,15,54,55 ,56 BOEING B-737-700C/-700ER W CFM56-7B27/2 DAC 134.00 88.2 40 8,15,54,55 ,56 BOEING B-777-300 PW4090 445.00 88.2 25* 8,15,59 LEARJET LEARJET 25D CJ610-6 13.30 88.2 40 8,13 LEARJET LEARJET 25F CJ610-6 13.30 88.2 40 4,8 BOEING B-737-700 CFM56-7B20/2 DAC 129.20 88.1 40 8,15,54 BOEING B-737-700 CFM56-7B22/2 DAC 129.20 88.1 40 8,15,54 BOEING B-737-700 CFM56-7B24/2 DAC 129.20 88.1 40 8,15,54 BOEING B-737-700 CFM56-7B26/2 DAC 129.20 88.1 40 8,15,54 FOKKER F-27-200 MK532-7 41.00 88.1 - BOEING B-737-500 CFM56-3-B1 114.00 88.0 30* 8,15 BOEING B-737-500 CFM56-3-B1(R) 114.00 88.0 30* 8,15 BOEING B-737-700 CFM56-7B20/2 DAC 128.00 88.0 40 8,15,54 BOEING B-737-700 CFM56-7B22/2 DAC 128.00 88.0 40 8,15,54 BOEING B-737-700 CFM56-7B24/2 DAC 128.00 88.0 40 8,15,54 BOEING B-737-700 CFM56-7B26/2 DAC 128.00 88.0 40 8,15,54 BOEING B-737-700W CFM56-7B20/2 DAC 129.20 88.0 40 8,15,54,56 BOEING B-737-700W CFM56-7B22/2 DAC 129.20 88.0 40 8,15,54,56 BOEING B-737-700W CFM56-7B24/2 DAC 129.20 88.0 40 8,15,54,56 BOEING B-737-700W CFM56-7B26/2 DAC 129.20 88.0 40 8,15,54,56 BOEING B-737-200 JT8D-9QN 95.00 87.9 30* 2,8,14,15 BOEING B-737-200 JT8D-9QN 101.70 87.9 30* 2,8,14,15 BOEING B-737-200 JT8D-9QN 103.00 87.9 30* 2,8,14,15 BOEING B-737-700W CFM56-7B20/2 DAC 128.00 87.9 40 8,15,54,56 BOEING B-737-700W CFM56-7B22/2 DAC 128.00 87.9 40 8,15,54,56 PAGE 20A 5
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-737-700W CFM56-7B24/2 DAC 128.00 87.9 40 8,15,54,56 BOEING B-737-700W CFM56-7B26/2 DAC 128.00 87.9 40 8,15,54,56 BOEING B-757-200 PW2037 210.00 87.9 30 8,15 BOEING B-757-200 PW2037(BG-3) 210.00 87.9 30 8,15,39 BOEING B-757-200 PW2040 210.00 87.9 30 8,15 BOEING B-737-900ER/BBJ 3 CFM56-7B26 157.30 87.8 40 8,15 BOEING B-737-900ER/BBJ 3 CFM56-7B27 157.30 87.8 40 8,15 BOEING B-737-900ER/BBJ 3 CFM56-7B27/B1 157.30 87.8 40 8,15 BOEING B-777-200 GE90-76B(BLK IV) 470.00 87.8 25* 8,15,58 BOEING B-777-200 GE90-77B(BLK IV) 470.00 87.8 25* 8,15,58 BOEING B-777-200 GE90-85B(BLK IV) 470.00 87.8 25* 8,15,58 BOEING B-777-200 GE90-90B(BLK IV) 470.00 87.8 25* 8,15,58 BOEING B-777-200 GE90-94B(BLK IV) 470.00 87.8 25* 8,15,58 BOEING B-737-300 CFM56-3-B1 110.00 87.7 30* 8,15 BOEING B-737-300 CFM56-3B-2 110.00 87.7 30* 8,15 BOEING B-737-600 CFM56-7B/2 DAC (B18 120.50 87.7 40 8,15,54 derate) BOEING B-737-600 CFM56-7B20/2 DAC 120.50 87.7 40 8,15,54 BOEING B-737-600 CFM56-7B22/2 DAC 120.50 87.7 40 8,15,54 BOEING B-777-200 GE90-76B 460.00 87.7 25* 8,15,57 BOEING B-777-200 GE90-77B 460.00 87.7 25* 8,15,57 BOEING B-777-200 GE90-85B 460.00 87.7 25* 8,15,57 BOEING B-777-200 GE90-90B 460.00 87.7 25* 8,15,57 BAE SYSTEMS (AVRO) 146-RJ 100 LF507-1F 88.50 87.6 33 8,15,22 BAE SYSTEMS (BAe) BAe-146-300A LF507 88.50 87.6 33 8,15,22 BOEING B-737-900ER/BBJ 3 W CFM56-7B26 157.30 87.6 40 8,15,56 BOEING B-737-900ER/BBJ 3 W CFM56-7B27 157.30 87.6 40 8,15,56 BOEING B-737-900ER/BBJ 3 W CFM56-7B27/B1 157.30 87.6 40 8,15,56 PAGE 21A
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-777-200 GE90-76B 445.00 87.6 25* 8,15,57 BOEING B-777-200 GE90-76B(BLK IV) 445.00 87.6 25* 8,15,58 BOEING B-777-200 GE90-77B 445.00 87.6 25* 8,15,57 BOEING B-777-200 GE90-77B(BLK IV) 445.00 87.6 25* 8,15,58 BOEING B-777-200 GE90-85B 445.00 87.6 25* 8,15,57 BOEING B-777-200 GE90-85B(BLK IV) 445.00 87.6 25* 8,15,58 BOEING B-777-200 GE90-90B 445.00 87.6 25* 8,15,57 BOEING B-777-200 GE90-90B(BLK IV) 445.00 87.6 25* 8,15,58 BOEING B-777-200 GE90-94B(BLK IV) 445.00 87.6 25* 8,15,58 DASSAULT FALCON 50 TFE731-3-1C 35.72 87.6 48 8,15 AIRBUS A-310-203 CF6-80A3 267.85 87.5 40 8,15 AIRBUS A-310-203C CF6-80A3 267.85 87.5 40 8,15 BOEING B-737-500 CFM56-3-B1 105.00 87.5 30* 8,15 BOEING B-737-500 CFM56-3-B1(R) 105.00 87.5 30* 8,15 BOEING B-737-800 CFM56-7B24 146.30 87.5 40 8,15 BOEING B-737-800/BBJ 2 CFM56-7B26; -7B26/B1 146.30 87.5 40 8,15 BOEING B-737-800/BBJ 2 CFM56-7B27/B1; -7B27/B2 146.30 87.5 40 8,15 BOEING B-737-800/BBJ 2 CFM56-7B27; -7B27/B3 146.30 87.5 40 8,15 BOEING B-737-900 CFM56-7B24 147.30 87.5 40 8,15 BOEING B-737-900 CFM56-7B26 147.30 87.5 40 8,15 BOEING B-737-900 CFM56-7B27 147.30 87.5 40 8,15 BOEING B-737-900 CFM56-7B27/B1 147.30 87.5 40 8,15 BOEING B-737-900ER/BBJ 3 CFM56-7B26 149.30 87.5 40 8,15 BOEING B-737-900ER/BBJ 3 CFM56-7B27 149.30 87.5 40 8,15 BOEING B-737-900ER/BBJ 3 CFM56-7B27/B1 149.30 87.5 40 8,15 BOEING B-737-900W CFM56-7B24 147.30 87.5 40 8,15,56 BOEING B-737-900W CFM56-7B26 147.30 87.5 40 8,15,56 PAGE 22A
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-737-900W CFM56-7B27 147.30 87.5 40 8,15,56 BOEING B-737-900W CFM56-7B27/B1 147.30 87.5 40 8,15,56 AIRBUS A-310-203 CF6-80A3 261.24 87.4 40 8,15 BAE SYSTEMS (AVRO) 146-RJ 70 LF507-1F 83.50 87.4 33 8,15,22 BAE SYSTEMS (AVRO) 146-RJ 70 LF507-1F 83.50 87.4 33 8,15,22,43 BOEING B-727-200 JT8D-7QN 142.50 87.4 30* 2,8,15 BOEING B-737-800 CFM56-7B24 144.00 87.4 40 8,15 BOEING B-737-800/BBJ 2 CFM56-7B26; -7B26/B1 144.00 87.4 40 8,15 BOEING B-737-800/BBJ 2 CFM56-7B27/B1; -7B27/B2 144.00 87.4 40 8,15 BOEING B-737-800/BBJ 2 CFM56-7B27; -7B27/B3 144.00 87.4 40 8,15 BOEING B-737-800/BBJ 2 SFP CFM56-7B26; -7B26/B1 146.30 87.4 40 8,15,60 BOEING B-737-800/BBJ 2 SFP CFM56-7B27/B1; -7B27/B2 146.30 87.4 40 8,15,60 BOEING B-737-800/BBJ 2 SFP CFM56-7B27; -7B27/B3 146.30 87.4 40 8,15,60 BOEING B-737-800SFP CFM56-7B24 146.30 87.4 40 8,15,60 BOEING B-737-800W CFM56-7B24 146.30 87.4 40 8,15,56 BOEING B-737-800W/BBJ 2 CFM56-7B26; -7B26/B1 146.30 87.4 40 8,15,56 BOEING B-737-800W/BBJ 2 CFM56-7B27/B1; -7B27/B2 146.30 87.4 40 8,15,56 BOEING B-737-800W/BBJ 2 CFM56-7B27; -7B27/B3 146.30 87.4 40 8,15,56 BOEING B-737-900 CFM56-7B24 146.30 87.4 40 8,15 BOEING B-737-900 CFM56-7B26 146.30 87.4 40 8,15 BOEING B-737-900 CFM56-7B27 146.30 87.4 40 8,15 BOEING B-737-900 CFM56-7B27/B1 146.30 87.4 40 8,15 BOEING B-737-900W CFM56-7B24 146.30 87.4 40 8,15,56 BOEING B-737-900W CFM56-7B26 146.30 87.4 40 8,15,56 BOEING B-737-900W CFM56-7B27 146.30 87.4 40 8,15,56 BOEING B-737-900W CFM56-7B27/B1 146.30 87.4 40 8,15,56 MCDONNELL DOUG. DC-09-40 (ABS STC165CH) JT8D-9 101.00 87.4 40 8,15,16 PAGE 23A
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 BAE SYSTEMS (AVRO) 146-RJ 85 LF507-1F 85.00 87.3 33 8,15,22 BAE SYSTEMS (BAe) BAe-146-300A ALF-502R-5 83.00 87.3 33 8,15,22 BOEING B-737-800/BBJ 2 SFP CFM56-7B26; -7B26/B1 144.00 87.3 40 8,15,60 BOEING B-737-800/BBJ 2 SFP CFM56-7B27/B1; -7B27/B2 144.00 87.3 40 8,15,60 BOEING B-737-800/BBJ 2 SFP CFM56-7B27; -7B27/B3 144.00 87.3 40 8,15,60 BOEING B-737-800/BBJ 2 SFP W CFM56-7B26; -7B26/B1 146.30 87.3 40 8,15,56,60 BOEING B-737-800/BBJ 2 SFP W CFM56-7B27/B1; -7B27/B2 146.30 87.3 40 8,15,56,60 BOEING B-737-800/BBJ 2 SFP W CFM56-7B27; -7B27/B3 146.30 87.3 40 8,15,56,60 BOEING B-737-800SFP CFM56-7B24 144.00 87.3 40 8,15,60 BOEING B-737-800SFP W CFM56-7B24 146.30 87.3 40 8,15,56,60 BOEING B-737-800W CFM56-7B24 144.00 87.3 40 8,15,56 BOEING B-737-800W/BBJ 2 CFM56-7B26; -7B26/B1 144.00 87.3 40 8,15,56 BOEING B-737-800W/BBJ 2 CFM56-7B27/B1; -7B27/B2 144.00 87.3 40 8,15,56 BOEING B-737-800W/BBJ 2 CFM56-7B27; -7B27/B3 144.00 87.3 40 8,15,56 BOEING B-737-900ER/BBJ 3 W CFM56-7B26 149.30 87.3 40 8,15,56 BOEING B-737-900ER/BBJ 3 W CFM56-7B27 149.30 87.3 40 8,15,56 BOEING B-737-900ER/BBJ 3 W CFM56-7B27/B1 149.30 87.3 40 8,15,56 DASSAULT FALCON 50 (M1230) TFE731-3-1C 35.71 87.3 48 8,15 MCDONNELL DOUG. DC-09-40 (ABS STC165CH) JT8D-11 99.00 87.3 40 8,15,16 BAE SYSTEMS (AVRO) 146-RJ 100 LF507-1F 83.00 87.2 33 8,15,22 BAE SYSTEMS (BAe) BAe-146-200A ALF-502R-5 81.00 87.2 33 8,15,22 BAE SYSTEMS (BAe) BAe-146-300A LF507 83.00 87.2 33 8,15,22 BOEING B-737-800/BBJ 2 SFP W CFM56-7B26; -7B26/B1 144.00 87.2 40 8,15,56,60 BOEING B-737-800/BBJ 2 SFP W CFM56-7B27/B1; -7B27/B2 144.00 87.2 40 8,15,56,60 BOEING B-737-800/BBJ 2 SFP W CFM56-7B27; -7B27/B3 144.00 87.2 40 8,15,56,60 BOEING B-737-800SFP W CFM56-7B24 144.00 87.2 40 8,15,56,60 BOEING B-757-200 PW2037 198.00 87.2 30 8,15 PAGE 24A
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 PW-2037(BG-3) 198.00 87.2 30 8,15,39 BOEING B-757-200 PW2040 198.00 87.2 30 8,15 MCDONNELL DOUG. DC-09-30 (ABS STC165CH) JT8D-11 101.00 87.2 40 8,15,16 MCDONNELL DOUG. DC-09-30 (ABS STC165CH) JT8D-9 102.00 87.2 40 8,15,16 MCDONNELL DOUG. DC-09-30 (ABS STC1613GL) JT8D-7 101.00 87.1 40 8,15,16 MCDONNELL DOUG. DC-09-30 (ABS STC1613GL) JT8D-9 101.00 87.1 40 8,15,16 MCDONNELL DOUG. DC-09-30 (ABS STC165CH) JT8D-7 101.00 87.1 40 8,15,16 BAE SYSTEMS (BAe) BAe-146-100A ALF-502R-3A/-5 77.50 87.0 33 8,15,22 BAE SYSTEMS (BAe) BAe-146-200A ALF-502R-3A/-5 77.50 87.0 33 8,15,22 BAE SYSTEMS (BAe) BAe-146-300A ALF-502R-5 84.50 87.0 33 8,15,22 BOEING B727-100RE(Rohr) JT8D-217C/JT8D-9 142.50 87.0 30 8,15,37 BOEING B727-100RE(Rohr) JT8D-219/JT8D-7B 142.50 87.0 30 8,15,37 BOEING B727-100RE(Rohr) JT8D-219/JT8D-9 142.50 87.0 30 8,15,37 FAIRCHILD F-27-F RR DART MK529 36.70 87.0 - MCDONNELL DOUG. DC-09-30 (ABS STC1613GL) JT8D-7 99.00 87.0 40 8,15,16 MCDONNELL DOUG. DC-09-30 (ABS STC1613GL) JT8D-9 99.00 87.0 40 8,15,16 MCDONNELL DOUG. DC-09-30 (ABS STC165CH) JT8D-9 99.00 87.0 40 8,15,16 BOEING B-737-700C/-700ER/BBJ CFM56-7B20 134.00 86.9 40 8,15,55 BOEING B-737-700C/-700ER/BBJ CFM56-7B22 134.00 86.9 40 8,15,55 BOEING B-737-700C/-700ER/BBJ CFM56-7B24 134.00 86.9 40 8,15,55 BOEING B-737-700C/-700ER/BBJ CFM56-7B26; -7B26/B1 134.00 86.9 40 8,15,55 BOEING B-737-700C/-700ER/BBJ CFM56-7B27; -7B27/B3 134.00 86.9 40 8,15,55 BOEING B-737-800 CFM56-7B24/2 DAC 146.30 86.9 30* 8,15,54 BOEING B-737-800 CFM56-7B26/2 DAC 146.30 86.9 30* 8,15,54 BOEING B-737-800 CFM56-7B27/2 DAC 146.30 86.9 30* 8,15,54 BOEING B-737-800 CFM56-7B27/2B1 DAC 146.30 86.9 30* 8,15,54 BOEING B-737-700C/-700ER/BBJ W CFM56-7B20 134.00 86.8 40 8,15,55,56 PAGE 25A 11
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-737-700C/-700ER/BBJ W CFM56-7B22 134.00 86.8 40 8,15,55,56 BOEING B-737-700C/-700ER/BBJ W CFM56-7B24 134.00 86.8 40 8,15,55,56 BOEING B-737-700C/-700ER/BBJ W CFM56-7B26; -7B26/B1 134.00 86.8 40 8,15,55,56 BOEING B-737-700C/-700ER/BBJ W CFM56-7B27; -7B27/B3 134.00 86.8 40 8,15,55,56 BOEING B-737-800 CFM56-7B24/2 DAC 144.00 86.8 30* 8,15,54 BOEING B-737-800 CFM56-7B26/2 DAC 144.00 86.8 30* 8,15,54 BOEING B-737-800 CFM56-7B27/2 DAC 144.00 86.8 30* 8,15,54 BOEING B-737-800 CFM56-7B27/2B1 DAC 144.00 86.8 30* 8,15,54 FOKKER F-27-500/600 MK532-7R 42.00 86.8 - MCDONNELL DOUG. DC-09-20 (ABS STC1613GL) JT8D-9 93.40 86.8 40 8,15,16 AIRBUS A321-211 CFM56-5B3/P; Mod No. 166.44 86.7 25 8,15 27772 BAE SYSTEMS (AVRO) 146-RJ 85 LF507-1F 77.50 86.7 33 8,15,22 BOEING B-737-700 CFM56-7B20 129.20 86.7 40 8,15 BOEING B-737-700 CFM56-7B22 129.20 86.7 40 8,15 BOEING B-737-700 CFM56-7B24 129.20 86.7 40 8,15 BOEING B-737-700 CFM56-7B26 129.20 86.7 40 8,15 BOEING B-737-800W CFM56-7B24/2 DAC 144.00 86.7 30* 8,15,54,56 BOEING B-737-800W CFM56-7B24/2 DAC 146.30 86.7 30* 8,15,54,56 BOEING B-737-800W CFM56-7B26/2 DAC 146.30 86.7 30* 8,15,54,56 BOEING B-737-800W CFM56-7B26/2 DAC 144.00 86.7 30* 8,15,54,56 BOEING B-737-800W CFM56-7B27/2 DAC 144.00 86.7 30* 8,15,54,56 BOEING B-737-800W CFM56-7B27/2 DAC 146.30 86.7 30* 8,15,54,56 BOEING B-737-800W CFM56-7B27/2B1 DAC 144.00 86.7 30* 8,15,54,56 BOEING B-737-800W CFM56-7B27/2B1 DAC 146.30 86.7 30* 8,15,54,56 BOEING B-737-900ER/BBJ 3 CFM56-7B26 157.30 86.7 30* 8,15 BOEING B-737-900ER/BBJ 3 CFM56-7B27 157.30 86.7 30* 8,15 BOEING B-737-900ER/BBJ 3 CFM56-7B27/B1 157.30 86.7 30* 8,15 PAGE 26A 5
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 PW2037 210.00 86.7 25* 8,15 BOEING B-757-200 PW2037(BG-3) 210.00 86.7 25* 8,15,39 BOEING B-757-200 PW2040 210.00 86.7 25* 8,15 MCDONNELL DOUG. DC-09-10 (ABS STC1563GL) JT8D-7 81.70 86.7 40 8,15,16 BOEING B-737-700 CFM56-7B20 128.00 86.6 40 8,15 BOEING B-737-700 CFM56-7B22 128.00 86.6 40 8,15 BOEING B-737-700 CFM56-7B24 128.00 86.6 40 8,15 BOEING B-737-700 CFM56-7B26 128.00 86.6 40 8,15 BAE SYSTEMS (BAe) BAe-146-100A ALF-502R-3A/-5 72.40 86.5 33 8,15,22 BOEING B-737-700W CFM56-7B20 128.00 86.5 40 8,15,56 BOEING B-737-700W CFM56-7B22 128.00 86.5 40 8,15,56 BOEING B-737-700W CFM56-7B24 128.00 86.5 40 8,15,56 BOEING B-737-700W CFM56-7B26 128.00 86.5 40 8,15,56 BOEING B-737-900ER/BBJ 3 W CFM56-7B26 157.30 86.5 30* 8,15,56 BOEING B-737-900ER/BBJ 3 W CFM56-7B27 157.30 86.5 30* 8,15,56 BOEING B-737-900ER/BBJ 3 W CFM56-7B27/B1 157.30 86.5 30* 8,15,56 BOEING B-757-200 PW2037 (CBQFC) 210.00 86.5 30 8,15,40 BOEING B-757-200 PW2037 (nCBQFC) 210.00 86.5 30 8,15,41 BOEING B-757-200 PW2040 (CBQFC) 210.00 86.5 30 8,15,40 BOEING B-757-200 PW2040 (nCBQFC) 210.00 86.5 30 8,15,41 BOEING B-727-100 (Dee Hwd) TAY651-54 142.50 86.4 30 8,15 BOEING B-737-700C/-700ER CFM56-7B20/2 DAC 134.00 86.4 30* 8,15,54,55 BOEING B-737-700C/-700ER CFM56-7B22/2 DAC 134.00 86.4 30* 8,15,54,55 BOEING B-737-700C/-700ER CFM56-7B24/2 DAC 134.00 86.4 30* 8,15,54,55 BOEING B-737-700C/-700ER CFM56-7B26/2 DAC 134.00 86.4 30* 8,15,54,55 BOEING B-737-700C/-700ER CFM56-7B27/2 DAC 134.00 86.4 30* 8,15,54,55 BOEING B-737-900ER/BBJ 3 CFM56-7B26 149.30 86.4 30* 8,15 PAGE 27A
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-737-900ER/BBJ 3 CFM56-7B27 149.30 86.4 30* 8,15 BOEING B-737-900ER/BBJ 3 CFM56-7B27/B1 149.30 86.4 30* 8,15 BOEING B-737-700C/-700ER W CFM56-7B20/2 DAC 134.00 86.3 30* 8,15,54,55 ,56 BOEING B-737-700C/-700ER W CFM56-7B22/2 DAC 134.00 86.3 30* 8,15,54,55 ,56 BOEING B-737-700C/-700ER W CFM56-7B24/2 DAC 134.00 86.3 30* 8,15,54,55 ,56 BOEING B-737-700C/-700ER W CFM56-7B26/2 DAC 134.00 86.3 30* 8,15,54,55 ,56 BOEING B-737-700C/-700ER W CFM56-7B27/2 DAC 134.00 86.3 30* 8,15,54,55 ,56 FOKKER F-28 MK4000 SPEY MK555-15H 64.00 86.3 - GULFSTREAM GIIB/GIII (HAT STC ST01567LA) SPEY MK 511-8 58.50 86.3 39 8,15,16 GULFSTREAM GIIB/GIII (HAT STC ST01567LA) SPEY MK 511-8 58.50 86.3 39 8,15,16 BOEING B-737-600 CFM56-7B18 120.50 86.2 40 8,15 BOEING B-737-600 CFM56-7B20 120.50 86.2 40 8,15 BOEING B-737-600 CFM56-7B22 120.50 86.2 40 8,15 BOEING B-737-700 CFM56-7B20/2 DAC 128.00 86.2 30* 8,15,54 BOEING B-737-700 CFM56-7B20/2 DAC 129.20 86.2 30* 8,15,54 BOEING B-737-700 CFM56-7B24/2 DAC 129.20 86.2 30* 8,15,54 BOEING B-737-700 CFM56-7B24/2 DAC 128.00 86.2 30* 8,15,54 BOEING B-737-700 CFM56-7B26/2 DAC 129.20 86.2 30* 8,15,54 BOEING B-757-200 PW2037 198.00 86.2 25* 8,15 BOEING B-757-200 PW-2037(BG-3) 198.00 86.2 25* 8,15,39 BOEING B-757-200 PW2040 198.00 86.2 25* 8,15 BOEING B-757-300 RB211-535E4 224.00 86.2 30 8,15,35 BOEING B-757-300 RB211-535E4B 224.00 86.2 30 8,15,35 BOEING B-757-300 RB211-535E4C 224.00 86.2 30 8,15,35 BOEING B-727-200 JT8D-15QN 142.50 86.1 30* 2,8,14,15 BOEING B-727-200 JT8D-17QN 142.50 86.1 30* 2,8,14,15 BOEING B-727-200 JT8D-17QN 158.00 86.1 30* 2,8,14,15 PAGE 28A