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 VICKERS ARMSTRONGS VISCOUNT 745 RR DART6 MK510 72.50 78.1 - 11 BAE SYSTEMS (BAe) BAE-748 SERIES 2A RR DART MK532-2L 44.50 78.0 15 8,15 BAE SYSTEMS (BAe) BAe-748 SERIES 2B RR-DART MK535- 46.50 78.0 15 8,15
W/HUSHKIT BOEING B-737-900ER/BBJ 3 CFM56-7B27 187.70 78.0 1 8,15 BOEING B-767-300/300ER PW4060 PHASE 3 (FB2C) 412.00 78.0 - 8,15,23 BOEING B-777-200 GE90-85B(BLK IV) 632.50 78.0 5 8,15,58 FOKKER F-27-200 MK532-7 43.50 78.0 - 5 FOKKER F-27-500/600 MK532-7R 43.50 78.0 - 5 AIRBUS A-300B4-2C CF6-50C 330.00 77.9 - 4,8,9 BOEING B-737-500 CFM56-3-B1 139.00 77.9 8,15 BOEING B727-100RE(Rohr) JT8D-219/JT8D-9 174.50 77.8 5 8,15,37 BOEING B-767-300/300ER CF6-80C2B7F 407.00 77.8 5 8,15 LEARJET LEARJET 24B/D W/RAISBECK CJ610-6 13.50 77.8 10 8,13 BOEING B-737-400 CFM56-3-B1 138.50 77.7 5 8,15 BOEING B-737-400 CFM56-3-B1 138.50 77.7 8,15 BOEING B-767-200/200ER CF6-80C2B4 387.00 77.7 1 8,15 SABRELINER CORP. SABRE 75A CF700-2D-2 23.00 77.7 - 4 BOEING B-737-900ER/BBJ 3 CFM56-7B27/B1 187.70 77.6 1 8,15 BOEING B727-100RE(Rohr) JT8D-217C/JT8D-9 169.50 77.5 5 8,15,37 BOEING B-777-200 PW4074 535.00 77.5 5 8,15 BOEING B-777-200 PW4077 545.00 77.5 5 8,15 BOEING B-777-200 PW4090 at PW4074 rating 535.00 77.5 5 8,15,59 BOEING B-777-200 PW4090 at PW4077 rating 545.00 77.5 5 8,15,59 MCDONNELL DOUG. MD-80 JT8D-219 140.00 77.5 0 8,15 MCDONNELL DOUG. MD-87 JT8D-219 140.00 77.4 0 8,15 AIRBUS A-310-221 JT9D-7R4D1 313.05 77.3 8,15 AIRBUS A-310-308 CF6-80C2A8 361.55 77.3 8,15 PAGE 12T
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 AIRBUS A320-232 V2527-A5 182.98 77.3 8,15 BOEING B-767-200/200ER PW4056 PHASE 3 (FB2C) 395.00 77.3 - 8,15,23 FAIRCHILD F-27-F RR DART MK529 38.50 77.3 - AIRBUS A-310-203 CF6-80A3 313.05 77.2 8,15 AIRBUS A-310-203C CF6-80A3 313.05 77.2 8,15 BOEING B-737-400 CFM56-3C-1 150.00 77.2 5 8,15 BOEING B-737-900ER/BBJ 3 W CFM56-7B27 187.70 77.2 1 8,15,56 BOEING B-757-300 RB211-535E4 275.00 77.2 5 8,15,35 AIRBUS A-300B2-1C CF6-50C 312.40 77.1 - 4,8,9 AIRBUS A319-111 CFM56-5B5/P; Mod No. 166.44 77.1 8,15 27772 AIRBUS A319-111 CFM56-5B5/P; Mod No. 166.44 77.1 8,15 27772 AIRBUS A321-211 CFM56-5B3/P; Mod No. 205.02 77.1 8,15 27772 BOEING B727-100RE(Rohr) JT8D-219/JT8D-7B 169.50 77.1 5 8,15,37 BOEING B-737-700C/-700ER/BBJ CFM56-7B22 171.00 77.1 1 8,15,55 BOEING B-737-900 CFM56-7B24 174.20 77.1 1 8,15 BOEING B-737-900W CFM56-7B24 174.20 77.1 1 8,15,56 BOEING B-767-200 JT9D-7R4D 315.00 77.1 1 8,15 BOEING B-767-300/300ER CF6-80C2B4 380.00 77.1 5 8,15 BOEING B-777-200 GE90-94B(BLK IV) 656.00 77.0 5 8,15,58 DASSAULT FALCON 20 CF700-2D-2 28.60 77.0 10 8,15 DASSAULT FALCON 20-Basic/D/E CF700-2D-2 28.66 77.0 15 8,15 AIRBUS A-310-222 JT9D-7R4E1 313.05 76.9 8,15 BOEING B727-100RE(Rohr) JT8D-219/JT8D-9 169.50 76.9 5 8,15,37 BOEING B-737-700C/-700ER CFM56-7B22/2 DAC 171.00 76.9 1 8,15,54,55 BOEING B-737-800SFP CFM56-7B24 174.20 76.9 1 8,15,60 AIRBUS A-300B1 CF6-50A 302.00 76.8 - 4,8,9 AIRBUS A-300B2-1A CF6-50A 301.40 76.8 - 4,8,9 PAGE 13T 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
***TAKEOFF*** TOGW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES BOEING B-737-800 CFM56-7B24 174.20 76.8 1 8,15 BOEING B-737-900ER/BBJ 3 W CFM56-7B27/B1 187.70 76.8 1 8,15,56 BAE SYSTEMS (BAe) BAe-146-200A ALF-502R-5 93.00 76.7 18 8,15,22 BAE SYSTEMS (BAe) BAe-146-200A ALF-502R-3A/-5 89.50 76.5 18 8,15,22 BOEING B-737-800 CFM56-7B24/2 DAC 174.20 76.5 1 8,15,54 BOEING B-777-300 RR TRENT 884 550.00 76.5 5 8,15 BOEING B-767-300/300ER RB211-524G 340.00 76.4 5 8,15 AIRBUS A-310-203C CF6-80A3 305.55 76.3 8,15 MCDONNELL DOUG. DC-09-10 (ABS STC1563GL) JT8D-7 90.70 76.3 10 8,15,16 AIRBUS A-310-324 PW4152 330.69 76.2 8,15 AIRBUS A321-231 V2533-A5 205.02 76.2 8,15 BOEING B-767-200/200ER PW4052 351.00 76.2 1 8,15 BOEING B-777-200 RR TRENT 884 545.00 76.1 5 8,15 RAYTHEON HAWKER 125- 700A TFE731-3R-1H 25.50 76.1 - 8,15,20,26 AEROSPATIALE MOHAWK 298 PT6A-45A 23.40 76.0 - 4 AIRBUS A-300B2-1C CF6-50C 302.00 76.0 - 4,8,9 BOEING B-737-700C/-700ER/BBJ W CFM56-7B22 171.00 76.0 1 8,15,55,56 BOEING B-737-800W CFM56-7B24 174.20 76.0 1 8,15,56 FOKKER F-27 MK500/600 MK552-7R 45.90 76.0 0 15,16 FOKKER F-27-100 RR DART6 MK514 39.00 76.0 - 11 GULFSTREAM 500S IO-540-E1B5 6.80 76.0 - 10 AIRBUS A-300B2-K-3C CF6-50C 312.40 75.9 - 4,8,9 AIRBUS A-310-222 JT9D-7R4E1 305.55 75.9 8,15 BOEING B-737-800SFP W CFM56-7B24 174.20 75.9 1 8,15,56,60 BOEING B-757-200 PW2037 255.50 75.9 5 8,15 BOEING B-757-200 PW2037(BG-3) 255.50 75.9 5 8,15,39 BOEING B-757-200 RB211-535C 240.00 75.9 5 8,15 PAGE 14T
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 BOEING B-767-300/300ER CF6-80C2B2F 351.00 75.9 5 8,15 FOUND AIRCRAFT CANADA FBA-2C1 IO-540-D4A5 3.20 75.9 - 11,21 BAE SYSTEMS (BAe) BAe-146-300A LF507 101.50 75.8 8,15,22 BOEING B-767-200/200ER CF6-80C2B2 351.00 75.8 1 8,15 RAYTHEON HAWKER 125- 600A TFE731-3-1H 25.50 75.8 8,15 RAYTHEON HAWKER 125- 700A TFE731-3-1H 25.50 75.8 - 8,15,26 BAE SYSTEMS (AVRO) 146-RJ 100 LF507-1F 101.50 75.7 18 8,15,22 BOEING B727-100RE(Rohr) JT8D-217C/JT8D-9 160.50 75.7 5 8,15,37 BOEING B-737-700C/-700ER W CFM56-7B22/2 DAC 171.00 75.7 1 8,15,54,55,56 BOEING B-737-800W CFM56-7B24/2 DAC 174.20 75.7 1 8,15,54,56 BOEING B-767-300 JT9D-7R4D(B) 300.00 75.7 5 8,15 AIRBUS A-310-308 CF6-80C2A8 346.12 75.6 8,15 BOEING B-737-300 CFM56-3B-2 139.50 75.6 1 8,15 BOEING B-747-400D CF6-80C2B1F W/N1 MOD 600.00 75.6 10 8,15 BOEING B-767-300/300ER RB211-524H 340.00 75.5 5 8,15 FOKKER F-28 MK4000 SPEY MK555-15H 73.00 75.5 15 BOEING B-737-700C/-700ER/BBJ CFM56-7B24 171.00 75.4 1 8,15,55 RAYTHEON HAWKER 125- 700A TFE731-3-1H 24.20 75.4 8,15,26 BOEING B-737-400 CFM56-3B-2 138.50 75.3 5 8,15 BOEING B-737-800/BBJ 2 CFM56-7B26; -7B26/B1 174.20 75.3 1 8,15 BOEING B-747-400D CF6-80C2B1F 600.00 75.3 10 8,15 FOKKER F-27 MK500/600 MK552-7R 45.00 75.3 0 15,16 BOEING B-737-900 CFM56-7B26 174.20 75.2 1 8,15 BOEING B-737-900W CFM56-7B26 174.20 75.2 1 8,15,56 BOEING B-777-200 GE90-77B(BLK IV) 545.00 75.2 5 8,15,58 BOEING B-737-700 CFM56-7B20 154.50 75.1 1 8,15 BOEING B-737-700C/-700ER CFM56-7B24/2 DAC 171.00 75.1 1 8,15,54,55 PAGE 15T
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 BOEING B-737-700C/-700ER/BBJ CFM56-7B20 154.50 75.1 1 8,15,55 BOEING B-737-800/BBJ 2 SFP CFM56-7B26; -7B26/B1 174.20 75.1 1 8,15,60 BOEING B-757-300 RB211-535E4B 275.00 75.1 5 8,15,35 BOEING B-757-300 RB211-535E4C 275.00 75.1 5 8,15,35 BOEING B-777-200 GE90-76B 545.00 75.1 5 8,15,57 BOEING B-777-200 GE90-76B(BLK IV) 545.00 75.1 5 8,15,58 BEECH C35 E-185-11 2.70 75.0 - 11 BEECH E35 E-225-8 2.70 75.0 - 11 BOEING B-737-800 CFM56-7B26/2 DAC 174.20 75.0 1 8,15,54 BOEING B-777-300 RR TRENT 892 550.00 75.0 5 8,15 LOCKHEED 1329-25 JETSTAR w/STAR 3 TFE731-3 44.50 75.0 20 8,15,34 BOEING B-737-700 CFM56-7B20/2 DAC 154.50 74.9 1 8,15,54 BOEING B-737-700C/-700ER CFM56-7B20/2 DAC 154.50 74.9 1 8,15,54,55 BOEING B-777-200 GE90-77B 545.00 74.9 5 8,15,57 BOEING B-777-200 PW4090 545.00 74.9 5 8,15,59 BOEING B-737-700C/-700ER/BBJ W CFM56-7B24 171.00 74.8 1 8,15,55,56 BOEING B-737-900 CFM56-7B24 164.00 74.8 1 8,15 BOEING B-737-900W CFM56-7B24 164.00 74.8 1 8,15,56 BOEING B-767-300 JT9D-7R4E 300.00 74.8 5 8,15 LOCKHEED 1329-23 JETSTAR w/STAR 3 TFE731-3 44.25 74.7 20 8,15,33 MCDONNELL DOUG. MD-87 JT8D-217A 125.00 74.7 0 8,15 AIRBUS A-310-204 CF6-80C2A2 313.05 74.6 8,15 AIRBUS A320-231 V2500-A1; Mod No. 23408 171.95 74.6 8,15 AIRBUS A320-231 V2500-A1; Mod No. 23408 171.95 74.6 8,15 BOEING B-777-200 RR TRENT 892 545.00 74.6 5 8,15 BOMBARDIER BD-700-1A10 (Global Express) BR700-710-A2-20 96.00 74.6 16 8,15 LEARJET LEARJET 24F CJ610-6 12.90 74.6 20 4,8 PAGE 16T
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 BOEING B-737-700C/-700ER W CFM56-7B24/2 DAC 171.00 74.5 1 8,15,54,55,56 BOEING B-737-800/BBJ 2 CFM56-7B27; -7B27/B3 174.20 74.5 1 8,15 BOEING B-737-800/BBJ 2 SFP CFM56-7B27; -7B27/B3 174.20 74.5 1 8,15,60 BOEING B-737-900 CFM56-7B27 174.20 74.5 1 8,15 BOEING B-737-900W CFM56-7B27 174.20 74.5 1 8,15,56 BOEING B-767-300 CF6-80A 300.00 74.5 5 8,15 MCDONNELL DOUG. MD-87 JT8D-217C 125.00 74.5 0 8,15 AIRBUS A319-132 V2524-A5 166.44 74.4 8,15 BOEING B-777-300 PW4098 550.00 74.4 5 8,15 MOONEY M20F w/MODWORK STC# IO-360-E5 2.74 74.4 - 11,21 SA02204AT BOEING B-737-400 CFM56-3C-1 138.50 74.3 5 8,15 BOEING B-737-700C/-700ER/BBJ W CFM56-7B20 154.50 74.3 1 8,15,55,56 BOEING B-737-700W CFM56-7B20 154.50 74.3 1 8,15,56 BOEING B-767-200/200ER PW4052 335.00 74.3 1 8,15 CESSNA 207 IO-520-F 3.80 74.3 - 11 GENERAL DYNAMICS CV-580 501-D13 54.60 74.3 - 10 BOEING B-737-600 CFM56-7B18 145.50 74.2 1 8,15 BOEING B-737-700C/-700ER/BBJ CFM56-7B26; -7B26/B1 171.00 74.2 1 8,15,55 BOEING B-737-800 CFM56-7B27/2 DAC 174.20 74.2 1 8,15,54 BOEING B-737-900 CFM56-7B27/B1 174.20 74.2 1 8,15 BOEING B-737-900W CFM56-7B27/B1 174.20 74.2 1 8,15,56 BOEING B-737-800/BBJ 2 CFM56-7B27/B1; -7B27/B2 174.20 74.1 1 8,15 BOEING B-737-800/BBJ 2 SFP CFM56-7B27/B1; -7B27/B2 174.20 74.1 1 8,15,60 BOEING B-737-800W/BBJ 2 CFM56-7B26; -7B26/B1 174.20 74.1 1 8,15,56 AIRBUS A319-114 CFM56-5A5 163.14 74.0 10 8,15 BOEING B-737-600 CFM56-7B/2 DAC (B18 145.50 74.0 1 8,15,54 derate) BOEING B-737-700C/-700ER W CFM56-7B20/2 DAC 154.50 74.0 1 8,15,54,55,56 PAGE 17T
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 BOEING B-737-700W CFM56-7B20/2 DAC 154.50 74.0 1 8,15,54,56 BOEING B-737-800/BBJ 2 SFP W CFM56-7B26; -7B26/B1 174.20 74.0 1 8,15,56,60 GULFSTREAM G200 PW306A 34.85 74.0 25 8,15,44 GULFSTREAM G200 PW306A 34.85 74.0 25 8,15,45 BOEING B-737-700C/-700ER CFM56-7B26/2 DAC 171.00 73.9 1 8,15,54,55 BOEING B-737-800 CFM56-7B27/2B1 DAC 174.20 73.9 1 8,15,54 BOEING B-737-800W CFM56-7B26/2 DAC 174.20 73.8 1 8,15,54,56 BOEING B-767-200/200ER CF6-80C2B4 351.00 73.8 1 8,15 AIRBUS A-320-211 CFM56-5A1 162.00 73.7 - 8,15 BAE SYSTEMS (AVRO) 146-RJ 85 LF507-1F 97.00 73.7 18 8,15,22 BOEING B-737-900ER/BBJ 3 CFM56-7B26 164.00 73.7 1 8,15 BOEING B-757-200 PW2040 255.50 73.7 5 8,15 BOEING B-757-200 RB211-535E4 255.50 73.7 5 8,15,35 BOEING B-757-200 RB211-535E4 255.50 73.7 5 8,15,36 BOEING B-767-300 CF6-80A2 300.00 73.7 5 8,15 BOEING B-737-300 CFM56-3-B1 124.50 73.6 1 8,15 BOEING B-737-700C/-700ER/BBJ CFM56-7B27; -7B27/B3 171.00 73.6 1 8,15,55 BOMBARDIER BD-700-1A10 (Global Express) BR700-710-A2-20 93.50 73.6 16 8,15 CIRRUS DESIGN CORP. SR 22 IO-550-N 3.40 73.6 - 11,21 BAE SYSTEMS (AVRO) 146-RJ 70 LF507-1F 90.00 73.4 18 8,15,22 BAE SYSTEMS (BAe) BAe-146-300A LF507 95.00 73.4 8,15,22 BOEING B-737-700 CFM56-7B22 154.50 73.4 1 8,15 BOEING B-737-700C/-700ER/BBJ CFM56-7B22 154.50 73.4 1 8,15,55 BOEING B-737-800/BBJ 2 SFP W CFM56-7B27; -7B27/B3 174.20 73.4 1 8,15,56,60 BOEING B-737-800W/BBJ 2 CFM56-7B27; -7B27/B3 174.20 73.4 1 8,15,56 AIRBUS A319-112/P CFM56-5B6/P 166.44 73.3 10 8,15 AIRBUS A320-214/P CFM56-5B4/P 171.95 73.3 10 8,15 PAGE 18T
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 BAE SYSTEMS (AVRO) 146-RJ 100 LF507-1F 95.00 73.3 18 8,15,22 BOEING B-737-700C/-700ER CFM56-7B27/2 DAC 171.00 73.3 1 8,15,54,55 BOEING B-767-200/200ER PW4056 340.00 73.3 1 8,15 AEROSPATIALE ATR72-200 PW124/HS 14SF11 48.50 73.2 15 15 AIRBUS A319-131 V2522A5 158.73 73.2 10 8,15 BOEING B-737-800W/BBJ 2 CFM56-7B27/B1; -7B27/B2 174.20 73.2 1 8,15,56 GULFSTREAM GIIB/GIII (HAT STC ST01567LA) SPEY MK 511-8 69.70 73.2 10 8,15,16 BOEING B-737-600 CFM56-7B20 145.50 73.1 1 8,15 BOEING B-737-700 CFM56-7B22/2 DAC 154.50 73.1 1 8,15,54 BOEING B-737-700C/-700ER CFM56-7B22/2 DAC 154.50 73.1 1 8,15,54,55 BOEING B-737-700C/-700ER/BBJ W CFM56-7B26; -7B26/B1 171.00 73.1 1 8,15,55,56 BOEING B-737-800W CFM56-7B27/2 DAC 174.20 73.1 1 8,15,54,56 LEARJET LEARJET 24E CJ610-6 12.90 73.1 20 4,8 BEECH B55 IO-470-L 5.10 73.0 - 11 BOEING B-737-800/BBJ 2 SFP W CFM56-7B27/B1; -7B27/B2 174.20 73.0 1 8,15,56,60 BOEING B-737-900 CFM56-7B26 164.00 73.0 1 8,15 BOEING B-737-900ER/BBJ 3 CFM56-7B27 164.00 73.0 1 8,15 BOEING B-737-900ER/BBJ 3 W CFM56-7B26 164.00 73.0 1 8,15,56 BOEING B-737-900W CFM56-7B26 164.00 73.0 1 8,15,56 CESSNA T210L TSI0-520-R 3.80 73.0 - 11 GULFSTREAM GIIB/GIII (QTA STC ST03621AT) SPEY MK 511-8 69.70 73.0 0 8,15,16 MCDONNELL DOUG. MD-90-30 V2525-D5 166.00 73.0 5 8,15 AIRBUS A-320-231 V2500.A1 162.00 72.9 8,15 BAE SYSTEMS (AVRO) 146-RJ 70 LF507-1F 95.00 72.9 18 8,15,22,43 BOEING B-737-600 CFM56-7B20/2 DAC 145.50 72.9 1 8,15,54 BOEING B-737-800W CFM56-7B27/2B1 DAC 174.20 72.9 1 8,15,54,56 BOEING B-767-200 JT9D-7R4D 282.00 72.9 1 8,15 PAGE 19T
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 BOEING B-777-200 GE90-85B 545.00 72.9 5 8,15,57 BOEING B-737-700C/-700ER W CFM56-7B26/2 DAC 171.00 72.8 1 8,15,54,55,56 BOEING B-737-800SFP CFM56-7B24 155.50 72.8 1 8,15,60 BOEING B-757-200 RB211-535C 220.00 72.8 5 8,15 BOEING B-737-800 CFM56-7B24 155.50 72.7 1 8,15 BOEING B-737-900ER/BBJ 3 CFM56-7B27/B1 164.00 72.7 1 8,15 BOEING B-767-300/300ER CF6-80C2B6F 345.00 72.7 5 8,15 AIRBUS A-310-221 JT9D-7R4D1 275.57 72.6 8,15 BOEING B-737-700C/-700ER/BBJ W CFM56-7B27; -7B27/B3 171.00 72.6 1 8,15,55,56 BOEING B-777-200 GE90-76B 506.00 72.6 5 8,15,57 BOEING B-777-200 GE90-76B(BLK IV) 506.00 72.6 5 8,15,58 BOEING B-777-200 GE90-77B(BLK IV) 506.00 72.6 5 8,15,58 DASSAULT FALCON 50 (M1230) TFE731-3-1C 40.78 72.6 20 8,15 BAE SYSTEMS (JETSTREAM) JETSTREAM 4100 TPE331-14-801H/802H/805H 24.00 72.5 12,15 BOEING B-737-700C/-700ER/BBJ W CFM56-7B22 154.50 72.5 1 8,15,55,56 BOEING B-737-700W CFM56-7B22 154.50 72.5 1 8,15,56 BOEING B-777-200 GE90-77B 506.00 72.5 5 8,15,57 BOEING B-777-200 GE90-85B(BLK IV) 545.00 72.5 5 8,15,58 ESTUMKEDA LTD d.b.a MAC-145B IO-540-T4B5 2.85 72.5 - 11,21 MICCO AIRCRAFT CO.
GULFSTREAM GIIB/GIII (HAT STC ST01567LA) SPEY MK 511-8 68.20 72.5 10 8,15,16 AIRBUS A-310-203 CF6-80A3 275.57 72.4 8,15 AIRBUS A-310-204 CF6-80C2A2 295.41 72.4 8,15 AIRBUS A-310-304 CF6-80C2A2 295.41 72.4 8,15 BAE SYSTEMS (BAe) BAe-146-100A ALF-502R-3A/-5 84.00 72.4 18 8,15,22 BOEING B-737-800 CFM56-7B24/2 DAC 155.50 72.4 1 8,15,54 BOEING B-737-900 CFM56-7B27 164.00 72.4 1 8,15 BOEING B-737-900W CFM56-7B27 164.00 72.4 1 8,15,56 PAGE 20T
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 BOEING B-757-200 PW2040 (nCBQFC) 255.50 72.4 5 8,15,41 BOEING B-757-200 RB211-535E4B 255.50 72.4 5 8,15,36 GULFSTREAM GIIB/GIII (QTA STC ST03621AT) SPEY MK 511-8 68.20 72.4 0 8,15,16 RAYTHEON HAWKER 125- 3A/RA TFE731-3-1H 23.60 72.4 - 8,15 RAYTHEON HAWKER 125- 400A TFE731-3-1H 23.60 72.4 - 8,15 AEROSPATIALE ATR72-210 PW127/HS 14SF11 48.50 72.3 15 15 BOEING B-737-700C/-700ER W CFM56-7B27/2 DAC 171.00 72.3 1 8,15,54,55,56 BOEING B-737-900ER/BBJ 3 W CFM56-7B27 164.00 72.3 1 8,15,56 BOEING B-757-200 RB211-535E4B 255.50 72.3 5 8,15,35 CIRRUS DESIGN CORP. SR 20 (2 Bladed Prop) IO-360-ES 2.90 72.3 - 11,21 BOEING B-737-500 CFM56-3-B1(R) 115.50 72.2 8,15 BOEING B-737-700C/-700ER W CFM56-7B22/2 DAC 154.50 72.2 1 8,15,54,55,56 BOEING B-737-700W CFM56-7B22/2 DAC 154.50 72.2 1 8,15,54,56 DASSAULT FALCON 900 (M1196) TFE731-5AR-1C 46.50 72.2 20 8,15 BOEING B-717-200 BR700-715A1-30 (MP) 121.00 72.1 5 8,15,53 BOEING B-737-900 CFM56-7B27/B1 164.00 72.1 1 8,15 BOEING B-737-900W CFM56-7B27/B1 164.00 72.1 1 8,15,56 BOEING B-777-200 RR TRENT 875 458.00 72.1 5 8,15 CIRRUS DESIGN CORP. SR 20 (3 Bladed Prop) IO-360-ES 2.90 72.1 - 11,21 DASSAULT FALCON 20-C5/D5/E5 (M3547) TFE731-5BR-2C 30.50 72.1 15 8,15 IAI 1125 ASTRA TFE731-3A-200G 24.65 72.1 12 8,15 BOEING B-717-200 BR700-715A1-30 121.00 72.0 5 8,15,52 BOEING B-737-700 CFM56-7B24 154.50 72.0 1 8,15 BOEING B-737-700C/-700ER/BBJ CFM56-7B24 154.50 72.0 1 8,15,55 BOEING B-737-900ER/BBJ 3 W CFM56-7B27/B1 164.00 72.0 1 8,15,56 BOEING B-777-200 GE90-94B(BLK IV) 580.00 72.0 5 8,15,58 DASSAULT FALCON 20-C5/D5/E5 (M3500) TFE731-5AR-2C 29.10 72.0 15 8,15 PAGE 21T
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 FOKKER F100 RR TAY MK620-15 95.00 72.0 - 8,15 PIPER PA-28-235 O-540-B4B5 3.00 72.0 - 11 BOEING B-737-800W CFM56-7B24 155.50 71.9 1 8,15,56 GULFSTREAM GII TT (QTA STC ST03621AT) SPEY MK 511-8 65.50 71.9 0 8,15,16 MITSUBISHI MU300 DIAMOND I JT15D-4 14.10 71.9 - 12 AEROSPATIALE ATR72-210 PW127/HS 14SF11 47.40 71.8 15 15 BEECH BEECHJET 400 JT15D-5 15.80 71.8 - 15 BOEING B-737-700 CFM56-7B24/2 DAC 154.50 71.8 1 8,15,54 BOEING B-737-700C/-700ER CFM56-7B24/2 DAC 154.50 71.8 1 8,15,54,55 BOEING B-737-800SFP W CFM56-7B24 155.50 71.8 1 8,15,56,60 BOEING B-777-200 GE90-90B 545.00 71.8 5 8,15,57 GULFSTREAM GIISP (HAT STC ST01567LA) SPEY MK 511-8 64.80 71.8 20 8,15,16 MITSUBISHI MU300-10 DIAMOND II JT15D-5 15.80 71.8 - 15 RAYTHEON HAWKER 125-1000A PW305 31.00 71.8 8,15 BOEING B-737-800W CFM56-7B24/2 DAC 155.50 71.7 1 8,15,54,56 DASSAULT FALCON 20-G (M2500) ATF3-6-2C 32.00 71.7 10 8,15 DASSAULT FALCON 200 ATF3-6A-4C 32.00 71.7 5 8,15 IAI 1124IW WESTWIND IW TFE731-3-1G 23.50 71.7 12 15 BAE SYSTEMS (JETSTREAM) JETSTREAM 4100 TPE331-14-801H/802H 23.00 71.6 12,15 BOEING B-737-600 CFM56-7B22 145.50 71.6 1 8,15 GULFSTREAM GII (QTA STC ST03621AT) SPEY MK 511-8 64.80 71.6 0 8,15,16 LEARJET LEARJET 35A TFE731-2 18.00 71.6 8 15 LEARJET LEARJET 36A TFE731-2 18.00 71.6 8 15 SHORTS SKYVAN TPE-331-201 12.50 71.6 15 BOEING B-737-300 CFM56-3B-2 124.50 71.5 1 8,15 BOEING B-737-700C/-700ER/BBJ W CFM56-7B24 154.50 71.4 1 8,15,55,56 BOEING B-737-700W CFM56-7B24 154.50 71.4 1 8,15,56 PAGE 22T
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 210 IO-520-L 3.80 71.4 - 10,11 DASSAULT FALCON 20-Basic/D/E/F CF700-2D-2Q 28.66 71.4 0 8,15 (M2851) DASSAULT FALCON 20-F5 (M3547) TFE731-5BR-2C 30.50 71.4 10 8,15 BOEING B-737-600 CFM56-7B22/2 DAC 145.50 71.3 1 8,15,54 BOEING B-737-800/BBJ 2 CFM56-7B26; -7B26/B1 155.50 71.3 1 8,15 BOEING B-737-800/BBJ 2 SFP CFM56-7B26; -7B26/B1 155.50 71.3 1 8,15,60 BOEING B-767-200/200ER CF6-80A 279.90 71.3 1 8,15 BOEING B-777-200 PW4074 440.90 71.3 5 8,15 BOEING B-777-200 PW4090 at PW4074 rating 447.40 71.3 5 8,15,59 BOEING B-777-200 RR TRENT 877 458.00 71.3 5 8,15 BAE SYSTEMS (AVRO) 146-RJ 70 LF507-1F 84.00 71.2 18 8,15,22 BOEING B-737-700C/-700ER W CFM56-7B24/2 DAC 154.50 71.2 1 8,15,54,55,56 BOEING B-737-700W CFM56-7B24/2 DAC 154.50 71.2 1 8,15,54,56 DASSAULT FALCON 900 TFE731-5AR-1C 45.50 71.2 20 8,15 RAYTHEON HAWKER 125- 1A TFE731-3-1H 21.70 71.2 8,15 RAYTHEON HAWKER 125- 3A TFE731-3-1H 21.70 71.2 8,15 SHORTS 3-30 PT6A-45A 22.40 71.2 - 8,15 BAE SYSTEMS (AVRO) 146-RJ 85 LF507-1F 89.50 71.1 18 8,15,22 BEECH C99 AIRLINER PT6A-34 11.30 71.1 - 5,11 BOEING B-737-800 CFM56-7B26/2 DAC 155.50 71.1 1 8,15,54 MCDONNELL DOUG. MD-90-30 V2525-D5 156.00 71.1 5 8,15 AIRBUS A-320-111 CFM56-5A1 149.90 71.0 8,15 BEECH 35-B33 I0-470-K 3.00 71.0 - 10,11 BEECH A36 IO-520-BA 3.60 71.0 - 11 BEECH B36TC BONANZA TSIO-520U 3.85 71.0 - 11 BEECH B55(3BLD) IO-470-L 5.10 71.0 - 11 BOEING B-737-500 CFM56-3-B1 115.50 71.0 8,15 PAGE 23T