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-747-400 PW4056 PKG A (FB2T) 875.00 89.8 10 8,15 IAI 1121 COMMODORE CJ610-5 18.50 89.7 - 4 IAI 1123 WESTWIND CJ610-9 20.70 89.7 - 4 MESSERSCHMITT HFB-320 HANSA CJ610-9 20.30 89.7 - 13 BOEING B-747-200/300 CF6-50E2 775.00 89.6 10 8,15 MCDONNELL DOUG. DC-08-63 (TNC QN) JT3D-7 355.00 89.6 12 8,15 BOEING B-747-200/300 CF6-50E 775.00 89.4 10 8,15 BOEING B-747-400F PW4056 PKG A (FB2T) 875.00 89.4 10 8,15 MCDONNELL DOUG. DC-08-63 (BAC/BACII) JT3D-7 353.00 89.2 12 8,15,16 MCDONNELL DOUG. DC-08-63 (BAC/R1) JT3D-7 355.00 89.2 12 8,15,16 BOEING B-727-200 (Fed Ex) JT8D-9 189.20 89.1 8,15,25,28 BOEING B-727-200 JT8D-15QN 190.50 89.0 5 2,8,14,15 BOEING B-747-400 RB211-524H 875.00 89.0 10 8,15 BOEING B-747-400F RB211-524H 875.00 89.0 10 8,15 MCDONNELL DOUG. DC-08-61 (BAC/BAC II) JT3D-3B 325.00 88.8 15 8,15,16 MCDONNELL DOUG. DC-08-62 (BAC/BACII) JT3D-7 350.00 88.8 12 8,15,16 MCDONNELL DOUG. DC-08-62 (BAC/R1) JT3D-3B 335.00 88.8 12 8,15,16 MCDONNELL DOUG. DC-10-30 CF6-6K 455.00 88.8 - 15 LOCKHEED 1329 JETSTAR JT12A-8 42.00 88.7 - 8,13 BOEING B-727-200 JT8D-17QN 190.50 88.5 5 2,8,14,15 BOEING B-727-200 (Fed Ex) JT8D-17 199.50 88.5 8,15,25,28 MCDONNELL DOUG. DC-10-10 CF6-6D 440.00 88.5 5 15 MCDONNELL DOUG. DC-09-50 JT8D-15 121.00 88.4 - 1,8,15 MCDONNELL DOUG. DC-10-40 JT9D-20 484.00 88.4 10 15 MCDONNELL DOUG. DC-09-30 JT8D-17 121.00 88.2 - 1,8,15 MCDONNELL DOUG. DC-09-50 JT8D-17 121.00 88.2 - 1,8,15 BOEING B-727-200 JT8D-7QN 172.50 88.0 5 2,8,15 PAGE 3T
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-727-200 (Fed Ex) JT8D-7 178.00 88.0 8,15,24,29 BOEING B-737-200 JT8D-15QN 117.00 88.0 1 2,8,15 BOEING B-737-200 JT8D-9QN 117.00 88.0 1 2,8,14,15 BOEING B-747-400F CF6-80C2B1F W/N1 MOD 875.00 88.0 10 8,15 BOEING B-747-400F RB211-524G 830.00 88.0 10 8,15 BOEING B-747-400 CF6-80C2B1F 875.00 87.9 10 8,15 BOEING B-747-400 CF6-80C2B1F W/N1 MOD 875.00 87.9 10 8,15 BOEING B-747-400 RB211-524G 820.00 87.9 10 8,15 SABRELINER CORP. SABRE 70 JT12A-8 21.00 87.9 - 8,12 MCDONNELL DOUG. DC-08-62 (BAC/BACII) JT3D-7 335.00 87.8 12 8,15,16 MCDONNELL DOUG. DC-08-62 (BAC/R1) JT3D-7 335.00 87.8 12 8,15,16 BOEING B-747-400 PW4056 PHASE 3 (FB2B) 875.00 87.6 10 8,15 AIRBUS UK 1-11-400 MK511-W/HUSHKIT 89.50 87.5 8 15 BOEING B-727-200 JT8D-15QN 184.20 87.5 5 2,8,14,15 BOEING B-747-400 PW4056 PHASE 1/PKG B 875.00 87.5 10 8,15 BOEING B-747-400F CF6-80C2B1F 875.00 87.5 10 8,15 MCDONNELL DOUG. DC-09-40 JT8D-11 114.00 87.5 - 1,8,15 BOEING B-737-200 JT8D-17QN 122.50 87.3 1 2,8,14,15 BOEING B-747-400 PW4056 PHASE 3 (FB2C) 875.00 87.3 10 8,15 BOEING B-727-200 (Fed Ex) JT8D-17 190.50 87.2 8,15,25,28 MCDONNELL DOUG. DC-10-30 CF6-50C2 590.00 87.2 15 8,15 LOCKHEED L-1011-1 RB211-22C 430.00 87.1 10 MCDONNELL DOUG. DC-09-30 JT8D-7 108.00 87.1 - 8,15 BOEING B-727-200 (Fed Ex) JT8D-15 190.50 87.0 8,15,25 BOEING B-737-200 JT8D-9QN 114.50 87.0 1 2,8,14,15 BOEING B-747-200/300 CF6-80C2B1F 833.00 86.9 10 8,15 LOCKHEED L-1011-1 RB211-22C 422.00 86.9 10 PAGE 4T
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-727-100 (Fed Ex) JT8D-7 174.50 86.8 8,15,16,28 BOEING B-747-400D CF6-80C2B1F W/N1 MOD 833.00 86.8 10 8,15 BOEING B-727-200 JT8D-9QN 172.50 86.7 5 2,8,14,15 BOEING B-747-400 PW4056 PKG A (FB2T) 820.00 86.7 10 8,15 BOEING B-747-400F PW4056 PKG A (FB2T) 830.00 86.7 10 8,15 BOEING B-747-400F RB211-524H 830.00 86.7 10 8,15 MCDONNELL DOUG. DC-10-30 CF6-50C2B 590.00 86.7 - 8,15 BOEING B-727-200 (Fed Ex) JT8D-7 172.60 86.6 8,15,24,29 MCDONNELL DOUG. DC-09-30 JT8D-9 108.00 86.5 - 8,15 BOEING B-747-400 RB211-524H 820.00 86.3 10 8,15 BOEING B-747-400D CF6-80C2B1F 833.00 86.3 10 8,15 BOEING B-747-400F PW4056 FB2B/2C 875.00 86.3 10 8,15 MCDONNELL DOUG. DC-09-30 JT8D-9 110.00 86.3 - 1,8,15 BOEING B-727-100 JT8D-7FCD 169.50 86.1 5 3,8,14,15 BOEING B-747-200/300 CF6-80C2B1F 820.00 86.1 10 8,15 BOEING B-747-400 PW4056 PHASE 3 (FB2C) 875.00 86.1 10 8,15,23 BOEING B-727-200 (Fed Ex) JT8D-9 173.88 86.0 8,15,24,28 GENERAL DYNAMICS CV-440 R-2800 48.00 86.0 - 5 MCDONNELL DOUG. DC-09-50 JT8D-17 115.00 85.9 - 1,8,15 AIRBUS UK 1-11-200 SPEY-MK506 80.00 85.8 8 15 BOEING B-737-200 JT8D-7QN 109.00 85.8 1 2,8,14 MCDONNELL DOUG. DC-09-30 JT8D-15 114.00 85.8 - 1,8,15 MCDONNELL DOUG. DC-09-40 JT8D-15 114.00 85.8 - 1,8,15 BOEING B-747-400F CF6-80C2B1F W/N1 MOD 830.00 85.6 10 8,15 MCDONNELL DOUG. DC-08-72 CFM56-2-C1 362.50 85.6 12 BOEING B-727-200 (Fed Ex) JT8D-9 165.60 85.5 8,15,24,28 MCDONNELL DOUG. DC-09-30 JT8D-7 108.00 85.5 - 1,8,15 PAGE 5T
AC36-3H 4/5/2012 APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
MANUFACTURER MCDONNELL DOUG.
AIRPLANE DC-09-30 ENGINE ***TAKEOFF*** JT8D-9 TOGW 1000 LBS
108.00 EST dBA
85.4 FLAPS - NOTES 1,8,15 LOCKHEED L-1011-1 RB211-22C 416.00 85.3 10 8 MCDONNELL DOUG. DC-10-10 CF6-6D1 440.00 85.3 8 15 RAYTHEON HAWKER 125- 400A VIPER-522 23.60 85.3 8,15 BOEING B-727-100 (Fed Ex) JT8D-7 160.50 85.2 8,15,16,28 BOEING B-727-200 (Fed Ex) JT8D-9 175.00 85.2 8,15,24,29 BOEING BOEING B-727-200 RE (ROHR STC SA4363NM) B-737-200 JT8D-217C/JT8D-15 JT8D-15QN
209.42
115.50
85.2
85.2 5 1 8,15,37,47 2,8,15 BOEING B-747-400 CF6-80C2B1F 820.00 85.2 10 8,15 BOEING B-747-400 CF6-80C2B1F W/N1 MOD 820.00 85.2 10 8,15 BOEING B-747-400F CF6-80C2B1F 830.00 85.2 10 8,15 LOCKHEED L-1011-1 RB211-22C 396.00 85.2 10 4,8 MCDONNELL DOUG. DC-10-10 CF6-6D 410.00 85.2 14 15 BOEING
LOCKHEED B-727-200 RE (ROHR STC SA4363NM) L-1011 JT8D-217C/JT8D-17 RB211-22B
209.50
430.00
85.1
85.1 5 14 8,15,37,48 4,5 BOEING B-727-100 JT8D-9FCD 169.50 85.0 5 3,8,15 BOEING B-777-300 RR TRENT 884 660.00 85.0 5 8,15 DOUGLAS DC-3 R-1830-90C 25.20 85.0 - 5 MCDONNELL DOUG. DC-10-40 JT9D-20 430.00 85.0 10 15 BOEING B-737-200 JT8D-9QN 109.00 84.8 1 2,8,14,15 MCDONNELL DOUG. DC-09-40 JT8D-11 107.00 84.8 - 1,8,15 RAYTHEON HAWKER 125- 3A/R VIPER-522 22.70 84.8 - 8,15 RAYTHEON HAWKER 125- 3A/RA VIPER-522 22.70 84.8 8,15 LEARJET LEARJET 23 CJ610-1 12.50 84.7 - 4,8 SABRELINER CORP. SABRE 60 JT12A-8 20.10 84.7 - 8,12 BOEING B-737-200 JT8D-17QN 115.50 84.5 1 2,8,14,15 BOEING B-747-400 PW4056 PHASE 3 (FB2B) 820.00 84.5 10 8,15 PAGE 6T
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 MCDONNELL DOUG. DC-10-30 CF6-50C2 555.00 84.4 10 8,15 BOEING B-747-400 PW4056 PHASE 1/PKG B 820.00 84.3 10 8,15 MCDONNELL DOUG. DC-09-50 JT8D-15 110.00 84.3 - 1,8,15 GULFSTREAM GULFSTREAM II SPEY MK511-8 65.50 84.2 10 8,15,16 AIRBUS UK 1-11-200 MK506-W/HUSHKIT 80.00 84.1 8 BOEING B-747-400 PW4056 PHASE 3 (FB2C) 820.00 84.1 10 8,15 MCDONNELL DOUG. DC-08-71 CFM56-2-C1 337.00 84.1 15 SABRELINER CORP. SABRE 60A JT12A-8 22.70 83.8 - 8,12 BOEING B-727-100 JT8D-7FCD 160.50 83.7 5 3,8,14,15 BOEING B-747-400F PW4056 FB2B/2C 830.00 83.7 10 8,15 MCDONNELL DOUG. MD-80 JT8D-217A 160.00 83.7 2 8,15 MCDONNELL DOUG. DC-10-30 CF6-50C2B 555.00 83.6 5 8,15 SABRELINER CORP. SABRE 40A JT12A-8 19.60 83.4 - 8,12 BOEING B-777-300 PW4090 660.00 83.3 5 8,15,59 BOEING B-747-400 PW4056 PHASE 3 (FB2C) 820.00 83.2 10 8,15,23 MCDONNELL DOUG. MD-80 JT8D-209 149.50 83.2 0 8,15 BOEING B-727-200 RE (ROHR STC JT8D-217C/JT8D-9 198.50 83.1 5 8,15,37,46 SA4363NM) MCDONNELL DOUG. MD-80 JT8D-217C 160.00 83.1 2 8,15 RAYTHEON HAWKER 125- 1A VIPER-522 21.20 83.1 - 8,15 BOEING B-777-300 RR TRENT 892 660.00 82.9 5 8,15 BOEING B-727-200 RE (ROHR STC JT8D-217C/JT8D-17A 203.10 82.8 5 8,15,37 SA4363NM) GULFSTREAM GULFSTREAM IIB/GIII SPEY MK511-8 69.70 82.8 10 8,15,16 LEARJET LEARJET 25B/C CJ610-6 15.00 82.8 20 4,8,18 BOEING B-767-300/300ER RB211-524G 407.00 82.6 5 8,15 GULFSTREAM GULFSTREAM II SPEY MK511-8 62.00 82.6 - 8,15 MCDONNELL DOUG. DC-10-30 CF6-6K 410.00 82.6 - 8,15 BOEING B-777-200 RR TRENT 884 632.50 82.5 5 8,15 PAGE 7T 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
MANUFACTURER BOEING
AIRPLANE B-727-100 ENGINE ***TAKEOFF*** JT8D-9FCD TOGW 1000 LBS
160.50 EST dBA
82.4 FLAPS 5 NOTES 3,8,15 BOEING B-737-200 JT8D-7QN 100.50 82.4 1 2,8,14 BOEING B-767-200 JT9D-7R4E 360.00 82.3 1 8,15 LEARJET LEARJET 25 B/C/D/F XR CJ610-6/8A 16.30 82.3 10 8,13 LOCKHEED 1329-25 JETSTAR TFE731-3-IE 43.80 82.3 20 4 BOEING BOEING B-727-200 RE (ROHR STC SA4363NM) B-777-200 JT8D-219/JT8D-9 RR TRENT 892
198.70
656.00
82.2
82.1 5 5 8,15,37,46 8,15 MCDONNELL DOUG. MD-80 JT8D-219 160.00 82.1 2 8,15 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-737-200 (AVAERO) JT8D-219/JT8D-15 JT8D-219/JT8D-15 JT8D-219/JT8D-17 JT8D-219/JT8D-9 JT8D-15
198.70
197.00
198.70
198.70
123.50
82.0
82.0
82.0
81.9
81.9 5 5 5 5 1 8,15,37,50,51 8,15,37,50,51 8,15,37 8,15,37,49,51 8,15,32 BOEING B-737-200 ADV (AVAERO) JT8D-9 121.50 81.9 1 8,15,31 RAYTHEON HAWKER 125- 600A VIPER 601-22 25.50 81.9 - 8,15,16 BOEING B-737-200 (AVAERO) JT8D-9 120.50 81.8 1 8,15,31 BOEING B-737-200 (AVAERO) JT8D-15 124.50 81.7 1 8,15,31 BOEING B-737-200 ADV (AVAERO) JT8D-15 123.50 81.7 1 8,15,32 BOEING B-737-200 ADV (AVAERO) JT8D-15 124.50 81.6 1 8,15,31 BOEING B-767-300 JT9D-7R4D(B) 351.00 81.6 5 8,15 BOEING B-727-100 (Dee Hwd) TAY651-54 169.50 81.5 8,15 BOEING B-737-200 (AVAERO) JT8D-9 117.50 81.5 1 8,15,30 BOEING B-767-300/300ER RB211-524H 407.00 81.5 5 8,15 MCDONNELL DOUG. MD-80 JT8D-217 149.50 81.4 0 8,15 BOEING B-727-100 (Fed Ex) JT8D-9 160.50 81.3 8,15,16,29 BOEING B-737-100 (AVAERO) JT8D-7 114.50 81.3 1 8,15,30 BOEING B-737-200 (AVAERO) JT8D-7 114.50 81.3 1 8,15,30 PAGE 8T
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-737-200 ADV (AVAERO) JT8D-9 117.50 81.3 1 8,15,30 BOEING B-777-200 PW4090 656.00 81.3 5 8,15,59 LOCKHEED L-188 501-D13 116.00 81.3 - 4,8 MCDONNELL DOUG. DC-09-30 (ABS STC165CH) JT8D-9 111.70 81.3 0 8,15,16 MCDONNELL DOUG. DC-09-40 (ABS STC165CH) JT8D-9 111.70 81.3 0 8,15,16 BOEING B-737-200 ADV (AVAERO) JT8D-7 114.50 81.2 1 8,15,30 BOEING B-767-300/300ER PW4056 407.00 81.2 5 8,15 BOEING B-777-200 RR TRENT 895 656.00 81.2 5 8,15 MCDONNELL DOUG. MD-87 JT8D-217A 149.50 81.2 1 8,15 MCDONNELL DOUG. DC-09-30 (ABS STC165CH) JT8D-7 108.50 81.1 0 8,15,16 BOEING B-777-300 PW4098 660.00 81.0 5 8,15 MCDONNELL DOUG. DC-09-30 (ABS STC1613GL) JT8D-7 105.00 81.0 0 8,15,16 NIHON YS-11A-200 DART MK 542 54.00 81.0 - 5 MCDONNELL DOUG. DC-10-10 CF6-6D1 386.50 80.9 15 15 MORANE-SAULNIER MS 760B (PARIS II) MARBORE VI C2 8.65 80.9 10 19 BOEING B-767-300 JT9D-7R4E 351.00 80.8 5 8,15 BOEING B-737-200 ADV (AVAERO) JT8D-9 115.50 80.6 1 8,15,30 BOEING B-767-300 CF6-80A 351.00 80.6 5 8,15 LEARJET LEARJET 24D CJ610-6 13.50 80.6 - 8 MCDONNELL DOUG. MD-87 JT8D-217C 149.50 80.6 1 8,15 SABRELINER CORP. SABRE 80A CF700-2D-2 25.50 80.5 - 12 BOEING B-727-200 RE (ROHR STC JT8D-217C/JT8D-17 190.50 80.4 5 8,15,37,48 SA4363NM) BOEING B-737-400 CFM56-3-B1 142.50 80.4 8,15 BOEING B-737-400 CFM56-3-B1 142.50 80.4 5 8,15 BOEING B-767-300/300ER CF6-80C2B4F W/N1 MOD 412.00 80.3 5 8,15 MCDONNELL DOUG. MD-80 JT8D-209 140.00 80.3 0 8,15 MCDONNELL DOUG. DC-09-30 (ABS STC1613GL) JT8D-7 103.00 80.2 0 8,15,16 PAGE 9T
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 GULFSTREAM GULFSTREAM II SPEY MK511-8 62.00 80.1 - 8,15,16 MCDONNELL DOUG. DC-09-40 (ABS STC165CH) JT8D-11 111.00 80.1 0 8,15,16 BOEING B-737-200 (AVAERO) JT8D-15 118.50 80.0 1 8,15,30 BOEING B-747-100 CF6-45A2 570.00 80.0 10 8,15 BOEING B-767-300/300ER PW4060 408.00 80.0 5 8,15 MCDONNELL DOUG. DC-09-30 (ABS STC1613GL) JT8D-9 105.00 80.0 0 8,15,16 AIRBUS A-310-322 JT9D-7R4E1 337.30 79.9 8,15 MCDONNELL DOUG. DC-09-30 (ABS STC165CH) JT8D-11 111.00 79.9 0 8,15,16 BOEING B-727-200 RE (ROHR STC JT8D-219/JT8D-9 190.50 79.8 5 8,15,37,46 SA4363NM) BOEING B-767-300/300ER CF6-80C2B4 407.00 79.8 5 8,15 MCDONNELL DOUG. DC-09-30 (ABS STC165CH) JT8D-7 105.00 79.8 0 8,15,16 BOEING B-737-200 ADV (AVAERO) JT8D-15 118.50 79.7 1 8,15,30 BOEING B-767-300 CF6-80A2 351.00 79.7 5 8,15 BOEING B-777-200 RR TRENT 895 632.50 79.7 5 8,15 LEARJET LEARJET 25D CJ610-6 15.00 79.7 8 8,13 LEARJET LEARJET 25F CJ610-6 15.00 79.7 8 4,8 MCDONNELL DOUG. DC-09-10 JT8D-7 90.70 79.7 10 8,15 MCDONNELL DOUG. MD-87 JT8D-219 149.50 79.7 1 8,15 SABRELINER CORP. SABRE 80 CF700-2D-2 23.30 79.6 15 12 AIRBUS A-300B4-2C CF6-50C 346.50 79.4 - 4,8,9 MCDONNELL DOUG. DC-09-30 (ABS STC1613GL) JT8D-9 103.00 79.3 0 8,15,16 FOKKER F-28 MK1000 SPEY MK555-15 65.00 79.2 6 4 AIRBUS A-300B CF6-50A 302.00 79.1 - 4,8 BOEING B-727-200 RE (ROHR STC JT8D-217C/JT8D-9 184.00 79.1 5 8,15,37,46 SA4363NM) BOEING B-767-300/300ER CF6-80C2B6 412.00 79.1 5 8,15 AIRBUS A-310-322 JT9D-7R4E1 330.69 79.0 8,15 BOEING B-777-200 RR TRENT 875 545.00 79.0 5 8,15 PAGE 10T
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 RR TRENT 877 555.00 79.0 5 8,15 AIRBUS A-310-304 CF6-80C2A2 346.12 78.9 8,15 BOEING B-737-900ER/BBJ 3 CFM56-7B26 187.70 78.9 1 8,15 MCDONNELL DOUG. DC-09-30 (ABS STC165CH) JT8D-9 105.00 78.8 0 8,15,16 BOEING B-727-200 RE (ROHR STC JT8D-217C/JT8D-15 184.00 78.7 5 8,15,37,47 SA4363NM) BOEING B-767-300/300ER CF6-80C2B6F W/N1 MOD 408.00 78.7 5 8,15 BOEING B-777-200 GE90-85B 632.50 78.7 5 8,15,57 BOEING B-777-200 GE90-90B 656.00 78.7 5 8,15,57 MCDONNELL DOUG. MD-80 JT8D-217 140.00 78.7 0 8,15 MCDONNELL DOUG. MD-80 JT8D-217A 140.00 78.7 0 8,15 BOEING B727-100RE(Rohr) JT8D-217C/JT8D-9 174.50 78.6 5 8,15,37 MCDONNELL DOUG. DC-09-10 JT8D-7 90.70 78.6 10 1,8,15 AIRBUS A-300B4-2C CF6-50C 336.60 78.5 - 4,8,9 BOEING B-767-300/300ER CF6-80C2B6F 408.00 78.5 5 8,15 BOEING B-737-400 CFM56-3B-2 150.00 78.4 5 8,15 BOEING B-737-500 CFM56-3-B1(R) 132.80 78.4 8,15 AEROSPATIALE NORD-262C BASTAN-VIIA 22.90 78.3 - 4,8 AIRBUS A-300B2-1A CF6-50A 312.40 78.3 - 4,8,9 BAE SYSTEMS (BAe) BAe-748 SERIES 2B RR-DART-MK535 46.50 78.3 15 8,15 MCDONNELL DOUG. DC-09-20 (ABS STC1613GL) JT8D-9 100.00 78.3 0 8,15,16 MCDONNELL DOUG. MD-80 JT8D-217C 140.00 78.3 0 8,15 AIRBUS A-310-324 PW4152 346.12 78.2 8,15 BOEING B-737-300 CFM56-3-B1 139.50 78.2 1 8,15 BOEING B-767-300/300ER CF6-80C2B7F 412.00 78.2 5 8,15 BOEING B727-100RE(Rohr) JT8D-219/JT8D-7B 174.50 78.1 5 8,15,37 BOEING B-737-900ER/BBJ 3 W CFM56-7B26 187.70 78.1 1 8,15,56 BOEING B-777-200 GE90-90B(BLK IV) 656.00 78.1 5 8,15,58 PAGE 11T
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