AC36-3H 4/5/2012 APPENDIX 2, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
TOGW MLW TO APP APP MANUFACTURER AIRPLANE ENGINE 1000 LBS 1000 LBS dBA dBA FLAPS NOTES FOKKER F70 RR TAY MK620-15 81.00 75.00 65.4 78.6 42 8,15 FOKKER F70 RR TAY MK620-15 92.00 81.00 69.2 79.0 42 8,15 FOUND AIRCRAFT FBA-2C1 IO-540-D4A5 3.20 3.20 75.9 63.1 - 11,21 CANADA GENERAL DYNAMICS CV-440 R-2800 48.00 47.20 86.0 84.0 - 5 GENERAL DYNAMICS CV-580 501-D13 54.60 52.00 74.3 85.7 - 10 GULFSTREAM 112 IO-360-C1D6 2.70 2.70 63.0 62.0 - 11 GULFSTREAM 500S IO-540-E1B5 6.80 6.80 76.0 77.0 - 10 GULFSTREAM 560E GO-480-C1B6 6.50 6.50 59.0 73.0 - 11 GULFSTREAM 680FL IGSO-540-B1A 8.50 8.00 64.0 74.0 - 11 GULFSTREAM 690B TPE-331-5-251K 10.30 9.70 66.0 76.0 - 10 GULFSTREAM 690C COMMANDER 840 TPE-331-5 10.30 9.70 61.3 77.4 - 5,11 GULFSTREAM 690D COMMANDER 900 TPE-331-5 10.70 10.60 61.7 77.4 - 10 GULFSTREAM 695 TPE-331-10 10.30 9.70 62.0 77.4 - 5,15 GULFSTREAM 695 COMMANDER 980 TPE-331-10 10.30 9.70 62.0 77.4 - 5,11 GULFSTREAM 695A COMMANDER 1000 TPE-331-10 11.20 10.60 61.6 77.9 - 5,11 GULFSTREAM AA-1B O-235 1.60 1.60 57.1 59.0 - 11 GULFSTREAM AA-5A O-320-E2G 2.20 2.20 60.0 61.0 - 11 GULFSTREAM AA-5B TIGER O-360-A4K 2.20 2.20 57.4 52.0 - 10,11 GULFSTREAM G100 TFE731-40R-200G 24.65 20.70 67.0 81.2 40 8,15 GULFSTREAM G200 PW306A 34.85 28.00 74.0 81.4 40 8,15,45 GULFSTREAM G200 PW306A 34.85 28.00 74.0 83.1 40 8,15,44 GULFSTREAM GA-7 O-320-D1D 3.80 3.80 63.0 72.0 - 4 GULFSTREAM GII (QTA STC ST03621AT) SPEY MK 511-8 62.00 58.50 70.2 89.4 39 8,15,16 GULFSTREAM GII (QTA STC ST03621AT) SPEY MK 511-8 64.80 58.50 71.6 89.4 39 8,15,16 GULFSTREAM GII TT (QTA STC ST03621AT) SPEY MK 511-8 65.50 58.50 71.9 89.4 39 8,15,16 GULFSTREAM GIIB/GIII (HAT STC ST01567LA) SPEY MK 511-8 68.20 58.50 72.5 86.3 39 8,15,16 GULFSTREAM GIIB/GIII (HAT STC ST01567LA) SPEY MK 511-8 69.70 58.50 73.2 86.3 39 8,15,16 PAGE 42
APPENDIX 2, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
TOGW MLW TO APP APP MANUFACTURER AIRPLANE ENGINE 1000 LBS 1000 LBS dBA dBA FLAPS NOTES GULFSTREAM GIIB/GIII (QTA STC ST03621AT) SPEY MK 511-8 68.20 58.50 72.4 89.5 39 8,15,16 GULFSTREAM GIIB/GIII (QTA STC ST03621AT) SPEY MK 511-8 69.70 58.50 73.0 89.5 39 8,15,16 GULFSTREAM GIISP (HAT STC ST01567LA) SPEY MK 511-8 62.00 58.50 70.6 86.1 39 8,15,16 GULFSTREAM GIISP (HAT STC ST01567LA) SPEY MK 511-8 64.80 58.50 71.8 86.1 39 8,15,16 GULFSTREAM GULFSTREAM I RR DART MK529 35.10 33.60 71.0 85.9 - 15 GULFSTREAM GULFSTREAM II SPEY MK511-8 62.00 58.50 80.1 83.9 20* 8,15,16 GULFSTREAM GULFSTREAM II SPEY MK511-8 62.00 58.50 82.6 83.9 20* 8,15 GULFSTREAM GULFSTREAM II SPEY MK511-8 62.00 58.50 82.6 90.6 39 8,15 GULFSTREAM GULFSTREAM II SPEY MK511-8 65.50 58.50 84.2 90.7 39 8,15,16 GULFSTREAM GULFSTREAM IIB/GIII SPEY MK511-8 69.70 58.50 82.8 82.5 20* 8,15,16 GULFSTREAM GULFSTREAM IIB/GIII SPEY MK511-8 69.70 58.50 82.8 89.7 39 8,15,16 GULFSTREAM GULFSTREAM IV RR TAY 611-8 73.20 58.50 64.2 80.7 39 8,15 GULFSTREAM GULFSTREAM IV - SP RR TAY 611-8 74.60 66.00 64.9 81.3 39 8,15 GULFSTREAM G-V BR700-710A1-10 90.50 75.30 68.0 82.0 39 8,15 IAI 1121 COMMODORE CJ610-5 18.50 18.50 89.7 100.0 - 4 IAI 1123 WESTWIND CJ610-9 20.70 19.00 89.7 99.0 - 4 IAI 1124 WESTWIND TFE731-3-1G 22.90 19.00 67.4 84.0 40 8,15 IAI 1124A WESTWIND II TFE731-3-1G 23.50 19.00 70.3 84.2 40 15 IAI 1124IW WESTWIND IW TFE731-3-1G 23.50 19.00 71.7 84.0 40 15 IAI 1125 ASTRA TFE731-3A-200G 23.50 20.70 70.3 80.4 40 8,15 IAI 1125 ASTRA TFE731-3A-200G 24.65 20.70 72.1 80.4 40 8,15 LEARJET LEARJET 23 CJ610-1 12.50 11.90 84.7 89.7 - 4,8 LEARJET LEARJET 24B/D W/RAISBECK CJ610-6 13.50 11.90 77.8 92.0 40 8,13 LEARJET LEARJET 24D CJ610-6 13.50 11.90 80.6 89.4 40 8 LEARJET LEARJET 24D CJ610-6 13.50 11.90 80.6 94.7 40 4,8,17 LEARJET LEARJET 24E CJ610-6 12.90 11.90 73.1 88.3 40 4,8 LEARJET LEARJET 24F CJ610-6 12.90 11.90 74.6 88.3 40 4,8 PAGE 43
AC36-3H 4/5/2012 APPENDIX 2, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
TOGW MLW TO APP APP MANUFACTURER AIRPLANE ENGINE 1000 LBS 1000 LBS dBA dBA FLAPS NOTES LEARJET LEARJET 25 B/C/D/F XR CJ610-6/8A 16.30 13.30 82.3 92.0 40 8,13 LEARJET LEARJET 25B/C CJ610-6 15.00 13.30 82.8 93.8 40 4,8,18 LEARJET LEARJET 25D CJ610-6 15.00 13.30 79.7 88.2 40 8,13 LEARJET LEARJET 25F CJ610-6 15.00 13.30 79.7 88.2 40 4,8 LEARJET LEARJET 31 TFE731-2-3B 17.00 15.30 68.9 82.9 40 13,15 LEARJET LEARJET 35 TFE731-2 17.00 14.30 70.4 83.1 40 4 LEARJET LEARJET 35 W/CENTURY III TFE731-2 17.00 14.30 65.6 81.6 40 8,15 LEARJET LEARJET 35A TFE731-2 18.00 15.30 71.6 81.7 40 15 LEARJET LEARJET 35A/36A TFE731-2 18.30 15.30 65.1 81.7 40 8,15 LEARJET LEARJET 36 TFE731-2 17.00 14.30 70.6 83.1 40 4 LEARJET LEARJET 36 W/CENTURY III TFE731-2 17.00 14.30 65.6 81.6 40 8,15 LEARJET LEARJET 36A TFE731-2 18.00 15.30 71.6 81.7 40 15 LEARJET LEARJET 45 TFE731-20R-1B 20.50 19.20 60.7 81.5 40 8,15 LEARJET LEARJET 55 TFE731-3B 20.50 17.00 67.0 81.5 40 15 LEARJET LEARJET 55B TFE731-3A-2B 21.50 18.00 68.4 81.9 40 LEARJET LEARJET 60 PW305A 23.10 19.50 60.9 77.4 40 8,15 LEARJET LEARJET 60 PW305A 23.50 19.50 60.9 77.4 40 8,15 LOCKHEED 1329 JETSTAR JT12A-8 42.00 35.00 88.7 101.0 50 8,13 LOCKHEED 1329-23 JETSTAR w/STAR 3 TFE731-3 44.25 36.00 74.7 88.3 59 8,15,33 LOCKHEED 1329-25 JETSTAR TFE731-3-IE 43.80 36.00 82.3 88.3 50 4 LOCKHEED 1329-25 JETSTAR w/STAR 3 TFE731-3 44.50 36.00 75.0 88.3 59 8,15,34 LOCKHEED L-1011 RB211-22B 430.00 358.00 85.1 91.3 33* 4,5 LOCKHEED L-1011 RB211-22B 430.00 358.00 85.1 92.1 42 4,5 LOCKHEED L-1011-1 RB211-22C 396.00 358.00 85.2 90.0 33* 4,8 LOCKHEED L-1011-1 RB211-22C 416.00 358.00 85.3 90.8 33* 8 LOCKHEED L-1011-1 RB211-22C 422.00 358.00 86.9 91.4 33* LOCKHEED L-1011-1 RB211-22C 430.00 358.00 87.1 92.7 42 PAGE 44
APPENDIX 2, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
TOGW MLW TO APP APP MANUFACTURER AIRPLANE ENGINE 1000 LBS 1000 LBS dBA dBA FLAPS NOTES LOCKHEED L-188 501-D13 116.00 95.70 81.3 89.5 - 4,8 MAULE MX7-235 0540-JIA5D 2.50 2.50 63.2 62.7 - 11 MCDONNELL DOUG. DC-08-50 (QNC QN) JT3D-3B 309.80 240.00 90.3 94.5 - 8,12 MCDONNELL DOUG. DC-08-61 (BAC/BAC II) JT3D-3B 325.00 240.00 88.8 91.2 35 8,15,16 MCDONNELL DOUG. DC-08-61 (QNC QN) JT3D-3B 309.80 240.00 90.3 94.5 - 8,12 MCDONNELL DOUG. DC-08-62 (BAC/BACII) JT3D-3B 335.00 240.00 90.0 89.8 35 8,15,16 MCDONNELL DOUG. DC-08-62 (BAC/BACII) JT3D-3B 335.00 250.00 90.0 90.0 35 8,15,16 MCDONNELL DOUG. DC-08-62 (BAC/BACII) JT3D-3B 348.00 240.00 91.1 89.8 35 8,15,16 MCDONNELL DOUG. DC-08-62 (BAC/BACII) JT3D-7 335.00 250.00 87.8 93.1 35 8,15,16 MCDONNELL DOUG. DC-08-62 (BAC/BACII) JT3D-7 350.00 240.00 88.8 93.0 35 8,15,16 MCDONNELL DOUG. DC-08-62 (BAC/R1) JT3D-3B 335.00 250.00 88.8 89.3 35 8,15,16 MCDONNELL DOUG. DC-08-62 (BAC/R1) JT3D-3B 350.00 240.00 90.0 88.9 35 8,15,16 MCDONNELL DOUG. DC-08-62 (BAC/R1) JT3D-7 335.00 250.00 87.8 93.1 35 8,15,16 MCDONNELL DOUG. DC-08-63 (ADC QN) JT3D-3B 355.00 245.00 91.7 96.0 50 8,15 MCDONNELL DOUG. DC-08-63 (BAC/BACII) JT3D-7 353.00 258.00 89.2 93.2 35 8,15,16 MCDONNELL DOUG. DC-08-63 (BAC/BACII) JT3D-7 353.00 275.00 89.2 93.5 35 8,15,16 MCDONNELL DOUG. DC-08-63 (BAC/R1) JT3D-7 355.00 275.00 89.2 93.5 35 8,15,16 MCDONNELL DOUG. DC-08-63 (TNC QN) JT3D-3B 350.00 250.00 90.5 95.4 50 8,15 MCDONNELL DOUG. DC-08-63 (TNC QN) JT3D-7 355.00 275.00 89.6 95.2 35 8,15 MCDONNELL DOUG. DC-08-63F (ADC QN) JT3D-7 355.00 245.00 91.0 95.9 50 8,15 MCDONNELL DOUG. DC-08-71 CFM56-2-C1 337.00 245.00 84.1 88.8 46 MCDONNELL DOUG. DC-08-72 CFM56-2-C1 362.50 245.00 85.6 88.6 46 MCDONNELL DOUG. DC-08-73 CFM56-2-C1 362.50 245.00 85.6 88.6 46 MCDONNELL DOUG. DC-09-10 JT8D-7 90.70 81.70 78.6 89.1 50 1,8,15 MCDONNELL DOUG. DC-09-10 JT8D-7 90.70 81.70 79.7 95.7 50 8,15 MCDONNELL DOUG. DC-09-10 (ABS STC1563GL) JT8D-7 90.70 81.70 76.3 86.7 40 8,15,16 MCDONNELL DOUG. DC-09-20 (ABS STC1613GL) JT8D-9 100.00 93.40 78.3 86.8 40 8,15,16 PAGE 45
AC36-3H 4/5/2012 APPENDIX 2, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
TOGW MLW TO APP APP MANUFACTURER AIRPLANE ENGINE 1000 LBS 1000 LBS dBA dBA FLAPS NOTES MCDONNELL DOUG. DC-09-30 JT8D-15 114.00 101.00 85.8 90.9 50 1,8,15 MCDONNELL DOUG. DC-09-30 JT8D-17 121.00 101.00 88.2 92.2 50 1,8,15 MCDONNELL DOUG. DC-09-30 JT8D-7 108.00 99.00 85.5 89.9 50 1,8,15 MCDONNELL DOUG. DC-09-30 JT8D-7 108.00 99.00 87.1 96.0 50 8,15 MCDONNELL DOUG. DC-09-30 JT8D-9 108.00 99.00 85.4 90.6 50 1,8,15 MCDONNELL DOUG. DC-09-30 JT8D-9 108.00 99.00 86.5 93.8 50 8,15 MCDONNELL DOUG. DC-09-30 JT8D-9 110.00 99.00 86.3 90.8 50 1,8,15 MCDONNELL DOUG. DC-09-30 (ABS STC1613GL) JT8D-7 103.00 99.00 80.2 87.0 40 8,15,16 MCDONNELL DOUG. DC-09-30 (ABS STC1613GL) JT8D-7 105.00 101.00 81.0 87.1 40 8,15,16 MCDONNELL DOUG. DC-09-30 (ABS STC1613GL) JT8D-9 103.00 99.00 79.3 87.0 40 8,15,16 MCDONNELL DOUG. DC-09-30 (ABS STC1613GL) JT8D-9 105.00 101.00 80.0 87.1 40 8,15,16 MCDONNELL DOUG. DC-09-30 (ABS STC165CH) JT8D-11 111.00 101.00 79.9 87.2 40 8,15,16 MCDONNELL DOUG. DC-09-30 (ABS STC165CH) JT8D-7 105.00 101.00 79.8 87.1 40 8,15,16 MCDONNELL DOUG. DC-09-30 (ABS STC165CH) JT8D-7 108.50 101.00 81.1 87.1 40 8,15,16 MCDONNELL DOUG. DC-09-30 (ABS STC165CH) JT8D-9 105.00 99.00 78.8 87.0 40 8,15,16 MCDONNELL DOUG. DC-09-30 (ABS STC165CH) JT8D-9 111.70 102.00 81.3 87.2 40 8,15,16 MCDONNELL DOUG. DC-09-40 JT8D-11 107.00 102.00 84.8 90.0 50 1,8,15 MCDONNELL DOUG. DC-09-40 JT8D-11 114.00 102.00 87.5 90.9 50 1,8,15 MCDONNELL DOUG. DC-09-40 JT8D-15 114.00 102.00 85.8 90.9 50 1,8,15 MCDONNELL DOUG. DC-09-40 (ABS STC165CH) JT8D-11 111.00 99.00 80.1 87.3 40 8,15,16 MCDONNELL DOUG. DC-09-40 (ABS STC165CH) JT8D-9 111.70 101.00 81.3 87.4 40 8,15,16 MCDONNELL DOUG. DC-09-50 JT8D-15 110.00 110.00 84.3 89.5 - 1,8,15 MCDONNELL DOUG. DC-09-50 JT8D-15 121.00 110.00 88.4 89.5 40* 1,8,15 MCDONNELL DOUG. DC-09-50 JT8D-15 121.00 110.00 88.4 92.0 50 1,8,15 MCDONNELL DOUG. DC-09-50 JT8D-17 115.00 104.00 85.9 89.5 - 1,8,15 MCDONNELL DOUG. DC-09-50 JT8D-17 121.00 110.00 88.2 89.5 40* 1,8,15 MCDONNELL DOUG. DC-09-50 JT8D-17 121.00 110.00 88.2 92.3 50 1,8,15 PAGE 46
APPENDIX 2, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
TOGW MLW TO APP APP MANUFACTURER AIRPLANE ENGINE 1000 LBS 1000 LBS dBA dBA FLAPS NOTES MCDONNELL DOUG. DC-10-10 CF6-6D 410.00 363.50 85.2 90.3 35* 15 MCDONNELL DOUG. DC-10-10 CF6-6D 410.00 363.50 85.2 95.1 50 15 MCDONNELL DOUG. DC-10-10 CF6-6D 440.00 363.50 88.5 91.1 35* 15 MCDONNELL DOUG. DC-10-10 CF6-6D 440.00 363.50 88.5 95.7 50 15 MCDONNELL DOUG. DC-10-10 CF6-6D1 386.50 363.50 80.9 89.8 35* 15 MCDONNELL DOUG. DC-10-10 CF6-6D1 386.50 363.50 80.9 94.7 50 15 MCDONNELL DOUG. DC-10-10 CF6-6D1 440.00 363.50 85.3 95.7 50 15 MCDONNELL DOUG. DC-10-30 CF6-50A 519.60 403.00 91.4 93.0 35* 15 MCDONNELL DOUG. DC-10-30 CF6-50A 519.60 403.00 91.4 96.0 50 15 MCDONNELL DOUG. DC-10-30 CF6-50A 565.00 403.00 95.7 93.4 35* 15 MCDONNELL DOUG. DC-10-30 CF6-50C 565.00 411.00 94.1 96.2 50 15 MCDONNELL DOUG. DC-10-30 CF6-50C1 562.00 403.00 93.9 97.1 50 15 MCDONNELL DOUG. DC-10-30 CF6-50C1 572.00 421.00 94.6 93.5 35* 15 MCDONNELL DOUG. DC-10-30 CF6-50C1 590.00 411.00 96.4 97.3 50 15 MCDONNELL DOUG. DC-10-30 CF6-50C2 555.00 403.00 84.4 94.2 50 8,15 MCDONNELL DOUG. DC-10-30 CF6-50C2 590.00 411.00 87.2 95.1 50 8,15 MCDONNELL DOUG. DC-10-30 CF6-50C2B 555.00 424.00 83.6 94.2 50 8,15 MCDONNELL DOUG. DC-10-30 CF6-50C2B 590.00 411.00 86.7 95.1 50 8,15 MCDONNELL DOUG. DC-10-30 CF6-50CA 565.00 424.00 95.7 96.3 50 15 MCDONNELL DOUG. DC-10-30 CF6-6K 410.00 403.00 82.6 88.7 35* 8,15 MCDONNELL DOUG. DC-10-30 CF6-6K 455.00 403.00 88.8 94.2 50 15 MCDONNELL DOUG. DC-10-40 JT9D-20 430.00 403.00 85.0 94.5 50 15 MCDONNELL DOUG. DC-10-40 JT9D-20 484.00 403.00 88.4 89.4 35* 15 MCDONNELL DOUG. DC-10-40 JT9D-20 484.00 403.00 88.4 94.5 50 15 MCDONNELL DOUG. DC-10-40 JT9D-20 530.00 403.00 91.7 90.2 35* 15 MCDONNELL DOUG. DC-10-40 JT9D-20 530.00 403.00 91.7 94.9 50 15 MCDONNELL DOUG. DC-10-40 JT9D-59A 555.00 403.00 90.6 94.9 35* 15 PAGE 47
AC36-3H 4/5/2012 APPENDIX 2, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
TOGW MLW TO APP APP MANUFACTURER AIRPLANE ENGINE 1000 LBS 1000 LBS dBA dBA FLAPS NOTES MCDONNELL DOUG. DC-10-40 JT9D-59A 555.00 403.00 90.6 97.1 50 15 MCDONNELL DOUG. DC-10-40 JT9D-59A 572.00 403.00 91.8 94.9 35* 15 MCDONNELL DOUG. DC-10-40 JT9D-59A 572.00 403.00 91.8 97.1 50 15 MCDONNELL DOUG. MD-80 JT8D-209 140.00 128.00 80.3 83.5 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-209 140.00 128.00 80.3 83.8 40 8,15 MCDONNELL DOUG. MD-80 JT8D-209 149.50 130.00 83.2 83.5 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-209 149.50 130.00 83.2 83.9 40 8,15 MCDONNELL DOUG. MD-80 JT8D-217 140.00 128.00 78.7 83.5 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-217 140.00 128.00 78.7 83.8 40 8,15 MCDONNELL DOUG. MD-80 JT8D-217 149.50 130.00 81.4 83.5 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-217 149.50 130.00 81.4 83.9 40 8,15 MCDONNELL DOUG. MD-80 JT8D-217A 140.00 128.00 78.7 83.5 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-217A 140.00 128.00 78.7 83.8 40 8,15 MCDONNELL DOUG. MD-80 JT8D-217A 160.00 150.00 83.7 83.9 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-217A 160.00 150.00 83.7 85.0 40 8,15 MCDONNELL DOUG. MD-80 JT8D-217C 140.00 128.00 78.3 83.5 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-217C 140.00 128.00 78.3 83.8 40 8,15 MCDONNELL DOUG. MD-80 JT8D-217C 160.00 150.00 83.1 83.9 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-217C 160.00 150.00 83.1 85.0 40 8,15 MCDONNELL DOUG. MD-80 JT8D-219 140.00 128.00 77.5 83.5 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-219 140.00 128.00 77.5 83.8 40 8,15 MCDONNELL DOUG. MD-80 JT8D-219 160.00 150.00 82.1 83.9 28* 8,15 MCDONNELL DOUG. MD-80 JT8D-219 160.00 150.00 82.1 85.0 40 8,15 MCDONNELL DOUG. MD-87 JT8D-217A 125.00 120.00 74.7 83.3 28* 8,15 MCDONNELL DOUG. MD-87 JT8D-217A 125.00 120.00 74.7 83.7 40 8,15 MCDONNELL DOUG. MD-87 JT8D-217A 149.50 130.00 81.2 83.6 28* 8,15 MCDONNELL DOUG. MD-87 JT8D-217A 149.50 130.00 81.2 84.3 40 8,15 PAGE 48
APPENDIX 2, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
TOGW MLW TO APP APP MANUFACTURER AIRPLANE ENGINE 1000 LBS 1000 LBS dBA dBA FLAPS NOTES MCDONNELL DOUG. MD-87 JT8D-217C 125.00 120.00 74.5 83.3 28* 8,15 MCDONNELL DOUG. MD-87 JT8D-217C 125.00 120.00 74.5 83.7 40 8,15 MCDONNELL DOUG. MD-87 JT8D-217C 149.50 130.00 80.6 83.6 28* 8,15 MCDONNELL DOUG. MD-87 JT8D-217C 149.50 130.00 80.6 84.3 40 8,15 MCDONNELL DOUG. MD-87 JT8D-219 140.00 128.00 77.4 83.5 28* 8,15 MCDONNELL DOUG. MD-87 JT8D-219 140.00 128.00 77.4 84.2 40 8,15 MCDONNELL DOUG. MD-87 JT8D-219 149.50 130.00 79.7 83.6 28* 8,15 MCDONNELL DOUG. MD-87 JT8D-219 149.50 130.00 79.7 84.3 40 8,15 MCDONNELL DOUG. MD-90-30 V2525-D5 156.00 142.00 71.1 83.3 40 8,15 MCDONNELL DOUG. MD-90-30 V2525-D5 166.00 142.00 73.0 83.3 40 8,15 MCDONNELL DOUG. MD-90-30 V2528-D5 156.00 142.00 69.0 83.3 40 8,15 MCDONNELL DOUG. MD-90-30 V2528-D5 166.00 142.00 71.0 83.3 40 8,15 MESSERSCHMITT HFB-320 HANSA CJ610-9 20.30 19.40 89.7 99.0 - 13 MITSUBISHI MU-2B-26A TPE-331-5-252M 10.00 10.00 64.0 76.0 - 4 MITSUBISHI MU-2B-36A TPE-331-5-252M 11.00 10.20 66.0 76.0 - 4 MITSUBISHI MU300 DIAMOND I JT15D-4 14.10 13.20 71.9 77.2 30 12 MITSUBISHI MU300-10 DIAMOND II JT15D-5 15.80 14.20 71.8 83.0 - 15 MOONEY M20C 0-360-A1D 2.60 2.60 65.0 62.0 - 11 MOONEY M20F w/MODWORK STC# IO-360-E5 2.74 2.74 74.4 62.0 - 11,21 SA02204AT MOONEY M20J I0-360-A1B6D 2.70 2.70 58.0 62.0 - 4 MOONEY M20M TIO-540-AF1A 3.20 3.20 63.9 63.3 - 11,21 MOONEY M20M TIO-540-AF1A 3.37 3.37 64.8 63.3 - 11,21 MORANE-SAULNIER MS 760B (PARIS II) MARBORE VI C2 8.65 6.96 80.9 91.5 55 19 NIHON YS-11A-200 DART MK 542 54.00 52.90 81.0 90.0 - 5 OSTMECKLENBURGISCH OMF-100-160 O-320-D2A 1.96 1.96 61.0 61.0 - 11,21
E FLUGZEUGBAU PIPER 601P IO-540-S1A5 6.00 6.00 70.0 73.0 - 11 PIPER CHEYENNE 400LS TPE-331-14 12.05 11.10 57.0 78.5 - 11 PAGE 49
AC36-3H 4/5/2012 APPENDIX 2, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
TOGW MLW TO APP APP MANUFACTURER AIRPLANE ENGINE 1000 LBS 1000 LBS dBA dBA FLAPS NOTES PIPER PA-18-150 0-320-A2B 1.80 1.80 53.0 61.0 - 11 PIPER PA-23-250 IO-540-C4B5 5.20 4.94 68.0 73.0 - 11 PIPER PA-24-260 IO-540-B1A5 3.20 3.20 65.0 63.0 - 11 PIPER PA-28-140 O-320-E3D 2.20 2.20 60.0 61.0 - 11 PIPER PA-28-151 O-320-E3D 2.20 2.20 60.0 61.0 - 11 PIPER PA-28-161 O-320-D3G 2.40 2.40 59.0 61.0 - 11 PIPER PA-28-181 O-360-A4M 2.55 2.50 60.0 62.0 - 11 PIPER PA-28-200 I0-360-C1C 2.70 2.70 63.0 61.0 - PIPER PA-28-235 O-540-B4B5 3.00 3.00 72.0 63.0 - 11 PIPER PA-28-236 O-540-J3A5D 3.00 3.00 68.0 63.0 - 11 PIPER PA-28RT-201(2BLD) I0-360-C1C6 2.80 2.80 67.0 62.0 - 11 PIPER PA-28RT-201T(3BLD) TSIO-360-FB 2.90 2.90 67.0 62.0 - 11 PIPER PA-30 TWIN COMANCHE IO-320-B 3.60 3.60 56.0 70.6 - 11 PIPER PA-31-310 TI0-540-A2C 6.50 6.50 69.0 73.0 - 11 PIPER PA-31-325 TIO-540-F2BD 6.50 6.50 70.0 74.0 - 11 PIPER PA-31-350 TI0-540-J2BD 7.00 7.00 71.0 74.0 - 11 PIPER PA-31T PT6A-28 9.00 9.00 62.0 74.0 - 4 PIPER PA-32-300 IO-540-K1G5D 3.40 3.40 71.0 64.0 - PIPER PA-32R-300 IO-540-K1G5D 3.60 3.60 71.0 64.0 - 11 PIPER PA-32R-301 IO-540-K1G5D 3.60 3.60 70.0 64.0 - 11 PIPER PA-32R-301T TIO-540-S1AD 3.60 3.60 69.0 64.0 - 11 PIPER PA-32RT-300 IO-540-K1A5D 3.60 3.60 71.0 64.0 - 11 PIPER PA-34-200T TSI0-360-E 4.80 4.50 64.0 72.0 - 11 PIPER PA-34-220T TSIO-360-KB 4.75 4.50 64.0 72.0 - 11 PIPER PA-38-112 O-235-L2C 1.70 1.70 56.0 60.0 - 11 PIPER PA-42 CHEYENNE PT6A-41 10.50 9.40 70.3 77.1 - 10,11 PIPER PA-44-180 O-360-E1A6D 3.80 3.80 62.0 71.0 - 11 PAGE 50
APPENDIX 2, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
TOGW MLW TO APP APP MANUFACTURER AIRPLANE ENGINE 1000 LBS 1000 LBS dBA dBA FLAPS NOTES PIPER PA-44-180T(2BLD) TO-360-E1A6D 3.90 3.90 62.0 71.0 - 11 PIPER PA-44-180T(3BLD) TO-360-E1A6D 3.90 3.90 60.0 71.0 - 11 PIPER PA-46-31P MALIBU TSIO-520-BE 4.10 4.10 70.0 63.9 - 11 PIPER PA-602P IO-540-AA1A5 6.00 6.00 66.0 73.0 - 11 PIPER PA-60-600 IO-540-K1J5 5.50 5.50 66.0 73.0 - 11 RAYTHEON HAWKER 125- 1A TFE731-3-1H 21.20 19.55 70.4 83.3 25* 8,15 RAYTHEON HAWKER 125- 1A TFE731-3-1H 21.20 19.55 70.4 85.8 45 8,15 RAYTHEON HAWKER 125- 1A TFE731-3-1H 21.70 19.55 71.2 83.3 25* 8,15 RAYTHEON HAWKER 125- 1A TFE731-3-1H 21.70 19.55 71.2 85.8 45 8,15 RAYTHEON HAWKER 125- 1A VIPER-522 21.20 19.60 83.1 98.5 50 8,15 RAYTHEON HAWKER 125- 3A TFE731-3-1H 21.70 20.00 71.2 83.5 25* 8,15 RAYTHEON HAWKER 125- 3A TFE731-3-1H 21.70 20.00 71.2 86.0 45 8,15 RAYTHEON HAWKER 125- 3A/R VIPER-522 22.70 20.00 84.8 98.7 50 8,15 RAYTHEON HAWKER 125- 3A/RA TFE731-3-1H 23.60 20.00 72.4 83.0 25* 8,15 RAYTHEON HAWKER 125- 3A/RA TFE731-3-1H 23.60 20.00 72.4 85.5 45 8,15 RAYTHEON HAWKER 125- 3A/RA VIPER-522 22.70 20.00 84.8 98.7 45 8,15 RAYTHEON HAWKER 125- 400A TFE731-3-1H 23.60 20.00 72.4 83.0 25* 8,15 RAYTHEON HAWKER 125- 400A TFE731-3-1H 23.60 20.00 72.4 85.5 45 8,15 RAYTHEON HAWKER 125- 400A VIPER-522 23.60 20.00 85.3 98.7 45 8,15 RAYTHEON HAWKER 125- 600A TFE731-3-1H 25.50 22.00 75.8 83.6 25* 8,15 RAYTHEON HAWKER 125- 600A TFE731-3-1H 25.50 22.00 75.8 86.1 45 8,15 RAYTHEON HAWKER 125- 600A VIPER 601-22 25.50 22.00 81.9 96.0 45 8,15,16 RAYTHEON HAWKER 125- 700A TFE731-3-1H 24.20 22.00 75.4 83.6 25* 8,15,26 RAYTHEON HAWKER 125- 700A TFE731-3-1H 24.20 22.00 75.4 86.1 45 8,15,26 RAYTHEON HAWKER 125- 700A TFE731-3-1H 25.50 22.00 75.8 83.6 25* 8,15,26 RAYTHEON HAWKER 125- 700A TFE731-3-1H 25.50 22.00 75.8 86.1 45 8,15,26 RAYTHEON HAWKER 125- 700A TFE731-3R-1H 25.50 22.00 76.1 83.5 25* 8,15,20,26 PAGE 51
AC36-3H 4/5/2012 APPENDIX 2, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
TOGW MLW TO APP APP MANUFACTURER AIRPLANE ENGINE 1000 LBS 1000 LBS dBA dBA FLAPS NOTES RAYTHEON HAWKER 125- 700A TFE731-3R-1H 25.50 22.00 76.1 86.0 45 8,15,20,26 RAYTHEON HAWKER 125- 800A TFE731-5R-1H 27.40 23.35 69.7 82.5 25* 8,15 RAYTHEON HAWKER 125- 800A TFE731-5R-1H 27.40 23.35 69.7 82.5 25* 8,15,20 RAYTHEON HAWKER 125- 800A TFE731-5R-1H 27.40 23.35 69.7 85.0 45 8,15 RAYTHEON HAWKER 125- 800A TFE731-5R-1H 27.40 23.35 69.7 85.0 45 8,15,20 RAYTHEON HAWKER 125- 800XP TFE731-5BR-1H 28.00 23.35 68.2 82.6 45 8,15 RAYTHEON HAWKER 125-1000A PW305 31.00 25.00 71.8 82.2 25* 8,15 RAYTHEON HAWKER 125-1000A PW305 31.00 25.00 71.8 82.9 45 8,15 SAAB 2000 AE2100A 49.60 47.40 63.5 78.9 20 8,15 SAAB SF340A (Dowty props) GE CT7-5A2 27.27 26.50 62.7 75.8 20 8,15 SAAB SF340A (Dowty props) GE CT7-5A2 28.00 27.20 62.9 82.0 20 8,15 SAAB SF340B (Dowty props) GE CT7-9B 28.50 28.00 63.4 82.0 20 8,15 SAAB SF340B (Dowty props) GE CT7-9B 29.00 28.50 64.1 82.0 20 8,15 SAAB SF340B (HS14RF-19 props) GE CT7-9B 28.50 28.00 63.5 78.8 20 8,15 SAAB SF340B (HS14RF-19 props) GE CT7-9B 29.00 28.50 64.2 78.8 20 8,15 SAAB FAIRCHILD SF340 GE CT7-5A2 27.30 26.50 65.3 80.0 35 12 SABRELINER CORP. SABRE 40A JT12A-8 19.60 17.50 83.4 92.0 - 8,12 SABRELINER CORP. SABRE 60 JT12A-8 20.10 17.50 84.7 92.0 24 8,12 SABRELINER CORP. SABRE 60A JT12A-8 22.70 20.60 83.8 95.4 - 8,12 SABRELINER CORP. SABRE 65 TFE731-3R-1D 24.00 21.80 70.8 81.7 - 8,12 SABRELINER CORP. SABRE 70 JT12A-8 21.00 18.50 87.9 93.8 - 8,12 SABRELINER CORP. SABRE 75A CF700-2D-2 23.00 22.00 77.7 90.3 25 4 SABRELINER CORP. SABRE 80 CF700-2D-2 23.30 22.00 79.6 90.3 25 12 SABRELINER CORP. SABRE 80A CF700-2D-2 25.50 22.00 80.5 91.0 - 12 SHORTS 3-30 PT6A-45A 22.40 22.10 71.2 81.8 - 8,15 SHORTS 3-60 PT6A-65R 26.40 26.10 67.9 80.1 30 8,15 SHORTS SD3-60-300 PT6A-67R 27.10 26.50 68.3 84.0 30 13 PAGE 52
4/5/2012 APPENDIX 2, CHANGE 1 AC 36-3H MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MANUFACTURER SHORTS
AIRPLANE SKYVAN ENGINE TPE-331-201 TOGW 1000 LBS
12.50 MLW 1000 LBS
12.50 TO dBA
71.6 APP dBA
77.3 FLAPS APP 46 NOTES VICKERS ARMSTRONGS VISCOUNT 745 RR DART6 MK510 72.50 64.00 78.1 84.6 - 11 PAGE 53