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
Reference Notes * Less than maximum flap setting.
1. Engines equipped with P-36 acoustical treatment.
2. Quiet nacelles and double wall fan duct treatment.
3. Double wall fan duct treatment.
4. Retain from AC 36-3A.
5. Estimated using non-certification measurement data.
6. Nacelle with fixed lip inlet.
7. Increased takeoff thrust rating.
8. Thrust cutback used.
9. ICAO Annex 16 certification data source.
10. DOT/FAA noise measurements.
11. Propeller noise estimation model.
12. Certification spectra analyzed to obtain dBA.
13. Estimated using certification data from aircraft with similar engines.
14. Estimated using the Integrated Noise Model (INM).
15. Based on manufacturer’s data.
16. Equipped with hushkit.
17. Equipped with Learavia engine suppressor nozzle and ECR 936.
18. Equipped with Learavia engine suppressor nozzle.
19. DGAC noise measurements.
20. Equipped with thrust reversers.
21. Estimated using 14 CFR part 36, Appendix G certification data.
22. Airbrake open on approach.
23. Equipped with Noise Reduction Inlet.
24. Fed Ex lightweight hushkit
25. Fed Ex heavyweight hushkit
26. Data for TFE-731-3R-1H also applies to TFE-731-3-1H
27. Equipped with modification M3530
28. Equipped with Boeing inlet.
29. Equipped with Burbank Aeronautical Corporation inlet.
30. AvAero lightweight hushkit
31. AvAero heavyweight hushkit
32. AvAero heavyweight hushkit with lightweight hushkit nozzle
33. Equipped with STAR3 STC ST00258SE
34. Equipped with STAR3 STC ST00259SE
35. Engines equipped with 48 fan outlet guide vanes Page 1