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 BOEING B-747-400F PW4056 PKG A (FB2T) 830.00 630.00 86.7 94.1 25* 8,15 BOEING B-747-400F PW4056 PKG A (FB2T) 875.00 666.00 89.4 94.0 25* 8,15 BOEING B-747-400F PW4056 PKG A (FB2T) 875.00 666.00 89.4 94.4 30 8,15 BOEING B-747-400F RB211-524G 830.00 630.00 88.0 92.6 25* 8,15 BOEING B-747-400F RB211-524G 830.00 630.00 88.0 92.8 30 8,15 BOEING B-747-400F RB211-524G 875.00 666.00 90.4 92.5 25* 8,15 BOEING B-747-400F RB211-524G 875.00 666.00 90.4 93.1 30 8,15 BOEING B-747-400F RB211-524H 830.00 630.00 86.7 92.6 25* 8,15 BOEING B-747-400F RB211-524H 830.00 630.00 86.7 92.8 30 8,15 BOEING B-747-400F RB211-524H 875.00 666.00 89.0 92.5 25* 8,15 BOEING B-747-400F RB211-524H 875.00 666.00 89.0 93.1 30 8,15 BOEING B-747-SP JT9D-7A 660.00 450.00 94.9 92.8 30 4,6 BOEING B-747-SP JT9D-7A 690.00 450.00 96.1 93.1 30 4,6 BOEING B-747-SP JT9D-7F 660.00 475.00 94.9 93.1 30 4,6 BOEING B-747-SP JT9D-7FWET 695.00 475.00 96.2 93.5 30 4,6 BOEING B-747-SR JT9D-7A 570.00 564.00 90.0 95.6 30 4,6 BOEING B-747-SR JT9D-7A 610.00 564.00 92.9 96.1 30 4,6 BOEING B-757-200 PW2037 220.00 198.00 69.6 86.2 25* 8,15 BOEING B-757-200 PW2037 220.00 198.00 69.6 87.2 30 8,15 BOEING B-757-200 PW2037 255.50 210.00 75.9 86.7 25* 8,15 BOEING B-757-200 PW2037 255.50 210.00 75.9 87.9 30 8,15 BOEING B-757-200 PW2037 (CBQFC) 220.00 198.00 68.0 85.0 25* 8,15,40 BOEING B-757-200 PW2037 (CBQFC) 220.00 198.00 68.0 86.0 30 8,15,40 BOEING B-757-200 PW2037 (CBQFC) 255.50 210.00 74.3 85.5 25* 8,15,40 BOEING B-757-200 PW2037 (CBQFC) 255.50 210.00 74.3 86.5 30 8,15,40 BOEING B-757-200 PW2037 (nCBQFC) 220.00 198.00 68.1 85.1 25* 8,15,41 BOEING B-757-200 PW2037 (nCBQFC) 220.00 198.00 68.1 86.0 30 8,15,41 PAGE 27
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 BOEING B-757-200 PW2037 (nCBQFC) 255.50 210.00 74.5 85.6 25* 8,15,41 BOEING B-757-200 PW2037 (nCBQFC) 255.50 210.00 74.5 86.5 30 8,15,41 BOEING B-757-200 PW-2037(BG-3) 220.00 198.00 69.6 86.2 25* 8,15,39 BOEING B-757-200 PW-2037(BG-3) 220.00 198.00 69.6 87.2 30 8,15,39 BOEING B-757-200 PW2037(BG-3) 255.50 210.00 75.9 86.7 25* 8,15,39 BOEING B-757-200 PW2037(BG-3) 255.50 210.00 75.9 87.9 30 8,15,39 BOEING B-757-200 PW2040 220.00 198.00 67.9 86.2 25* 8,15 BOEING B-757-200 PW2040 220.00 198.00 67.9 87.2 30 8,15 BOEING B-757-200 PW2040 255.50 210.00 73.7 86.7 25* 8,15 BOEING B-757-200 PW2040 255.50 210.00 73.7 87.9 30 8,15 BOEING B-757-200 PW2040 (CBQFC) 220.00 198.00 66.6 85.0 25* 8,15,40 BOEING B-757-200 PW2040 (CBQFC) 220.00 198.00 66.6 86.0 30 8,15,40 BOEING B-757-200 PW2040 (CBQFC) 255.50 210.00 72.2 85.5 25* 8,15,40 BOEING B-757-200 PW2040 (CBQFC) 255.50 210.00 72.2 86.5 30 8,15,40 BOEING B-757-200 PW2040 (nCBQFC) 220.00 198.00 66.7 85.1 25* 8,15,41 BOEING B-757-200 PW2040 (nCBQFC) 220.00 198.00 66.7 86.0 30 8,15,41 BOEING B-757-200 PW2040 (nCBQFC) 255.50 210.00 72.4 85.6 25* 8,15,41 BOEING B-757-200 PW2040 (nCBQFC) 255.50 210.00 72.4 86.5 30 8,15,41 BOEING B-757-200 RB211-535C 220.00 198.00 72.8 88.9 25* 8,15 BOEING B-757-200 RB211-535C 220.00 198.00 72.8 90.0 30 8,15 BOEING B-757-200 RB211-535C 240.00 210.00 75.9 89.2 25* 8,15 BOEING B-757-200 RB211-535C 240.00 210.00 75.9 89.2 30 8,15 BOEING B-757-200 RB211-535E4 220.00 198.00 67.8 84.5 25* 8,15,35 BOEING B-757-200 RB211-535E4 220.00 198.00 68.1 84.5 25* 8,15,36 BOEING B-757-200 RB211-535E4 220.00 198.00 67.8 84.9 30 8,15,35 BOEING B-757-200 RB211-535E4 220.00 198.00 68.1 84.9 30 8,15,36 BOEING B-757-200 RB211-535E4 255.50 210.00 73.7 84.9 25* 8,15,35 PAGE 28
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 BOEING B-757-200 RB211-535E4 255.50 210.00 73.7 84.9 25* 8,15,36 BOEING B-757-200 RB211-535E4 255.50 210.00 73.7 85.3 30 8,15,36 BOEING B-757-200 RB211-535E4 255.50 210.00 73.7 85.3 30 8,15,35 BOEING B-757-200 RB211-535E4B 220.00 198.00 67.1 84.5 25* 8,15,36 BOEING B-757-200 RB211-535E4B 220.00 198.00 66.7 84.5 25* 8,15,35 BOEING B-757-200 RB211-535E4B 220.00 198.00 66.7 84.9 30 8,15,35 BOEING B-757-200 RB211-535E4B 220.00 198.00 67.1 84.9 30 8,15,36 BOEING B-757-200 RB211-535E4B 255.50 210.00 72.3 84.9 25* 8,15,35 BOEING B-757-200 RB211-535E4B 255.50 210.00 72.4 84.9 25* 8,15,36 BOEING B-757-200 RB211-535E4B 255.50 210.00 72.4 85.3 30 8,15,36 BOEING B-757-200 RB211-535E4B 255.50 210.00 72.3 85.3 30 8,15,35 BOEING B-757-300 RB211-535E4 236.00 210.00 71.0 85.1 25 8,15,35 BOEING B-757-300 RB211-535E4 236.00 210.00 71.0 85.7 30 8,15,35 BOEING B-757-300 RB211-535E4 275.00 224.00 77.2 85.6 25 8,15,35 BOEING B-757-300 RB211-535E4 275.00 224.00 77.2 86.2 30 8,15,35 BOEING B-757-300 RB211-535E4B 235.87 210.00 69.0 85.1 25 8,15,35 BOEING B-757-300 RB211-535E4B 235.87 210.00 69.0 85.7 30 8,15,35 BOEING B-757-300 RB211-535E4B 275.00 224.00 75.1 85.6 25 8,15,35 BOEING B-757-300 RB211-535E4B 275.00 224.00 75.1 86.2 30 8,15,35 BOEING B-757-300 RB211-535E4C 235.87 210.00 69.0 85.1 25 8,15,35 BOEING B-757-300 RB211-535E4C 235.87 210.00 69.0 85.7 30 8,15,35 BOEING B-757-300 RB211-535E4C 275.00 224.00 75.1 85.6 25 8,15,35 BOEING B-757-300 RB211-535E4C 275.00 224.00 75.1 86.2 30 8,15,35 BOEING B-767-200 JT9D-7R4D 282.00 257.00 72.9 90.4 30 8,15 BOEING B-767-200 JT9D-7R4D 315.00 270.00 77.1 89.2 25* 8,15 BOEING B-767-200 JT9D-7R4E 360.00 300.00 82.3 89.5 25* 8,15 BOEING B-767-200 JT9D-7R4E 360.00 300.00 82.3 91.3 30 8,15 PAGE 29
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 BOEING B-767-200/200ER CF6-80A 279.90 257.00 71.3 89.1 30 8,15 BOEING B-767-200/200ER CF6-80C2B2 300.00 270.00 70.3 88.4 30 8,15 BOEING B-767-200/200ER CF6-80C2B2 351.00 300.00 75.8 88.4 30 8,15 BOEING B-767-200/200ER CF6-80C2B4 351.00 270.00 73.8 88.4 30 8,15 BOEING B-767-200/200ER CF6-80C2B4 387.00 300.00 77.7 88.4 30 8,15 BOEING B-767-200/200ER PW4052 335.00 270.00 74.3 90.0 30 8,15 BOEING B-767-200/200ER PW4052 351.00 285.00 76.2 90.0 30 8,15 BOEING B-767-200/200ER PW4056 340.00 270.00 73.3 89.1 30 8,15 BOEING B-767-200/200ER PW4056 PHASE 3 (FB2C) 395.00 300.00 77.3 88.4 30 8,15,23 BOEING B-767-300 CF6-80A 300.00 280.00 74.5 89.1 25* 8,15 BOEING B-767-300 CF6-80A 300.00 280.00 74.5 89.2 30 8,15 BOEING B-767-300 CF6-80A 351.00 320.00 80.6 89.2 25* 8,15 BOEING B-767-300 CF6-80A 351.00 320.00 80.6 89.4 30 8,15 BOEING B-767-300 CF6-80A2 300.00 280.00 73.7 89.1 25* 8,15 BOEING B-767-300 CF6-80A2 300.00 280.00 73.7 89.2 30 8,15 BOEING B-767-300 CF6-80A2 351.00 320.00 79.7 89.2 25* 8,15 BOEING B-767-300 CF6-80A2 351.00 320.00 79.7 89.4 30 8,15 BOEING B-767-300 JT9D-7R4D(B) 300.00 280.00 75.7 89.7 25* 8,15 BOEING B-767-300 JT9D-7R4D(B) 300.00 280.00 75.7 91.2 30 8,15 BOEING B-767-300 JT9D-7R4D(B) 351.00 320.00 81.6 90.8 25* 8,15 BOEING B-767-300 JT9D-7R4D(B) 351.00 320.00 81.6 92.3 30 8,15 BOEING B-767-300 JT9D-7R4E 300.00 280.00 74.8 89.7 25* 8,15 BOEING B-767-300 JT9D-7R4E 300.00 280.00 74.8 91.2 30 8,15 BOEING B-767-300 JT9D-7R4E 351.00 320.00 80.8 90.8 25* 8,15 BOEING B-767-300 JT9D-7R4E 351.00 320.00 80.8 92.3 30 8,15 BOEING B-767-300/300ER CF6-80C2B2F 300.00 280.00 70.8 88.4 25* 8,15 BOEING B-767-300/300ER CF6-80C2B2F 300.00 280.00 70.8 88.6 30 8,15 PAGE 30
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 BOEING B-767-300/300ER CF6-80C2B2F 351.00 340.00 75.9 88.7 25* 8,15 BOEING B-767-300/300ER CF6-80C2B2F 351.00 340.00 75.9 90.0 30 8,15 BOEING B-767-300/300ER CF6-80C2B4 380.00 280.00 77.1 88.4 25* 8,15 BOEING B-767-300/300ER CF6-80C2B4 380.00 280.00 77.1 88.5 30 8,15 BOEING B-767-300/300ER CF6-80C2B4 407.00 320.00 79.8 88.5 25* 8,15 BOEING B-767-300/300ER CF6-80C2B4 407.00 320.00 79.8 89.3 30 8,15 BOEING B-767-300/300ER CF6-80C2B4F W/N1 MOD 295.00 280.00 69.0 88.4 25* 8,15 BOEING B-767-300/300ER CF6-80C2B4F W/N1 MOD 295.00 280.00 69.0 88.6 30 8,15 BOEING B-767-300/300ER CF6-80C2B4F W/N1 MOD 412.00 320.00 80.3 88.5 25* 8,15 BOEING B-767-300/300ER CF6-80C2B4F W/N1 MOD 412.00 320.00 80.3 89.4 30 8,15 BOEING B-767-300/300ER CF6-80C2B6 288.70 280.00 67.6 88.4 25* 8,15 BOEING B-767-300/300ER CF6-80C2B6 288.70 280.00 67.6 88.5 30 8,15 BOEING B-767-300/300ER CF6-80C2B6 412.00 320.00 79.1 88.5 25* 8,15 BOEING B-767-300/300ER CF6-80C2B6 412.00 320.00 79.1 89.3 30 8,15 BOEING B-767-300/300ER CF6-80C2B6F 345.00 280.00 72.7 88.4 25* 8,15 BOEING B-767-300/300ER CF6-80C2B6F 345.00 280.00 72.7 88.6 30 8,15 BOEING B-767-300/300ER CF6-80C2B6F 408.00 320.00 78.5 88.5 25* 8,15 BOEING B-767-300/300ER CF6-80C2B6F 408.00 320.00 78.5 89.4 30 8,15 BOEING B-767-300/300ER CF6-80C2B6F W/N1 MOD 288.70 280.00 67.6 88.4 25* 8,15 BOEING B-767-300/300ER CF6-80C2B6F W/N1 MOD 288.70 280.00 67.6 88.6 30 8,15 BOEING B-767-300/300ER CF6-80C2B6F W/N1 MOD 408.00 320.00 78.7 88.5 25* 8,15 BOEING B-767-300/300ER CF6-80C2B6F W/N1 MOD 408.00 320.00 78.7 89.4 30 8,15 BOEING B-767-300/300ER CF6-80C2B7F 407.00 320.00 77.8 88.5 25* 8,15 BOEING B-767-300/300ER CF6-80C2B7F 407.00 320.00 77.8 89.4 30 8,15 BOEING B-767-300/300ER CF6-80C2B7F 412.00 340.00 78.2 88.7 25* 8,15 BOEING B-767-300/300ER CF6-80C2B7F 412.00 340.00 78.2 90.3 30 8,15 BOEING B-767-300/300ER PW4056 295.00 280.00 68.9 89.9 25* 8,15 PAGE 31
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 BOEING B-767-300/300ER PW4056 295.00 280.00 68.9 90.2 30 8,15 BOEING B-767-300/300ER PW4056 407.00 320.00 81.2 90.2 25* 8,15 BOEING B-767-300/300ER PW4056 407.00 320.00 81.2 90.5 30 8,15 BOEING B-767-300/300ER PW4060 315.00 280.00 70.3 89.9 25* 8,15 BOEING B-767-300/300ER PW4060 315.00 280.00 70.3 90.2 30 8,15 BOEING B-767-300/300ER PW4060 408.00 320.00 80.0 90.2 25* 8,15 BOEING B-767-300/300ER PW4060 408.00 320.00 80.0 90.5 30 8,15 BOEING B-767-300/300ER PW4060 PHASE 3 (FB2C) 412.00 320.00 78.0 88.7 30 8,15,23 BOEING B-767-300/300ER RB211-524G 340.00 280.00 76.4 88.7 30 8,15 BOEING B-767-300/300ER RB211-524G 340.00 280.00 76.4 88.7 25* 8,15 BOEING B-767-300/300ER RB211-524G 407.00 320.00 82.6 88.7 25* 8,15 BOEING B-767-300/300ER RB211-524G 407.00 320.00 82.6 89.2 30 8,15 BOEING B-767-300/300ER RB211-524H 340.00 280.00 75.5 88.7 25* 8,15 BOEING B-767-300/300ER RB211-524H 340.00 280.00 75.5 88.7 30 8,15 BOEING B-767-300/300ER RB211-524H 407.00 320.00 81.5 88.7 25* 8,15 BOEING B-767-300/300ER RB211-524H 407.00 320.00 81.5 89.2 30 8,15 BOEING B-777-200 GE90-76B 506.00 445.00 72.6 87.6 25* 8,15,57 BOEING B-777-200 GE90-76B 506.00 445.00 72.6 88.5 30 8,15,57 BOEING B-777-200 GE90-76B 545.00 460.00 75.1 87.7 25* 8,15,57 BOEING B-777-200 GE90-76B 545.00 460.00 75.1 88.7 30 8,15,57 BOEING B-777-200 GE90-76B(BLK IV) 506.00 445.00 72.6 87.6 25* 8,15,58 BOEING B-777-200 GE90-76B(BLK IV) 506.00 445.00 72.6 88.5 30 8,15,58 BOEING B-777-200 GE90-76B(BLK IV) 545.00 470.00 75.1 87.8 25* 8,15,58 BOEING B-777-200 GE90-76B(BLK IV) 545.00 470.00 75.1 88.8 30 8,15,58 BOEING B-777-200 GE90-77B 506.00 445.00 72.5 87.6 25* 8,15,57 BOEING B-777-200 GE90-77B 506.00 445.00 72.5 88.5 30 8,15,57 BOEING B-777-200 GE90-77B 545.00 460.00 74.9 87.7 25* 8,15,57 PAGE 32
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 BOEING B-777-200 GE90-77B 545.00 460.00 74.9 88.7 30 8,15,57 BOEING B-777-200 GE90-77B(BLK IV) 506.00 445.00 72.6 87.6 25* 8,15,58 BOEING B-777-200 GE90-77B(BLK IV) 506.00 445.00 72.6 88.5 30 8,15,58 BOEING B-777-200 GE90-77B(BLK IV) 545.00 470.00 75.2 87.8 25* 8,15,58 BOEING B-777-200 GE90-77B(BLK IV) 545.00 470.00 75.2 88.8 30 8,15,58 BOEING B-777-200 GE90-85B 545.00 445.00 72.9 87.6 25* 8,15,57 BOEING B-777-200 GE90-85B 545.00 445.00 72.9 88.5 30 8,15,57 BOEING B-777-200 GE90-85B 632.50 460.00 78.7 87.7 25* 8,15,57 BOEING B-777-200 GE90-85B 632.50 460.00 78.7 88.7 30 8,15,57 BOEING B-777-200 GE90-85B(BLK IV) 545.00 445.00 72.5 87.6 25* 8,15,58 BOEING B-777-200 GE90-85B(BLK IV) 545.00 445.00 72.5 88.5 30 8,15,58 BOEING B-777-200 GE90-85B(BLK IV) 632.50 470.00 78.0 87.8 25* 8,15,58 BOEING B-777-200 GE90-85B(BLK IV) 632.50 470.00 78.0 88.8 30 8,15,58 BOEING B-777-200 GE90-90B 545.00 445.00 71.8 87.6 25* 8,15,57 BOEING B-777-200 GE90-90B 545.00 445.00 71.8 88.5 30 8,15,57 BOEING B-777-200 GE90-90B 656.00 460.00 78.7 87.7 25* 8,15,57 BOEING B-777-200 GE90-90B 656.00 460.00 78.7 88.7 30 8,15,57 BOEING B-777-200 GE90-90B(BLK IV) 545.00 445.00 70.6 87.6 25* 8,15,58 BOEING B-777-200 GE90-90B(BLK IV) 545.00 445.00 70.6 88.5 30 8,15,58 BOEING B-777-200 GE90-90B(BLK IV) 656.00 470.00 78.1 87.8 25* 8,15,58 BOEING B-777-200 GE90-90B(BLK IV) 656.00 470.00 78.1 88.8 30 8,15,58 BOEING B-777-200 GE90-94B(BLK IV) 580.00 445.00 72.0 87.6 25* 8,15,58 BOEING B-777-200 GE90-94B(BLK IV) 580.00 445.00 72.0 88.5 30 8,15,58 BOEING B-777-200 GE90-94B(BLK IV) 656.00 470.00 77.0 87.8 25* 8,15,58 BOEING B-777-200 GE90-94B(BLK IV) 656.00 470.00 77.0 88.8 30 8,15,58 BOEING B-777-200 PW4074 440.90 440.90 71.3 88.7 25* 8,15 BOEING B-777-200 PW4074 440.90 440.90 71.3 89.5 30 8,15 PAGE 33
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 BOEING B-777-200 PW4074 535.00 445.00 77.5 88.7 25* 8,15 BOEING B-777-200 PW4074 535.00 445.00 77.5 89.5 30 8,15 BOEING B-777-200 PW4077 445.00 440.90 70.8 88.7 25* 8,15 BOEING B-777-200 PW4077 445.00 440.90 70.8 89.5 30 8,15 BOEING B-777-200 PW4077 545.00 445.00 77.5 88.7 25* 8,15 BOEING B-777-200 PW4077 545.00 445.00 77.5 89.5 30 8,15 BOEING B-777-200 PW4090 545.00 445.00 74.9 88.5 25* 8,15,59 BOEING B-777-200 PW4090 545.00 445.00 74.9 89.1 30 8,15,59 BOEING B-777-200 PW4090 656.00 470.00 81.3 89.0 25* 8,15,59 BOEING B-777-200 PW4090 656.00 470.00 81.3 89.5 30 8,15,59 BOEING B-777-200 PW4090 at PW4074 rating 447.40 445.00 71.3 88.5 25* 8,15,59 BOEING B-777-200 PW4090 at PW4074 rating 447.40 445.00 71.3 89.1 30 8,15,59 BOEING B-777-200 PW4090 at PW4074 rating 535.00 470.00 77.5 89.0 25* 8,15,59 BOEING B-777-200 PW4090 at PW4074 rating 535.00 470.00 77.5 89.5 30 8,15,59 BOEING B-777-200 PW4090 at PW4077 rating 447.50 445.00 70.7 88.5 25* 8,15,59 BOEING B-777-200 PW4090 at PW4077 rating 447.50 445.00 70.7 89.1 30 8,15,59 BOEING B-777-200 PW4090 at PW4077 rating 545.00 470.00 77.5 89.0 25* 8,15,59 BOEING B-777-200 PW4090 at PW4077 rating 545.00 470.00 77.5 89.5 30 8,15,59 BOEING B-777-200 RR TRENT 875 458.00 445.00 72.1 88.6 25* 8,15 BOEING B-777-200 RR TRENT 875 458.00 445.00 72.1 89.6 30 8,15 BOEING B-777-200 RR TRENT 875 545.00 470.00 79.0 89.1 25* 8,15 BOEING B-777-200 RR TRENT 875 545.00 470.00 79.0 90.0 30 8,15 BOEING B-777-200 RR TRENT 877 458.00 445.00 71.3 88.6 25* 8,15 BOEING B-777-200 RR TRENT 877 458.00 445.00 71.3 89.6 30 8,15 BOEING B-777-200 RR TRENT 877 555.00 470.00 79.0 89.1 25* 8,15 BOEING B-777-200 RR TRENT 877 555.00 470.00 79.0 90.0 30 8,15 BOEING B-777-200 RR TRENT 884 545.00 445.00 76.1 88.6 25* 8,15 PAGE 34
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 BOEING B-777-200 RR TRENT 884 545.00 445.00 76.1 89.6 30 8,15 BOEING B-777-200 RR TRENT 884 632.50 470.00 82.5 89.1 25* 8,15 BOEING B-777-200 RR TRENT 884 632.50 470.00 82.5 90.0 30 8,15 BOEING B-777-200 RR TRENT 892 545.00 445.00 74.6 88.6 25* 8,15 BOEING B-777-200 RR TRENT 892 545.00 445.00 74.6 89.6 30 8,15 BOEING B-777-200 RR TRENT 892 656.00 470.00 82.1 89.1 25* 8,15 BOEING B-777-200 RR TRENT 892 656.00 470.00 82.1 90.0 30 8,15 BOEING B-777-200 RR TRENT 895 632.50 445.00 79.7 88.6 25* 8,15 BOEING B-777-200 RR TRENT 895 632.50 445.00 79.7 89.6 30 8,15 BOEING B-777-200 RR TRENT 895 656.00 470.00 81.2 89.1 25* 8,15 BOEING B-777-200 RR TRENT 895 656.00 470.00 81.2 90.0 30 8,15 BOEING B-777-300 PW4090 450.00 445.00 69.2 88.2 25* 8,15,59 BOEING B-777-300 PW4090 450.00 445.00 69.2 89.0 30 8,15,59 BOEING B-777-300 PW4090 660.00 524.00 83.3 89.6 25* 8,15,59 BOEING B-777-300 PW4090 660.00 524.00 83.3 90.2 30 8,15,59 BOEING B-777-300 PW4098 550.00 445.00 74.4 88.8 25* 8,15 BOEING B-777-300 PW4098 550.00 445.00 74.4 89.7 30 8,15 BOEING B-777-300 PW4098 660.00 524.00 81.0 90.1 25* 8,15 BOEING B-777-300 PW4098 660.00 524.00 81.0 91.0 30 8,15 BOEING B-777-300 RR TRENT 884 550.00 445.00 76.5 88.4 25* 8,15 BOEING B-777-300 RR TRENT 884 550.00 445.00 76.5 89.5 30 8,15 BOEING B-777-300 RR TRENT 884 660.00 524.00 85.0 89.8 25* 8,15 BOEING B-777-300 RR TRENT 884 660.00 524.00 85.0 90.7 30 8,15 BOEING B-777-300 RR TRENT 892 550.00 445.00 75.0 88.4 25* 8,15 BOEING B-777-300 RR TRENT 892 550.00 445.00 75.0 89.5 30 8,15 BOEING B-777-300 RR TRENT 892 660.00 524.00 82.9 89.8 25* 8,15 BOEING B-777-300 RR TRENT 892 660.00 524.00 82.9 90.7 30 8,15 PAGE 35
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 BOMBARDIER BD-700-1A10 (Global Express) BR700-710-A2-20 93.50 78.50 73.6 83.2 30 8,15 BOMBARDIER BD-700-1A10 (Global Express) BR700-710-A2-20 96.00 78.50 74.6 83.2 30 8,15 BOMBARDIER CL-600-2C10 (CRJ700) CF34-8C1 72.50 66.90 68.2 82.5 45 8,15 BOMBARDIER CL-600-2C10 (CRJ700) CF34-8C1 75.00 66.90 69.1 82.5 45 8,15 BOMBARDIER DHC-6 PT6A-27 12.50 12.50 67.0 78.0 4 BOMBARDIER DHC-6 PT6A-27 12.50 12.50 67.0 78.0 - 4 BOMBARDIER DHC-7 PT6A-50 45.50 42.00 69.0 84.0 25 15 BOMBARDIER DHC-8 102 PW120 34.50 33.90 66.7 81.2 35 15 BOMBARDIER DHC-8 103 PW121 34.50 33.90 65.7 81.2 35 15 BOMBARDIER DHC-8 106 PW121 36.30 33.90 66.4 81.2 35 15 BOMBARDIER DHC-8 201/202 PW123 36.30 33.90 66.4 81.2 35 15 BOMBARDIER DHC-8 311 PW123 43.00 42.00 65.4 80.7 35 8,15 BOMBARDIER DHC-8 314 PW123 43.00 42.00 67.1 80.6 35 8,15 BOMBARDIER DHC-8-400 (Q400) PWC 150A 61.70 60.50 61.0 81.6 35 8,15,42 BOMBARDIER DHC-8-400 (Q400) PWC 150A 61.70 60.50 61.0 83.4 15 8,15 BOMBARDIER DHC-8-400 (Q400) PWC 150A 65.20 62.00 62.5 81.7 35 8,15,42 BOMBARDIER DHC-8-400 (Q400) PWC 150A 65.20 62.00 62.5 83.3 15 8,15 BOMBARDIER DHC-8-401 (Q400) PWC 150A 61.70 60.50 61.0 81.6 35 8,15,42 BOMBARDIER DHC-8-401 (Q400) PWC 150A 61.70 60.50 61.0 83.4 15 8,15 BOMBARDIER DHC-8-401 (Q400) PWC 150A 65.20 62.00 62.5 81.7 35 8,15,42 BOMBARDIER DHC-8-401 (Q400) PWC 150A 65.20 62.00 62.5 83.3 15 8,15 BOMBARDIER DHC-8-402 (Q400) PWC 150A 61.70 60.50 61.0 81.6 35 8,15,42 BOMBARDIER DHC-8-402 (Q400) PWC 150A 61.70 60.50 61.0 83.4 15 8,15 BOMBARDIER DHC-8-402 (Q400) PWC 150A 65.20 62.00 62.5 81.7 35 8,15,42 BOMBARDIER DHC-8-402 (Q400) PWC 150A 65.20 62.00 62.5 83.3 15 8,15 BRITTEN-NORMAN ISLANDER BN-2B O-540-E4C5 6.20 6.20 68.0 73.0 - 11 CANADAIR CHALLENGER CL-600 ALF-502L 40.40 36.00 66.9 81.7 45 12 PAGE 36
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 CANADAIR CHALLENGER CL-600 ALF-502L 41.25 36.00 67.5 81.7 45 15 CANADAIR CHALLENGER CL-601 CF34-1A 43.10 36.00 66.4 80.4 - 15 CANADAIR CHALLENGER CL-601 CF34-1A 45.10 36.00 67.0 80.4 45 15 CANADAIR CHALLENGER CL-601 CF34-3A/A1/A2 45.10 36.00 66.5 80.4 45 15 CANADAIR RJ (CL-600-2B19) CF34-3A1 47.50 44.70 62.7 81.4 45 15 CANADAIR RJ (CL-600-2B19) CF34-3A1 53.00 47.00 67.2 81.4 45 15 CASA AIRCRAFT C-212-CC TPE 331-10/10R-501C/511C 16.98 16.42 65.7 79.7 40 15 CASA AIRCRAFT C-212-CD TPE 331-10R-512C/502C 16.98 16.42 64.7 80.5 40 15 CASA AIRCRAFT C-212-CE TPE 331-10R-512C/502C 16.98 16.42 64.7 80.5 40 15 CASA AIRCRAFT C-212-CF TPE 331-10R-501C/511C 16.98 16.42 65.7 79.7 40 15 CASA AIRCRAFT C-212-DE PT6A-5B 16.98 16.42 68.0 76.9 40 15 CASA AIRCRAFT C-212-DF TPE 331-10R-502C/512C/513C 16.98 16.42 64.7 80.5 40 15 CASA AIRCRAFT C-295 PW 127 GM 46.30 45.63 69.9 81.6 15 15 CASA AIRCRAFT CN-235-100 CT7-9C 33.29 32.85 68.8 80.8 23 15 CASA AIRCRAFT CN-235-200 CT7-9C 34.83 34.39 70.1 79.9 40 15 CASA AIRCRAFT CN-235-300 CT7-9C3 34.83 34.39 69.1 80.2 15 15 CESSNA 150 0-200-A 1.60 1.60 56.0 59.0 - 11 CESSNA 150M O-200-A 1.60 1.60 55.0 59.0 - 11 CESSNA 152 0-235-L2C 1.70 1.70 55.0 59.0 - 11 CESSNA 170B C-145-2H 2.20 2.20 68.0 61.0 - 11 CESSNA 172 O-320-E2D 2.30 2.30 61.0 61.0 - 11 CESSNA 172N 0-320-H2AD 2.30 2.30 63.0 62.0 - 10 CESSNA 177RG I0-360-A1B6 2.80 2.80 65.0 62.0 - 11 CESSNA 180 O-470-J 2.80 2.80 69.0 63.0 - 11 CESSNA 182P O-470-S 3.00 3.00 70.0 56.0 - 10,11 CESSNA 182Q 0-470-U 3.00 3.00 69.0 56.0 - 10,11 CESSNA 185F I0-520-D 3.40 3.40 66.0 64.0 - 11 PAGE 37
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 CESSNA 206 IO-520-A 3.30 3.30 70.2 63.5 - 11 CESSNA 206H IO-580-AIA 3.60 3.60 69.3 63.7 - 11,21 CESSNA 207 IO-520-F 3.80 3.80 74.3 63.8 - 11 CESSNA 210 IO-520-L 3.80 3.80 71.4 67.1 - 10,11 CESSNA 310Q I0-470-V0 5.20 5.20 68.0 73.7 - 10,11 CESSNA 310R TSIO-520-BB 5.50 5.50 65.0 73.0 - 11 CESSNA 320C TSI0-470-D 5.20 5.20 70.0 73.0 - 11 CESSNA 337H IO-360-G 4.60 4.60 70.0 72.0 - 11 CESSNA 340A TSIO-520-MB 6.00 6.00 66.0 73.0 - 11 CESSNA 401 TSIO-520-E 6.30 6.30 67.0 73.0 - 11 CESSNA 402C TSIO-520-VB 6.90 6.90 68.0 74.0 - 11 CESSNA 404 GTSIO-520-M 8.40 8.40 61.0 74.0 - 11 CESSNA 414A TSIO-520-N 6.80 6.80 67.0 73.0 - 11 CESSNA 421C GTSIO-520-L 7.50 7.50 61.0 74.0 - 11 CESSNA 500 JT15D-1 10.90 10.90 67.0 77.7 40 15 CESSNA 560 JT15D-5A 15.90 15.20 68.7 80.5 35 8,15 CESSNA CARAVAN I PT6A-114 7.30 7.30 64.9 73.0 - CESSNA CITATION BRAVO (550) PW530A 14.80 13.50 61.3 82.3 40 8,15 CESSNA CITATION ENCORE (560) PW535A 16.63 15.20 58.3 83.0 35 8,15 CESSNA CITATION EXCEL (560XL) PW545 20.00 18.70 60.6 85.0 35 8,15 CESSNA CITATION I JT15D-1A 11.90 11.40 67.3 77.7 40 8,15 CESSNA CITATION II (550) JT15D-4 13.30 12.70 62.6 79.3 40 8,15 CESSNA CITATION II (550) JT15D-4 14.60 13.50 67.4 79.8 40 8,15 CESSNA CITATION III (650) TFE731-3B-100S 21.50 19.00 68.8 81.1 20* 8,15 CESSNA CITATION III (650) TFE731-3B-100S 22.00 20.00 69.3 81.4 20* 7,8,15 CESSNA CITATION III (650) TFE731-3B-100S 22.00 20.00 69.3 84.8 37 7,8,15 CESSNA CITATION JET (525) FJ44-1A 10.40 9.70 60.3 81.7 35 8,15 PAGE 38