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
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 CITATION JET II (525A) FJ44-2C 12.38 11.50 62.7 80.3 35 8,15 CESSNA CITATION ULTRA (560) JT15D-5D 16.30 15.20 67.1 78.0 35 8,15 CESSNA CITATION V (560) JT15D-5A 16.30 15.20 69.4 80.5 35 8,15 CESSNA CITATION VI (650) TFE731-3C-100S 22.00 20.00 69.3 84.8 40 8,15 CESSNA CITATION VII (650) TFE731-4C-3S 23.00 20.00 65.7 78.0 20* 8,15 CESSNA CITATION VII (650) TFE731-4C-3S 23.00 20.00 65.7 81.6 40 8,15 CESSNA CITATION VII (650) TFE731-4R-3S 22.45 20.00 65.4 81.6 40 8,15 CESSNA CONQUEST I PT6A-112 8.20 8.20 63.0 75.0 - 10,11 CESSNA CONQUEST II TPE-331-8 9.80 9.80 63.0 76.5 - 5,11 CESSNA S550 (SII) JT15D-4B 15.10 14.40 64.8 79.6 35 8,15 CESSNA T206H TIO-540-AJIA 3.60 3.60 65.6 63.8 - 11,21 CESSNA T210L TSI0-520-R 3.80 3.80 73.0 64.0 - 11 CESSNA T210M TSI0-520-R 3.80 3.80 71.0 64.0 - 11 CESSNA TU206G TSI0-520-M 3.60 3.60 71.0 64.0 - 11 CIRRUS DESIGN CORP. SR 20 (2 Bladed Prop) IO-360-ES 2.90 2.90 72.3 61.9 - 11,21 CIRRUS DESIGN CORP. SR 20 (3 Bladed Prop) IO-360-ES 2.90 2.90 72.1 61.9 - 11,21 CIRRUS DESIGN CORP. SR 22 IO-550-N 3.40 3.40 73.6 63.8 - 11,21 CLASSIC AIRCRAFT WACO CLASSIC F-5 R-755-B2 2.70 2.70 57.8 63.4 - 11 CONCORDE CONCORDE O-593/M-602 400.00 112.9 109.5 - 4,8 DASSAULT FALCON 10 TFE731-2 19.30 17.64 69.4 81.8 30* 8,15 DASSAULT FALCON 10 TFE731-2-1C 19.30 17.64 69.4 85.3 52 8,15 DASSAULT FALCON 20 CF700-2D-2 28.60 27.30 77.0 90.1 25* 8,15 DASSAULT FALCON 20-Basic/D/E CF700-2D-2 28.66 27.32 77.0 90.3 40 8,15 DASSAULT FALCON 20-Basic/D/E/F (M2851) CF700-2D-2Q 28.66 27.32 71.4 88.9 40 8,15 DASSAULT FALCON 20-C5/D5/E5 (M3500) TFE731-5AR-2C 29.10 27.73 72.0 81.8 40 8,15 DASSAULT FALCON 20-C5/D5/E5 (M3530) TFE-731-5BR-2C 29.10 27.73 69.2 81.8 40 8,15 DASSAULT FALCON 20-C5/D5/E5 (M3547) TFE731-5BR-2C 30.50 28.88 72.1 82.2 40 8,15 PAGE 39
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 DASSAULT FALCON 20-F5 TFE731-5AR-2C 29.10 27.76 70.6 79.4 25* 8,15 DASSAULT FALCON 20-F5 (M3500) TFE731-5AR-2C 29.10 27.73 70.6 81.0 40 8,15 DASSAULT FALCON 20-F5 (M3530) TFE-731-5BR-2C 29.10 27.73 68.1 81.0 40 8,15 DASSAULT FALCON 20-F5 (M3547) TFE731-5BR-2C 30.50 28.88 71.4 81.3 40 8,15 DASSAULT FALCON 20-G (M2500) ATF3-6-2C 32.00 27.56 71.7 84.1 40 8,15 DASSAULT FALCON 50 TFE731-3-1C 38.80 35.70 70.9 82.0 20* 8,15 DASSAULT FALCON 50 TFE731-3-1C 38.80 35.72 70.9 87.6 48 8,15 DASSAULT FALCON 50 ( M1810) TFE731-40-1 40.79 35.72 70.6 84.5 48 8,15 DASSAULT FALCON 50 (M1230) TFE731-3-1C 40.78 35.71 72.6 82.0 20* 8,15 DASSAULT FALCON 50 (M1230) TFE731-3-1C 40.78 35.71 72.6 87.3 48 8,15 DASSAULT FALCON 50 (M2193) TFE731-40-1 40.79 35.72 70.6 84.5 48 8,15 DASSAULT FALCON 200 ATF3-6A-4C 32.00 27.60 71.7 84.1 40 8,15 DASSAULT FALCON 900 TFE731-5AR-1C 45.50 42.00 69.2 81.0 20* 8,15 DASSAULT FALCON 900 TFE731-5AR-1C 45.50 42.00 71.2 82.6 40 8,15 DASSAULT FALCON 900 (M1196) TFE731-5AR-1C 46.50 42.00 72.2 82.6 40 8,15 DASSAULT FALCON 900B (M1200) TFE731-5BR-1C 46.50 42.00 69.9 82.6 40 8,15 DASSAULT FALCON 900EX (M3000) TFE731-60-1 49.00 44.50 68.2 82.9 40 8,15 DASSAULT FALCON 2000 CFE738-1-1B 36.50 33.00 64.0 83.8 40 8,15 DASSAULT FALCON 2000EX (M1826) PW308C 41.30 39.30 67.3 81.6 40 DASSAULT FALCON 2000EX (M1842) PW308C 42.20 39.30 68.3 81.6 40 DASSAULT FALCON 7X (SFI) PW307A 69.00 62.40 70.5 84.0 40 DASSAULT FALCON 900DX (M4000, M3755, TFE731-60(-1C) 46.70 42.20 66.4 82.5 40 M3758) DASSAULT FALCON 900LX (M5281) TFE731-60(-1C) 49.00 44.50 66.5 82.5 40 DOUGLAS DC-3 R-1830-90C 25.20 24.40 85.0 84.0 - 5 EMBRAER EMB 110-P2 PT6A-34 12.50 12.50 71.0 76.0 - 4 EMBRAER EMB-120 BRASILIA PW115 21.20 21.20 63.2 81.8 45 12 EMBRAER EMB-145ER AE3007A 45.41 41.22 65.9 82.9 45 8,15 PAGE 40
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 EMBRAER EMB-145LR AE3007A1/1 48.50 42.54 68.0 82.5 45 8,15 ESTUMKEDA LTD d.b.a MAC-145B IO-540-T4B5 2.85 2.74 72.5 63.1 - 11,21 MICCO AIRCRAFT CO.
EXTRA FLUGZEUGBAU EA 400 TSIOL-550-A 4.41 4.41 67.9 64.0 - 11,21 FAIRCHILD F-27-F RR DART MK529 38.50 36.70 77.3 87.0 - 11 FAIRCHILD DORNIER 328-100 Mod 10 PW 119B 30.84 29.17 66.6 83.0 12 15,38 FAIRCHILD DORNIER 328-100 Mod 20 PW 119C 30.84 29.17 67.0 83.0 12 15,38 FAIRCHILD DORNIER 328-300 PW306B 33.51 31.06 62.2 79.5 32 8,15 FAIRCHILD DORNIER 328-300 Mod 10 PW306B 34.52 31.72 62.7 80.3 32 8,15 FAIRCHILD DORNIER DORNIER 228 TPE-331-5-252D 13.10 12.60 66.3 74.7 - FAIRCHILD DORNIER SA226-AC METRO III TPE-331-11U 14.50 14.00 69.2 78.5 - 10,11 FAIRCHILD DORNIER SA226-AT TPE-331-3U-303G 12.50 12.50 71.0 76.0 - 4 FAIRCHILD DORNIER SA226-T TPE-331-3U-303G 12.50 12.50 71.0 76.0 - 4 FAIRCHILD DORNIER SA226-T(B) MERLIN IIIB TPE-331-10U 12.50 12.50 68.9 78.5 - 5,11 FAIRCHILD DORNIER SA226-TC METRO II TPE-331-3UW-303G 12.50 12.50 71.0 76.0 - 4 FAIRCHILD DORNIER SA227-AT MERLIN III C TPE-331-10U 13.20 13.20 69.5 78.5 - 5,11 FAIRCHILD DORNIER SA227-AT MERLIN IV C TPE-331-11U 14.50 14.00 69.2 78.5 - 10,11 FOKKER F100 RR TAY MK620-15 95.00 88.00 72.0 83.3 42 8,15 FOKKER F100 RR TAY MK650-15 98.00 88.00 69.9 82.1 25* 8,15 FOKKER F100 RR TAY MK650-15 98.00 88.00 69.9 82.8 42 8,15 FOKKER F-27 MK500/600 MK552-7R 45.00 41.00 75.3 79.1 40 15,16 FOKKER F-27 MK500/600 MK552-7R 45.90 43.50 76.0 79.4 40 15,16 FOKKER F-27-100 RR DART6 MK514 39.00 37.50 76.0 82.6 - 11 FOKKER F-27-200 MK532-7 43.50 41.00 78.0 88.1 - 5 FOKKER F-27-500/600 MK532-7R 43.50 42.00 78.0 86.8 - 5 FOKKER F-28 MK1000 SPEY MK555-15 65.00 59.00 79.2 94.1 42 4 FOKKER F-28 MK1000 SPEY MK555-15 65.00 59.00 79.2 94.7 42 4 FOKKER F-28 MK4000 SPEY MK555-15H 73.00 64.00 75.5 86.3 - PAGE 41