APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH***
MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES CESSNA CITATION III (650) TFE731-3B-100S 20.00 81.4 20* 7,8,15 GULFSTREAM G200 PW306A 28.00 81.4 40 8,15,45 DASSAULT FALCON 20-F5 (M3547) TFE731-5BR-2C 28.88 81.3 40 8,15 GULFSTREAM GULFSTREAM IV - SP RR TAY 611-8 66.00 81.3 39 8,15 BOMBARDIER DHC-8 102 PW120 33.90 81.2 35 15 BOMBARDIER DHC-8 103 PW121 33.90 81.2 35 15 BOMBARDIER DHC-8 106 PW121 33.90 81.2 35 15 BOMBARDIER DHC-8 201/202 PW123 33.90 81.2 35 15 GULFSTREAM G100 TFE731-40R-200G 20.70 81.2 40 8,15 CESSNA CITATION III (650) TFE731-3B-100S 19.00 81.1 20* 8,15 AEROSPATIALE ATR72-210 PW127/HS 247F 47.07 81.0 33 8,15 DASSAULT FALCON 20-F5 (M3500) TFE731-5AR-2C 27.73 81.0 40 8,15 DASSAULT FALCON 20-F5 (M3530) TFE-731-5BR-2C 27.73 81.0 40 8,15 DASSAULT FALCON 900 TFE731-5AR-1C 42.00 81.0 20* 8,15 CASA AIRCRAFT CN-235-100 CT7-9C 32.85 80.8 23 15 BOMBARDIER DHC-8 311 PW123 42.00 80.7 35 8,15 GULFSTREAM GULFSTREAM IV RR TAY 611-8 58.50 80.7 39 8,15 BOMBARDIER DHC-8 314 PW123 42.00 80.6 35 8,15 CASA AIRCRAFT C-212-CD TPE 331-10R-512C/502C 16.42 80.5 40 15 CASA AIRCRAFT C-212-CE TPE 331-10R-512C/502C 16.42 80.5 40 15 CASA AIRCRAFT C-212-DF TPE 331-10R- 16.42 80.5 40 15 502C/512C/513C CESSNA 560 JT15D-5A 15.20 80.5 35 8,15 CESSNA CITATION V (560) JT15D-5A 15.20 80.5 35 8,15 CANADAIR CHALLENGER CL-601 CF34-1A 36.00 80.4 45 15 CANADAIR CHALLENGER CL-601 CF34-1A 36.00 80.4 - 15 CANADAIR CHALLENGER CL-601 CF34-3A/A1/A2 36.00 80.4 45 15 IAI 1125 ASTRA TFE731-3A-200G 20.70 80.4 40 8,15 PAGE 41A
AC36-3H 4/5/2012 APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH*** MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES CESSNA CITATION JET II (525A) FJ44-2C 11.50 80.3 35 8,15 FAIRCHILD DORNIER 328-300 Mod 10 PW306B 31.72 80.3 32 8,15 CASA AIRCRAFT CN-235-300 CT7-9C3 34.39 80.2 15 15 SHORTS 3-60 PT6A-65R 26.10 80.1 30 8,15 BAE SYSTEMS (BAe) BAe-748 SERIES 2B RR-DART MK535- 43.00 80.0 27 8,15
W/HUSHKIT BEECH B60 TI0-541-E1C4 6.80 80.0 - 10,11 SAAB FAIRCHILD SF340 GE CT7-5A2 26.50 80.0 35 12 CASA AIRCRAFT CN-235-200 CT7-9C 34.39 79.9 40 15 CESSNA CITATION II (550) JT15D-4 13.50 79.8 40 8,15 CASA AIRCRAFT C-212-CC TPE 331-10/10R-501C/511C 16.42 79.7 40 15 CASA AIRCRAFT C-212-CF TPE 331-10R-501C/511C 16.42 79.7 40 15 CESSNA S550 (SII) JT15D-4B 14.40 79.6 35 8,15 FAIRCHILD DORNIER 328-300 PW306B 31.06 79.5 32 8,15 DASSAULT FALCON 20-F5 TFE731-5AR-2C 27.76 79.4 25* 8,15 FOKKER F-27 MK500/600 MK552-7R 43.50 79.4 40 15,16 CESSNA CITATION II (550) JT15D-4 12.70 79.3 40 8,15 AEROSPATIALE SN601 CORVETTE JT15D-4 12.40 79.1 35 4 FOKKER F-27 MK500/600 MK552-7R 41.00 79.1 40 15,16 FOKKER F70 RR TAY MK620-15 81.00 79.0 42 8,15 SAAB 2000 AE2100A 47.40 78.9 20 8,15 SAAB SF340B (HS14RF-19 props) GE CT7-9B 28.50 78.8 20 8,15 SAAB SF340B (HS14RF-19 props) GE CT7-9B 28.00 78.8 20 8,15 FOKKER F70 RR TAY MK620-15 75.00 78.6 42 8,15 FAIRCHILD DORNIER SA226-AC METRO III TPE-331-11U 14.00 78.5 - 10,11 FAIRCHILD DORNIER SA226-T(B) MERLIN IIIB TPE-331-10U 12.50 78.5 - 5,11 FAIRCHILD DORNIER SA227-AT MERLIN III C TPE-331-10U 13.20 78.5 - 5,11 FAIRCHILD DORNIER SA227-AT MERLIN IV C TPE-331-11U 14.00 78.5 - 10,11 PAGE 42A
APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH***
MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES PIPER CHEYENNE 400LS TPE-331-14 11.10 78.5 - 11 BOMBARDIER DHC-6 PT6A-27 12.50 78.0 4 CESSNA CITATION ULTRA (560) JT15D-5D 15.20 78.0 35 8,15 CESSNA CITATION VII (650) TFE731-4C-3S 20.00 78.0 20* 8,15 GULFSTREAM 695A COMMANDER 1000 TPE-331-10 10.60 77.9 - 5,11 BEECH SUPER KINGAIR 200 PT6A-41 12.50 77.8 - 11 BEECH SUPER KINGAIR B200 PT6A-41 12.50 77.8 - 10,11 BEECH SUPER KINGAIR B200T/CT PT6A-42 12.50 77.8 - 5,11 CESSNA 500 JT15D-1 10.90 77.7 40 15 CESSNA CITATION I JT15D-1A 11.40 77.7 40 8,15 GULFSTREAM 690C COMMANDER 840 TPE-331-5 9.70 77.4 - 5,11 GULFSTREAM 690D COMMANDER 900 TPE-331-5 10.60 77.4 - 10 GULFSTREAM 695 TPE-331-10 9.70 77.4 - 5,15 GULFSTREAM 695 COMMANDER 980 TPE-331-10 9.70 77.4 - 5,11 LEARJET LEARJET 60 PW305A 19.50 77.4 40 8,15 BEECH F90 KINGAIR PT6A-135 10.90 77.3 - 5,11 SHORTS SKYVAN TPE-331-201 12.50 77.3 46 MITSUBISHI MU300 DIAMOND I JT15D-4 13.20 77.2 30 12 BEECH B100 KINGAIR TPE-331-6 11.20 77.1 - 11 BEECH C99 AIRLINER PT6A-34 11.30 77.1 - 5,11 PIPER PA-42 CHEYENNE PT6A-41 9.40 77.1 - 10,11 BEECH 1900/1900C PT6A-65B 16.10 77.0 - 10 BEECH 58P TSIO-520WB 6.20 77.0 - 10,11 BEECH 58TC TSIO-520-WB 6.20 77.0 - 10,11 GULFSTREAM 500S IO-540-E1B5 6.80 77.0 - 10 CASA AIRCRAFT C-212-DE PT6A-5B 16.42 76.9 40 15 BEECH B200/T/CT/C;C-12F(4 BLD) PT6A-42 12.50 76.6 - PAGE 43A
AC36-3H 4/5/2012 APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH*** MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES CESSNA CONQUEST II TPE-331-8 9.80 76.5 - 5,11 BAE SYSTEMS (JETSTREAM) JETSTREAM 4100 TPE331-14-801H/802H 22.30 76.4 15 12,15 BAE SYSTEMS (JETSTREAM) JETSTREAM 4100 TPE331-14-801H/802H/805H 23.30 76.3 15 12,15 EMBRAER EMB 110-P2 PT6A-34 12.50 76.0 - 4 FAIRCHILD DORNIER SA226-AT TPE-331-3U-303G 12.50 76.0 - 4 FAIRCHILD DORNIER SA226-T TPE-331-3U-303G 12.50 76.0 - 4 FAIRCHILD DORNIER SA226-TC METRO II TPE-331-3UW-303G 12.50 76.0 - 4 GULFSTREAM 690B TPE-331-5-251K 9.70 76.0 - 10 MITSUBISHI MU-2B-26A TPE-331-5-252M 10.00 76.0 - 4 MITSUBISHI MU-2B-36A TPE-331-5-252M 10.20 76.0 - 4 BEECH 300/300C KING AIR PT6A-60A 14.00 75.9 - SAAB SF340A (Dowty props) GE CT7-5A2 26.50 75.8 20 8,15 BEECH C90 PT6A-21 9.70 75.0 - 10 BEECH H18 R-985AN-14B 9.50 75.0 - 11 CESSNA CONQUEST I PT6A-112 8.20 75.0 - 10,11 BAE SYSTEMS (JETSTREAM) JETSTREAM 31 TPE331-10U-501H 14.60 74.7 - 15 FAIRCHILD DORNIER DORNIER 228 TPE-331-5-252D 12.60 74.7 - BEECH 99A PT6A-27 10.40 74.0 - 4 BEECH A100 PT6A-28 11.20 74.0 - 4 BEECH B80 IGS0-540-A1D 8.80 74.0 - 11 BEECH E55 (2 BLD) I0-520-C 5.30 74.0 - 11 BEECH E55 (3BLD) IO-520-C 5.30 74.0 - 11 CESSNA 402C TSIO-520-VB 6.90 74.0 - 11 CESSNA 404 GTSIO-520-M 8.40 74.0 - 11 CESSNA 421C GTSIO-520-L 7.50 74.0 - 11 GULFSTREAM 680FL IGSO-540-B1A 8.00 74.0 - 11 PIPER PA-31-325 TIO-540-F2BD 6.50 74.0 - 11 PAGE 44A
APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH***
MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES PIPER PA-31-350 TI0-540-J2BD 7.00 74.0 - 11 PIPER PA-31T PT6A-28 9.00 74.0 - 4 BEECH 65 QUEENAIR IGSO-480-A1B6 7.40 73.8 - 11 CESSNA 310Q I0-470-V0 5.20 73.7 - 10,11 BEECH 58/58A BARON (3 BLD) IO-550-C 5.40 73.3 - 11 BEECH 58 (2BLD) I0-520-C 5.40 73.0 - 11 BEECH 58 (3BLD) IO-520-C 5.40 73.0 - 11 BEECH B55 IO-470-L 5.10 73.0 - 11 BEECH B55(3BLD) IO-470-L 5.10 73.0 - 11 BRITTEN-NORMAN ISLANDER BN-2B O-540-E4C5 6.20 73.0 - 11 CESSNA 310R TSIO-520-BB 5.50 73.0 - 11 CESSNA 320C TSI0-470-D 5.20 73.0 - 11 CESSNA 340A TSIO-520-MB 6.00 73.0 - 11 CESSNA 401 TSIO-520-E 6.30 73.0 - 11 CESSNA 414A TSIO-520-N 6.80 73.0 - 11 CESSNA CARAVAN I PT6A-114 7.30 73.0 - GULFSTREAM 560E GO-480-C1B6 6.50 73.0 - 11 PIPER 601P IO-540-S1A5 6.00 73.0 - 11 PIPER PA-23-250 IO-540-C4B5 4.94 73.0 - 11 PIPER PA-31-310 TI0-540-A2C 6.50 73.0 - 11 PIPER PA-602P IO-540-AA1A5 6.00 73.0 - 11 PIPER PA-60-600 IO-540-K1J5 5.50 73.0 - 11 CESSNA 337H IO-360-G 4.60 72.0 - 11 GULFSTREAM GA-7 O-320-D1D 3.80 72.0 - 4 PIPER PA-34-200T TSI0-360-E 4.50 72.0 - 11 PIPER PA-34-220T TSIO-360-KB 4.50 72.0 - 11 BEECH D95A TRAVELAIR IO-320-B1B 4.20 71.1 - 11 PAGE 45A
AC36-3H 4/5/2012 APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH*** MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES BEECH 76 I0-360-A1G6D 3.90 71.0 - 11 PIPER PA-44-180 O-360-E1A6D 3.80 71.0 - 11 PIPER PA-44-180T(2BLD) TO-360-E1A6D 3.90 71.0 - 11 PIPER PA-44-180T(3BLD) TO-360-E1A6D 3.90 71.0 - 11 PIPER PA-30 TWIN COMANCHE IO-320-B 3.60 70.6 - 11 BEECH 35-B33 I0-470-K 3.00 68.0 - 10,11 CESSNA 210 IO-520-L 3.80 67.1 - 10,11 BEECH 35-C33A I0-520-B 3.30 64.0 - 11 BEECH A36 IO-520-BA 3.60 64.0 - 11 BEECH A36 BONANZA IO-550-B 3.65 64.0 - 11 BEECH B36TC BONANZA TSIO-520U 3.85 64.0 - 11 BEECH F33A I0-520-B 3.40 64.0 - 11 BEECH V35B (3BLD) I0-520-B 3.40 64.0 - 11 BELLANCA 17-30A I0-540-T4B5D 3.30 64.0 - 4 CESSNA 185F I0-520-D 3.40 64.0 - 11 CESSNA T210L TSI0-520-R 3.80 64.0 - 11 CESSNA T210M TSI0-520-R 3.80 64.0 - 11 CESSNA TU206G TSI0-520-M 3.60 64.0 - 11 EXTRA FLUGZEUGBAU EA 400 TSIOL-550-A 4.41 64.0 - 11,21 PIPER PA-32-300 IO-540-K1G5D 3.40 64.0 - PIPER PA-32R-300 IO-540-K1G5D 3.60 64.0 - 11 PIPER PA-32R-301 IO-540-K1G5D 3.60 64.0 - 11 PIPER PA-32R-301T TIO-540-S1AD 3.60 64.0 - 11 PIPER PA-32RT-300 IO-540-K1A5D 3.60 64.0 - 11 PIPER PA-46-31P MALIBU TSIO-520-BE 4.10 63.9 - 11 CESSNA 207 IO-520-F 3.80 63.8 - 11 CESSNA T206H TIO-540-AJIA 3.60 63.8 - 11,21 PAGE 46A
APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH***
MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES CIRRUS DESIGN CORP. SR 22 IO-550-N 3.40 63.8 - 11,21 CESSNA 206H IO-580-AIA 3.60 63.7 - 11,21 CESSNA 206 IO-520-A 3.30 63.5 - 11 CLASSIC AIRCRAFT WACO CLASSIC F-5 R-755-B2 2.70 63.4 - 11 MOONEY M20M TIO-540-AF1A 3.37 63.3 - 11,21 MOONEY M20M TIO-540-AF1A 3.20 63.3 - 11,21 ESTUMKEDA LTD d.b.a MAC-145B IO-540-T4B5 2.74 63.1 - 11,21 MICCO AIRCRAFT CO.
FOUND AIRCRAFT CANADA FBA-2C1 IO-540-D4A5 3.20 63.1 - 11,21 BEECH E35 E-225-8 2.70 63.0 - 11 BEECH K35/M35 IO-470-C 3.00 63.0 - 11 CESSNA 180 O-470-J 2.80 63.0 - 11 PIPER PA-24-260 IO-540-B1A5 3.20 63.0 - 11 PIPER PA-28-235 O-540-B4B5 3.00 63.0 - 11 PIPER PA-28-236 O-540-J3A5D 3.00 63.0 - 11 MAULE MX7-235 0540-JIA5D 2.50 62.7 - 11 BEECH A24R I0-360-A1B6 2.80 62.0 - 11 BEECH C23 0-360-A4K 2.50 62.0 - 11 BEECH C24R IO-360-A1B6 2.80 62.0 - 11 BEECH C35 E-185-11 2.70 62.0 - 11 BELLANCA 8GCBC 0-360-C2E 2.20 62.0 - 11 CESSNA 172N 0-320-H2AD 2.30 62.0 - 10 CESSNA 177RG I0-360-A1B6 2.80 62.0 - 11 GULFSTREAM 112 IO-360-C1D6 2.70 62.0 - 11 MOONEY M20C 0-360-A1D 2.60 62.0 - 11 MOONEY M20F w/MODWORK STC# IO-360-E5 2.74 62.0 - 11,21 SA02204AT MOONEY M20J I0-360-A1B6D 2.70 62.0 - 4
PIPER PA-28-181 O-360-A4M 2.50 62.0 - 11
PAGE 47A
AC36-3H 4/5/2012 APPENDIX 1, CHANGE 1
ESTIMATED MAXIMUM A-WEIGHTED SOUND LEVELS
MEASURED IN ACCORDANCE WITH PART-36 APPENDIX -C- PROCEDURES
***APPROACH*** MLW MANUFACTURER AIRPLANE ENGINE 1000 LBS EST dBA FLAPS NOTES PIPER PA-28RT-201(2BLD) I0-360-C1C6 2.80 62.0 - 11 PIPER PA-28RT-201T(3BLD) TSIO-360-FB 2.90 62.0 - 11 CIRRUS DESIGN CORP. SR 20 (2 Bladed Prop) IO-360-ES 2.90 61.9 - 11,21 CIRRUS DESIGN CORP. SR 20 (3 Bladed Prop) IO-360-ES 2.90 61.9 - 11,21 BEECH A-23 IO-360-A 2.40 61.0 - 11 CESSNA 170B C-145-2H 2.20 61.0 - 11 CESSNA 172 O-320-E2D 2.30 61.0 - 11 GULFSTREAM AA-5A O-320-E2G 2.20 61.0 - 11 OSTMECKLENBURGISCHE OMF-100-160 O-320-D2A 1.96 61.0 - 11,21
FLUGZEUGBAU PIPER PA-18-150 0-320-A2B 1.80 61.0 - 11 PIPER PA-28-140 O-320-E3D 2.20 61.0 - 11 PIPER PA-28-151 O-320-E3D 2.20 61.0 - 11 PIPER PA-28-161 O-320-D3G 2.40 61.0 - 11 PIPER PA-28-200 I0-360-C1C 2.70 61.0 - BEECH 77 O-235-L2C 1.70 60.0 - 11 BELLANCA 7GCAA 0-320-A2B 1.70 60.0 - 4 PIPER PA-38-112 O-235-L2C 1.70 60.0 - 11 CESSNA 150 0-200-A 1.60 59.0 - 11 CESSNA 150M O-200-A 1.60 59.0 - 11 CESSNA 152 0-235-L2C 1.70 59.0 - 11 GULFSTREAM AA-1B O-235 1.60 59.0 - 11 CESSNA 182P O-470-S 3.00 56.0 - 10,11 CESSNA 182Q 0-470-U 3.00 56.0 - 10,11 GULFSTREAM AA-5B TIGER O-360-A4K 2.20 52.0 - 10,11 PAGE 48A
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 AEROSPATIALE ATR42-300 PW120/HS 14SF5 34.72 34.17 66.5 84.9 30 15 AEROSPATIALE ATR42-300 PW120/HS 14SF5 37.26 36.16 68.4 84.7 30 15 AEROSPATIALE ATR42-320 PW121/HS 14SF5 35.60 35.27 66.7 84.8 30 15 AEROSPATIALE ATR42-320 PW121/HS 14SF5 37.26 36.16 67.7 84.7 30 15 AEROSPATIALE ATR72-200 PW124/HS 14SF11 44.07 43.87 70.7 82.7 30 15 AEROSPATIALE ATR72-200 PW124/HS 14SF11 48.50 47.07 73.2 82.4 30 15 AEROSPATIALE ATR72-210 PW127/HS 14SF11 47.40 47.07 71.8 82.2 33 15 AEROSPATIALE ATR72-210 PW127/HS 14SF11 48.50 47.07 72.3 82.2 33 15 AEROSPATIALE ATR72-210 PW127/HS 247F 47.40 47.07 66.4 81.0 33 8,15 AEROSPATIALE ATR72-210 PW127/HS 247F 48.50 47.07 67.0 81.0 33 8,15 AEROSPATIALE MOHAWK 298 PT6A-45A 23.40 23.00 76.0 86.0 - 4 AEROSPATIALE NORD-262C BASTAN-VIIA 22.90 22.70 78.3 88.9 - 4,8 AEROSPATIALE SN601 CORVETTE JT15D-4 13.90 12.40 63.8 79.1 35 4 AIRBUS A-300B CF6-50A 302.00 269.00 79.1 90.9 25 4,8 AIRBUS A-300B1 CF6-50A 302.00 269.00 76.8 90.7 15* 4,8,9 AIRBUS A-300B1 CF6-50A 302.00 269.00 76.8 91.4 25 4,8,9 AIRBUS A-300B2-1A CF6-50A 301.40 281.10 76.8 90.7 25 4,8,9 AIRBUS A-300B2-1A CF6-50A 301.40 281.10 76.8 91.4 15* 4,8,9 AIRBUS A-300B2-1A CF6-50A 312.40 286.70 78.3 90.4 15* 4,8,9 AIRBUS A-300B2-1A CF6-50A 312.40 286.70 78.3 90.9 25 4,8,9 AIRBUS A-300B2-1C CF6-50C 302.00 281.10 76.0 90.4 15* 4,8,9 AIRBUS A-300B2-1C CF6-50C 302.00 281.10 76.0 90.7 25 4,8,9 AIRBUS A-300B2-1C CF6-50C 312.40 286.70 77.1 90.4 15* 4,8,9 AIRBUS A-300B2-1C CF6-50C 312.40 286.70 77.1 90.9 25 4,8,9 AIRBUS A-300B2-K-3C CF6-50C 312.40 286.70 75.9 90.7 15* 4,8,9 AIRBUS A-300B2-K-3C CF6-50C 312.40 286.70 75.9 91.3 25 4,8,9 PAGE 1
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 AIRBUS A-300B4-2C CF6-50C 330.00 293.30 77.9 90.0 15* 4,8,9 AIRBUS A-300B4-2C CF6-50C 330.00 293.30 77.9 91.5 25 4,8,9 AIRBUS A-300B4-2C CF6-50C 336.60 293.30 78.5 90.0 15* 4,8,9 AIRBUS A-300B4-2C CF6-50C 346.50 293.30 79.4 90.0 15* 4,8,9 AIRBUS A-310-203 CF6-80A3 275.57 261.24 72.4 87.4 40 8,15 AIRBUS A-310-203 CF6-80A3 313.05 267.85 77.2 87.5 40 8,15 AIRBUS A-310-203C CF6-80A3 305.55 267.85 76.3 87.5 40 8,15 AIRBUS A-310-203C CF6-80A3 313.05 267.85 77.2 87.5 40 8,15 AIRBUS A-310-204 CF6-80C2A2 295.41 268.96 72.4 89.0 40 8,15 AIRBUS A-310-204 CF6-80C2A2 313.05 268.96 74.6 89.0 40 8,15 AIRBUS A-310-221 JT9D-7R4D1 275.57 261.24 72.6 89.0 40 8,15 AIRBUS A-310-221 JT9D-7R4D1 313.05 267.85 77.3 89.2 40 8,15 AIRBUS A-310-222 JT9D-7R4E1 305.55 267.85 75.9 89.2 40 8,15 AIRBUS A-310-222 JT9D-7R4E1 313.05 268.96 76.9 89.2 40 8,15 AIRBUS A-310-304 CF6-80C2A2 295.41 273.37 72.4 89.1 40 8,15 AIRBUS A-310-304 CF6-80C2A2 346.12 273.37 78.9 89.1 40 8,15 AIRBUS A-310-308 CF6-80C2A8 346.12 273.37 75.6 88.9 40 8,15 AIRBUS A-310-308 CF6-80C2A8 361.55 273.37 77.3 88.9 40 8,15 AIRBUS A-310-322 JT9D-7R4E1 330.69 271.16 79.0 90.1 40 8,15 AIRBUS A-310-322 JT9D-7R4E1 337.30 273.37 79.9 90.1 40 8,15 AIRBUS A-310-324 PW4152 330.69 271.16 76.2 91.6 40 8,15 AIRBUS A-310-324 PW4152 346.12 273.37 78.2 91.6 40 8,15 AIRBUS A319-111 CFM56-5B5/P; Mod No. 27772 123.45 121.25 65.9 84.1 20* 8,15 AIRBUS A319-111 CFM56-5B5/P; Mod No. 27772 123.45 121.25 65.9 84.9 40 8,15 AIRBUS A319-111 CFM56-5B5/P; Mod No. 27772 166.44 149.91 77.1 84.3 20* 8,15 AIRBUS A319-111 CFM56-5B5/P; Mod No. 27772 166.44 149.91 77.1 85.4 40 8,15 AIRBUS A319-112/P CFM56-5B6/P 123.45 121.25 64.9 84.1 20* 8,15 PAGE 2
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 AIRBUS A319-112/P CFM56-5B6/P 123.45 121.25 64.9 84.9 40 8,15 AIRBUS A319-112/P CFM56-5B6/P 166.44 149.91 73.3 84.3 20* 8,15 AIRBUS A319-112/P CFM56-5B6/P 166.44 149.91 73.3 85.4 40 8,15 AIRBUS A319-114 CFM56-5A5 123.45 121.25 64.6 84.5 40 8,15 AIRBUS A319-114 CFM56-5A5 163.14 149.91 74.0 84.9 40 8,15 AIRBUS A319-131 V2522A5 123.45 121.25 65.7 82.9 40 8,15 AIRBUS A319-131 V2522A5 158.73 149.91 73.2 83.5 40 8,15 AIRBUS A319-132 V2524-A5 123.45 121.25 64.3 82.9 40 8,15 AIRBUS A319-132 V2524-A5 166.44 149.91 74.4 83.5 40 8,15 AIRBUS A-320-111 CFM56-5A1 149.90 139.90 71.0 85.2 20* 8,15 AIRBUS A-320-111 CFM56-5A1 149.90 139.90 71.0 85.9 35 8,15 AIRBUS A-320-211 CFM56-5A1 149.90 142.20 70.7 84.4 20* 8,15 AIRBUS A-320-211 CFM56-5A1 162.00 142.20 73.7 85.6 35 8,15 AIRBUS A320-214/P CFM56-5B4/P 132.27 127.86 65.2 84.2 20* 8,15 AIRBUS A320-214/P CFM56-5B4/P 132.27 127.86 65.2 85.1 35 8,15 AIRBUS A320-214/P CFM56-5B4/P 171.95 149.91 73.3 84.1 20* 8,15 AIRBUS A320-214/P CFM56-5B4/P 171.95 149.91 73.3 85.5 35 8,15 AIRBUS A-320-231 V2500.A1 149.90 142.20 70.3 83.1 20* 8,15 AIRBUS A-320-231 V2500.A1 162.00 142.20 72.9 84.7 40 8,15 AIRBUS A320-231 V2500-A1; Mod No. 23408 127.86 142.20 65.5 83.1 20* 8,15 AIRBUS A320-231 V2500-A1; Mod No. 23408 127.86 142.20 65.5 84.7 40 8,15 AIRBUS A320-231 V2500-A1; Mod No. 23408 171.95 142.20 74.6 83.1 20* 8,15 AIRBUS A320-231 V2500-A1; Mod No. 23408 171.95 142.20 74.6 84.7 40 8,15 AIRBUS A320-232 V2527-A5 132.27 123.45 66.1 83.5 40 8,15 AIRBUS A320-232 V2527-A5 182.98 149.91 77.3 83.5 40 8,15 AIRBUS A321-211 CFM56-5B3/P; Mod No. 27772 165.34 143.29 69.8 85.2 21* 8,15 AIRBUS A321-211 CFM56-5B3/P; Mod No. 27772 165.34 143.29 69.8 86.0 25 8,15 PAGE 3
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 AIRBUS A321-211 CFM56-5B3/P; Mod No. 27772 205.02 166.44 77.1 85.6 21* 8,15 AIRBUS A321-211 CFM56-5B3/P; Mod No. 27772 205.02 166.44 77.1 86.7 25 8,15 AIRBUS A321-231 V2533-A5 165.34 143.29 68.1 84.3 21* 8,15 AIRBUS A321-231 V2533-A5 165.34 143.29 68.1 84.9 25 8,15 AIRBUS A321-231 V2533-A5 205.02 166.44 76.2 84.9 21* 8,15 AIRBUS A321-231 V2533-A5 205.02 166.44 76.2 85.5 25 8,15 AIRBUS UK 1-11-200 MK506-W/HUSHKIT 80.00 71.00 84.1 90.3 45 15 AIRBUS UK 1-11-200 SPEY-MK506 80.00 71.00 85.8 94.3 45 15 AIRBUS UK 1-11-400 MK511-W/HUSHKIT 89.50 78.00 87.5 92.5 45 15 AIRBUS UK 1-11-400 SPEY-MK511 89.50 78.00 90.5 96.2 45 8,15 AIRBUS UK 1-11-500 SPEY-MK512 99.70 87.00 89.9 98.6 45 4 AIRBUS UK 1-11-500 SPEY-MK512 104.50 87.00 90.5 98.6 45 4 BAE SYSTEMS (AVRO) 146-RJ 70 LF507-1F 84.00 83.50 69.3 85.7 24* 8,15,22,43 BAE SYSTEMS (AVRO) 146-RJ 70 LF507-1F 84.00 83.50 71.2 85.7 24* 8,15,22 BAE SYSTEMS (AVRO) 146-RJ 70 LF507-1F 84.00 83.50 71.2 87.4 33 8,15,22 BAE SYSTEMS (AVRO) 146-RJ 70 LF507-1F 84.00 83.50 69.3 87.4 33 8,15,22,43 BAE SYSTEMS (AVRO) 146-RJ 70 LF507-1F 90.00 83.50 73.4 85.7 24* 8,15,22 BAE SYSTEMS (AVRO) 146-RJ 70 LF507-1F 90.00 83.50 73.4 87.4 33 8,15,22 BAE SYSTEMS (AVRO) 146-RJ 70 LF507-1F 95.00 83.50 72.9 85.7 24* 8,15,22,43 BAE SYSTEMS (AVRO) 146-RJ 70 LF507-1F 95.00 83.50 72.9 87.4 33 8,15,22,43 BAE SYSTEMS (AVRO) 146-RJ 85 LF507-1F 89.50 77.50 71.1 85.2 24* 8,15,22 BAE SYSTEMS (AVRO) 146-RJ 85 LF507-1F 89.50 77.50 71.1 86.7 33 8,15,22 BAE SYSTEMS (AVRO) 146-RJ 85 LF507-1F 97.00 85.00 73.7 85.6 24* 8,15,22 BAE SYSTEMS (AVRO) 146-RJ 85 LF507-1F 97.00 85.00 73.7 87.3 33 8,15,22 BAE SYSTEMS (AVRO) 146-RJ 100 LF507-1F 95.00 83.00 73.3 85.5 24* 8,15,22 BAE SYSTEMS (AVRO) 146-RJ 100 LF507-1F 95.00 83.00 73.3 87.2 33 8,15,22 BAE SYSTEMS (AVRO) 146-RJ 100 LF507-1F 101.50 88.50 75.7 85.8 24* 8,15,22 PAGE 4