APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA)
MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES MAULE 2.30 LYCOMING 1 175 3 HARTZELL 76 2 2600 70.90 0.90 71.8 M-6-180 2.30 0-360-CIF HC-C2YR-1BF/F7666A V MAULE 2.30 LYCOMING 1 235 HARTZELL 78 2 2400 72.60 -5.00 67.6 M-6-235 2.30 0-540-J1A5D/-W1A5D HC-E2YR-1BF/F8468A V MAULE 2.50 LYCOMING 1 235 HARTZELL 81 2 2700 71.3 M-6-235 2.50 O-540-J1A5D HC-C2YR-1BF/F8468A V MAULE 2.50 LYCOMING 1 235 3 HARTZELL 78 2 2400 72.60 -0.30 72.3 M-7-235 2.50 O-540-J1A5D HC-C2YR-1BF/F8468A V MAULE 2.50 LYCOMING 1 235 3 HARTZELL 81 2 2400 74.70 -2.50 72.2 M-7-235 2.50 O-540-J1A5D HC-C2YR-1BF/F8468A V MITSUBISHI 10.47 AIRESEARCH 2 665 4 HARTZELL 98 4 1591 77.40 -2.90 74.8 MU-2B-40 9.96 TPE331-10-501 HC-B4TN-5DL/LT1028 V MITSUBISHI 11.56 AIRESEARCH 2 715 4 HARTZELL 98 4 1591 77.70 -1.40 76.5 MU-2B-60 11.60 TPE331-10-501M HC-B4TN-5DL/LT1028 V MOONEY 2.74 LYCOMING 1 192 MCCAULEY 74 2 2700 75.30 -1.30 74.0 M20J 2.74 IO-360-A3B6D B2D34C212/78CDA-4 V MOONEY 2.90 PORSCHE 7 HARTZELL 74 3 76.6 M20L 2.92 PRM3200N03 BHC-J2YF-1C/B7421 V MOONEY AIRCRAFT 2.90 TELEDYNE 1 210 4 MCCAULEY 74 2 2700 76.60 -1.10 75.4 M20K 2.90 TSI0-360-GB1 2A34C216/90DHB-16E V PARTENAVIA 4.39 AVCO LYCOMING 2 HARTZELL 76 2 2575 75.4 P68-TC 4.39 TO-360-C1A60 HC-C2YK-2CUF V PIPER 1.75 LYCOMING 1 150 7 SENSENICH 74 2 2700 69.00 -3.10 65.9 PA-18-150 1.75 0-320-A2B M74DM6-0-56 F PIPER 5.20 LYCOMING 2 250 6 HARTZELL 77 2 2575 76.80 -1.10 75.7 PA-23-250 4.94 I0-540-C4B5 HC-E2YR-28465-7R V Page 15
APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA)
MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES PIPER 5.20 LYCOMING 2 250 4 HARTZELL 77 2 2575 77.00 -0.80 76.2 PA-23T-250 4.94 TIO-540-C1A HC-E2YR-28465-7R V PIPER 2.33 LYCOMING 1 160 5 SENSENICH 74 2 2700 71.40 0.60 72.0 PA-28-161 2.33 0-320-D3G 74DM6-0-60 F PIPER 2.55 LYCOMING 1 180 5 SENSENICH 76 2 2700 73.40 0.50 73.9 PA-28-181 2.55 O-360-A4M 76EM8S5-062 F PIPER 3.00 LYCOMING 1 235 5 HARTZELL 80 2 2400 72.50 0.40 72.9 PA-28-236 3.00 0-540-J3A5D HC-F2YR-1F/F8468A-4 V PIPER 2.65 LYCOMING 1 200 MCCAULEY 74 2 2700 75.50 0.00 75.5 PA-28R-200 2.65 IO-360-CIC B2D34C213 V PIPER 2.65 LYCOMING 1 200 HARTZELL 74 2 2700 75.50 0.00 75.5 PA-28R-200 2.65 IO-360-CIC HC-C2YK-1(1)/F766A V PIPER 2.90 CONTINENTAL 1 200 2 HARTZELL 76 2 2575 69.10 0.50 69.6 PA-28R-201T 2.90 TSIO-360-FB PHC-C3YF-1F/7663-2R V PIPER 2.75 LYCOMING 1 200 5 MCCAULEY 74 2 2700 74.40 1.10 75.5 PA-28RT-201 2.75 I0-360-C1C6 B2D34213/90DHA-16 V PIPER 2.90 CONTINENTAL 1 200 4 HARTZELL 76 3 2575 72.50 0.30 72.8 PA-28RT-201T 2.90 TSIO-360F PHC-C3YF-1F/F7663-2 V PIPER 2.90 CONTINENTAL 1 200 2 HARTZELL 76 2 2575 69.10 0.30 69.4 PA-28RT-201T 2.90 TSIO-360-F BHC-C2YF-1F/F8459A V PIPER 6.50 LYCOMING 2 275 4 HARTZELL 80 3 2400 77.00 -1.60 75.4 PA-31 6.50 TIO-540-2AC HC-E3YR-2ATF FC846 V PIPER 6.50 LYCOMING 2 275 4 HARTZELL 80 3 2400 78.00 -1.10 76.9 PA-31-325 6.50 TI0-540-F2BD HC-E3YR-2ATF FC846 V PIPER 7.01 LYCOMING 2 315 4 HARTZELL 80 3 2400 78.00 0.90 78.9 PA-31-350 7.01 TIO-540-J2BD HC-E3YR-2ATF FC846 V Page 16
APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA)
MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES PIPER 7.80 PRATT&WHITNEY 2 620 4 HARTZELL 93 3 1900 76.50 -5.00 71.5 PA-31P 7.80 PT6A-135 HC-B3TN-3C/T10178-8 V PIPER 9.00 PRATT&WHITNEY 2 620 4 HARTZELL 93 3 2000 79.20 -5.00 74.2 PA-31T 9.00 PT6A-28 HC-B3TN-3B/T-10173B V PIPER 8.70 PRATT&WHITNEY 2 455 4 HARTZELL 93 3 2000 76.60 -1.60 75.0 PA-31T1 8.70 PT6A-11 HC-B3TN-3B/T-10173B V PIPER 9.47 PRATT&WHITNEY 2 620 4 HARTZELL 93 3 1900 79.20 -2.10 77.1 PA-31T2 PT6A-135 HC-B3TN-3B/T-10173B V PIPER 9.00 PRATT&WHITNEY 2 455 1 HARTZELL 93 3 2200 76.60 -1.00 75.6 PA-31T3 PT6A-11 HC-B3TN-3B/T-10173K V PIPER 8.97 PRATT&WHITNEY 2 620 4 HARTZELL 93 3 2000 78.20 -4.00 74.2 PA-31T-62 8.97 PT6A-28 HC-BTN-3B V PIPER 3.40 LYCOMING 1 300 HARTZELL 80 2 2700 80.50 -1.20 79.3 PA-32-300 3.40 I0-540-K1A5 HC-C2YR-1( )F/F8475D V PIPER 3.60 LYCOMING 1 300 5 HARTZELL 78 3 2700 78.10 -0.60 77.5 PA-32-301 3.60 I0-540-K1G5 HC-C3YR-1( )F/F7663R V PIPER 3.60 LYCOMING 1 294 5 HARTZELL 80 2 2600 77.30 -0.60 76.7 PA-32-301 3.60 IO-540-K1G5D HC-C2YR-1( )F/F8475D V PIPER 3.60 LYCOMING 1 300 4 HARTZELL 78 3 2700 76.10 -1.30 74.8 PA-32-301T 3.60 TI0-540-SIAD HC-E3YR-1( )F/F7673D V PIPER 3.60 LYCOMING 1 294 4 HARTZELL 80 2 2575 75.70 -1.30 74.4 PA-32-301T 3.60 TIO-540-SIAD HC-E2YR-1( )F/F8477 V PIPER 3.60 LYCOMING 1 300 5 HARTZELL 78 3 2700 78.10 0.30 78.4 PA-32R-301 3.60 IO-540-K1G5D HC-C3YR-1( )F/F7663R V PIPER 3.60 LYCOMING 1 294 5 HARTZELL 80 2 2600 77.30 0.30 77.6 PA-32R-301 3.60 IO-540-K1G5D HC-C2YR-1( )F/F8475D V Page 17
APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA)
MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES PIPER 3.60 LYCOMING 1 294 4 HARTZELL 80 2 2575 75.70 0.40 76.1 PA-32R-301T 3.60 TIO-540-SAID HC-E2YR-1( )F/F8477 V PIPER 3.60 LYCOMING 1 300 4 HARTZELL 78 3 2700 76.10 0.40 76.5 PA-32R-301T 3.60 TIO-540-SAID HC-E3YR-1/F7673 V PIPER 3.60 LYCOMING 1 300 HARTZELL 80 2 2400 75.40 0.00 75.4 PA-32RT-300 3.60 IO-540-S1AD HC-E2YR-1BF/F8477-4 V PIPER 4.60 CONTINENTAL 2 200 4 HARTZELL 76 2 2575 75.70 -2.20 73.5 PA-34-200T 4.30 TS10-360-E FC8459-8R/FJC8459-8R V PIPER 4.60 TELEDYNE 2 200 4 MCCAULEY 76 3 2575 78.60 -2.20 76.4 PA-34-200T 4.30 TS10-360-E/EB 80HA-4/L80HA-4 V PIPER 4.70 CONTINENTAL 2 200 4 HARTZELL 76 2 2600 74.20 -2.80 71.4 PA-34-220T 4.50 TSIO-360-KB BHC-C2YF-2CKUF/FC V PIPER 4.70 CONTINENTAL 2 200 4 MCCAULEY 76 3 2600 77.00 -2.80 74.2 PA-34-220T 4.50 TSIO-360-KB 3AF32C50B/82NFA-6 V PIPER 1.68 LYCOMING 1 112 5 SENSENICH 72 2 2600 67.80 0.00 67.8 PA-38-112 1.68 O-235-L2C 72CK-O-56 F PIPER 11.20 PRATT+WHITNEY 2 720 4 HARTZELL 95 3 2000 80.30 -3.50 76.8 PA-42 10.23 PT6A-41 HC-B3TN-3B/T10173A V PIPER 12.05 GARRETT 2 1000 4 DOWTY ROTOL 106 4 1540 75.10 -5.00 70.1 PA-42-1000 11.10 TPE331-14A-801Y R339/4-123-F/8RH R34 V PIPER 3.80 LYCOMING 2 180 5 HARTZELL 73 2 2700 77.20 -2.50 74.7 PA-44-180 3.80 0-360-A1H6 HC-C2Y(K,R)-2CEUF/F V PIPER 3.80 LYCOMING 2 180 5 HARTZELL 73 3 2700 78.10 -2.50 75.6 PA-44-180 3.80 O-360-E1A6D HC-C3YR-2EUF/FC-76 V PIPER 3.92 LYCOMING 2 180 4 HARTZELL 73 3 2575 74.70 -2.30 72.4 PA-44-180T 3.80 TO-360-E1A6D HC-C3YR-2EUF FC-76 V Page 18
APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA)
MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM MdBA PC CdBA NOTES PIPER 3.92 LYCOMING 2 180 4 HARTZELL 74 2 2575 73.80 -2.30 71.5 PA-44-180T 3.80 TO-360-E1A6D HC-C2YR-2CUF FC766 V PIPER 4.10 CONTINENTAL 310 4 HARTZELL 80 2 74.50 0.00 74.5 PA-46-310P 3.90 TSIO-520-BE BHC-C2YF-1BF/F8052 V PIPER 4.30 LYCOMING 350 4 HARTZELL 80 2 2500 75.20 -0.50 74.7 PA-46-350P 4.10 TIO-540-AE2A HC-I2YR-1 V PIPER 5.49 LYCOMING 2 284 HARTZELL 78 3 2520 82.40 -2.40 80.0 PA-600A 5.49 IO-540-K1J5 HC-C3YR-2UF FG-848 V PIPER 5.97 LYCOMING 2 290 HARTZELL 78 2 81.50 -1.70 79.8 PA-601P 5.97 I0-540-S1A5/-P1A5 HC-C3YR-2/C8468-8R V PIPER 6.00 LYCOMING 2 290 4 HARTZELL 78 3 2425 81.90 -2.60 79.3 PA-602P 6.00 IO-540-AA1A5 HC-3YR-2UF/FC8468-8 V PIPER 6.32 LYCOMING 2 350 4 HARTZELL 76 3 2500 80.80 -1.90 78.9 PA-60-700P TIO-540-U2A HC-C3YR-2UF/FC7451 V SIAI MARCHETTI 2.43 AVCO LYCOMING 1 HARTZELL 76 2700 73.2 F-260C 2.43 AEIO-540-D4A5 HC-C2YK-1BF V SIAI MARCHETTI 7.50 ALLISON 2 HARTZELL 90 3 2030 74.3 SF 600 7.50 250-B17C HC-B3TF-7A/T10173-1 V SIAI MARCHETTI 2.56 ALLISON 320 4 HARTZELL 76 3 2030 77.00 -5.00 72.0 SF260 2.56 250-B17D HC-B3TF-7A SOCATA 2.54 LYCOMING 1 180 HARTZELL 74 2 2700 70.7 TB 10 2.41 O-360-A1-AD HC-C2YK-1BF/F 7666 V SOCATA 3.09 LYCOMING 1 250 HARTZELL 80 2 2575 74.0 TB 20 2.94 IO-540-C4D5D HC-C2YK-IBF/F 8477-4 V SOCATA 3.09 LYCOMING 1 310 HARTZELL 80 2 2575 75.4 TB 21 2.94 IO-540-AB1AD HC-C2YK-IBF/F 8477-4 V Page 19
APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MLWMODEL MFR, MODEL NO. SHP EXH MFR, MODEL DIAM BLADES RPM MdBA PC CdBA NOTES
(1000#) (IN) PITCH SOCATA 2.34 LYCOMING 1 160 SENSENICH 74 2 2700 72.2 TB 9 2.34 O-320-D2A 74 DM 658-O-54 F TAYLORCRAFT 1.20 AVCO LYCOMING 1 118 3 HENDRICKSON 71 2 2500 72.60 -5.00 67.6 BC-12D 1.20 I0-360-E2A H73-A50 F TAYLORCRAFT 1.50 CONTINENTAL 1 100 5 MCCAULEY 69 2 2750 69.10 -0.70 68.4 F-19 1.50 0-200-A 1A105/SCM6950 F TAYLORCRAFT 1.50 LYCOMING 1 112 5 SENSENICH 71 2 2800 69.00 -0.20 68.8 F-21 1.50 0-235-L2C 72CK-0-50 F TRIDENT 3.80 TELEDYNE 1 232 7 HARTZELL 84 3 4000 78.20 -1.00 77.2 TR-1 3.80 TIARA 6-285-C4 HC-H3YF-3LF/FL-C96 V Page 20
11/15/01 AC36-1H Appendix 7 Appendix 7 Notes 1 Maximum Takeoff Weight Greater Than 12,500 lb. - Aircraft Certificated To FAR Part 41 Or FAR Part 23 Commuter Category Exhaust Configurations (Reciprocating Engines) 1 Stub Pipes 2 Small Collector, Short Exhaust Pipe 3 Baffles In Collector and/or Cones In Exhaust Pipe 4 Turbine Or Turbocharger 5 Heat Muff 6 Collector Wraparound Manifold Straight Pipe 7 Manifold Muffler 8 Resonator Muffler Page 21
11/15/01 AC36-1H Appendix 7
EQUATIONS FOR THE CALCULATION OF NOISE CERTIFICATION
LIMITS FOR PROPELLER DRIVEN SMALL AIRPLANES AND COMMUTER CATEGORY AIRPLANES 14 CFR PART 36, APPENDIX F NOISE LIMIT (dBA) Up To And Including 1,320 lb. 68 dB(A) ( W -1320)Over 1,320 lb. Up To And Including 3,300 lb. 68 +Ł dB(A)165 ł Over 3,300 lb. 80 dB(A) W = Takeoff Gross Weight In Pounds Page 22
11/15/01 АC36-1H Appendix 7 NOISE CERTIFICATION REQUIREMENTS - FAR PART 36, APPENDIX F
PROPELLER DRIVEN SMALL AIRPLANES AND COMMUTER CATEGORY AIRPLANES 88 86 84 82 80 80 78 Noise Level (dBA) 76 74 72 70 68 66 64 62 60 2000 4000 6000 8000 10000 12000 14000 16000 18000 20000 Weight (Ibs) Page 23
APPENDIX 8, CHANGE 1 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX G) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM NOTES ADAM AIRCRAFT INDUSTRIES 7.00 CONTINENTAL 2 HARTZELL 3 2700 87.8 A500 6.75 TSIO-550-E PHC-H3YF-2UF/FC7693 V AGUSTA SpA 2.60 LYCOMING 1 260 HARTZELL 76 2 2700 79.3 F260 E 2.60 AEIO-540-D/E4A5 HC-C2YK-4F/FC8477-8 V AQUILA TECHNISCHE ENTWIC 1.65 ROTAX 1 MT-PROPELLER 2 2260 65.2 AT01 1.65 912 S3 MTV-21-A/175-05 V AVIAT 2.00 LYCOMING 1 SENSENICH 2 2700 75.2 A-1B (WITH ENG. OPT.) 2.00 0-320-D2A 74DM6S8-0-58 F AVIAT AIRCRAFT INC. 2.25 LYCOMING 1 HARTZELL 76 2 2700 80.2 9 A-1C-180 2.25 O-360-A1P HC-C2YK-1BF/F7666A F AVIAT AIRCRAFT INC. 2.25 LYCOMING 1 MT-PROPELLER 80.7 2 2600 80.2 9 A-1C-180 2.25 O-360-A1P (175 HP DE MTV-15-B/205-58 F AVIAT AIRCRAFT INC. 2.25 LYCOMING 1 HARTZELL 80 2 2600 80.2 9 A-1C-180 2.25 O-360-A1P (175 HP DE HC-C2YR-1BF/F8477-4 F AVIAT AIRCRAFT INC. 2.25 LYCOMING 1 HARTZELL 80 2 2700 80.1 9 A-1C-200 2.25 IO-360-A1D6 HC-C2YR-1BF/F8477-4 F AVIAT AIRCRAFT INC. 2.25 LYCOMING 1 MT-PROPELLER 80.7 2 2650 82.8 9 A-1C-200 2.25 IO-360-A1D6 (196 HP D MTV-15-B/205-58 F CESSNA 2.30 THIELERT 1 MT-PROPELLER 3 2300 77.0 172K,L,&M (THIELERT STC ST0 2.30 TAE 125-01 MTV-6-A/187-129 V CESSNA 2.45 THIELERT 1 MT-PROPELLER 3 2300 70.9 172K,L,,M&P (THIELERT STC ST 2.45 TAE 125-01 MTV-6-A/187-129 V CESSNA 2.30 THIELERT 1 MT-PROPELLER 3 2300 75.7 172N&P (THIELERT STC ST0130 2.30 TAE 125-01 MTV-6-A/187-129 V CESSNA 2.45 LYCOMING 1 152.6 8 MCCAULEY 75 2 2210 73.3 172R 2.45 IO360-L2A 1C235LFA/7570 F Page 1
APPENDIX 8, CHANGE 1 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX G) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM NOTES CESSNA 2.30 THIELERT 1 MT-PROPELLER 3 2300 77.4 172R&S (THIELERT STC ST0130 2.30 TAE 125-01 MTV-6-A/187-129 V CESSNA 2.45 THIELERT 1 MT-PROPELLER 3 2300 71.3 172R&S (THIELERT STC ST0130 2.45 TAE 125-01 MTV-6-A/187-129 V CESSNA 2.95 CONTINENTAL TCM 1 HARTZELL 80 3 2700 77.8 182Q (BONAIRE STC# SA01218A 2.95 IO-550D PHC-G3YF-1RF/F8468 V CESSNA 3.10 LYCOMING 1 221.3 8 MCCAULEY 82 2 2400 79.7 182S 3.10 IO-540-AB1A5 B2D34C235/90DKB-8 V CESSNA 3.10 LYCOMING 1 229.3 8 MCCAULEY 79 3 2400 77.7 182S 3.10 IO-540-AB1A5 B3D36C431/80VSA-1 V CESSNA 3.60 LYCOMING 1 300 8 MCCAULEY 79 3 2700 84.5 206H 3.60 IO-540-X144 XB3D36C432-X/G80VS V CESSNA 3.60 LYCOMING 1 MCCAULEY 79 3 2500 79.6 206H 3.60 IO-580-AIA B3D36C432/80VSA-1 V CESSNA 3.60 LYCOMING 1 300 8 CESSNA 79 3 2500 79.8 206H 3.60 IO-580-X130 P4327345-01 V CESSNA 8.00 PRATT & WHITNEY 1 675 2 MCCAULEY 106 3 1900 79.0 208 8.00 PT6A-114A 3GFR34C703-106GA V CESSNA 8.00 PRATT & WHITNEY 1 600 MCCAULEY 106 3 1900 81.6 208/208A 8.00 PT6A-114 3GFR34C703-X/X-106G V CESSNA 8.75 PRATT & WHITNEY 1 600 MCCAULEY 106 3 1900 84.2 208B 8.75 PT6A-114 3GFR34C703-X/X-106G V CESSNA 8.75 PRATT & WHITNEY 1 675 HARTZELL 100 3 1900 80.1 208B 8.75 PT6A-114A HCBCMN3/M10083 V CESSNA 8.75 PRATT & WHITNEY 1 675 MCCAULEY 106 3 1900 82.7 208B 8.75 PT6A-114A 3GFR34C703-X/X-106G V Page 2
APPENDIX 8, CHANGE 1 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX G) MANUFACTURER MTOW ENGINE DATA PROPELLER DATA NOISE LEVEL (dBA) MODEL MLW (1000#) MFR, MODEL NO. SHP EXH MFR, MODEL DIAM (IN) BLADES PITCH RPM NOTES CESSNA 3.60 LYCOMING 1 MCCAULEY 79 3 2500 75.8 T206H 3.60 TIO-540-AJIA B3D36C432/80VSA-1 V CESSNA 3.60 LYCOMING 1 305.9 4 CESSNA 79 3 2500 75.8 T206H 3.60 TIO-540-X143 XB3D36432-X/80VSA-1 V CESSNA 3.80 CONTINENTAL TCM 1 MCCAULEY 80 3 2700 82.0 TU206G(WIPAIRE) TSIO-520M D3A34C402/90DFA-10 V CESSNA 3.80 CONTINENTAL TCM 1 MCCAULEY 80 3 2700 84.3 U206F(WIPAIRE) 3.80 IO-550-F D3A34C402/90DFA-10 V CESSNA 3.80 CONTINENTAL TCM 1 MCCAULEY 80 3 2700 84.3 U206G(WIPAIRE) 3.80 IO-550-F D3A34C402/90DFA-10 V CIRRUS DESIGN CORP. 2.90 CONTINENTAL 1 HARTZELL 76 2 2700 82.5 SR 20 2.90 IO-360-ES BHC-J2YF-1BF/F7694 V CIRRUS DESIGN CORP. 2.90 CONTINENTAL 1 HARTZELL 74 3 2700 82.5 SR 20 2.90 IO-360-ES PHC-J3YF-1MF/F7392-1 V CIRRUS DESIGN CORP. 3.40 CONTINENTAL 1 HARTZELL 78 3 2700 83.7 SR 22 3.40 IO-550-N PHC-J3YF-1RFX/F7694 V CLASSIC AIRCRAFT 2.95 JACOBS 1 SENSENICH 92 2 2200 79.4 F5C 2.95 R755B2 W96JB-4-68 F CUB CRAFTERS INCORPORATE 2.30 LYCOMING 1 MCCAULEY 2 2700 82.8 CC18 2.30 O-360-C4P 1A200FA8242 F CUB CRAFTERS INCORPORATE 2.30 LYCOMING 1 SENSENICH 2 2700 77.1 CC18 2.30 O-360-C4P M76EM8-0-56 F DATWYLER (MDC) 2.03 LYCOMING 1 MCCAULEY 74 2 2700 67.9 MD3-160(MUFFLED EXHAUST) 2.03 0-320-D2A 1C172/AGM7462 F DATWYLER (MDC) 2.03 LYCOMING 1 MCCAULEY 74 2 2700 71.7 MD3-160(STNDRD EXHAUST) 2.03 0-320-D2A 1C172/AGM7462 F Page 3