APPENDIX 6 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN
AIRPLANES IN THE TRANSPORT CATEGORY MANUFACTULEL MTOW MLW ENGINE DATA PROPELLER DIAM BLADES ELAPS NOISE LEVEL (EPNdB) MODE 1000# MER, MODEL NO. SHE RPM MER, MODEL (N) PICH IQ AF TO SL AP STAGE NOTES DEHAVILLAND 43.00 PRATT& WHITNEY 2 2249 1200 HAMILTON STANDARD 156 5 35 80.7 87.2 93.3 DHC-8-314 42.00 PW123 14SF-15 DEHAVILLAND 41.10 PRATT&WHITNEY 2 2142 1200 HAMILTON STANDARD 156 5 35 79.5 87.0 93.3 3 DHC-8-315 40.00 PW123E 14SF-15
- DEHAVILLAND 43.00 PRATT& WHITNEY 2 2142 1200 HAMILTON STANDARD 156 5 35 80.0 86.9 93.3 DHC-8-315 42.00 PW123E 14SF-15 DORNIER 30.84 PRATT& WHITNEY 2 2180 HARTZELL 142 12 32 82.1 83.8 94.8
• 328-100/MOD 10 29.16 PW119B HD-E6C-3B V EMBRAER 21.17 PRATT&WHITNEY 2 1500 HAMILTON STD. 126 15 25 76.6 81.6 92.5 EMB-120 21.17 PW 115 14RF-9 EMBRAER 25.40 PRATT& WHITNEY 2 HAMILTON STD. 126 15 25 81.2 83.5 92.3 EMB-120 24.80 PW118 14RF-9 V FOKKER 45.85 PRATT& WHITNEY 2 8 26 81.0 85.0 96.8 3 50 41.82 125B FOKKER 45.00 ROLLS ROYCE 2 DOWTY ROTOL 138 40 90.6 92.2 100.3 2 F27 MK500 42.00 DART 7/MK535-7R R193-4-30-4 FOKKER 45.00 ROLLS ROYCE 2 DOWTY ROTOL 138 40 86.9 90.1 94.3 3 F27 MK500 43.50 DART 7/MK 535-7 R193-4-30-4 V FOKKER 45.00 ROLLS ROYCE 2 DOWTY ROTOL 138 0 40 87.4 89.8 94.3 3 1 F27 MK500 43.50 DART 7/MKS35-7R R193-4-30-4 FOKKER 45.90 ROLLS ROYCE 2 DOWTY ROTOL 138 4 0 40 87.6 89.8 94.3 1 F27 MK500 43.50 DART 7/MK551-7R R193-4-30-4 V FOKKER 45.00 ROLLS ROYCE 2307 DOWTY ROTOL 138 40 87.4 89.8 94.1 1 F27 MK500/600 41.00 DART 7/MKS52-7R R193-4-30-4 V FOKKER 45.90 ROLLS ROYCE 2 2307 DOWTY ROTOL 138 40 87.6 89.8 94.3 F27 MK500/600 43.50 DART 7/MK552-7R R193-4-30-4 V Page 5
8/27191 AC 36-1G APPENDIX 6 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN
AIRPLANES IN THE TRANSPORT CATEGORY MANUFACTURER MTOW MLW ENGINE DATA PROPELLER wid BLADES FLAPS NOISE LEVEL (EPNdB) MOREL 1000฿ MER, MODEL NO. MER MODEL (IN) PICH IQ AP IQ SLAP STAGE NOTES FOKKER 45.00 ROI LS ROYCE 2 DOWTY ROTOL 138 4 40 90.6 92.2 100.3 2 F27 MK600 42.00 DART7 MK532-7R R193-4-30-4 JETSTREAM 23.00 ALLIEDSIGNAL 2 1500 1552 MCCAULEY 114 5 9 15 85.8 83.5 87.8 JETSTREAM 4100 22.30 TPE-331-14 B/CSJF936C1101/2L114G LOCKHEED 155.00 ALLISON 4 4050 1020 HAMILTON STD 162 18 35 94.8 96.7 98.1 L382G 135.00 501-D22A 54H60 MCDONNELL DOUGLAS 28.75 PRATT&WHITNEY 2 HARTZELL 115 0 45 82.4 84.4 91.9 3 DCIC (BTC STC) 28.75 PT6A-67R HC-B5MA-3/M11276 SAAB 50.20 ALLISON 2 DOWTY ROTOL 15 35 78.4 87.5 87.9 3 2000(w/PECS mod) 48.50 AE2100A R381/6-123-F/5 SAAB 28.50 GENERAL ELECTRIC 2 1384 HAMILTON STD. 132 4 15 20 77.7 86.1 90.1 340B 28.00 CT7-9B 14RF-19 SAAB 28.50 GENERAL ELECTRIC 2 1384 DOWTY ROTOL 132 4 15 20 78.0 85.9 91.6 3 3408 28.00 CT7-9B R375/4-123-F/21 v SAAB 28.50 GENERAL ELECTRIC 2 1384 DOWTY ROTOL 132 15 20 78.0 85.9 91.6 340B 28.00 CT7-9B R354/4-123-F/13/20 SAAB 28.00 GENERAL ELECTRIC 2 1384 DOWTY ROTOL 132 4 20 78.2 85.8 84.4 SF340A 27.20 CT7-5A2 R375/4-123-F/21 SAAB 28.00 GENERAL ELECTRIC 1384 DOWTY ROTOL 132 4 15 20 78.2 85.8 84.4 3 SF340A 27.20 CT7-512 R354/4-123-F/13/20 SAAB FAIRCHILD 27.00 GENERAL ELECTRIC 2 1210 DOWTY ROTOL 126 15 35 79.3 87.6 89.6 3 340 26.50 CT7-5A R320/4-123-F/1 v SAAB FAIRCHILD 27.00 GENERAL ELECTRIC 1210 DOWTY KOTOL 126 4 15 35 79.5 87.4 89.6 3 340 26.50 CT7-7F R320/4-123-F/1 SAAB-SCANIA 27.27 GENERAL ELECTRIC 1735 DOWTY ROTOL 132 35 77.5 86.2 86.3 3 340 A W/APU 26.50 CT7-5A2 R354/4-123-F13 Page 6
APPENDIX 6 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN
AIRPLANES IN THE TRANSPORT CATEGORY
MANUFACTURER MTOW MLW ENGINE DATA PROPELLER DIAM BLADES FLAPS NOISE LEVEL (EPNIB) MODEL 1000# MER MODEL - NO. SUP RPM MFR, MODEL PITCH TO AP TO SL AP STAGE NOTES SHORT BROS. 22.00 PRATT&WHITNEY 1120 1675 HARTZELL 5 35 88.5 ฿3.9 92.8 SD3-30 21.61 PT6A-45 HC-3SMP-34/M10282B-6 SHORT BROS. 26.00 PRATT& WHITNEY 2 1327 HARTZELL 111 5 30 84.4 83.7 89.9 3 SD3-60 25.70 PT6A-65R HC-BSMP-3C/M10876K SHORT BROS. 27.10 PRATT& WHITNEY 1700 HARTZELL, 108 15 15 80.0 82.7 94.3 3 :SD3-60-300 25.70 PT6A-67R HC-A6A-3/A1046F Paget
AC36-1G 08/27/97 Appendix 6 Appendix 6 Notes Equipped With Standard Hushkit Full Thrust Takeoff 650 Meter Sideline See Appendix 1 For Charts And Equations For The Calculation Of Noise Certification Limits Page 8
APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DIAM BLADES NOISE LEVEL (dBA) MLW MODEL 1000# MER, MODEL NO. SHP RPM EXH MIR. MODEL MaBA PC CdBA NOTES AEROTECH/AUST. 9.10 ALLISON 2 HARTZELL 91 3 78.0 -2.1 75.9 N225 250-B17E HC-A3VF-7B/V10133N- ANDERSON GREEN 3.15 AVCO LYCOMING 250 2575 HARTZELL 77 2 75.2 - 1.5 73.7 WOOD 51 3.15 0-540-14D5 HC-E2YR-1S/8465-7R BEECH 12.50 PRATT&WHITNEY 2 847 2000 HARTZELL 98 3 82.8 -3.6 79.2
(200) 12.50 PT6A-41 HC-B3TN-3G/T10178H BEECH 16.60 PRATT&WHITNEY 2 1100 1700 2 HARTZELL 110 80.5 3.0 77.4 1900/1900C 16.10 PT6A-65B HCB4MP-3A/M10877K BEECH 14.40 PRATT & WHITNEY 1200 1700 McCAULEY 104 84.3 -5.5 79.3 2000 XPT6A-67 D-L104DSZ-O BEECH 5.50 TCM 300 2700 MCCAULEY 77 80.7 -3.3 77.4 58/58A 5.40 10-550-C 3AF32C512/82-NEA-5 BEECH 3.60 TELEDYNE 260 2700 MCCAULEY 80 78.8 -0.6 78.2 A36 3.60 I0-520-B 3A32C760/82 NB-2 BEECH 3.60 TELEDYNE 228 2350 5 MCCAULEY 84 78.0 -0.6 77.4 A36 3.60 I0-520-N 2A36C23/84B-0 BEECH 3.65 TCM 300 2700 MCCAULEY 80 78.2 - 1.6 76.7 A36 3.65 10-550-B 3A32C406/82NDB-2 BEECH 3.65 TELEDYNE 300 2700 MCCAULEY 80 79.5 - 0.3 79.2 A36TС 3.65 TSIO-520-U 3A32C760/82 NB-2 BEECH 11.80 AIRESEARCH 2 715 2000 1 HARTZELL 90 80.2 -29 77.3 B100 11.20 TPE331-6-252B HC-B4TN-5C/T10173F BEECH 12.50 PRATT&WHITNEY 845 2000 HARTZELL, 99 82.8 - 3.6 79.2 B200 12.50 PT6A41 HC-B3TN-3GAT10178H BEECH 12.50 PRATT& WHITNEY 850 2000 HARTZELL 98 82.8 -3.6 79.2 B200/B200C 12.50 PT6A-42 HC-B3TN-3G/T10178H Page 1
APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW MLW ENGINE DATA PROPELLER DIAM BLADES NOISE LEVEL (dBA) MODEL 1000# MER, MODEL NO. RPM EXH MER, MODEL PITCH MaBA PC CaBA NOTES BEECH 12.50 PRATT& WHITNEY 2 850 2000 2 MCCAULEY 98 3 79.3 -3.9 75.4 B200/B200C 12.50 PT6A-42 3GFR34C702/100LA-2 BEECH 12.50 PRATT& WHITNEY 2 850 2000 MCCAULEY 94 80.7 -3.9 76.8 B200/B200C/C12F 12.50 PT6A-42 4HFR34C754/94LA-0 BEECH 12.50 PRATT&WHITNEY 845 2000 HARTZELL 99 3 82.8 -3.3 79.5 B200CT 12.50 PT6A-42 HC-B3TN-3G/T10178H BEECH 12.50 PRATT&WHIINEY 850 2000 MCCAULEY 98 79.3 - 3.8 75.5 B200T/B200CT 12.50 PT6A-42 3GFR34C702/100LA-Z BEECH 12.50 PRATT&WHITNEY 2 $50 2000 MCCAULEY 94 4 80.7 -3.8 76.8 B200T/B200CT 12.50 PTGA-42 4HFR34C754/94LA-O v BEECH 15.00 PRATT&WHITNEY 2 1050 1700 2 HARTZELL 105 75.9 -3.8 72.1 1 B300 PT6A-60A HC-B4MP-3/M10476K BEECH 3.86 TELEDYNE 293 2700 MCCAULEY 78 78.7 0.5 79.2 B36TC 3.86 TS10-520-U 82NDA4 BEECH 5.10 TELEDYNE 2 221 2550 HARTZELL 76 3 77.7 -3.0 74.7 B55 5.10 10-470-1. PHC-C3YF-2/FC7663-2 v BEECH 5.10 TELEDYNE 223 2550 HARTZELL 78 81.0 -3.0 78.0 B5S 5.10 10-470-1 BHC-C2YF-2CH/FC846 BEECH 5.40 TELEDYNE 2 254 2550 2 HARTZELL 78 $2.0 -3.1 78.9 B58 5.40 10-520-C BHC-J2YF-2C/FC8475- BEECH 5.40 TELEDYNE 2 256 2650 2 HARTZELL 76 81.9 -3.1 78.8 B58 3.40 10-520-C PHC-J3YF-2/FC7663-D V BEECH 5.50 TCM 2 300 2700 HARTZELL 78.5 -3.1 75.4 B58 5.40 10-550-C4B FC-7063Q BEECH 6.10 TELEDYNE 301 2600 2 HARTZELL 78 80.6 -1.5 79.1 B58P 6.10 TSIO-520-L PHC-J3YF-2/FC7663-D Page 2
AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F) MANUFACTURER MTOW ENGINE DATA PROPELLER DIAM. BLADES VER TATTESION MODEL MLW 1000# MER MODEL NO. SHP. BPM EXH MER, MODEL ON PITCH SION BEECH 6.20 CONTINENTAL 2 294 2600 HARTZELL 78 78.2 -2.1 191 B58P 6.20 TS10-520-WB PHC-J3YF-2UF/FC7663 BEECH 6.10 TELEDYNE 294 2600 HARTZELL 78 78.2 -2.1 76.1 B 58TC 6.10 TS10-520-WB PHC-J3YF-2UF/FC7663 BEECH 6.20 CONTINENTAL 2 301 2600 2 HARTZELL 78 10.6 .1.5 79.1 B58TC 6.20 TS10-520-L PHC-J3Y-2F/FC7663-D BEECH 6.78 LYCOMING 2 296 2750 HARTZELL 74 3 $2.1 -2.5 79.6 B60 6.78 TIO-541-EIC4 HC-F3YR-2UF/FC7479 BEECH 9.02 PRATT&WHITNEY 700 1900 HARTZELL 93 76.2 -5.8 70.4 B65-90 $.55 PT6A-135 HC-B3TN-2(B)T10173 BEECH 3.98 LYCOMING 165 2700 HARTZELL 76 2 79.5 -2.3 77.2 B76 0-360-A1G6D HC-M2YR-2CLUF/FC7 BEECH 3.90 LYCOMING 165 2700 2 HARTZELL 76 80.2 - 1.5 78.7 B76 3.90 0-360-A1G6D HC-M2YR-2CEUF/FC7 BEECH 1.68 LYCOMING 115 2700 SENSENICH 72 2 65.1 -1.3 63.8 B77 1.68 0-235-12C 72CKS12-0-52 BEECH 5.30 TCM 2 300 2700 2 HARTZELL 74 4 78.5 -3.1 75.4 B95-C55 5.30 10-550-C FC-7063Q BEECH 2.45 LYCOMING 163 2700 SENSENICH 76 73.3 0.0 73.3 C23 2.45 0-360-A45 76EM8S5-0-60 F BEECH 2.75 LYCOMING 202 2700 HARTZELL 76 2 73.0 - 1.3 71.7 C24R 2.75 0-360-A1B6 HC-M2YR-1BF/FC7666 BEECH 9.66 PRATT&WHITNEY 2 550 2200 HARTZELL 93 78.7 4.4 74.3 C90 9.17 PT6A-21 HC-B3TN-2B/T10173B- BEECH 10.10 PRATT&WHITNEY 550 2200 HARTZELL 93 78.7 4.4 74.3 C90A PT6A-21 HC-B3TN-2(B) Page 3
8/27/97 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F)
MANUFACTURER MTOW MLW ENGINE DATA PROPELLER MODEL 1000# MER, MODEL NO. SHE RPM EXH MER MODEL SALON BEECH 11.30 PRATT&WHITNEY 2 715 2200 HARTZELL 93 3 EGL 6 5L C99 11.30 PT6A-34 HC-B3TN-3/T10173B-8 BEECH 5.30 TCM 300 2700 2 HARTZELL 74 4 78.5 -3.4 75.0 D5S 5.30 10-550-C FC-7063Q V BEECH 5.30 TELEDYNE 2 256 2650 2 HARTZELL 76 3 81.9 -3.2 78.7 E55 5.30 10-520-C PIIC-J3Y-2F/FC7663-2R V BEECH 5.30 TELEDYNE 2 254 2550 2 HARTZELL, 78 2 82.0 -3.2 78.8 ESS 5.30 10-520-C ПИС-C237-2C/C8475- BEECH 5.30 TCM 2 300 2700 2 HARTZELL 74 78.5 -3.4 75.0 ESS 5.30 IO-550-C FC-7063Q BEECH 5.30 TCM 2 300 2700 HARTZELL 74 78.5 -3.4 75.0 ESS 5.30 10-550-C FC-7063Q v BEECH 5.30 TCM 2 300 2700 HARTZELL 74 78.5 -3.4 75.0 ESS 5.30 10-550-C FC 7063Q BEECH 10.10 PRATT& WHITNEY 2 550 2200 HARTZELL 93 79.0 -4.0 75.0 E90 9.70 PT6A-28 HC-B3TN-2B/T10173B- BEECH 3.40 TELEDYNE 260 2700 MCCAULEY 80 78.3 - 1.4 76.9 F33 AC 3.40 I0-520-B 3A32C76/82NB-2 BEECH 3.40 TELEDYNE 225 2550 5 MCCAULEY 84 78.1 - 1.5 76.5 F33 AC 3.40 I0-520-BA 2A36C23/84 B-0 BEECH 10.95 PRATT&WHITNEY 754 1900 HARTZELL 92 77.9 - 5.0 72.9 F90 SUPER 10.95 PT6A-135 HC-B4TN-3B/T10173F BEECH 3.40 TELEDYNE 260 2700 5 MCCAULEY $0 3 78.8 -2.0 76.8 V3≤B 3.40 I0-520-R 3A32C76/82 NA-2 v BEECH 3.40 TELEDYNE 228 2550 MCCAULEY 84 78.1 - 1.5 76.6 V35B 3.40 10-520-BA 2A36C23/84B-0 v Page 4
8/27/97 APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F)
MANUFACTURER MTOW ENGINE DATA PROPELLER VIP THAT ISION MLW MODEL 1000# MIR, MODEL NO. SHIP RPM EXH MER, MODEL SHON BELLANCA 3.20 CONTINENTAL 225 2550 MCCAULEY 78 79.4 - 1.9 77.5 17-30A 3.20 I0-520-K D3A34C401/90DFA-12 BELLANCA 1.65 LYCOMING 115 2700 2 SENSENICH 72 2 71.5 -2.7 68.8 7ECA 1.65 0-235-K2C 74DM658-1-56 F BELLANCA 1.65 LYCOMING 150 2700 2 SENSENICH 73 71.5 -4.7 66.8 7GCAA 1.65 0-320-A2I3/-A2D 74DM658-1-56 F BELLANCA 1.65 LYCOMING 150 2700 SENSENICH 73 71.5 -4.6 66.9 7GCBC 1.65 0-320-A2B/A2D 74DM6S8-1-56 BELLANCA 1.80 LYCOMING 150 2700 2 MCCAULEY 80 68.4 1.9 70.3 TOCBC SEAPLANE L.BO 0-320 1A175GMA/8040 F BELLANCA 2.15 LYCOMING 180 2700 2 HARTZELL 76 2 76.3 -3.4 72.9 8GCBC 2.15 0-360-C1A/-CIE HC-C2YR-IBF/F7666A Fr BELLANCA 2.15 LYCOMING 149 2700 2 MCCAULEY 80 2 76.3 -3.5 72.8 8GCBC 2.15 0-360-C2A/-C2E 1A200/HFA BELLANCA 1.80 LYCOMING 150 2700 2 HARTZELI, 72 2 72.2 -2.2 70.0 8KCAB 1.80 AEIO-320-E1B HC-C2YL-4F/FC7663-4 BELLANCA 1.80 LYCOMING 150 2700 2 SENSENICH 74 2 72.2 -3.0 69.2 8KCАB 1.80 AEIO-320-E2B 74DM6S8-0 F BELLANCA 1.80 LYCOMING 180 2700 2 HARTZELL 74 72.2 - 5.0 67.2 8KCAB 1.80 AEIO-360-HI A HC-C2YR-4CF/FC7666 CESSNA 1.67 LYCOMING 110 2550 MCCAULEY 69 2 65.8 -1.0 64.8 152 1.67 0-235-L2C 1A102/TCM6955 Fr CESSNA 1.67 LYCOMING 1 110 2550 MCCAULEY 69 2 66.7 -0.4 66.3 152/A152 1.67 0-235-L2C IA103/TCM6958 F CESSNA 2.30 LYCOMING 160 2700 MCCAULEY 75 2 74.3 -0.5 73.8 172N (LAND) 2.30 0-320-H2AD 1C160/DTM 7557 F Page 5
8/27/97 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CER PART 36, APPENDIX F)
MANUFACTURER MTOW MLW ENGINE DATA PROPELLER DIAM BLADES VERAN SION MODEL 1000# MFR, MODEL NO. SHP RPM EXH MER, MODEL INI STION CESSNA 2.20 LYCOMING 160 2700 MCCAULEY ZZL 172N (SEA) 2.18 0-320-H2AD IA175/ETM8042 F CESSNA 2.40 LYCOMING 160 2700 MCCAULEY 75 2 74.3 -0.5 B'EL 172P 0-320-D25 1C160/DTM7557 F CESSNA 2.65 LYCOMING 180 2700 MCCAULEY 76 2 73.4 73.9 172RG 2.65 0-360-F1A6 B2D34C220/80VLA-3.5 CESSNA 2.50 LYCOMING 180 2700 MCCAULEY 76 2 72.0 -0.3 71.7 177B 2.50 IO-360-A1F6D B2D34C211/82PCA-6 CESSNA 2.80 LYCOMING 200 2700 MCCAULEY 78 76.3 -0.7 75.6 177RG 2.80 IO-360-AIB6D B2D34C207/78TCA-0 V CESSNA 2.95 TCM 230 2400 MCCAULEY 88 2 74.0 -2.2 71.8 180K (AMPHIB) 2.95 0-470-U C2A34C204/90DCA-2 CESSNA 2.80 TCM 230 2400 MCCAULEY 90 2 73.0 -3.0 70.0 180K (LAND) 2.80 O-470-U C2A34C204/90DCB-0 v CESSNA 2.95 TCM 230 2400 MCCAULEY 82 2 72.0 -2.9 69.1 182Q 2.95 O-470-U D2A34C203/90DCA-8 CESSNA 3.10 TCM 230 2400 MCCAULEY 82 2 72.0 - 2.9 69.1 182R 0-470-V D2A34C203/90DCA-8 CESSNA 3.80 TCM 285 2700 MCCAULEY 80 79.0 0.8 79.8 207A 3.80 IO-520-F D3A32C404/80VA-0 CESSNA 3.80 TCM 1 285 2700 MCCAULEY 80 77.8 -0.1 77.7 207A 3.80 IO-520-F D3A32C90/82NC-2 CESSNA 7.30 PRATT&WHITNEY 600 1900 HARTZELL 100 3 72.8 - 1.1 71.7 208 7.30 PT6A-114 HC-B3MN-3 CESSNA 8.00 PRATT&WHITNEY 600 1900 HARTZELL 100 72.8 0.7 73.5 208 7.80 PT6A-114 HC-B3MN-3 Page 6
APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CER PART 36, APPENDIX F) MANUFACTURER MTOW MLW ENGINE DATA PROPELLER DIAM. BLADES VIP THAT SION MODEL 1000฿ MFR, MODEL NO. SHP ВРМ ЕХЦ MER, MODEL MaDA PC CaBA SALÖN CESSNA 8.00 PRATT& WHIINEY 600 1900 2 HARTZELL 100 72.8 0.7 73.5 208 A 7.80 PT6A-114 HC-B3MN-3 CESSNA 8.75 PRATT&WHIINEY 600 1900 2 HARTZELL 100 72.8 2.3 75.1 2088 8.50 PT6A-114 HC-B3MN-3 CESSNA 3.80 TCM 285 2700 MCCAULEY 80 3 79.6 0.3 79.9 210M 3.80 IO-520-L-3A D3A34C404/80VA-0 V CESSNA 3.80 TCM 285 2700 MCCAULEY 80 79.6 0.0 79.6 210N 3.80 IO-520-L-3A D3A34C404/80VA-0 CESSNA 3.85 TCM 285 2700 McC AULEY 80 79.6 -0.6 79.0 210R 3.85 IO-520-L D3A34C404/8OVA-0 CESSNA 5.50 TCM 285 2700 MCCAULEY 77 82.0 -2.9 79.1 310R 5.41 IO-520-M 3AF32C87/82NC-5.5 CESSNA 5.99 ICM 300 2700 4 MCCAULEY 77 3 79.6 - 1.5 78.1 335 5.99 TSIO-520-EB 3AF32C87/82NC-5.5 CESSNA 4.63 TCM 195 2600 MCCAULEY 78 2 78.6 1.3 79.9 337H 4.41 TSIO-360-C D2AF34C310/90DEA-12 v CESSNA 4.63 TCM 195 2600 MCCAULEY 76 2 78.6 1.3 79.9 337H 4.41 TSIO-360-C D2AF34C307/L78CBA- CESSNA 5.99 TCM 310 2700 MCCAULEY 76 82.0 -5.5 76.5 340 А 5.99 TSIO-520-N 3AF32C93/82NC-S.5 CESSNA 5.99 TCM 2 310 2700 MCCAULEY 77 83.4 -3.7 79.7 340A 5.99 TSIO-520-N JAF32C93/82NC-5.5 V CESSNA 6.85 TCM 2 300 2700 MCCAULEY 76 81.6 -2.8 78.8 402B 6.85 TSIO-520-E 3AF32C87M/82NC-5.5 CESSNA 6.85 TCM 2 325 2700 4 MCCAULEY 76 80.8 -2.2 78.6 402C 6.85 TSIO-520-UB 3AF32C92N/82NC-6.5 V Page 7
APPENDIX 7 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (14 CFR PART 36, APPENDIX F)
MANUFACTURER MTOW ENGINE DATA PROPELLER DIAM BLADES NOISE LEVEL (JBA) MLW MODEL 1000# MER, MODEL NO. SHP RPM EXH MFR, MODEL (IN) PITCH MOhA PC CdBA NOTES CESSNA 6.85 TCM 310 2600 MCCAULEY 77 3 77.2 -2.1 75.1 402C 6.85 TSIO-520-VB 3AF32C93/82NC-5.5 CESSNA 8.40 TCM 2 375 3350 4 MCCAULEY 90 3 81.6 .2.7 78.9 404 8.09 GTSIO-520-M 3FF32C501/90UMB-0
8.40 PRATT&WHITNEY 2 550 2000 4 HARTZELL 93 3 81.1 - 5.0 76.1 404 8.10 PT6A-34 HCB3TN-3B/T10173-8R
9.36 PRATT&WHITNEY 500 1900 MCCAULEY 93 75.0 -3.0 72.0 406 9.36 PT6A-112 3GFR34C701/93KB-0 v
6.75 TCM 298 2600 4 MCCAULEY 77 3 79.1 -2.5 76.6
6.75 TSIO-520-N 3AF32C93/82NC-5.5
7.45 TCM 375 3350 4 MCCAULEY 80.3 -3.6 76.7 7 21 GTSIO-520-L 3FF32CS01/90UMB-0
8.20 PRATT&WHITNEY 2 450 1900 MCCAULEY 93 3 75.7 4.3 71.4 425 8.00 PT6A-112 36FR34C701/93KB-0
8.20 PRATT&WHITNEY 2 450 1900 4 HARTZELL 93 75.7 -4.3 71.4 425 8.00 PT6A-112 HC-B3TN-3C/T10178B-
8.60 PRATT&WHITNEY 2 450 1900 HARTZELL 93 3 75.7 -3.4 72.3
8.00 PT6A-112 HC-B3TN-3C/T10178B-
9.85 AIRESEARCH 2 636 1990 MCCAULEY 90 78.0 4.0 74.0 441 9.36 TPE331-8-401S 36FR34C601/93JA CESSNA 9.85 AIRESEARCH 2 636 1990 HARTZELL 90 3 78.0 -4.0 74.0 441 9.36 TPE331-8-401S HC-B3TN-5E/T10178-1 CESSNA 3.27 TCM 1 285 2700 MCCAULEY 80 78.9 - 1.2 77.7 A185F (AMPHIB) 3.12 IO-520-D D3A34C403/80VA-0 CESSNA 3.32 TCM 1 285 2700 MCCAULEY 80 78.9 -i0 77.9 A185F (FLOAT) 3.32 10-520-D-24 D3A32C90/82NC-2 Page 8