APPENDIX 9
AIRCRAFT NOISE DATA FOR FOREIGN CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (ICAO ANNEX 16, CHAPTER 6) MANUFACTURER MTOW MLW ENGINE DATA PROPELLER Sauvid Tvid MODEL 1000# MER, MODEL NO. SHP EXH MFG MODEL INT SAION DORNIER 13.15 GARRETT 2 HARTZELL 107 75.3 228-201 TPE331-5-252D HC-B4TN-SML/LT10574 DORNIER 9.59 PRATT+WHITNEY 2 399 HARTZELL 100 70.8 - 5.0 65.8 DO-28-D PT-GA-110 HC-B-3TN-3D V FOKKER 2.61 AVCO LYCOMING 1 260 HARTZELL 85 3 68.8 -0.1 68.7 P-149D GO-480-B1A6 HC-A3V20-ID/V8433SP V FUI HEAVY IND. 2.54 LYCOMING 180 MCCAULY 74 73.1 0.5 73.6 FA-200-180 IO-360-B1B B2D34-CS3/74E-O V GREAT LAKES AIRCRAFT 1.80 LYCOMING 177 HARTZELL 74 2 74.4 -5.0 69.4 2T-1A-2 AEJO-360-B1G6 HC-C2YK-4BF V GULFSTREAM AMERICAN 1.52 LYCOMING 1 108 2500 MC CAULEY 71 68.3 0.3 68.6 AA-LA 0-235-C2C SCM1A105/7154 F GULFSTREAM AMERICAN 2.20 LYCOMING 150 2680 MC CAULEY 73 73.3 -0.6 72.7 AA-SA O-320-E2G IC172/BTM7359 F LEICHIFLUG-TECHNIK 2.65 LYCOMING 197 HARTZELL 74 2 72.9 O.1 73.0 LFU-205 IO-360-AIC HC-C2YK-1B/F7666A-2 LET KONVICE 1.28 VK 50 HOFFMANN 51 2 $9.5 59.5 BLANIK-L-13M VW 1500-FR HO-11-130B-100D F MBB 1.39 CONTINENTAL 69 MCCAULY 69 2 66.9 66.9 BO-208 0-200-A 1A-100MCM-6950 F MBB 1.39 CONTINENTAL 99 MCCAULY 69 67.3 67.3 BO-208 0-200-A 1A-100MCM-6955 F MBB 1.39 CONTINENTAL 99 MCCAULY 67 67.5 +1.0 66.5 BO-208 0-200-A 1A-100MCM-6758 F MBB 1.81 LYCOMING 1 147 HARTZELL 76 2 70.7 - 1.6 69.1 BO-209 0-320-EIF HC-C2YL-1B/7663A-6 '
8/27/97
AIRCRAFT NOISE DATA FOR FOREIGN CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (ICAO ANNEX 16, CHAPTER 6)
MANUFACTURER MTOW MLW ENGINE DATA PROPELLER VITE ASTON MODEL 1000# MER, MODEL NO. SHE BPM EXH MEG, MODEL MBB 1.81 LYCOMING 157 HARTZELL 76 2 70.8 67.6 BO-209 1O-320-DIA HC-C2YL-1B/7663-SP MBB 1.81 LYCOMING 147 MCCAULY OL 2 70.6 60- L'69 BO-209-FF 0-320-E2F IC-172MGM70-5-66 F MB B 2.31 LYCOMING 197 HARTZELL 76 2 72.8 72.8 SIAT 223 10-360-CID6 HC-C2YK-IBF MORANE SAULNTER 1.87 CONTINENTAL 145 MCCAULY 76 71.3 -0.3 70.3 MS-885 0-300-A 1C-172MDM-7652 F MORAVAN CSSR 2.98 MORAVAN 168 AVIA-PRAHA 79 71.7 1.4 73.1 ZLIN 43 M337A V500 A MUDRY CAARP 1.83 LYCOMING 241 2700 HOFFMANN 71 67.0 67.0 CAP 10 10 360 B2F MO 29 HM 80170 PARTENAVIA 4.32 LYCOMING 2 200 2700 HARTZELL 72 79.6 -5.0 74.6 P 68 B I0-360-AIB6 HC-C2YK-2CF/FC7666A PILATUS BRITTEN 6.31 LYCOMING 2 300 2500 4 HARTZELL 80 80.7 -5.0 75.7 BN 2A-2 IO-540-K1B5 HC-C2YK-2CF/FC8477A PILATUS BRITTEN 9.50 LYCOMING 3 260 2500 6 HARTZELL 78 79.4 -2.0 77.4 BN-2A МКШ-2 0_540-EACS HC-C2YK-CUF/FC8477A PILATUS BRITTEN 9.50 LYCOMING 260 2500 6 HARTZELL 80 80.0 -2.0 78.0 BN-2A MKI-2 0-540-E4C5 HC-2CYK-2CUF/FC8477 PILATUS BRITTEN 10.01 LYCOMING 260 2500 6 HARTZELL 78 79.4 -0.9 78.5 BN-2A MKIII-3 O-540-E4CS HC-C2YK-2CUF/FC8477 PILATUS BRITTEN 10.01 LYCOMING 260 2500 6 HARTZELL 80 80.0 -0.9 79.1 BN-2A МКШ-3 0-540-E4CS HC-C2YK-2CUF/FC8477 PILATUS BRITTEN 6.31 LYCOMING 2 300 2500 4 HARTZELL 78 77.9 -5.0 72.9 BN-ZA-Z IO-540-KIB5 HC-C2YK 2CF/FC8477A Page 3
APPENDIX 9.
AIRCRAFT NOISE DATA FOR FOREIGN CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (ICAO ANNEX 16, CHAPTER 6) MANUFACTURER MTOW MLW ENGINE DATA PROPELLER DIASL BLADES NOISE LEVEL (dBA) MODEL 1000# MFR, MODEL NO. SHP REM EXH MFG,MODEL PITCH MDBA PC CORA NOTES PILATUS BRITTEN 6.59 LYCOMING 2 300 2500 4 HARTZELL 80 2 80.7 4.0 76.7 BN-2A-21 IO-540-K1B5 HC-C2YK-2CF/FC8477A PILATUS BRITTEN 6.59 LYCOMING 2 300 2500 4 HARTZELL 78 2 77.9 -4.0 73.9 BN-2A-21 IO-540-K1BS HC-C2YK-2CF/FC8477-6 PILATUS BRITTEN 6.30 LYCOMING 2 256 HARTZELL 79 82.3 - 3.7 78.6 BN-2A-6 0-540-E4CS HC-C2YK-2CF/FC8+77A PILATUS BRITTEN 6.59 ALLISON 2 320 4 HARTZELL 72.3 -4.1 68.2 BN-2T 250-B17C HC-C3YF-SF/FC8475FK- PILATUS-PORTER 4.85 AIRESEARCH 576 HARTZELL 102 74.6 - 5.0 69.6 PC-6C1-H2/PC-6T ТРЕ331-1-100 HC-B3TN-SC/T10178C/- v PIPER 2.16 LYCOMING 2700 SENSENICH 74 70.6 0.9 71.5 PA-28-150 O-320-E2A M74-DM-58 POLISH 2.87 PZI-FRANKLIN 2 260 2050 2 104 2 72.3 -3.8 68.5 PZL-104 2.87 AI-14R US 122 POLISH 2.87 PZI-FRANKLIN 2 260 2050 5 104 2 65.4 -3.8 61.6 PZL-104 W/ T-05 2.87 AI-14R US 122 POLISH 1.70 PZL-FRANKLIN 125 2050 2 70 2 67.0 2.8 69.8 PZL-110 1.70 4A. 235 B US 135 F REIMS AVIATION 1.68 LYCOMING 109 2550 MCCAULEY 69 2 65.7 -1.0 64.7 F 152 П C235 L2C IA 103/TCM 6958 F REIMS AVIATION 2.29 LYCOMING 150 2700 MCCAULEY 75 2 72.7 1.2 73.9 F 172 M C 320 E2D IC 16//DTM 7557 F REIMS AVIATION 2.29 LYCOMING 160 2700 MCCAULEY 75 2 73.4 -0.1 73.3 F 172 N C 320 H2AD IC 160/DTM 7557 F REIMS AVIATION 2.95 CONTINENTAL 230 2600 MCCAULEY 82 2 77.4 - 1.4 76.0 F 182 P 0 470 S 2A 34C 66 Page 4
APPENDIX 9
AIRCRAFT NOISE DATA FOR FOREIGN CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (ICAO ANNEX 16, CHAPTER 6) MANUFACTURER MTOW MLW ENGINE DATA PROPELLER DIAM BLADES NOISE LEVEL (dBA) MODEL 1000# MER MODEL NO. SHP RPM EXH MFG, MODEL PITCH MDBA PC CDBA NOTES REIMS AVIATION 2.95 CONTINENTAL. 230 2400 MCCAULEY 82 2 72.1 -2.4 69.7 F 182 Q 2.95 0470 U 2A 34C 204 v REIMS AVIATION 2.56 CONTINENTAL 195 2600 MCCAULEY 77 2 73.2 - 1.1 72.1 FR 172K 10 360 K 2A 34C 203 V REIMS AVIATION 3.09 LYCOMING 235 2400 MCCAULEY 82 2 73.1 -2.5 70.6 FR 182 0540J3CSD B2D 34C 214 ROBIN 1.98 LYCOMING 118 2700 MCCAULEY 71 68.2 2.4 70.6 DR 400/120A 1.98 0 235 L2A IA 135 DCM 7150 F ROBIN 2.31 LYCOMING 160 2700 SENSENICH 74 72.9 0.3 73.2 DR 400/160 2.31 0 320 D 74 DM 65264 ROBIN 2.43 LYCOMING 180 2600 SENSENICH 76 72.2 0.9 73.1 DR 400/180 2.43 0 360 А ЗА 76EM855-064 F ROBIN 2.20 LYCOMING 180 2700 SENSENICH 76 2 74.1 -2.5 71.6 DR 400/180R 2.20 0-360 A3A 76 EM 855058 F ROBIN 1.98 LYCOMING 116 2700 SENSENICH 72 2 69.6 2.0 71.6 DR400/120 1.98 0 235-L2A 72 CKS-6-056 F ROBIN 3.09 CONTINENTAL 285 4000 HOFFMANN 79 3 74.2 - 1.3 72.9 HR 100-285 3.09 TARA 6 285 B 2000TR/MN ROBIN 1.76 LYCOMING 112 2600 SENSENICH 72 2 67.3 0.2 67.5 R 2112 1.76 0 235 L2A 72 CK 56-056 F ROBIN 1.76 LYCOMING 160 2600 SENSENICH 72 2 72.4 -2.6 69.8 R 2160 1.76 0 320 D 74DM65 5264 F SAAB FAIRCHILD 4.41 LYCOMING 197 HARTZELL 74 2 73.8 0.7 74 5 MF1-15-200A 10-360-A1B6 HC-2CYK-4BF SCHEIBE FLUGZEUGBAU 1.34 LIMBACH 48 HOFFMANN 59 2 58.3 -10 57.3 SF-25C SL-1700-EA HO-11-150B-75L F Page 5
APPENDIX 9
AIRCRAFT NOISE DATA FOR FOREIGN CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (ICAO ANNEX 16, CHAPTER 6)
MANUFACTURER MTOW MLW ENGINE DATA PROPELLER DIAM BLADES VIP THAT ASION MODEL 1000# MER, MODEL NO. SHIP RPM EXH MEG, MODEL (IN) PITCH MDBA PC CDBA NOTES SCHEIBE FLUGZEUGBAU 0.85 HIRTH-MOT.BAU 28 HOFFMANN 47 2 67.7 0.2 67.9 SF-27 M-B 17IR-4E HO-02-120-50 F SCHEMPP-HIRTH 1.50 BINDER MOT. BAU 52 HOFFMANN 62 2 65.2 1.4 66.6 CM WB-2 HO-11 158B-70 F SCHEMPP-HIRTH 1 32 SCHEMPP-HIRTH SO ILOFFMANN 57 63.6 1.8 65.4 NIMBUS-2M SM-1 (O-28280F) HO-11 145-B80 F SHORT BROS. 12.57 AIRESEARCH 715 HARTZELL 98 81.9 -4.7 77.2 SKYVAN ТРЕ-331-2-201А HC-H3TN-SE/T10282HB V SLINGSBY ENGINEERING 1.65 LYCOMING 118 2800 2 HOFFMAN 20 2 70.9 •2.3 68.6 T 67A O-235-L2A HO14-178-120 F SOC. AERONAUT. 2.65 LYCOMING 177 SENSENICH 76 2 74.0 0.2 74.2 JODEL D 140B 0-360-AZA 76EM8-0-60 F SOCATA 1.70 LYCOMING 110 2600 MCCAULEY 69 2 67.6 1.0 68.6 110 ST 0-2351.-2A IA 103TCM 6958 F SOCATA 1.98 LYCOMING 160 2700 SENSENICH 74 2 73.8 -2.2 71.6 150 SV 0 326 D2A M 74 DM 61 SOCATA 2.09 LYCOMING 130 2700 SENSENICH 76 73.1 -0.8 72.3 180 T 2.09 0 360 АЗА 76 EM8 060 F SOCATA 2.65 LYCOMING 1 235 2575 HARTZELL 80 2 74.3 0.7 73.6 235 E 2.65 0 540 B4B5 HCC2 YK184684 SOCATA 1.70 ROLLS ROYCE 1 100 2750 MCCAULEY 67 2 68.8 68.8 880 B 1.70 0 200 A 1A 101 DCM/6948 SOCATA 2.31 LYCOMING 185 2700 HOFFMANN 73 2 71.3 71.3 893 E 2.31 0 360 АЗА HO 27 HM/186 135 SOCATA 2.29 LYCOMING 180 2700 HARTZELL 74 2 72.4 -0.9 71.5 TB 10 0-360-A1AD HC-C2YK-IBF-F7666-A2 Page 6
APPENDIX 9
AIRCRAFT NOISE DATA FOR FOREIGN CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (ICAO ANNEX 16, CHAPTER 6)
MANUFACTURER MTOW MLW ENGINE DATA PROPELLER DIAM BLADES MODEL 1000# MER, MODEL NO. SHP RPM EXH MFG, MODEL SALON SOCATA 2.34 LYCOMING 160 2700 SENSENICH 74 72.5 TB 9 0 320 D2A 74 DM6 61 F SPORTAVIA PUTZ. 1.54 CONTINENT AL 38 HOFFMANN 72 2 66.0 66.0 ELSTER B C90-12F HO-14-183 100 F SPORTAVIA PUTZ. 1.43 LIMBACH 71 HOFFMANN 59 63.4 - 1.3 62.1 RF-5 L.2100-EIX HO-VR/L-150A SPORTAVIA PUTZ. 1.98 LYCOMING 150 HOFFMANN 70 2 71.2 - 1.1 70.1 RF6-B 0-320-A1B HO-23 178-145 F SPORTAVIA PUTZ. 2.43 LYCOMING 180 HOFFMANN 70 66.3 -0.9 65.9 RS-180 0-360-A3A HO-27-HM-180138 F SPORTAVIA PUTZ. 2.45 LYCOMING 180 MCCAULY 75 73.8 73.8 RS-180 0.360-A3A 1A170/FFA7563 WASSMER 1.76 ROLLS ROYCE 134 2700 HOFFMANN 69 2 68.3 68.3 WA SO 0 200 A HO 14.175.113 ZAKLADY SZCYBOWCOWE 1.54 LIMBACH 1 59 HOFFMANN 57 68.9 0.3 69.2 SZD 45 SL-1700-EC HO-11-145 B75D Page 7 ......
08/27/97 AC36-1G Appendıx 9 Exhaust Configurations (Reciprocating Engines) Stub Pipes Small Collector, Short Exhaust Pipe 3 Turbine Or Turbocharger 4 Collector Wraparound Manifold Straight Pipe Manifold Muffler Page 8
APPENDIX 10 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED HELICOPTERS (14 CFR PART 36, APPENDIX H) MGW ENGINE DATA MAIN ROTOR TAIL BOTOR NOISE LEVEL (FPNdB)
MANUFACTURER MLW MODEL 1000M MER MODEL NO. MER MODEL BLADES DIA(ET) MER,MODEL BLADES DIA(FL) EQ STAGE NOTES AGUSTA 6.23 TURBOMECA 2 36.1 6.6 89.1 91.7 91.1 N A109K2 6.28 ARRIEL 1K1 BELL HELI TEXTRON 4.45 ALLISON BELL HELI TEXT 2 37.0 BELL, HELI TEXT 5.4 85.2 88.4 90.7 2061-4 4.45 250-C30P 206-015-001-107 206-016-201-127 BELL HELI TEXTRON 8.40 ALLISON BELL HELI TEXT 2 42.0 BELL HELI TEXT 6.8 90.5 89.1 94.2 2 230 FXD SKD GR 8.40 250-C30G/2 222-018-501-101 222-016-001-107 BELL HELI TEXTRON B.40 ALLISON BELL, HELI TEXT 2 42.0 BELL HELI TEXT 6.8 90.8 89.1 94.2 2 230 RIR WHL, GR 8.40 250-C30G/2 222-018-501-101 222-016-001-107 BELL HELI TEXTRON 11.90 PRATT&WHITNEY BELL, HELI TEXT 4 46.0 BELL HELI TEXT 2 8.6 93.4 92.8 95.6 2 412 HP 11.90 PTST-JE 412-015-300-109 212-010-750-105 BELL HELI TEXTRON 11.90 PRATT& WHITNEY BELL HELI TEXT 4 46.0 BELL HELI TEXT 2 8.6 93.4 93.2 95.6 412 SP 11.90 PT6T-3B 412-015-300-109 212-010-750-105 BELL HELI TEXTRON 11.90 PRATT&WHITNEY 2 BELL HELI TEXT 4 46.0 BELL HELI TEXT 2 8.6 93.4 92.8 95.6 2 412EP 11.90 PT6T-3D 412-015-300-109 212-010-750-105 BELL HELI TEXTRON 9.00 ALLISON 2 BELL HELI TEXT 42.0 BELL HELI TEXT 2 6.9 91.6 92.4 93.8 2 430 9.00 250-C40B 430-015-001-101 222-016-001-111 BOEING 3.35 ALLISON MCDONNELL DOUG 27.4 MCDONNELL DOUG 80.2 85.4 87.9 2 MD 520N 3.35 250-C20RJ2 369D21102-503 NOTAR EHI 31.50 GE 61.0 13.1 93.1 97.6 99.5 2 EH 101/300/500 31.50 CT7-6A EUROCOPTER 20.20 TURBOMECA 4 53.1 4 10.4 93.2 94.2 96.5 AS 3321.2 20.20 MAKILA 1A2 EUROCOPTER 4.96 TURBOMECA AEROSPATIALE 35.1 AEROSPATIALE 2 6.1 87.1 89.8 91.4 AS 350 B2 ARRIEL IDI 355A31.0001 355A12.0031 OR 0040 EUROCOPTER 4.63 TURBOMECA 35.1 2 6.1 86.8 91.1 91.3 2 AS 350BA 4.63 ARRIEL 1B EUROCOPTER 5.60 TURBOMECA EUROCOPTER 35.6 EUROCOPTER 2 6.2 86.2 88.8 92.9 2 AS 355 N 5.40 ARRIUS 1A/4M STARFLEX 355A340004- 350A33-0008-03/04 EUROCOPTER 5.29 ALLISON 35.1 2 6.1 87.6 89.0 03.8 AS 355F2R 5.29 250-C20F Page 1
APPENDIX 10 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED HELICOPTERS (14 CFR PART 36, APPENDIX H) MGW ENGINE DATA MAIN ROTOR TAIL, ROTOR NOISE LEVEL. (EPNdB) MANUFACTURER MODEL MLW 1000* MER, MODEL NO. MER.MODEL BLADES DIA(EL) MFR, MODEL BLADES DIA(FT.) TO AP STAGE NOTES EUROCOPTER 3.60 TURBOMECA 2 35.1 6.1 86.2 88.8 92.9 2 AS 355N 3.60 ARRIUS 3191M EUROCOPTER 9.37 TURBOMECA 2 39.2 3.6 91.0 93.3 96.1 2 AS 365N2 9.37 ARRIEL 1C2 EUROCOPTER 7.39 LYCOMING 2 4 36.1 2 6.4 90.8 90.0 96.0 2 BK 117B2 7.39 LTS-101-7500:
EUROCOPTER 7.39 TURBOMECA 2 4 36.1 2 6.4 89.7 90.6 96.0 BK 117C1 7.39 ARRIEL 1E2 SIKORSKY 10.80 TURBOMECA 2 SIKORSKY 4 44.0 SIKORSKY 8.O 92.8 92.5 95.6 2 S-76A STC: 568NE 10.80 ARRIEL, 1S 76150-9000/09100 76101-05101-041 SIKORSKY 11.70 TURBOMECA 2 SIKORSKY 4 44.0 SIKORSKY 8.0 93.2 96.0 97.7 S-76C 11.70 ARRIEL 151 76150-09199-41 76101-05501-041 SIKORSKY 11.70 TURBOMECA SIKORSKY 4 44.0 SIKORSKY 8.0 91.6 93.9 96.1 2 S-76C+ (PLUS) 11.70 ARRIEL 2S1 76150-09100-41 76101-05501-041 Page 2
AC36-1G 08/27/97 Appendix 10
EQUATIONS FOR THE CALCULATION OF NOISE CERTIFICATION LIMITS
AT TAKEOFE, SIDELINE, AND APPROACH STAGE 2 Takeoff Limits Flyover Limits Approach Limits (EPNdB) (EPNdB) (EPNdB) Up To And Including 1,764 1b. 89 88 90 W log - 1081,764 1081,764 Over 1,764 Ib. To 176,370 lb. 89 + 3.01 1,764 88 + 3.01 90 + 3.01 1og 2 log 2 log 2 Over 176,370 Ib. 109 108 110 Page 3
08/27/97 AC36-1G Appendix 10
NOISE CERTIFICATION REQUIREMENTS - HELICOPTERS
TAKEOFF 110 Stage 2 109 105 EPNL 10 100 1000 Takeoff Weight (1,000 Ibs) Page 4
AC36-1G 08/27/97 Appendix 10
NOISE CERTIFICATION REQUIREMENTS - HELICOPTERS
FLYOVER 115 110 Stage 2 108 105 10 100 1000 Takeoff Weight (1,000 1bs) Page 5