APPENDIX 9 MODEL
MANUFACTURER ROBIN DR 400/160 MTOW MLW 1000#
2.31
2.31
MFR, MODEL
ENGINE DATA SHPNO.
AIRCRAFT NOISE DATA FOR FOREIGN CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (ICAO ANNEX 16, CHAPTER 6)
RPM MFG, MODEL
PROPELLER BLADESDIAM (IN) PITCHEXH LYCOMING 1 160 2700 SENSENICH 74 DM 65264 74 2 F0 320 D
MDBA PC CDBA NOISE LEVEL (dBA)
72.9 0.3 73.2 NOTES ROBIN DR 400/180
2.43
2.43
LYCOMING 0 360 A 3A 1 180 2600 SENSENICH 76EM855-064 76 2 F
72.2 0.9 73.1 ROBIN DR 400/180R
2.20
2.20
LYCOMING 0-360 A3A 1 180 2700 SENSENICH 76 EM 855058 76 2 F
74.1 -2.5 71.6 ROBIN DR400/120
1.98
1.98
LYCOMING 0 235-L2A 1 116 2700 SENSENICH 72 CKS-6-056 72 2 F
69.6 2.0 71.6 ROBIN HR 100-285
3.09
3.09
CONTINENTAL TIARA 6 285 B 1 285 4000 HOFFMANN 2000TR/MN 79 3 V
74.2 -1.3 72.9 ROBIN R 2112
1.76
1.76
LYCOMING 0 235 L2A 1 112 2600 SENSENICH 72 CK 56-056 72 2 F
67.3 0.2 67.5 ROBIN R 2160
1.76
1.76
LYCOMING 0 320 D 1 160 2600 SENSENICH 74DM65 5264 72 2 F
72.4 -2.6 69.8
SAAB FAIRCHILD MFI-15-200A
4.41 LYCOMING IO-360-A1B6 1 197 HARTZELL HC-2CYK-4BF 74 2 V
73.8 0.7 74.5
SCHEIBE FLUGZEUGBAU SF-25C
1.34 LIMBACH SL-1700-EA 1 48 HOFFMANN HO-11-150B-75L 59 2 F
58.3 -1.0 57.3
SCHEIBE FLUGZEUGBAU SF-27 M-B
0.85 HIRTH-MOT.BAU 171R-4E 1 28 HOFFMANN HO-02-120-50 47 2 F
67.7 0.2 67.9
SCHEMPP-HIRTH CM
1.50 BINDER MOT.BAU WB-2 1 52 HOFFMANN HO-11 158B-70 62 2 F
65.2 1.4 66.6
SCHEMPP-HIRTH NIMBUS-2M
1.32 SCHEMPP-HIRTH SM-1 (O-28280R) 1 50 HOFFMANN HO-11 145-B80 57 2 F
63.6 1.8 65.4 SHORT BROS.
SKYVAN
12.57 AIRESEARCH TPE-331-2-201A 2 715 HARTZELL HC-B3TN-SE/T10282HB 98 3 V
81.9 -4.7 77.2
SLINGSBY ENGINEERING T 67A
1.65 LYCOMING O-235-L2A 1 118 2800 2 HOFFMAN HO14-178-120 70 2 F
70.9 -2.3 68.6 Page 5
APPENDIX 9 MODEL
MANUFACTURER SOC.AERONAUT.
JODEL D 140B MTOW MLW 1000#
2.65
MFR, MODEL
ENGINE DATA SHPNO.
AIRCRAFT NOISE DATA FOR FOREIGN CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (ICAO ANNEX 16, CHAPTER 6)
RPM MFG, MODEL
PROPELLER BLADESDIAM (IN) PITCHEXH LYCOMING 1 177 SENSENICH 76EM8-0-60 76 2 F0-360-A2A
MDBA PC CDBA NOISE LEVEL (dBA)
74.0 0.2 74.2 NOTES SOCATA 110 ST
1.70 LYCOMING 0-235L-2A 1 110 2600 MCCAULEY 1A 103TCM 6958 69 2 F
67.6 1.0 68.6 SOCATA 150 SV
1.98 LYCOMING 0 326 D2A 1 160 2700 SENSENICH M 74 DM 61 74 2 F
73.8 -2.2 71.6 SOCATA 180 T
2.09
2.09
LYCOMING 0 360 A3A 1 180 2700 SENSENICH 76 EM8 060 76 2 F
73.1 -0.8 72.3 SOCATA 235 E
2.65
2.65
LYCOMING 0 540 B4B5 1 235 2575 HARTZELL HCC2 YK184684 80 2 V
74.3 -0.7 73.6 SOCATA 880 B
1.70
1.70
ROLLS ROYCE 0 200 A 1 100 2750 MCCAULEY 1A 101 DCM/6948 67 2 F
68.8 68.8 SOCATA 893 E
2.31
2.31
LYCOMING 0 360 A3A 1 185 2700 HOFFMANN HO 27 HM/186 135 73 2 F
71.3 71.3 SOCATA TB 10
2.29 LYCOMING 0-360-A1AD 1 180 2700 HARTZELL HC-C2YK-1BF-F7666-A 74 2 V
72.4 -0.9 71.5 SOCATA TB 9
2.34 LYCOMING 0 320 D2A 1 160 2700 SENSENICH 74 DM6 61 74 2 F
71.2 1.3 72.5 SPORTAVIA PUTZ.
ELSTER B
1.54 CONTINENTAL C90-12F 1 88 HOFFMANN HO-14-183 100 72 2 F
66.0 66.0 SPORTAVIA PUTZ.
RF-5
1.43 LIMBACH L2100-EIX 1 71 HOFFMANN HO-VR/L-150A 59 2 V
63.4 -1.3 62.1 SPORTAVIA PUTZ.
RF6-B
1.98 LYCOMING 0-320-A1B 1 150 HOFFMANN HO-23 178-145 70 2 F
71.2 -1.1 70.1 SPORTAVIA PUTZ.
RS-180
2.45 LYCOMING 0-360-A3A 1 180 MCCAULY 1A170/FFA7563 75 2 F
73.8 73.8 SPORTAVIA PUTZ.
RS-180
2.43 LYCOMING 0-360-A3A 1 180 HOFFMANN HO-27-HM-180138 70 2 F
66.8 -0.9 65.9 Page 6
APPENDIX 9 MODEL
MANUFACTURER
WASSMER WA 80 MTOW MLW 1000#
1.76
MFR, MODEL
ENGINE DATA SHPNO.
AIRCRAFT NOISE DATA FOR FOREIGN CERTIFICATED PROPELLER DRIVEN SMALL AIRPLANES (ICAO ANNEX 16, CHAPTER 6)
RPM MFG, MODEL
PROPELLER BLADESDIAM (IN) PITCHEXH ROLLS ROYCE 1 134 2700 HOFFMANN HO 14.175.113 69 2 F0 200 A
MDBA PC CDBA NOISE LEVEL (dBA)
68.3 68.3 NOTES
ZAKLADY SZCYBOWCOWE SZD 45
1.54 LIMBACH SL-1700-EC 1 59 HOFFMANN HO-11-145 B75D 57 2 F
68.9 0.3 69.2 Page 7
11/15/01 AC36-1H Appendix 9 Exhaust Configurations (Reciprocating Engines) 1 Stub Pipes 2 Small Collector, Short Exhaust Pipe 3 Turbine Or Turbocharger 4 Collector Wraparound Manifold Straight Pipe 5 Manifold Muffler Page 8
APPENDIX 10 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED HELICOPTERS (14 CFR PART 36, APPENDIX H) MODEL
MANUFACTURER MGW MLW 1000# MFR, MODEL
ENGINE DATA NO.
MAIN ROTOR MFR, MODEL BLADES DIA(FT.)
TAIL ROTOR MFR, MODEL BLADES DIA(FT.) FO TO AP STAGE NOTES NOISE LEVEL (EPNdB) AGUSTA 6.28 PRATT&WHITNEY 2 AGUSTA 4 36.00 AGUSTA 2 6.60 90.8 91.4 91.4 2 A109E 6.28 206C AGUSTA 6.28 TURBOMECA 2 AGUSTA 4 36.00 AGUSTA 2 6.60 90.9 91.8 93.3 2 A109E 6.28 ARRIUS 2K1 AGUSTA 6.28 TURBOMECA 2 AGUSTA 4 36.00 AGUSTA 2 6.60 89.1 91.7 91.1 2 A109K2 6.28 ARRIEL 1K1 BELL HELI TEXTRON 4.45 ALLISON 1 BELL HELI TEXT 2 37.00 BELL HELI TEXT 2 5.40 85.2 88.4 90.7 2 206L-4 4.45 250-C30P 206-015-001-107 206-016-201-127 BELL HELI TEXTRON 8.40 ALLISON 2 BELL HELI TEXT 2 42.00 BELL HELI TEXT 2 6.83 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 8.40 ALLISON 2 BELL HELI TEXT 2 42.00 BELL HELI TEXT 2 6.83 90.8 89.1 94.2 2 230 RTR WHL GR 8.40 250-C30G/2 222-018-501-101 222-016-001-107 BELL HELI TEXTRON 11.90 PRATT&WHITNEY 2 BELL HELI TEXT 4 46.00 BELL HELI TEXT 2 8.60 93.4 92.8 95.6 2 412 HP 11.90 PT6T-3E 412-015-300-109 212-010-750-105 BELL HELI TEXTRON 11.90 PRATT&WHITNEY 2 BELL HELI TEXT 4 46.00 BELL HELI TEXT 2 8.60 93.4 93.2 95.6 2 412 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 46.00 BELL HELI TEXT 2 8.60 93.4 92.8 95.6 2 412EP 11.90 PT6T-3D 412-015-300-109 212-010-750-105 BELL HELI TEXTRON 6.00 PRATT&WHITNEY 2 BELL HELI TEXT 4 37.00 BELL HELI TEXT 2 5.67 89.1 88.0 91.2 2 427 6.00 PW207D 427-015-001-125 427-016-001-109 BELL HELI TEXTRON 6.35 PRATT&WHITNEY 2 BELL HELI TEXT 4 37.00 BELL HELI TEXT 2 5.67 89.0 88.5 91.2 2 427 6.35 PW207D 427-015-001-125 427-016-001-109 BELL HELI TEXTRON 9.00 ALLISON 2 BELL HELI TEXT 4 42.00 BELL HELI TEXT 2 6.90 91.6 92.4 93.8 2 430 9.00 250-C40B 430-015-001-101 222-016-001-111 BOEING 3.35 ALLISON 1 MCDONNELL DOUG 5 27.35 MCDONNELL DOUG 80.2 85.4 87.9 2 MD 520N 3.35 250-C20R/2 369D21102-503 NOTAR EHI 31.50 GE 3 5 61.00 4 13.10 93.1 97.6 99.5 2 EH 101/300/500 31.50 CT7-6A EUROCOPTER 20.20 TURBOMECA 2 4 53.10 4 10.40 93.2 94.2 96.5 2 AS 332L2 20.20 MAKILA 1A2 Page 1
APPENDIX 10 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED HELICOPTERS (14 CFR PART 36, APPENDIX H) MODEL
MANUFACTURER MGW MLW 1000# MFR, MODEL
ENGINE DATA NO.
MAIN ROTOR DIA(FT.)MFR, MODEL BLADES
TAIL ROTOR MFR, MODEL BLADES DIA(FT.) FO TO NOTES NOISE LEVEL (EPNdB)
STAGEAP EUROCOPTER 4.96 TURBOMECA 1 AEROSPATIALE 3 35.07 AEROSPATIALE 2 6.10 87.1 89.8 91.4 2 AS 350 B2 ARRIEL 1D1 355A31.0001 355A12.0031 OR 0040 EUROCOPTER 4.63 TURBOMECA 1 3 35.10 2 6.10 86.8 91.1 91.3 2 AS 350BA 4.63 ARRIEL 1B EUROCOPTER 5.60 TURBOMECA 2 EUROCOPTER 3 35.60 EUROCOPTER 2 6.20 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 2 3 35.10 2 6.10 87.6 89.0 93.8 2 AS 355F2R 5.29 250-C20F EUROCOPTER 5.60 TURBOMECA 2 3 35.10 2 6.10 86.2 88.8 92.9 2 AS 355N 5.60 ARRIUS 3191M EUROCOPTER 9.37 TURBOMECA 2 4 39.20 11 3.60 91.0 93.3 96.1 2 AS 365N2 9.37 ARRIEL 1C2 EUROCOPTER 7.39 LYCOMING 2 4 36.10 2 6.40 90.8 90.0 96.0 2 BK 117B2 7.39 LTS-101-750B1 EUROCOPTER 7.39 TURBOMECA 2 4 36.10 2 6.40 89.7 90.6 96.0 2 BK 117C1 7.39 ARRIEL 1E2 SIKORSKY 10.80 TURBOMECA 2 SIKORSKY 4 44.00 SIKORSKY 4 8.00 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 44.00 SIKORSKY 4 8.00 93.2 96.0 97.7 2 S-76C 11.70 ARRIEL 1S1 76150-09199-41 76101-05501-041 SIKORSKY 11.70 TURBOMECA 2 SIKORSKY 4 44.00 SIKORSKY 4 8.00 91.6 93.9 96.1 2 S-76C+ (PLUS) 11.70 ARRIEL 2S1 76150-09100-41 76101-05501-041 Page 2
11/15/01 AC36-1H Appendix 10
EQUATIONS FOR THE CALCULATION OF NOISE CERTIFICATION LIMITS
AT TAKEOFF, SIDELINE, AND APPROACH STAGE 2 Takeoff Limits Flyover Limits Approach Limits (EPNdB) (EPNdB) (EPNdB) Up to and including 1,764 pounds 89 88 90 W W Wlog log log1 764 89 + 301 , 88 + 3 01.. {{{{{{ 1 764 ,
log 2 1 764 ,
log 2 { { {{ { { 3 01 {{ . {{ { { Between 1,764 pounds and 176,370 pounds 90 + log 2 { { { { { { 176,370 pounds or more 109 108 110 Page 3
11/15/01 AC36-1H
Appendix 10
NOISE CERTIFICATION REQUIREMENTS - HELICOPTERS
TAKEOFF 109 85 90 95 100 105 110 115 EPNL Stage 2 89 1 10 100 1000
Takeoff Weight (1,000 lbs) Page 4
11/15/01 AC36-1H
Appendix 10
NOISE CERTIFICATION REQUIREMENTS - HELICOPTERS
SIDELINE 108 85 90 95 100 105 110 115 EPNL 88 Stage 2 1 10 100 1000
Takeoff Weight (1,000 lbs) Page 5
11/15/01 AC36-1H
Appendix 10
NOISE CERTIFICATION REQUIREMENTS - HELICOPTERS
APPROACH 110 85 90 95 100 105 110 115 EPNL Stage 2 1 10 100 1000
Takeoff Weight (1,000 lbs) Page 6
APPENDIX 11 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED HELICOPTERS (14 CFR PART 36, APPENDIX J)
MANUFACTURER MGW MLW
ENGINE DATA MAIN ROTOR TAIL ROTOR NOISE LEVEL (SEL) MODEL 1000# MFR, MODEL NO. MFR, MODEL BLADES DIA(FT.) MFR, MODEL BLADES DIA(FT.) FO STAGE NOTES AGUSTA 6.00 PRATT & WHITNEY 1 AGUSTA 4 35.50 AGUSTA 2 6.60 85.9 2 A119 6.00 PT6B-37 BELL HELI TEXTRON 4.55 ALLISON 2 BELL HELI TEXT 2 37.00 BELL HELI TEXT 2 5.40 85.2 2 206L-4 w/STC00036SE 4.55 250-C20R 206-015-001-107 206-016-201-127 BELL HELI TEXTRON 5.00 ALLISON 1 BELL HELI TEXT 4 35.00 BELL HELI TEXT 2 5.40 85.1 2 407 5.00 250-C47B 407-015-001-101 406-016-100-101 BOEING 4.10 ALLISON 1 6 27.50 13 79.0 2 MD 600N 250-C47 BOEING 6.00 PRATT & WHITNEY 2 MCDONNELL DOUGLA 5 33.85 MCDONNELL DOUGLA 13 1.83 82.1 2 MD 900 6.00 PW206A NOTAR ENSTROM 2.60 LYCOMING 1 ENSTROM 3 32.00 ENSTROM 2 4.70 79.0 2 280FX/F-28F 2.60 H10-360-F1AD 28-14003-6 28-150079-5 ENSTROM 2.85 ALLISON 1 ENSTROM 3 32.00 ENSTROM 2 5.00 83.6 2 6 480 2.85 250-C20W 4143000-3 28-150079-7 ENSTROM 3.00 ALLISON 1 ENSTROM 3 32.00 ENSTROM 2 5.00 83.7 2 480B 3.00 250-C20W 4143000-3 28-150079-7 ENSTROM 2.85 ALLISON 1 ENSTROM 3 32.00 ENSTROM 2 5.00 82.4 2 TH28/480 2.85 250-C20W 4143000-1 28-150073-3 EUROCOPTER 3.70 PRATT & WHITNEY 1 4 32.80 8 78.7 2 EC 120 PT6B-37 EUROCOPTER 5.80 PRATT & WHITNEY 2 4 33.50 81.6 2 EC135P PW206B EUROCOPTER 5.80 TURBOMECA 2 4 33.50 80.2 2 EC135T ARRIUS 2B KAMAN 6.00 TEXTRON LYCOMING 1 KAMAN 2 48.20 82.5 2 4 K-1200 6.00 T5317A-1 K-1200(2)2 Rotors ROBINSON 2.40 LYCOMING 1 ROBINSON 2 33.00 ROBINSON 2 4.83 81.9 2 R44 2.40 O-540-F1B5 C016-2 C029-1 SCHWEIZER 2.05 LYCOMING 1 SCHWEIZER 3 26.83 SCHWEIZER 2 4.25 78.8 2 1 269C 2.05 IO-360-D1A 269A1002 269A6034-19 Page 1
APPENDIX 11 AIRCRAFT NOISE DATA FOR U.S. CERTIFICATED HELICOPTERS (14 CFR PART 36, APPENDIX J)
MANUFACTURER MGW MLW
ENGINE DATA MAIN ROTOR TAIL ROTOR NOISE LEVEL (SEL) MODEL 1000# MFR, MODEL NO. MFR, MODEL BLADES DIA(FT.) MFR, MODEL BLADES DIA(FT.) FO STAGE NOTES SCHWEIZER 2.05 LYCOMING 1 SCHWEIZER 3 26.83 SCHWEIZER 2 4.25 81.1 2 2 269C 2.05 IO-360-D1A 269A1002 269A6034-19 SCHWEIZER 2.05 LYCOMING 1 SCHWEIZER 3 26.83 SCHWEIZER 2 4.25 79.2 2 3 269C 2.05 IO-360-D1A 269A1002 269A6034-19 SCHWEIZER 1.75 LYCOMING 1 SCHWEIZER 3 26.83 SCHWEIZER 2 4.25 81.8 2 5 269C-1 1.75 O-360-C1A 269A1002 269A6034-19 SCHWEIZER 2.26 ALLISON 1 SCHWEIZER 3 27.26 SCHWEIZER 2 4.25 80.6 2 269D (330SP) 2.26 250-C20W 269A1002-11 269A6034-29 SCHWEIZER 2.55 ALLISON 1 SCHWEIZER 3 27.51 SCHWEIZER 2 4.25 81.5 2 269D Configuration A 2.55 250-C20W 269A1002-13 269A6034-29 SCHWEIZER 2.20 ALLISON 1 SCHWEIZER 3 26.83 SCHWEIZER 2 4.25 79.4 2 269D/330 2.20 250-220W 269 A 1002 269 A 6034-19 SCHWEIZER 2.05 LYCOMING 1 3 26.80 2 4.30 78.8 2 1 300C(1) H10-360-DIA SCHWEIZER 2.05 LYCOMING 1 3 26.80 2 4.30 81.1 2 2 300C(2) H10-360-DIA SCHWEIZER 2.05 LYCOMING 1 3 26.80 2 4.30 79.2 2 3 300C(3) H10-360-DIA Page 2