Noise Certification Limits for Appendix 3 AC 36-2C Propeller-Driven Aircraft Under 12,500 Ibs
100.
= 90 gP 82 80 70 68 60 0 165 495 990 1320 3300 3630
1. Airplane Type Certificate Applied For on or After October 10, 1973 2/12/06
2. Airplane Type Certificate Applied For on or After January 1, 1975, or application for a standard or restricted category airworthiness certificate
EQUATIONS FOR THE 2/12/86
CALCULATION OF NOISE CERTIFICATION LIMITS
FOR PROPELLER-DRIVEN AIRCRAFT UNDER 12,500 LBS Application for Type Certification on or After October 10, 1973:
LIMIT Up to and including 1,320 1bs 68 dB (A) Over 1,320 1bs up to and including to 3,630 1bs 68 + 1 dB for each 165 1b increment of I.O. weight above 1320 1bs.
Over 3,630 lbs up to and including 12,500 lbs 82 dB (A) Application for Type Certification on or After January 1, 1975 or application for a standard or restricted category airworthiness certificate after January 1, 1980.
Up to and including 1320 1bs. 68 dB (A) Over 1320 1bs. up to and including 3300 1bs. 68 + 1dB (A) 165 1b. for each Appendix AC 36-2C increment of T.O. weight above 1320 lbs.
Over 3300 1bs. up to and including 12500 1bs. 80 dB (A)
2/12/36
APPENDIX IV
MEASURED OR ESTIMATED NOISE LEVELS FROM UNCERTIFICATED AIRPLANES
CIVIL SUPERSONIC AIRCRAFT
ENGINES TAKEOFF SIDELINE APPROACH AIRFLANE MODEL NO . THRUST GR. WGT. M/EST. M/EST. M/EST.
1000 LBS. 1000 LBS. EPNDE EPNDE EPNDA
- . ... - - ... - I. - ... - - . - 4 38. 6 360.0 110.0 114.0 110,0 Appendix 4 AC 36-2C
APPENDIX
NO DATA SHEET FOR ROTARY WING AIRCRAFT VH VNE: ROTORS MAIN/TAII NOISE LEVELS E PNL 2/12/86
MANUFACCURER MTOW NUMBCE CNC COMMON NAME ENGINE MAKE FER КМН : KMH: DIAM NUM FLYOVER: T/O APP REFERENCE AND MODEL LES AND MODEL CNG KT ‹M › BL R PM 500FT APP 1 6 DEC AEROSFATIALE 1896 87 89.2 91 WC/B W/P 25 SQUIRREL 4180 : LYCOMING 86 AS 350 LYCOMING LTS 101 AEROSCATIALE 10995 1550 18 207 92 SUP/ FRELON 24243ITUREOMECA 00 990 SA 321 TURMO 3C AEROSVATIALE 1475 1570 207 92. 9 8 WG/B W/P 25 SUF / FRELON 25302 / TURBOMECA 990 SA 321F TURMO 3E6 AEROSFATIALE 5540 15 93
PUMA TURBOMECA SA 330 TURMO 4C AEROSPATIALE 7042 95 95 79-03 PUMA 15532 TURBOMECA SA 330J "URMO 4C AEROSPATIALE 800 92 89.5 79-03 GAZELLE 3968 URBOMECA SA 341G ASTAZOU ЗА AEROSPATIALE 1896 95 WG/B W/P 25
GAZELLE TURBOMECA ЗА 342 ASTAZOU AEROSPATIALE 2994: WG/B W/P 25 DAUPHIN 6601! TURBOMECA SA 360C I ASTAZOU 18A AEROSPATIALE 33931 8 9 94.0 WG/B W/P 25 DAUPHIN & 74811 TURBOMECA SA 365 ASTAZOU ARRIEL AEROSPATIALE 8488 98 (2) Appendix 5 AC 36-2C DAUPHIN-2 18716 TURBOMECA SA 365N ARRIEL 1C AGUSTA 2599: 96.0 5730 ALLISON A109 250-C208 BELL 1814 241 241 85 LONGRANGER 4000: ALLISON 130 150 206L 250-C20B
APPENDIX V NOISE DATA SHEET FOR ROTARY WING AIRCRAFT Appendix AC VY : VH VNE ROTORS MAIN/TAIL NOISE LEVELS EPNL 36-2C
MANUFAC TURER MTOW NUMBER ENG HP COMMON NAME ENGINE MAKE ER КМИ : KMH: 01 AM : NUM FLYOVER! TIO APP REFERENCE AND MODEL CBS AND MODEL ENG KT: KT MPH : (M ) DC 500ET АРР 16 DEG BELL 645 55 194: 185 94.6 95 FAA-EE-79-03 4 - 1 0500 PRATT WHITNEY 310 BEtt 1B92 280 90 ฿ 9 FAA-RD - 77-94 2950 AVCO- LYCOMING 420 435-G1A BELC 3560 575 451 87 98. FAA -EE- 7849 LYCOMING 1621 188 BELL 222 L510-6500- EOEING 20411 ~ 3750 97.0 97.0 102. MANUTACTURER 45006 LYCOMING VERTOL 234 T55 - L- 11C HUGHES 816 190: 3 82.0 - 2
LYCOMING 309C HIO-360-D1A HUGHES 03 A - 2
ALLISON 369А 163-A-5A HUGHES 400! 50! 03 85. 8 85. 87 FAA-EE-79-03 ISON 500C 250-C18A HUCHES 839 420 05 8 8 : ALLISON S00D 250-C20B MESSERSCEMITT 2300 70: 88.4 89. 91.7 FAA-EE-79-03 5071 ALLISON 30 30-105 250-C18 KIL 450 89 96.5 IWC/B W/P 25 ISOTOV 2 2/12/86 MI 2 GTO - 350P MIL 42500 5500 103. 107 . 8IWG/B W/P 25 93710 SOL 30 SA I D-25V/TV- 2BM M: L 1436 1700 21. : 97.6 100. 01WG/B W/P 25 ISOTOV 2 MI
ATTENDIX NOISE DATA SHEET FOR ROTARY WING 2/12/86
VY VH VNE/ROTORS MAIN/TA NOISE LEVELS E PNL MANUFACTURER MTOW NUMBER ENC НР
COMMON NAME KG ENGINE MAKE PER KMH KMI DI AM INUM FLYOVER TIO APP REFERENCE ANI! MODEL CBS AND MODEL ENG КТ : MPH ( M) OL RPM 500 ГТ APP DEG S! KORSKY 10000: 1400 267 92.6 95.9 H - 3 220491 CENERAL ELECTRIC S -61 IT58-GE-10 SIKORSKY 19459 4800 22. 97.0 99.0 1WG /B W/P 25 42907: PRATT WHITNEY S-64 JFTD12-5A SIKORSKY H-53 16775 36988: GENERAL ELÉCTRIC 3780 76 196 170 97. 95 99.9 FAA-EE-79-03 5 - 65 T64 SIKORSKY 4545: 650 293 8 9 95. AA-EE-81-16 (1) 10021: ALLISON 146: 178 S -17 6r 250-C30 SIKORSKY 9185 89 96.7 IAEE-80-16 BLACKHAWK 20250 I GENERAL ELECTRIC 165: 224 35 UH- 60A T700-GE-700 WESTLAND 5600 120 IMANUFACTURER W-30 12347: ROLLS ROYCE 138 W30+100 : R.R GEM41 - 1 MK510 :
REFERENCES
(1) Data calculated from this report.
(2) Jata not corrected to standard reference day nor corrected to eference flight path (as measured data).
A-2 Advisory Circular 36-2 Dated 2/6/78 Appendix 5 AC 36-2C WC/B W/P 25 ICAO WorkingGroup 12/14/78
Helicopters at Takeoff, Approach and Flyover ICAO Noise Certification Limits for Appendix 5 AC 36-2C 110 100 INdE 2/12/86 100 1000 1737 10,000 100.000 176,370 1,000,000 Weight
*U.S. G.P.0.:1993-301-717:80364 2/12/86
EQUATIONS FOR THE CALCULATION OF
ICAO HELICOPTER NOISE STANDARDS
AT TAKEOFF, APPROACH, AND FLYOVER Takeoff Limits Approach Limits Flyover Limits EPNdB EPNdR EPNdB Up to and including 1,737 1bs 86 87 85 Over 1,737 1bs to 176,370 1bs 83.61+9.97 1og M 84.61+9.97 10g M 82.61+9.97 1og M Over 176,370 1bs 106 107 105 M = Maximum Takeoff Mass in 1000 1bs Appendix 5 AC 36-2C