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