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Aviation History
1999
1999 - 1953.PDF
J'JJJL J 'ffi Si / Si U fUSi a Si A P Manufacturer Powerplant HIMrcttpter France AS532SC Cougar MM 2 x l,357kW Turbomeca Makila 1A1 GKN Westland Helicopters Sea King Super Lynx Kama SH-2G Super Seasprite Kamov Ka-27/Ka-28 Mil MU4 Haze Sikorsky SH-60B Seahawk Kawasaki Heavy Industries XOH-1 Bell Helicopter Textron 0H-58D Kiowa Warrior I SPECIAL FORCES Boeing Helicopters MH47E Special Operations Kamov Ka-29 Sikorsky HH/MH-60G Pave Hawk MH-60K Black Hawk I TRAINING Bell Helicopter Textron TH67 Creek Enstrom Helicopter 280FX Shark TH28 480 Mil Mi-34 I TRANSPORT Bell/Boeing CV-22 Osprey Boeing Helicopters CH47D Chinook CH47F Chinook CH47SD International Chinook Mil Mi-26A Sikorsky Aircraft CH-53E Super Stallion UlarHJde Aviation Plant/Mil r*8AMTsh Bell Helicopter Textron Bell 412EP UH-1HP Huey II UH-1Y 2 x l,238kW Rolls-Royce Gnome H1400-1T 2 x l,208kW LHTEC CTS8004N turboshaft 2 x 835kW Rolls-Royce Gem 42-1 turboshaft 2 x 1.260kW GE T70CK3E401 turboshaft 2 x l,636kW Klimov TV3-117 turboshaft 2 x 1.268kW Klimov TV3-117 turboshaft 2 x l,342kW GE T70CK3E401C turboshaft 2 x595kW Mitsubishi MG5 turboshaft 1 x 485kW Allison T703-AD-700 Turboshaft 2 x 3,629kW AlliedSignal T55 L-714A 2 x l,660kW Klimov TV3-117 turboshaft 2 x l,370kW GET70CM5E-701C turboshaft 2 x l,445kW GET70OCE-701C turboshaft 1 x 313kW Allison 25OC20J turboshaft 1 x 336kW Allison 25OC20R/4 turboshaft 1 x 170kW Textron Lycoming Turbo HI0-360-RLAD piston 1 x 313kW Allison 250C20W turboshaft 1 x 313kW Allison 25OC20W turboshaft 1 x 243kW OKBM M-14V-26 piston 2 x 4,586kW R-R AE1107C turboshaft 2 x 2,796kW Textron LycomingT55-L-L712 turboshaft 2 x 3,529kW AlliedSignal T55-L-714A turboshaft 2 x 3,529kW AlliedSignal T55 L-712A/714A turboshaft 2 x 8,493kWProgress ZMKB D-136 turboshaft 3 X 2,605kW GE T64GE-10J turboprop 2 x l,397kW Klimov TV3-117 turboshaft 1 x l,342kW Pratt & Whitney Canada PT6T Twin Pac 3D turboshaft 1 x l,342kW AlliedSignal T53-L-703 2 x l,957kW GE T700-GE-701C turboshaft :uselage length (m) Overall length (m) 15.53 18.70 17.20 22.15 13.33 15.24 12.25 16.08 11.30 18.40 25.32 15.25 19.76 12.00 10.50 12.85 15.88 30.14 11.30 12.30 15.30 19.76 15.30 19.76 9.50 11.82 8.70 8.90 9.10 9.30 9.10 9.30 8.85 11.40 17.48 17.48 15.55 30.14 15.88 30.14 15.88 30.14 33.73 40.00 22.35 30.20 18.30 25.30 12.90 17.07 12.80 17.62 12.80 17.62 Fuselage height (m) Main rotor diam (m) 4.92 15.60 5.13 18.90 3.67 12.80 4.58 13.41 5.40 15.90 6.93 21.30 3.79 16.36 3.80 11.50 3.93 10.60 5.59 18.29 5.40 15.90 5.13 16.40 5.13 16.40 2.90 10.20 2.70 9.80 2.90 9.80 2.90 9.80 2.75 10.00 5.38 11.60 5.78 18.29 5.78 18.29 5.78 18.29 8.15 32.00 8.90 24.08 5.65 21.30 3.30 14.00 3.60 14.63 3.60 14.63 MTOW (kg) OEW(kg) 9,000 4,558 - 9,707 5,447 5,330 3,656 6,124 4,017 12,600 14,000 8,900 9,500 6,190 3,500 2,500 2,497 1,497 24,494 12,210 11,500 5,520 11,085 6,560 11,085 5,580 1,520 772 1,180 719 1,293 760 1,293 760 1,450 950 21,565 15,032 22,680 10,615 24,494 11,549 24,494 11.549 56,000 28,600 33,340 15,072 11,100 7,055 5,397 3,100 4,762 2,449 8,391 5,158 Max internal load (kg) Max external load (kg) 4,442 4,500 3,692 4,260 1,674 1,360 2,110 990 5,000 5,100 3,300 2,722 n/a 1,000 998 998 12,284 11,794 5,000 4,000 4,525 4,070 4,525 4,070 750 750 460 460 533 533 533 533 500 0 12,285 10,340 12,943 12,700 12,943 12,700 20,000 20,000 13,610 14,515 4,000 4,000 2,296 2,296 3,213 3,213 Max op ceiling (ftl 16,995 10,000 12,000 20,400 17,100 11,500 14,300 12,000 10,150 14,098 19,000 14,200 ' 13,500 12,000 13,000 13,000 9,840 26,000 11,000 11,100 11,100 11,800 18,500 15,485 13,100 16,100 44 FLIGHT INTERNATIONAL 30 June - 6 July 1999
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