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Aviation History
2002
2002 - 0364.PDF
Directory: civil rotorcraft Model Main rotor MTOW Max payload Useful load Load (ext) Max speed diameter (m) (kg) (kg) (kg) (kg) (kt) 1 x 477kW P&WC PW207E. Uprated powerplant version. Upgrades available for PW206-powered machine MD500E 8 1,360 - 690 690 1 x 336kW R-R 250-C20-B/J/JN/F/W. 1 x 336kW R-R 250C20R MD530F 8 1,405 - 685 685 1 x 3l3kW R-R 250-C30 MD520N 8 1,519 - 800 800 1 x 447kW R-R 250-C20R. NOTAR tail MD600N 8 1,860 152 152 152 152 Max cruise (kt) 135 135 125 134 Range clean (km) 376 381 409 707 HIGE (ft) 8,500 16,000 9,000 11,100 HOGE («) 6,000 14,400 5,600 6,000 Max op ceiling (ft) 13,900 18,700 18,700 13,500 Max crew/ pax 1/5 1/5 1/5 1/6 125 159 115 138 113 648 800 420 9.836 5,772 15,747 4,918 1,179 907 1,179 1 x 447kW R-R 250-C47M. Stretch of MD520N. Yaw stability augmentation upgrade available MM (Moskovsky Vertolyotny Zavod/MIL Helicopter Plant), 2 Sokolnichyesky Val, Moscow, Russia Mi-17 21 13.000 4,000 - 5,000 2 x 1471kW Klimov TV3-117VM. Kazan builds Mi-172 version Mi-26TC 32 56,000 20,000 27,800 2 x 7450kW Lotarev D-136. 2 x 8382kW Ivchenko Progress ZMKB D-136 Mi-34C 10 1,450 550 1 x 243kW OKBM M-14V-26. Mil studying Turbomeca Arrius 2F powered Mi-34A version capable of carrying an addition passenger Mi-38 21 15.600 6,000 7,200 - 154 148 820 2 x 1603kW P&WC PW127. Collaboration with Mil & Eurocopter, Kazan continues prototype development/production. First flight scheduled for 1Q2002. Delivery in 2005 Mil/Ulan-Ude Aviation Plant Manufacturer (Moskovsky Vertolyotny Zavod/MIL Helicopter Plant), 2 Sokolnichyesky Val, Moscow, Russia MH-171A 21 13,000 4,000 - 4,000 125 115 610 9,836 2 x 1471kW Klimov TV3-117VM. Commercial export version of the Mi-8AMT, CIS type certificate. Collaboration between Eurocopter, Kazan and Mil Mitsubishi Heavy Industries Helicopter Dept, Aircraft & Special Vehicle HQ 5-1, Marunouchi 2-chome, Tokyo, Japan MH2000 12 4.500 1,920 2,000 1,600 150 135 2 x 653kW Mitsubishi MG5-110. Dual operating rotor speeds: 100% NR & 90% NR PZL-Swldnik Aleja Lotnikow Polskich 1, Swidnik, Poland www.pzl.swidnik.pl PZLSW-4 9 1,800 750 736 736 156 130 2 x 336kW R-R 250-C20-B/J/JN/F/W. 2 x 459kW PW200/9. Economy and high-performance versions under development. 780 900 11,803 4,921 16,404 9,185 17,060 5,772 15,747 8,860 5,800 15,000 11,483 9,514 19.685 2,550 2,100 141 131 235 PZLW-3ASokol 16 6,400 2,100 2 x 622kW PZL-Rzeszow PZL-10W FAR 129 cerified. Robinson Helicopter 2901 Airport Drive, Torrance, California, USA R22 Beta II 8 621 183 1 x 98kW Textron Lycoming 0-360-J2A R44 Raven 10 1,088 351 434 1 x 168kW Textron Lycoming 0-540-F1B5. Raven is skidded version, Clipper has floats S-58T Parts 2241 Statham Blvd, Oxnard, California, USA S-58T 17 5,900 2,460 1,417 1,417 2 x 1,342kW P&WC PT6T-3B. 2 x 1,398kW P&WC PT6T-6/6B. S-58 rebuild Schweizer Aircraft PO Box 147, New York, USA www.schweizer-aircraft.com 300C 8 930 - 431 1 x 142kW Textron Lycoming HIO-360-D1A 2 300CB 8 794 - 300 1 x 134kW Textron Lycoming HO-360-C1A 330SP 8 1,025 - 508 1 x 313kW R-R 250-C20W derated to 175kW 333 8 1,157 - 590 1 x 313kW R-R 250-C20W derated to 190kW Improved version of 330 with new dynamics and higher performance Sikorsky Aircraft 6900 Main Street S702A, PO Box 9729, Stratford, Connecticut, USA www.sikorsky.com S-76C+ 13 5,306 - 1,616 - 155 155 431 503 102 130 124 95 94 108 120 96 113 110 86 80 105 105 798 500 650 450 386 590 713 11.480 8,069 19.680 9,400 6,400 5,200 14,000 2,000 14,000 10,800 7.000 13,600 8,700 12,000 8,600 14,000 4,800 10,000 11.200 10,000 5,100 13,000 5.650 1,800 12,700 2 x 638kW Turbomeca Arriel-2S1. Block upgrade being planned for 2004 including new glass cockpit, uprated -S2S engine, redesigned tail rotor. Versions: SAR, EMS, VIP 165 151 996 10,700 6,370 15,000 130 130 110 110 99 745 465 666 20,000 20,000 9,000 12,400 20,000 16,400 20,000 12,000 9,400 14,100 3/26 1/3 2/32 3/26 1/4 2/12 1/1 1/3 2/16 1/2 1/3 1/3 2/13 S-92 17 11,861 11,475 4,400 4,536 2 x 1,877kW GE CT7-8. Certification end 2002 and first delivery to Cougar in August 2003. Tridair Helicopters 3000 Airway Avenue, Suite 300, Costa Mesa, California, USA www.tridair.com 206L-3ST Gemini ST 11 1,932 682 806 2 x 336kW R-R 250-C20R. Twin-engined conversion of Bell 206L-3 LongRanger 206L-4S Gemini ST 11 2,068 819 806 2 x 336kW R-R 250-C20R. Twin-engined conversion of Bell 206L-4 LongRanger Vertical Aviation Technologies 1609 Hangar Rd, Sanford Park, Florida, USA www.vertical-aviation.com Hummingbird 10 1,225 454 454 - 99 1 x 194kW Textron Lycoming VO-435. First re-engined helicopter due to fly shortly. Plans to build all new airframes. Based on Sikorsky S-52 Whisper Jet 2923 Carner Avenue, Sanford, Florida, USA www.whisper-jet.com S-55QT 12 3,500 - 1.548 2,500 - 90 557 1,200 1 x 775kW Honeywell TSE331-10. Five-blade ultra quiet version S-55T developed by Vertical Aviation and built by Whisper Jet. FAA certified and in service with Papillon Grand Canyon Helicopters. 2/22 2/6 1/3 2/9 48 5-11 FEBRUARY 2002 FLIGHT INTERNATIONAL www.fliqhtinternational.com
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