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The Washington T-411 Wolverine is an American homebuilt aircraft that was produced by Washington Aeroprogress of Seattle, Washington, introduced in the 1990s. When it was available the aircraft was supplied as a kit or in the form of plans for amateur construction.〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition'', page 294. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1〕 ==Design and development== Developed from the Russian Khrunichev T-411 Aist, the T-411 Wolverine features a strut-braced high-wing, a five seat enclosed cabin with doors, fixed conventional landing gear with wheel pants and a single engine in tractor configuration.〔 Like its Russian predecessor the T-411 Wolverine was designed for operations from unprepared surfaces.〔 The aircraft is made from a mix of steel and aluminum, covered in doped aircraft fabric. Its span wing is supported by "V" struts and jury struts and has a wing area of . The cabin width is . The acceptable power range is and the standard engines used are the Vedeneyev M14P radial engine, the Continental IO-550 and the Lycoming O-540 horizontally opposed powerplants. The aircraft includes provisions for floats and skis.〔 The T-411 Wolverine has a typical empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload for the pilot, passengers and baggage is .〔 The standard day, sea level, no wind, take off with a engine is and the landing roll is .〔 The manufacturer estimated the construction time from the supplied kit as 1000 hours.〔 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「Washington T-411 Wolverine」の詳細全文を読む スポンサード リンク
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