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The Paxman Viper is an Canadian homebuilt aircraft that was designed by Elbert Paxman and produced by Paxman's Northern Aircraft of Glenwood, Alberta, introduced in 1994. When it was available the aircraft was supplied as a kit for amateur construction.〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition'', page 218. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1〕 ==Design and development== The Viper was designed for the Canadian advanced ultralight category. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed conventional landing gear and a single engine in tractor configuration.〔 The aircraft airframe is made from wood, covered in doped aircraft fabric. Its span wing has a wing area of . The acceptable power range is and the standard engine used is a Suzuki automotive conversion powerplant.〔 The Viper 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, passenger 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 500 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「Paxman Viper」の詳細全文を読む スポンサード リンク
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