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The Frontier MD-II was an American homebuilt aircraft that was designed and produced by Frontier Aircraft Inc of Vail, Colorado, introduced in 1990s. When it was available the aircraft was supplied as a kit for amateur construction.〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition'', page 167. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1〕 ==Design and development== The MD-II featured a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit accessed via doors, fixed conventional landing gear with wheel pants and a single engine in tractor configuration.〔 The aircraft was fabricated from 2024-T3 aluminum sheet. Its span wing employed a USA 35B airfoil, mounted flaps and had a wing area of . The cabin width was . The acceptable power range was and the standard powerplant used was the Avia M 332 (LOM) four cylinder, inverted, air-cooled, supercharged, inline aircraft engine.〔 With the Avia engine the MD-II had a typical empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload for pilot, passenger and baggage was .〔 The manufacturer estimated the construction time from the supplied kit as 1500 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「Frontier MD-II」の詳細全文を読む スポンサード リンク
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