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The Brutsche Freedom 210 STOL was a proposed American STOL homebuilt aircraft that was designed by Neal H. Brutsche and intended to be produced by Brutsche Aircraft Corporation of Salt Lake City, Utah, introduced in the mid-1990s. The aircraft was planned to be supplied as a kit for amateur construction.〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition'', page 346. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1〕〔(【引用サイトリンク】title=American airplanes: Bo - Bu )〕 ==Design and development== The Freedom 210 STOL was to be a follow-on design to the single-seat Brutsche Freedom 40. It features a cantilever high-wing, a four-seat enclosed cabin, fixed conventional landing gear with wheel pants and a single engine in tractor configuration.〔〔 The aircraft was to be made from aluminum sheet. Its span wing was to mount almost full span Fowler flaps and feature a wing area of . The cabin width was to be , accessed via swing-up doors in width. The acceptable power range was to be and the standard engines used are the Lycoming O-360 or the fuel-injected Lycoming IO-360 powerplant. Kit options included a heater, upholstery, cargo tie-downs and floats.〔〔 The aircraft was to have 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 was to be .〔 The standard day, sea level, no wind, take off with a engine was to be and the landing roll is .〔 The manufacturer estimated the construction time from the supplied kit would be 1400 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「Brutsche Freedom 210 STOL」の詳細全文を読む スポンサード リンク
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