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The DTA Voyageur is a French ultralight trike, designed by Jean-Michel Dizier and produced by DTA sarl of Montélimar. The aircraft is supplied complete and ready-to-fly.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 210. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕〔Bertrand, Noel; Rene Coulon; et al: ''World Directory of Leisure Aviation 2003-04'', page 99. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X〕 ==Design and development== The aircraft was initially designed as an agricultural aircraft to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of . The Voyageur is intended as a bush aircraft for flying from unprepared surfaces and as such mounts heavy duty landing gear, tundra tires and lacks a cockpit fairing and a front wing strut.〔〔 The Voyageur has a maximum gross weight of , depending on the wing fitted. It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit, tricycle landing gear without wheel pants and a single engine in pusher configuration.〔〔 The aircraft is made from bolted-together aluminum tubing, with its double surface wing covered in Dacron sailcloth. When fitted with a DTA Dynamic 450 wing it has a span of , supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. The powerplant is a twin cylinder, liquid-cooled, two-stroke, dual-ignition Rotax 582 engine or the four cylinder, air and liquid-cooled, four-stroke, dual-ignition Rotax 912S engine.〔〔 A number of different wings can be fitted to the basic carriage, including the DTA Dynamic 450, the DTA Dynamic 15/430 DTA Magic and DTA Diva.〔〔 The Voyageur II model is accepted as a light-sport aircraft in the United States.〔 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「DTA Voyageur」の詳細全文を読む スポンサード リンク
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