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The Aircraft Technologies Acro 1 is an American aerobatic homebuilt aircraft that was designed by Fred Meyer and produced by Aircraft Technologies of Lilburn, Georgia. 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 109. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1〕 Neither plans nor kits are available anymore and the aircraft is out of production. ==Design and development== Designed as a high-speed, long-range cross country and aerobatic aircraft, the Acro 1 features a cantilever low-wing, a single-seat enclosed cockpit under a bubble canopy, fixed conventional landing gear and a single engine in tractor configuration. The aircraft is stressed to +/-15g.〔 The aircraft is made from graphite and fiberglass composites. Its span wing has a wing area of and has no flaps. The acceptable power range is and the standard engine used is the Lycoming IO-360 powerplant which gives it a cruise speed of . A fuel capacity of provides a range of .〔 The Acro 1 has an empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload is .〔 The manufacturer estimates the construction time from the supplied kit as 700 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「Aircraft Technologies Acro 1」の詳細全文を読む スポンサード リンク
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