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The Fisher Boomerang is a single-seat conventional landing gear, high-winged monoplane ultralight aircraft designed by Michael Fisher and introduced in mid-1982.〔Taylor, John WR: ''Janes All the Worlds Aircraft 1983-84'', Janes Publishing Company, 1983, p.660.〕〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page E-7. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕 ==Development== The Boomerang was intended to meet the requirements of the US FAR 103 ''Ultralight Vehicles'' category, including that category's maximum empty weight. The aircraft has a standard empty weight of .〔 The aircraft is a single-seat ultralight with a high wing and a conventional three-axis type with ailerons, elevators and rudder. The airframe structure is of 6061T6 and 2024T3 aluminum tube, covered with Stits Polyfibre aircraft fabric. The landing gear is of a fixed taildragger configuration without suspension on the main wheels. Wings were available in several spans, from , the longer span being used for the two seat variant.〔〔 The Boomerang is fitted with a Kawasaki 340 engine as standard equipment or optionally a Kawasaki 440A engine, both with a reduction drive system. The aircraft has an empty weight of and a gross weight of , giving a useful load of .〔〔 The aircraft was discontinued due to poor sales.〔 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「Fisher Boomerang」の詳細全文を読む スポンサード リンク
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