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Airsport Sonet : ウィキペディア英語版 | Airsport Sonet
The Airsport Sonet ((英語:Sonnet)) is a Czech ultralight aircraft, designed and produced by Airsport of Zbraslavice. The aircraft is supplied in complete, ready-to-fly form.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 24. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The aircraft was derived from the Airsport Sonata motor glider and designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, a T-tail, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.〔 The Sonet is made from composites. Its polyhedral wing comes in three optional spans: , and . It requires an engine of about and no more than . Standard engines available are the Rotax 582 two-stroke and the HKS 700E four-stroke powerplant.〔
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「Airsport Sonet」の詳細全文を読む
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