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AirLony Highlander : ウィキペディア英語版 | AirLony Highlander
The Airlony Highlander is a Czech ultralight biplane that was designed and produced by AirLony of Štětí, introduced in 1998.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 23. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a biplane wing configuration, a two-seats-in-tandem open cockpit, fixed conventional landing gear and a single engine in tractor configuration.〔 The aircraft has a composite fuselage and wooden-framed span wings with doped aircraft fabric covering. Engines in the can be used. The Highlander was designed for, but never approved for aerobatics.〔
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「AirLony Highlander」の詳細全文を読む
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