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Stoddard-Hamilton Glasair III : ウィキペディア英語版 | Stoddard-Hamilton Glasair III __NOTOC__ The Stoddard-Hamilton Glasair III is an American two-seat dual-control monoplane designed and built by Stoddard-Hamilton Aircraft of Arlington, Washington as an addition to the Glasair range of aircraft for amateur construction.〔〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 103. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The Glasair III is an all-composite cantilever low-wing monoplane. It is an improved variant of the earlier Glasair II with a retractable landing gear and powered by a Lycoming IO-540-K1H5 engine. It has two seats side-by-side with dual controls, the aircraft can be fitted with wing tip fuel tanks.〔〔
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「Stoddard-Hamilton Glasair III」の詳細全文を読む
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