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DAR Solo
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DAR Solo : ウィキペディア英語版
DAR Solo

The DAR Solo is a Bulgarian ultralight aircraft, designed by Tony Ilieff and produced by Aeroplanes DAR, first flying in August 2008.
The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 20. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕
==Design and development==
The aircraft was designed to comply with the US light-sport aircraft rules as well as the German 120 kg class and deregulated 115 kg class in the United Kingdom. It features a strut-braced high wing, a single-seat open cockpit, tricycle landing gear and a single engine in tractor configuration.〔
The aircraft is built with a composite fuselage and an aluminum wing. Its span wing has flaperons and employs a single strut on each side supported by an optional jury strut. The standard engine is the Hirth F33 two-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「DAR Solo」の詳細全文を読む



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