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Ikarus C52
The Ikarus C52 is a German ultralight aircraft, designed and produced by Comco Ikarus, introduced at the Aero show held in Friedrichshafen in 2011. The aircraft is supplied as a complete ready-to-fly-aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 36. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕
==Design and development==
An evolution of the Ikarus C42, the C52 was designed to comply with the Fédération Aéronautique Internationale microlight rules. It not only updates the older design, but offers more comforts. The C-52 is not intended to replace the C42 in production, but instead to act as a higher-end complimentary model. Like the C42, it features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed open cockpit, fixed tricycle landing gear and a single engine in tractor configuration.〔
The aircraft differs from the earlier C42 primarily in that the landing gear is a cantilever design, the tail is constructed of carbon fibre and the engine mount was redesigned. Its span wing employs V-struts with jury struts and has an area of . Standard engines available are the Rotax 912UL and the Rotax 912ULS four-stroke powerplants.〔
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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