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Phoenix Air Phoenix
The Phoenix Air Phoenix is a Czech low-wing, two-seat motor glider, designed and produced by Phoenix Air and provided as a complete ready-to-fly aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 135. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕
==Design and development==
The Phoenix is a derivative of the Urban Air Lambada motorglider, developed by Martin Stepaneck who was formerly with Urban Air before that company's demise. The Phoenix was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a cantilever wing, a T-tail, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed conventional landing gear and a single engine in tractor configuration.〔
The aircraft is made from composites. Its span wing is convertible to , by removing the wing tips and then re-installing shorter tips and the winglets for faster cruising speed when flying as a microlight. With the wing tips removed it has a wingspan of for storage. Standard engines available are the Rotax 912UL, the Rotax 912ULS, Jabiru 2200 and the HKS 700E four-stroke powerplants. With the 912S engine the aircraft can be employed as a glider tug. An electric-powered version is under development.〔
The European version has a gross weight of , while the LSA version has a gross weight of . The design appears on the Federal Aviation Administration's list of approved special light-sport aircraft.〔〔
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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