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The Bilsam Sky Cruiser is a Polish microlight aircraft designed and produced by Bilsam Aviation of Poznań, introduced in the early 2000s. The aircraft is supplied as a complete ready-to-fly-aircraft, as a kit and in the form of plans for amateur construction.〔Bertrand, Noel; Rene Coulon; et al: ''World Directory of Leisure Aviation 2003-04'', page 128. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X〕 The manufacturer's website is non-functional and has been so since about 2008, so it is not clear if the company is still in business. ==Design and development== The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of . The aircraft has a maximum gross weight of . With a Rotax 912 ULS engine it is an accepted US light sport aircraft and also a Transport Canada accepted Advanced Ultra-Light Aeroplane.〔 Originally shown as a pusher configuration design in 2003, by 2004 the aircraft had been redesigned. In its production configuration the Sky Cruiser features a cantilever high-wing, a two-seats-in-side-by-side configuration enclosed cabin with doors for access, fixed tricycle landing gear with wheel pants and a single engine in tractor configuration.〔 The aircraft is made from composite material. Its span wing mounts flaps and has a wing area of . The standard engine used is the Suzuki automotive conversion powerplant.〔 The aircraft has a typical empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload for pilot, passenger and baggage is .〔 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「Bilsam Sky Cruiser」の詳細全文を読む スポンサード リンク
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