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CEI Free Spirit Mk II : ウィキペディア英語版 | CEI Free Spirit Mk II
The CEI Free Spirit Mk II, also called the Cabrinha Free Spirit Mark II and the Cabrinha Model 423, is a three-seat American homebuilt aircraft that was designed by Richard Cabrinha and produced by CEI of Auburn, California, introduced at AirVenture in 1995. The aircraft was intended to be supplied as a kit for amateur construction, but only prototypes seem to have been completed.〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition'', page 131. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1〕 ==Design and development== The design goals of the Free Spirit Mk II included long range, high speed and a high rate of climb. The aircraft features a cantilever low-wing, a two-seats-in-side-by-side configuration, plus a jump seat in an enclosed cockpit, retractable tricycle landing gear and a single engine in tractor configuration.〔 The aircraft is made from lightweight pre-molded composites. Its span wing employs a NASA NLF(1)-0215F natural laminar flow airfoil, mounts flaps and has a very small wing area of , giving a high wing loading of 25.0 lb/sq ft (122 kg/m2). The cabin width is . The acceptable power range is and the standard engine used is the Lycoming IO-360 powerplant.〔 The Free Spirit Mk II has a typical empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload for crew, passengers 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「CEI Free Spirit Mk II」の詳細全文を読む
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