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Harris Geodetic LW 108 : ウィキペディア英語版 | Harris Geodetic LW 108
The Harris Geodetic LW 108 is an American homebuilt aircraft that was designed by J. Warren Harris of Vernal, Utah and made available in the form of plans for amateur construction.〔Plane and Pilot: ''1978 Aircraft Directory'', page 143. Werner & Werner Corp, Santa Monica CA, 1977. ISBN 0-918312-00-0〕 ==Design and development== The aircraft features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed landing gear and a single engine in tractor configuration.〔 The aircraft is made from spruce and plywood, with the fuselage a geodetic airframe structure, producing a strong, lightweight and low-drag shape. Its wing has a span of . The standard engine recommended was the Continental A80.〔 The aircraft has an empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload 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「Harris Geodetic LW 108」の詳細全文を読む
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