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Scheibe SF 40 : ウィキペディア英語版 | Scheibe SF 40
The Scheibe SF 40 is a German two-seat ultralight aircraft designed and built by Scheibe Aircraft. ==Design== The SF 40 is a two-seat low-wing ultralight monoplane with a fixed tricycle landing gear.〔 It has a fabric-covered steel-tube fuselage with fabric-covered glass-fibre wings.〔 The first SF 40 powered by a Sauer four-stroke engine flew in 1995 but after five were built it was replaced in 1997 by an improved variant, the SF 40C.〔 The SF 40C is powered by a Rotax 912 engine with a two-bladed propellor, a shorter wing span than the original with increased fuel capacity.〔 The SF 40C was awarded a type certificate in May 1998.〔
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「Scheibe SF 40」の詳細全文を読む
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