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The Fieseler F 4 was developed, built and flown as a two-seat sports and travel aircraft at the Fieseler Flugzeugbau. ==Design and development== After the failure of the Fieseler F 3 Wespe, Fieseler developed a sport aircraft with emphasis placed on safety, quality, efficiency, and convenience, designated Fieseler F 4. The F 4 was a two-seat low-wing monoplane, with a welded steel tube fuselage and wooden wings covereed with aircraft linen. The wings, attached to the fuselage, were braced with profile wires from the top of the fuselage and the undercarriage. Fitted with balloon tires the undercarriage was attachedforward of the centre of gravity, reducing the danger of nose-over during a difficult landing. Fuel was carried in a gravity tank and transferred using flexible hoses. Well padded seats in the cockpits with moveable armrests increased comfort and adjustable rudder pedals accommodated pilots of varying heights. A luggage compartment behind the pilot's seat also gave access to controls and equipment in the fuselage. Initially powered by a Argus As 16 engine, the F 4 was later powered by a Salmson 9 AD engine. 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「Fieseler F 4」の詳細全文を読む スポンサード リンク
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