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Yakovlev AIR-6
The Yakovlev AIR-6 was a Soviet light utility aircraft of the 1930s. It was a single-engined high-winged monoplane designed by Alexander Sergeyevich Yakovlev, which was ordered into production, over 100 being built.
==Design and development==
In 1932, the Soviet aircraft designer Alexander Sergeyevich Yakovlev, working as an engineering supervisor at the Polikarpov OKB, designed the AIR-5, a five-seat high-winged monoplane with a steel-tube fuselage and a wooden wing, powered by an American Wright J-4 Whirlwind radial engine giving 149 kW (200 hp). Although the AIR-5 successfully passed State acceptance trials, no production followed, as there was no suitable Soviet replacement for the imported engine.〔Gunston 1995, pp. 451, 453–454.〕〔Gordon, Komissarov and Komissarov 2005, pp. 23–23.〕
Yakovlev instead designed a scaled-down aircraft of similar layout to the AIR-5, but powered by a readily available 75 kW (100 hp) Shvetsov M-11 engine, to serve as a light utility aircraft. The new design, the AIR-6, was a high-winged monoplane using much of the structural design of the AIR-5, (and also featuring landing struts from the Polikarpov U-2 and tail surfaces from the Tupolev I-5 fighter), with a pilot and one or two passengers sitting in tandem in an enclosed cockpit.〔Gunston 1995, p. 454.〕〔Gordon, Komissarov and Komissarov 2005, p. 24.〕
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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