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Cessna Skymaster
The Cessna Skymaster is a United States twin-engine civil utility aircraft built in a push-pull configuration. Its engines are mounted in the nose and rear of its pod-style fuselage. Twin booms extend aft of the wings to the vertical stabilizers, with the rear engine between them. The horizontal stabilizer is aft of the pusher propeller, mounted between and connecting the two booms.〔Wood, Derek: ''Jane's World Aircraft Recognition Handbook'', page 471. Jane's Publishing Company, 1985. ISBN 0-7106-0343-6〕 The combined tractor and pusher engines produce 'centerline' thrust and a unique sound.〔Plane and Pilot: ''1978 Aircraft Directory'', page 92. Werner & Werner Corp Publishing, 1978. ISBN 0-918312-00-0〕
==Development==
The first Skymaster, model 336, had fixed landing gear and first flew on February 28, 1961.〔Taylor, Michael: ''Encyclopedia of Modern Military Aircraft'', page 67. Gallery Books, 1987. ISBN 0-8317-2808-6〕〔 It went into production in May 1963,〔 and 195 were produced through mid 1964.〔
In February 1965 Cessna introduced the model 337 Super Skymaster.〔Green, William: ''Observers Aircraft'', page 46. Frederick Warne Publishing, 1974. ISBN 0-7232-1526-X〕 The model was larger, and had more powerful engines, retractable landing gear, and a dorsal air scoop for the rear engine ("Super" was subsequently dropped from the name).〔 In 1966 the turbocharged T337 was introduced, and in 1973 the pressurized P337G entered production.〔
Cessna built 2993 Skymasters of all variants, including 513 military O-2 versions.〔 Production in America ended in 1982 but continued with Reims in France with the FTB337 STOL and the military FTMA ''Milirole''.〔
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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