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Cessna 308 : ウィキペディア英語版
Cessna 308

The Cessna 308 was a prototype military light transport aircraft based on the successful Cessna 305 observation aircraft. Only one aircraft was completed and the project did not proceed further, due to a lack of orders.
==Development==
The Cessna 308 was conceived as an enlarged model 305 that would carry four people for the military light transport role and was developed in response to a US Army requirement.〔
The resulting design was first flown in July 1951. While the aircraft was based on the model 305, it incorporated a four-place cabin similar to the then current production Cessna 170. The prototype was powered by a Lycoming GSO-580 geared, supercharged, eight-cylinder engine, producing . The prototype featured a wingspan, taildragger landing gear and a gross take-off weight. In trials the 308 proved capable of operating from rough fields carrying a payload, with a range of .〔
The US Army chose the de Havilland Canada DHC-2 Beaver for the intended light transport role putting it into service as the L-20A. As a result, development of the Cessna 308 was not continued beyond the completion of a single prototype.〔

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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