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The General Aircraft GAL 33 Cagnet was a British light trainer aircraft designed by General Aircraft Ltd which flew from 1939 to 1941. Only one example was constructed. ==Design== The Cagnet was a two-seat pusher propeller aircraft. The side-by-side seating was in an open cockpit just ahead of the strut-mounted inline engine. The low cantilever wings featured a gull shape, with twin booms mounted, one at each wing's bend point. A horizontal stabilizer and elevator ran between twin fins with rudders, one at the end of each boom. The fixed landing gear used a nosewheel. First flight was in 1939; the aircraft bore the serial number ''T46''. General Aircraft proposed the Cagnet as a basic trainer. It was tested as a Flying Observation post trainer by the Royal School of Army Co-operation from February through June 1940 (with military serial number ''W7646''). After that testing, it underwent various other tests. Its final flight was in 1941. The engine was a Blackburn Cirrus Minor, which gave a cruising speed of 100 mph (160 km/h). 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「General Aircraft Cagnet」の詳細全文を読む スポンサード リンク
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