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Saab 91 Safir : ウィキペディア英語版
Saab 91 Safir

The Saab 91 Safir (Swedish: "sapphire") is a three (91A, B, B-2) or four (91C, D) seater, single engine trainer aircraft. The Safir was built by Saab AB in Linköping, Sweden, (203 aircraft) and by ''De Schelde'' in Dordrecht, Netherlands (120 aircraft).
==Design and development==

The Safir's first flight on 20 November 1945.〔Taylor 1966, p. 125.〕 The all-metal Safir was designed by Anders J. Andersson, who had previously worked for Bücker, where he designed the all-wood Bücker Bü 181 "Bestmann". The Safir thus shared many conceptual features of its design with the Bestmann.
The Saab 91A is powered by a 125 hp four cylinder de Havilland Gipsy Major 2c piston engine, or a 145 hp Gipsy Major 10 piston engine. The 91B, B-2 and C have a six-cylinder Lycoming O-435A engine with 190 hp. The 91D has a four-cylinder Lycoming O-360-A1A engine with 180 hp.
The "Safir" was later used as a platform to test at low speeds the new swept wing for the Saab 29 and Saab 32 jet fighters.

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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