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Cirrus Vision SF50 : ウィキペディア英語版 | Cirrus Vision SF50
The Cirrus Vision SF50 is a single-engine, low-wing, seven-seat, very light jet aircraft under development by Cirrus Aircraft. The aircraft was initially developed under the project name "The Jet", but Cirrus announced the marketing name of "Vision SJ50" on July 9, 2008. In March 2009, the aircraft was redesignated the "Vision SF50".〔 〕 The prototype aircraft was first shown publicly at the annual Cirrus Migration on June 26, 2008, and first flown on July 3, 2008. The SF50 is intended to be a step up aircraft for pilots who have flown the Cirrus SR20, SR22 and other high-performance light aircraft.〔 ==Design and development==
The Vision SF50 will be equipped with a CAPS parachute and will be made of a composite material.〔 It is the first aircraft of its kind to fill the gap between high performance pistons, traditional turboprop twins and light business jets. The SF50 is designed for 12,000 flight hours.〔(【引用サイトリンク】title=Oshkosh: Cirrus enters final stretch of SF50 testing )〕
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「Cirrus Vision SF50」の詳細全文を読む
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