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Cessna Citation M2
The Cessna Citation M2 is a turbofan-powered light corporate jet built by the Cessna Aircraft Company in Wichita, Kansas. The Citation M2 is based on the earlier Model 525 CitationJet (CJ1).
==Design and development==
The original Model 525 CitationJet was launched in 1989.〔 The M2 was launched in September 2011 and it was described as a new light business jet.〔 The M2 is based on the then out-of-production CJ1 variant and features a new cabin layout and a more efficient version of the Williams FJ44 engine.〔 The M2 first flew on 9 March 2012.〔〔The initial M2 prototype, which first flew on 9 March, is not considered a conforming airframe; it aircraft will serve as a conforming platform for testing of the Garmin G3000 avionics and Williams FJ44-1AP-21 turbofan engines, which will be its primary role in the certification program. The certification program will involve only one other aircraft, which is expected to join the program in May. The second aircraft (which will be considered completely conforming to the certificated design) will be used for aerodynamics testing. (Launches M2 Flight Test Program&channel=busav Aviation Week & Space Technology website, accessed 22 March 2012 )〕〔(Cessna Launches Aggressive Nine-Month M2 Flight Test Program )〕 An M2 may cost around per nautical mile to operate, whereas the G650 and similar may cost $5-6.〔 (Table ) (Mission Costs for Turboprops Greater Than 12,500 lb., Jets Less Than 20,000 lb. )〕
The Citation M2 is a low-wing cantilever monoplane with retractable tricycle landing gear, a pressurized cabin, a T-tail, and is powered by two Williams FJ44-1AP-21 turbofan engines that are pylon-mounted on the rear fuselage.
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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