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・ Flight controller
・ Flight controller (disambiguation)
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・ Flight Crash Companion
・ Flight Crew (film)
・ Flight deck
・ Flight Deck (California's Great America)
・ Flight Deck (Canada's Wonderland)
・ Flight Deck (disambiguation)
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・ Flight Design Axxess
・ Flight Design C4
Flight Design CT
・ Flight Design Exxtacy
・ Flight Design MC
・ Flight director
・ Flight director (aeronautics)
・ Flight dispatcher
・ Flight Distance (hip hop group)
・ Flight distance record
・ Flight dynamics
・ Flight dynamics (fixed-wing aircraft)
・ Flight dynamics (spacecraft)
・ Flight Dynamics Flightsail
・ Flight Dynamics Flightsail VII
・ Flight endurance record
・ Flight engineer


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Flight Design CT : ウィキペディア英語版
Flight Design CT

The Flight Design CT series is a family of high-wing, tricycle undercarriage, two seat, ultralight and light-sport aircraft produced by Flight Design (Flightdesign Vertrieb) of Germany. The family includes the original CT and the CT2K, CTSW, CTLS and the new MC models.〔Hunt, Adam: ''One of aviation’s best kept secrets - Flight Design CT2K – Flight report'', COPA Flight page C-1. Canadian Owners and Pilots Association, October 2004〕
==Design and development==

All models in the series mount a Rotax 912UL or Rotax 912ULS engine in tractor configuration.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 50-51. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕
The aircraft are of composite construction, with carbon fiber being the primary material. This allows a very aerodynamic shape to the fuselage and very high useful loads (almost equal to the weight of the aircraft itself).〔
One reviewer of the CT2K writing COPA Flight in October 2004 described the aircraft as "fast, comfortable, roomy and very capable of long cross country flights for little money" and faulted the aircraft only for its difficulty slowing down from its cruise speed of 130 knots to its final approach speed of 50 knots, requiring careful planning to lose 80 knots between entering the circuit and stabilizing the aircraft on final approach.〔
Although the standard and required equipment varies by country, the CTSW has a standard Ballistic Recovery Systems parachute for the airframe. The BRS can be used to lower the entire aircraft to the ground in a controlled descent in the event of major structural failure, incapacitation of the pilot, or engine failure over mountainous terrain.

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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