Английская Википедия:Colyaer Freedom S100

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The Colyaer Freedom S100 is a Spanish amphibious ultralight and light-sport aircraft, designed and produced by Colyaer of Portonovo.[1]

Design and development

The Freedom was subject to a lengthy eleven-year development process between 1995 and 2006. It was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a cantilever high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, retractable tricycle landing gear, wing-tip pontoons and a single engine in pusher configuration.[1][2]

The Freedom is made entirely from carbon fibre, Kevlar and fibreglass composites. Its Шаблон:Convert span wing has an area of Шаблон:Convert and flaps that can be deployed for landing and reflexed for cruise flight. The long wingspan gives the Freedom a glide ratio of 20:1 and allows power-off soaring flights. The standard engine is the Шаблон:Convert Rotax 912ULS four-stroke powerplant.[1]

In 2015 the aircraft was marketed by Galicia Avionica SL.[3]

Specifications (Freedom S100)

Шаблон:Aircraft specs

References

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External links

Шаблон:Commons category

Шаблон:Colyaer aircraft

  1. 1,0 1,1 1,2 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 36. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. Шаблон:Cite web
  3. Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 57. Flying Pages Europe SARL, 2015. Шаблон:ISSN