Английская Википедия:Airsport Sonet

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The Airsport Sonet (Шаблон:Lang-en) is a Czech ultralight aircraft, designed and produced by Airsport of Zbraslavice. The aircraft is supplied in complete, ready-to-fly form.[1][2]

Design and development

The aircraft was derived from the Airsport Sonata motor glider and designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, a T-tail, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.[1][2]

The Sonet is made from composites. Its polyhedral wing comes in three optional spans: Шаблон:Convert, Шаблон:Convert and Шаблон:Convert. It requires an engine of about Шаблон:Convert and no more than Шаблон:Convert. Standard engines available are the Шаблон:Convert Rotax 582 two-stroke and the Шаблон:Convert HKS 700E four-stroke powerplant.[1][2][3]

Specifications (Sonet 11.4)

Шаблон:Aircraft specs

Шаблон:Aircontent

References

Шаблон:Reflist

External links

Шаблон:Airsport aircraft

  1. 1,0 1,1 1,2 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 24. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. 2,0 2,1 2,2 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 24. Flying Pages Europe SARL, 2015. Шаблон:ISSN
  3. Шаблон:Cite web