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Dova DV-1 Skylark : ウィキペディア英語版 | Dova DV-1 Skylark
The Dova DV-1 Skylark is a Czech ultralight and light-sport aircraft produced by Dova Aircraft of Paskov. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 42. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development==
The DV-1 was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a cantilever low-wing, a T-tail, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed tricycle landing gear with wheel pants and a single engine in tractor configuration.〔 The aircraft is made from aluminum sheet. Its span wing has an area of and is equipped with flaps and winglets. Standard engines available are the Rotax 912UL, Rotax 912ULS, turbocharged Rotax 914 and the BMW 1100 four-stroke powerplants.〔
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