Английская Википедия:ATEC 212 Solo

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The ATEC 212 Solo is a Czech ultralight aircraft, designed and produced by ATEC v.o.s. of Libice nad Cidlinou. The aircraft is supplied as a complete ready-to-fly-aircraft.[1][2]

Design and development

The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, a single-seat, enclosed cockpit with a bubble canopy, fixed conventional landing gear and a single engine in tractor configuration.[1][2]

The 212 Solo is made from carbon fibre and was derived from the ATEC 321 Faeta and ATEC 122 Zephyr 2000 designs. Its Шаблон:Convert span wing employs an SM701 airfoil and slotted flaps. Standard engines available are the Шаблон:Convert Rotax 582 two-stroke and the Шаблон:Convert Rotax 912UL four-stroke powerplant.[1][2]

Specifications (212 Solo)

Шаблон:Aircraft specs

References

Шаблон:Reflist

External links

Шаблон:ATEC aircraft

  1. 1,0 1,1 1,2 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 28. 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 29. Flying Pages Europe SARL, 2015. Шаблон:ISSN