Английская Википедия:ATEC 321 Faeta

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The ATEC 321 Faeta is a Czech ultralight and light-sport aircraft, designed and produced by ATEC v.o.s. of Libice nad Cidlinou. It was developed from the earlier ATEC 122 Zephyr 2000. The aircraft is supplied as a complete ready-to-fly-aircraft.[1][2][3]

Design and development

The Faeta was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed tricycle landing gear, a T-tail and a single engine in tractor configuration. It is an approved SLSA in the USA.[1][2][3][4]

The aircraft fuselage is made with a carbon fibre shell and composite sandwich bulkheads. The Шаблон:Convert span wing is made from carbon fibre sandwiches built upon a laminated wooden spar. The wing varies from the Zephyr in that it has a different tapered planform and uses a new airfoil. The design attempts to provide a lower empty weight and stall speed than the 122 Zephyr. The standard engine available is the Шаблон:Convert Rotax 912ULS four-stroke powerplant.[1][2][3]

The Nordic Omsider amphibian prototype uses the wings and part of the tail from the Faeta.[3]

Specifications (321 Faeta)

Шаблон:Aircraft specs


References

Шаблон:Reflist

External links

Шаблон:Commons category

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 Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 124. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
  3. 3,0 3,1 3,2 3,3 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 29 and 70. Flying Pages Europe SARL, 2015. Шаблон:ISSN
  4. Шаблон:Cite web