Английская Википедия:ATEC 122 Zephyr 2000
The ATEC 122 Zephyr 2000 is a Czech ultralight aircraft, designed by Oldrich Olansky and produced by ATEC v.o.s. of Libice nad Cidlinou. The aircraft is supplied as a complete ready-to-fly-aircraft or as a kit for amateur construction.[1][2][3][4]
Design and development
The Zephyr was designed to comply with the Fédération Aéronautique Internationale microlight 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.[1][2][3]
The aircraft's fuselage is made from composites with wooden bulkheads. The semi-tapered Шаблон:Convert span wing is made from plywood with composite spars and leading edges and employs a UA-2 airfoil. The wing is covered with doped aircraft fabric. The standard engine factory-supplied was the Шаблон:Convert Rotax 912ULS four-stroke powerplant.[1][2][3][4]
The Zephyr is noted for its low payload. With a useful load of Шаблон:Convert and full fuel of Шаблон:Convert, this leaves only Шаблон:Convert for occupants and baggage.[1][2][3]
The Zephyr was later developed into the ATEC 321 Faeta.[1]
Variants
- Zephyr 2000
- base model for FAI microlight category.[1]
- Zephyr 2550
- Light-sport aircraft model[2][3]
Specifications (122 Zephyr 2000)
References
External links
- ↑ 1,0 1,1 1,2 1,3 1,4 1,5 Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 124. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
- ↑ 2,0 2,1 2,2 2,3 2,4 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 27. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ↑ 3,0 3,1 3,2 3,3 3,4 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 29. Flying Pages Europe SARL, 2015. Шаблон:ISSN
- ↑ 4,0 4,1 Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 118. BAI Communications, 15 July 1998. Шаблон:ISBN
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