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The ATEC 122 Zephyr 2000 is a Czech ultralight aircraft, that was designed by Oldrich Olansky and produced by ATEC v.o.s. of Libice nad Cidlinou. The aircraft was supplied as a complete ready-to-fly-aircraft or as a kit for amateur construction.〔Bertrand, Noel; Rene Coulon; et al: ''World Directory of Leisure Aviation 2003-04'', page 124. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X〕〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 27. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition'', page 118. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1〕 ==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.〔〔 The aircraft's fuselage is made from composites with wooden bulkheads. The semi-tapered 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 Rotax 912ULS four-stroke powerplant.〔〔〔 The Zephyr is noted for its low payload. With a useful load of and full fuel of , this leaves only for occupants and baggage.〔〔 The Zephyr was later developed into the ATEC 321 Faeta.〔 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「ATEC 122 Zephyr 2000」の詳細全文を読む スポンサード リンク
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