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ATEC 321 Faeta
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.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 28. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕〔Bertrand, Noel; Rene Coulon; et al: ''World Directory of Leisure Aviation 2003-04'', page 124. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X〕
==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.〔〔
The aircraft fuselage is made with a carbon fibre shell and composite sandwich bulkheads. The span wing is made from carbon fibre sandwiches built upon a wooden spar. The wing varies from the Zephyr in that it has a different tapered planform and uses a new airfoil. The standard engine available is the Rotax 912ULS four-stroke powerplant.〔〔
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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