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翻訳と辞書　辞書検索 [ 開発暫定版 ] スポンサード リンク ATEC 212 Solo ： ウィキペディア英語版 ATEC 212 Solo 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.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 28. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==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.〔 The 212 Solo is made from carbon fibre and was derived from the ATEC 321 Faeta and ATEC 122 Zephyr 2000 designs. Its span wing employs an SM701 airfoil and slotted flaps. Standard engines available are the Rotax 582 two-stroke and the Rotax 912UL 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）』 ■ウィキペディアで「ATEC 212 Solo」の詳細全文を読む スポンサード リンク 翻訳と辞書 : 翻訳のためのインターネットリソース Copyright(C) kotoba.ne.jp 1997-2016. All Rights Reserved.