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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 Norman Aviation Nordic II ： ウィキペディア英語版 Norman Aviation Nordic II The Norman Aviation Nordic II is a Canadian advanced ultralight aircraft, designed by Jacques Norman and produced by Norman Aviation of Saint-Anselme, Quebec, first flying in 1986. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft and remained in production through 2012.〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook'', page 214. BAI Communications. ISBN 0-9636409-4-1〕〔Downey, Julia: ''1999 Kit Aircraft Directory'', Kitplanes, Volume 15, Number 12, December 1998, page 58. Primedia Publications. ISSN 0891-1851〕 ==Design and development== The Nordic II was designed to comply with the Canadian ultralight rules. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit with doors, fixed conventional landing gear and a single engine in tractor configuration.〔 The aircraft fuselage is made from welded steel tubing, with its wings made from wood and all surfaces covered in doped aircraft fabric. Its span wing has an area of and mounts flaps. The wing is supported by V-struts and jury struts. The cockpit width is . The standard engines used are the Rotax 582 two-stroke, the Rotax 912UL or Subaru EA four-stroke powerplants.〔 Construction time from the factory supplied kit is estimated at 300 hours.〔 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「Norman Aviation Nordic II」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.