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ECi O-320
The ECi O-320 is part of a family of normally aspirated, air-cooled, four-cylinder, direct-drive engines developed for ceritified and experimental aircraft. Its cylinders are arranged in horizontally opposed configuration and a displacement of 320 cubic inches (5.24 L). It is based on the Lycoming O-320 engine with ECi cylinder assemblies.〔(【引用サイトリンク】url=http://www.eaa.org/news/2013/2013-08-12_proposed-AD-demands-removal-of-thousands-of-ECI-titan-cylinders.asp )〕〔(【引用サイトリンク】url=http://www.aopa.org/News-and-Video/All-News/2008/September/18/ECi-AD-affects-13-000-Titan-cylinders )〕 ==Design and development== ECi developed engine kits starting in 1995.
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「ECi O-320」の詳細全文を読む
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