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Ehroflug Coach II S : ウィキペディア英語版
Ehroflug Coach II S

The Ehroflug Coach II S is a Swiss ultralight aircraft, designed by Egon Scheibe and produced by Ehroflug of Altnau. It was introduced in 1989. The aircraft is supplied as plans, as a kit for amateur construction or as a complete ready-to-fly-aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 44. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition'', page 149. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1〕
==Design and development==
The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a strut-braced parasol wing a two-seats-in-side-by-side configuration open cockpit, fixed conventional landing gear and a single engine in tractor configuration.〔〔
The aircraft fuselage is made from welded steel tubing, with the wing built from aluminium tubing with wooden ribs. The airframe is covered in doped aircraft fabric. Its span wing has an area of and is supported by cabane struts, V-struts and jury struts. The wings are quickly detachable for storage. Standard engines available are the Sauer 2.1 four-stroke Volkswagen air-cooled engine and the Rotax 582 two-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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