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Thruster T600 Sprint
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Thruster T600 Sprint : ウィキペディア英語版
Thruster T600 Sprint

The Thruster T600 Sprint is a British ultralight aircraft, designed and produced by Thruster Air Services of Langworth, Lincolnshire and introduced in the mid-1990s. 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 81. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕
==Design and development==
The aircraft complies with the Fédération Aéronautique Internationale microlight rules and UK certified under BCAR Section "S". It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit accessed via doors, fixed tricycle landing gear or conventional landing gear and a single engine in tractor configuration.〔
The aircraft is made from bolted-together aluminum tubing, with its flying surfaces covered in treated Dacron sailcloth. Fittings and mounts are 316 stainless steel and 4130 steel. Its span wing has an area of and flaps. The engine is mounted on the keel tube, above the cockpit. Standard engines available are the Rotax 582 two-stroke and the Jabiru 2200 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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