Thruster T600 Sprint

T600 Sprint
Role Ultralight aircraft
National origin United Kingdom
Manufacturer Thruster Air Services
Introduction mid-1990s
Status In production (2012)
Unit cost
£30,000 (assembled, 2011)

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.[1]

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.[1]

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 9.60 m (31.5 ft) span wing has an area of 15.70 m2 (169.0 sq ft) and flaps. The engine is mounted on the keel tube, above the cockpit. Standard engines available are the 64 hp (48 kW) Rotax 582 two-stroke and the 85 hp (63 kW) Jabiru 2200 four-stroke powerplant.[1][2]

Specifications (T600 Sprint)

Data from Bayerl and Thruster Air Services[1][2]

General characteristics

Performance

See also

Similar aircraft

References

  1. 1 2 3 4 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 81. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. 1 2 Thruster Air Services (n.d.). "Thruster T600 Sprint - 450kg Standard Specifications". Retrieved 9 September 2012.
This article is issued from Wikipedia - version of the 5/13/2016. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.