Skyleader GP One

GP One
Role Ultralight aircraft
National origin Czech Republic
Manufacturer Skyleader Aircraft
Introduction 2010
Status In production (2011)
Unit cost
55,000 (assembled, 2011)

The Skyleader GP One is a Czech ultralight aircraft, designed and produced by Skyleader Aircraft and introduced at the AERO Friedrichshafen show in 2010. The aircraft is supplied as a complete ready-to-fly-aircraft.[1]

Design and development

The GP One was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever high-wing, a two-seats-in-side-by-side configuration enclosed cockpit accessed by doors, fixed tricycle landing gear and a single engine in tractor configuration.[1]

The aircraft is made from carbon fibre and has a predicted empty weight of 280 kg (617 lb). Its 10.2 m (33.5 ft) span wing has an area of 11.165 m2 (120.18 sq ft) and mounts flaps. The standard engine available is the 80 hp (60 kW) Rotax 912UL four-stroke powerplant. Deliveries were expected to start in 2012.[1]

Specifications (GP One)

The first production Skyleader 'GP One' light sport aircraft is parked at Manapouri Airport, New Zealand
Skyleader 'GP One' light sport aircraft at Manapouri Airport, New Zealand

Data from Bayerl and Skyleader[1][2]

General characteristics

Performance

References

  1. 1 2 3 4 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 76. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. "Skyleader - Products - Skyleader GP One - Technical Data". Skyleader.aero. Retrieved 2012-09-06.

External links

This article is issued from Wikipedia - version of the Friday, February 26, 2016. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.