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][2]
GP One
Role
Ultralight aircraft
Type of aircraft
National origin
Czech Republic
Manufacturer
Skyleader Aircraft
Introduction
2010
Status
In production (2011)
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][2]
The aircraft is made from carbon fibre and has a predicted empty weight of 280kg (617lb). Its 10.2m (33.5ft) span wing has an area of 11.165m2 (120.18sqft) and mounts flaps. The standard engine available is the 80hp (60kW) Rotax 912UL four-stroke powerplant.[1][2]
Production started in 2011, with the first customer deliveries in 2012.[2]
Specifications (GP One)
Skyleader 'GP One' light sport aircraft at Manapouri Airport, New Zealand
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