Top speed 215 km/h Length 6.25 m | Wingspan 10 m | |
Skyleader gp one light sport aircraft flying in nz at lake manapouri
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.
Contents
- Skyleader gp one light sport aircraft flying in nz at lake manapouri
- Skyleader gp one light sport aircraft 1st flight in new zealand
- Design and development
- Specifications GP One
- References
Skyleader gp one light sport aircraft 1st flight in new zealand
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.
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.
Production started in 2011, with the first customer deliveries in 2012.
Specifications (GP One)
Data from Bayerl and Skyleader
General characteristics
Performance