| GP One | |
|---|---|
| |
| Role | Ultralight aircraft |
| National origin | Czech Republic |
| Manufacturer | Skyleader Aircraft |
| Introduction | 2010 |
| Status | In production (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][2]
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 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.[1][2]
Production started in 2011, with the first customer deliveries in 2012.[2]
Data from Bayerl and Skyleader[1][3]
General characteristics
Performance
