Skyleader GP One explained

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]}

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 2800NaN0. Its 10.21NaN1 span wing has an area of 11.165m2 and mounts flaps. The standard engine available is the 800NaN0 Rotax 912UL four-stroke powerplant.^{[1] [2]}

Production started in 2011, with the first customer deliveries in 2012.^[2]

External links

• • Photo of a Skyleader GP One

Notes and References

1. Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 76. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
2. Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 80. Flying Pages Europe SARL, 2015.