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
National origin Czech Republic
Manufacturer Skyleader Aircraft
Introduction 2010
Status In production (2011)

Design and development

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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]

Specifications (GP One)

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Data from Bayerl and Skyleader[1][3]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 6.25 m (20 ft 6 in)
  • Wingspan: 10.2 m (33 ft 6 in)
  • Height: 2.1 m (6 ft 11 in)
  • Wing area: 11.165 m2 (120.18 sq ft)
  • Aspect ratio: 9.32:1
  • Empty weight: 280 kg (617 lb)
  • Gross weight: 472.5 kg (1,042 lb)
  • Fuel capacity: 105 litres (23 imp gal; 28 US gal)
  • Powerplant: 1 × Rotax 912UL four cylinder, liquid and air-cooled, four stroke aircraft engine, 60 kW (80 hp)
  • Propellers: 3-bladed ground adjustable, composite

Performance

  • Maximum speed: 215 km/h (134 mph, 116 kn)
  • Cruise speed: 193 km/h (120 mph, 104 kn)
  • Stall speed: 64 km/h (40 mph, 35 kn)
  • Never exceed speed: 260 km/h (160 mph, 140 kn)
  • Range: 1,370 km (850 mi, 740 nmi)
  • Endurance: 6.1 hours plus 0.5 hour reserve
  • Wing loading: 42.3 kg/m2 (8.7 lb/sq ft)

References

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  1. ^ a b c d Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 76. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. ^ a b c d Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 80. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  3. ^ "Skyleader - Products - Skyleader GP One - Technical Data". Skyleader.aero. Archived from the original on 15 September 2011. Retrieved 6 September 2012.
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