Skyleader GP One
| GP One | |
|---|---|
| |
| Role | Ultralight aircraft
|
| National origin | Czech Republic |
| Manufacturer | Skyleader Aircraft
|
| Introduction | 2010 |
| Status | In production (2011) |
The Skyleader GP One is a
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
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
Production started in 2011, with the first customer deliveries in 2012.[2]
Specifications (GP One)
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 × 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
- ^ 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
- ^ ISSN 1368-485X
- ^ "Skyleader - Products - Skyleader GP One - Technical Data". Skyleader.aero. Archived from the original on 15 September 2011. Retrieved 6 September 2012.