Skyleader GP One
| GP One | |
|---|---|
.jpg) | |
| Role | Ultralight aircraft |
| National origin | Czech Republic |
| Manufacturer | Skyleader Aircraft |
| Introduction | 2010 |
| Status | In production (2011) |
| Unit cost |
€55,000 (assembled, 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]
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]
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. Deliveries were expected to start in 2012.[1]
Specifications (GP One)
Data from Bayerl and Skyleader[1][2]
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)
- Cruising speed: 193 km/h (120 mph; 104 kn)
- Stall speed: 64 km/h (40 mph; 35 kn)
- Never exceed speed: 260 km/h (162 mph; 140 kn)
- Range: 1,370 km (851 mi; 740 nmi)
- Endurance: 6.1 hours plus 0.5 hour reserve
- Wing loading: 42.3 kg/m2 (8.7 lb/sq ft)
