Specifications (Rotax 912ULS)
Data from Jane's All the World's Aircraft 2010/11
General characteristics
- Capacity: 2
- Length: 5.69 m (18 ft 8 in)
- Wingspan: 9.04 m (29 ft 8 in)
- Height: 2.00 m (6 ft 7 in)
- Wing area: 9.40 m2 (101.2 sq ft)
- Empty weight: 284 kg (626 lb) including parachhute
- Max takeoff weight: 472.5 kg (1,042 lb)
- Fuel capacity: 65 L (15.8 imp gal, 19.0 US gal) standard
- Powerplant: 1 × Rotax 912ULS 4- cylinder flat four, air and water cooled, 73.5 kW (98.6 hp)
- Propellers: 3-bladed Junkers or Duc, ground adjustable pitch/
Performance
- Cruising speed: 243 km/h (151 mph; 131 kn) at 75% power
- Stall speed: 64 km/h (40 mph; 35 kn)
- Never exceed speed: 290 km/h (180 mph; 157 kn)
- Range: 648 km (403 mi; 350 nmi)
- g limits: +4/−2
- Rate of climb: 7.5 m/s (1,480 ft/min)
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