Crew: 2
Length: 6.60 m (21 ft 8 in)
Wingspan: 9.00 m (29 ft 6 in)
Height: 2.58 m (8 ft 6 in) with optional rudder extension 2.88 m (9 ft 5 in)
Wing area: 12.87 m2 (138.5 sq ft) gross
Airfoil: NACA 65-018 (modified)
Empty weight: 286 kg (631 lb)
Max takeoff weight: 450 kg (992 lb) European ultralight; experimental 560 kg (1,234 lb); Australian and New Zealand version 600 kg (1,323 lb).
Fuel capacity: 78 litres (20.6 US gal; 17.2 Imp gal). Australia and New Zealand version with standard long range tanks: capacity = 150 litres (39.6 US gal; 33.0 Imp gal).
Powerplant: 1 Rotax 912 ULS air partly water cooled, four cylinder, 73 kW (98 hp)80 hp
Performance
Maximum speed: 198 km/h (123 mph, 107 kn)
Cruise speed: 179 km/h (111 mph, 97 kn) at 75% power
Stall speed: 48 km/h (30 mph, 26 kn) full flaps
Never exceed speed: 230 km/h (140 mph, 124 kn)
Endurance: 4 h with standard tanks 8 h with long range tanks
g limits: +6/-3
Rate of climb: 6.1 m/s (1,200 ft/min) at 49 knots, fitted with a Rotax 912 ULS engine.

Airplane time state:
TTAF 398 hours
TTE 207 hours

Standard analog instruments

9/10

9/10