Crew: 2
Length: 6.4 m (21 ft 0 in)
Wingspan: 9.3 m (30 ft 6 in)
Height: 2.49 m (8 ft 2 in)
Wing area: 13.2 m2 (142 sq ft)
Empty weight: 304 kg (670 lb)
Max takeoff weight: 550 kg (1,213 lb)
Fuel capacity: 90 L (24 US gal; 20 imp gal) total with 80 L (21 US gal; 18 imp gal) usable (70 L (18 US gal; 15 imp gal) total in earlier versions)
Powerplant: 1 Rotax 912ULS 4-cylinder air-cooled horizontally-opposed piston engine, 73.5 kW (98.6 hp)
Propellers: 2-bladed GT-172/164, 1.72 m (5 ft 8 in) diameter fixed pitch wooden propeller
Performance
Maximum speed: 235 km/h (146 mph, 127 kn) at sea level
Cruise speed: 210 km/h (130 mph, 110 kn) at 75% power with propeller 2,200 rpm
Stall speed: 70 km/h (43 mph, 38 kn) flaps down
Never exceed speed: 270 km/h (170 mph, 150 kn)
Range: 800 km (500 mi, 430 nmi)
Endurance: 4.5-5 hours
Service ceiling: 4,510 m (14,800 ft)
g limits: +3.8 -1.5
Maximum glide ratio: 13
Rate of climb: 6 m/s (1,200 ft/min)
Take-off run: 143 m (469 ft)
Landing run: 100 m (328 ft)

Airplane time state:
TTAF 1225
TTE 1225

VFR analog instrumentation

8/10

9/10