Crew: 2
Length: 6.4 m (21 ft 0 in)
Wingspan: 8.7 m (28 ft 7 in)
Height: 2.5 m (8 ft 2 in)
Empty weight: 356 kg (785 lb)
Max takeoff weight: 450 kg (
Fuel capacity: 90 L (24 US gal; 20 imp gal) total with 80 L (21 US gal; 18 imp gal) usable
Powerplant: Rotax 912ULS 4-cylinder air-cooled horizontally-opposed piston engine, 73.5 kW (98.6 hp)
Propellers: 3-bladed variable pitch
Performance
Maximum speed: 213 km/h (132 mph, 115 kn) Max cruise speed TAS
Stall speed: 72 km/h (45 mph, 39 kn) flaps down
Range: 1,296 km (805 mi, 700 nmi)
Rate of climb: 4.9 m/s (960 ft/min)
Take-off run: 214 m (702 ft)
Landing run: 154 m (505 ft)
Take-Off Distance: 369 m (1,211 ft)

Airplane time state:
TTAF 1200
TTE 1020

Standard avionics VFR

9/9

10/10

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