Speeds
| Never exceed speed (VNE) | 265 km/h (143 kts) |
| Cruise speed (Vc) | 230 km/h (124 kts) |
| Manoeuvring speed (VA) | 145 km/h (78 kts) |
| Stall speed without flaps (VS1) | 72 km/h (39 kts) |
| Stall speed in landing configuration (VS0) | 61 km/h (33 kts) |
Weights
| Maximum take-off weight | 600 kg/ 1323 lbs (UL/LSA) |
| Empty weight | 340 kg/ 750 lbs |
Engine and propeller
| Type | Rotax 912 UL/ULS, 914 UL, 912iS |
| Power | 80 – 115 HP |
| Propeller | Propeller 2 or 3 blades adjustable on the ground or in flight |
Fuel tank capacity
| Tank capacity | 120 l/ 90 kg/ 31,7 US gal |
| Endurance | 8,5 h + 30 min reserve |
| Range | 1600 km |
Take-off
| Take-off distance (up to 15 m / 50 ft) | 250 m / 820 ft |
| Take-off run | 90 m - 100 m / 300 ft – 330 ft |
Landing
| Landing distance (from 15 m / 50 ft) | 200 m / 660 ft |
| Landing ground roll | 100 m / 330 ft |
Dimensions
| Wing span | 9,9 m / 32 ft 5.7 in |
| Length | 7,1 m / 23 ft 3.5 in |
| Height | 2,46 m / 8 ft 0.8 in |
| Wing area | 11,85 m2 / 38 sq ft 10.5 sq in |
| Aspect ratio | 7,78 |
| Cabin width | 1,28 m / 4 ft 2.4 in |
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