Speeds
| Never-exceed speed (VNE) | 250 km/h (140 kts) |
| Cruise speed (Vc) | 175 km/h (119 kts) |
| Manoeuvring speed (VA) | 149 km/h (77 kts) |
| Stall speed without flaps (VS1) | 55 km/h (38 kts) |
| Stall speed in landing configuration (VS0) | 50 km/h (27 kts) |
Weights
| Maximum take-off weight | 472,5kg/600 kg (UL/LSA) |
| Empty weight 298 kg / 657 lbs | 297,5 kg |
Engine and propeller
| Type | Rotax 912 UL |
| Power | 80 HP |
| Propeller | 3 listá na zemi stavitelná |
Fuel tank capacity
| Tank capacity | 105 l / 27,7 US gal |
| Endurance | 7 h + 30 min reserve |
| Range | 1200 km |
Take-off
| Take-off distance (up to 15 m / 50 ft) | 185 m / 610 ft – 660 ft |
| Take-off run | 110 m / 300 ft – 330 ft |
Landing
| Landing distance (from 15 m / 50 ft) | 200 m / 660 ft |
| Take-off run | 120 m / 360 ft |
Dimensions
| wing span | 10,2 m |
| length | 6,25 m |
| height | 2,1 m |
| wing area | 11,165 m2 |
| Aspect ratio | 9,32 |
| cabin width | 1,2 m |
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