Speeds
| Never-exceed speed (VNE) | 260 km/h (140 kts) |
| Cruise speed (Vc) | 220 km/h (119 kts) |
| Manoeuvring speed (VA) | 142 km/h (77 kts) |
| Stall speed without flaps (VS1) | 71 km/h (38 kts) |
| Stall speed in landing configuration (VS0) | 50 km/h (27 kts) |
Weights
| Maximum take-off weight | 450 kg / 992 lbs (472.5 kg / 1042 lbs with rescue system) |
| Empty weight | 298 kg / 657 lbs* |
*may vary based on actual aircraft equipment installed
Engine & Propeller
| Type | Rotax® 912 UL, ULS ; 914 UL ; 912iS fuel injection |
| Power | 80 – 115 HP |
| Propeller | Propeller 2 or 3 blades adjustable on the ground or in flight |
Fuel tank capacity
| Tank capacity | 90 l / 23,7 US gal / 67 kg |
| Endurance | 5,5 hrs + 30 min reserve |
| Range | 1050 km / 567 NM |
Take-off
| Take-off distance (up to 15 m / 50 ft) | 185 m – 200 m/ 610 ft – 660 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 6 in |
| Length | 7 m/ 22 ft 11.5 in |
| Height | 2,6 m/ 8 ft 6 in |
| Wing area | 11,85 m2/ 38 sq ft 10.5 sq in |
| Aspect ratio | 7,78 |
| Cabin width | 1,18 m3/ 3 ft 10.4 in |
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