Speeds
| Never exceed speed (VNE) | 260 km/h (140 kts) |
| Cruise speed (Vc) | 225 km/h (121 kts) |
| Manoeuvring speed (VA) | 142 km/h (77 kts) |
| Stall speed without flaps (VS1) | 65 km/h (35 kts) |
| Stall speed in landing configuration (VS0) | 58 km/h (31 kts) |
Weights
| Maximum take-off |
472.5kg / 580kg / 1042lbs / 1277 lbs (UL/LSA) |
| Empty weight | 311 kg / 686 lbs* |
*may vary based on actual aircraft equipment installed
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 | 90 l/ 67 kg/ 23,7 US gal |
| Endurance | 4,5 h + 30 min reserve |
| Range | 760 km / 410 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 5.7 in |
| Length | 7,0 m / 22 ft 11.6 in |
| Height | 2,6 m / 8 ft 6.3 in |
| Wing area | 11,85 m2 / 38 sq ft 10.5 sq in |
| Aspect ratio | 7,78 |
| Cabin width | 1,18 m / 3 ft 10.5 in |
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