Speeds
| Never-exceed speed (VNE) | 260 km/h (140 kts) |
| Cruise speed (Vc) | 200 km/h (108 kts) |
| Manoeuvring speed (VA) | 142 km/h (77 kts) |
| Stall speed without flaps (VS1) | 74 km/h (40 kts) |
| Stall speed in landing configuration (VS0) | 67 km/h (36 kts) |
Weights
| Maximum take-off | UL/ LSA MTOM 600 kg / 1320 lbs. |
| Empty weight | 320 kg / 705 lbs* |
*may vary based on actual aircraft equipment installed
Engine and Propeller
| Type | Rotax 912 UL/ULS/iS , Continental O-200D |
| Power | 80 – 100 HP |
| Propeller | Propeller 2 or 3 blades adjustable on the ground or in flight |
Fuel tank capacity
| Tank capacity |
80 (120) l / 21.1 (31.7) US gal / 59.5 (89.3) kg / 132 (197) lbs
|
| Endurance |
4,5 (7)h + 30 min reserve
|
| Range |
850 (1250)km/ 460 (675)NM
|
Take-off
| Take-off distance (up to 15 m / 50 ft) | 200 m / 660 ft |
Landing
| Landing distance (from 15 m / 50 ft) | 200 m / 660 ft |
Dimensions
| Wing span | 9,1 m / 29 ft 10 in |
| Length | 6,3 m/ 20 ft 8 in |
| Height | 2,36 m/ 7 ft 8.9 in |
| Wing area | 11,47 m2/ 37 sq ft 7.5 sq in |
| Aspect ratio | 7,8 |
| Cabin width | 1,28 m/ 4 ft 2.4 in |
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