TECHNICAL DATA
| SPEEDS |
KILOMETERS |
KNOTS |
MILES |
| Never exceed speed (VNE) |
260 km/h |
140 knots |
162 mph |
| Cruise speed @ 75% power (Vc) |
195 km/h |
105 knots |
122 mph |
| Maneuvering speed (VA) |
142 km/h |
77 knots |
88 mph |
| Min. speed without lift flaps (VS1) |
65 km/h |
35 knots |
40 mph |
| Min. speed with lift flaps (VS0) |
58 km/h |
31 knots |
36 mph |
| WEIGHT |
|
| Max. take-off weight |
UL/ LSA up to 580 kg / 1278 lbs. |
| Basic empty weight |
311 kg / 686 lbs. |
| ENGINE & PROPELLER |
|
| Engine type |
Rotax® 912 UL, ULS ; 914 UL ; 912iS fuel injection |
| Maximum power |
80HP – 115HP turbocharged |
| Propeller |
2 or 3 blade – on the ground or in flight adjustable |
| FUEL CAPACITY & ENDURANCE |
|
| Fuel capacity |
64 L / 16.9 US gal / 102 lbs / 46 kg |
| with additional tanks |
90 L / 23.8 US gal / 143 lbs / 67 kg |
| Endurance |
4.5+0.5h (standard) / 6.5+0.5h (additional tanks) |
| Range |
810 km / 430 nm / 500 miles (standard) /
1100 km / 590 nm / 680 miles (w/ additional tanks) |
| TAKE-OFF & LANDING |
|
| Take-off distance |
185-200 m / 600 – 660 ft |
| Take-off run |
90-100 m / 300 – 330 ft |
| Landing distance |
200 m / 660 ft |
| Landing run |
100 m / 330 ft |
| DIMENSIONS |
|
| Wing span |
9.9 m / 32 ft 5,5 in |
| Overall length |
7.0 m / 23 ft 7.5 in |
| Overall height |
2.6 m / 7 ft 2.6 in |
| Wing area |
11.85 m2 / 127.5 sq. ft |
| Aspect ration |
7.78 |
| Cabin width |
1.18 m / 3ft 10.5 in |
*Values depending on the aircraft configuration
PHOTOGALLERY
