 |
 |
| Engine |
ROTAX-912ULS2 |
| Engine power, h.p. |
97 |
| Maximum take-off weigh, kg |
540 |
| Maximum fuel weight, kg |
37 |
| Maximum speed, km/h |
122 |
| Lift-off speed, km/h |
79 |
| Landing speed, km/h |
72 |
| Maximum rate of climb, m/s |
2,5 |
| Take-off run, m |
95 |
| Landing roll, m |
135 |
| Service ceiling, m |
2200 |
| Head wind at take-off and landing, m/s |
10 |
| Crosswind at take-off, m/s |
6 |
| Flight elapsed time, h |
3 |
|
AVIATIKA-MAI-890U
