 |
 |
| Engine |
ROTAX-912A |
| Engine power, h.p. |
80 |
| Maximum take-off weigh, kg |
540 |
| Maximum fuel weight, kg |
37 |
| Maximum speed, km/h |
130 |
| Lift-off speed, km/h |
70 |
| Landing speed, km/h |
70 |
| Maximum rate of climb, m/s |
3,65 |
| Take-off run, m |
85 |
| Landing roll, m |
100 |
| Service ceiling, m |
3800 |
| Head wind at take-off and landing, m/s |
10 |
| Crosswind at take-off, m/s |
6 |
| Flight elapsed time |
2hrs 40min |
|
AVIATIKA-MAI-890
