| Maximal horizontal flight speed |
158 km/h |
| Cruise speed |
125 km/h |
| Rate of climb near ground |
4 m/s |
| Service ceiling |
4000 m |
| |
| Liftoff speed |
65 km/h |
| Landing speed |
60 km/h |
| Takeoff run |
50 m |
| Landing run |
30 m |
| |
| Maximum take-off weight |
450 kg |
| Maximum overloads |
+4.4/-2.2 |
| Maximum operational speed (not exceeded) |
180 km/h |
| Maximal maneuvering speed |
159 km/h |
| Stalling speed (In landing configuration) |
57 km/h |
| Baking at turns |
45° |
| Allowable windspeed |
| head |
12 km/s |
| side (45°) |
7 M/c |
| side (90°) |
5 km/s |
| |
| Volume of fuselage fuel tank (main) |
40 liters |
| Volume of wing fuel tanks |
50 liters |
| Hourly fuel consumption |
| at take-off |
14-17 liters/hour |
| at cruise |
11-15 liters/hour |
