| DIMENSIONS |
| Length |
7.10 m |
| Height |
2.70 m |
| Wing span |
9.74 m |
| Wing area |
12.28 m2 |
| Capacity of the two fuel tanks |
96 dm3 |
|
| ENGINE |
| Manufacturer |
PZL |
| Model |
F.4A-235B 3 |
| Rating |
90kW (125 HP) |
| Number of Cylinders |
4 |
|
| PROPELLER |
| Manufacturer |
PZL |
| Model |
US 135000 PZL |
| Number of Blades |
2 |
| Type |
Fixed-pitch metal |
|
| MASSES |
| Max. certified mass in normal category |
850 kgs |
| Max. mass in utility category |
770 kgs/750 kgs |
| Mass empty |
525 kgs |
|
| PERFORMANCE |
| T.O. mass 850 kgs, standard atmosphere conditions, S. L. |
| Never exceed speed VNE |
250 km/h |
| Normal operating speed VNO |
195 km/h |
| Stall speed (flaps down) |
80 km/h |
| Rate of climb 2.85 |
m/s |
| Service ceiling |
3200 m |
| Range |
680 km |
| T.O. length to clear 15 m |
260 m |
| Landing length from 15 m |
270 m |
