| Category |
Normal |
Utility |
| Load factor (g) |
+3,8 / -1,52 |
+4,4 / -1,76 |
| Takeoff distance (ground roll) |
295 m |
968 ft |
170 m |
558 ft |
| Takeoff distance (over 50 ft obstacle) |
640 m |
2100 ft |
450 m |
1476 ft |
| Max. rate of climb (sea level) |
4,9 m/s |
965 ft/min |
7,4 m/s |
1457 ft/min |
| Max. speed (sea level) |
260 km/h |
140 knots |
266 km/h |
144 knots |
| Cruising speed (2200 RPM, 6000ft) |
243 km/h |
131 knots |
249 km/h |
135 knots |
| Main tanks capacity |
2×61 litres |
2×16,1 gals |
2×61 litres |
2×16,1 gals |
| Auxiliary tanks capacity |
2×51 litres |
2×13,4 gals |
|
|
| Range (2000 RPM, 10000 ft, max. fuel capacity) |
1100 km |
599 NM |
460 km |
248 NM |
| Basic dimensions |
| Wing span |
10,14 m |
33,25 ft |
| Length |
7,58 m |
24,86 ft |
| Height |
2,91 m |
9,55 ft |
| Propeller (constant speed) |
| Manufacturer |
MT Propeller, Germany |
| Type |
MTV-9-B/195-45 (3-blade) |
| Engine |
| Manufacturer |
TEXTRON Lycoming, USA |
| Type |
IO-540-C4D5 |
| Max. power (2400 RPM) |
235 HP |
| Max. cruising power (2200 RPM) |
175 HP |
| Economy cruising power (2000 RPM) |
140 HP |
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