|
General Data
|
| Crew |
2 |
| Height |
2.7 m |
| Length |
7.745 m |
| Wing span |
9.3 m |
| Wing area |
15 sq. m |
| Dihedral |
2 degrees |
| Wing incidence |
2 degrees |
| Propeller diameter |
2.4 m (V530TA-D35 constant speed propeller) |
| Wheel track |
2.715 m |
| Engine |
M-14P, 360 hp, 9 cylinder radial |
|
Weights, Fuel & Oil
|
| Dry weight |
1035 kg |
| Maximum takeoff weight |
1315 kg |
| Maximum landing weight |
1315 kg |
| Weight of crew with parachutes |
180 kg |
| Fuel weight |
90 kg |
| Oil weight |
10 kg |
| Maximum fuel load |
120 L |
| Maximum oil load |
16 L |
| C of G limits (%) |
17.5 - 27.0 |
|
Performance
|
| Maximum level airspeed (at altitude 1000 m) |
270 km/h |
| Range (10% fuel reserve at 190 km/h) |
465 km (2 h 30 min) |
| Takeoff roll |
180 - 200 m |
| Landing roll |
330 m |
| Stall speed, engine at idle - erect flight, clean |
120 km/h |
| Stall speed, engine at idle - flaps, gear down |
110 km/h |
| Stall speed, engine at idle - inverted |
150 km/h |
| Approach speed |
160 km/h |
| Touchdown speed |
115 - 120 km/h |
| Takeoff speed |
120 km/h |
| Climb speed |
170 km/h |
| Maximum ceiling (no oxygen equipment fitted) |
4000 m |
|
Limitations
|
| Never exceed speed (VNE) |
420 km/h |
| Maximum manoeuvring speed |
360 km/h |
| G limits |
+7/-5 |
| Maximum gear extended speed |
200 km/h |
| Maximum flaps extended speed |
170 km/h |
| Minimum fuel qty for aerobatics |
24 L |
| Maximum inverted flight time |
2 min (followed by at least 3 min of erect flight) |
| Maximum oil load for cross-country |
16 L |
| Maximum oil load for aerobatics |
10 L |
| Minimum oil load |
8 L |
