DIMENSIONS
| Wing span |
8.3 m |
| Length |
5.69 m |
| Height |
2.05 m |
AIRSPEED
| Maximum permissible operating flight speed |
240 km/h |
| Maximum cruising speed |
210 km/h |
| Maximum maneuvering speed |
170 km/h |
MAXIMUM PERMISSIBLE WIND SPEED
AND WEATHER MINIMUM
| Head wind during takeoff and landing |
15 m/s |
| Tail wind during takeoff and landing |
5 m/s |
| Cross-wind component at right angle to runway |
8 m/s
|
| Cloud ceiling, at least |
150 m |
| Horizontal visibility, at least |
3000 m |
ENGINE, BRIEF DESCRIPTION
| Engine manufacturer |
BOMBARDIER-ROTAX (Austria) |
| Type of engine |
four-stroke, with four opposed cylinders |
| Make of engine |
ROTAX-912ULS |
| Cooling |
composite water-air |
| Engine power, hp (kW): |
|
- maximum takeoff |
100 (73,9) at crankshaft rotation frequency of 5800 rpm |
|
- nominal |
93 (69) at CS rotation frequency of 5500 rpm |
|
- in cruising mode |
68,5 (51) at CS rotation frequency of 5000 rpm |
LIMITATIONS
| Maximum takeoff weight |
730 kg |
| Maximum landing weight |
730 kg |
| Maximum payload |
219,9 kg |
| Maximum aircraft operational empty weight |
510,1 kg |
| Fuel tank capacity |
100 L |
| Takeoff run |
220 m |
| Flight range |
900 km |
ENGINE CONTROL UNIT MARKING
Integrated engine control electronic device “FLYdat” with digital display is mounted in the aircraft. This device has no special marking. Should any parameter exceeds permissible limits, a respective display starts blinking and “FLYdat” warning annunciator turns on.
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