DIMENSIONS
| Wing span, m (ft) |
9.8 (32.14) |
| Length, m (ft) |
5.96 (19.54) |
| Height, m (ft) |
2.92 (9.57) |
PILOT’S COCKPIT
| Length, m (ft) |
4.84 (15.87) |
| Width, m (ft) |
1.22 (4) |
| Height, m (ft) |
1.25 (4.1) |
| Number of seats |
2 pers. |
AIRSPEED
| Maximum permissible operating flight speed, km/h (mph) |
240 (149) |
| Maximum cruising speed, km/h (mph) |
210 (130) |
| Maximum maneuvering speed, km/h (mph) |
170 (105) |
| Minimum permissible speed |
| - flaps retracted, knots (mph) |
59 (68) |
| - flaps extended by 20°, knots (mph) |
54 (62) |
| - flaps extended by 40°, knots (mph) |
49 (56) |
STALLING SPEED
| Vso (in landing configuration), knots (mph) |
41 (47) |
| Vs1 (in take off configuration), knots (mph) |
43 (50) |
| Vs (in cruise configuration), knots (mph) |
45 (53) |
MAXIMUM PERMISSIBLE WIND SPEED
AND WEATHER MINIMUM
| Head wind during takeoff and landing, m/s (mph) |
10 (22) |
| Tail wind during takeoff and landing, m/s (mph) |
5 (11) |
| Cross-wind component at the angle of 90 to runway, m/s (mph) |
6 (13,2) |
| Cloud ceiling, at least, m (ft) |
150 (492) |
| Horizontal visibility, at least, m (ft) |
3000 (9840) |
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, kg (lbs) |
600 (1320) |
| Maximum landing weight, kg (lbs) |
600 (1320) |
| Maximum payload, kg (lbs) |
216,5 (477) |
| Aircraft operational weight, kg (lbs) |
336 (739,2) |
| Empty weight, kg (lbs) |
350 (770) |
| Maximum aircraft operational empty weight, kg (lbs) |
383,5 (845) |
| Gas type |
Auto gas, premium |
| Fuel tank capacity, L (Gal) |
65 (17.1) |
| Takeoff run, m (ft) |
70 (230) |
| Flight range, km (mile) |
650 (404) |
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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