|
|
Performance
| Performance |
|
Rotax 912 UL |
| Max allowed speed VNE |
|
230 km/h |
124 kts |
| Stall speed (450 kg) |
|
65 km/h |
35 kts |
| Rate of climb (450 kg) |
|
4,6 m/s |
900 fpm |
| Take-off run from runway (450 kg) |
|
191 m |
| Landing run to runway |
|
65 m |
| Fuel tanks |
|
85 liters |
Cruise performance
| with engine |
|
Rotax 912 UL |
| rpm |
|
4400 |
4600 |
4800 |
5000 |
5200 |
5400 |
|
calibrated airspeed [CAS] |
|
149 km/h |
156 km/h |
163 km/h |
170 km/h |
177 km/h |
184 km/h |
| with engine |
|
Rotax 912 ULS |
| rpm |
|
4400 |
4600 |
4800 |
5000 |
5200 |
5400 |
| calibrated airspeed [CAS] |
|
157 km/h |
164 km/h |
171 km/h |
178 km/h |
185 km/h |
192 km/h |
With engine 912 UL
| with engine |
|
Rotax 912 UL |
| Cruise speed |
|
140 km/h |
150 km/h |
160 km/h |
170 km/h |
179 km/h |
|
|
76 kts |
81 kts |
86 kts |
92 kts |
97 kts |
| consumption |
|
12,0 l/h |
13,0 l/h |
14,1 l/h |
15,3 l/h |
16,4 l/h |
| endurance |
|
7 t 5 min |
6 t 32 min |
6 t 2 min |
5 t 34 min |
5 t 10 min |
| range |
|
992 km |
980 km |
964 km |
945 km |
925 km |
|
|
|
in finnish