|
Engine group |
|
|
|
Engine |
|
Rotax 912 ULS2 with 100HP |
|
Propeller |
|
Carbon propeller (adjustable on the ground) |
|
Fuel pump |
|
Auxiliary electrical fuel pump |
|
|
|
|
Performances |
|
|
|
VNO |
|
232km/h
|
|
VNE |
|
250km/h (Speed never to exceed) |
|
VC |
|
215km/h (at 75% power setting) |
|
VB |
|
209km/h |
|
VFE |
|
120km/h (Max. with full flaps) |
|
VS |
|
65km/h |
|
VR |
|
75km/h with 15° flaps |
|
VREF |
|
90km/h with 40° flaps – Landing at 65km/h |
|
Rate
of climb |
|
6.2m/s with 0° flaps, 110 km/h and 472.5kg total weight |
|
Takeoff distance |
|
120m |
|
Landing distance |
|
160m |
|
Range |
|
~1200km |