Technical Characteristics
| Length |
m |
6.90 |
| Height |
m |
2.40 |
| Wing Span |
m |
8.60 |
| Wing Surface |
m2 |
11.80 |
| MTOW |
Kg |
450/550 |
| Landing run |
m |
140 |
| Take off run |
m |
160 |
| Engine |
- |
Rotax 912 UL |
| Power |
HP |
80 |
| Fuel Consumption 75% |
l/h |
15.0 |
| Fuel Capacity |
l |
50 x 2 |
| Stall speed VS (VSo full flaps) |
Km/h |
63 (59) |
| Never exceeded speed VNE |
Km/h |
240 |
| Cruise speed at 75% |
Km/h |
190 |
| Loaf Factor |
g |
+4 / -2 |
|
