|
| SPECIFICATIONS |
DIMENSIONS with folded wings |
|
| Wing span | 9.75 m | |
| Length | 6.45 m | 6.20 m |
| Height | 2.45 m | 1.80 m |
| Cabin width | 1.18 m | 2.46 m |
| Wheelbase | 2.00 m | |
| Wing area | 13.44 m2 | |
| Aspect ratio | 6.6 | |
| Belgian dry empty weight | 257 kg | |
| Max payload | 450 kg | |
| Wing loading factor | 33.48 kg/m2 |
| PERFORMANCE | |||
|
Rotax 912 (80 HP) |
Rotax 912 S (100 HP) |
Rotax 914 T (turbo 115 HP) |
|
|
VNE |
175 Km/h | 185 Km/h | 195 Km/h |
| Cruise speed 75% | 150 Km/h | 160 Km/h | 170 Km/h |
| Stall speed (without flaps) | 55 Km/h | 55 Km/h | 55 Km/h |
| Stall speed (with flaps) | 50 Km/h | 50 Km/h | 50 Km/h |
| Rate of climb | 6 m/s | 8 m/s | 10 m/s |
| Endurance with max payload at cruise speed 75% (5000 rpm) | 5 h | 4 u 30 min | 4 u 30 min |
| Fuel capacity | 87 l | 87 l | 87 l |
| Take-off distance | 40 m | 30 m | 30 m |
| Landing distance | 55 m | 55 m | 55 m |
| Max ceiling | 5000 m | 5000 m | 7000 m |