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Click here to View the Rotax 914 engine Spec sheet in PDF Format |
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Technical |
| Tare Mass |
245 kg |
| MTOW |
550 kg |
| Total Payload |
305 kg |
| Engine |
Rotax 914 Turbo |
| Rotor |
Composite |
| Trim |
Electro Pneumatic |
| Main Landing Gear |
Composite material |
| Endurance |
+/- 4 hrs |
Brakes |
Hydraulic disc brakes
with parking brake |
| Performance |
| Max Speed (VNE) |
180 Kmh (112 Mph) |
Minimum Speed (Pilot only)
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30 Kmh (18 Mph) |
| Climb rate |
Full Load 1500 ft/min |
| Fuel consumption |
Pilot Only +/- 15 L/hr at 115 Km/h (70 mph) |
| Take-off distance: Full Load Full Load |
+/- 50 Meter
(wind and surface dependant) |
| Rotor Head |
ELA with integrated parking brake,
pre-rotator & trim |
Propeller
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Carbon Fiber |
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