Cruise speed
90 km/h
consommation
9 l/h
Max load
462 kg
Max glide
8.5
Cruise speed
90 km/h
Max speed
130 km/h
Power
100 hp
Max Load
462 kg
Max speed
130 km/h
Cruise speed
90 km/h
Power
100 hp
Autonomy
6h15
Accessible Performance
The NuviX & Skypper evo system optimized for medium-power engines and equipped with the CORSET system, is particularly maneuverable and enjoyable at any chosen speed. It will adapt to all situations, from training to daily flights.
Add to this a large payload capacity and low fuel consumption, and the NuviX & Skypper evo combination is perfect for all your adventures.
Again, on the front of the stage, the Skypper produced has more than 500 copies since 2011 gets an improvement in evo version.
While retaining its sporting and recreational character, it is intended for "pleasure flight", training center, competition, travel, etc.
The Skypper evo further optimizes the comfort, safety and design of its predecessor.
- Reinforcement of the front axle
- Three-wheel brake
- Carbon Fiber SPRADLING upholstery
- Central bag
- Rear seat box
- Resized Dashboard
- New instruments
- Removable fairing
- Optional Rotax 912 iS
With or without fairing, enjoy the light, easy-to-use, compact & economical tandem!
Developed specifically to provide a modern wing for the early generations of Skypper and earlier trikes, the NuviX inherits some of the technologies of its predecessor, the BioniX. This 15m² variable configuration wing is equipped with the Corset© system and a structure similar to that of the BioniX. The most accessible of the Corset© wings is optimized for extreme maneuverability at low speeds.
- CORSET®
- Trilam UV-Stop fabric
- Leading edge in "Lite Skin®" fabric
- 90% double surface
The NuviX is the most cost-effective of the variable configuration wings. Versatile, modern, and high-performing, it is ideal for medium-power engines (60 to 80 HP) and can be adapted to Air Création trikes in the GTE range.
Rotax 912
| Max Speed (level) | 120 km/h |
| Cruising Speed | 90 km/h |
| Stall Speed | 61 km/h |
| Speed not to exceed | 163 km/h |
| Max Speed (not to exceed in very turbulent air) | 122 km/h |
| Max glide speed | 80 km/h |
| Max glide ratio | 8.5 |
* in two-seater, onboard load 180 kg
| Rate of climb | 5 m/s |
| Take-off distance | 85 m |
| Passage of 15 m | 210 m |
| Landing distance | 50 m |
| Passage of 15 m | 150 m |
* in two-seater, onboard load 180 kg
| Height | 3 m |
| Wingspan | 10 m |
| Lenght | 3 m |
| Wing area | 15 m² |
| Profile type | 90% |
| Ability | 2 |
| Empty weight | 229 kg |
| Maximum mass | 462 kg |
| Payload | 233 kg |
| Engine | Rotax 912 UL |
| Power | 80 hp |
| Propeller | Helix H50 F |
| Reduction | 2,43:1 |
| Tank capacity | 55 l |
| Consumption | 9 l/h |
| Autonomy | 6h |
* in two-seater, onboard load 180 kg
Rotax 912 S
| Max Speed (level) | 130 km/h |
| Cruising Speed | 90 km/h |
| Stall Speed | 61 km/h |
| Speed not to exceed | 163 km/h |
| Max Speed (not to exceed in very turbulent air) | 122 km/h |
| Max glide speed | 80 km/h |
| Max glide ratio | 8.5 |
* in two-seater, onboard load 180 kg
| Rate of climb | 6 m/s |
| Take-off distance | 75 m |
| Passage of 15 m | 180 m |
| Landing distance | 50 m |
| Passage of 15 m | 150 m |
* in two-seater, onboard load 180 kg
| Height | 3 m |
| Wingspan | 10 m |
| Lenght | 3 m |
| Wing area | 15 m² |
| Profile type | 90% |
| Ability | 2 |
| Empty weight | 231 kg |
| Maximum mass | 462 kg |
| Payload | 231 kg |
| Engine | Rotax 912 ULD |
| Power | 100 hp |
| Propeller | Helix H50 F |
| Reduction | 2,43:1 |
| Tank capacity | 55 l |
| Consumption | 9 l/h |
| Autonomy | 6h |
* in two-seater, onboard load 180 kg
Rotax 912 iS
| Max Speed (level) | 130 km/h |
| Cruising Speed | 90 km/h |
| Stall Speed | 61 km/h |
| Speed not to exceed | 163 km/h |
| Max Speed (not to exceed in very turbulent air) | 122 km/h |
| Max glide speed | 80 km/h |
| Max glide ratio | 8.5 |
* in two-seater, onboard load 180 kg
| Rate of climb | 6 m/s |
| Take-off distance | 75 m |
| Passage of 15 m | 180 m |
| Landing distance | 50 m |
| Passage of 15 m | 150 m |
* in two-seater, onboard load 180 kg
| Height | 3 m |
| Wingspan | 10 m |
| Lenght | 3 m |
| Wing area | 15 m² |
| Profile type | 90% |
| Ability | 2 |
| Empty weight | 235 kg |
| Maximum mass | 462 kg |
| Payload | 227 kg |
| Engine | Rotax 912 iS |
| Power | 100 hp |
| Propeller | Helix H50 F |
| Reduction | 2,43:1 |
| Tank capacity | 55 l |
| Consumption | 8,5 l/h |
| Autonomy | 6h15 |
* in two-seater, onboard load 180 kg
Dimensions
