ULM
Travair
Produits
Services
Rally
|
GENERAL
| Engine | Rotax 912 ULS100 bhp @ 5800rpm (5 min max) 95 bhp@ 5500rpm (continuous) | |
| Propeller | 3 Blades variable pitch inflight (IVOPROP - USA) | |
| Fuel capacity | 1 tank in each wing total 134 lit ; usable 130 lit | |
| Weights | mtow 450 kg empty dry254 kg max useful 196 kg max in baggagespace 20kg | |
| wing loading | 38,75 kg / m² v power loading | 4.5 kg/hp |
AIRSPEED
| Vne | 250 km/h |
| Vno | 240 km/h |
| Maneuvering | 180 km/h |
| Vfe | 110 km/h |
|
Cruise 75 % ( 2000 ft ,ISA conditions) |
210 km/autonomie 1520 km |
| Vso | 57 km/h |
| Rate of climb at sea level | 1200 ft/min |
| Service ceiling | 12000 ft |
TAKE OFF (sea level , ISA conditions)
| Ground roll | 90 m |
| 50 ft obstacle clearance | 180 m |
LANDING (sea level , ISA conditions)
| Ground roll | 110 m |
| 50 ft obstacle clearance | 330 m |
DIMENSIONS
| Length | 7.08 m |
| Height | 2.31 m |
| Wing span | 9.00 m |
| Cabin width | 1.16 m |