Spécifications techniques
The VUT100 Cobra is a light, multi-purpose, all-metal airplane of the new generation.
The airplane is designed for:
- touring and sport/pleasure flying
- basic and advanced training of private and military pilots
- night flight and instrument flight training
- private and business travelling
- aero-towing and other special purposes
- general commercial use
Technical data
| Model | VUT100-120i | VUT100-131i |
| General dimensions | ||
| Length | 26.3 ft (8 m) | |
| Wing span | 33.5 ft (10.2 m) | |
| Internal dimension | ||
| Cabin length | 122 in (3.1 m) | |
| Cabin width | 51.5 in (1.31 m) | |
| Cabin height | 48 in (1.22 m) | |
| Seats | 4 | |
| Powerplant | ||
| Engine | Lycoming IO-360-A1B6 | Lycoming IO-580-B1A |
| Power | 200 hp | 315 hp |
| Propeller | Hartzell HC-F3YR-1RF | Hartzell HC-F3YR-1RF |
| Diameter | 74 in (188 cm) | 76 in (193 cm) |
| Type | 3 blade, constant speed | |
| Weights | ||
| Max. take-off | 2,930 lb (1,330 kg) | 3,200 lb (1,450 kg) |
| Useful load | 1,105 lb (500 kg) | 1,260 lb (570 kg) |
| Fuel - usable | 90U.S.galls (340 litres) | |
| Load factors | +3.8g -1.52g (Normal category airplane) / +4.4g -1.76g (Utility category airplane) |
|
| Performance | ||
| Max. level speed | 155 kts (287 km/h) | 175 kts (324 km/h) |
| Max. rate of climb | 1,000 fpm (5 m/s) | |
| Stall speed | 50 kts (93 km) | 55 kts (103 km) |
| Range | 1,080 nm (2,000 km) | 1,000 nm (1,830 km) |
| Endurance | 8 hours | 6 hours |
| All data in this table is preliminary and may be changed any time without notice. | ||
Range diagram
