Swift Aircraft Swift
| Swift | |
|---|---|
| Role | Aerobatic two seat lightplane |
| National origin | United Kingdom |
| Manufacturer | Swift Aircraft |
| First flight | Not yet occurred (February 2012) |
The Swift Aircraft Swift is a
Design and development
Variants
Specifications (Swift II)
Data from Jane's All the World's Aircraft 2011/12[1] Performance estimated.
General characteristics
- Capacity: 2
- Length: 6.565 m (21 ft 6 in)
- Wingspan: 8.055 m (26 ft 5 in) including winglets
- Height: 2.015 m (6 ft 7 in)
- Empty weight: 372 kg (820 lb)
- Max takeoff weight: 743 kg (1,638 lb)
- Fuel capacity: 187 L (49.4 US gal; 41.1 Imp gal)
- Powerplant: 1 × Textron Lycoming air-cooled flat-six engine, 194 kW (260 hp)
- Propellers: 3-bladed MT-Propeller, constant speed
Performance
- Maximum speed: 340 km/h (210 mph, 180 kn)
- Cruise speed: 302 km/h (188 mph, 163 kn) at 75% power
- Stall speed: 93 km/h (58 mph, 50 kn) flaps down
- g limits: +6/-4
- Rate of climb: 10.7 m/s (2,110 ft/min) maximum, at sea level
Avionics
- EFIS.
- Bendix/King IFR.
References
- ^ Jackson, Paul (2011). Jane's All the World's Aircraft 2011-12. Coulsdon, Surrey: IHS Jane's. ISBN 978-0-7106-2955-5.
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