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Revision as of 09:13, 18 July 2011
| Twin-R | |
|---|---|
| Role | Four seat twin engine kitbuilt |
| Manufacturer | Dyn'Aéro |
| Designer | Piérre and Christophe Robin |
| First flight | 3 March 2011 |
| Developed from | Dyn'Aéro MCR4S |
The Dyn'Aéro Twin-R is
Design and development
The Twin-R flew for the first time on 3 March 2011 piloted by Christian Briand.[1]
Specifications (kitbuilt)
Data from Jane's All the World's Aircraft 2011/12[2]
General characteristics
- Capacity: 4
- Length: 7.10 m (23 ft 4 in)
- Wingspan: 9.24 m (30 ft 4 in)
- Height: 1.90 m (6 ft 3 in)
- Wing area: 8.60 m2 (92.6 sq ft)
- Empty weight: 425 kg (937 lb)
- Max takeoff weight: 950 kg (2,094 lb)
- Fuel capacity: 110 L (24.2 Imp gal, 29.1 US gal) standard. Can be increased to 200 L (44 Imp gal, 52.8 US) gal
- Powerplant: 2 × Rotax 912ULS flat four, air and water cooled piston, 73.5 kW (98.6 hp) each
- Propellers: 2-bladed
Performance
- Maximum speed: 335 km/h (208 mph, 181 kn)
- Cruise speed: 326 km/h (203 mph, 176 kn) normal, at 75% power at 2,438 m (8,000 ft)
- Stall speed: 92 km/h (57 mph, 50 kn) flaps down
- Range: 2,129 km (1,323 mi, 1,150 nmi) with maximum fuel
- Rate of climb: 7.6 m/s (1,500 ft/min)
Avionics
Dyson Skyview 3-screen EFIS recommended
References
- ^ "First flight of Twin-R". Retrieved 2011-07-17.
- ^ Jackson, Paul (2011). Jane's All the World's Aircraft 2011-12. Redhill, UK: IHS Jane's. p. 201. ISBN 978-0-7106-2955-5.
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