Caudron C.240
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| C.240 | |
|---|---|
| Role | Touring |
| Manufacturer | Caudron |
| Designer | Paul Deville |
| First flight | 1931 |
| Produced | 1931 |
| Number built | 1 |
The Caudron C.240 was a four-seat touring aircraft produced in France in 1931. It was a single-engined, low-wing, cantilever monoplane constructed using wood and metal.
Caudron were unable to find customers for this aircraft so further development was abandoned.
Specifications (C.240)
General characteristics
- Crew: One pilot
- Capacity: 3 passenger
- Length: 10.05 m (32 ft 11.7 in)
- Wingspan: 15.00 m (49 ft 2.6 in)
- Height: 3.00 m (9 ft 10 in)
- Wing area: 32.80 m2 (353.06 ft2)
- Empty weight: 800 kg (1760 lb)
- Gross weight: 1300 kg (2860 lb)
- Powerplant: 1 × Salmson 9Ac, 89.5 kW (120 hp)
Performance
- Maximum speed: 165 km/h (103 mph)
- Range: 650 km (406 miles)
- Service ceiling: 3,500 m (11,500 ft)
References
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Wikimedia Commons has media related to Caudron aircraft. |
