Caudron C.240

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

Wikimedia Commons has media related to Caudron aircraft.

• aviafrance.com
• Уголок неба