Development and Design
In the early 1930s, the Caudron company proactively developed the C.240, a light multi-purpose aircraft. Its chief designer was Paul Deville, who spearheaded this ambitious initiative.
Technical Specifications
The C.240 was a four-seat, low-wing monoplane. It featured a mixed construction and was powered by a single Salmson 9Ac engine, capable of producing 120 horsepower.
Limited Production
Despite its innovative design and multi-purpose capabilities, Caudron unfortunately failed to secure any customers for the aircraft. As a result, only one prototype of the C.240 was ever built, remaining a unique example.
Technical Specifications
| Modification | С.2 40 |
| Wingspan, m | 15.00 |
| Length, m | 10.05 |
| Height, m | 3.00 |
| Wing area, m2 | 32.80 |
| Empty weight | 800 |
| Maximum takeoff weight | 1300 |
| Engine type | 1 Piston engine Salmson 9Ac |
| Power, hp | 1 x 120 |
| Maximum speed, km/h | 165 |
| Cruising speed, km/h | 145 |
| Practical range, km | 650 |
| Service ceiling, m | 3500 |
| Crew | 1 crew member |
| Payload | up to 3 passengers |
Image and diagram gallery of the Caudron C.240
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VANCOUVER: Caudron C.240 [online]. wp.archivoaereo.com; [cited 2026-07-07]. Available at: https://wp.archivoaereo.com/en/caudron-c-240-2/