Caudron C.240
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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ArchivoAéreo Editorial Team
A group of aviation researchers and enthusiasts dedicated to documenting and preserving global aeronautical history. All articles are reviewed to ensure historical accuracy.
Sources & Accuracy
The information presented in this technical sheet has been compiled from declassified flight manuals, historical archives, and specialized literature. While we strive for maximum accuracy, some performance data may vary depending on the specific variant or operational conditions.