C.140
Development and Origin
The C.140 was a reconnaissance aircraft developed by the French firm Caudron. This aircraft was built specifically under commission from the Aviation Ministry.
Presentation and Outcome
It was first presented in February 1928. However, following the completion of trials, the military declined to place an order for this aircraft.
Technical Specifications
| Modification | C. 140 |
| Wingspan, m | 11.30 |
| Length, m | 7.84 |
| Height, m | 3.20 |
| Wing area, m2 | 28.00 |
| Empty weight | 896 |
| Maximum takeoff weight | 1300 |
| Engine type | 1 Piston engine Salmson 9 |
| Power, hp | 1 x 260 |
| Maximum speed, km/h | 185 |
| Cruising speed, km/h | 151 |
| Practical range, km | 560 |
| Practical ceiling, m | 5000 |
| Crew, crew members | 2 |
Image and diagram gallery of the C.140
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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.