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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