In the late 1920s, Paul Deville, a designer at Société des Avions Caudron, developed the Caudron C.180 transport aircraft project. This innovative aircraft was intended for use in French colonies, reflecting an ambitious vision for colonial aviation of that era.
Development and Design of the Caudron C.180
The Caudron C.180 was envisioned as a twelve-seater, all-metal, cantilever high-wing monoplane. It was powered by three nine-cylinder Lorraine 9Na Algol engines, each delivering 300 hp, providing substantial capability for its intended transport missions.
Operational History and Variants
The sole prototype of the aircraft was built in 1930 and showcased at the Paris Air Show in December of the same year. Despite its advanced design, the Caudron C.180 did not receive any orders. Subsequently, a similar aircraft, the Caudron C.181, was manufactured, equipped with three Gnone et Rhone K-7 engines of the same power.
Technical Specifications
| Modification | C.180 |
| Wingspan, m | 24. 50 |
| Length, m | 15. 13 |
| Height, m | 3. 78 |
| Wing area, m2 | 70.00 |
| Empty weight | 2600 |
| Maximum takeoff weight | 5000 |
| Engine type | 3 Piston engine Lorraine 9Na Algol |
| Power, hp | 3 x 300 |
| Maximum speed, km/h | 225 |
| Cruising speed, km/h | 195 |
| Practical range, km | 1000 |
| Service ceiling, m | 3450 |
| Crew, crew members | 2 |
| Payload | up to 10 passengers |
Image and diagram gallery of the Caudron C.180
 C.180 |
 C.180 |
 C.180 |
 C.180 |
 C.180 |