Caudron C.67
The Caudron C.67: Origins and Design
In the spring of 1922, the Caudron company, under Paul Deville’s innovative design, completed the construction of the Caudron C.67, a light sport aircraft. This model was configured as an elegant single-seat, single-strut biplane, powered by a three-cylinder Anzani air-cooled engine producing 25 hp (19 kW).
Performance and Public Appearances
Throughout 1922, the Caudron C.67 distinguished itself through active participation in various demonstration flights, where it impressed audiences with the execution of complex aerobatic maneuvers. Concluding a busy year, the aircraft was prominently displayed at the prestigious Paris Air Show, capturing significant attention.
A Unique Prototype Without Production
Despite its excellent flight characteristics and the interest generated at exhibitions, the Caudron C.67 failed to secure orders for series production. As a result, this advanced sport biplane remained a single prototype, solidifying its status as an exclusive and unique aircraft in aviation history.
Technical Specifications
| Modification | C.67 |
| Wingspan, m | 7.30 |
| Length, m | 5.80 |
| Height, m | 2.40 |
| Wing area, m2 | 14.00 |
| Empty weight | 210 |
| Maximum takeoff weight | 324 |
| Engine type | 1 Piston engine Anzani |
| Power, hp | 1 x 25 |
| Maximum speed, km/h | 95 |
| Cruising speed, km/h | 75 |
| Service ceiling, m | 1300 |
| Crew | 1 |
Image and diagram gallery of the Caudron C.67
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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.