Caudron C.720
Development and Purpose
The Caudron C.720 was an advanced training aircraft, developed by the French firm Caudron. It was specifically designed to prepare fighter pilots, providing them with a dedicated platform to hone their flying skills.
First Flight and Cancellation
The prototype’s maiden flight occurred in January 1936. Despite exhibiting promising flight characteristics, the C.720 project was ultimately discontinued. The company opted to prioritize the development of a more advanced and superior model, the Caudron C.690, focusing resources on that design instead.
Technical Specifications
| Modification | C.720 |
| Wingspan, m | 7.67 |
| Length, m | 7.93 |
| Height, m | 2.60 |
| Wing area, m2 | 9.00 |
| Empty weight | 657 |
| Maximum takeoff weight | 844 |
| Engine type | 1 Piston engine Renault 4Pei |
| Power, hp | 1 x 155 |
| Maximum speed, km/h | 292 |
| Cruising speed, km/h | 258 |
| Practical range, km | 750 |
| Practical ceiling, m | 6500 |
| Crew, crew members | 1 |
Image and diagram gallery of the Caudron C.720
 Caudron C.720 |
 Caudron C.720 |
 Caudron C.720 |
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.