C.400 Phalene
In 1934, l’Armée de l’Air ordered a light utility aircraft from the Caudron firm. The C.400 Phalene was released that same year based on this order. It was a modification of the C.282/8 Phalene aircraft.
Development and Initial Production
A total of 40 aircraft were built. Later, 29 of these planes were transferred by the military for civilian use, highlighting their versatility and adaptability beyond military operations.
Later Use and Modifications
In the post-war years, several C.400 aircraft were modified under the designation C.401. These modifications extended their operational life and usefulness in civilian aviation.
Technical Specifications
| Modification | C. 400 |
| Wingspan, m | 11.62 |
| Aircraft length, m | 8.46 |
| Aircraft height, m | 2.20 |
| Wing area, m2 | 23.20 |
| Empty weight | 590 |
| Maximum takeoff weight | 950 |
| Engine type | 1 Piston engine Renault 4Pdi |
| Power, hp | 1 x 120 |
| Maximum speed, km/h | 185 |
| Cruising speed, km/h | 155 |
| Practical range, km | 650 |
| Service ceiling, m | 4250 |
| Crew, crew members | 1 |
| Payload: | up to 3 passengers |
Image and diagram gallery of the C.400 Phalene
 C.400 Phalene |
 C.400 Phalene |
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.