Caudron C.183
In 1925, the Caudron firm released the C.183 transport aircraft. It was a modification of the C.81, sharing the same wingspan but being 1.1 meters longer and 60 kg heavier. This development aimed to improve upon its predecessor’s capabilities.
Origin and Development of the Caudron C.183
Its powerplant also differed significantly from the C.81. Instead of the nose-mounted Lorraine-Dietrich 12Db engine, a more powerful Salmson CM19 (550 hp) was used. Despite this increased engine power, its passenger capacity and flight characteristics remained at approximately the same level as the C.81.
Limited Production and Legacy
Consequently, only a single unit of the C.183 was ever produced. Its registration number, F-ESAI, was inherited directly from the C.81, highlighting its limited production run and close lineage to the earlier model.
Technical Specifications
| Modification | C.183 |
| Wingspan, m | 26.30 |
| Aircraft length, m | 17.10 |
| Aircraft height, m | 4.85 |
| Wing area, m2 | 145.00 |
| Empty weight | 4223 |
| Maximum takeoff weight | 6430 |
| Engine type | 1 Piston engine Salmson CM19 + 2 Piston engines Salmson CM.9 |
| Power, hp | 1 x 550 + 2 x 260 |
| Maximum speed, km/h | 145 |
| Cruising speed, km/h | 139 |
| Practical range, km | 450 |
| Practical ceiling, m | 3750 |
| Crew | 2 crew |
| Payload | up to 7 passengers |
Image and diagram gallery of the Caudron C.183
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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.