Caudron C.161
The Caudron C.161: A Versatile Aircraft
In 1927, the Caudron company released the C.161, a light multi-purpose aircraft. It was designed for use in sports and for initial training at aero clubs. The C.161 was a two-seater biplane, equipped with a 60 hp Salmson 5Ac engine.
The Evolution: Caudron C.168
In the same year, a modified version of the aircraft, designated Caudron C.168, was released. It differed from its predecessor mainly by featuring a six-cylinder Anzani engine, delivering 70 hp (52 kW).
Success and European Distribution
This C.168 version proved to be quite successful. It was supplied to several European countries, cementing its role as a reliable and effective aircraft in its class.
Technical Specifications
| Modification | C. 161 |
| Wingspan, m | 9.00 |
| Aircraft length, m | 6.45 |
| Aircraft height, m | 2.42 |
| Wing area, m2 | 20.00 |
| Empty weight | 361 |
| Maximum takeoff weight | 584 |
| Engine type | 1 Piston engine Salmson 5Ac |
| Power, hp | 1 x 60 |
| Maximum speed, km/h | 142 |
| Cruising speed, km/h | 115 |
| Service ceiling, m | 3450 |
| Crew | 2 |
Image and diagram gallery of the Caudron C.161
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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.