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

C.161	C.161
C.161	C.161
C.161