Development and Design
In 1933, Aeronautica Caproni built the Ca.125, a light multi-purpose aircraft intended to replace the veteran Ca.100. This project resulted in a two-seater, single-strut biplane of mixed construction.
Technical Specifications
The Ca.125 was equipped with a 135 hp six-cylinder air-cooled Colombo S.63 engine. Its versatile design allowed the aircraft to be used for both training and touring purposes.
Variants and Production
Only two examples of the Ca.125 were produced: a land-based version and a floatplane variant. These aircraft showcased Caproni’s commitment to innovation in the light aviation sector.
Technical Specifications
| Modification | Ca. 125 |
| Upper wingspan, m | 8.85 |
| Aircraft length, m | 7.25 |
| Aircraft height, m | 2.55 |
| Wing area, m2 | 19.00 |
| Empty weight | 545 |
| Maximum takeoff weight | 815 |
| Engine type | 1 Piston engine Colombo S.63 |
| Power, hp | 1 x 135 |
| Maximum speed, km/h | 220 |
| Cruising speed, km/h | 185 |
| Practical range, km | 900 |
| Service ceiling, m | 5500 |
| Crew | 2 |
Image gallery of the Ca.125
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