Auguste Mudry established Avions Mudry et Cie in Bern in 1958. The company’s first (and most successful) project was the two-seater light aerobatic aircraft, the Mudry CAP.10 B, which could also be used for sports or training purposes.
Innovative Design and Features
This aircraft was a cantilever low-wing monoplane featuring a wooden frame and a mixed plywood-and-fabric skin. The production variant was equipped with a four-cylinder Avco Lycoming AEIO-360-B2F piston engine.
Operational History and Production
The CAP.10 prototype first took to the air in August 1968 (the CAP.10 B aircraft differed with a redesigned tail). By early 1992, a total of 260 machines had been built. Almost half of them were intended for military customers.
Technical Specifications
| Modification | CAP 10 |
| Wingspan, m | 8.06 |
| Length, m | 7.16 |
| Height, m | 2.55 |
| Wing area, m2 | 10.85 |
| Empty weight | 550 |
| Normal takeoff weight | 760 |
| Maximum takeoff weight | 830 |
| Fuel capacity, l | 108 |
| Engine type | 1 Piston engine Textron Lycoming AEIO-360-B2F |
| Power, hp | 1 x 180 |
| Maximum speed at altitude, km/h | 340 |
| Maximum speed at sea level, km/h | 270 |
| Cruising speed, km/h | 250 |
| Practical range, km | 1000 |
| Maximum rate of climb, m/min | 480 |
| Practical ceiling, m | 5000 |
| Max. operational G-load | 6 |
| Crew, crew members | 2 |
Image gallery of the Mudry CAP.10 B
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APA: Mudry CAP.10 B (). Mudry CAP.10 B. archivoaereo.com. https://archivoaereo.com/en/mudry-cap-10-b-2/
VANCOUVER: Mudry CAP.10 B [online]. archivoaereo.com; [cited 2026-05-16]. Available at: https://archivoaereo.com/en/mudry-cap-10-b-2/