Mudry CAP.10 B

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 and diagram gallery of the Mudry CAP.10 B

CAP.10	CAP.10
CAP.10	CAP.10
CAP.10	CAP.10
CAP.10	CAP.10
CAP.10