Müller, Jacques V.

Jacques V. Müller was born in Luxembourg in 1881 and emigrated to the USA in 1900 to join his sister, who ran a farm there. He settled in Salina, Kansas, where he experimented with balloons and from 1909 reportedly built four airplanes. In 1914 he returned to Luxembourg, where he started a mine and a pigment factory.

Mudry CAP 20

The CAP 20 is a single seat derivative of the CAP 10.

The CAP 20A is a single seat derivative of the CAP 10 with a no dihedral wing and lengthened landing gear.

The CAP 20B is a modified CAP 20A with new wings and larger ailerons.

CAP-20L

The CAP 20L is a shorter airplane than its predecessor, the 20, and it seems to benefit from a much increased rudder area. Lightened for competition (hence the L designation, for leger), the CAP 20L also has a new wing design.

CAP 20

Mudry CAP 10

The CAP 10 was developed by CAARP and first flown in 1968.

The CAP 10 aerobatic trainer is a side-by-side monoplane, powered by a 190 hp injected Lycoming engine.

The construction is all wood with a cotton-covered rear-fuselage. (By law, all fabric must be replaced every 3 yrs in France). In 1967 they were priced at US$30,000 with no radio or gyros.

Production of the CAP.10B lightweight, fully aerobatic piston-engined primary trainer continued, and 88 have been delivered to military customers by 1987.

Mudry CAP-10B

Total production exceeded 220 aircraft by 1997, and a glider-towing version, the CAP.10R, was available.

Gallery

CAP 10
Engine: Lycoming IO-360-B2F
Wing span: 26 ft 5 in / 8,06 m
Length: 23 ft 11 in / 7.30 m
Empty weight equipped: 1168 lb / 530 kg
MTOW aerobatic: 1666 lb / 756 kg
MTOW utility: 1829 lb / 830 kg
Max cruise 75%: 129 kt / 149 mph / 240 kph
ROC SL: 1180+ fpm / 360+ m/min
Service ceiling: 18,050+ ft / 5500+ m
Range: 647 nm / 745 mi / 1200 km
Seats: 2 side-by-side
Baggage: 44 lb / 20 kg
Cabin max width: 3 ft 5 in / 1.054 m

CAP 10B
Engine: Lycoming AEIO-360-B2F, 180 hp
TBO: 1400 hrs
Prop: Hoffmann 2-blade, 67-in
Seats: 2
Length: 23 ft
Height: 7.5 ft
Wingspan: 26.4 ft
Wing area: 117 sq.ft
Wing aspect ratio: 5.96
Maximum ramp weight: 1829 lb
Maximum takeoff weight: 1829 lbs
Standard empty weight: 1200 lbs
Maximum useful load: 629 lbs
Maximum landing weight: 1829 lb
Wing loading: 15.6 lbs/sq.ft
Power loading: 10.1 lbs/hp
Maximum usable fuel: 246 lbs
Best rate of climb: 1600 fpm
Service ceiling: 16,400 ft
Maximum speed: 146 kt
Normal cruise @ 65% pwr @ 8000 ft: 139 kt
Fuel flow @ normal cruise: 51 pph
Endurance at normal cruise: 4.6 hrs
Stalling speed clean: 50 kt
Stalling speed flaps down: 44 kt
Turbulent-air penetration speed: 126 kt
Fixed tail wheel under carriage

Mudry

Mudry et Compagnie
Established 1958 by M. Auguste Mudry in the former SAN factory at Bernay, Normandy. Built CAARP-developed CAP 10 two-seat and CAP 20 single-seat aerobatic aircraft. Merged in early 1978 with CAARP. Became known as Avions Mudry et Cie until assets purchased by AeroTech Europe.

A subsidiary of Aeronautical Service, Akrotech Europe has taken over assets of Avions Mudry et Cie, continuing production of the CAP 10B two-seat aerobatic and club trainer (first flown 1968) and CAP 232 single-seat aerobatic competition monoplane (first flown July 1994). Also produces the CAP 222, a version of the US AkroTech Giles G-202 two-seat kit-built aerobatic competition aircraft and trainer.

Mudry was bought out by the group which owns Robin Aircraft and as a result the Barouder became available through Bul Aéro (1998).