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Mudry CAP 10


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

Production of the CAP.10B light-weight, 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.

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



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