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Mudry CAP 10

mudrycap10


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
Mudry CAP-10B


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

 

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

 

 


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