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CAP / Mudry / Apex Cap 10

CAP / Mudry CAP 10B, Aerobatic-Center, D-EXXX, c/n 259 © Karsten Palt
Photo ©: Karsten Palt

Cap 10

Aerobatic Aircraft

The Mudry CAP 10 is a single engine two seat light aerobatic aircraft produced by the French manufacturer Avions Mudry et Cie, later CAP Aviation and APEX Aircraft.
Crew1
Passengers1
 
Propulsion1 Piston Engine
Engine ModelLycoming AEIO-360-B2F
Engine Power136 kW182 hp
 
max. Cruise Speed300 km/h162 kts
  186 mph
max. Speed (vne)341 km/h184 kts
  212 mph
Service Ceiling5.000 m16.404 ft
Rate of climb480 m/min1575 ft/min
Range1.000 km540 NM
621 mi.
 
Empty Weight550 kg1.213 lbs
max. Takeoff Weight760 kg1.675 lbs
max. Landing Weight760 kg1.675 lbs
 
Wing Span8,06 m26,4 ft
Wing Area10,9 m117 ft
Length7,00 m23,0 ft
Height1,76 m5,8 ft
 
First Flight08/1968
Production Statusout of production
Production Range1969-2008
Total Production> 300
Developed fromPiel CP30 Emeraude
 
ICAO CodeCP10
FAA TCDSA36EU
EASA TCDSA.370
 
Data for (Version)APEX CAP 10B
VariantsCAP 10, CAP 10B

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