The CAP 230 was primarily developed in 1985 for the French Air Force. From the basic CAP 21 airframe, trailing edge apex triangular surfaces were added to the basic trapezoidal wing. The CAP 230 keeps a full wooden construction and certified to cope with +10/-10 G-forces.
The CAP 231 was developed in 1990. The fuselage design remained unchanged and only leading edge triangular apex surfaces were added to reduce buffeting during high G pullups. The CAP 231 was world champion in 1990.
Construction: Balsa and ply
Aileron Control: Dual servos
Wheels: Main -- (65mm) Tailwheel-- (25mm)
Covering: Polycote ESC
Motor Mount: Power Module
Engine Mount: Two-piece composite
Fuel Tank: 300cc
Cockpit: with clear cockpit with dummy pilot
Build Time: 5-7 hours for assembly.
Warranty: trial fit at the factory make sure this kit to be free from defects in bother material and workmanship at the date of purchase. This warranty does not cover any component parts damaged by use or modification.
ARF scale Cap 232, Fuel Tank, Spinner
Landing Gear Wheels and Instruction Manual
Servos: 5 standard (2-aileron 2-flaps 1-elevator 1-rudder 1-throttle)
Engine .46-.55 2-stroke or .70-.90 4-stroke glow engine