Manufacturer Comments:
In the air, the CAP 232's large rudder makes for easier handling, and the rear-mounted rudder servo features a shorter linkage that tightens the coupling for greater authority. A dual elevator pushrod system allows for infinite individual adjustablilty of each elevator half. With its ability to perform even the most radical freesytle aerobatics, this is one plane that's ready, willing and able to unleash a flier's "wild side".
The fuselage builds flat on the board and uses sheeting on the turtle deck, so there's less carving and sanding

A small number of interlocking, die-cut parts help ensure straight, strong assembly

The fuel tank tray has been designed for easy removal, and a separate smaller hatch allows for quick inspection of the fuel lines

With a .46 engine installed, the CAP 232 is very aerobatic, and this size power plant and muffler fits cleanly inside the 3-piece ABS cowl

Lightweight construction thanks to the expert use of lightening holes throughout the airframe

An adjustable engine mount made of reinforced nylon comes with the kit that perfectly fits any 2-stroke or 4-stroke engine within the recommended range
Fuselage construction provides an excellent example of the CAP 232's builder-friendly engineering. It goes together flat on the board, and balsa sheeting replaces much time-consuming carving and sanding. Great Planes gave the CAP 232 slight dihedral, large control surfaces, and lots of lightening holes to reduce weight. For all of these reasons, it's remarkably stable during stalls and slow flight-ideal for inexperienced low-wing pilots.
Inspecting the CAP 232's fuel lines is as simple as removing the cowl and lifting up the small hatch shown here. You also have fast, easy access to the fuel tank which sets into a handy, removable tray.
Seller Comments:
Cap 232 Airplane, needs to be Built, it is a working gas airplane model. Wingspan of 60". Does not have engine or Remote control. brand new in box, been looked at once and never attempted to built due to lack of time.
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