Brake rudder pedal system for light aircraft

A brake rudder pedal system for a light aircraft having a pedal assembly comprising rudder and steering operation means for manipulating a rudder and steering mechanism, and brake operation means for operating a brake mechanism, said pedal assembly comprising:

• a pair of pedal bodies whose tops are rotatably supported between hull frames;
• said rudder and steering operation means being rotatably connected to said pedal bodies thereoutside, said means having upper first arms connected to a rudder operating flexible cable and to moving-left-and-right flexible cable, and lower second arms connected to the steering mechanism by a steering rod;
• said brake operating means having a brake pedal whose lower portion is rotatably supported to said pedal bodies, and a brake lever connected to said brake pedal and for operating said brake mechanism;
• and
• pedal position controller means having a control handle rotatably disposed on a gauge board cover, a pair of transmission flexible cables rotated while connected to said control handle, a control nut supported to said pedal bodies to be movable forward and rearward, a support block supported to said connection arm to be movable forward and rearward, and a control screw rod supported to said support block while idling at its original position, said control screw rod being screw-fastened to said nut and whose top is fixedly connected to said transmission flexible cable.