As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHEN QUICK, FIRM PRESSURE APPLIED TO THE CAPTAIN'S TOE BREAKS, THE ENTIRE FOOT PEDAL ASSEMBLY SLIDES FORWARD. REPLACED CAPTAIN'S RUDDER PEDAL ADJUSTMENT SHAFT, BOSS, AND BUSHINGS. PERFORMED OPS TEST IAW AMM 27-20-00-710-802. NO DEFECTS. RETURNED TO SERVICE.