As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL STABILIZER TO RUDDER ATTACH FITTING NR 2 HINGE; BEARING IS CORRODED AND BINDING. RUDDER HINGE ARM NR 2 REMOVED PER AMM 55-36-44-4. RUDDER HINGE ARM MODIFIED PER WORK STEPS OF SB A300-55-6022 REV 03, PARA 3-F(2),(B) 2. PER E A 6-5540-136664, RUDDER HINGE ARM REINSTALLED PER AMM 55-36-44-4. FUNCTIONAL TEST OF RUDDER MECHANICAL CONTROLS COMPLETED ON WORK CARD 63C0501.