As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RUSTED PISTON END AT RUDDER TRIM TAB ACTUATOR ON AFT ACCESSORY COMPARTMENT. RUDDER TRIM LOAD-FEEL SPRING ASSY WAS REMOVED AND INSTALLED IAW AMM 27-207. AREA AT SHAFT OF RUDDER TRIM LOAD-FEEL SPRING ASSY WAS REWORKED MEASUREMENT ORIGINAL 0.686" AND MINIMUM REMAINING IS .685" IS WITHIN LIMITS IAW DWG NR 3652587, REV D CADMIUM PLATE WAS APPLY IAW DWG 3652587, REV B AND DPS 9.74.