As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HEAVY CHECK MAINTENANCE FOUND CORRODED ANGLE 3 EA AND 3 EA CRACK RECEPTACLE ON PANEL 1441FR. REMOVED THE CORROSION ON THE ANGLE 3 ON THE 1441FR PANEL. THE BLENDED AREA IS 18.0" X 2.0" X .008". NOMINAL THICKNESS OF THE ANGLE IS 0.050". REMOVED AND REPLACED THE ANGLE REF SRM 51-40-02 AND 51-40-08. A/C REMAINS IN CHECK.