As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SAL - DURING C5 CHECK DISCOVERED CORROSION ON INTERNAL STRUCTURE, REINFORCEMENT PLATE, LOCATED BETWEEN FS 65 TO FS 66 AND BETWEEN STR 36L TO STR 42L. CORROSION LIMITS WERE NOT FOUND IN THE SRM. MAINTENANCE REMOVED AND INSTALLED NEW REINFORCEMENT PLATE LOCATED BETWEEN FS 65 TO FS 66 AND BETWEEN STR 36L TO STR 42L IAW AIRBUS 320 SRM 51-42-11 PARAGRAPH 6.