As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C5 CHECK DISCOVERED CORROSION ON ANGLE LOCATED AT FR 71 + 1" ON THE LOWER LOBE FUSELAGE TAIL SECTION CAVITY, INTERIOR CUT OUT OF ACCESS DOOR NR 312AR. CORROSION WAS FOUND TO BE OUT OF LIMITS. ANGLE WAS REMOVED AND REPLACED IAW AIRBUS 320 SRM 51-72-11.