As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE COMPLYING WITH HIDDEN DAMAGE INSPECTION FOR S00012, FOUND CORNER FITTING (ITEM 30 FIG 2 SHEET 1 SRM 52-31-00 PG 12) CRACKED WITH PREVIOUS REPAIR, AND CRACK HAS MIGRATED 1 INCH PAST STOP DRILL. REMOVED AND REPLACED CORNER FITTING IAW A300-600 SRM 51-72-10.