As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION DAMAGE WAS FOUND ON FUSELAGE INTERNAL SKIN, PN 1146T3241-12, JUST AFT OF STA 1540 BETWEEN S39L & 39R IN THE AREA WHERE A DRAIN VALVE AND AN EXISTING REPAIR EXIST. AMOUNT OF MATERIAL REMOVED TO CLEAN THE DAMAGE EXCEEDS LIMIT 0.15T IAW 767-300 SRM 53-00-01 ALLOWANBLE DAMAGE 1. REF FIG 1 OF RI-53-00-14514 REV A.