As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE AFT PRESSURE BULKHEAD FWD FACE LWR RIM FR 80/82 HAS 3 EA AREAS OF EXFOLIATED CORROSION & 1 EA AREA OF CORROSION EXTENDING INTO THE CLEAT PROFILE. DEFECT MEASURES 15"SQ. AFTER REMOVAL OF LEVEL 1 CORROSION, FOUND ANGLES TO BE OUT OF LIMITS IAW SRM 53-19-17, FIG 104. R & R 3EA DOWN-HOLDERS AND 1EA CONNECTING SECTION IAW SRM 51-72-10, PGS 1-3. FABRICATED 1EA REPLACEMENT DOWN-HOLDER AND INSTALLED IAW DWG A53981823 AND SRM 51-72-10, PGS 1-3.