As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT CARGO PIT; FWD BULKHEAD AT FRAME 54; THE CEILING PANEL ATTACH ANGLE IS CORRODED FROM RBL 37 TO 48 CM (14" TO 18.5"). REMOVED CORROSION IAW SRM 51-74-10. ORIGINAL MATERIAL THICKNESS .098. REMAINING MATERIAL .043. MATERIAL REMOVED .055. OUT OF LIMITS IAW SRM 53-10-00. REMOVED ANGLE IAW SRM 51-40-21. FABBED NEW ANGLE IAW DWG A53410767. ALODINED IAW SRM 51-21-10. PRIMED AND PAINTED IAW SRM 51-23-10. PART MARKED ANGLE IAW GMM 7-0-1001. INSTALLED ANGLE IAW SRM 51-40-21. MINOR REPAIR.