As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STIFFENER ON REAR PRESSURE BULKHEAD AT LBL 36, FS 621 IS CRACKED. REMOVED CRACKED STIFFNER ANGLE ON RT PRESSURE BULKHEAD AT LBL36, FS621.00 IAW SRM 51-42-06. LOCATED, DRILLED NEW STIFFNER ANGLE IAW SRM 51-40-11. INSTALLED FASTENERS AT LBL36 FS621, REF SRM 51-42-06 AND SRM 51-42-21 AND DWG NR 601R-36008.