As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK IN TPE INSPECTION FOUND PRESSURE BULKHEAD SUPPORT ANGLE CRACK AT STA 1521 BETWEEN X=15 & X=-15 (REF EGAT NRC U05078). REPLACED THE SUPPORT ANGLE ON PRESSURE BULKHEAD AT STA 1521 BETWEEN X=15 & X=-15 IAW MD-11 SRM 51-35-01 VOL 2 REV 40. CONDITION CHECK NORMAL AND JOB COMPLETED.