As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BS 178 FWD PRESSURE BULKHEAD CENTER WEB RBL 5.7 HAS 1/2 INCH CRACK; WL 198-200 RBL 5.7 HAS 3/8 INCH CRACK UNDER STIFFENER. REMOVED DAMAGE AND INSTALLED DOUBLER AND REPAIR FILLERS IAW SRM 53-10-08 FIG 209; NDT VERIFIES CRACKS COMPLETELY REMOVED.