As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WEB CORROSION REPAIR INSPECTION OF THE FS 1016 BULKHEAD WEB REVEALED CORROSION AT THE BL 0 STIFFENER NEAR THE BOTTOM OF BULKHEAD AT WL 190-200. AN OIL CAN CONDITION WAS DISCOVERED JUST OUTBOARD OF THE CORROSION AREA. BOTH DAMAGES WERE REMOVED WITH A WEB CUTOUT AND REPAIRED WITH ALUMINUM REPAIR DOUBLERS IAW BAC S/B 737-53A1075 AND IAW ER/A 385542-14AD, REV A.