As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(AFT PRESSURE BULKHEAD) WORN AREA ON AFT PRESSURE BULKHEAD LEFT AND BELOW PRESSURE RELIEF VALVE. BLENDED OUT WORN AREA TO A DEPTH OF .010. DYE CHECKED AREA. NO CRACKS FOUND. ALODINED AND PRIMED BLEND AREA THEN INSTALLED DOUBLER PER ESO.