What was found
DURING ACCEPTANCE INSPECTION, CRACKS WERE FOUND IN THE AFT PRESSURE BULKHEAD DOOR JAMB AT THE UPPER FOWARD RIGHT CORNER. THE FRAME WAS REPLACED AND THE SKIN WAS REPAIRED IAW THE DC-9 SRM 53-05 FIG 76.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ACCEPTANCE INSPECTION, CRACKS WERE FOUND IN THE AFT PRESSURE BULKHEAD DOOR JAMB AT THE UPPER FOWARD RIGHT CORNER. THE FRAME WAS REPLACED AND THE SKIN WAS REPAIRED IAW THE DC-9 SRM 53-05 FIG 76.