What was found
DURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER Z24R END CLIPS CRACKED AT FS 1072 AND LONGERON 15 RIGHT. REPLACED STIFFENER END CLIPS IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER Z24R END CLIPS CRACKED AT FS 1072 AND LONGERON 15 RIGHT. REPLACED STIFFENER END CLIPS IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.