What was found
DURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER Z24L END CLIPS CRACKED AT FS 1072 AND LONGERON 15L. REPLACED STIFFENER END CLIPS IAW DC-9 SRM CHAPTER 51-30-1.
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 Z24L END CLIPS CRACKED AT FS 1072 AND LONGERON 15L. REPLACED STIFFENER END CLIPS IAW DC-9 SRM CHAPTER 51-30-1.