What was found
CRACKED STIFFENER AT THE 12 HR POSITION, ON AFT CABIN PRESSURE BULKHEAD. THE STIFFENER WAS REPLACED IAW DWG 9915562, REV P, AND SRM 51-41-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED STIFFENER AT THE 12 HR POSITION, ON AFT CABIN PRESSURE BULKHEAD. THE STIFFENER WAS REPLACED IAW DWG 9915562, REV P, AND SRM 51-41-05.