What was found
CRACKED STIFFNER ON THE AFT PRESSURE BULKHEAD UNDER LONGERON END 3R. THE STIFFENER WAS REPLACED IAW SRM 51-30-5, 51-30-2, AND 51-10-3 PAR. 14 AND 21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED STIFFNER ON THE AFT PRESSURE BULKHEAD UNDER LONGERON END 3R. THE STIFFENER WAS REPLACED IAW SRM 51-30-5, 51-30-2, AND 51-10-3 PAR. 14 AND 21.