What was found
CRACKED END STIFFENER AT LONGERON 14R OF THE AFT PRESSURE BULKHEAD. THE STIFFENER WAS REPLACED IAW SRM 51-30-5 , 51-10-4 , 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 END STIFFENER AT LONGERON 14R OF THE AFT PRESSURE BULKHEAD. THE STIFFENER WAS REPLACED IAW SRM 51-30-5 , 51-10-4 , 51-10-3 PAR. 14 AND 21.