What was found
CRACK ON UPPER OF AFT PRESSURE BULKHEAD STIFFENER 4 AND STA X=60. ANGLE WAS REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON UPPER OF AFT PRESSURE BULKHEAD STIFFENER 4 AND STA X=60. ANGLE WAS REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-4.