What was found
AFT PRESSURE BULKHEAD SUPPORT ANGLE WAS CRACKED AT STRINGER 39L. REPLACED THE SUPPORT ANGLE IAW SRM 51-42-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT PRESSURE BULKHEAD SUPPORT ANGLE WAS CRACKED AT STRINGER 39L. REPLACED THE SUPPORT ANGLE IAW SRM 51-42-11.