What was found
INSPECTION FOUND A 2 INCH CRACK AT LOWER ATTACH POINT OF VERTICAL STIFFENER AT AFT CARGO FORWARD PRESSURE BULKHEAD STA 727, LBL 18. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK AT LOWER ATTACH POINT OF VERTICAL STIFFENER AT AFT CARGO FORWARD PRESSURE BULKHEAD STA 727, LBL 18. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2.