What was found
INSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM LOWER CHORD STIFFENER AT STA 328, LBL 24. THE STIFFENER WAS REMOVED, A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM LOWER CHORD STIFFENER AT STA 328, LBL 24. THE STIFFENER WAS REMOVED, A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.