What was found
INSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM LOWER CHORD STIFFENER AT STA 344, BL 0. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.
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 344, BL 0. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.