As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 2ND FASTENER HOLE FROM OTBD. STEEL PLATE REMOVED IAW SRM 51-40-02. FABRICATED IAW DWG 65B09631, REV: AG AND INSTALLED IAW SRM 51-40-02.