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 1180 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 7TH FASTENER HOLE FROM OTBD. STEEL PLATE REMOVED IAW SRM 51-40-02. FABRICATED IAW DWG 65B09631 REV AG AND INSTALLED SRM 51-40-02.