As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CLT - MAJOR REPAIR - C22 CHECK - AN 8 INCH CRACK ON FLOORBEAM UPPER CHORD SUPPORT ANGLE AT BS 380 - 400, BL 0. INSTALLED REPAIR IAW SRM 51-20-01, 50-30-50-11 FIG 1 DETAIL 1 AND 51-40-03. *SUPPLEMENT* IDENTIFIED PART AS "FLOORBEAM UPPER CHORD SUPPORT ANGLE".