As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CLT - DURING VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1.1 INCH CRACK AT A PREVIOUS REPAIRED AREA FWD ADN AFT BS 767 STRINGER 18L ON THE SKIN. FWD AREA CUTOUT 6 INCH BY 6 INCH AFT AREA 4 INCH BY 2 INCH CUTOUT. INSTALLED DOUBLER PER REPAIR DOCUMENT SRM 53-30-3 FIG 17. (M)