As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CLT - INSPECTION VISUAL FOUND DAMAGED INNER, OUTER CHORD, WEGB AND FORMED ANGLES APPROX 8 INCHES BY 2 INCHES LOCATED AT THE FUSELAGE FRAME LOCATED AT BS 188 FROM 7 INCHES RIGHT OF BL 0 TO 23 INCHES RIGHT OF BL 0. INSTALLED REPAIR CHORD AND WEB AS PER BOEING SRM 51-70-11, 51-70-12 AND 51-70-13. (M)