As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A-CHECK INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO HAVE A .2" (5MM) CRACK AT FRAME 75 BETWEEN STR 2R & 3R. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.