As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 5A INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED BELOW STR 2R AT FR 75. MX REMOVED THE DAMAGED SECTION AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.