As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A-CK INSPECTION, THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 JUST BELOW STR2R. MX PERFORMED A DOUBLER REPAIR WITH DRAG ANGLE IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02353, AND ACFT APPROVED FOR SERVICE.