As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 5A INSPECTION, THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 79 BELOW STRINGER 03L. MX PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.