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 FUSELAGE WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 77 BELOW STRINGER 04R. MX PERFORMED A FILLER/ DOUBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.