As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A-CK INSP THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET AT FRAME 77 BELOW STRINGER 03L. MX REMOVED THE DAMGE, AND PERFORMED AN INSERTION/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.