As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 5A INSP THE LAFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FR78 STR 09L AROUND 1 RIVET. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A DOUBLER REPAIR ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.