As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SHV - DURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 79 STRINGER 6R-7R. DAMAGE FOUND TO BE AT STRINGER 5R-6R AND NOT STRINGER 6R-7R. MAINTENANCE PERFORMED REPAIR TO EXTERNAL FUSELAGE SKIN AT FRAME 79 STRINGER 5R-6R AND INITIATED DMI IAW EC5330-02483. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.