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 78 STRINGER 7R-8R. DAMAGE WAS FOUND TO BE AT STRINGER 5R-6R AND NOT 7R-8R. MAINTNENANCE PERFORMED REPAIR TO EXTERNAL FUSELAGE AT FRAME 78 STRINGER 5R-6R AND INITIATED DMI IAW EC5330-02483. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.