As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SHV - DURING C-CHECK THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75, STRINGERS 1R-2R, EMANATING FROM THE FRAME 75 FITTING. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-02353. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.