As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SHV - DURING C-CHECK CORROSION FOUND ON INTERNAL FUSELAGE SKIN BETWEEN FRAMES 57-58, STRINGER 21L-21R. MAINTENANCE PERFORMED REPAIR ON INTERNAL FUSELAGE SKIN, BETWEEN FRAMES 57-58 STRINGER 21L-21R IAW EC5330-02475. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.