As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SHV - DURING C-CHECK IT WAS FOUND THAT THE CENTER FUSELAGE SKIN HAD AN INTERNAL GOUGE BETWEEN FRAMES 16 AND 17, AND STRINGERS 3R AND 4R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145XR SRM 53-21-01. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)