As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HEAVY CHECK, FOUND INTERNAL FUSELAGE SKIN AT BS 234 AND STR 23S HAS GOUGE IN SKIN AT PREVIOUS REPAIR. MAINTENANCE DID PERMANENT REPAIR TO SKIN, PN 85360122 BETWEEN FRAME BS X236.0-BS X258.5 AND STR 23S-24S IAW RD 8/4-53-4897, ISSUE 2 DATED 8 FEB 2016. ACFT REMAINS IN RFD FOR COMPLETION.