As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER OFF LOAD, DISCOVERED DAMAGE TO ACFT WING/FUSELAGE FAIRING APPROX 30 INCHES FWD OF CENTER CARGO DOOR FWD EDGE. REPAIRED DAMAGED FORMED ANGLE COMMON TO THE WING/FUSELAGE FAIRING AT AREA NOTED AS PER GUIDELINES IN THE DC-10 SRM CHAPTER 51 STANDARD PRACTICES AND 53-00-01 FIG 8.