As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
2 INCH HOLE IN BELLY OF ACFT AT 2 FT AFT OF AVIONICS COMPARTMENT. INSP HOLE AFTER REMOVAL OF FWD BUG BIN FWD CENTER PANEL. FOUND NO STRUCTURAL DAMAGE OTHER THAN 2.5 INCH X 4.38 MAC IN EXTERIOR SKIN. REMOVED DAMAGED PORTION OF SKIN FROM FS 105-F5111 BETWEEN L 35 & H & L36, INSTALLED REPAIR I/A/W DC-8 SRM 53-2-1 FIG 7