As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A MAINTENANCE VISIT, FOUND ADDITIONAL DRILLING HOLES IN THE FUSELAGE TO VERTICAL ATTACHMENT ANGLE AT STA 1766. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04249 AND DC-8 SRM 53-2-5 FIGURE 16A SHEET 1.