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 FUSELAGE SKIN HAS NUMEROUS GOUGES AND BLEND-OUTS LOCATED DIRECTLY BELOW MAIN CARGO DOOR CUTOUT. *S/D* BLEND-OUT DAMAGE BEYOND IAW DC-8 SRM 53-2-0 LIMITATIONS. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-03754.