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 LOWER FUSELAGE SKIN CRACKED AND CORRODED AT STA 1400 TO 1440 AND LONGERONS 31R TO 36. REMOVED DAMAGED SECTION BY CUTOUT. TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER AND FINGER DOUBLERS AND INSTALLED IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04148 AND DC-8 SRM 53-4-1 FIGURE 17 ITEM B.