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 THAT THE PREVIOUS BLEND OUT NEEDS THICKNESS CHECKED AT STA 1690 TO 1700 AND L10L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 AND EO NR 00-107 WITH APPROVED 8110-3 DATED 5-24-00.