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 CORROSION DAMAGE TO THE FUSELAGE INT ON ATTACH ANGLE AT STA 857 TO 859 AND L11R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-8 FIG 1B. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).