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 DAMMAGE TO THE COCKPIT PANEL 676B ALONG EDGE & SCREW HOLES AT FR -52X-20,Z0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SKIN IAW DC-8 SRM 51-1-4 AND 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).