As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO WING PRESSURE PANEL ATTACH ANGLE FROM STA 960 TO STA 980 AT RIGHT BUTT LINE8.0. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED ATTACH ANGLE AND STRINGER FITTING IAW DC-8 SRM 51-1-20, 51-1-21 AND 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).