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 EXTERIOR SKIN AT STA 1265 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED SKIN IAW PD 08-53-053 AND DC-8 SRM 53-2-1 FIG 7 SHEET 4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).