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 EXTERIOR FUSELAGE SKIN/PLATING BEYOND LIMITATIONS IAW DC-8 SRM AT, STA 39 AND LONGERON 33 RIGHT. REMOVED ALL CORROSION DAMGE AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH D53-R01.