What was found
DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, INTERNAL SKIN SECTION, BETWEEN STA 49.5 AND STA 64, AND BETWEEN LONGERONS 33 RIGHT AND LONGERON 35 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).