What was found
DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO EXTERNAL SKIN SECTION BETWEEN STA 25 AND STA 55 BETWEEN LONGERONS 23 RIGHT AND LONGERON 25 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).