What was found
DURING A MAINTENANCE VISIT, FOUND WORN AREA, WING, LT I/B FLAP ATTACH FITTING AT STA 3 WORN GREATER THAN 20 PERCENT OF THE MATERIAL THICKNESS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED AND REPAIRED IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06151.