What was found
DURING A MAINTENANCE VISIT, FOUND LEFT WING OUTBOARD FLAP WEDGE HAD PREVIOUS BLENDOUT ON TOP INBOARD CORNER AT THE ATTACH SEAM GOUGED, BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05117.