What was found
DURING A ROUTINE C CHECK, INSPECTION FOUND LT WING INBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIRS BETWEEN STA XW 87.000 AND XW 91.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR, AND REMOVED PLATING SEGMENT. PERFORMED NDT INSPECTION AND FABRICATED NEW PLATING SEGMENT + INTERNAL SPLICE + EXTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND NEW REPAIRED PARTS INTERNAL PART. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-3845 AND FAA FORM 8110-3 NR 05019, DC8 SRM CHAPTERS 51-1-11, 51-1-20D, 51-1-21, 51-1-22, 51-1-26, 51-3-1, 51-3-2.