What was found
DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING FORWARD TOP PANEL PLATING CRACK DAMAGE AT STA XRS 144.00 FRONT SPAR. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED AREA. PERFORMED NDT INSPECTION. FABRICATED EXTERNAL DOUBLER AND FILLER PLUG. CLEANED, TREATED AND PRIMED AREA AND REPAIRED PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIRED PARTS IAW SEMAN DWG ED-3833 AND FAA FORM 8110-3 NR 05020, DC8 SRM 51-1-11, 51-1-15, 51-120D, 51-1-22, 51-1-26, 51-3-0, 51-3-1, 51-3-2, 51-6-0.