What was found
DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING UPPER FRONT SPAR CAP STRUCTURE CRACK DAMAGE BETWEEN STA XFS-6 CAP. MAJOR REPAIR ACCOMPLISHED BY REMOVING FASTENERS. REMOVING CORROSION FROM SLANT PANEL UPPER CAP AND FOUND OUT OF LIMITS. CLEANED, TREATED AND PRIMED AREA. INSTALLED DOUBLER, REMOVED UPPER SPAR CAP (DAMAGED). REMOVED STIFFENER AND PERFORMED NDT INSPECTION. APPLIED SEALANT TO FAYING SURFACES AND INSTALLED DOUBLER, ANGLE DOUBLER. INSTALLED KIT, TORQUE AND LEAK CHECKED IAW S/B DC8-57-072 R03 DWG DACO 5892075, CN1, DC8 SRM 51-1-8, 51-1-11, 51-1-15, 51-1-20D, 51-1-26, 51-3-0, 51-3-1, 51-3-2, DPS 1.05-8, 3.67-3, 2.5.