What was found
DURING ROUTINE C CHECK INSPECTION, LT WING T/E WEB UPPER PART CRACKED 1/2, XCW 69.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-6 FIG. 15, EO SEMAN NR 2005836 DATE 06-25-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA IAW DC-8 SRM 57-2-6 FIG. 15. PERFORMED NDT INSPECTION IAW NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER, FILLERS (02 EA) IAW DC-8 SRM 57-2-6 FIG. 15. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW DC-8 SRM 57-2-6 FIG. 15, DC-8 SRM 51-3-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 SRM 51-3-1.