What was found
DURING C CHECK INSPECT, LT WING, SKIN UPPER PART WITH 02 CRACKS 1", 1/2", XRS 74.000 S-9 - S10. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG 10, EO SEMAN NR 2005833 DATE 06-14-05. REMOVED DAMAGED AREA IAW DC-8 SRM 57-2-1 FIG 10 (SHEET 3). PERFORMED NDT INSPECT IAW DC-8 NDT SPM PART 06-10-01-001. NO CRACK, CORROSION FOUND. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.125), (02 EA) FILLERS PLUG (ALCLAD 7075 T6 0.175) PART DOUBLER FROM 0.125 TO 0.080 OVER 4 LENGTH (TYP BOTH ENDS) IAW DC-8 SRM 57-2-1 FIG 10 (SHEET 3). CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW DC-8 SRM 57-2-1 FIG 10 (SHEET 3), DC-8