What was found
DURING C CHECK INSPECTION, NR 3 RT STUB WING LWR SKIN CRACK 2 AT STA XW 255.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 37, EO SEMAN NR 20051284 DATED 09-27-05. REMOVED FASTENERS IAW DC8 SRM 51-1-20D. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 2G. FAB`D REPAIR DOUBLER (AL7075T6 0.125”) IAW DC8 SRM 57-2-1 FIG 37. TAPERED DOUBLER FROM 0.125” TO 0.050” IAW DC8 SRM 57-2-1 FIG 37 NOTE 7. CLEANED, TREATED AND PRIMED AREA, REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-1 FIG 37, DC8 SRM 51-1-20D, DC8 SRM 51-3-1.