What was found
DURING ROUTINE C CHECK INSPECTION, RT WING UPPER SKIN CRACKED 1INCH, STA. XRS 74. 869, S-10. REMOVED EXISTING REPAIR DOUBLERS SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA IAW SEMAN DWG ED 3981. PERFORMED NDT INSPECTION IAW SPM PART 06-10-01-001. FABRICATED EXTERNAL REPAIR DOUBLER (ALCLAD 7075 T6 0.160”) + (03 EA) FILLER PLUG (ALCLAD 7075 T6) IAW SEMAN DWG ED 3981. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS (INTERNAL PART) IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 3981, SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1.