What was found
DURING ROUTINE C CHECK INSPECTION, LT WING. SLANT PANEL UPPER PART CORRODED, XFS 38.750 - XFS 70.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 37, EO NR 20051004 DATE 06-16-05. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 21. SMOOTHED AND PERFORMED BLEND OUT TO CORRODED AREA IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.125) IAW SRM 57-2-1 FIG. 37. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER INTERNAL PART (NEW) IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-12. INSTALLED REPAIR DOUBLER AND NEW FASTENERS IAW SRM 57-2-1 FIG. 37, SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1.