What was found
DURING ROUTINE C CHECK INSPECTION, LT WING. STUB WING UPPER SURFACE STA XS 250.000 XS 240.000 HAS TWO CRACKS OF .5 INCH. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 38, TR NR 57-85, EO SEMAN NR 2005983 DATE 06-18-05. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1. TRIMMED OUT DAMAGED AREA IAW SRM 57-2-1 FIG. 38. PERFORMED VISUAL INSPECTION, NO CRACK, CORROSION FOUND. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.071) + FILLER (ALCLAD 7075 T6 0.063) IAW SRM 57-2-1 FIG. 38, SRM 57-3-1 FIG. 3. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM 57-2-1 FIG. 38, SRM 51-3-0 PAGE 1, SRM 51-1-20D PAGE 9. TOR