What was found
LT WING FRONT SPAR VERTICAL STIFFENER AT WS 90 SHOWS CRACK FROM BOTTOM END. REMOVED FASTENERS FOR ACCESS IAW SRM 51-30-2 HFEC AT ANGLE MARKED END OF CRACK NDT MAN PART6 51-00-00 FIG23 STOP DRILLED .250 END OF CRACK IAW SRM51-10-1 FAB REPAIR MAT USED 7075 T6 .063 PO NR 9002695 DIM 7.5 INCHES X 2.7500 INCHES IAW SRM 57-20-2 FIG1 AND 51-30-5 TREATED AND PRIMED PART AND AREA IAW SRM 51-10-2 INSTALLED REPAIR IAW SRM 57-20-2 FIG1 AND 51-30-2.