What was found
RIGHT INNER WING CTR L/E FORMER 1.000 INCH CRACK, STA XFS 385.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED REINFORCING ANGLE (2024T3 0.040) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 51-1-20D PG 9, SRM 57-2-0 PG 9, 10.