What was found
RIGHT WING CTR L/E FORMER 1.000 CRACKED, STA XFS 484.000 (UPPER SECTION). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 57-2-0 PG 9-10.