What was found
RIGHT WING CTR L/E FORMER 0.250 CRACKED, STA XFS 316.500. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER ON RIGHT WING CTR L/E, STA XFS 316.500 IAW SRM 57-2-0 PG 9-10, IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9.