What was found
RIGHT STUB WING FORMER CRACK 0.250, STA XFS 548.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (ALCLAD 2024T3 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B PG 16, 17. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10, SRM 51-1-21 PG 1.