What was found
LT WING CTR L/E UPPER FORMER CRACK 1" STA XFS 427.000. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (AL7075"0" 0.080") IAW SRM 57-3-0 FIG 1G, SRM 57-2-0 PG 9-10. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PG 1, 13, 17 FROM 7075"0" TO 7075T6. CLEANED, TREATED AND PRIMED AREA AND NEW ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED NEW ANGLE DOUBLER IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1.