As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT OUTER WING L/E FORMER UPPER PART WITH 1 INCH CRACK AT STA XFS 766.500. REMOVED FASTENERS PER SRC2 PG 1. STOP DRILLED CRACK PER SRM 57-20 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE DOUBLER PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1.