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 HAS A 1 INCH CRACK AT STA XFS 772.500. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024 T3 AL 0.032) PER SRM 57-2-0. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1.