As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING CTR L/E FORMER UPPER PART WITH 1 INCH CRACK AT STA XFS 416.500. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCEMENT ANGLE (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCEMENT ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1.