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 PART WITH 2 INCH CRACK AT STA XFS 521.250. STOP DRILLED CRACK PER SRM 57-2-0. FABRICATED DOUBLER ANGLE (2024.T3 AL 0.063) PER SRM PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 57-2-0 PG 9-10.