As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING O/B L/E FRAME AT STA XRS 616.250 WITH A 1/2 INCH CRACK IN IT. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 AL 0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-20D PG 9.