As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING L/E FRAME UPPER PART AT STA 649.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNESS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE PER SRM57-2-0 PG 9-10 AND SRM 51-1-21-PG 1.