As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING CTR L/E FORMER UPPER PART AT STA XFS 372.000 WITH .500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED .500 CRACK ON CENTER L/E FORMER UPPER PART IAW SRM 57-2-0 PG 9-10. FABRICATED A DOUBLER ANGLE 2024T3 AL.032 IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE ON CTR L/E FORMER UPPER PART, STA XFS 372.000 IAW SRM 57-2-0 PG 9-10.