As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING CTR L/E FORMER CRACKED 1.000 AT STA XFS 385.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE DOUBLER WITH NEW FASTENERS ON LEFT WING CTR L/E FORMER IAW SMR 57-2-0 PG 9-10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1.