As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING T/E ATTACH ANGLE HAS A GOUGE ON THE OTBD END; LWR SURFACE UNDER PANEL 572 PB. CHECKED DAMAGE AND FOUND TO BE OUT OF LIMITS IN REF TO SRM 57-51-11; FIG 102; ORIGINAL THICKNESS IS 0.048; REMAINING THICKNESS IS 0.015. CUT OUT DAMAGE IN REF SRM 57-51-11; FIG 207. FABRICATED REPAIR ANGLE AND FILLER IN REF TO SRM 57-51-11; FIG 207. ALODINED ; PRIMED AND PAINTED IN REF AMM 51-23-10-0. INSTALLED THE REPAIR IN REF TO SRM 57-51-11; FIG 207.