As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING, WING SIDE OTBD FLAP OTBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW EA 1-5750-76015A. UPPER EXISTING THICKNESS;0.401" MATERIAL REMOVED: 0.002" REMAINING THICKNESS : 0.399" LOWER EXISTING THICKNESS : 0.417" MATERIAL REMOVED: 0.002" REMAINING THICKNESS : 0.415" . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.