As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE CENTER SUPPORT ANGLE STRUCTURE FOUND CHAFED. REMOVED AS PER CMM 20-11-02 AND FOUND WITHIN DRAWING ARC2126 DESIGN LIMIT. ORIGINAL THICKNESS = 0.180", REMAINING THICKNESS = 0.175", MATERIAL REMOVED = 0.005". REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.