As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.093 FINAL DIAMETER: 1.126 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.