As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04 PG. 621-622. ORIGINAL THK. 1.1565" FINAL 1.1895" MAX. ALLOWABLE 1.150". FABRICATED BUSHING AND INSTALLED AS PER E.A.1-5750-97766.