As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG 442-444. ORIGINAL THK 1.1875" FINAL 1.257" MAX ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PER E.A.1-5750-104705. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.