As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT 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 1.187" FINAL 1.257" MAX ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-104706. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.