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 HAND CLEANED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG. 442-444. ORIGINAL 1.2555" FINAL 1.2555" MAX ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PER E.A. 1-5750-106570. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.