As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING I/B FLAP O/B HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. LT FWD I/B FLAP O/B HINGE PIVOT HOLE SPOTFACE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-07 PG.403-404. ORIGINAL THK I/B 0.461" O/B 0.435" REMAINING THK I/B 0.445" O/B 0.426". MATERIAL REMOVED I/B 0.016" O/B 0.009". MIN ALLOWABLE 0.450". REPAIR CARRIED OUT AS PER E.A.1-5750-104702. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.