As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING O/B FLAP I/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL LUG THICKNESS: 0.403, MATERIAL REMOVED: 0.005, REMAINING THICKNESS OF LUG: 0.398 REWORKED AREA REPAIRED AS PER EA 1-5750-76670. LT O/B FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR.