As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT I/B BORE SURFACE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING THICKNESS: 0.729", MATERIAL REMOVED: 0.026" REMAINING THICKNESS: 0.703". REPAIR SHIM FABRICATED AND INSTALLED AS PER EO 1-5750-T0335622 PART 1 STEP 2. FLIGHT SURFACES EO 1-5750-7-5002-RT WING OUTBD FLAP INBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.