As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) PIVOT BORE CORROSION. HINGE PIVOT BORE(NR 4 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA: 2.309", FINAL HOLE DIA: 2.315", MAXIMUM ALLOWABLE DIA: 2.3135. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-341992 P1 STEP 1B AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.