As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT INBOARD HOLE BORE CORRODED. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM57-52-03. EXISTING HOLE DIA: 1.294", FINAL HOLE DIA: 1.327", MAXIMUM ALLOWABLE HOLE DIA: 1.220". OVERSIZE BUSHING FABRICATED AND INSTALLED PER EA 1-5750-127720 B PART 5 STEP 1A AND 1E. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57504773 FOR WORK DETAILS.