As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING I/B FLAP ASSY O/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE CORROSION. HINGE PIVOT INBD BORE (HOLE G & F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.2565", FINAL HOLE DIA: 1.281", MAXIMUM ALLOWABLE DIA: 1.220Ï¿½. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-69374 C PART 5 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.