As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING I/B FLAP ASSY O/B AFT HINGE (FLAP SIDE) PIVOT O/B BORE CORROSION. HINGE PIVOT O/B BORE (HOLE A & B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.255", FINAL HOLE DIA: 1.283", MAXIMUM ALLOWABLE DIA: 1.220. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0324370 C PART 4 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.