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 O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA 1.188"-1.220, FINAL HOLE DIA: 1.250", MAXIMUM ALLOWABLE DIA 1.220. REPAIR BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-71744 C PART 5 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.