As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT INBD LUG HOLE FOUND CORROSION. CORROSION (HOLE F AND G) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-73337 D PART 4 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.