As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING OUTBOARD FLAP VANE NO. 4 SUPPORT FITTING ECCENTRIC BORE HOLE FOUND CORROSIONS. SUPPORT FITTING HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0343882 PART 1 STEP 1A. TRACK SUPPORT FITTINGS CORROSION REPAIR AND INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.