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 NR 5 SUPPORT FITTING BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R, FIG 201. AN OVERSIZED BUSHING WAS FABRICATED IAW EA1-5750-T0335345, PART 1, STEP 1A. INSTALLED IAW AMM 27-50-32-4. LT WING FLAP VANE ADJUSTEMENT AND TEST CARRIED OUT IAW AMM 27-50-30-5 AND FOUND SATISFACTORY.