What was found
LEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) PIVOT BORE CORRODED. CORROSION FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335583, PART 1, STEP 1A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) PIVOT BORE CORRODED. CORROSION FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335583, PART 1, STEP 1A.