What was found
RIGHT WING OUTBD FLAP INBD FWD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133 PART 1, STEP 1A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING OUTBD FLAP INBD FWD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133 PART 1, STEP 1A.