What was found
LEFT WING OTBD FLAP INBD FWD HINGE, WING SIDE, PIVOT HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328351 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 HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328351 PART 1 STEP 1A.