What was found
LEFT WING OTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING OTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1B.