What was found
LEFT WING INBD FLAP FWD (WING SIDE) OTBD HINGE PIVOT HOLE BORE CORRODED. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-07 AND PER EA 1-5750-T0328840 D, PART 1, STEP 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING INBD FLAP FWD (WING SIDE) OTBD HINGE PIVOT HOLE BORE CORRODED. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-07 AND PER EA 1-5750-T0328840 D, PART 1, STEP 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.