What was found
RIGHT 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 EA 1-5750-73360 D, PART 3, STEP 1. THE REPAIR WAS 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.
RIGHT 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 EA 1-5750-73360 D, PART 3, STEP 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.