What was found
LEFT WING OTBD FLAP, INBD FWD HINGE BRACKET PIVOT BORE FOUND CORROSION. EXCEEDED LIMITS IAW CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330806 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 FWD HINGE BRACKET PIVOT BORE FOUND CORROSION. EXCEEDED LIMITS IAW CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330806 PART 1 STEP 1B.