What was found
LEFT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORRODED. REWORKED IAW CMM 57-44-09. OUT OF LIMITS, A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335621, PART 1, STEP 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORRODED. REWORKED IAW CMM 57-44-09. OUT OF LIMITS, A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335621, PART 1, STEP 2.