As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT HAND INBD FLAP PIVOT POINT OUTBOARD BORE HAS GROOVE MARK. REMOVED CORROSION IAW DAC CMM 57-52-01. BEGINNING DIAMETER 1.1875 INCH FINAL 1.2552 INCH . FABBED REPAIR BUSHING IAW DACCMM 57-52-01 AND EA8-5750-81475 MPI IAW DACCMM 5752-01 AND DPS 4.704 CAD PLATED, INSTALLED AND HONED BUSHING IAW DACCMM 57-52-01.