As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 3 HAS CORROSION IN BORE. REMOVED CORROSION IAW DACCMM 57-44-07. BEGINNING BORE 2.5850 INCH FINAL 2.626 INCH MATERIAL. REMOVED .041 INCH. FABRICATED BUSHING IAW DACCMM 57-44-07 AND EA8-5750-81473. ACCOMPLISHED MPI IAW DPS 4.704. CAD PLATED BUSHING IAW DACCMM 57-44-07. ALODINED AND PRIMED BORE IAW DC10 SRM 51-21-01 VOLUME II. INSTALLED AND HONED BUSHING IAW DACCMM 57-44-07.