What was found
LEFT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT OUTBOARD BORE CORRODED. REMOVED CORROSION FROM BORE IAW DAC CMM 57-52-01. ALODINED AND PRIMED BORE IAW DC10-10 SRM 51-21-01 VOL 2, FABRICATED AND INSTALLED FINAL HONED NEW OVERSIZED BUSHING TO 0.9995-1.0005 IAW DAC CMM 57-52-01 AND EA 8-5750-83998, WINGS LEFT INBOARD FLAP, OUTBOARD HINGE BRACKET OVERSIZE PIVOT BORES AND STRAP REPAIR. REFERENCE NON-ROUTINE N00468.