What was found
LEFT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION FROM BORE IAW DAC CMM 57-52-01, ALODINE AND PRIMED BORE IAW DC19-10 SRM 51-21-01 VOL 2. FABRICATED AND INSTALLED AND FINAL HONED NEW OVERSIZED BUSHING TO 0.9995-1,0005 INCHES IAW DAC CMM 57-52-01 AND EA 8-5750-83998, WINGS-LEFT INBOARD FLAP, OUTBOARD HINGE BRACKET OVERSIZE PIVOT BORES AND STRAP-REPAIR.