What was found
DURING A MAINTENANCE VISIT, FOUND CRACK IN BUSHING HOLE OF THE 5751153-7 FLAP LINK, AT XF=219 LINK, LOC RT OB FLAP DRIVE FWD LINK. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER TIMCO ENGINEERING SKETCH REO-03127.