As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT APPROXIMATELY 70 KNOTS THE ANTI-SKID INOP LIGHT CAME ON. ABORTED THE TAKEOFF. REMOVED THE LT ANTI-SKID TRANSDUCER WIRE BUNDLE FROM LEFT GEN TO WHEEL WELL CONNECTOR DUE TO OPEN. INSTALLED NEW WIRE BUNDLE IAW CE5650 M/M CH 32-42-00. OPS CHECKED GOOD.