As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AIRCRAFT REJECTED TAKEOFF AT 65 KNOTS WITH 63,600 KG WEIGHT, DUE TO CONFIGURATION ALARM WAS SHOWED. PERFORMED TAKEOFF WARNING SYS TEST IAW AMM 31-51-00-730-803 & FIM 27-81 TASK 811 PROCEDURE, SHOWING FAILURE CODE 31-55008. THE CB P6-3, C-18 & D18 WERE REESTABLISHED & THE FIM 31-51 TASK 801 WAS PERFORMED, NO FAILURE WAS FOUND. THE HIGH ENERGY STOP INSPECTION WAS NOT NECESSARY DUE TO THE MAXIMUM GROSS WEIGHT 54 800 KG & BRAKES ON SPEED 110 KNOTS WERE NOT EXCEEDED IAW MM 05-51-07.