As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) WHEN TAKEOFF POWER APPLIED, CONFIGURATION WARNING HORN CAME ON AND ENGINE INDICATING AND CREW ALERT SYSTEM MESSAGE SPOILERS ANNUNCIATED, LEVER IN FORWARD DOWN POSITION, TAKEOFF REJECTED. SPEED BRAKE CONTROL ROD ADJUSTED PER MM 27-62-04. AUTO SPEED BRAKE TEST CARRIED OUT, SYSTEM SERVICEABLE.