As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHEN SPEED BRAKE APPLIED PARTIALLY OR FULLY IN FLIGHT, AIRCRAFT ROLLS TO THE RIGHT. A 10 TO 15 DEGREES OF TRIM LT CONTROL WHEEL INPUT REQUIRED FOR LEVEL FLIGHT. FOUND NR 2 AND NR 3 FLIGHT SPOILERS OUT OF LIMITS. ADJUSTED NR 2 AND NR 3 FLIGHT SPOILER ACTUATOR INPUT RODS PER BMM 27-61-00. OPERATES NORMALLY WITHIN LIMITS.