As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DELAYED ROLL WITH RIGHT AILERON INPUT. PITCH NORMAL, LEFT AILERON NORMAL. FOUND AILERON CONTROL WHEEL FORCE VERY LOW (BREAKOUT FORCE 5 IN LB) ADJUSTED AILERON FEEL & CENTERING UNIT AS PER MM 27-11-00-820-804. PERFORMED AILERON TRAVEL TEST AS PER MM 27-11-00-700-809. CHECKED SPOILER DEFLECTION AS PER MM 27-61-00-820-804. ALL CHECKED GOOD.