As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ACFT REQUIRES LARGER THAN NORMAL INPUTS ON ROLL AXIS. PARTICULARLY NOTICEABLE AT SLOW SPEEDS DURING LANDING. DURING LANDING WITH 10 KT CROSSWIND, YOKE WAS AT LT STOP AND COULD NOT STOP ACFT ROLL. FOUND LT ROLL SPOILER PCU BELL CRANK STIFF. LUBRICATED AND C/W AILERON/SPOILER ROLL CONTROL SYS. OP'S TEST IAW MM 27-10-00.