As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
HIGHER THAN NORMAL CONTROL FORCE REQUIRED WHEN APPLYING AND NEUTRALIZING RT ROLL INPUTS FROM CTR OS ON BOTH YOKES IN FLIGHT. INSPECTED RIGGING OF AILERON FEEL AND SENSORY MECHANISM ON BOTH SIDES. ADJUSTED IAW AMM 27-11-00. OPS CHECK GOOD.