As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON CLIMB-OUT WITH A/P ON NOTICED CONTROL WHEEL DEFECTED 2 DEGREES RIGHT WITH A/P OFF RUDDER TRIM PLACED 7 DEGREES RIGHT TO CENTER WHEEL. REMOVED LEFT INBD AIL PCA OUTBD PCA LT SYS OK TO INSTALL PCA S/N 3666. INSTALLED LEFT INBD AIL OUTBD PCA INSTALLATION OK. ADJ TEST OK. SAFTY AND SECURITY CHECK OK RII INSPECTIONS C/W MM 27-11-48 FOR REMOVAL AND INSTALLATION OF LT I/B AILERON PCA.