What was found
WHEN AUTOPILOT A-SIDE ENGAGED SYSTEM FLAGGED FAIL CYCLED TO B-SIDE, AND DEFECTED RIGHT RUDDER INPUTS RUDDER INPUTS BECAME INCREASINGLY AGGRESSIVE PIC AND SIC COMMAND BARS SHOWED 2-3 DEGREES TO BANK DISAGREEMENT. RAN AUTOPILOT TEST IAW CE650 MM 22-10-00; NO DEFECTS NOTED. PERFORMED GROUND CHECK OF THE SPZ-8000 SYSTEM IAW HONEYWELL TECH PUB A15-1146-058 CHAPTER 22-05-07, FOUND NO ERRORS. NO FAULTS STORED IN FLIGHT FAULT SUMMARY. SWAPPED FGC'S & PERFORMED OPS CHECKS. OPS CHECKED GOOD PER ABOVE REFERENCES.