As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON LANDING THE POWER LEVERS WERE BROUGHT TO IDLE AND LEFT ENGINE FAILED (AT IDLE). ADJUSTED FLOW DIVIDER TO FUEL CONTROL INTERCONNECT ROD FOR PROPER IDLE DETENT. RIGGED AFT POWER CONTROL CABLE TO PROVIDE SLIP FIT OF ROD END AT BOLT. GROUND RAN AND NUMEROUS RAPID POWER LEVER REDUCTIONS TO IDLE DID NOT CAUSE ENGINE TO SHUT DOWN, ALL WORK PERFORMED IN ACCORDANCE WITH CESSNA 560 MAINTENANCE MANUAL CHAPTER 76-11-00.