As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING C-CHECK, THE LT ENGINE THRUST LEVER CONTROL CABLE (T1A) WAS FOUND TO BE CHAFED AND HAD BROKEN CABLE STRANDS. DURING INSTALLATION OF NEW CABLE, IT WAS FOUND THAT THE T1A CABLE HAD BEEN ROUTED UNDER THE CABLE GUARD INSTEAD OF OVER, CONTRIBUTING TO THE ABOVE MENTIONED DAMAGE TO THE THRUST LEVER CONTROL CABLE. TIMES 60322.07 CYCLES 56643.