As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) IN REFERENCE TO SERVICE DIFFICULTY ADVISORY AV-96-06, INSPECTION CARRIED OUT ON THE CLEVIS PIN IN THE POWER LEVER SYSTEM. THE PINS IN THE LEFT AND RIGHT ENGINES WERE NOTICEABLY WORN, AND THE COTTER PIN HOLES ELONGATED. BOTH CLEVIS AND COTTER PINS WERE REPLACED.