As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING A ROUTINE LANDING GEAR INSPECTION THE RT UPPER TORQUE LINK SHAFT WAS FOUND TO BE PROTRUDING FROM THE RT TORQUE LINK. THE SHAFT HAD FRACTURED INSIDE THE STRUT. PROTRUDING PORTION WAS APPROX 1 1/2` LONG. THE REMAINING PORTION OF THE SHAFT WAS REMOVED. GEAR STRUT WAS INSPECTED AND THE SHAFT WAS REPLACED.