As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(AUS) CONTROL CABLES ATTACHED TO PRIMARY CONTROL QUADRANT IN CONTROL COLUMN YOKE HAD FAULTY SWAGING - DURING TESTING CABLES PULLED THROUGH THE NICOPRESS SLEEVES AT A LOAD OF 610 LBS (NORMAL FAILURE LOAD 2200 LBS TO 2300LBS) - AIRCRAFT IS IMPORTED FROM THE USA AND IS UNDERGOING INITIAL COFA - US REGISTRATION N94022