As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING FINAL APPROACH LONG TRIM WAS STUCKED, THE NOSE COMPENSATION UP WAS NOT POSSIBLE. THE PRIMARY ACTUATOR ENGINE WAS REPLACE. THE GEAR BOX ASSY TRIM AND ALTRENATE ENGINE WERE REPLACED IAW MM AND RELAY LONGITUDINAL TRIM WAS REPLACED IAW, TESTS CORRECT.