What was found
DURING INSPECTION, FOUND DAMAGE THREADS ON THE BOLT OF THE HORIZONAL STAB TRIM ACTUATOR SUPPORT PLATE. DAMAGE TRIM ACTUATOR WAS REMOVED. SAME SERVICEABLE STAB TRIM ACTUATOR WAS AS REINSTALLED IAW AMM 27-41-81. TESTED OK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND DAMAGE THREADS ON THE BOLT OF THE HORIZONAL STAB TRIM ACTUATOR SUPPORT PLATE. DAMAGE TRIM ACTUATOR WAS REMOVED. SAME SERVICEABLE STAB TRIM ACTUATOR WAS AS REINSTALLED IAW AMM 27-41-81. TESTED OK.