What was found
UNABLE TO TRIM AIRCRAFT AFTER TAKEOFF. RECEIVED PRI STAB TRIM FAIL CAS SHORTLY AFTER. ACTIVATED SECONDARY TRIM AND WAS ABLE TO TRIM. POWERED ON THE ACFT AND VERIFED "PRI STAB TRIM FAIL" CAS HARD FAILED. REMOVED H STAB TRIM ACTUATOR AND INSTALLED A CUS SUPP OVERHUALED HSTA SATISFACTORILY PERFORMED PITCH TRIM RIGGING, STABILIZER TRIM POINTER RIGGING, AND PRIMARY STABILIZER TRIM ACTUATOR TRAVEL CHECK IAW CE-680A AMM 27-40-05 WITH NO DEFECTS NOTED. CAL TOOLING: TORQUE WRENCH TL-104160 INCLINOMETER TL-00557