What was found
RUDDER FAIL CAS ON SHORT FINAL. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RUDDER REMOTE ELECTRONICS UNIT 16. PERFORMED SUCCESSFUL RUDDER ACTUATING SYSTEM IBIT SUITE A TEST. PERFORMED SUCCESSFUL RUDDER FUNCTIONAL TEST. CLOSED LEFT AND RIGHT VERTICAL STABILIZER ACCESS PANELS. NO DEFECTS NOTED AT THIS TIME. WORK COMPLETED IAW G650 AMM 27-25-01, 27-20-00, 27-02-01,27-01-01 AND 20-00-00.