What was found
RUDDER RATIO EICAS AFTER TAKEOFF BRIEFED CREW ; NO OVERWEIGHT LANDING,PILOT STATED PLANE FLEW FINE ,JUST EICAS MSG AFTER TAKEOFF PERFORMED FIM TASK RUDDER RATION EICAS MSG 27-21 FAULT TREE PERFORMED YAW DAMPER SYSTEM BITE AS PER FIM 22-21 FAULT TREE 803 804.RUDDER RATIO CONTROL MODULE BITE TEST PER FIM TASK 27-09 AT THIS TIME NO FAULTS WERE OBSERVED AND NO INDICATIONS ON FAULT TREE 814.SAM BITE PROCEDURE 27-09 FAULT TREE 811 AND OVERHEAD PANEL OR EICAS WERE SEEN. SPOILER CONTROL MOD.BITE TEST PER FIM 27-09 FAULT TREE 807.ALSO