by expat » Thu Sep 15, 2005 1:40 am
Hi Alrot
You are still not quite there. A yaw damper, as Midnight says is to limit Dutch Roll as indicated in his diagram. In most aircraft it is an automatic action, no pilot input is required, or he would be pumping the rudder pedals from lift off to landing to counteract this problem. A large aircraft, for example a 737, 747 does not naturally fly straight, but will have this very gentle roll motion. As the aircraft starts to Dutch Roll, the rudder is automatically deflected in the opposite direction to counteract this roll motion. It is a very small deflection, a couple of degrees only.
It is not in an emergency a button to limit the rudder movement. In an emergency, you may want all deflection that you can have. I think that you are also confusing a yaw damper with a rudder travel limiter. So here it is condensed.
Yaw damper.....automatic deflection of the rudder by a couple of degrees in the opposite direction of the Dutch Roll.
Rudder travel limiter..... Limits the amount of rudder deflection in connection with the aircrafts speed, that is, low speed allows a larger rudder movement. At high speed limits the movement, so that the pilot cannot give full deflection above a speed decided by the aircraft designer. Thus preventing stress on the aircraft and loss of control.
As for your button, if the system is not functioning correctly, the crew have the option to turn it off.
Hope this helps a little.
Matt
Last edited by
expat on Thu Sep 15, 2005 1:45 am, edited 1 time in total.
"A bit of a pickle" - British translation: A catastrophically bad situation with potentially fatal consequences.
PETA

People Eating Tasty Animals.
B1 (Cat C) licenced engineer, Boeing 737NG 600/700/800/900 Airbus A318/19/20/21 and Dash8 Q-400
1. Captain, if the problem is not entered into the technical logbook.........then the aircraft does not have a problem.
2. And, if you have time to write the fault on a napkin and attach to it to the yoke.........you have time to write it in the tech log....see point 1.