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How It Works: Yaw Damper

A) The soul of a yaw damper rests with rudder servos, accelerometers and rate sensors, often located in the tail of the airplane. B) In most aircraft, the yaw damper sensors are constantly talking back and forth to the primary onboard reference system, such as the ADAHRS. C) The yaw damper on some aircraft turns on and off automatically, making it one more thing the PIC need not worry about forgetting. Illustration by Tim Barker
Gemini Sparkle

Key Takeaways:

  • A yaw damper automatically controls an aircraft's movement around its vertical axis by applying rudder inputs, preventing "fishtailing" in single-engine planes and inhibiting "Dutch roll" in swept-wing aircraft.
  • It uses sensors like accelerometers to detect yaw movements and communicates with avionics systems to provide calming rudder pressure, ensuring coordinated turns and enhancing passenger comfort.
  • While some systems are pilot-selectable, modern yaw dampers (e.g., Cirrus SR22) can engage and disengage automatically at specific altitudes; however, pilots may need to deactivate them during critical phases like takeoff or landing in certain aircraft to maintain full control authority or facilitate engine failure identification.
  • Over-reliance on yaw dampers can diminish a pilot's manual rudder skills, which becomes apparent when flying aircraft without the system or with an inoperative damper.
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In its most basic form, a yaw damper inhibits movement of an aircraft around its vertical axis, performing like an automated set of feet on the rudder pedals.

Rob Mark

Rob Mark is an award-winning journalist, business jet pilot, flight instructor, and blogger.

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