since 1940

Aircraft parts
for those who work on airplanes

  Home |  Software | Knowledge Base |  Customer service |  Products  

Home> Maintaining your Continental  and Lycoming engine  

Cessna Nose Wheel Shimmy

Download Shimmy Program (325KB)

This article is from an attachment to Cessna Service Information Letter SE84-21 dated November 9, 1984

 Nose wheel shimmy conditions may be caused by any one of the following, but are usually the result of a little of all four problems.

 1. Nose wheel and tire assembly balance.

 This is the most important point to check in trying to solve a nose wheel shimmy condition. It's also one of the most overlooked points, probably due to the lack of availability of aircraft wheel balancing equipment in the field. All Cessna Dealers have wheel- balancing equipment.

 2. The torque links (scissors)

 The torque link bushings and bolts should be checked for looseness and wear. One way to determine if the torque links are the cause is to replace the three castellated nuts on the torque link bolts with regular nuts, and perform this test: Tighten the nuts tighter than you would normally tighten a castellated nut to squeeze the links together to remove any excessive looseness. Make sure that the shimmy dampener and the nose gear strut are properly serviced. A high speed taxi test should tell you if the torque links are the cause. If they are, replace bushings and bolts as necessary and reinstall with castellated nuts.

 3. The steering arm assembly shims (fixed gear aircraft only)

 These shims are located between the bottom of the steering arm and the bottom of the shock strut outer tube. After a period of time, these shims will wear, allowing the steering arm to move up and down. When this happens, any shimmy movement becomes a vertical movement rather than a horizontal movement that can be dampened out by the shimmy dampener. These shims are available in various thickness and are used as necessary to obtain a snug fit. Access to the shims requires removal of the shock strut assembly from the aircraft.

 4. The shimmy dampener

 The shimmy dampener should be properly serviced and the attach points checked for looseness. The shimmy dampener should provide the same amount of resistance from one end of the piston rod travel to the other. Since most of the shimmy dampener piston travels in the center of the housing, the center portion of the housing will usually show the most wear. When the housing becomes worn to the point that the piston can no longer provide a good seal, the fluid will bypass around the piston instead of going through the orifices in the piston. When this happens , you loose the restriction that provides the dampening action for the nose wheel assembly.

 Many times the nose wheel fairing is blamed for a shimmy condition. Unless the fairing is actually loose, it will not cause a shimmy. However, the added weight of the wheel fairing may allow the nose wheel assembly to resonate after a shimmy has started.

 
In combat, you are a beautiful target for enemy airmen while floating down, calm and serene, under your sky umbrella. Parachute Sense US NAVY 1944



 

 


 

online privacy policies 
site terms of use
terms and conditions of sale

Information about how to download this site for off-line reading

  Webmaster: john@sacskyranch.com 

Copyright 2003 by Sacramento Sky Ranch Inc. All rights reserved.  Prices subject to change without notice. Not responsible for typographical or misprint.
Disclaimer: sacskyranch.com contains abundant information relating to aircraft maintenance. The information provided  is not intended to supercede or supplement the F.A.A. approved  maintenance and/or operator’s manuals. Those F.A.A. approved manuals must be utilized when performing maintenance and/or operating aircraft.