Aircraft experienced nosewheel shimmy leading to nose gear failure upon landing.

The pilot stated that he landed the airplane on the main landing gear and then lowered the nose landing gear on the runway. The nosewheel started to shimmy, and the pilot applied aft pressure on the control yoke; however, the nose landing gear strut assembly subsequently separated from the airplane and the airplane veered right and came to rest in the grass off the right side of the runway. The pilot further stated that he had experienced a shimmy event about 50 flight hours before the accident, and he decided to install a shimmy dampener on the airplane. Metallurgical examination of the components revealed the nose landing gear separated due to a preexisting fatigue crack caused by the earlier shimmy event and the subsequent incorrect installation of the shimmy dampener. Specifically, the shimmy dampener alignment pin had not been installed, which rendered the shimmy dampener ineffective.

| NTSB Final | ERA12LA431| Full |

Posted By: Brett Ferrell
Monday July 2nd, 2012 at 6:25 PM

Categories: Accidents
Tags: 2012 Accident GA Leder N224SM Non-Fatal RG Thomson Velocity XL

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