Resumen
We are adopting a new airworthiness directive (AD) for Bell Helicopter Textron Canada Limited (Bell) Model 429 helicopters. This AD requires inspecting each tail rotor (T/R) pitch link (link) bearing bore for corrosion and pitting and either replacing the T/R link or applying sealant. This AD also requires a recurring inspection of the sealant and repeating the inspections for corrosion and pitting if any sealant is missing. This AD is prompted by an incident in which a helicopter experienced an in-flight failure of a T/R link. These actions are intended to detect corrosion or pitting and to prevent failure of a T/R link and subsequent loss of control of the helicopter.
Detalles de la directiva
Número de AD
FAA-2016-2068
Número de documento
2016-01747
Tipo
Rule
Fecha de publicación
February 2, 2016
Fecha de entrada en vigor
February 2, 2016
Fabricante afectado
Bell Helicopter Textron Canada Limited
Criticidad
important
Emergencia
No
Docket ID
Docket No. FAA-2016-2068
Temas
Documentos oficiales
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