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AD FAA-2016-2068

Airworthiness Directives; Bell Helicopter Textron Canada Limited

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

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de Bell Helicopter Textron Canada Limited →

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