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Airworthiness Directives; Bell Helicopter Textron Canada Limited

airworthiness · Rule · Final rule; request for comments. · Published 2016-02-02 · Effective 2016-02-02 · 81 FR 5367

Document

Document number
2016-01747
Federal Register citation
81 FR 5367
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2016-02-02
Effective date
2016-02-02
FAA docket
Docket No. FAA-2016-2068

Abstract

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.

Source

Authoritative
Federal Register document
Machine
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