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Airworthiness Directives; Bell Helicopter Textron Canada Limited Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 2015-10-27 · Effective 2015-11-12 · 80 FR 65618

Document

Document number
2015-27137
Federal Register citation
80 FR 65618
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Bell Helicopter Textron Canada Limited
Publication date
2015-10-27
Effective date
2015-11-12
FAA docket
Docket No. FAA-2015-4345

Abstract

We are superseding emergency airworthiness directive (AD) No. 2015-16-51 (Emergency AD 2015-16-51) for Bell Helicopter Textron Canada Limited (Bell) Model 429 helicopters. Emergency AD 2015-16-51 required inspections of each inboard and outboard tail rotor pitch link assembly for axial or radial bearing play, and if there was axial or radial bearing play, removing the tail rotor pitch link and inspecting for wear. Emergency AD 2015-16-51 was prompted by several reports of worn tail rotor pitch link spherical bearings. We are issuing this supersedure to retain the inspection requirements in Emergency AD 2015- 16-51 while revising the applicability and compliance time to clarify that all Bell Model 429 helicopters require recurring inspections regardless of hours time-in-service (TIS) accumulated on the helicopter. These actions are intended to prevent pitch link failure and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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