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Airworthiness Directives; Bell Textron Canada Limited Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 2026-08-28 · Effective 2026-09-14 · 91 FR 55446

Document

Document number
2026-17615
Federal Register citation
91 FR 55446
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Bell Textron Canada Limited
Publication date
2026-08-28
Effective date
2026-09-14
FAA docket
Docket No. FAA-2026-8788

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Bell Textron Canada Limited Model 222 helicopters. The FAA previously sent this AD as an emergency AD to all known U.S. owners and operators of these helicopters. This AD was prompted by a report of in- flight fatigue failure of a tail rotor pitch horn. This AD requires removing the affected tail rotor pitch horn and associated tail rotor pitch links from service and installing a serviceable tail rotor pitch horn and associated tail rotor pitch links. This AD also prohibits installing an affected tail rotor pitch horn on any helicopter. The FAA is issuing this AD to address the unsafe condition on these products.

Source

Authoritative
Federal Register document
Machine
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