Airworthiness Directive

AD 2026-17-51 91 FR 55446

Federal Aviation Administration · 14 CFR part 39

FR document
2026-17615
Amendment
39-23453
Published
2026-08-28
Models covered
1
Last live check
2026-09-01
AD

2026-17-51

FR doc 2026-17615 · 91 FR 55446

AD 2026-17-51Published 2026-08-28Effective 2026-09-14

Federally required — FAA rule. Every Airworthiness Directive is a legally enforceable FAA rule (14 CFR 39.3); operating a product that does not meet it is a violation (14 CFR 39.7).

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.

Full official 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.

Applies to 1 model in our index

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