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Final rule 2026-17615

Airworthiness Directives; Bell Textron Canada Limited Helicopters

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: FederalRegister.gov API v1Recently refreshed. Last successful refresh: 2026-08-28 08:49:02 UTC.

Source-supplied record

Document details

Document number
2026-17615
Published
Aug 28, 2026
Effective
Sep 14, 2026
Comments close
Not supplied
Federal Register citation
91 FR 55446

Docket identifiers

  • Docket No. FAA-2026-8788
  • Project Identifier MCAI-2026-00842-R
  • Amendment 39-23453
  • AD 2026-17-51

CFR references

  • Title 14, part 39