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Final rule 2026-13685

Airworthiness Directives; Bell Textron Canada Limited Helicopters

The FAA is superseding Airworthiness Directive (AD) 2025-09- 03, which applied to certain Bell Textron Canada Limited (Bell) Model 430 helicopters. AD 2025-09-03 reduced the life limits on the main rotor (M/R) clevises, universal bearings, and universal to pitch link bolts and required re-identifying the M/R pitch link assemblies with new part numbered assemblies. Since the FAA issued AD 2025-09-03, the FAA received comments proposing changes to the actions of AD 2025-09- 03. This AD requires changes to the actions in AD 2025-09-03 and addresses the comments received on that AD. The FAA is issuing this AD to address the unsafe condition on these products.

Source: FederalRegister.gov API v1Recently refreshed. Last successful refresh: 2026-07-31 22:49:02 UTC.

Source-supplied record

Document details

Document number
2026-13685
Published
Jul 7, 2026
Effective
Aug 11, 2026
Comments close
Not supplied
Federal Register citation
91 FR 41539

Docket identifiers

  • Docket No. FAA-2026-3476
  • Project Identifier MCAI-2025-01366-R
  • Amendment 39-23395
  • AD 2026-13-12

CFR references

  • Title 14, part 39