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The FAA proposes to supersede Airworthiness Directive (AD) 2025-09-03, which applies 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, universal to pitch link bolts, the tube assembly, and the rod end assembly and requires replacing the M/R pitch link assemblies with re-identified 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 proposed AD proposes changes to actions in AD 2025-09-03 and addresses the comments received. The FAA is proposing this AD to address the unsafe condition on these products.
Published
Apr 7, 2026
Comments Close
May 22, 2026(46d)
Citation
91 FR 17610
Agencies
2
46 days remaining — closes May 22, 2026.
Full text not available in our database.
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Docket No. FAA-2026-3476
Project Identifier MCAI-2025-01366-R
2120-AA64
14 CFR 39