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Airworthiness directives › 2025-09-03

AD 2025-09-03 Airworthiness Directives; Bell Textron Canada Limited Helicopters

Superseded. This directive was replaced by AD 2026-13-12. Work to the current one.
2025-05-13
2025-04-28
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Airframe
2026-13-12

Models named: 430. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Bell Textron Canada Limited Model 430 helicopters, serial numbers 49001 through 49129 inclusive, certificated in any category.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

Except as specified in paragraphs (h) and (i) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, Transport Canada AD CF-2024-40, dated December 3, 2024 (Transport Canada AD CF-2024-40).

Unsafe condition

This AD was prompted by an in-flight failure of the main rotor (M/R) pitch link clevis (clevis) due to fatigue damage and excessive wear. The FAA is issuing this AD to detect and address wear and damage of the M/R pitch link assembly components. The unsafe condition, if not addressed, could result in crack initiation at the M/R clevis neck and failure of the M/R pitch link, which could result in loss of control of the helicopter.

Affected ADs

This AD replaces AD 2021-24-09, Amendment 39-21830 (86 FR 66158, November 22, 2021).

Read the original on the Federal Register →

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1