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Final ruleTakes effect Nov. 12, 2026

Airworthiness Directives; Airbus Helicopters

Built by the Tribune's code from the Federal Register. No AI wrote this page. Published in the Federal Register Oct. 27, 2026. Document 2026-21854. Updated Nov. 5, 2026.

What it does

The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model SA 365 N helicopters. This AD was prompted by reports of tightening torque loss on the input flange nut due to circular wear on the faces of the flange, the slip ring, and the input flange. This condition, if not addressed, could lead to degradation or jamming of the input roller bearings and loss of yaw control of the helicopter. This AD requires repetitive functional inspections (checks) and, depending on the results of the inspections, corrective actions. The FAA is issuing this AD to address the unsafe condition on these products.

The Federal Aviation Administration's summary, as published in the Federal Register.

What changed in the regulation

1 part of Title 14 of the Code of Federal Regulations:

14 CFR 39

Compared with

The Federal Aviation Administration has published 476 final rules in 2026 so far, compared with 518 in all of 2025.

Counted by the Tribune from Federal Register records since Jan. 1, 2025.

Before this

1075 earlier Federal Register documents under regulation identifier 2120-AA64 since Jan. 1, 2025.

Since then:

What happens next and when

This AD is effective November 12, 2026.

The agency's dates, word for word.

Document number2026-21854
ActionFinal rule; request for comments.
AgenciesTransportation Department; Federal Aviation Administration
PublishedOct. 27, 2026
Effective dateNov. 12, 2026
Comments closeDec. 11, 2026
Regulation identifier (RIN)2120-AA64
DocketFAA-2026-11815

Source: the Federal Register (public domain). The document in the Federal Register