Skip to content
Politically.com Search all
Menu

Final rule 2026-16641

Airworthiness Directives; Airbus Helicopters

The FAA is superseding Airworthiness Directive (AD) 2023-25- 14, which applied to certain Airbus Helicopters Model EC130T2 helicopters. AD 2023-25-14 revised the procedures for inspecting the vibration level on the tail rotor drive shaft and, depending on these results, required replacing certain parts. Since the FAA issued AD 2023-25-14, the manufacturer developed a modification of the rear drive shaft, sliding flange, and equipped splined sleeve. This AD requires installing this modification and repetitively inspecting the vibration level of the tail rotor drive shaft. This AD also prohibits the installation of certain parts and prohibits the performance of a balance correction unless certain requirements are met. The FAA is issuing this AD to address the unsafe condition on these products.

Source: FederalRegister.gov API v1Recently refreshed. Last successful refresh: 2026-08-15 08:49:02 UTC.

Source-supplied record

Document details

Document number
2026-16641
Published
Aug 14, 2026
Effective
Sep 18, 2026
Comments close
Not supplied
Federal Register citation
91 FR 52494

Docket identifiers

  • Docket No. FAA-2026-4644
  • Project Identifier MCAI-2024-00418-R
  • Amendment 39-23440
  • AD 2026-16-10

CFR references

  • Title 14, part 39