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Final rule 2026-01180

Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Deutschland GmbH (AHD) Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, EC635T2+, and EC135T3 helicopters. This AD was prompted by reports of ruptured and deformed flexible couplings. This AD requires inspecting the axial displacement of the tail rotor drive shaft and, depending on the results, taking corrective actions including inspecting the flexible couplings. This AD also prohibits installing a tail rotor drive shaft unless certain procedures are followed. 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
2026-01180
Published
Jan 22, 2026
Effective
Feb 26, 2026
Comments close
Not supplied
Federal Register citation
91 FR 2681

Docket identifiers

  • Docket No. FAA-2025-0629
  • Project Identifier MCAI-2023-01183-R
  • Amendment 39-23237
  • AD 2026-02-01

CFR references

  • Title 14, part 39