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Final rule 2026-16507

Airworthiness Directives; Airbus Helicopters

The FAA is adopting a new airworthiness directive (AD) for certain Airbus Helicopters Model AS350B2 helicopters. This AD was prompted by a report of magnetization on the solenoid valves for the three main servo-controls, the regulator block, and the tail servo- control due to a diode not properly installed in the hydraulic circuit. This AD requires performing a cut-off test of the rear rotor actuator valve and, depending on the results of the test, performing corrective actions. The FAA is issuing this AD to address the unsafe condition on these products.

Source: FederalRegister.gov API v1Recently refreshed. Last successful refresh: 2026-08-13 08:49:02 UTC.

Source-supplied record

Document details

Document number
2026-16507
Published
Aug 13, 2026
Effective
Sep 17, 2026
Comments close
Not supplied
Federal Register citation
91 FR 52221

Docket identifiers

  • Docket No. FAA-2026-4646
  • Project Identifier MCAI-2025-01763-R
  • Amendment 39-23435
  • AD 2026-16-05

CFR references

  • Title 14, part 39