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Final rule 2025-17850

Airworthiness Directives; Airbus Helicopters

The FAA is adopting a new airworthiness directive (AD) for certain Airbus Helicopters Model AS 332L2 and EC 225LP helicopters. This AD was prompted by reports of overlengthened and deformed attachment bolts installed on the link of the main gearbox (MGB) suspension bar attachment bracket. This AD requires replacing certain attachment bolts on the MGB suspension bar fittings, inspecting the removed bolts, and reporting the results of this inspection to Airbus Helicopters. 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
2025-17850
Published
Sep 16, 2025
Effective
Oct 21, 2025
Comments close
Not supplied
Federal Register citation
90 FR 44493

Docket identifiers

  • Docket No. FAA-2025-0914
  • Project Identifier MCAI-2024-00413-R
  • Amendment 39-23136
  • AD 2025-18-09

CFR references

  • Title 14, part 39