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Final rule 2026-11215

Airworthiness Directives; Airbus SAS Airplanes

The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A350-941 airplanes. This AD was prompted by a determination that double overcoating sealant was not applied during production on certain fasteners in the center wing box (CWB) and belly faring junction for both left-hand (LH) and right-hand (RH) sides, and certain fasteners are also susceptible to rotation. This AD requires replacing each affected part and applying additional head nut cap protection. 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
2026-11215
Published
Jun 4, 2026
Effective
Jul 9, 2026
Comments close
Not supplied
Federal Register citation
91 FR 33593

Docket identifiers

  • Docket No. FAA-2026-2280
  • Project Identifier MCAI-2025-01562-T
  • Amendment 39-23369
  • AD 2026-11-08

CFR references

  • Title 14, part 39