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Final rule 2026-11511

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 manufacturing investigation that found improper application of the fastener retorque process at the center wing box (CWB) and belly fairing (BF) junctions could lead to insufficient clamping. 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
2026-11511
Published
Jun 9, 2026
Effective
Jul 14, 2026
Comments close
Not supplied
Federal Register citation
91 FR 34750

Docket identifiers

  • Docket No. FAA-2026-3475
  • Project Identifier MCAI-2025-01561-T
  • Amendment 39-23374
  • AD 2026-12-04

CFR references

  • Title 14, part 39