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Dossier Executive final rule 27-oct-2026 Takes effect · 01-dec-2026 · in 21 days
Finalized regulation — legally enforceable once its effective date arrives.

Airworthiness Directives; Airbus SAS Airplanes

Key claim: The FAA proposes requiring operators of Airbus A350-941 and A350-1041 jets to inspect a door girt-bar safety hook for parts stuck by excess sealant, correct any problems, and follow extra maintenance rules.

Abstract

(Proposed Rule · Transportation Department, Federal Aviation Administration) The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus SAS Model A350-941 and -1041 airplanes. This proposed AD was prompted by a girt bar fitting safety hook on an airplane in the production line was found stuck in the upward position due to excessive sealant applied between the girt bar fitting and door mat. This proposed AD would require a detailed inspection of each affected part and applicable corrective actions, and provide additional requirements for maintenance. The FAA is proposing this AD to address the unsafe condition on these products.

[This finding represents 2 closely related documents issued 2026-10-08 (same source, same action). Related: fedreg:2026-20700]

Why this matters

Door girt bars arm the emergency escape slides, so a safety hook obstructed by excess sealant could delay or prevent slide deployment in an evacuation. This proposed AD continues a steady cadence of FAA directives targeting manufacturing-quality escapes on the Airbus A350 fleet, keeping routine production defects from becoming in-service safety hazards.

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Airworthiness Directives; Airbus SAS Airplanes
Stage: final rule · federal-register · 27-oct-2026

If you fly on an Airbus A330-941, operators of your aircraft are now required to upgrade its flight-control computer software and stop using the older parts implicated in a triple-computer landing fault.

Operators of certain Airbus A330-941 jets must install a new flight-control computer software standard and related modifications, and may no longer install specified older parts, after a triple computer fault at landing.

Cross-references (0)

None recorded — doctrine links and citations appear here as scans and citation sweeps find them.

Externo: fedreg:2026-21861

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