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Airworthiness directives › 2026-12-04

AD 2026-12-04 Airworthiness Directives; Airbus SAS Airplanes

2026-07-14
2026-06-09
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Airframe
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Models named: A350-941. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Airbus SAS Model A350-941 airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2025-0209, dated September 24, 2025 (EASA AD 2025-0209).

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, EASA AD 2025-0209.

Unsafe condition

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. The FAA is issuing this AD to address improperly torqued fasteners that could lead to insufficient clamping and potentially compromise the airplane's structural integrity and compliance with electromagnetic hazard requirements. The unsafe condition, if not addressed, could, in case of a fuel leak, create a source of ignition and possibly result in an uncontrolled fire.

Affected ADs

None.

Read the original on the Federal Register →

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1