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Airworthiness Directive 2025-14-06

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Official AD 2025-14-06 · FR doc 2025-13593 · 2025-07-21 · airframe

Airworthiness Directives; Airbus SAS Airplanes

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A350-941 and -1041 airplanes. This AD was prompted by reports of deep spot faces on rib 9 at the lower flange bolting with the lower spar. This AD requires a special detailed inspection for discrepancies of certain pylon bolts, and applicable corrective actions. The FAA is issuing this AD to address the unsafe condition on these products.

Which aircraft AD 2025-14-06 applies to

MakesAirbus
ModelsA350-941, A350-1041, A350

Applies to airplanes having manufacturer serial numbers listed in Airbus Service Bulletin A350-54-P011, dated July 4, 2024.

Whether AD 2025-14-06 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of compliance — The specific action taken (inspected, replaced, modified) and to what revision.
Date — When the work was done.
Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.
Signature & certificate — The A&P/IA who returned it to service, with certificate number.
Is AD 2025-14-06 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

Look up a tail number →Read the full directive (Federal Register)

Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.