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Airworthiness directives › 2026-17-01

AD 2026-17-01 Airworthiness Directives; Airbus SAS Airplanes

2026-10-01
2026-08-27
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Airframe
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Models named: A320-211, -212, -214, -216, -231, -232, -233, A321-111, -112, -131. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Airbus SAS Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2025-0193, dated September 8, 2025 (EASA AD 2025-0193), having an extended service goal (ESG) in the airworthiness limitations section of the instructions for continued airworthiness.

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 2025-0193.

Unsafe condition

This AD was prompted by a fatigue test that identified cracks in the area of the fastener holes at the forward and aft upper corner of the bulk cargo door at section 16 and 17. The FAA is issuing this AD to address cracks in the forward and aft upper corner of the bulk cargo door, which, if not addressed, could affect the structural integrity of the airplane.

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