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Airworthiness directives › 2026-10-15

AD 2026-10-15 Airworthiness Directives; Airbus SAS Airplanes

2026-07-06
2026-05-29
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Airframe
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Models named: A318-111, -112, -122, A319-111, -113, -114, -115, -131, -132, -133. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Airbus SAS airplanes specified in paragraphs (c)(1) through (4), certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2025-0078, dated April 9, 2025 (EASA AD 2025-0078). (1) Model A318-111, -112, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, -214, -216, -232, -233, -251N, -252N, -253N, -271N, -272N, and -273N airplanes. (4) Model A321-211, -212, -213, -231, -232, -251N, 252N, -253N, -271N, -272N, -251NX, -252NX, -253NX, -271NX, and -272NX airplanes.

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 2025-0078.

Unsafe condition

This AD was prompted by the detection of a deviation from the manufacturing process during a review of the cold working process in the assembly line. The FAA is issuing this AD to address reduced fatigue life of the affected areas of the forward pressure bulkhead connection to, and fuselage skin at, certain frames. The unsafe condition, if not addressed, could result in reduced 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