AD 2025-17-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | SAS | Airworthiness Directives; Airbus SAS Airplanes |
Unsafe Condition
fatigue cracking, accidental damage, or corrosion in principal structural elements, which could result in reduced structural integrity of the airplane.
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Required Actions
revising the existing maintenance or inspection program, as applicable, to incorporate new airworthiness limitations, as specified in EASA AD 2024-0208, and doing the tasks specified in paragraph (3) of EASA AD 2024-0208.
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Compliance Time
within 90 days after the effective date of this AD, or at the applicable thresholds as incorporated by the requirements of paragraph (3) of EASA AD 2024-0208, whichever occurs later.
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Affected Aircraft
Airbus SAS Model A318-111, -112, -121, and -122 airplanes; A319-111, -112, -113, -114, -115, -131, -132, -133, -151N, -153N, and -171N airplanes; A320-211, -212, -214, -216, -231, -232, -233, -251N, -252N, -253N, -271N, -272N, and -273N airplanes; and A321-111, -112, -131, -211, -212, -213, -231, -232, -251N, -252N, -253N, -271N, -272N, -251NX, -252NX, -253NX, -253NY, -271NX, and -272NX airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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