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Airworthiness directives › 2022-22-10

AD 2022-22-10 Airworthiness Directives; Airbus SAS Airplanes

Superseded. This directive was replaced by AD 2025-02-04. Work to the current one.
2022-12-30
2022-11-25
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Airframe
2025-02-04

Models named: A318-111, -112, -121, -122, A319-111, -113, -114, -115, -131, -132. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Airbus SAS Model airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before February 2, 2022. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, -151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216, -231, -232, -233, -251N, -252N, -253N, -271N, -272N, and -273N airplanes. (4) Model A321-111, -112, -131, -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

This paragraph restates the requirements of paragraph (i) of AD 2020-21-11, with a new terminating action. For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or before November 13, 2019, except for Model A319-171N airplanes: Except as specified in paragraph (h) of this AD, comply with all required actions and compliance times specified in, and in accordance with, European Union Aviation Safety Agency (EASA) AD 2020-0080, dated April 1, 2020 (EASA AD 2020-0080). Accomplishing the revision of the existing maintenance or inspection program required by paragraph (j) of this AD terminates the requirements of this paragraph.

Unsafe condition

This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. The FAA is issuing this AD to address failure of certain life-limited parts, which could result in reduced structural integrity of the airplane.

Affected ADs

This AD replaces AD 2020-21-11, Amendment 39-21284 (85 FR 65674, October 16, 2020) (AD 2020-21-11).

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