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Airworthiness directives › 2022-06-21

AD 2022-06-21 Airworthiness Directives; Airbus SAS Airplanes

2022-05-10
2022-04-05
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Airframe
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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 airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2021-0167, dated July 14, 2021 (EASA AD 2021-0167). (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes. (4) Model A321-111, -112, -131, -211, -212, -213, -231, and -232 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 2021-0167.

Unsafe condition

This AD was prompted by a report that additional affected configurations were identified to be subject to widespread fatigue damage at certain stringer attachments and, for certain airplanes, it was determined that additional modification work is necessary. The FAA is issuing this AD to prevent fatigue cracking in the stringer attachment holes of the wings, which could result in reduced structural integrity of the wings.

Affected ADs

This AD replaces AD 2018-09-09, Amendment 39-19266 (83 FR 19925, May 7, 2018; corrected May 15, 2018 (83 FR 22354)).

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