Airworthiness directives › 2020-21-11
AD 2020-21-11 Airworthiness Directives; Airbus SAS Airplanes
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 the Airbus SAS 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 November 13, 2019. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, -151N, and -153N 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 (g) of AD 2019-19-15, with no changes. For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or before November 30, 2018: Within 90 days after November 14, 2019 (the effective date of AD 2019-19-15), revise the existing maintenance or inspection program, as applicable, to incorporate Airbus SAS A318/A319/A320/A321 Airworthiness Limitations Section (ALS) Part 1 Safe Life Airworthiness Limitations (SL-ALI), Revision 06, Issue 02, dated November 30, 2018. The initial compliance time for doing the revised actions is at the applicable time specified in Airbus SAS A318/A319/A320/A321 ALS Part 1 Safe Life Airworthiness Limitations (SL-ALI), Revision 06, Issue 02, dated November 30, 2018, or within 90 days after November 14, 2019, whichever occurs later. Accomplishing the maintenance or inspection program revision required by paragraph (i) 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 the failure of certain life-limited parts, which could result in reduced structural integrity of the airplane.
Affected ADs
This AD replaces AD 2015-22-08, Amendment 39-18313 (80 FR 68434, November 5, 2015) (“AD 2015-22-08”); AD 2018-17-19, Amendment 39-19373 (83 FR 44460, August 31, 2018) (“AD 2018-17-19”); and AD 2019-19-15, Amendment 39-19751 (84 FR 54480, October 10, 2019) (“AD 2019-19-15”).
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