Airworthiness directives › 2018-23-14
AD 2018-23-14 Airworthiness Directives; Airbus SAS Airplanes
Models named: A330-201, -202, -203, -223, -243, A330-223F, -243F, A330-301, -302, -303. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category, with an original certificate of airworthiness or original export certificate of airworthiness issued on or before November 29, 2017. (1) Airbus SAS Model A330-201, -202, -203, -223, and -243 airplanes. (2) Airbus SAS Model A330-223F and -243F airplanes. (3) Airbus SAS Model A330-301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
Within 90 days after the effective date of this AD, revise the existing maintenance or inspection program, as applicable, to incorporate the information specified in the service information identified in paragraphs (g)(1), (g)(2), and (g)(3) of this AD. The initial compliance times for accomplishing the tasks are at the applicable times specified in the service information identified in paragraphs (g)(1), (g)(2), and (g)(3) of this AD, or within 90 days after the effective date of this AD, whichever occurs later. (1) Airbus A330 Airworthiness Limitations Section (ALS) Part 1, Safe Life Airworthiness Limitation Items (SL-ALI), Revision 09, dated September 18, 2017. (2) Airbus A330 ALS Part 1, SL-ALI, Variation 9.2, dated November 28, 2017. (3) Airbus A330 ALS Part 1, SL-ALI, Variation 9.3, dated November 29, 2017.
Unsafe condition
This AD was prompted by revisions to certain airworthiness limitation item (ALI) documents, which specify more restrictive instructions and/or airworthiness limitations. We are issuing this AD to address fatigue cracking, accidental damage, or corrosion in principal structural elements, and possible failure of certain life limited parts, which could result in reduced structural integrity of the airplane.
Affected ADs
This AD affects AD 2017-10-24, Amendment 39-18898 (82 FR 24035, May 25, 2017) (“AD 2017-10-24”).
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