Airworthiness directives › 2017-04-05
AD 2017-04-05 Airworthiness Directives; Airbus Airplanes
Models named: A300 B2-1A, B2-1C, B4-2C, B2K-3C, B4-103, B2-203, B4-203. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to all Airbus Model A300 B2-1A, B2-1C, B4-2C, B2K-3C, B4-103, B2-203, and B4-203 airplanes, certificated in any category.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
This paragraph restates the requirements of paragraph (s) of AD 2011-10-17, with changes. Within 3 months after June 17, 2011 (the effective date of AD 2011-10-17): Revise the maintenance program to incorporate the structural inspections and inspection intervals defined in the Airbus A300 ALI Document AI/SE-M2/95A.1308/07, Issue 4, dated June 2008. Thereafter, except as required by paragraph (h) of this AD and except as provided by paragraph (j)(1) of this AD, no alternative structural inspections or inspection intervals may be approved. The initial ALI tasks must be done at the times specified in Airbus A300 ALI Document AI/SE-M2/95A.1308/07, Issue 4, dated June 2008.
Unsafe condition
This AD was prompted by a revision of certain airworthiness limitations item (ALI) documents, which specify more restrictive instructions and/or airworthiness limitations. We are issuing this AD to detect and correct fatigue cracking, damage, and corrosion in certain structure; such fatigue cracking, damage, and corrosion could result in reduced structural integrity of the airplane.
Affected ADs
This AD replaces AD 2011-10-17, Amendment 39-16698 (76 FR 27875, May 13, 2011) (“AD 2011-10-17”).
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