Airworthiness directives › 2017-15-03
AD 2017-15-03 Airworthiness Directives; Airbus Airplanes
Models named: A300-B4-601, B4-603, B4-620, B4-622, A300-B4-605R, B4-622R. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to Airbus Model A300-B4-601, B4-603, B4-620, and B4-622 airplanes, and Model A300-B4-605R and B4-622R airplanes, certificated in any category, except airplanes on which Airbus Modification 10324 or 10325 has been embodied in production.
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 2014-08-02, with revised compliance times and service information. At the time specified in paragraph (g)(1) or (g)(2) of this AD, whichever occurs earlier, modify the profile of stringer run-outs at rib 14 of both wings, including a high frequency eddy current inspection of the fastener holes for defects and all applicable repairs, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A300-57-6046, Revision 02, dated June 21, 2013; or Revision 03, including Appendix 01, dated February 4, 2015; except as required by paragraph (h) of this AD. Do all applicable repairs before further flight. As of the effective date of this AD, only Airbus Service Bulletin A300-57-6046, Revision 03, including Appendix 01, dated February 4, 2015, may be used. (1) Before the accumulation of 42,500 total flight cycles, or within 2,000 flight cycles after May 21, 2014 (the effective date of AD 2014-08-02), whichever occurs later. (2) Before the accumulation of 30,000 total flight cycles, or within 2,000 flight cycles after the effective date of this AD, whichever occurs later.
Unsafe condition
This AD was prompted by an evaluation by the design approval holder indicating that certain wing skin stringers are subject to widespread fatigue damage. We are issuing this AD to prevent cracking in the bottom wing skin stringers, which could result in reduced structural integrity of the wings.
Affected ADs
This AD replaces AD 2014-08-02, Amendment 39-17826 (79 FR 21392, April 16, 2014) (“AD 2014-08-02”).
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