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Airworthiness directives › 2014-08-02

AD 2014-08-02 Airworthiness Directives; Airbus Airplanes

Superseded. This directive was replaced by AD 2017-15-03. Work to the current one.
2014-05-21
2014-04-16
39-17826
FAA-2013-0668
Airframe
2017-15-03

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 Airbus 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

You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.

Required actions

Before the accumulation of 42,500 total flight cycles, or within 2,000 flight cycles after the effective date of this AD, whichever occurs later, 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 Mandatory Service Bulletin A300-57-6046, Revision 02, dated June 21, 2013, except as required by paragraph (h) of this AD. Do all applicable repairs before further flight.

Unsafe condition

This AD was prompted by reports of cracks found in the bottom wing skin stringers at rib 14 during full-scale fatigue testing and in service. 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

None.

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