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Airworthiness directives › 2019-12-04

AD 2019-12-04 Airworthiness Directives; Airbus SAS Airplanes

2019-08-07
2019-07-03
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Airframe
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Models named: A300 B4-603, B4-620, B4-622, B4-605R, B4-622R, C4-605R Variant F, F4-605R, F4-622R. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Airbus SAS Model A300 B4-603, B4-620, B4-622, B4-605R, B4-622R, C4-605R Variant F, F4-605R, and F4-622R airplanes, certificated in any category, as identified in European Aviation Safety Agency (EASA) AD 2018-0229, dated October 23, 2018 (“EASA AD 2018-0229”).

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with EASA AD 2018-0229.

Unsafe condition

This AD was prompted by reports of cracking of the frame (FR) 47 angle fitting. The FAA is issuing this AD to address cracking of the FR47 angle fitting, which could result in reduced structural integrity of the airplane.

Affected ADs

(1) This AD replaces AD 2018-19-18, Amendment 39-19418 (83 FR 49793, October 3, 2018) (“AD 2018-19-18”). (2) This AD affects AD 2014-20-18, Amendment 39-17991 (79 FR 65879, November 6, 2014) (“AD 2014-20-18”).

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