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Airworthiness directives › 2019-19-17

AD 2019-19-17 Airworthiness Directives; Airbus SAS Airplanes

2019-11-14
2019-10-10
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Airframe
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Models named: A300 B4-601, B4-603, B4-620, B4-622, A300 B4-605R, B4-622R, A300 F4-605R, A300 C4-605R Variant F. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2019-0044, dated March 7, 2019 (“EASA AD 2019-0044”). (1) Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes. (2) Model A300 B4-605R and B4-622R airplanes. (3) Model A300 F4-605R airplanes. (4) Model A300 C4-605R Variant F airplanes.

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 2019-0044.

Unsafe condition

This AD was prompted by reports of cracking due to fatigue-related stress in the radius of frame 40, adjacent to the tension bolts at the center/outer wing junction. The FAA is issuing this AD to address fatigue cracking on the forward fittings in the radius of frame 40, adjacent to the tension bolts in the center section of the wings, which could result in reduced structural integrity of the wings.

Affected ADs

This AD replaces AD 2000-03-20 R1, Amendment 39-12298 (66 FR 34530, June 29, 2001) (“AD 2000-03-20 R1”).

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