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Airworthiness directives › 2024-26-06

AD 2024-26-06 Airworthiness Directives; Airbus SAS Airplanes

2025-03-11
2025-02-04
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Airframe
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Models named: A330-201, -202, -203, -223, -223F, -243, -243F, -301, -302, -303. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Airbus SAS airplanes specified in paragraphs (c)(1) and (2) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024-0016, dated January 11, 2024 (EASA AD 2024-0016). (1) Model A330-201, -202, -203, -223, -223F, -243, -243F, -301, -302, -303, -321, -322, -323, -341, -342, -343, and -941 airplanes. (2) Model A340-211, -212, -213, -311, -312, and -313 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 2024-0016.

Unsafe condition

This AD was prompted by tests that demonstrated that when the upper secondary load path (SLP) of the trimmable horizontal stabilizer actuator (THSA) is engaged, the THSA might not stall, with consequently no indication of SLP engagement, and by the recent determination that the required actions of AD 2022-16-06 cannot be accomplished on certain airplanes. The FAA is issuing this AD to prevent damage on the upper THSA SLP attachment with consequent mechanical disconnection of the THSA, that could result in loss of control of the airplane.

Affected ADs

This AD replaces AD 2022-16-06, Amendment 39-22135 (87 FR 51588, August 23, 2022) (AD 2022-16-06).

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