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Airworthiness directives › 2015-23-05

AD 2015-23-05 Airworthiness Directives; Airbus Airplanes

2015-12-28
2015-11-20
39-18321
FAA-2014-1043
Airframe
—

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

Applicability*9

This AD applies to the airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A330-201, -202, -203, -223, -223F, -243, and -243F airplanes. (2) Airbus Model A330-301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes. (3) Airbus 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

For the purpose of this AD, a Societé Anonyme de Recherche Mécanique Appliquée (SARMA) strut is a strut on which the diameter of the strut end is less than 43 millimeters. All other struts are Technical Airborne Components Industries (TAC) struts.

Unsafe condition

This AD was prompted by reports of cracked support strut body ends at a certain frame location of the trimmable horizontal stabilizer (THS). We are issuing this AD to detect and correct cracked support strut body ends of the THS, which could lead to the loss of all four THS support struts and which would make the remaining structure unable to carry limit loads, resulting in the loss of the horizontal tail plane.

Affected ADs

None.

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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