Airworthiness Directives (ADs)
CAA-2014-01-006A
The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.
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Issue Date
- 2014/02/05
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Applicability
- Airbus A330-201, A330-202, A330-203, A330-223, A330-243 A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers (MSN) on which Airbus modification 44205 has been embodied in production, except those on which Airbus modification 52974 or 53223 has been embodied in production, and
Airbus A340-311, A340-312 and A340-313 aeroplanes, all MSN on which Airbus modification 44205 has been embodied in production, except those on which Airbus modification 52974 or 53223 has been embodied in production.
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Model Number
- AIRBUS A330 and A340-300 aeroplanes
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CAA AD Number
- CAA-2014-01-006A
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2014-0012R1
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Effective Date
- 2014/01/24
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Subject
- Fuselage – Longitudinal Doubler at Vertical Tail Plane Attachment Cut Out – Inspection / Modification
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Reference Publications (Revision/ATA/SB)
- ATA 53, This AD revises EASA AD 2014-0012(CAA-2014-01-006) dated 10 January 2014, which superseded EASA AD 2007-0284 dated 12 November 2007.
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Remarks
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