Airworthiness Directives (ADs)
CAA-2014-06-009
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
- 2014/06/18
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Applicability
- Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers, except those on which Airbus modification (Mod) 55792 or Mod 55306 has been embodied in production, and except those on which Airbus Repair Instruction R57115092 has been embodied in service on both Right Hand (RH) and Left Hand (LH) sides.
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313, aeroplanes, all manufacturer serial numbers except those on which Airbus Mod 55792 or Mod 55306 has been embodied in production, and except those on which Airbus Repair Instruction R57115092 has been embodied in service on both RH and LH sides.
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Model Number
- A330 and A340 aeroplanes
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CAA AD Number
- CAA-2014-06-009
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2014-0149
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Effective Date
- 2014/06/27
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Subject
- Wings – Center Wing Box Fastener Holes at Frame 40 Vertical Web – Inspection
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Reference Publications (Revision/ATA/SB)
- ATA 57. Ref. Airbus SB A330-57-3114 original issue dated 12 March 2013. and Airbus SB A330-57-3115 original issue dated 04 April 2013. and Airbus SB A330-57-3116 original issue dated 12 March 2013. and Airbus SB A340-57-4123 original issue dated 12 March 2013. and Airbus SB A340-57-4124 original issue dated 04 April 2013 or Revision 01 dated 22 August 2013. and Airbus SB A340-57-4125 original issue dated 12 March 2013.
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Remarks
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