Airworthiness Directives (ADs)
CAA-2011-09-003A
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
- 2013/01/15
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Applicability
- Airbus A330-301, A330-321, A330-322, A330-341 and A330-342 aeroplanes, all manufacturer serial numbers on which Airbus Service Bulletin (SB) A330-53-3093 has been embodied in service, except those on which Airbus SB A330-53-3145 has been embodied in service.
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all manufacturer serial numbers on which Airbus SB A340-53-4104 has been embodied in service.
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Model Number
- AIRBUS A330 and A340-200/-300 aeroplanes
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CAA AD Number
- CAA-2011-09-003A
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2011-0171R1
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Effective Date
- 2013/01/18
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Subject
- Fuselage – Frame (FR) 40 / Fuselage Skin Panel Junction –
Inspection
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Reference Publications (Revision/ATA/SB)
- This AD revises EASA AD 2011-0171(CAA-2011-09-003) dated 07 September 2011. Ref. Airbus SB A330-53-3193 original issue dated 20 April 2011 or Revision 1 dated 17 September 2012.
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Remarks
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