Airworthiness Directives (ADs)
CAA-2010-02-004
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
- 2010/02/19
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Applicability
- Airbus A330 aeroplanes, models -201, -202, - 203, - 223, -243, -301, -302, -303, -321, -322, -323, -341, -342 and -343, all manufacturer serial numbers, except those on which Airbus modification 55306 or 55792
has been embodied in production.
Airbus A340 aeroplanes, models -211, -212, -213, -311, -312, -313, all manufacturer serial numbers, except those on which Airbus modification 55306 or 55792 has been embodied in production.
This AD is not applicable to Airbus A340 -200/-300 aeroplanes repaired in accordance with Repair Drawing R57115053 or R57115051 or
R57115047 (installation of Titanium Doubler on both sides) which are affected by EASA AD 2006-0314.
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Model Number
- A330 and A340-200/-300 aeroplanes
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CAA AD Number
- CAA-2010-02-004
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2010-0024
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Effective Date
- 2010/02/26
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Subject
- Wings – Centre Wing Box – Keel Beam Fastener Holes at
Frame FR40 - Inspection
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Reference Publications (Revision/ATA/SB)
- ATA 57
This AD supersedes EASA AD 2006-0315R1(CAA-2006-10-011A).
Ref.Airbus Service Bulletin A330-57-3081 Revision 03;
Airbus Service Bulletin A340-57-4089 Revision 03;
Airbus Service Bulletin A330-57-3098 at Original issue, Revision 01;
Airbus Service Bulletin A340-57-4106 at Original issue, Revision 01;
Airbus Service Bulletin A330-57-3090 at Original issue;
Airbus Service Bulletin A340-57-4098 at Original issue.
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Remarks
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