Airworthiness Directives (ADs)
CAA-2014-01-003(已有後續修訂版)
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
- 2014/01/13
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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), except those on which Airbus modification (Mod) 55306 or 55792 has been embodied in production.
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all MSN, except those on which Airbus Mod 55306 or 55792 has been embodied in production and except those on which Airbus Repair Drawing
R57115053 or R57115051 or R57115047 has been embodied in service on both right-hand (RH) and left-hand (LH) sides.
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Model Number
- AIRBUS A330 and A340-200/-300 aeroplanes
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CAA AD Number
- CAA-2014-01-003(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2014-0010
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Effective Date
- 2014/01/22
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Subject
- Wings – Centre Wing Box Keel Beam Fastener Holes at Frame 40 –
Inspection
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Reference Publications (Revision/ATA/SB)
- ATA 57. This AD supersedes EASA AD 2010-0024(CAA-2010-02-004) dated 12 February 2010.
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Remarks
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