Airworthiness Directives (ADs)
CAA-2011-10-006修訂
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
- 2012/03/27
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Applicability
- Airbus A330-201, A330-202, A330-203, A330-223, and A330-243 aeroplanes,all manufacturer serial numbers (MSN), except those on which Airbus modification 200242 has been embodied in production.
Airbus A330-223F and A330-243F aeroplanes, all MSN, except:
- aeroplanes on which Airbus modification 58623 has been embodied in production and on which Airbus modification 200281 has not been embodied in production, or- aeroplanes on which Airbus modification 200242 has been embodied in
production.
Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313,
A340-541, A340-542, A340-642 and A340-643 aeroplanes, all MSN, except aeroplanes on which Airbus modification 200242 has been embodied in production.
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Model Number
- AIRBUS A330-200 and A340 aeroplanes
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CAA AD Number
- CAA-2011-10-006修訂
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2011-0196Correction
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Effective Date
- 2011/10/21
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Subject
- Fuel / Main Transfer System – Rear and/or Center Tank Fuel Pump
Control Circuit – Modification
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Reference Publications (Revision/ATA/SB)
- (i)Airbus SB A330-28-3113 original issue, dated 19 July 2011.
(ii)Airbus SB A340-28-4129 original issue, dated 19 July 2011.
(iii)Airbus SB A340-28-5051 original issue, dated 01 September 2011.
(iv)The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
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Remarks
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