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Airworthiness Directives (ADs)

CAA-2011-10-006(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.

Issue Date
2011/10/17
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 and 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, and - 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.
Model Number
AIRBUS A330-200 and A340 aeroplanes
CAA AD Number
CAA-2011-10-006(已有後續修訂版)
Aeronautics Authority of Original AD
EASA
Original AD Number
2011-0196
Effective Date
2011/10/21
Subject
Fuel / Main Transfer System – Rear and/or Center Tank Fuel Pump Control Circuit – Modification
Reference Publications (Revision/ATA/SB)
ATA 28. Ref. Airbus SB A330-28-3113 original issue, dated 19 July 2011 and Airbus SB A340-28-4129 original issue, dated 19 July 2011 and Airbus SB A340-28-5051 original issue, dated 01 September 2011.
Remarks
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