Airworthiness Directives (ADs)
CAA-2009-12-006(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.
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Issue Date
- 2009/12/11
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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 if equipped with a
Hamilton Sundstrand RAT turbine lower gear box assembly, as identified by
Part Number (P/N) in Hamilton Sundstrand Service Bulletin (SB) ERPS06G-
29-6.
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313
aeroplanes, all manufacturer serial numbers if equipped with Hamilton
Sundstrand RAT turbine lower gear box assembly, as identified by P/N in
Hamilton Sundstrand SB ERPS06G-29-6.
Airbus A340-541, A340-542, A340-642 and A340-643 aeroplanes, all serial
numbers if equipped with Hamilton Sundstrand RAT turbine assembly, as
identified by P/N in Hamilton Sundstrand SB ERPS33G-29-1
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Model Number
- A330 and A340 aeroplanes
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CAA AD Number
- CAA-2009-12-006(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2009-0260
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Effective Date
- 2009/12/24
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Subject
- Hydraulic Power – Ram Air Turbine (RAT) Balance Weight Screws
– Inspection / Replacement
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Reference Publications (Revision/ATA/SB)
- ATA 29
Ref. Airbus AOT A330-29A3110, A340-29A4085, A340-500/600-29A5015; Hamilton Sundstrand SB ERPS06G-29-6, ERPS33G-29-1.
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Remarks
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