Airworthiness Directives (ADs)
CAA-2011-09-008(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
- 2011/09/21
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Applicability
- Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all manufacturer serial numbers, except those on which Airbus modification (mod.) 52980 has been embodied in production on both Main
Landing Gear (MLG), and Aeroplanes on which Airbus mod. 54500 has been embodied in production
are not affected by this AD.
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Model Number
- AIRBUS A340-200/-300 aeroplanes
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CAA AD Number
- CAA-2011-09-008(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2011-0178
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Effective Date
- 2011/09/30
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Subject
- Landing Gear – Main Landing Gear Retraction Actuator Piston
Rod – Inspection / Modification
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Reference Publications (Revision/ATA/SB)
- ATA 32. This AD supersedes EASA AD 2006-0301R2(CAA-2003-12-014F) dated 10 September 2009. Ref. Airbus SB A340-32-4212 Revision 05 dated 26 September 2008, and Airbus SB A340-32-4213 Revision 01 dated 16 September 2005, and Airbus SB A340-32-4222 Revision 03 dated 28 January 2011.
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Remarks
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