Airworthiness Directives (ADs)
CAA-2011-09-008A
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
- 2012/03/15
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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).
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Model Number
- Airbus A340-200, and A340-300 aeroplanes
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CAA AD Number
- CAA-2011-09-008A
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2011-0178R1
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Effective Date
- 2012/03/20
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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)
- (i)This AD revises EASA AD 2011-0178 dated 16 September 2011(CAA-2011-09-008 dated 21 September 2011) which superseded EASA AD 2006-0301R2 dated 10 September 2009(CAA-2003-12-014F dated 14 September 2009).
(ii)Airbus SB A340-32-4212 Revision 05 dated 26 September 2008.
(iii)Airbus SB A340-32-4213 Revision 01 dated 16 September 2005.
(iv)Airbus SB A340-32-4222 Revision 03 dated 28 January 2011.
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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