Airworthiness Directives (ADs)
CAA-2012-02-010(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
- 2012/03/05
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Applicability
- Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-111, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers (MSN).
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Model Number
- AIRBUS A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2012-02-010(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2012-0032
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Effective Date
- 2012/03/09
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Subject
- Wings – Outer Wing Main Landing Gear Support Rib 5 Fitting – Inspection / Modification
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Reference Publications (Revision/ATA/SB)
- ATA 57. This AD supersedes EASA AD 2011-0011(CAA-2011-01-010) dated 21 January 2011.
Ref. Airbus SB A320-57-1118 Revision 03 dated 23 April 2007, Revision 04 dated 04 June 2008, and Airbus SB A320-57-1138 Revision 01 dated 27 October 2006, and Airbus Alert SB A320-57A1166 Revision 01 dated 19 October 2011, and Airbus Repair Instructions R572-58376 Issue C, R572-58507 Issue A, R572-58209 Issue A, R572-45020 Issue A and R572-45019 Issue A, R572-48341 Issue A, and Airbus SB A320-57-1168 Original issue dated 07 November 2011.
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Remarks
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