Airworthiness Directives (ADs)
CAA-2016-06-010
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
- 2016/06/23
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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, A320-211, 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
- A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2016-06-010
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2016-0113
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Effective Date
- 2016/06/29
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Subject
- Flight Controls – Flap Interconnecting Strut – Identification / Modification / Replacement
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Reference Publications (Revision/ATA/SB)
- ATA 27. This AD supersedes EASA AD 2012-0012(CAA-2012-01-010) dated 23 January 2012. Ref. Publications: Airbus SB A320-27-1206 Revision 02 dated 02 November2015.
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Remarks
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