Airworthiness Directives (ADs)
CAA-2016-10-011
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
- 2016/10/31
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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, except those on which Airbus modification (mod) 153724 was embodied in production.
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Model Number
- A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2016-10-011
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2016-0212
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Effective Date
- 2016/11/08
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Subject
- Fuselage – Central Vertical Strut at Frame 65 – Modification
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Reference Publications (Revision/ATA/SB)
- ATA 53. Ref. Publications: Airbus SB A320-53-1262 Revision 01 dated 29 July 2016. and Airbus SB A320-53-1333 original issue dated 29 July 2016. and Airbus SB A320-53-1334 original issue dated 29 July 2016.
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Remarks
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