Airworthiness Directives (ADs)
CAA-2023-07-005
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
- 2023/07/24
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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: - aeroplanes on which Airbus modification (mod) 161255 was embodied in production;
- A318 aeroplanes on which Airbus mod 39195 was embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service; and
- A319 aeroplanes on which Airbus mod 28238, mod 28162 and mod 28342 were embodied in production.
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Model Number
- Airbus A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2023-07-005
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2023-0150
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Effective Date
- 2023/08/03
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Subject
- Fuselage – Crossbeam Splicing at Frames 16 and 20 – Inspection
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Reference Publications (Revision/ATA/SB)
- This AD supersedes EASA AD 2016-0139(CAA-2016-07-007) dated 14 July 2016.
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Remarks
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