Airworthiness Directives (ADs)
CAA-2025-04-004
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
- 2025/04/17
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Applicability
- Airbus A318-111, A318-112 and A318-122 aeroplanes, all manufacturer serial numbers (MSN); and 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, A320-232, A320-233, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, A321-211, A321-212, A321-213, A321-231, A321-232, A321-251N, A321-251NX, A321-252N, A321-252NX, A321-253N, A321-253NX, A321-271N, A321-271NX, A321-272N, and A321-272NX aeroplanes, all MSN up to MSN 09287 inclusive, on which Airbus modification (mod) 157159 is embodied in production;
except aeroplanes in any of the following configuration:
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Airbus A318 aeroplanes on which Airbus mod 39195 was embodied in production or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service;
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Airbus A319 CEO aeroplanes, on which Airbus mod 28162 and mod 28238 and mod 28342 were embodied in production;
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Airbus A320 NEO aeroplanes on which Airbus mod 162339 was embodied in production.
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Model Number
- Airbus A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2025-04-004
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2025-0078
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Effective Date
- 2025/04/23
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Subject
- Fuselage – Centre Fuselage Skin and Forward Pressure Bulkhead – Inspection
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Reference Publications (Revision/ATA/SB)
- ATA 53. Ref. Publications: Airbus SB A320-53-1519 at original issue dated 18 November 2024. and Airbus SB A320-53-1520 at original issue dated 18 November 2024.
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Remarks
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