Airworthiness Directives (ADs)
CAA-2024-10-018A(已被CAA-2025-07-010取代)
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
- 2025/07/28
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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:
- A319 aeroplanes on which Airbus modification (mod) 28238, mod 28162 and mod 28342 have been embodied in production; and
- A318 aeroplanes on which mod 39195 has been embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 has been embodied in service.
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Model Number
- Airbus A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2024-10-018A(已被CAA-2025-07-010取代)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2024-0210R1
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Effective Date
- 2025/07/29
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Subject
- Fuselage – Inner Cap and Frame Flange at Frame 68 Stringer 22 – Inspections
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Reference Publications (Revision/ATA/SB)
- This AD revises EASA AD 2024-0210(CAA-2024-10-018) dated 29 October 2024.
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Remarks
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