Airworthiness Directives (ADs)

Aviation Industry

CAA-2024-07-012(已修訂版為CAA-2024-07-012A)

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.

Issue Date: 2024/08/05

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, A321-232, aeroplanes, all manufacturer serial numbers (MSN), except: - A318 aeroplanes on which Airbus modification (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, and - all aeroplanes on which mod 157159 was embodied in production.

Model Number: Airbus A318, A319, A320 and A321 aeroplanes

CAA AD Number: CAA-2024-07-012(已修訂版為CAA-2024-07-012A)

Aeronautics Authority of Original AD: EASA

Original AD Number: 2024-0147

Effective Date: 2024/08/13

Subject: Fuselage – Centre Fuselage Forward Pressure Bulkhead – Inspection

Reference Publications (Revision/ATA/SB): This AD supersedes EASA AD 2014-0209(CAA-2014-09-007) dated 19 September 2014.

Remarks

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