Airworthiness Directives (ADs)
CAA-2024-03-010(已被CAA-2024-03-010修訂取代)
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
- 2024/03/21
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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 （MSN）, except those having Airbus modification （mod） 151574 embodied in production.
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Model Number
- Airbus A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2024-03-010(已被CAA-2024-03-010修訂取代)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2024-0077
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Effective Date
- 2024/04/02
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Subject
- Fuselage – Pressure Panel Longitudinal Beams – Inspection / Repair / Modification
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Reference Publications (Revision/ATA/SB)
- This AD supersedes EASA AD 2016-0206（CAA-2016-10-006修訂） dated 13 October 2016, including its Correction dated 14 October 2016.
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Remarks
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