Airworthiness Directives (ADs)
CAA-2020-03-002(已有後續修訂版)
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
- 2020/03/03
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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 those on which Airbus modification (mod) 153126 or mod 153742 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-2020-03-002(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2020-0037
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Effective Date
- 2020/03/12
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Subject
- Fuselage – Frame Foot Coupling at Frame 43 – Inspection / Repair
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Reference Publications (Revision/ATA/SB)
- ATA 53. Ref. Publications: Airbus SB A320-53-1269 original issue dated 17 January 2013, or Revision 01 dated 10 July 2013, or Revision 02 dated 07 February 2019. and Airbus SB A320-53-1270 original issue dated 17 January 2013, or Revision 01 dated 27 September 2013, or Revision 02 dated 11 April 2014.
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Remarks
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