Airworthiness Directives (ADs)
CAA-2014-07-021(已被CAA-2020-07-005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
- 2014/08/01
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Applicability
- Airbus 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 30975 has been embodied in production.
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Model Number
- Airbus A319, A320 and A321 series aeroplanes.
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CAA AD Number
- CAA-2014-07-021(已被CAA-2020-07-005取代)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2014-0177
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Effective Date
- 2014/08/08
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Subject
- Fuselage – Rear Fuselage Clips, Shear Webs and Angles – Replacement
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Reference Publications (Revision/ATA/SB)
- Airbus SB A320-53-1266 original issue dated 11 January 2013, or Revision 01 dated 20 June 2013. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
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Remarks
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