Airworthiness Directives (ADs)
CAA-2013-10-020(已被CAA-2019-06-001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
- 2013/11/04
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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 on which Airbus modification (mod.) 21202 has been embodied in production, except those on which mod.152569 has been embodied in production.
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Model Number
- AIRBUS A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2013-10-020(已被CAA-2019-06-001取代)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2013-0261
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Effective Date
- 2013/10/11
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Subject
- Fuselage – Side Box Beam Flange in Frame 43 Area – Inspection / Repair / Modification
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Reference Publications (Revision/ATA/SB)
- ATA 53. Ref. Airbus SB A320-53-1258 original issue, dated 18 October 2012, and Airbus SB A320-53-1251 original issue, dated 16 November 2012, or Revision 01, dated 18 October 2013.
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Remarks
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