Airworthiness Directives (ADs)
CAA-2018-10-021(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
- 2018/11/08
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Applicability
- Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132 and A319-133, aeroplanes, all manufacturer serial numbers, except those on which Airbus modification (mod) 161306 has been embodied in production.
Airbus 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 mod 161271 has been embodied in production.
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Model Number
- A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2018-10-021(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2018-0233
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Effective Date
- 2018/11/09
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Subject
- Fuselage – Cargo Compartment Fitting Brackets, Tack and Rivet Holes – Inspection / Repair
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Reference Publications (Revision/ATA/SB)
- ATA 53. This AD supersedes EASA AD 2013-0310(CAA2013-12-015) dated 20 December 2013. Ref. Publications: Airbus SB A320-53-1257 original issue dated 21 December 2012, or Rev. 01 dated 28 April 2016, or Rev. 02 dated 29 November 2016. and Airbus SB A320-53-1261 original issue dated 21 December 2012, or Rev. 01 dated 30 June 2015, or Rev. 02 dated 01 March 2016, or Rev. 03 dated 08 August 2016, or Rev. 04 dated 03 May 2017. and Airbus SB A320-53-1360 original issue dated 01 December 2016, or Rev. 01 dated 01 March 2018. and Airbus SB A320-53-1364 original issue dated 04 May 2018. and Airbus SB A320-53-1365 original issue dated 17 April 2018.
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Remarks
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