Airworthiness Directives (ADs)
CAA-2017-11-007(已被CAA-2018-12-014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
- 2017/11/28
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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, A320-251N, A320-271N, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, A321-232, 321-251N, A321-253N, A321-271N, A321-272N aeroplanes, all manufacturer serial numbers.
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Model Number
- A318, A319, A320, and A321 aeroplanes
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CAA AD Number
- CAA-2017-11-007(已被CAA-2018-12-014取代)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2017-0231
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Effective Date
- 2017/12/05
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Subject
- Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 – Damage Tolerant Airworthiness Limitation Items – Implementations
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Reference Publications (Revision/ATA/SB)
- ATA 05. This AD supersedes EASA AD 2016-0239(CAA-2016-12-001) dated 02 December 2016 and EASA AD 2015-0038R1 dated 09 February 2017. Ref. Publications: Airbus A318/A319/A320/A321 ALS Part 2 Revision 06 dated 10 April 2017. and Airbus A318/A319/A320/A321 ALS Part 2 Variation 6.1 dated 18 May 2017. and Airbus A318/A319/A320/A321 ALS Part 2 Variation 6.2 dated 24 May 2017. and Airbus A318/A319/A320/A321 ALS Part 2 Variation 6.3 dated 24 October 2017. and Airbus SB A320-53-1339 original issue dated 01 November 2017.
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Remarks
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