Airworthiness Directives (ADs)
CAA-2016-07-007(已被CAA-2023-07-005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
- 2016/07/20
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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: Aeroplanes on which Airbus modification (mod) 161255 has been embodied in production;
A319 aeroplanes on which mod 28238, and mod 28162, and mod 28342 have concurrently been embodied in production;
A318 aeroplanes on which mod 39195 has been embodied in production.
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Model Number
- A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2016-07-007(已被CAA-2023-07-005取代)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2016-0139
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Effective Date
- 2016/07/28
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Subject
- Fuselage – Crossbeam Splicing at Frames 16 and 20 – Inspection
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Reference Publications (Revision/ATA/SB)
- ATA 53. Ref. Publications: Airbus SB A320-53-1286 original issue dated 29 June 2015, or Revision 1 dated 22 December 2015. and Airbus SB A320-53-1295 original Issue dated 29 June 2015.
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Remarks
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