Airworthiness Directives (ADs)
CAA-2021-11-005
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
- 2021/11/12
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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) 157039 has been embodied in production;
- A319 aeroplanes on which mod 28238, mod 28162 and mod 28342 have been embodied in
production; and - A318 aeroplanes on which mod 39195 has been embodied in production, or Airbus Service
Bulletin (SB) A320-00-1219 has been embodied in service.
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Model Number
- Airbus A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2021-11-005
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2021-0242
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Effective Date
- 2021/11/22
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Subject
- Fuselage – Door Stop Fitting Holes at Frame 66/68 – Inspection / Repair
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Reference Publications (Revision/ATA/SB)
- This AD supersedes EASA AD 2016-0238(CAA-2016-12-002修訂) dated 02 December 2016, including its Correction dated 04 January 2017.
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Remarks
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