Airworthiness Directives (ADs)
CAA-2022-07-014(已被CAA-2024-03-008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
- 2022/08/04
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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, except:
- A318 aeroplanes on which Airbus modification (mod) 39195 was embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service; and
- A319 aeroplanes on which Airbus mod 28162, mod 28238 and mod 28342 were embodied in production.
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Model Number
- Airbus A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2022-07-014(已被CAA-2024-03-008取代)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2022-0151
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Effective Date
- 2022/08/09
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Subject
- Fuselage – Lateral Cockpit Window Frame Upper Stiffener – Inspection
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Reference Publications (Revision/ATA/SB)
- This AD supersedes EASA AD 2019-0067R1(CAA-2019-03-016A) dated 11 September 2019.
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Remarks
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