Airworthiness Directives (ADs)

Aviation Industry

CAA-2020-02-002

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.

Issue Date: 2020/02/10

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) 158423 was embodied in production; - A318, A319 and A320 aeroplanes on which Airbus mod 160000 was embodied in production; - A319 and A320 aeroplanes on which Airbus Service Bulletin (SB) A320-57-1193 was embodied in service; - A321 aeroplanes on which Airbus mod 160021 was embodied in production; - A318 aeroplanes on which Airbus mod 39195 was embodied in production, or Airbus SB A320-00-1219 was embodied in service; and - A319 aeroplanes on which Airbus mod 28238, mod 28162 and mod 28342 were embodied in production.

Model Number: Airbus A318, A319, A320 and A321 aeroplanes

CAA AD Number: CAA-2020-02-002

Aeronautics Authority of Original AD: EASA

Original AD Number: 2020-0019

Effective Date: 2020/02/19

Subject: Fuselage – Lateral Window Frame Upper Fastener Holes – Inspection

Reference Publications (Revision/ATA/SB): ATA 53. Ref. Publications: Airbus SB A320-53-1335 original issue dated 12 March 2019. and Airbus SB A320-53-1336 original issue dated 12 March 2019. and irbus SB A320-53-1448 original issue dated 05 August 2019. and Airbus SB A320-53-1449 original issue dated 05 August 2019.

Remarks

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