Airworthiness Directives (ADs)
CAA-2020-01-004(已有後續修訂版)
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
- 2020/01/17
-
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 meeting one of the configuration criteria below:
- A318 aeroplanes on which Airbus modification (mod) 39195 was embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service;
- A319 aeroplanes on which Airbus mod 28238 and mod 28162 and mod 28342 were embodied in production.
-
Model Number
- A318, A319, A320 and A321 aeroplanes
-
CAA AD Number
- CAA-2020-01-004(已有後續修訂版)
-
Aeronautics Authority of Original AD
- EASA
-
Original AD Number
- 2020-0005
-
Effective Date
- 2020/01/27
-
Subject
- Fuselage – Windshield Central Lower Node Continuity Fittings – Inspection / Modification
-
Reference Publications (Revision/ATA/SB)
- ATA 53. Ref. Publications:
Airbus Service Bulletin A320-53-1329 original issue dated 21 December 2018. and Airbus Service Bulletin A320-53-1331 original issue dated 14 January 2019.
-
Remarks
-
Download
-
