Airworthiness Directives (ADs)
CAA-2024-07-006
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
- 2024/07/15
-
Applicability
- Airbus A318-111, A318-112, A318-121, A318-122 aeroplanes, all manufacturer serial numbers (MSN), except aeroplanes on which Airbus modification (mod) 39195 was embodied in production, or on which Airbus Service Bulletin (SB) A320-00-1219 was embodied in service; and
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 and A320-233 aeroplanes, all MSN having mod 31067 embodied in production, except aeroplanes having a configuration as below: aeroplanes on which Airbus mod 160001 was embodied in production, or on which Airbus SB A320-57-1193 has been embodied in service; and Airbus A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all MSN, except aeroplanes on which Airbus mod 160021 was embodied in production.
-
Model Number
- Airbus A318, A319, A320 and A321 aeroplanes
-
CAA AD Number
- CAA-2024-07-006
-
Aeronautics Authority of Original AD
- EASA
-
Original AD Number
- 2024-0135
-
Effective Date
- 2024/07/24
-
Subject
- Fuselage – Centre Fuselage – Keel Beam Bottom Panel – Inspection
-
Reference Publications (Revision/ATA/SB)
- ATA 53. Ref. Publications: Airbus SB A320-53-1526 original issue dated 11 December 2023.
-
Remarks
-
Download
-
