Airworthiness Directives (ADs)
CAA-2024-05-006A
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
- 2024/05/27
-
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, A319-151N, A319-153N, A319-171N, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, A321-232, A321-251N, A321-251NX, A321-252N, A321-252NX, A321-253N, A321-253NX, A321-271N, A321-271NX, A321-272N, A321-272NX aeroplanes, all manufacturer serial numbers, except those aeroplanes on which Airbus modification （mod） 165315 has been embodied in production.
-
Model Number
- Airbus A318, A319, A320 and A321 aeroplanes
-
CAA AD Number
- CAA-2024-05-006A
-
Aeronautics Authority of Original AD
- EASA
-
Original AD Number
- 2024-0097R1
-
Effective Date
- 2024/05/30
-
Subject
- Fuselage – Centre Fuselage / Main Landing Gear Door Keel Beam Hinge and Actuator Fittings – Inspection
-
Reference Publications (Revision/ATA/SB)
- This AD revises EASA AD 2024-0097（CAA-2024-05-006） dated 02 May 2024, which superseded EASA AD 2012-0118 dated 04 July 2012.
-
Remarks
-
Download
-
