AD NO.
2024-0135
SUBJECT
ATA 53 – Fuselage – Centre Fuselage – Keel Beam Bottom Panel – Inspection
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.
ISSUED BY
EASA