AD NO.
2025-0078
SUBJECT
ATA 53 – Fuselage – Centre Fuselage Skin and Forward Pressure Bulkhead – Inspection
APPLICABILITY
Airbus A318-111, A318-112 and A318-122 aeroplanes, all manufacturer serial numbers (MSN); 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, A320-232, A320-233, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, 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, and A321-272NX aeroplanes, all MSN up to MSN 09287 inclusive, on which Airbus modification (mod) 157159 is embodied in production; except aeroplanes in any of the following configuration: – Airbus A318 aeroplanes on which Airbus mod 39195 was embodied in production or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service; – Airbus A319 CEO aeroplanes, on which Airbus mod 28162 and mod 28238 and mod 28342 were embodied in production; – Airbus A320 NEO aeroplanes on which Airbus mod 162339 was embodied in production.
ISSUED BY
EASA