AD NO.
2025-0111
SUBJECT
ATA 53 – Fuselage – Service Door Stop Fitting Hole – Inspection / Repair
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, A319-173N, 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, A321-253NY, A321-271N, A321-271NX, A321-271NY, A321- 272N and A321-272NX aeroplanes, all manufacturer serial numbers, except: – Aeroplanes having the modification SB, as defined in this AD, embodied after 6 100 flight cycles (FC) since aeroplane first flight; or – A318 aeroplanes on which Airbus modification (mod) 39195 was embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service; or – A319 aeroplanes on which Airbus mod 28238, mod 28162 and mod 28342 were embodied in production; or – A319 NEO aeroplanes on which Airbus mod 162338 was embodied in production; or – A320 NEO aeroplanes on which Airbus mod 162339 was embodied in production or – A319 NEO, A320 NEO and A321 NEOaeroplanes on which Airbus mod 171840 was embodied in production.
ISSUED BY
EASA