AD NO.
2024-0217
SUBJECT
ATA 53 – Fuselage – Double Joggle Area at Frame 16 and Frame 20 – Inspection
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, A320-216, 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 and A321-272NX aeroplanes, all manufacturer serial numbers (MSN), except aeroplanes in any of the configurations below: – Aeroplanes on which Airbus modification (mod) 160917 has been embodied in production; – A318 aeroplanes on which Airbus mod 39195 has been embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 has been embodied in service; – A319 aeroplanes on which Airbus mod 28238, mod 28162 and mod 28342 have been embodied in production; – A319 aeroplanes on which Airbus mod 162338 has been embodied in production; – A320 aeroplanes on which Airbus mod 162339 has been embodied in production; – CEO aeroplanes on which Airbus SB A320-53-1378, SB A320-53-1379, SB A320-53-1380 and SB A320-53-1381 have been embodied in service; – NEO aeroplanes on which Airbus SB A320-53-1422, SB A320-53-1423, SB A320-53-1424, and SB A320-53-1425 have been embodied in service.
ISSUED BY
EASA