AD NO.
2023-0150
SUBJECT
ATA 53 – Fuselage – Crossbeam Splicing at Frames 16 and 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, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers, except: – aeroplanes on which Airbus modification (mod) 161255 was embodied in production; – A318 aeroplanes on which Airbus mod 39195 was embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service; and – A319 aeroplanes on which Airbus mod 28238, mod 28162 and mod 28342 were embodied in production.
ISSUED BY
EASA