交通部民用航空局

發布日期

2025/04/17

適用性說明

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.

型別

Airbus A318, A319, A320 and A321 aeroplanes

民航局AD編號

CAA-2025-04-004

原發布國

EASA

原AD編號

2025-0078

生效日期

2025/04/23

主旨摘要

Fuselage – Centre Fuselage Skin and Forward Pressure Bulkhead – Inspection

參考資訊（版本/ATA/SB）

ATA 53. Ref. Publications: Airbus SB A320-53-1519 at original issue dated 18 November 2024. and Airbus SB A320-53-1520 at original issue dated 18 November 2024.

存檔序號

114-04-005

專業分項

Structure

產品類別

Airplane

備註

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