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適航指令資料庫查詢

CAA-2024-05-006

依據民用航空法規,航空器所有人或使用人除應遵守本國民航局所發布適航指令,亦應遵守航空器設計國之民航主管機關所通告之適航指令。

發布日期
2024/05/17
適用性說明
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, A320-215, 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, A321-271N, A321-271NX, A321-272N, A321-272NX aeroplanes, all manufacturer serial numbers, except those aeroplanes on which Airbus modification (mod) 165315 has been embodied in production.
型別
Airbus A318, A319, A320 and A321 aeroplanes
民航局AD編號
CAA-2024-05-006
原發布國
EASA
原AD編號
2024-0097
生效日期
2024/05/16
主旨摘要
Fuselage – Centre Fuselage / Main Landing Gear Door Keel Beam Hinge and Actuator Fittings – Inspection
參考資訊(版本/ATA/SB)
This AD supersedes EASA AD 2012-0118(CAA-2012-07-002) dated 04 July 2012.
存檔序號
113-05-007
專業分項
Structure
產品類別
Airplane
備註
檔案下載
CAA-2024-05-006.pdf

1.本局早期(2012年前)所發布AD目前未提供檔案下載服務。如欲查詢,請自行連結原發布國民航主管機關網頁,再依”原AD編號”查詢。

2.我國目前所引進航空產品原發布國民航主管機關網頁聯結如下:
CanadaEASAFAAIsraelJapanCABUKBrazilCAA-CZ

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