適航指令資料庫查詢
CAA-2024-10-018
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。
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發布日期
- 2024/11/01
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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, 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:
- A319 aeroplanes on which Airbus modification (mod) 28238, mod 28162 and mod 28342 have been embodied in production; and
- A318 aeroplanes on which mod 39195 has been embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 has been embodied in service.
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型別
- Airbus A318, A319, A320 and A321 aeroplanes
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民航局AD編號
- CAA-2024-10-018
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原發布國
- EASA
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原AD編號
- 2024-0210
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生效日期
- 2024/11/12
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主旨摘要
- Fuselage – Inner Cap and Frame Flange at Frame 68 Stringer 22 – Inspections
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參考資訊（版本/ATA/SB）
- This AD supersedes EASA AD 2022-0030(CAA-2022-03-001) dated 25 February 2022.
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存檔序號
- 113-10-021
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專業分項
- Structure
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產品類別
- Airplane
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備註
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檔案下載
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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：
Canada、EASA、FAA、Israel、JapanCAB、UK、Brazil、CAA-CZ