適航指令資料庫查詢
CAA-2014-01-006A
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
- 2014/02/05
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適用性說明
- Airbus A330-201, A330-202, A330-203, A330-223, A330-243 A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers (MSN) on which Airbus modification 44205 has been embodied in production, except those on which Airbus modification 52974 or 53223 has been embodied in production, and
Airbus A340-311, A340-312 and A340-313 aeroplanes, all MSN on which Airbus modification 44205 has been embodied in production, except those on which Airbus modification 52974 or 53223 has been embodied in production.
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型別
- AIRBUS A330 and A340-300 aeroplanes
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民航局AD編號
- CAA-2014-01-006A
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原發布國
- EASA
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原AD編號
- 2014-0012R1
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生效日期
- 2014/01/24
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主旨摘要
- Fuselage – Longitudinal Doubler at Vertical Tail Plane Attachment Cut Out – Inspection / Modification
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參考資訊（版本/ATA/SB）
- ATA 53, This AD revises EASA AD 2014-0012(CAA-2014-01-006) dated 10 January 2014, which superseded EASA AD 2007-0284 dated 12 November 2007.
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存檔序號
- 103-01-015
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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