適航指令資料庫查詢
CAA-2014-01-003(已有後續修訂版)
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
- 2014/01/13
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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), except those on which Airbus modification (Mod) 55306 or 55792 has been embodied in production.
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all MSN, except those on which Airbus Mod 55306 or 55792 has been embodied in production and except those on which Airbus Repair Drawing
R57115053 or R57115051 or R57115047 has been embodied in service on both right-hand (RH) and left-hand (LH) sides.
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型別
- AIRBUS A330 and A340-200/-300 aeroplanes
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民航局AD編號
- CAA-2014-01-003(已有後續修訂版)
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原發布國
- EASA
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原AD編號
- 2014-0010
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生效日期
- 2014/01/22
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主旨摘要
- Wings – Centre Wing Box Keel Beam Fastener Holes at Frame 40 –
Inspection
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參考資訊（版本/ATA/SB）
- ATA 57. This AD supersedes EASA AD 2010-0024(CAA-2010-02-004) dated 12 February 2010.
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存檔序號
- 103-01-004
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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