適航指令資料庫查詢
CAA-2010-02-004
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
- 2010/02/19
-
適用性說明
- Airbus A330 aeroplanes, models -201, -202, - 203, - 223, -243, -301, -302, -303, -321, -322, -323, -341, -342 and -343, all manufacturer serial numbers, except those on which Airbus modification 55306 or 55792
has been embodied in production.
Airbus A340 aeroplanes, models -211, -212, -213, -311, -312, -313, all manufacturer serial numbers, except those on which Airbus modification 55306 or 55792 has been embodied in production.
This AD is not applicable to Airbus A340 -200/-300 aeroplanes repaired in accordance with Repair Drawing R57115053 or R57115051 or
R57115047 (installation of Titanium Doubler on both sides) which are affected by EASA AD 2006-0314.
-
型別
- A330 and A340-200/-300 aeroplanes
-
民航局AD編號
- CAA-2010-02-004
-
原發布國
- EASA
-
原AD編號
- 2010-0024
-
生效日期
- 2010/02/26
-
主旨摘要
- Wings – Centre Wing Box – Keel Beam Fastener Holes at
Frame FR40 - Inspection
-
參考資訊（版本/ATA/SB）
- ATA 57
This AD supersedes EASA AD 2006-0315R1(CAA-2006-10-011A).
Ref.Airbus Service Bulletin A330-57-3081 Revision 03;
Airbus Service Bulletin A340-57-4089 Revision 03;
Airbus Service Bulletin A330-57-3098 at Original issue, Revision 01;
Airbus Service Bulletin A340-57-4106 at Original issue, Revision 01;
Airbus Service Bulletin A330-57-3090 at Original issue;
Airbus Service Bulletin A340-57-4098 at Original issue.
-
存檔序號
- 99-02-006
-
專業分項
- Structure
-
產品類別
- Airplane
-
備註
-
檔案下載
-
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