適航指令資料庫查詢
CAA-2006-10-011(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
- 2006/10/19
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適用性說明
- AIRBUS A330 aircraft, models -201, -202, - 203, - 223, -243, -301, -321, -
322, -323, -341, -342 and -343, all serial numbers, except those on which
AIRBUS modification 49202 has been embodied in production or AIRBUS
Service Bulletin (SB) A330-57-3090 has been embodied in service.
AIRBUS aircraft A340-200 and A340-300 series, all certified models, all
serial numbers, except those on which AIRBUS modification 49202 has
been embodied in production or AIRBUS Service Bulletin (SB) A340-57-
4098 has been embodied in service.
This Airworthiness Directive (AD) is not applicable to A340-200/-300
aircraft repaired in accordance with Repair Drawing R57115053 or
R57115051 or R57115047 (installation of Titanium Doubler) which are
covered by EASA AD 2006 - 0314.
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型別
- A330 and A340-200/-300 aircraft
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民航局AD編號
- CAA-2006-10-011(已有後續修訂版)
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原發布國
- EASA
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原AD編號
- 2006-0315
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生效日期
- 2006/10/27
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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
AIRBUS Service Bulletin A330-57-3081 Revision 02;
AIRBUS Service Bulletin A340-57-4089 Revision 02
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存檔序號
- 95-10-032
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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