適航指令資料庫查詢
CAA-2014-03-010
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
- 2014/03/24
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適用性說明
- Airbus A318-111, A318-112, 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 those on which Airbus modification (mod) 33844 (improvement of aerodynamic shape for CFM pylon), or mod 33847 (improvement of aerodynamic shape for IAE pylon), as applicable, has been embodied in production.
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型別
- AIRBUS A318, A319, A320 and A321 aeroplanes
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民航局AD編號
- CAA-2014-03-010
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原發布國
- EASA
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原AD編號
- 2014-0064
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生效日期
- 2014/03/28
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主旨摘要
- Nacelles / Pylons – Forward Corner Fittings of Pylon Aft Secondary Structure – Inspection / Replacement
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參考資訊（版本/ATA/SB）
- ATA 54. Airbus SB A320-54-1022 original issue dated 07 July 2009, or Revision 01 dated 29 September 2011, or Revision 02 dated 12 July 2013. and Airbus SB A320-54-1019 original issue dated 20 November 2007, or Revision 01 dated 10 April 2008.
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存檔序號
- 103-03-012
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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