適航指令資料庫查詢
CAA-2017-06-005
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
- 2017/06/13
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適用性說明
- Airbus A318-111, A318-112, A318-121, A318-122, 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 (MSN), except those on which Airbus modification (mod) 160000 (A319 and A320 structural reinforcement for sharklet installation) or mod 160021 (A321 structural reinforcement for sharklet installation) was implemented 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-2017-06-005
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原發布國
- EASA
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原AD編號
- 2017-0099
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生效日期
- 2017/06/22
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主旨摘要
- Wings – Front Spar Vertical Stringers – Inspection
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參考資訊（版本/ATA/SB）
- ATA 57. This AD supersedes EASA AD 2014-0069(CAA-2014-03-016) dated 19 March 2014. Ref. Publications: Airbus SB A320-57-1016 Revision 02 dated 20 January 1998. and Airbus SB A320-57-1017 original issue dated 03 September 1991, or Revision 01 dated 17 March 1997. and Airbus SB A320-57-1178 Revision 01 dated 28 May 2014, or Revision 02 dated 20 November 2015, or Revision 03 dated 29 November 2016. and Airbus SB A320-57-1200 original issue dated 20 November 2015.
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存檔序號
- 106-06-006
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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