適航指令資料庫查詢
CAA-2013-10-020(已被CAA-2019-06-001取代)
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
- 2013/11/04
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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 on which Airbus modification (mod.) 21202 has been embodied in production, except those on which mod.152569 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-2013-10-020(已被CAA-2019-06-001取代)
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原發布國
- EASA
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原AD編號
- 2013-0261
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生效日期
- 2013/10/11
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主旨摘要
- Fuselage – Side Box Beam Flange in Frame 43 Area – Inspection / Repair / Modification
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參考資訊（版本/ATA/SB）
- ATA 53. Ref. Airbus SB A320-53-1258 original issue, dated 18 October 2012, and Airbus SB A320-53-1251 original issue, dated 16 November 2012, or Revision 01, dated 18 October 2013.
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存檔序號
- 102-10-026
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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