適航指令資料庫查詢
CAA-2012-07-002(已被CAA-2024-05-006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
- 2012/07/06
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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.
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型別
- A318, A319, A320 and A321 aeroplanes.
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民航局AD編號
- CAA-2012-07-002(已被CAA-2024-05-006取代)
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原發布國
- EASA
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原AD編號
- 2012-0118
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生效日期
- 2012/07/18
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主旨摘要
- Fuselage – Centre Fuselage / Main Landing Gear (MLG) Door Keel Beam Hinge and Actuator Fittings – Inspection.
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參考資訊（版本/ATA/SB）
- (i) This AD supersedes EASA AD 2007-0161 (CAA-2007-06-008) dated 11 June 2007. (ii)Airbus SB A320-53-1195 Revision 03, dated 08 November 2011.(iii) Airbus SB A320-53-1196 Revision 02, dated 08 November 2011.(iv) Airbus A318/A319/A320/A321 ALI document reference AI/SE-4/95A.0252/96 issue 11, approved by EASA on 09 November 2010.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
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存檔序號
- 101-07-003
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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