適航指令資料庫查詢
CAA-2012-06-005B(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
- 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, A320-111, 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 that have received AIRBUS modification (mod) 33844 (CFM56 engines), or mod 33847 (IAE V2500 engines) or mod 33687 (PW6000 engines) in production, which introduce an improved aerodynamic pylon shape.
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型別
- Airbus A318, A319, A320, A321 aeroplanes.
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民航局AD編號
- CAA-2012-06-005B(已有後續修訂版)
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原發布國
- EASA
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原AD編號
- 2012-0100R2
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生效日期
- 2012/07/09
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主旨摘要
- Nacelles/Pylons – Aft Pylon Moveable Fairing Rib 5 – Inspection / Repair
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參考資訊（版本/ATA/SB）
- (i) This AD revises EASA AD 2012-0100R1 dated 19 June 2012(CAA-2012-06-005A).
(ii) Airbus SB A320-54A1026 Original issue dated 19 April 2012.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
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存檔序號
- 101-07-001
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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