適航指令資料庫查詢
CAA-2010-06-007
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
- 2010/06/29
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適用性說明
- Airbus Model A318-111, A318-112, A318-121, and A318-122 aeroplanes;
Model A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319- 132, and A319-133 aeroplanes; Model A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, and A320-233 aeroplanes, and Model A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, that are equipped with a Hamilton Sundstrand Ram Air Turbine (RAT) model ERPS08M as identified by Part-Number (P/N) in
Hamilton Sundstrand Service Bulletin (SB) ERPS08M-29-8 original issue dated 17 June 2009
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型別
- AIRBUS A318, A319, A320, and A321 aeroplanes
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民航局AD編號
- CAA-2010-06-007
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原發布國
- EASA
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原AD編號
- 2010-0120
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生效日期
- 2010/07/05
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主旨摘要
- Hydraulic Power – Hamilton Sundstrand Ram Air Turbine Balance
Weight Screws – Inspection / Replacement
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參考資訊（版本/ATA/SB）
- ATA 29. This AD supersedes EASA AD 2009-0259 (CAA-2009-12-005) dated 10 December 2009. Ref. Airbus AOT (All Operators Telex) No.A320-29A1150 original issue and Hamilton Sundstrand Service Bulletin No. ERPS08M-29-8 original issue.
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存檔序號
- 99-06-008
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專業分項
- Systems
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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