適航指令資料庫查詢
CAA-2012-10-015A
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
- 2018/03/12
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適用性說明
- EC 155 B, EC 155 B1, SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all manufacturer serial numbers (MSN), if equipped with a 10-blade Tail Rotor Hub (TRH) with Part number (P/N) 365A33351100, P/N 365A33351101 or P/N 365A33351102 installed on the quiet fenestron tail rotor, except helicopters modified in production in accordance with Airbus Helicopters (AH) modification (mod) 0764B51; and
AS 365 N3 helicopters, all MSN, if equipped with an 11-blade TRH with P/N 365A33216001 or P/N 365A33216003 installed on the quiet fenestron tail rotor.
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型別
- AIRBUS EC 155, SA 365 and AS 365 helicopters
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民航局AD編號
- CAA-2012-10-015A
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原發布國
- EASA
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原AD編號
- 2012-0227R1
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生效日期
- 2018/03/08
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主旨摘要
- Tail Rotor – Tail Rotor Hub – Inspection / Replacement
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參考資訊（版本/ATA/SB）
- ATA 64. This AD revises EASA AD 2012-0227(CAA-2012-10-015) dated 29 October 2012, which superseded EASA AD 2011-0144 dated 26 July 2011. Ref. Publications: Eurocopter ASB AS365-05.00.60 Revision 2 dated 09 October 2012. and AH Service Bulletin AS365-64.00.30 original issue dated 13 February 2018.
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存檔序號
- 107-03-008
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專業分項
- Structure
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產品類別
- Helicopter
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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