適航指令資料庫查詢
CAA-2012-10-015(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。
-
發布日期
- 2012/10/31
-
適用性說明
- Eurocopter EC 155 B, EC 155 B1, SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all serial numbers, 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; and Eurocopter AS 365 N3 helicopters, all serial numbers, if equipped with an 11-blade TRH with P/N 365A33216001 or P/N 365A33216003 installed on the quiet fenestron tail rotor.
-
型別
- Eurocopter EC 155, SA 365 and AS 365 Helicopters
-
民航局AD編號
- CAA-2012-10-015(已有後續修訂版)
-
原發布國
- EASA
-
原AD編號
- 2012-0227
-
生效日期
- 2012/11/07
-
主旨摘要
- Tail Rotor – Tail Rotor Hub – Inspection / Replacement
-
參考資訊(版本/ATA/SB)
- (i) This AD supersedes EASA AD 2011-0144(CAA-2011-07-019). (ii)Eurocopter EC 155 ASB 05A021 Revision 1 dated 20 July 2011. Eurocopter ASB AS365-05.00.60 Revision 2 dated 09 October 2012. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
-
存檔序號
- 101-10-018
-
專業分項
- Structure,Airworthiness
-
產品類別
- Helicopter
-
備註
-
檔案下載
-
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