適航指令資料庫查詢
CAA-2011-08-012(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
- 2011/08/29
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適用性說明
- EC 155 B, EC 155 B1, SA 365 N, SA 365 N1, AS 365 N2, AS 365 N3 and SA 366 G1 helicopters, all serial numbers except helicopters on which MOD 0767B65 has been embodied in-production or having embodied MOD 0767B65 in-service through accomplishment of Eurocopter AS365 Service Bulletin (SB) No. 67.00.12. or SA 366 SB No. 67.07 or EC 155 SB No. 67-009 Revision 1, as applicable to helicopter version.
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型別
- EUROCOPTER AS 365, EC 155, SA 365 and SA 366
helicopters
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民航局AD編號
- CAA-2011-08-012(已有後續修訂版)
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原發布國
- EASA
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原AD編號
- 2011-0154
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生效日期
- 2011/09/05
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主旨摘要
- Rotor Flight Controls – Collective Pitch Lever Restraining Tab –
Inspection / Adjustment
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參考資訊（版本/ATA/SB）
- ATA 67. This AD supersedes DGAC France AD F-2005-127 R1 dated 01 February 2006 and EASA approval number 2006-0019. Ref. Eurocopter AS 365 Alert Service Bulletin No. 67.00.10 Revision 1 dated 25 February 2009. and Eurocopter SA 366 Alert Service Bulletin No. 67.05 Revision 1 dated 25 February 2009. and Eurocopter EC 155 Alert Service Bulletin No. 67A007 Revision 1 dated 25 February 2009. and Eurocopter AS 365 Service Bulletin No. 67.00.12 dated 25 February 2009. and Eurocopter SA 366 Service Bulletin SB No. 67.07 dated 25 February 2009. and Eurocopter EC 155 Service Bulletin SB No. 67-009 Revision 1 dated 19 July 2010.
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存檔序號
- 100-08-013
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專業分項
- Systems
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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