適航指令資料庫查詢
CAA-2017-01-004
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
- 2017/01/18
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適用性說明
- SA 365 N1, AS 365 N2, AS 365 N3, SA 366 G1, EC 155 B and EC 155 B1 helicopters, all serial numbers, except helicopters equipped with a tail gearbox modified in accordance with Airbus Helicopters (AH) modification (mod) 07 65B63.
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型別
- AIRBUS HELICOPTERS SA 365 helicopter
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民航局AD編號
- CAA-2017-01-004
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原發布國
- EASA
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原AD編號
- 2017-0007
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生效日期
- 2017/01/27
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主旨摘要
- Tail Rotor – Pitch Control Rod Bearing – Inspection / Replacement
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參考資訊（版本/ATA/SB）
- ATA 65. This AD supersedes EASA AD 2016-0097R1(CAA-2016-05-008A) dated 25 May 2016. Ref. Publications: Eurocopter AS365 SB 65.00.17 Revision 1 dated 23 February 2011. and Eurocopter SA366 SB 65.04 Revision 1 dated 23 February 2011. and Eurocopter EC155 SB 65-006 Revision 1 dated 23 February 2011. and Airbus Helicopters ASB AS365-01.00.67 original issue dated 4 May 2016, or Revision 1 dated 03 June 2016, or Revision 2 dated 28 October 2016. and Airbus Helicopters ASB SA366-01.29 original issue dated 4 May 2016, or Revision 1 dated 03 June 2016, or Revision 2 dated 28 October 2016. and Airbus Helicopters ASB EC155-04A014 original issue dated 4 May 2016, or Revision 1 dated 03 June 2016, or Revision 2 dated 28 October 2016.
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存檔序號
- 106-01-006
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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