適航指令資料庫查詢
CAA-2012-09-003A(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
- 2013/10/28
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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 those modified in accordance with Eurocopter modification (mod) 07 65B63.
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型別
- EUROCOPTER SA 365, AS 365, SA 366 and EC 155 helicopters
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民航局AD編號
- CAA-2012-09-003A(已有後續修訂版)
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原發布國
- EASA
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原AD編號
- 2012-0170R1
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生效日期
- 2013/10/18
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主旨摘要
- Time Limits and Maintenance Checks – Tail Rotor Gearbox (TGB)
Oil Level and Magnetic Chip Detector – Inspection, and Tail Rotor – Pitch Control Rod Bearing – Inspection / Replacement
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參考資訊（版本/ATA/SB）
- ATA 05&65. This AD revises EASA AD 2012-0170(CAA-2012-09-003), dated 31 August 2012, which superseded EASA AD 2011-0145(CAA-2011-08-002) dated 02 August 2011. Ref. Eurocopter AS365 ASB No. 05.00.54 evision 4 dated 16 May 2011. and Eurocopter AS365 ASB No. 05.00.61 Revision 2 dated 05 July 2012, or Revision 3 dated 25 June 2013. and Eurocopter AS365 SB No. 65.00.17 Revision 1 dated 21 March 2011, and Eurocopter SA366 ASB No. 05.37 Revision 4 dated 16 May 2011, and Eurocopter SA366 ASB No. 05.41 Revision 2 dated 05 July 2012, and
Eurocopter SA366 SB No. 65.04 Revision 1 dated 21 March 2011, and
Eurocopter EC155 ASB No. 05A015 Revision 5 dated 25 July 2011, and
Eurocopter EC155 ASB No. 05A022 Revision 2 dated 04 July 2012, or
Revision 3 dated 25 June 2013, and Eurocopter EC155 SB No. 65-006 Revision 1 dated 21 March 2011.
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存檔序號
- 102-10-019
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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