適航指令資料庫查詢
CAA-2012-09-003(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
- 2012/09/06
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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.
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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-2012-09-003(已有後續修訂版)
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原發布國
- EASA
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原AD編號
- 2012-0170
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生效日期
- 2012/09/14
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主旨摘要
- Time Limits and Maintenance Checks – Tail Rotor Gearbox (TGB) Oil Level and Magnetic Chip Detector – Inspection
Tail Rotor – Pitch Control Rod Bearing – Inspection / Replacement
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參考資訊（版本/ATA/SB）
- (i) This AD supersedes EASA AD 2011-0145 (CAA-2011-08-002).(ii) Eurocopter ASB AS365 No. 05.00.54 Revision 4 dated 16 May 2011,
Eurocopter ASB SA366 No. 05.37 Revision 4 dated 16 May 2011,
Eurocopter ASB EC155 No. 05A015 Revision 5 dated 25 July 2011,
Eurocopter ASB AS365 No. 05.00.61 Revision 2 dated 05 July 2012,
Eurocopter ASB SA366 No. 05.41 Revision 2 dated 05 July 2012,
Eurocopter ASB EC155 No. 05A022 Revision 2 dated 04 July 2012,
Eurocopter SB AS365 No. 65.00.17 Revision 1 dated 21 March 2011,
Eurocopter SB SA366 No. 65.04 Revision 1 dated 21 March 2011, and
Eurocopter SB EC155 No. 65-006 Revision 1 dated 21 March 2011. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
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存檔序號
- 101-09-003
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專業分項
- Structure,Airworthiness
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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