適航指令資料庫查詢
CAA-2010-05-010A(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
- 2010/08/09
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適用性說明
- SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all serial numbers except 6698, 6701, 6723, 6737 and 6741, delivered before 01 May 2010, flying in IMC (Instrumental Meteorological Conditions), IFR (Instrument Flight Rules) or Night
VFR (Visual Flight Rules) conditions, if equipped with the vertical gyro units GV76-1 installed on the rear left hand (LH) or rear right hand (RH) rack, on which modification 365P081895 (reinforcement of rack for ertical gyro unit GV76-1 in the rear compartment) has not been incorporated.
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型別
- EUROCOPTER SA 365 and AS 365 helicopters
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民航局AD編號
- CAA-2010-05-010A(已有後續修訂版)
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原發布國
- EASA
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原AD編號
- 2010-0100R1
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生效日期
- 2010/08/18
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主旨摘要
- Navigation - Vertical Gyro Unit Data Output - Operational Limitation
/ Operational Procedure / Reinforcement
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參考資訊（版本/ATA/SB）
- ATA 34. This AD revises EASA Emergency AD 2010-0100-E(CAA-2010-05-010) dated 26 May 2010, which superseded EASA AD 2009-0241-E(CAA-2009-11-002 修訂) dated 05 November 2009 and its correction dated 10 December 2009. Ref. Eurocopter AS365 ASB No.01.00.61 Revision 3 dated 28 July 2010.
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存檔序號
- 99-08-002
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專業分項
- Avionics
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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