適航指令資料庫查詢
CAA-2010-12-010
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。
-
發布日期
- 2010/12/31
-
適用性說明
- Model S-76A, B, and C helicopters, with LITEF LCR-100, Attitude Heading and Reference System (AHRS) Unit, part number (P/N) 145130-7100, installed, certificated in any category.
-
型別
- Sikorsky Aircraft Corporation (Sikorsky) Model S76A, B, and C Helicopters
-
民航局AD編號
- CAA-2010-12-010
-
原發布國
- FAA
-
原AD編號
- 2010-26-09
-
生效日期
- 2011/01/12
-
主旨摘要
- This AD was prompted by the need to supersede the EAD to state the distinction between IFR and IMC as used in the operating limitations and to reduce the airspeed to 120 KIAS if both autopilots uncouple during IMC or night flight. The actions specified by this AD are intended to implement operating limitations based on an anomaly in the AHRS related to the 26 volt AC inverter that could result in a decoupling of both autopilots and to prevent loss of control of the helicopter during IMC and during night flight.
-
參考資訊（版本/ATA/SB）
- This supersedes an existing emergency airworthiness directive (EAD) No. 2010-11-52(CAA-2010-05-007).Ref:Sikorsky Alert Service Bulletin No. 76-34-11.
-
存檔序號
- 99-12-015
-
專業分項
- Avionics
-
產品類別
- Helicopter
-
備註
-
檔案下載
-
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