適航指令資料庫查詢
CAA-2011-10-005
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
- 2011/10/11
-
適用性說明
- This AD applies to The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any category, as identified in Boeing Special Attention Service Bulletin 737-27-1282, Revision 1, dated June 14, 2010.
-
型別
- The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER Series Airplanes
-
民航局AD編號
- CAA-2011-10-005
-
原發布國
- FAA
-
原AD編號
- 2011-20-10
-
生效日期
- 2011/11/09
-
主旨摘要
- We are issuing this AD to detect and correct contact between the wire bundle and the left forward rudder quadrant. Damage to the wire bundle from contact between the wire bundle and the left forward rudder quadrant could result in uncommanded stabilizer trim and autopilot disconnects due to shorted wires, potentially affecting the capability of the flightcrew during high work load and consequently reducing control of the airplane. Restricted movement of the rudder quadrant at full right rudder travel would reduce controllability of the airplane.
-
參考資訊(版本/ATA/SB)
- Boeing Special Attention Service Bulletin 737-27-1282, Revision 1.
-
存檔序號
- 100-10-006
-
專業分項
- Systems
-
產品類別
- Airplane
-
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