適航指令資料庫查詢
CAA-2002-10-007B
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
- 2007/02/06
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適用性說明
- Boeing Model 737-100, -200, -200C, -300, -400, -500, -600, -700, -
700C, -800 and -900 series airplanes.
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型別
- Boeing Model 737 airplanes.
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民航局AD編號
- CAA-2002-10-007B
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原發布國
- FAA
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原AD編號
- 2007-03-07
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生效日期
- 2007/02/16
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主旨摘要
- To prevent failure of one of the two
input control rods of the main rudder PCU, which, under certain conditions, could result in reduced
controllability of the airplane; and to prevent failure of any combination of two input control rods of
the main rudder PCU and/or standby rudder PCU, which could cause an uncommanded rudder
hardover event and result in loss of control of the airplane.
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參考資訊（版本/ATA/SB）
- Supersede AD 2002-20-07R1(CAA-2002-10-007A).Ref:Boeing Alert Service Bulletin 737-27A1280 ,ASB 737-27A1279 ,ASB 737-27A1280,ASB 737-27A1281,SB 737-22-1042 R1,SB 737-27A1206 R3,SB 737-27-1246, including Appendix A R1,SB 737-27-1247R1,SB 737-27-1252 R3,SB 737-27-1253 R3,SB 737-27-1255 R3,SB 737-27-1262,SB 737-27-1263 R1,SB 737-27-1264 R1,SB 737-55-1052 R1.SB 27-1026 and Smiths Aerospace Actuation Systems Service Bulletin 1150-
27-05A.
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存檔序號
- 96-02-001
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專業分項
- Operations
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產品類別
- Airplane
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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