交通部民用航空局

發布日期

2015/02/04

適用性說明

(1) The Boeing Company Model 717-200 airplanes. (2) The Boeing Company Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, and DC-10-40F airplanes; and Model MD-10-10F and MD-10-30F airplanes. (3) The Boeing Company Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) airplanes; Model MD-88 airplanes; and Model MD-90-30 airplanes.

型別

The Boeing Company Model 717-200, DC-10, MD-10, DC-9, MD-88 , MD-90-30 airplanes.

民航局AD編號

CAA-2015-01-006

原發布國

FAA

原AD編號

2015-02-05

生效日期

2015/03/05

主旨摘要

Navigation - Revise The Maintenance or Inspection Program

參考資訊（版本/ATA/SB）

(i) Special Compliance Item (SCI) 34-4, ''Functional Test of the Captain and First Officer's Altimeter,'' of Appendix A–''SCIs,'' to Boeing Report No. MDC-02K1003, ''Trijet Special Compliance Item Report,'' Revision K, dated February 1, 2013. There is no page ''i'' identified in this document. (ii) Special Compliance Item (SCI) 34-1–''Functional Test of the Captain and First Officer's Altimeter,'' of Appendix A ''SCIs,'' to Boeing Report No. MDC-92K9145, Twinjet Special Compliance Item Report, Revision M, dated February 5, 2013.

存檔序號

104-01-010

專業分項

Avionics,Airworthiness

產品類別

Airplane

備註

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