Honeywell HS-600 Inmarsat Aircraft Telecommunications Systems User Manual Manual
Honeywell International Inc. Inmarsat Aircraft Telecommunications Systems Manual
Manual
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| Document Description | Manual |
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| Date Submitted | 2002-05-23 00:00:00 |
| Date Available | 2002-11-07 00:00:00 |
| Creation Date | 2002-05-13 13:20:32 |
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| Document Title | Manual |
Honeywell Aerospace Electronic Systems CES--Phoenix P.O. Box 21111 Phoenix, Arizona 85036-1111 U.S.A. System Description and Installation Manual HS--600 High Speed Data System This document contains technical data and is subject to U.S. export regulations. These commodities, technology, or software were exported from the United States in accordance with the export administration regulations. Diversion contrary to U.S. law is prohibited. 23--20--31 Title Page T--1 Printed in U.S.A. Pub. No. A15--5111--006 30 May 2002 SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System PROPRIETARY NOTICE This document and the information disclosed herein are proprietary data of Honeywell. Neither this document nor the information contained herein shall be used, reproduced, or disclosed to others without the written authorization of Honeywell, except to the extent required for installation or maintenance of the recipient’s equipment. NOTICE -- FREEDOM OF INFORMATION ACT (5 USC 552) AND DISCLOSURE OF CONFIDENTIAL INFORMATION GENERALLY (18 USC 1905) This document is being furnished in confidence by Honeywell. The information disclosed herein fall within exemption (b) (4) of 5 USC 552 and the prohibitions of 18 USC 1905. S2002 Honeywell is a U.S. registered trademark of Honeywell. All other marks are owned by their respective companies. 23--20--31 Title Page T--2 Copyright 2002 Honeywell All Rights Reserved 30 May 2002 Please cut along the dotted line. FOR HONEYWELL USE ONLY REPORT OF POSSIBLE DATA ERROR CONTROL NO. DATE RECEIVED To help us improve the quality of our publication, Honeywell encourages any report of a possible data error. PUBLICATION INFORMATION Publication Number A15--5111--006 Volume No. (Book, or Addendum) High Speed Data Unit Publication Title ATA Number Document Type 23--20--31 Latest Issue Date From Title Page System Description and Installation Manual READER INFORMATION Please check all that apply: h Trainer h Technician h Librarian h Engineer h Other (Please specify) Your Name (optional) Company Name Street Address City, State (Province), Zip Code, Country Telephone No. FAX No. POSSIBLE DATA ERROR Page No. Paragraph Figure No. Table No. Description of Possible Data Error Please cut along the dotted line. HONEYWELL REPLY Please mail or FAX completed form to Technical Publications Quality Administrator. If returning by mail, please tape this form closed (U.S. postal regulations prohibit the use of staples). If sending by FAX, the Technical Publications’ U.S. FAX No. is (602- 436- 3900). If sending by email, the email address is tpqa@honeywell.com. Local reproduction of this form is encouraged. This form is based on electronic form INF--300, Revision 0 DO NOT STAPLE FOLD BUSINESS REPLY MAIL FIRST CLASS PERMIT NO. 3532, PHOENIX, AZ POSTAGE WILL BE PAID BY ADDRESSEE Honeywell Aerospace Electronic Systems CES--Phoenix P.O. Box 21111 Phoenix, Arizona 85036-1111 U.S.A. ATTN: Technical Publications Quality Administrator FOLD DO NOT STAPLE NO POSTAGE NECESSARY IF MAILED IN THE UNITED STATES Please cut along the dotted line. FOR HONEYWELL USE ONLY CUSTOMER RESPONSE CONTROL NO. DATE RECEIVED To help us improve the quality of our publications, Honeywell encourages readers to provide input to the customer--satisfaction survey below. We welcome all comments and recommendations. PUBLICATION INFORMATION Publication Number A15--5111--006 Volume No. (Book, or Addendum) High Speed Data Unit Publication Title ATA Number Document Type 23--20--31 Latest Issue Date From Title Page System Description and Installation Manual READER INFORMATION Please check all that apply: h Trainer h Technician h Librarian h Engineer h Other (Please specify) Your Name (optional) Company Name Street Address City, State (Province), Zip Code, Country Telephone No. FAX No. CUSTOMER--SATISFACTION SURVEY Please check the yes or no box to answer the following questions: Yes No 1. Is the Publication technically accurate? 2. Is information easy to find? 3. Is information complete? 4. Are figures easy to use? 5. Are tables easy to use 6. Is the Publication used for training? 7. Do you or your organization wish to remain on distribution for this publication? Please rate this publication in comparison to other documents you use. Good Fair Poor Please cut along the dotted line. Please provide comments, recommendations and/or improvements that you would like to see in this publication. Please mail or FAX completed form to Technical Publications Quality Administrator. If returning by mail, please tape closed (U.S. postal regulations prohibit the use of staples). If sending by FAX, the Technical Publications’ U.S. FAX No. is (602- 436- 3900). If sending by email, the email address is tpqa@honeywell.com. Local reproduction of this form is encouraged. DO NOT STAPLE FOLD BUSINESS REPLY MAIL FIRST CLASS PERMIT NO. 3532, PHOENIX, AZ POSTAGE WILL BE PAID BY ADDRESSEE Honeywell Aerospace Electronic Systems CES--Phoenix P.O. Box 21111 Phoenix, Arizona 85036-1111 U.S.A. ATTN: Technical Publications Quality Administrator FOLD DO NOT STAPLE NO POSTAGE NECESSARY IF MAILED IN THE UNITED STATES SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System RECORD OF REVISIONS For each revision, put the revised pages in your manual and discard the superseded pages. Write the revision number and date, date put in manual, and the incorporator’s initials in the applicable columns on the Record of Revisions. The initial H shows Honeywell is the incorporator. Revision Number Revision Date Date Put In Manual By Revision Number Revision Date 23--20--31 Date Put In Manual By Page RR--1 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Blank Page 23--20--31 Page RR--2 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System RECORD OF TEMPORARY REVISIONS Instructions on each page of a temporary revision tell you where to put the pages in your manual. Remove temporary revision pages only when discard instructions are given. For each temporary revision, put the applicable data in the record columns on this page. Temporary Revision Number Temporary Revision Date Temporary Revision Status Date Put in Manual By * Date Removed from Manual By * * The initial H in this column shows Honeywell has done this task. 23--20--31 Page RTR--1 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Blank Page 23--20--31 Page RTR--2 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System SERVICE BULLETIN LIST Service Bulletin Identified Mod Date Included in this Manual Description 23--20--31 Page SBL--1 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Blank Page 23--20--31 Page SBL--2 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System LIST OF EFFECTIVE PAGES Subheading and Page Date Title T--1 T--2 30 May 2002 30 May 2002 Record of Revisions RR--1 RR--2 30 May 2002 30 May 2002 Record of Temporary Revisions RTR--1 RTR--2 30 May 2002 30 May 2002 Service Bulletin List SBL--1 SBL--2 30 May 2002 30 May 2002 List of Effective Pages LEP--1 LEP--2 30 May 2002 30 May 2002 Table of Contents TC--1 TC--2 TC--3 TC--4 TC--5 TC--6 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 Introduction INTRO--1 INTRO--2 INTRO--3 INTRO--4 30 May 2002 30 May 2002 30 May 2002 30 May 2002 System Description and Operation 1--1 1--2 1--3 30 May 2002 30 May 2002 30 May 2002 Subheading and Page 1--4 1--5 1--6 1--7 1--8 1--9 1--10 1--11 1--12 1--13 1--14 Date 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 Mechanical Installation 2--1 2--2 F 2--3/2--4 F 2--5/2--6 F 2--7/2--8 2--9 2--10 2--11 2--12 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 Electrical Installation 3--1 3--2 3--3 3--4 3--5 3--6 3--7 3--8 3--9 3--10 F 3--11/3--12 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 indicates a changed or added page. indicates a foldout page. 23--20--31 Page LEP--1 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Subheading and Page Date Installation Check 4--1 4--2 4--3 4--4 30 May 2002 30 May 2002 30 May 2002 30 May 2002 Adjustment/test 5--1 5--2 5--3 5--4 5--5 5--6 5--7 5--8 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 Subheading and Page B--4 B--5 B--6 B--7 B--8 B--9 B--10 Date 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 Fault Isolation 6--1 6--2 30 May 2002 30 May 2002 Maintenance Practices 7--1 7--2 7--3 7--4 30 May 2002 30 May 2002 30 May 2002 30 May 2002 M4 Call Cause Code List A--1 A--2 A--3 A--4 A--5 A--6 A--7 A--8 A--9 A--10 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 30 May 2002 Inmarsat Registration Form B--1 B--2 B--3 30 May 2002 30 May 2002 30 May 2002 indicates a changed or added page. indicates a foldout page. 23--20--31 Page LEP--2 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. CONTENTS SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System TABLE OF CONTENTS Subject Page INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INTRO--1 1. Proprietary, Export, and Precautionary Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INTRO--1 A. Proprietary Notice . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INTRO--1 B. Export Notice . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INTRO--1 C. Special Precautions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INTRO--1 Content Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INTRO--2 A. How to Use This Manual . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INTRO--2 B. Weights and Measurements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INTRO--3 C. Acronyms and Abbreviations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INTRO--3 Customer Assistance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INTRO--4 A. Who to Contact . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INTRO--4 SYSTEM DESCRIPTION AND OPERATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--1 1. Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--1 A. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--1 B. Aero--H/H+ . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--3 C. Inmarsat High Speed Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--3 D. System Performance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--4 E. FCC Compliance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--5 System Components . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--6 A. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--6 Component Descriptions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--7 A. HS--600 High Speed Data Unit (HSU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--7 B. High Speed Combiner Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--12 C. RF Power Splitter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--13 D. HSU Mounting Tray . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--13 MECHANICAL INSTALLATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--1 1. Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--1 A. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--1 B. Equipment and Materials . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--1 Mechanical Installation Design . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--1 A. 2--1 2. 3. 2. 3. 2. HS--600 HSU Provisions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23--20--31 Page TC--1 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System B. High Speed Combiner Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--1 C. RF Power Splitter Provisions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--1 ELECTRICAL INSTALLATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--1 1. Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--1 A. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--1 B. Equipment and Materials . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--1 Electrical Installation Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--1 A. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--1 B. Power Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--1 C. Ground Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--2 (1) General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--2 (2) Chassis Grounding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--2 (3) Shield Grounds . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--3 (4) Power/Signal Grounds . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--4 Electrical Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--5 A. HS--600 HSU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--5 INSTALLATION CHECK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--1 1. Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--1 A. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--1 Installation Checkout . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--1 A. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--1 B. Cable Loss Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--1 (1) HS--600 HSU to HPA Path Loss . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--1 (2) HPA to Antenna Loss . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--1 C. Power Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--2 D. RF Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--2 ADJUSTMENT/TEST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--1 1. Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--1 A. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--1 Details . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--1 A. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--1 B. Software . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--1 C. System Initialization . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--1 2. 3. 2. 2. 23--20--31 Page TC--2 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System D. Typical Maintenance Port Start--Up Information . . . . . . . . . . . . . . . . . . . . . . . . 5--3 E. Maintenance Menu Items . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--6 FAULT ISOLATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--1 1. Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--1 A. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--1 MAINTENANCE PRACTICES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--1 1. Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--1 A. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--1 B. Equipment and Materials . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--1 Procedure for the HS--600 HSU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--1 A. Removal and Reinstallation Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--1 B. Adjustment Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--2 C. Repair Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--2 D. Return to Service Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--2 Procedure for the Combiner/Splitter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--2 A. Removal and Reinstallation Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--2 B. Adjustment Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--3 C. Repair Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--3 D. Return to Service Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--3 Instructions for Continued Airworthiness, Code of Federal Regulation CFR 91.213 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--4 A. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--4 B. Instructions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--4 APPENDIX A M4 CALL CAUSE CODE LIST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A--1 1. Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A--1 A. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A--1 APPENDIX B INMARSAT REGISTRATION FORM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B--1 1. Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B--1 A. B--1 2. 3. 4. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23--20--31 Page TC--3 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System List of Illustrations Figure Figure 1-1. High Speed Data System Block Diagram . . . . . . . . . . . . . . . . . . . . . . Page 1--1 Figure 1-2. HS--600 HSU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--8 Figure 1-3. High Speed Combiner Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--12 Figure 1-4. RF Power Splitter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--13 Figure 2-1. HSU Outline and Installation Diagram . . . . . . . . . . . . . . . . . . . . . . . . . 2--3 Figure 2-2. High Speed Combiner Outline and Installation Diagram . . . . . . . . . 2--7 Figure 2-3. RF Power Splitter Outline Diagram . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--9 Figure 2-4. Typical Dimensions for 4--MCU Tray Assemblies . . . . . . . . . . . . . . . . 2--10 Figure 2-5. Typical Dimensions for 8--MCU Tray Assemblies . . . . . . . . . . . . . . . . 2--11 Figure 3-1. Electric Cable Chart . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--2 Figure 3-2. Example 1, Multi--point Shield Ground . . . . . . . . . . . . . . . . . . . . . . . . 3--3 Figure 3-3. Example 2, Multi--point Shield Ground . . . . . . . . . . . . . . . . . . . . . . . . 3--3 Figure 3-4. Shield Grounding Example for Rack Mount Connectors . . . . . . . . . 3--4 Figure 3-5. Aircraft Grounding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--5 Figure 3-6. HSU ARINC 600 Connector (P1) Pin Layout . . . . . . . . . . . . . . . . . . . 3--6 Figure 3-7. Contact Arrangements for P1--C Bottom Insert, HSU ARINC 600 Connector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--9 Figure 3-8. HSU Data Loader Connector (J1) Pin Layout . . . . . . . . . . . . . . . . . . 3--9 Figure 3-9. RF System Interface . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--10 Figure 3-10. High Speed Data System Interconnect Diagram . . . . . . . . . . . . . . . . 3--11 Figure 4-1. RX Path Loss . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--3 Figure 4-2. TX Path Loss . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--3 Figure 5-1. SDU to PC Cable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--2 Figure 5-2. HSU RS--232 Maintenance Cable . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--2 23--20--31 Page TC--4 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System List of Tables Table Intro--1. Related Publications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INTRO--2 Table 1-1. SDU DLT RS--232 Port Configuration . . . . . . . . . . . . . . . . . . . . . . . . . 1--2 Table 1-2. SDU CMT Keystrokes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--2 Table 1-3. Type of Service . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--3 Table 1-4. Assumptions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--4 Table 1-5. Calculations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--4 Table 1-6. Total Number of Calls with Aero--H+ (Spot beam operation) and 10.5 Kbps Packet Data Rate . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--4 Table 1-7. Total Number of Calls with Aero--H+ (Spot beam operation) and 600 bps Packet Data Rate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--5 Table 1-8. Total Number of Calls with Aero--H+ (Global beam operation) and 10.5 Kbps Packet Data Rate . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--5 Table 1-9. Total Number of Calls with Aero--H+ (Global beam operation) and 600 bps Packet Data Rate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--5 Table 1-10. Components Supplied by Honeywell . . . . . . . . . . . . . . . . . . . . . . . . . 1--6 Table 1-11. Components/Parts Not Supplied by Honeywell . . . . . . . . . . . . . . . . 1--6 Table 1-12. HS--600 Leading Particulars . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--9 Table 1-13. DO--160D Environmental Categories . . . . . . . . . . . . . . . . . . . . . . . . . 1--10 Table 1-14. HSU Front Panel Light Description . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--11 Table 1-15. HSU Mounting Trays . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--14 Table 3-1. Contact Arrangements for P1--A Top Insert, HSU ARINC 600 Connector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--7 Table 3-2. Contact Arrangements for P1--B Top Insert, HSU ARINC 600 Connector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--8 Table 4-1. Power Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--2 Table 4-2. RF Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--2 Table 5-1. SDU to PC Wire List . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--1 Table 5-2. HSU to RS--232 Maintenance Port Wire List . . . . . . . . . . . . . . . . . . . 5--2 Table 5-3. Typical HS--600 Maintenance Port Information . . . . . . . . . . . . . . . . . 5--3 Table 5-4. Maintenance Menu Items . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--6 Table A--1. Call Cause Code List . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A--1 23--20--31 Page TC--5 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Blank Page 23--20--31 Page TC--6 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. INTRODUCTION SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System INTRODUCTION 1. Proprietary, Export, and Precautionary Data A. Proprietary Notice (1) This document and the information disclosed herein are proprietary data of Honeywell. Neither this document nor the information contained herein shall be used, reproduced, or disclosed to others without the written authorization of Honeywell, except to the extent required for installation or maintenance of the recipient’s equipment. FREEDOM OF INFORMATION ACT (5 USC 552) AND DISCLOSURE OF CONFIDENTIAL INFORMATION GENERALLY (18 USC 1905). (2) This document is being furnished in confidence by Honeywell. The information disclosed herein falls within exemption (b) (4) of 5 USC 552 and the prohibitions of 18 USC 1905. Copyright 2002 Honeywell. All Rights Reserved. (3) Honeywell is a U.S. registered trademark of Honeywell. All other marks are owned by their respective companies. B. Export Notice (1) This document contains unrestricted technical data and is being exported under license exception TSU/OTS in accordance with EAR Section 740.13(a). (2) These commodities, technology, or software were exported from the United States in accordance with the export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 7E994 Schedule B#4901.99.0050 C. Special Precautions (1) Warnings, cautions, and notes in this manual give the data that follows: • A WARNING is an operation or maintenance procedure or condition that, if not obeyed, can cause injury or death. • A CAUTION is an operation or maintenance procedure or condition that, if not obeyed, can cause damage to the equipment. • A NOTE gives data to make the work easier or gives directions to go to a procedure. (2) All personnel who operate equipment and do maintenance specified in this manual must know and obey the safety precautions. The warnings and cautions that follow apply to all parts of this manual. 23--20--31 Page INTRO--1 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System WARNING: BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATERIAL SAFETY DATA SHEETS FOR SAFETY INFORMATION. SOME MATERIALS CAN BE DANGEROUS. CAUTION: DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO MATERIALS SPECIFIED BY HONEYWELL. MATERIALS THAT ARE NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN VOID THE WARRANTY. CAUTION: THE HS--600 HIGH SPEED DATA SYSTEM CONTAINS ITEMS THAT ARE ELECTROSTATIC DISCHARGE SENSITIVE (ESDS). IF YOU DO NOT OBEY THE NECESSARY CONTROLS, A FAILURE OR UNSATISFACTORY OPERATION OF THE UNIT CAN OCCUR FROM ELECTROSTATIC DISCHARGE. USE APPROVED INDUSTRY PRECAUTIONS TO KEEP THE RISK OF DAMAGE TO A MINIMUM WHEN YOU TOUCH, REMOVE, OR INSERT PARTS OR ASSEMBLIES. 2. Content Data A. How to Use This Manual (1) This manual gives general system description and installation information for the HS--600 High Speed Data System. It also gives block diagram and interconnect information to permit a general understanding of the system interface. (2) The purpose of this manual is to help you install, operate, maintain, and troubleshoot the HS--600 High Speed Data System. Common system maintenance procedures are not presented in this manual. The best established shop and flight line practices should be used. (3) Related publications that are referred to in this manual are identified in Table Intro--1. Table Intro--1. Related Publications Publication Publication No. Handling, Storage, and Shipping Procedures for Honeywell Avionics Equipment Instruction Manual A09--1100--001 MCS--3000/6000 Multi--Channel Satellite Communications System Description, Installation, and Maintenance Manual C15--5111--005 MCS--4000/7000 Multi--Channel SATCOM System Description, Installation, and Maintenance Manual A15--5111--001 NOTES: 1. You can order a Honeywell publication from Honeywell as follows: Telephone No.: (602) 436--6900 Fax No.: (602) 436--1588 E--mail: cas--publications--distribution@honeywell.com 23--20--31 Page INTRO--2 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System B. Weights and Measurements (1) All weights and measurements are in U. S. values. (2) The letter symbols for units of measurement are the same as shown in ANSI/IEEE Std 260. C. Acronyms and Abbreviations (1) The acronyms and abbreviations that follow help the reader identify terms and definitions used by Honeywell. (2) The letter symbols for units of measurement are the same as shown in ANSI/IEEE Std 260. Term Definition ACSE ACU access control and signalling equipment antenna control unit BSU beam steering unit CCA CMT CNS/ATM circuit card assembly commissioning and maintenance terminal communication, navigation, and surveillance/air traffic management DLNA DLT diplexer/low noise amplifier data logging terminal ESD ESDS electrostatic discharge electrostatic discharge sensitive HGA HIRF HPA HSD HSU high gain antenna high intensity radiated electromagnetic frequencies high power amplifier high speed data high speed data unit ICAO IPC IPDS IRS ISDN International Civil Aviation Organization: Agency of the UN Illustrated Parts Catalog Inmarsat Packet Mode Data Service inertial reference system Integrated Services Digital Network LES LESA LRU land earth station land earth station assignment line replaceable unit 23--20--31 Page INTRO--3 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Term Definition M4 MCS MCU MEL MES MM/HSD MTBF multi--media mini--M multi--channel SATCOM modular concept unit minimum equipment list Mobile Earth Station Mini M/high speed data mean--time--between--failures NCSA network coordination station assignment PC PID PSTN personal computer personal identification number Public Switched Telephone Network RF RFU radio frequency radio frequency unit SATCOM SCPC SDM SDU SU satellite communications single channel per circuit System Definition Manual satellite data unit signal unit TDM TDMA time division multiplex time division multiple access 3. Customer Assistance A. Who to Contact (1) For assistance with installation, operation, or maintenance of the HS--600 High Speed Data System, contact your local Honeywell Dealer or regional Honeywell Customer Support Engineer. Additional assistance can be obtained from: • Honeywell Aviation Services, Customer Response Center (CRC) Commercial Electronic Systems 21111 N. 19th Avenue Phoenix, AZ 85027 TEL: FAX: (877) 436--2005 (Toll--Free) (602) 436--1501 23--20--31 Page INTRO--4 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEMS DESCRIPTION AND OPERATION SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System SECTION 1 SYSTEM DESCRIPTION AND OPERATION 1. Overview A. General (1) The HS--600 high speed data system provides multi--channel Inmarsat Aero cockpit and passenger voice, fax, and data, and multi--media mini--M (M4) circuit--mode services simultaneously. Figure 1-1 shows a block diagram of the high speed data (HSD) system. Figure 1-1. High Speed Data System Block Diagram 23--20--31 Page 1--1 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System (2) The HSD system is capable of being integrated with the MCS--3000, MCS--6000, MCS--4000, and MCS--7000 multi--channel (MCS) satellite communications (SATCOM) systems with Aero--H/H+ high gain antennas (HGA). The HSD system is interfaced with its own dedicated 40 W high power amplifier (HPA). (3) The L--band radio frequency (RF) outputs of the HSD system HPA and the satellite data unit (SDU)/radio frequency unit (RFU) 40 W HPA is combined with a high power combiner. The output of the high power combiner drives a common diplexer/low noise amplifier (DLNA) and a nominal 12 dB gain antenna. The SDU manages the satellite selection and steers the HGA. (4) The Aero--H/H+ SDU and HPA requires no hardware or operational software modifications, and operates without knowledge of the HSD system presence. However, each SDU used in conjunction with the HSD system will require advance configuration of its data logging terminal (DLT) parameter settings. (5) The SDU’s DLT RS--232 port must be configured to transmit the ASCII data given in Table 1-1, at a rate of approximately 1 Hz, for the functions in Table 1-1 to be performed in the HSD system (SDU to HSU transmit only). Table 1-1. SDU DLT RS--232 Port Configuration Data Function Satellite Selected Satellite selection Position (Latitude/Longitude) Spot beam selection Satellite--Relative Velocity Open--loop Doppler compensation Current Antenna Gain Antenna gain variation compensation Log--On Status Status of satellite selected indication (stable or not) (6) The SDU CMT keystrokes given in Table 1-2 (starting from the main menu) are required to configure the SDU to broadcast the desired data from its DLT port. Table 1-2. SDU CMT Keystrokes Keystroke HBA Description To logging menu 00020509Enter logging word B1 Set logging period C60 Set heading record frequency E1 Select DLT port for output D1 Enable logging 23--20--31 Page 1--2 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System (7) The DLT configuration settings remain in effect indefinitely, unless subsequently manually changed or a factory settings restart is performed. If the SDU in conjunction with the HSD system is replaced for any reason, the replacement SDU will require its DLT port to be configured appropriately. (8) The HSD system controls its HPA through the HPA’s commissioning and maintenance terminal (CMT) RS--232 input port (HSU to HPA transmit only), dynamically controlling the transmit RF carrier on/off state as well as the HPA’s backoff state. B. Aero--H/H+ (1) Aero--H/H+ is a multi--channel aeronautical system that can operate in both the Inmarsat--3 global and spot beams using either a fuselage-- or tail--mounted HGA. The type of antenna and the global/spot beam operation identify the type of service possible as given in Table 1-3. Table 1-3. Type of Service Global Beam Spot Beam High gain Yes No Yes No Yes 4.8 kbps 2.4 kbps 10.5 kbps Aero--H+ High gain Yes Yes Yes Yes Yes 4.8/2.4 kbps 2.4 kbps 10.5 kbps Aero Type Aero--H Antenna Voice 4.8 kbps Secure Voice 4.8 kbps Packet Mode Data (max) Voice 9.6 kbps Fax (max) PC Data (max) (2) When used within the spot beams, Aero--H+ voice and data rates are lower. Therefore, it requires less power so that call charges are reduced. All Honeywell/Thales aeronautical equipment complies with the International Civil Aviation Organization (ICAO) Agency of the UN requirements for aeronautical safety services. The equipment can be used for communication, navigation, and surveillance/air traffic management (CNS/ATM). C. Inmarsat High Speed Systems (1) Aero M4 circuit--mode service provides data rates of up to 64 kbps. M4 land earth stations (LES) serve as gateways to the Public Switched Telephone Network (PSTN) or the ISDN. (2) M4 is a companion to, but not a replacement for, an Aero--H system. As developments of the Mini--M, they do not comply with the ICAO requirements for aeronautical safety services and cannot be used for CNS/ATM. In other words, they can only be used for non--safety service data communications. 23--20--31 Page 1--3 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System D. System Performance (1) Currently, the numbers of simultaneous aeronautical voice and M4 data channels can only be obtained from theoretical calculations. Using the assumptions given in Table 1-4, the calculations are given in Table 1-5. The calculations for the total number of calls are given in Table 1-6 thru Table 1-9. Table 1-4. Assumptions Item dB Gain cell Watts 12 dB R/T power (10.5 Kbps assumed) 20.4 dBW 109.6 W R/T power (600 bps assumed) 5.9 dBW 3.9 W HPA power (same assumed for both) 16.0 dBW 40.0 W Cable Loss 4.7 dB Initial HSD channel power 22.5 dBW 177.8 W Settled HSD channel power 22.5 dBW 177.8 W Initial 8400 C channel EIRP 14.5 dBW 28.2 W Settled 8400 C channel EIRP 7.5 dBW 5.6 W Initial 21000 C channel EIRP 19.5 dBW 89.1 W Settled 21000 C channel EIRP 13.5 dBW 22.4 W Table 1-5. Calculations HGA Gain dBW Total Watts After R/T 600 bps (Watts) After R/T 10.5 Kbps (Watts) 12 23.3 214.8 210.9 105.2 Table 1-6. Total Number of Calls with Aero--H+ (Spot beam operation) and 10.5 Kbps Packet Data Rate M4 HSD Channels 8400 Voice Channels 21000 Voice Channels 5/6 (Note) NOTE: MCS 6000 = 5, MCS 7000 = 6 23--20--31 Page 1--4 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table 1-7. Total Number of Calls with Aero--H+ (Spot beam operation) and 600 bps Packet Data Rate M4 HSD Channels 8400 Voice Channels 21000 Voice Channels 5/6 (Note) NOTE: MCS 6000 = 5, MCS 7000 = 6 Table 1-8. Total Number of Calls with Aero--H+ (Global beam operation) and 10.5 Kbps Packet Data Rate M4 HSD Channels 8400 Voice Channels 21000 Voice Channels 1/2 Table 1-9. Total Number of Calls with Aero--H+ (Global beam operation) and 600 bps Packet Data Rate M4 HSD Channels 8400 Voice Channels 21000 Voice Channels (2) From these calculations the following points should be made: (a) There is an increased loss of 3.5 dB, due to the addition of the high power combiner with the HS--600 installation. It is essential that a 12 dB antenna is used to be able to support more than one Aero voice channel as well as a simultaneous Aero M4 HSD. E. FCC Compliance (1) This device complies with part 15 of the FCC rules. Operation is subject to the following two conditions: • This device may not cause harmful interference. • This device must accept any interference received, including interference that may cause undesired operation. 23--20--31 Page 1--5 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System 2. System Components A. General (1) Table 1-10 gives the component part numbers supplied by Honeywell. Table 1-11 gives components that are necessary, but are not supplied by Honeywell. Table 1-10. Components Supplied by Honeywell Component Model No. Honeywell Part No. High Speed Data Unit HS--600 7519300--901 High Speed Combiner Assembly -- 7519340--901 RF Power Splitter -- 7519349--1 High Power Amplifier (40 W) HP--600 7516250--XX050 (Note) NOTE: The HSD system requires an additional HPA. Only an HPA, Part No. 7516250--XX050 (software Mod F) can be used with the HS--600 system. Table 1-11. Components/Parts Not Supplied by Honeywell Component/Part Comments HSU Mounting Tray (4--MCU size unit) ARINC 600 4--MCU Mount, cooling air required. (Installer to supply mount.) HSU Mounting Tray (8--MCU size unit) ARINC 600 8--MCU Mount, cooling air required. (Installer to supply mount.) NOTE: Refer to paragraph 3.D. and Table 1-15 in this section for mounting tray information. 23--20--31 Page 1--6 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System 3. Component Descriptions A. HS--600 High Speed Data Unit (HSU) (1) The HSU is designed to perform reliably under field conditions and provide ease of maintenance when required. The HSU has a modular design to permit easy replacement of each circuit card assembly (CCA). All CCAs are built to standards that qualify them for both airline and business aircraft usage. (2) The HSU is packaged as a 4 modular concept unit (4--MCU). The mechanical chassis is constructed of aluminum alloy sheet metal. The HSU requires external cooling air in accordance with ARINC 600 or ARINC 404 to maintain the highest possible mean--time--between--failures (MTBF). In installations where this is not available, a mounting tray with an integral fan is required. Refer to Table 1-15. The HSU is shown in Figure 1-2. (3) Table 1-12 gives the leading particulars for the HSU and Table 1-13 gives the DO--160D categories that this equipment meets or exceeds. 23--20--31 Page 1--7 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Figure 1-2. HS--600 HSU 23--20--31 Page 1--8 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table 1-12. HS--600 Leading Particulars Characteristic Specification Dimensions (maximum): • Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.64 in. (194.06 mm) • Width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.90 in. (124.46 mm) • Height . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15.26 in. (387.60 mm) Weight (maximum) . . . . . . . . . . . . . . . . . . . . . . . 11.84 lb (5.37 kg) Power requirements (AC) (Note): • Nominal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 115 V rms, 400 Hz • Maximum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 134 V rms, 480 Hz • Minimum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 97 V rms, 320 Hz Power requirements (DC) Note): • Nominal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27.5 V dc • Maximum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32.2 V dc • Minimum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20.5 V dc Power Consumption . . . . . . . . . . . . . . . . . . . . . . 25 W nominal, 40 W maximum Cooling Requirements . . . . . . . . . . . . . . . . . . . . Select tray from Table 1-15 Connector P1 (Rear) . . . . . . . . . . . . . . . . . . . . . . Radiall Part No. 620--600--237 Mating Connector (P1) . . . . . . . . . . . . . . . . . . . . Radiall Part No. 620--600--238 • 22 AWG Contacts . . . . . . . . . . . . . . . . . . . . . . Radiall Part No. 620--200 • 20 AWG Contacts . . . . . . . . . . . . . . . . . . . . . . Radiall Part No. 620--310 • 16 AWG Contacts . . . . . . . . . . . . . . . . . . . . . . Radiall Part No. 620--330 • 12 AWG Contacts . . . . . . . . . . . . . . . . . . . . . . Radiall Part No. 620--340 • Size 5 Coax Contacts . . . . . . . . . . . . . . . . . . . Radiall Part No. 620--021 Mounting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Tray, ARINC 600 4--MCU Size Circuit Breaker Ratings: • 115 V ac Circuit Breaker . . . . . . . . . . . . . . . . 2 Amp typical • 28 V dc Circuit Breaker . . . . . . . . . . . . . . . . . 7.5 Amp typical User Interface (ISDN S/T) . . . . . . . . . . . . . . . . . ITU--T 1.430 (S/T interface) DSS1/EuroISDN Environmental . . . . . . . . . . . . . . . . . . . . . . . . . . . Unit must be installed inside pressurized bulkhead (cabin). 23--20--31 Page 1--9 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table 1-13. Description DO--160D Environmental Categories Category Temperature and Altitude XX In--Flight Loss of Cooling Temperature Variation Humidity Shock Vibration SB2 Explosion Proofness Waterproofness Fluids Susceptibility Sand and Dust Fungus Resistance Salt Spray Magnetic Effect Power Input Voltage Spike Audio Frequency Susceptibility Induced Signal Susceptibility Radio Frequency (RF) Susceptibility Emission of RF Energy Lightning Indirect Effects XXX XXXX Lightning Direct Effects Icing Electrostatic Discharge (ESD) 23--20--31 Page 1--10 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System (4) Table 1-14 gives a description of the HSU front panel lights during various HSU conditions. The PUSH TO TEST switch on the front panel of the HSU is not operational. Table 1-14. Condition HSU Front Panel Light Description Description Power Up Both PASS and FAIL lights are on steady. Software Boot Complete Both PASS and FAIL lights are off. The lights should go off within 30 seconds of power up. Receiver Activity If the SDU is logged on, the HS--600 is able to pick an LES to listen to, similar to the P--channel for the MCS. Once the receiver synchronizes on this time division multiplex (TDM) channel, the green PASS light flashes. The light flashes for each correctly received signal unit (SU). This should occur within 2 minutes of power up, if the SDU is logged on, or within 30 seconds after the SDU log--on, if beyond the initial 2 minutes. Since the flash rate is related to the received SUs, the rate varies as time goes on; it could even stop flashing with the light on or off. However, during an HSD call, SUs are received at a high rate, so the green PASS light will flash rapidly, appearing to be almost steady on. Failure The FAIL light will be on if any error occurs. 23--20--31 Page 1--11 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System B. High Speed Combiner Assembly (1) The high speed combiner assembly combines the signals from both HPAs which are then sent to the DLNA. Figure 1-3 shows the high speed combiner assembly. Figure 1-3. High Speed Combiner Assembly 23--20--31 Page 1--12 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System C. RF Power Splitter (1) The RF power splitter divides the signal from the DLNA which is then sent to the SDU and HSU. The unit weight is 2.5 oz. (70.87 grams). Figure 1-4 shows the RF power splitter. Figure 1-4. RF Power Splitter D. HSU Mounting Tray (1) The HS--600 HSU ARINC 600 connector, contacts, and mounting trays can be purchased from ECS or EMTEQ. The addresses for ECS and EMTEQ are as follows: Electronic Cable Specialists 5300 W. Franklin Drive Franklin, WI 53132 U.S.A. Telephone: (414) 421--5300 Fax: (414) 421--5301 EMTEQ S84 W. 18693 Enterprise Drive Muskego, WI 53150 U.S.A. Telephone: (262) 679--6170 / 1--888--679--6170 23--20--31 Page 1--13 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System (2) Table 1-15 gives a list of HSU mounting trays available through ECS. Contact EMTEQ for a list of HSU mounting trays available. Table 1-15. ECS Part No. HSU Mounting Trays Description Voltage 6050--101 4 MCU S/S tray with bottom fan 115 V ac 6049--101 4 MCU S/S tray with right side fan 115 V ac 6049--102 4 MCU S/S tray with left side fan 115 V ac 6083--102 4 MCU S/L tray with rear fan 115 V ac 6050--102 4 MCU S/S tray with bottom fan 28 V dc 200--89891--101 4 MCU S/S tray with left side fan 28 V dc 200--89892--101 4 MCU S/S tray with right side fan 28 V dc 6083--103 4 MCU S/L tray with rear fan 28 V dc 6292--101 8 MCU S/S standard tray 115 V ac 6288--101 8 MCU S/S tray w/bottom fan 115 V ac 6290--101 8 MCU S/S tray w/left side fan 115 V ac 6284--101 8 MCU S/S tray w/right side fan 115 V ac 6286--101 8 MCU S/L standard tray 115 V ac 23--20--31 Page 1--14 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. MECHANICAL INSTALLATION SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System SECTION 2 MECHANICAL INSTALLATION 1. Overview A. General (1) This section contains information on how and where to mount the HSU, combiner, and splitter. Figure 2-1 shows the HSU dimensions. Figure 2-2 shows the dimensions and mounting hole dimensions of the combiner. B. Equipment and Materials (1) For new HSU installations, refer to Table 1-11 for mounting tray information. See the applicable outline and installation diagram in this section for additional mounting information. 2. Mechanical Installation Design A. HS--600 HSU Provisions (1) Mechanical installation data for the HS--600 HSU is shown in Figure 2-1. The HSU is mounted in an ARINC 600 4--MCU mounting tray. The HSU requires external cooling air to maintain the highest possible MTBF. A mounting tray with an integral fan is required. Select a mounting tray from Table 1-15. Figure 2-4 shows typical 4--MCU tray assemblies with a fan. (2) The location of the mounting tray allows the interface cabling to other units to be as short as possible. The location must give protection against rain, condensation, solvents, and hydraulic fluid. The mounting tray must be electrically bonded to the aircraft frame by a low resistance path of less than 0.1 ohm. B. High Speed Combiner Assembly (1) Mechanical installation data for the combiner is shown in Figure 2-2. C. RF Power Splitter Provisions (1) Mechanical installation data for the splitter is shown in Figure 2-3. 23--20--31 Page 2--1 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Blank Page 23--20--31 Page 2--2 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Figure 2-1 (Sheet 1). HSU Outline and Installation Diagram 23--20--31 Page 2--3/2--4 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Figure 2-1 (Sheet 2). HSU Outline and Installation Diagram 23--20--31 Page 2--5/2--6 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Figure 2-2. High Speed Combiner Outline and Installation Diagram 23--20--31 Page 2--7/2--8 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Figure 2-3. RF Power Splitter Outline Diagram 23--20--31 Page 2--9 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Figure 2-4. Typical Dimensions for 4--MCU Tray Assemblies 23--20--31 Page 2--10 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Figure 2-5. Typical Dimensions for 8--MCU Tray Assemblies 23--20--31 Page 2--11 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Blank Page 23--20--31 Page 2--12 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. ELECTRICAL INSTALLATION SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System SECTION 3 ELECTRICAL INSTALLATION 1. Overview A. General (1) This section gives electrical installation procedures, power distribution, and interconnect information for the HSU, combiner, and splitter. (2) Procedures for proper shield, power, and signal grounding are also provided in this section. In addition, procedures for the various buses are included. B. Equipment and Materials (1) See leading particulars table for a list of mating connectors required to do the electrical installation. 2. Electrical Installation Procedure A. General (1) The information necessary to provide the electrical interconnects is contained in the following paragraphs. B. Power Requirements (1) AC Power -- The aircraft ac power inverters must supply single phase 115 V ac (min 97, max 134 V ac) 400± 80 Hz sine wave with a maximum total harmonic distortion of 5%. Under all load conditions, amplitude modulation of the power supply will not exceed 2% at any frequency. (Percent modulation is defined as one--half of the peak--to--peak modulation envelope divided by the carrier amplitude and multiplied by 100.) (2) DC Power -- The aircraft dc power supply must be 28 V dc (nominal). The normal minimum and maximum voltages permitted are 20.5 and 32.2 V dc respectively. (3) Power supply to the HSU -- The voltage level of the power supplied to the HSU is important in this installation. The potential is the difference between the power pins and power ground pins at the line replaceable unit (LRU). Excessive voltage drops in the power wire(s) and power ground wire(s) cause one or more of the following conditions: • The LRU draws additional current from the aircraft supply system. • Since the LRU is drawing more current, it produces more heat and more heat causes a lower LRU MTBF. (4) The recommended maximum total combined voltage drop (voltage drop of the power wire[s] plus voltage drop of the power ground wire[s]) is 1.0 V. Voltage drop is a function of current and resistance (resistance in this case is a function of wire gauge and wire length). See Figure 3-1 for determining proper wire gauge for LRU power and power ground wires. 23--20--31 Page 3--1 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Figure 3-1. Electric Cable Chart C. Ground Requirements (1) General (a) Proper grounding is a key factor in ensuring proper system operation under normal conditions, high intensity radiated electromagnetic frequencies (HIRF), and lightning environments. You must obey this section to satisfy these requirements. NOTE: HIRF and lightning requirements dictate that the shielded wires meet the requirements of paragraph 2.C.(3). Installation of this system into aircraft manufactured prior to the FAA requirements adheres to these practices whenever feasible. (2) Chassis Grounding (a) All rack mount/remote mount units are electrically bonded to the airframe. This is done by making sure the mating surfaces between the LRU mounting tray (or LRU mounting feet if a tray is not used) provide a low impedance (< 0.1 Ω) electrical path. 23--20--31 Page 3--2 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System (b) The mating surfaces must be free of all paint and other non--conductive elements and are burnished to ensure a good bond. If the aircraft mating surface is not conductive, a bonding strap of a least 1/4--inch wide (preferably 1/2--inch wide) tin coated copper braid can be used between the LRU mounting tray (or LRU itself if a tray is not used) and the nearest airframe grounding point. (3) Shield Grounds (a) The shield wires in the HSU have the shield grounded at both ends. This is called multi--point grounding and is specified to minimize the adverse effects of HIRF and lightning. (b) The shield must not be connected to any LRU or bulkhead connector pin. (c) Examples of multi--point shield grounding methods are shown in Figure 3-2 and Figure 3-3. The shield grounding method for rack mount units is detailed in Figure 3-4. This is the preferred shield grounding method for the HSU rack mount unit. Figure 3-2. Example 1, Multi--point Shield Ground Figure 3-3. Example 2, Multi--point Shield Ground 23--20--31 Page 3--3 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Figure 3-4. Shield Grounding Example for Rack Mount Connectors (4) Power/Signal Grounds (a) All dc power grounds are tied together; all ac power grounds are tied together; all signal grounds are tied together; and all lighting grounds are tied together. DC power, ac power, signal and light ground groups are then tied together at a single point and connected to the airframe. Figure 3-5 shows this aircraft grounding method. NOTE: It is very important this grounding technique be adhered to. Do not tie the various ground wires to multiple aircraft frame points and depend on the aircraft structure to supply a low impedance path for the individual grounds. Only chassis grounds and shield grounds are grounded at multiple points in the aircraft. 23--20--31 Page 3--4 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Figure 3-5. Aircraft Grounding (b) Because signal grounds are low currents, multiple signal grounds can be connected to remote aircraft terminal blocks other than the central grounding blocks as long as these remote terminal blocks are isolated from ground. The various remote signal ground blocks must all be grounded only at the aircraft central grounding point. If 10 signal grounds are connected to a remote terminal block, a minimum of one grounding wire must be run from this terminal block to the aircraft central grounding point. 3. Electrical Installation A. HS--600 HSU (1) The HSU rear ARINC 600 connector layout is shown in Figure 3-6. The contact arrangement for the various connector plugs are given in Table 3-1, Table 3-2, and Figure 3-7. Figure 3-8 shows the connector pin layout for the DATA LOADER connector located on the front of the HSU. The system interface is shown in Figure 3-9. See Figure 3-10 for the HSU interconnect information. 23--20--31 Page 3--5 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Figure 3-6. HSU ARINC 600 Connector (P1) Pin Layout 23--20--31 Page 3--6 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table 3-1. Contact Arrangements for P1--A Top Insert, HSU ARINC 600 Connector RSVD APM POWER RSVD APM GND RSVD APM WR PROT 2# DISC SPARE A RSVD APM RSVD DISC TX INH CHASSIS GND GC 10 DISC SPARE B ASYNC RI SIG GND ASYNC DTR ASYNC RXD SIG GND ASYNC RXD ASYNC DTR SIG GND ISDNU RING RSVD SPARE LO 26 RSVD VHF AUDIO OUT HI RSVD SPARE 29 RSVD SPARE HI 7 RESVD SPARE 266 RSVD SPARE HI 5 RSVD SPARE 39 RSVD SPARE 177 RSVD SPARE HI 26 RSVD VHF AUDIO OUT LO RSVD SPARE 78 RSVD SPARE LO 7 RSVD SPARE 110 RSVD SPARE LO 5 RSVD SPARE 88 RSVD SPARE 178 10 11 12 13 14 15 RSVD APM ENABLE 1# RSVD POTS TIP RSVD SPARE D/L 18 ASYNC DCD SIG GND CHASSIS GND GC ASYNC DSR RSVD APM ENABLE 2# ASYNC TXD RSVD RSVD APM POTS OUT CLK RING ASYNC CTS 10BT RX-- ASYNC DCD RSVD SPARE D/L 17 ASYNC TXD SIG GND ISDNS/T RX-- RSVD SPARE D/L 16 10BT TX-- RSVD SPARE D/L 15 ASYNC RI ASYNC CTS SIG GND RSVD SPARE 174 HTCE TXD HTCE TXD SIG GND RSVD SPARE 175 RSVD SPARE 199 ASYNC RTS ASYNC DSR SIG GND RSVD SPARE LO 27 RSVD VHF AUDIO IN HI RSVD SPARE 19 RSVD SPARE 197 RSVD SPARE 123 RSVD SPARE 207 RSVD SPARE 40 RSVD SPARE 179 RSVD SPARE 176 ASYNC RTS SIG GND RSVD SPARE HI 27 RSVD VHF AUDIO IN LOW RSVD SPARE 68 CHASSIS GND RSVD SPARE 34 RSVD SPARE HI 14 RSVD SPARE 89 RSVD SPARE 180 RSVD APM OUT DATA ISDNS/T RX+ RSVD SPARE 258 DISC DM RST* HTCE RXD RSVD APM IN DATA 10BT RX+ RSVD SPARE 257 GND CHASSIS ISDNS/T GND GC TX+ ISDNS/T 10BT TX-TX+ MAINT 232 RXD HTCE RXD SIG GND MAINT 232 TXD RSVD SPARE 212 RSVD SPARE 103 MAINT 232 TXD SIG GND RSVD SPARE 115 RSVD SPARE HI 11 RSVD SPARE HI 13 RSVD SPARE LO 11 RSVD SPARE LO 13 RSVD SPARE 36 RSVD SPARE 161 RSVD SPARE 85 RSVD SPARE 162 RSVD SPARE HI 4 RSVD SPARE HI 9 RSVD SPARE 43 RSVD SPARE HI 8 RSVD SPARE 83 RSVD SPARE LO 14 RSVD SPARE 195 RSVD SPARE 181 RSVD SPARE 92 RSVD SPARE LO 8 RSVD SPARE 202 RSVD SPARE HI 12 RSVD SPARE 196 RSVD SPARE 182 RSVD SPARE 107 RSVD SPARE HI 6 RSVD SPARE 201 RSVD SPARE LO 12 RSVD SPARE 268 RSVD SPARE 183 RSVD SPARE 120 RSVD SPARE LO 6 RSVD SPARE 203 RSVD SPARE 105 RSVD SPARE 23 RSVD SPARE 184 RSVD SPARE HI 1 RSVD SPARE 265 RSVD SPARE 204 RSVD SPARE 118 RSVD SPARE 72 RSVD SPARE 185 23--20--31 RSVD APM WR PROT 1# RSVD SPARE 198 MAINT 232 RXD SIG GND CHASSIS GND ISDNU TIP CHASSIS GND GC RSVD VHF KEYLINE GND RSVD SPARE LO 4 RSVD SPARE LO 9 RSVD SPARE LO 1 CHASSIS GND CHASSIS GND RSVD SPARE 267 RSVD SPARE 186 CHASSIS GND Page 3--7 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table 3-2. Contact Arrangements for P1--B Top Insert, HSU ARINC 600 Connector RSVD SPARE 229 RSVD SPARE 230 RSVD SPARE 231 RSVD SPARE 232 RSVD SPARE 233 RSVD SPARE 234 RSVD SPARE 235 RSVD SPARE 236 RSVD SPARE 237 CHASSIS GND RSVD SPARE RSVD SPARE 188 RSVD SPARE 189 RSVD SPARE 190 RSVD SPARE 191 RSVD SPARE 192 RSVD SPARE 193 RSVD SPARE 194 RSVD SPARE 238 RSVD SPARE 239 RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE 248 95 242 CHASSIS RSVD GND SPARE 24 RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE LO 2 LO 18 41 CHASSIS RSVD GND SPARE 15 RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE 22 101 113 CHASSIS RSVD GND SPARE 254 RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE RSVD SPARE 187 LO 24 240 44 25 HI 19 42 HI 15 10 33 11 108 12 104 13 28 14 15 255 HI 24 241 93 74 LO 19 91 LO 15 82 121 117 27 51 256 LO 25 46 HI 3 32 27 173 37 23 12 109 HI 25 LO 3 81 76 200 86 58 56 61 122 HI 17 31 253 47 HI 16 48 10 99 LO 17 243 73 80 HI 2 96 163 97 59 50 111 LO 28 244 GND 248 HI 18 38 164 20 D/L 36 102 HI 28 245 250 87 LO 16 69 D/L 35 57 53 55 114 23--20--31 LO 29 246 251 35 206 106 D/L 30 14 13 HI 29 247 GND 252 GND 90 RSVD SPARE 64 84 208 119 D/L 29 52 63 62 54 Page 3--8 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Figure 3-7. Contact Arrangements for P1--C Bottom Insert, HSU ARINC 600 Connector Figure 3-8. HSU Data Loader Connector (J1) Pin Layout 23--20--31 Page 3--9 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Figure 3-9. RF System Interface 23--20--31 Page 3--10 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Figure 3-10. High Speed Data System Interconnect Diagram 23--20--31 Page 3--11/3--12 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. INSTALLATION CHECK SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System SECTION 4 INSTALLATION CHECK 1. Overview A. General (1) The procedures that follow are designed to check for the satisfactory installation of the HS--600 HSD system prior to LRU installation. 2. Installation Checkout A. General (1) The HSD system aircraft installation checkout should include, but is not limited to, the following steps: • Cable loss checks • Power checks • RF checks. B. Cable Loss Checks (1) HS--600 HSU to HPA Path Loss (a) Measure the total cable and connector losses between the HSU TX output (BP13) to the HPA RF input (TP1C). (b) If necessary, install an attenuator to achieve a total loss of 19--21 dB. (2) HPA to Antenna Loss (a) Measure the total loss between the HS--600 HPA RF output (MP1C) to the antenna RF port (J2). (b) Enter this value into parameter No. 5 through the HS--600 maintenance port. Do no change any other parameters. Do no forget to save the changes. (c) Assuming that this value is equal to the SDU HPA to antenna loss, enter the value through the SDU CMT using the keystrokes listed below. If the loss is more than 1 dB different from the HS--600 HPA to antenna loss, measure the loss first before entering the value. (d) From the SDU main menu, make the following selections: • F) Physical Layer Menu • C) Power Control Menu • D) Manual Power Control Menu • B) HGA HPA to Antenna Loss. (e) Enter the loss value. If greater than 5 dB, enter 5 dB. 23--20--31 Page 4--1 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System C. Power Checks (1) Check the pins listed in Table 4-1. Table 4-1. LRU Power Checks Connector Pin Signal BP1 115 V ac (High) BP7 115 V ac (Low) BP2 28 V dc (High) BP3 28 V dc (Low) BP1 115 V ac (High) BP7 115 V ac (Low) HS--600 HSU HSD System HPA (Note) NOTE: The HPA is also available as 28V dc. See Honeywell Pub. No. C15--5111--005 for installation details. D. RF Checks (1) Check the pins listed in Table 4-2. Figure 4-1 shows the receive (RX) path loss and Figure 4-2 shows the transmit (TX) path loss. These losses are achieved by a combination of RF coaxial cable losses and installed RF attenuators (the latter, if required). Table 4-2. From LRU RX Splitter RF Attenuator Combiner RF Checks Connector Pin RX IN To LRU Connector Pin DLNA J2 (RX OUT) RX OUT MCS--3000 SDU or MCS--4000 SDU or MCS--7000 SDU BP13 (RX IN) RX OUT MCS--6000 RFU TP1C (RX IN) RX OUT RF Attenuator IN OUT HS--600 HSU BP12 (RX IN) DLNA J1 (TX IN) TX IN HSD System HPA MP1C (RX OUT) TX IN SATCOM System HPA MP1C (RX OUT) RF Attenuator IN HSD System HPA TP1C (RF IN) TX OUT HS--600 HSU BP13 (TX OUT) RF Attenuator OUT 23--20--31 Page 4--2 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Figure 4-1. RX Path Loss Figure 4-2. TX Path Loss 23--20--31 Page 4--3 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Blank Page 23--20--31 Page 4--4 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. ADJUSTMENT/TEST SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System SECTION 5 ADJUSTMENT/TEST 1. Overview A. General (1) This section provides instructions for adjusting/testing the HS--600 HSD system. 2. Details A. General (1) Access to the maintenance functions is obtained by connecting a personal computer (PC) to the RS--232 maintenance port connector. The maintenance port connector is a 9--pin sub--D connector that is connected to the HSU mounting tray connector. (2) To operate with a PC, the initial settings of the maintenance port must be as follows: • Speed, normally 115,200 bps • 8 data bits • No parity • 1 stop bit • Turn caps lock ON. B. Software (1) The software can be any communications package that can send and receive ASCII at 115,200 baud rate, 8 bits with no parity bit, and 1 stop bit. Among the programs that have been used are ProComm and HyperTerminal from Windows. C. System Initialization (1) Apply power to the SATCOM and HS--600 systems. (2) Connect a cable from the PC to the front of the SDU as given in Table 5-1. The cable connector that attaches to the front of the SDU is a 53--pin male connector. The cable connector that attaches to the PC is a 9--pin female sub--D connector. Refer to Figure 5-1. Table 5-1. SDU to PC Wire List From SDU Front Connector Pin To PC Connector Pin 42 43 49 23--20--31 Page 5--1 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Figure 5-1. SDU to PC Cable (3) Connect the PC using HyperTerminal, ProComm, or equivalent. (4) Set the terminal settings to: Direct Connect to Comm 1, 9600 N 81. (5) Press ENTER to see the SDU main menu. NOTE: Refer to paragraph 1.A.(5) in section 1 for the periodic data word setup. (6) Align the inertial reference system (IRS). (7) Remove the cable from the SDU to the PC. (8) Connect a cable from the HSU to the RS--232 maintenance port as given in Table 5-2. Table 5-2. HSU to RS--232 Maintenance Port Wire List From HSU Connector Pin To RS--232 Maintenance Port 9--Pin Female D--Type Connector Pin TP6G TP6F TP6J, TP6H (9) Connect a cable from the RS--232 maintenance port to the PC as shown in Figure 5-2. The cable connector that attaches to the HSU RS--232 maintenance port is a 9--pin male sub--D connector. The cable connector that attaches to the PC is a 9--pin female sub--D connector. Figure 5-2. HSU RS--232 Maintenance Cable 23--20--31 Page 5--2 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System (10) Set up the terminal according to paragraph 2.A.(2) of this section. (11) Once the SATCOM system is logged on, then the HS--600 system will log on. (12) View the maintenance port information for a typical start--up. Refer to paragraph 2.D. of this section. (13) Once WAIT FOR CALL is indicated, the system is ready for use. D. Typical Maintenance Port Start--Up Information (1) The information given in Table 5-3 is the typical output from the HS--600 maintenance port following a power cycle. The information assumes that the IRS has aligned and the multi--channel SATCOM has logged on. Table 5-3. Typical HS--600 Maintenance Port Information * * * * * * * * * * * * * * M4--IDU BOOT HEADER * * * ** * * * * * * * (1.) Download IDU Flash (2.) Boot from Flash (default), wait . . . Please input your choice: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ............................................................................................... ............................................................................................... ............................................................................................... ............................................................................................... ............................................................................................... ................................... . . . . . . . . . . . . . . . . . . . . . . . . . . . Time Out Booting from Flash Now, please wait . . . 00.250:MNS--NS |MNS_CONFIG_RQ |ff:ff: 0#270: 00 00 00 01 00 01 08 02 08 08 00.270:NS--MNS |MNS_CONFIG_CO |ff:ff: 0#270: 02 02 53 01 00 01 08 02 08 08 00.280:SM --CC |SM_CONFIG_RQ |ff:ff:ff#264: 00 00 00 01 00 41 61 10 00 80 00.290:CC --SM |SM_CONFIG_CO |ff:ff:ff#264:Config CC OK 02 00 43 01 00 41 00.290:SM --APP|SM_CONFIG_RQ |ff:ff:ff#0: 23--20--31 Page 5--3 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table 5-3. Typical HS--600 Maintenance Port Information (cont) Glocom Multi Channel M4 Terminal IDU software start up... IDU SW Version: A1.00 04/05/2002 Initializing channel 0... copy bulletin board from flash memory ok, issue no is 23 Initializing channel 1... copy bulletin board from flash memory ok, issue no is 23 !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! Waiting for LOG ON message from HTCE!!! !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! Power Control: PH(0) = 15.0 EIRP(0) = 25.0 PM(0) = 9.5 GH(0) = 58.0 Obo(0) = 2.0 Set Economy Flag = 0 IIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIII¯ § § § Press [ENTER] to start Maintenance Setting § § § EIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIII 00.900:APP--SM |SM_CONFIG_CO |ff:ff:ff#0:Config APP OK 20), ISDN module buffer allocated= 1 40), ISDN module buffer allocated= 1 * Have found “Format B” 60), ISDN module buffer allocated= 1 80), ISDN module buffer allocated= 1 ( 100), ISDN module buffer allocated= 1 * Have found “Format B” ( 120), ISDN module buffer allocated= 1 ( 140), ISDN module buffer allocated= 1 23--20--31 Page 5--4 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table 5-3. Typical HS--600 Maintenance Port Information (cont) * Waiting for MSG_LOGON_ACK from ACSE. CHNL 0(T=14109) changed to OC--Reg 2 * Current state is LOG_ON. CHNL 0(T=14111) , got sync response from ODU,now request DSP setting... CHNL 0(T=14112) , got DSP settings , now load FPGA program... Oscillate correction= --125 (i.e. FFFFFF83)! CHNL 0 Set Tx channel to 2AB4. CHNL 0(T=14228) ,DSP load FPGA ok,now load TDM code... CHNL 0(T=14228) ,STATE CHANGE FROM 0 ------>1 CHNL 0(T=14233) ,TDM Rx stopped! CHNL 0 Set Tx channel to 2AB4. CHNL 0 : Rx is 2ab4 CHNL 0(T=14233) ,STATE CHANGE FROM 1 ------>2 CHNL 0(T=14233) ,DSP load TDM ok,now tune to NCSC... CHNL 0(T=14300) ,Got frame synchronization ... CHNL 0(T=14300) ,Bulletin Board Update Ok...Issue No 23 CHNL 0(T=14300) ,STATE CHANGE FROM 2 ------>3 CHNL 0(T=14300) ,BB Update Ok,wait for SBS finishing... CHNL 0(T=14300) ,Init/ReInit SBS!! CHNL 0(T=14300) ,SBS started!! Position: Lat=33.000000, Long=--112.003326 CHNL 0 SBS ID = 6 CHNL 0(T=14303) ,SBS finished!! CHNL 0 : Rx is 24cc CHNL 0(T=14304) ,STATE CHANGE FROM 3 ------>6 CHNL 0(T=14304) ,Start ocean region registration... CHNL 0(T=14306) ,get sync on NCRA channel, continue ORR... Chl 0 wait timer TM081 for 2630 CHNL 0(T=14569) ,TM081 timer out ! CHNL 0 MESRR Tx: 249C CHNL 0 burst backoff 16 dBm CHNL 0 PwrCtrl cmd: 29 00 A0 00 00 CHNL 0 Set Tx channel to 249C. CHNL 0 Tell DSP Tx idle channel is 2AB4. CHNL 0(T=14569) ,send orr burst CHNL 0 : Rx is 2ab4 CHNL 0(T=14780) ,STATE CHANGE FROM 6 ------>4 CHNL 0(T=14780) ,Mes is in idle ,wait for call... CHNL 0(T=14780) ,TDM Rx stopped! CHNL 0 Set Tx channel to 2AB4. CHNL 0 : Rx is 2ab4 CHNL 0(T=14780) ,STATE CHANGE FROM 4 ------>2 CHNL 0(T=14827) ,Got frame synchronization ... CHNL 0(T=14827) ,Wait for call... CHNL 0(T=14827) ,STATE CHANGE FROM 2 ------>4 ( 160), ISDN module buffer allocated= 1 ( 180), ISDN module buffer allocated= 1 * Have found “Format B” 23--20--31 Page 5--5 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System E. Maintenance Menu Items (1) The maintenance menu items given in Table 5-4 can be accessed through the maintenance port by pressing the ENTER key after the HS--600 system has booted up. (See paragraph 2.D. in this section.) NOTE: Items listed in Table 5-4 are for reference only and will be set by the manufacturer. NOTE: Changes to the parameters listed in Table 5-4 should only be accomplished by qualified personnel or after consulting your Honeywell representative. Table 5-4. Maintenance Menu Items IIIIIIIIIIIIIIII Maintenance Parameters Setting IIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIII¯ § § § 1. P(tx) Initial EIRP: 25.0dBW § § 2. Ref. oscillator correction factor: --125Hz § § 3. Transmit Doppler compensation adjustment rate: 60Hz/sec § § 4. G(M--H) ISE MTU--to--HPA output gain: 40dB § § 5. HPA output to antenna input loss: 2dB § § 6. G(Amin) Minimum usable reported antenna gain: 7dB § § 7. P(omin) Max. allowed HPA average output power: 17.0dBW § § 8. Enabled BEARE Service Interface: 0 § § 9. Min. Frame No. for TX port: 3 § § A. HPA Format Selection: N § § S. Save setting and Exit § § § EIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIII Enter your selection: 1 P(tx) Initial EIRP, range 20 to 25dBW in 0.5dBW steps: 25.0Hz Please enter new value between 20.0 to 25.0): Keep current value! Enter your selection: 2 Reference oscillator correction factor range +/--2200Hz, in 1Hz step: --125Hz Please enter new value between --2200 to 2200(+/--XXXX): Keep current value! Enter your selection: 3 Transmit Doppler compensation adjustment rate, default is 60Hz/sec. Please make your choice : 1. 30Hz/sec. 2. 60Hz/sec. Enter your choice: Use default Transmit Doppler compensation adjustment rate, 60Hz/sec. 23--20--31 Page 5--6 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table 5-4. Maintenance Menu Items (cont) Enter your selection: 4 ISE MUT--TO--HPA output gain range 36 to 42 dB, in 1 dB steps: 40Hz Please enter new value between 36 to 42: Keep current value! Enter your selection: 5 HPA output to antenna input loss, range 1--6 dB, in 1dB steps: 2Hz Please enter new value between 1 to 6: Keep current value! Enter your selection: 6 Minimum usable reported antenna gain below which the ISE ceases operation of the HSD channel range 7 to 12 dB, in 1dB steps: 7Hz Please enter new value between 7 to 12: Keep current value! Enter your selection: 7 Maximum allowed HPA average output power, range 20 to 60W, or 13 to 18 dBW, in 0.5dB steps: 17.0Hz Please enter new value between 13.0 to 18.0): Keep current value! Enter your selection: 8 Enabled Bearer Service Interface, 0 for ISDN S/T and 1 for PCM: 0Hz Please enter new value between 0 to 1: Keep current value! Enter your selection: 9 Min. frame number for ack TX port: 3Hz Please enter new value between 2 to 12: Keep current value! Enter your selection: A (NOTE: Must be Upper Case) “A” or “B” for different HPA types: N Please enter your new character (A--B): Keep current value! 23--20--31 Page 5--7 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table 5-4. Maintenance Menu Items (cont) Enter your selection: S (NOTE: Must be Upper Case) Maintenance Parameters have been saved. The new maintenance parameters will be used by system. Please wait for system setup... NOTE: Must power cycle HS--600 for parameter save to take effect. * * * * * * * * * * * * * * * * Main Menu * * * * * * * * * * * * * * * * * * * 1.Protocol Mode 2.Manual Mode 3.Change Password Enter your selection: 1 NOTE: Press or power cycle to exit from this menu. * * * * * * * * * * * * * * * * * * Menu in protocol mode * * * * * * * * * * * * * * * * * * * * * * * * * * 1.Event Log ESC. Exit Enter your selection: * * * * * * * * * * * * * * * * * * Menu in protocol mode * * * * * * * * * * * * * * * * * * * * * * * * * * 1.Event Log ESC. Exit Enter your selection: 1 * * * * * * * * * * * * * * * * * Event Log Menu * * * * * * * * * * * * * * * * * * * * * 1.Display last 20 Event Log records 2.Display specified range of Event Log records 3.Display all Event Log records V.Verify a specified Event Log Record in Hex format C.Clear all Event Log records ESC. Exit Enter your selection: * * * * * * * * * * * * * * * * * * Menu in protocol mode * * * * * * * * * * * * * * * * * * * * * * * * * * 1.Event Log ESC. Exit Enter your selection: 23--20--31 Page 5--8 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. FAULT ISOLATION SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System SECTION 6 FAULT ISOLATION 1. Overview A. General (1) To be supplied. 23--20--31 Page 6--1 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Blank Page 23--20--31 Page 6--2 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. MAINTENANCE PRACTICES SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System SECTION 7 MAINTENANCE PRACTICES 1. Overview A. General (1) This section provides instructions for removing, reinstalling, and adjusting the HS--600 HSU, combiner, and/or splitter that has been previously installed by the aircraft manufacturer or completion center. Adjustment information is called out as required. CAUTION: SHOULD ANY INSTALLATION CRITICAL CASES ARISE WITH THE REINSTALLATION OF ANY UNIT, YOU MUST COMPLY 100 PERCENT WITH THE INSTRUCTION. CAUTION: TO PREVENT DAMAGE TO EQUIPMENT, TURN AIRCRAFT POWER OFF WHEN REMOVING OR INSTALLING LRUS. B. Equipment and Materials (1) No additional special equipment or materials, other than those commonly used in the shop, are required to install the units in existing trays and clamps, and adjust the system. Do not over tighten mounting screws. Where torque values are not given, it is acceptable to finger tighten the mounting screws. 2. Procedure for the HS--600 HSU A. Removal and Reinstallation Procedures (1) Remove the HSU. (a) Remove power from the HSU and the interfacing subsystems (such as SATCOM. Circuit breakers for the systems are typically located on the flight deck. (b) Loosen the mounting tray holddown clamps by rotating in a counterclockwise direction. (c) Slowly pull forward on the unit handle to separate the unit and tray connectors and slide the unit out of the tray, lifting slightly to clear the holddown clamps. (d) Place electrostatic protective covers on the HSU rear connector to protect the pins from damage. (e) Place the HSU in a protective static--resistant bag and protective carrying case. 23--20--31 Page 7--1 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System (2) Reinstall the HSU. (a) Remove the HSU from the protective carrying case and protective static--resistant bag. (b) Remove the electrostatic protective covers from the HSU rear connector. (c) Slide the unit into the mounting tray. CAUTION: WHEN PLACING THE UNIT ON THE MOUNTING TRAY, DO NOT FORCE FIT. IF MATING IS DIFFICULT, REMOVE THE UNIT AND CHECK FOR CONNECTOR PINS THAT CAN BE BENT OR OUT OF ALIGNMENT. ALSO VISUALLY CHECK THE ALIGNMENT OF THE RECEPTACLE ON THE MOUNTING TRAY. (d) Gently slide the unit backwards until its connectors are fully engaged with the mating connectors of the mounting tray. (e) Put the holddown clamps in place and tighten the knobs in a clockwise direction until the proper torque is applied (clutch engages). (f) Reapply power to the HSU and its interfacing equipment. NOTE: Upon applying primary power, the HSU will automatically power up and start a POST. B. Adjustment Procedures (1) Not applicable. C. Repair Procedures (1) Not applicable. D. Return to Service Procedures (1) Refer to test procedures in the INSTALLATION CHECK section of this manual. 3. Procedure for the Combiner/Splitter A. Removal and Reinstallation Procedures (1) Remove the combiner. (a) Remove power from the HSU. Circuit breakers for the HSU are typically located on the flight deck. (b) Locate the combiner. (c) Disconnect the aircraft connectors from the combiner and place protective covers on the connectors. (d) Remove the six screws holding the combiner in position. 23--20--31 Page 7--2 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System (2) Reinstall the combiner. (a) Attach the combiner using six screws. (b) Remove the protective covers from the connectors and install the aircraft connectors on the combiner. (c) Reapply power to the HSU and its interfacing equipment. (3) Remove the splitter. (a) Remove power from the HSU. Circuit breakers for the HSU are typically located on the flight deck. (b) Locate the splitter. (c) Disconnect the aircraft connectors from the splitter and place protective covers on the connectors. (d) Remove the two screws holding the splitter in position. (4) Reinstall the splitter. (a) Attach the splitter using two screws. (b) Remove the protective covers from the connectors and install the aircraft connectors on the splitter. (c) Reapply power to the HSU and its interfacing equipment. B. Adjustment Procedures (1) Not applicable. C. Repair Procedures (1) Not applicable. D. Return to Service Procedures (1) Refer to test procedures in the INSTALLATION CHECK section of this manual. 23--20--31 Page 7--3 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System 4. Instructions for Continued Airworthiness, Code of Federal Regulation CFR 91.213 A. General (1) Maintenance requirements and instructions for continued airworthiness of the HS--600 HSU components are contained in the following paragraphs: (2) Installation of the HSU on an aircraft by Supplemental Type Certificate or Form 337 obligates the aircraft operator to include the maintenance information provided by this manual in the operator’s Aircraft Maintenance Manual and the operator’s Aircraft Scheduled Maintenance Program. B. Instructions (1) Maintenance information for the HSU (system description, removal, installation, testing, etc.) is contained in this manual. (2) LRU part numbers and other necessary part numbers contained in this manual should be placed into the aircraft operator’s appropriate aircraft Illustrated Parts Catalog (IPC). (3) Wiring diagram information contained in this manual should be placed into the aircraft operator’s appropriate aircraft Wiring Diagram Manuals. (4) The high speed data system components are considered on--condition units and no additional maintenance is required other than a check for security and operation at normal inspection intervals. (5) If a system component is inoperative, remove unit, secure cables and wiring, collar applicable switches and circuit breakers, and placard them inoperative. Revise equipment list and weight and balance as applicable prior to flight and make a log book entry that unit was removed. Refer to section 91.213 of the CFR or the aircraft’s minimum equipment list (MEL). (6) The HSU components can be repaired only at a factory authorized repair center or an appropriately rated FAA Part 145 repair station. (7) Once repaired, reinstall the LRU in the aircraft in accordance with the original Form 337 approved data or instructions in this manual. Do a return--to--service test of the system and approve it for return to service with a log book entry required by section 43.9 of the FAR. (8) Scheduled Maintenance Program tasks to be added to the aircraft operator’s appropriate aircraft maintenance program are as follows: (a) Recommended Periodic Scheduled Servicing Tasks: None Required (b) Recommended Periodic Inspections: None Required (c) Recommended Periodic Scheduled Preventative Maintenance Tests (Tests to determine system condition and/or latent failures): None Required 23--20--31 Page 7--4 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. APPENDIX A SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System APPENDIX A M4 CALL CAUSE CODE LIST 1. Overview A. General (1) The following list of cause codes in Table A--1 describes the various conditions of a failed M4 terminal call. Table A--1. Cause Code Call Cause Code List Description Note 0001 Invalid LES code entry. 0003 Selected land earth station (LES) does not support M4 services. 0004 Invalid dialing sequence detected. 0005 Out of memory capacity. 0101 Cannot obtain the network coordination station assignment (NCSA) channel from the Bulletin Board. 0102 Cannot obtain the land earth station assignment (LESA) channel from the Bulletin Board. 0103 Failed to stop the time division multiplex (TDM) receive command before tuning to the NCSA/LESA channel. 0104 Failed to synchronize to the NCSA/LESA channel frequency. 0105 User cleared call before the single channel per circuit (SCPC) channel was assigned. 0106 Failed to receive the channel assignment. 0107 85H code (instead of channel assignment) received. 0108 DSP failed to reset after call clear. 0109 DSP failed to reset before loading the Mini M/high speed data (MM/HSD) service code. 0110 DSP failed to load the M1/M4 service code. 0111 Incorrect channel received from the channel assignment SU (86h). 0120 Erroneous frame number detected on 81H SU. Response SU (82H) not sent. 0121 Erroneous slot number detected on 81H. Response SU (82H) not sent. 0122 Failed to obtain the MESRP channel from the Bulletin Board. 0123 DSP did not report after response SU before it transmitted. 1001 Normal Clearing. 1. Mobile Earth Station (MES) is clearing the call as instructed by the relevant MES terminal equipment (i.e., normal clearing due to MES terminal “on--hook” etc.). 1011 MES Busy. 1. MES is rejecting the call because the specified MES terminal number is currently busy, and MES has not been authorized to divert calls which are addressed to that number. 23--20--31 Page A--1 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table A--1. Call Cause Code List (cont) Cause Code Description Note 1012 MES is clearing the fixed--originated call because subsequent to the acceptance of the call and signaling of the identity of the mobile terminal to which the call will actually be routed, that terminal has become busy and therefore cannot be rung. 1. 1021 Call Failed, MES Time--out, No Answer 1. MES is clearing the call because appropriate “off--hook” signaling has not been received from the addressed MES terminal (including any authorized diversions) within the allowed time limit. 1081 Call Failed, MES Terminal # Not Installed 1. MES is rejecting the call because the specified MES terminal number has not been installed, and MES has not been authorized to divert calls which are addressed to that number. 1091 Call Failed, MES Terminal # out of Service 1. MES is rejecting the call because the specified MES terminal number is currently out of service, and MES has not been authorized to divert calls which are addressed to that number. 1092 MES is clearing the fixed--originated call because subsequent to the acceptance of the call and the signaling of the identity of the mobile terminal to which the call will actually be routed, that terminal has become out--of--service and therefore cannot be rung. 1. 1141 Call Cleared, pre--empted at MES 1. MES clear: pre--emption for higher priority call. 1142 Call Refused due to Distress Call from MES 1. MES clear: (Fixed) MES has initiated a distress call. 1143 Call Cleared, pre--empted at MES 1. Fixed--originated call cleared by MES due to SATCOM reporting that it is no longer logged on. 1144 Attempted Call pre--empted by MES Distress 1. MES clear: (mobile) MES has initiated a distress call. 1145 Call Cleared, pre--empted by MES 1. Mobile--originated call cleared by MES due to SATCOM reporting that it is no longer logged on. 1146 Attempted Call Abandoned by MES Terminal 1. MES is prematurely clearing the mobile--originated call which is in the process of being established because the MES user has abandoned the call (by placing, the originating terminal “on--hook). 11A0 LES is clearing the call because the credit card being used is not valid (at this LES) for calls to the country indicated in the “Service Address’ information received from the MES. 1. 11D1 Call Failed, Request Data Invalid 1. LES is rejecting the call because the “Service Nature” and/or “Service Type” and/or “Channel parameter” information received from the MES is invalid (e.g., not currently defined in the SDM, mutually contradictory, or not applicable to a MES--originated call.) 23--20--31 Page A--2 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table A--1. Call Cause Code List (cont) Cause Code 11D2 Description Note Call Failed, Insufficient Digits in Service Address 1. LES is clearing the call because the “Service Address” information received from the MES is invalid (e.g., less than 2 digits). If the customer is dialing a valid phone number or prefix code, verify that the MES has a corresponding Inmarsat mobile number (IMN)s in the LES access control and signalling equipment (ACSE) database. 11D3 Call Failed, Invalid Service Address 1. LES is clearing the call because the “Service Address” information received from the MES is a 2--digit address which is either undefined or which is currently unavailable at this LES. 11D4 LES is clearing the call because the “credit card data” information received from the MES is invalid. (This does not imply that the credit card itself is invalid.) 1. 11D5 LES is clearing the call because the “Service Address” information received from the MES contains a country code which is regarded (by this LES) as invalid. 1. 11D6 LES is clearing the call because the “PID” information received from the MES in the “scrambling vector” message (type 8D) is not consistent with the personal identification number (PID) information in the fixed/MES--originated (PID) and PID/MES Registration Tables at the LES as it relates to this call. 1. 11D7 LES is failing the call because the service requested by the MES in the distress, urgency or safety access request is not 4.8 kbps AMBE telephony. 1. 11D8 LES is clearing the call because the service address received from the MES requesting distress, urgency or safety priority is not a two or three--digit code. 1. 11E0 LES is clearing the call because the credit card PIN received from the MES is not considered (at this LES) to be valid. 1. 11E1 LES is clearing the call because it has been determined that an excessive number of consecutive call attempts with invalid credit card have been made. 1. 1201 MES ack: received a simplex call. 1. 1202 (Spot Beam Handover): MES is ready to make the transition from the current beam to the next beam. 1. 1261 MES ack: received a simplex call (unstable). 1. 1262 Call Cleared, MES Timeout Distress Test 1. MES clear: distress test call has not been cleared in 120s. 1281 Call Failed, MES Cannot Accept 1. MES is rejecting the call because the MES is not equipped to provide the specified service. 1291 Call Failed, MES Cannot Accept at Present 1. MES is rejecting the call because although it is equipped to provide the specified service, it is not currently able to do so. 12B1 Call Cleared by MES for Unspecified Reason 1. MES is rejecting or clearing the call for a reason which is not covered by any of the currently defined “Cause” events. 23--20--31 Page A--3 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table A--1. Call Cause Code List (cont) Cause Code 12C1 Description Note Call Faded, No Scrambling Vector Ack 1. MES clear: Scrambling Vector Ack (95) not received by the MES. 12C2 MES is clearing the call because a “Credit Card Valid” message (type A7) has not been received by the MES within the allowed time limit. 1. 12C3 Call Failed, MES Timeout, No Terrestrial Answer 1. MES is clearing the call because an “LES Connect” message (type 8C) has not been received by the MES within the allowed time limit. 12C4 MES is clearing the call because the “authentication query” ISU message (type B4) and/or the 1., 2., “authentication query” SSU message (type B5) have not been received by the MES within the 13., 14., allowed time limit. 15. 12C5 MES is clearing the call because an expected supplementary services SU(s) has (have) not been received by the MES within the allowed time limit. 12C6 MES is clearing the call because the “supplementary services interrogation” ISU (type B2H), 1. and/or ”subscriber digits” SSU (type AD H) messages have not been received by the MES within the allowed time limit. 12C7 MES is clearing the call because a “SCPC channel release” SU (type 8AH) has not been received by the MES, in response to the transmission of a “notification acknowledge” message (type BAH) during the supplementary services call diversion information retrieval process, within the allowed time limit. 12C8 (Spot Beam Handover): MES is clearing the call session in the next beam because the MES 1. did not detect the LESH carrier on the new frequency. 12D1 Call Failed, Spot Beam Data Invalid 1. 1. 1. LES is rejecting the call because the “spot beam ID” information received from the MES is invalid, i.e., ID is not allocated on the satellite in use. 12D2 Call Failed, Invalid Scrambling Vector (LES is clearing the call because the “Scrambling Vector” information received from the the MES is invalid; i.e., 0000 H, 6959 H or 7 FFF H). 1. 1351 MES is clearing the call because the MES currently has insufficient free memory in which to store the short message. 1. 1361 Call Cleared by MES; Cable Unwrap 1. MES is clearing the call because the above--decks equipment is about to “cable unwrap”. 1362 Call Cleared, Long Interruption Reception 1., 3. MES is clearing the call because a long--term interruption (16 sec) in reception of LES carrier has occurred. The definition of a “long--term interruption” depends upon the service type. 1363 Call Cleared, MES Antenna Repointed (WS clear: switching ocean regions) 1. A secondary functional center of Multi--channel MES is clearing the call because the primary functional center has commanded the above--decks equipment to repoint to a different ocean region. 23--20--31 Page A--4 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table A--1. Cause Code Call Cause Code List (cont) Description Note 1391 Aero Class MES only: MES is clearing the call because the call has lasted more than 700 km in linear travelled distance. 1. 1392 Aeronautical Class MES only: MES is clearing the call because it has moved out of spot beam coverage. 1. 1393 Aeronautical Class MES only: MES in “cooperative mode” is clearing the call because of a preemption request from the master entity. Call cleared by MES due to reported antenna gain falling below the antenna gain threshold setting (Maintenance parameter #6) for more than 10 seconds. 1. 1393 Call cleared by the MES due to the reported antenna gain falling below the antenna gain threshold setting (maintenance parameter #6). 1. 1451 Call Failed, Terrestrial Circuits Congested 1. LES is rejecting the call because an appropriate terrestrial circuit is not currently available at this specific LES. 1452 Call Failed, LES Congested 1. LES is rejecting the call because an appropriate channel unit and associated terrestrial circuit are currently not available at this LES. 1502 (Spot Beam Handover): LES is ready to make the transition from the current beam to the next beam and is clearing the call session in the current beam (normal clear). 1. 1541 Call Cleared, pre--empted at LES. (LES clear: pre--empted by higher priority call.) 1. 1551 Call Failed, LES Congested, No Channel 1. LES is rejecting the call because an appropriate satellite channel is not currently available at this specific LES. 1552 LES reject: appropriate time division multiplex (TDM)/time division multiple access (TDMA) time slot not available. 1. 1581 Call Failed, Service Not Provided at this LES 1. LES is rejecting the call because the requested service is not provided by this specific LES. 1591 LES is rejecting the call because the requested service is temporarily not available at this specific LES. 1. 1592 LES is clearing the call because the specified credit card type is not currently supported by this specific LES. 1. 15A1 LES is rejecting the call because the specified MES is not authorized for any service (except Distress) at this specific LES. For a COMSAT LES, the phone is technically barred. For other LESs, the phone is either financially or technically barred. 1., 4. If the customer’s ISP or AA are authorized through this LES, verify that the MES ID has corresponding IMNs in the LES ACSE database. If the call setup proceeds to the point where the ACSE passes the call to the switch, check to see 1) if the area code is invalid, 2) if a valid area code is missing in the switch, 3)check to see if the ACSE passes the correct ICD message including the IMN (not all 9’s) to the switch. 15A2 LES is rejecting the call because the specified MES is not authorized to use specific requested service via this specific LES. 23--20--31 1. Page A--5 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table A--1. Cause Code Call Cause Code List (cont) Description Note 15A3 LES is clearing the call because the “credit card data” information received from the MES has been rejected by the credit card authorization process. 1. 15A4 LES is clearing the call because the data received from the MES in the “Authentication Reply” message (type B6) has been declared “invalid” by the LES authentication process. 1., 5. 15A5 LES is rejecting the call because the specified PID is not authorized for any service at this specific LES. 1. 15A6 LES is rejecting the call because the specified PID is not authorized to use specific requested service via this specific LES. (User not authorized/barred for service in the LES database.) 1. 15A7 LES is clearing the call because the service address received from the MES is not authorized for the requested priority. 1. 15B1 Call Cleared by LES for Unspecified Reasons 1. LES is rejecting or clearing the call for a reason which is not covered by any of the currently defined “Cause” events. 15C1 Call Failed, LES Timeout, No Assignment 1. LES is rejecting the call because an appropriate “Channel Assignment” message has not been received from the NCS by the LES within the allowed time limit. 15C2 LES is clearing the call because the “Service Address” information has not been received by the LES from MES within the allowed time limit. 1. 15C3 Call Failed, LES Timeout, No Scrambling Vector 1. LES is clearing the call because a “Scrambling Vector” message (type 8D) has not been received by the LES from the MES within the allowed time limit. 15C4 Call Failed, No Service Address or Vector 1. LES is clearing the call because neither the “Service Address” information nor a “Scrambling Vector” message (type 8D) has been received by the LES from the MES within the allowed time limit. 15C5 LES is clearing the call because the complete “credit card data” information has not been received by the LES within the allowed time limit. 1. 15C6 Call Failed, LES Timeout, No Return Carrier ID 1. LES is clearing the call because the Return Carrier Identifier (8B) was not received. 15C7 LES is clearing the call because an “MES Connect” message (type 99) has not been received by the LES within the allowed time limit. 1. 15C8 LES clear: SES Answer back not received. 1. 15C9 LES is clearing the call because an “Authentication Reply” message (type B6) has not been received by the LES within the allowed frame limit. 1., 6. 15CA LES is clearing the call because a “notification acknowledge” message (type BAH) has not 1. been received by the LES within the allowed time limit. 15CB LES is clearing the call because the request sequence number contained in the received 1. “notification acknowledge” message (type BA) is not valid (i.e. either not ‘0’ or not the next value in the sequence). 23--20--31 Page A--6 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table A--1. Call Cause Code List (cont) Cause Code Description Note 15CC Aeronautical Class MES only: (Spot Beam Handover): LES is terminating the procedure because it did not receive a response to the Handover Request from the NCS. 1. 15CD (Spot Beam Handover): LES is clearing the call session in the next beam because the MES did not indicate that it was ready to make the transition (possibly because the MES did not receive the Channel Assignment). 1. 15D1 LES is rejecting the call because the “Channel Assignment” message received from the NCS contains inappropriate or conflicting information. 1. 15D2 LES is clearing this MES ID and channel number in the busy lists at LES and NCS because a new call to/from this MES is being set--up (and thus any previous call to/from this MES cleared). 1. 15E1 Call Cleared, MES still Transmitting Fault 1. LES is attempting to clear an MES which has sent an SCPC channel release message but is found still to be transmitting 5.12 sec later. 1651 Call Failed, LES Congested, No Channel Unit 1. LES is rejecting the call because an appropriate channel unit is not currently available at this specific LES. 1661 Call Failed, Long Interruption in Reception 1. LES is clearing the call because of an interruption in reception of the MES carrier exceeding the allowed time limit of 62 seconds. 16C1 LES clear: SEST carrier not received. 1. 16C2 LES is clearing the call because an appropriate SCPC MES carrier has not been received by the LES (at the commencement of the call) within the allowed time limit. 1. 16C3 (Spot Beam Handover): LES is clearing the call session in the next beam because the LES did 1. not detect the MESH carrier on the new frequency 1790 LES is clearing the call because of a malfunction in the credit card validity checking database or in the communications links. 1. 1791 LES is clearing the call because of a malfunction in the authentication checking database or in the communication links. 1. 1811 NCS is rejecting the call because the specified MES ID is in the “S busy” list at the NCS. 1. 1812 NCS is rejecting the call because the specified MES is busy with an IPDS call at the NCS. 1. 1841 NCS is pre--empting the call in order to free the MES for an incoming call with priority 1. 1. 1842 NCS is pre--empting the call in order to free the MES for an incoming call with priority 2. 1. 1843 NCS is pre--empting the call in order to free the MES for an incoming call with priority 3. 1. 1844 NCS is pre--empting the call in order to assign the channel to another call with higher priority. 1. 1851 NCS is rejecting the call because an appropriate SCPC channel is not currently available. 1852 NCS is rejecting the call because no SCPC channel exists at the NCS which matches the 1., 9., contents of the Channel Parameters, Service Nature, Service Type, MES Category, Spot Beam 10., 11., 12. ID and Priority fields contained in the Request for Channel Assignment. 23--20--31 1., 7., 8. Page A--7 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table A--1. Cause Code 1853 Call Cause Code List (cont) Description Note NCS is rejecting the call because no SCPC channel is currently available for the specified 1. leasemarked MES. Contact the NCS to verify that the MES has frequencies in a lease pool available or request that the MES ID be removed from the leasemark pool. 1854 NCS is rejecting the call because the MES is outside the spot beam coverage area. 1855 NCS is rejecting the call because an appropriate SCPC channel is not currently available and 1. channel pre--emption failed. 1856 NCS is rejecting the call because the requested spot beam indicates failed spot beam selection 1. (“FF” ) and an appropriate global SCPC channel is not currently available. 1857 (Spot Beam Handover) NCS is rejecting the Handover Request because an appropriate SCPC 1. channel is not available in the next beam. 18A1 NCS is rejecting the call because the specified MES ID was not found in the “Forward and Return MES ID” cross--reference table. 18A2 NCS is rejecting the call because the specified MES is not authorized for any service (except 1. for Distress calls) at the NCS. 18A3 NCS is rejecting the call because the specified LES is not authorized for the requested service 1. at the NCS. 18A4 Reserved. 1. 18B1 NCS is rejecting or clearing the call for a reason which is not covered by any of the currently defined “Cause” events. 1. 18B2 NCS is rejecting the call because the requested service variant is invalid. 1. 18C1 NCS is rejecting the call because no message was received from the specified MES (in reaction to a Call Announcement message) within the allowed time limit. 1. 18C2 Reserved for B. 1. 18C3 NCS is rejecting the call because the specified MES was busy and the MES pre--emption failed 1. ( i.e. no response within the allowed time limit). 18D1 NCS is rejecting the call because the Request for Call Announcement or Request for Channel 1. Assignment contains invalid or inappropriate information. 18E1 NCS is rejecting the call because the specified MES ID is in the “MES busy” list at the NCS, and is listed as being busy with a call through the same LES that is now requesting a “call announcement” addressed to that MES. 1. 18E2 NCS is rejecting the call because the specified MES is busy with an IPDS call through the same LES which is requesting the call announcement. 1. 1C61 LES clear: LES to MSSC call set--up failure. 1. 1F01 LES is clearing the call because of the receipt of “on--hook” signaling from the relevant terrestrial circuit (i.e., normal clearing). 1. 1F11 LES is clearing the call because the terrestrial called party is engaged (busy). 1. 23--20--31 1. 1. Page A--8 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Table A--1. Call Cause Code List (cont) Cause Code 1F21 Description Note Call Failed, LES Timeout, No Answer 1. LES is clearing the call because appropriate “off--hook” signaling from the terrestrial called party has not been received by the LES within the allowed time limit. 1F61 Call Failed, Terrestrial Circuit Failure 1. LES is clearing the call because of the detection of a failure in the relevant terrestrial circuit. 1F62 Call Failed, Early Clear Terrestrial Circuit 1. LES is clearing the call before the “MES Connect”. NOTES: 1. These cause codes are defined by the Inmarsat System Definition Manual (SDM). 2. The user probably attempted to place a call too soon after logging in or too soon after the last call attempt. The user must wait at least 20 seconds before making a mobile--originated call. Ask the customer to be patient and try again. 3. If this cause code occurs during call setup, there could be a problem with a particular LES channel unit. The channel unit may need to be reset. This cause code may also occur after the call has been connected. This problem may also occur during an NCS outage. 4. Check which ISP or AA commissioned the phone or smart card. 5. Verify that the customer’s smart card information (including the Ki) is entered in the ACE database at the LES. For fixed--16--mobile calls through non--COMSAT LESs. Please dial the terminal IMN instead of the smart card IMN. 6. Verify that the customer’s smart card information (including Ki) is entered in the ACE database at the LES. 7. Verify that the appropriate NCS is operational. NCS channels for a particular spot beam could be blocked or unavailable. 8. Frequencies/channels at the NCS for a particular spot beam and for a specific service could be blocked or unavailable/not assigned or congested. 9. Verify that the LES is enabled for the particular service at the NCS 10. Verify that the MES/LES is lease--marked if appropriate 11. Verify that the Aero--HSD/F MES is using the new generation of signaling units 12. Verify that the MES is enabled for the particular service at the NCS; e.g., MPDS. 13. The antenna was not pointed correctly or is blocked. 14. The antenna cable is defective. 15. The M4 LES Channel Unit needs to be reset from the front panel. 23--20--31 Page A--9 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System Blank Page 23--20--31 Page A--10 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. APPENDIX B SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System APPENDIX B INMARSAT REGISTRATION FORM 1. Overview A. General (1) This appendix provides an example of the Inmarsat registration form required to activate the HSD system. 23--20--31 Page B--1 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System 23--20--31 Page B--2 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System 23--20--31 Page B--3 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System 23--20--31 Page B--4 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System 23--20--31 Page B--5 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System 23--20--31 Page B--6 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System 23--20--31 Page B--7 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System 23--20--31 Page B--8 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System 23--20--31 Page B--9 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document. SYSTEM DESCRIPTION AND INSTALLATION MANUAL HS--600 High Speed Data System 23--20--31 Page B--10 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.
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