Honeywell HS-600 Inmarsat Aircraft Telecommunications Systems User Manual Manual

Honeywell International Inc. Inmarsat Aircraft Telecommunications Systems Manual

Manual

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 theexport administration regulations. Diversion contrary to U.S. law is prohibited.HoneywellAerospace Electronic SystemsCES--PhoenixP.O. Box 21111Phoenix, Arizona 85036-1111U.S.A.Printed in U.S.A. Pub. No. A15--5111--00623--20--31Title Page T--130 May 2002System Description and InstallationManualHS--600High Speed Data System
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data SystemPROPRIETARY NOTICEThis document and the information disclosed herein are proprietary data of Honeywell. Neitherthis document nor the information contained herein shall be used, reproduced, or disclosed toothers without the written authorization of Honeywell, except to the extent required forinstallation or maintenance of the recipient’s equipment.NOTICE -- FREEDOM OF INFORMATION ACT (5 USC 552) ANDDISCLOSURE OF CONFIDENTIAL INFORMATION GENERALLY (18 USC 1905)This document is being furnished in confidence by Honeywell. The information disclosedherein fall within exemption (b) (4) of 5 USC 552 and the prohibitions of 18 USC 1905.S2002Honeywell is a U.S. registered trademark of Honeywell. All other marks are owned by their respective companies.Copyright 2002 HoneywellAll Rights Reserved23--20--31Title Page T--230 May 2002
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DO NOT STAPLEDO NOT STAPLEBUSINESS REPLY MAILFIRST CLASS PERMIT NO. 3532, PHOENIX, AZFOLDFOLDPOSTAGE WILL BE PAID BY ADDRESSEEHoneywellAerospace Electronic SystemsCES--PhoenixP.O. Box 21111Phoenix, Arizona 85036-1111U.S.A.ATTN: Technical PublicationsQuality AdministratorNO POSTAGENECESSARYIF MAILEDIN THEUNITED STATES
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page RR--1RECORD OF REVISIONSFor each revision, put the revised pages in your manual and discard the superseded pages. Writethe revision number and date, date put in manual, and the incorporator’s initials in the applicablecolumns on the Record of Revisions. The initial H shows Honeywell is the incorporator.RevisionNumberRevisionDateDate PutIn Manual ByRevisionNumberRevisionDateDate PutIn Manual By
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SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page RTR--1RECORD OF TEMPORARY REVISIONSInstructions 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 temporaryrevision, put the applicable data in the record columns on this page.TemporaryRevisionNumberTemporaryRevisionDateTemporaryRevisionStatusDate Putin Manual By *DateRemovedfrom Manual By ** The initial H in this column shows Honeywell has done this task.
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SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page SBL--1SERVICE BULLETIN LISTService BulletinIdentifiedModDate Includedin this Manual Description
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page SBL--2Blank Page
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page LEP--1LIST OF EFFECTIVE PAGESSubheading and Page Date Subheading and Page DateTitleT--1 30 May 2002T--2 30 May 2002Record of RevisionsRR--1 30 May 2002RR--2 30 May 2002Record of Temporary RevisionsRTR--1 30 May 2002RTR--2 30 May 2002Service Bulletin ListSBL--1 30 May 2002SBL--2 30 May 2002List of Effective PagesLEP--1 30 May 2002LEP--2 30 May 2002Table of ContentsTC--1 30 May 2002TC--2 30 May 2002TC--3 30 May 2002TC--4 30 May 2002TC--5 30 May 2002TC--6 30 May 2002IntroductionINTRO--1 30 May 2002INTRO--2 30 May 2002INTRO--3 30 May 2002INTRO--4 30 May 2002System Description and Operation1--1 30 May 20021--2 30 May 20021--3 30 May 20021--4 30 May 20021--5 30 May 20021--6 30 May 20021--7 30 May 20021--8 30 May 20021--9 30 May 20021--10 30 May 20021--11 30 May 20021--12 30 May 20021--13 30 May 20021--14 30 May 2002Mechanical Installation2--1 30 May 20022--2 30 May 2002F2--3/2--4 30 May 2002F2--5/2--6 30 May 2002F2--7/2--8 30 May 20022--9 30 May 20022--10 30 May 20022--11 30 May 20022--12 30 May 2002Electrical Installation3--1 30 May 20023--2 30 May 20023--3 30 May 20023--4 30 May 20023--5 30 May 20023--6 30 May 20023--7 30 May 20023--8 30 May 20023--9 30 May 20023--10 30 May 2002F3--11/3--12 30 May 2002Hindicates a changed or added page.F indicates a foldout page.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page LEP--2Subheading and Page Date Subheading and Page DateInstallation Check4--1 30 May 20024--2 30 May 20024--3 30 May 20024--4 30 May 2002Adjustment/test5--1 30 May 20025--2 30 May 20025--3 30 May 20025--4 30 May 20025--5 30 May 20025--6 30 May 20025--7 30 May 20025--8 30 May 2002Fault Isolation6--1 30 May 20026--2 30 May 2002Maintenance Practices7--1 30 May 20027--2 30 May 20027--3 30 May 20027--4 30 May 2002M4 Call Cause Code ListA--1 30 May 2002A--2 30 May 2002A--3 30 May 2002A--4 30 May 2002A--5 30 May 2002A--6 30 May 2002A--7 30 May 2002A--8 30 May 2002A--9 30 May 2002A--10 30 May 2002Inmarsat Registration FormB--1 30 May 2002B--2 30 May 2002B--3 30 May 2002B--4 30 May 2002B--5 30 May 2002B--6 30 May 2002B--7 30 May 2002B--8 30 May 2002B--9 30 May 2002B--10 30 May 2002Hindicates a changed or added page.F indicates a foldout page.
CONTENTS
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page TC--1TABLE OF CONTENTSSubject PageINTRODUCTION 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................................................2. Content Data INTRO--2..........................................................A. How to Use This Manual INTRO--2............................................B. Weights and Measurements INTRO--3.........................................C. Acronyms and Abbreviations INTRO--3.........................................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...................................................2. System Components 1--6...................................................A. General 1--6...........................................................3. 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............................................2. Mechanical Installation Design 2--1...........................................A. HS--600 HSU Provisions 2--1............................................
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page TC--2B. 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............................................2. 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..........................................3. Electrical Installation 3--5....................................................A. HS--600 HSU 3--5......................................................INSTALLATION CHECK 4--1....................................................1. Overview 4--1..............................................................A. General 4--1...........................................................2. 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...........................................................2. Details 5--1................................................................A. General 5--1...........................................................B. Software 5--1..........................................................C. System Initialization 5--1................................................
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page TC--3D. 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............................................2. 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........................................3. 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........................................4. Instructions for Continued Airworthiness, Code of Federal RegulationCFR 91.213 7--4...........................................................A. General 7--4...........................................................B. Instructions 7--4........................................................APPENDIX AM4 CALL CAUSE CODE LIST A--1...............................................1. Overview A--1..............................................................A. General A--1...........................................................APPENDIX BINMARSAT REGISTRATION FORM B--1..........................................1. Overview B--1..............................................................A. General B--1...........................................................
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page TC--4List of IllustrationsFigure PageFigure 1-1. High Speed Data System Block Diagram 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............................
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page TC--5List of TablesTable 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.......................................
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page TC--6Blank Page
INTRODUCTION
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page INTRO--1INTRODUCTION1. Proprietary, Export, and Precautionary DataA. Proprietary Notice(1) This document and the information disclosed herein are proprietary data ofHoneywell. 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’sequipment. FREEDOM OF INFORMATION ACT (5 USC 552) AND DISCLOSUREOF CONFIDENTIAL INFORMATION GENERALLY (18 USC 1905).(2) This document is being furnished in confidence by Honeywell. The informationdisclosed herein falls within exemption (b) (4) of 5 USC 552 and the prohibitions of 18USC 1905. Copyright 2002 Honeywell. All Rights Reserved.(3) Honeywell is a U.S. registered trademark of Honeywell. All other marks are owned bytheir respective companies.B. Export Notice(1) This document contains unrestricted technical data and is being exported underlicense exception TSU/OTS in accordance with EAR Section 740.13(a).(2) These commodities, technology, or software were exported from the United States inaccordance with the export administration regulations. Diversion contrary to U.S. lawis prohibited. ECCN: 7E994 Schedule B#4901.99.0050C. 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 notobeyed, can cause injury or death.•A CAUTION is an operation or maintenance procedure or condition that, if notobeyed, can cause damage to the equipment.•A NOTE gives data to make the work easier or gives directions to go to aprocedure.(2) All personnel who operate equipment and do maintenance specified in this manualmust know and obey the safety precautions. The warnings and cautions that followapply to all parts of this manual.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page INTRO--2WARNING: BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’MATERIAL SAFETY DATA SHEETS FOR SAFETY INFORMATION. SOMEMATERIALS CAN BE DANGEROUS.CAUTION: DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TOMATERIALS SPECIFIED BY HONEYWELL. MATERIALS THAT ARE NOTEQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CANVOID THE WARRANTY.CAUTION: THE HS--600 HIGH SPEED DATA SYSTEM CONTAINS ITEMS THAT AREELECTROSTATIC DISCHARGE SENSITIVE (ESDS). IF YOU DO NOTOBEY THE NECESSARY CONTROLS, A FAILURE ORUNSATISFACTORY OPERATION OF THE UNIT CAN OCCUR FROMELECTROSTATIC DISCHARGE. USE APPROVED INDUSTRYPRECAUTIONS TO KEEP THE RISK OF DAMAGE TO A MINIMUM WHENYOU TOUCH, REMOVE, OR INSERT PARTS OR ASSEMBLIES.2. Content DataA. How to Use This Manual(1) This manual gives general system description and installation information for theHS--600 High Speed Data System. It also gives block diagram and interconnectinformation to permit a general understanding of the system interface.(2) The purpose of this manual is to help you install, operate, maintain, and troubleshootthe HS--600 High Speed Data System. Common system maintenance proceduresare not presented in this manual. The best established shop and flight line practicesshould be used.(3) Related publications that are referred to in this manual are identified in Table Intro--1.Table Intro--1. Related PublicationsPublication Publication No.Handling, Storage, and Shipping Procedures for Honeywell AvionicsEquipment Instruction ManualA09--1100--001MCS--3000/6000 Multi--Channel Satellite Communications SystemDescription, Installation, and Maintenance ManualC15-- 5111 -- 005MCS--4000/7000 Multi--Channel SATCOM System Description,Installation, and Maintenance ManualA15-- 5111 -- 001NOTES:1. You can order a Honeywell publication from Honeywell as follows:Telephone No.: (602) 436--6900Fax No.: (602) 436--1588E--mail: cas--publications--distribution@honeywell.com
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page INTRO--3B. 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 inANSI/IEEE Std 260.C. Acronyms and Abbreviations(1) The acronyms and abbreviations that follow help the reader identify terms anddefinitions used by Honeywell.(2) The letter symbols for units of measurement are the same as shown inANSI/IEEE Std 260.Term DefinitionACSE access control and signalling equipmentACU antenna control unitBSU beam steering unitCCA circuit card assemblyCMT commissioning and maintenance terminalCNS/ATM communication, navigation, and surveillance/air traffic managementDLNA diplexer/low noise amplifierDLT data logging terminalESD electrostatic dischargeESDS electrostatic discharge sensitiveHGA high gain antennaHIRF high intensity radiated electromagnetic frequenciesHPA high power amplifierHSD high speed dataHSU high speed data unitICAO International Civil Aviation Organization: Agency of the UNIPC Illustrated Parts CatalogIPDS Inmarsat Packet Mode Data ServiceIRS inertial reference systemISDN Integrated Services Digital NetworkLES land earth stationLESA land earth station assignmentLRU line replaceable unit
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page INTRO--4Term DefinitionM4 multi--media mini--MMCS multi--channel SATCOMMCU modular concept unitMEL minimum equipment listMES Mobile Earth StationMM/HSD Mini M/high speed dataMTBF mean--time--between--failuresNCSA network coordination station assignmentPC personal computerPID personal identification numberPSTN Public Switched Telephone NetworkRF radio frequencyRFU radio frequency unitSATCOM satellite communicationsSCPC single channel per circuitSDM System Definition ManualSDU satellite data unitSU signal unitTDM time division multiplexTDMA time division multiple access3. Customer AssistanceA. WhotoContact(1) For assistance with installation, operation, or maintenance of the HS--600 HighSpeed Data System, contact your local Honeywell Dealer or regional HoneywellCustomer Support Engineer. Additional assistance can be obtained from:•HoneywellAviation Services, Customer Response Center (CRC)Commercial Electronic Systems21111 N. 19th AvenuePhoenix, AZ 85027TEL: (877) 436--2005 (Toll--Free)FAX: (602) 436--1501
SYSTEMS DESCRIPTIONAND OPERATION
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 1--1SECTION 1SYSTEM DESCRIPTION AND OPERATION1. OverviewA. General(1) The HS--600 high speed data system provides multi--channel Inmarsat Aero cockpitand passenger voice, fax, and data, and multi--media mini--M (M4) circuit--modeservices simultaneously. Figure 1-1 shows a block diagram of the high speed data(HSD) system.Figure 1-1. High Speed Data System Block Diagram
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 1--2(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 isinterfaced 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 satellitedata unit (SDU)/radio frequency unit (RFU) 40 W HPA is combined with a high powercombiner. The output of the high power combiner drives a common diplexer/low noiseamplifier (DLNA) and a nominal 12 dB gain antenna. The SDU manages the satelliteselection and steers the HGA.(4) The Aero--H/H+ SDU and HPA requires no hardware or operational softwaremodifications, and operates without knowledge of the HSD system presence.However, each SDU used in conjunction with the HSD system will require advanceconfiguration 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 inTable 1-1, at a rate of approximately 1 Hz, for the functions in Table 1-1 to beperformed in the HSD system (SDU to HSU transmit only).Table 1-1. SDU DLT RS--232 Port ConfigurationData FunctionSatellite Selected Satellite selectionPosition (Latitude/Longitude) Spot beam selectionSatellite--Relative Velocity Open--loop Doppler compensationCurrent Antenna Gain Antenna gain variation compensationLog--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) arerequired to configure the SDU to broadcast the desired data from its DLT port.Table 1-2. SDU CMT KeystrokesKeystroke DescriptionHBA To logging menu00020509 <cr> Enter logging wordB1 <cr> Set logging periodC60 <cr> Set heading record frequencyE1 <cr> Select DLT port for outputD1 <cr> Enable logging
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 1--3(7) The DLT configuration settings remain in effect indefinitely, unless subsequentlymanually changed or a factory settings restart is performed. If the SDU in conjunctionwith the HSD system is replaced for any reason, the replacement SDU will require itsDLT port to be configured appropriately.(8) The HSD system controls its HPA through the HPA’s commissioning andmaintenance 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’sbackoff state.B. Aero--H/H+(1) Aero--H/H+ is a multi--channel aeronautical system that can operate in both theInmarsat--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 servicepossible as given in Table 1-3.Table1-3. TypeofServiceAeroType AntennaGlobalBeamSpotBeamVoice9.6kbpsVoice4.8kbpsSecureVoice 4.8kbpsFax(max)PC Data(max)PacketModeData(max)Aero--H High gain Yes No Yes No Yes 4.8 kbps 2.4 kbps 10.5 kbpsAero--H+ High gain Yes Yes Yes Yes Yes 4.8/2.4kbps2.4 kbps 10.5 kbps(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. AllHoneywell/Thales aeronautical equipment complies with the International CivilAviation Organization (ICAO) Agency of the UN requirements for aeronautical safetyservices. The equipment can be used for communication, navigation, andsurveillance/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 earthstations (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. Asdevelopments of the Mini--M, they do not comply with the ICAO requirements foraeronautical safety services and cannot be used for CNS/ATM. In other words, theycan only be used for non--safety service data communications.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 1--4D. System Performance(1) Currently, the numbers of simultaneous aeronautical voice and M4 data channels canonly be obtained from theoretical calculations. Using the assumptions given inTable 1-4, the calculations are given in Table 1-5. The calculations for the totalnumber of calls are given in Table 1-6 thru Table 1-9.Table 1-4. AssumptionsItem dB WattsGain cell 12 dBR/T power (10.5 Kbps assumed) 20.4 dBW 109.6 WR/T power (600 bps assumed) 5.9 dBW 3.9 WHPA power (same assumed for both) 16.0 dBW 40.0 WCable Loss 4.7 dBInitial HSD channel power 22.5 dBW 177.8 WSettled HSD channel power 22.5 dBW 177.8 WInitial 8400 C channel EIRP 14.5 dBW 28.2 WSettled 8400 C channel EIRP 7.5 dBW 5.6 WInitial 21000 C channel EIRP 19.5 dBW 89.1 WSettled 21000 C channel EIRP 13.5 dBW 22.4 WTable 1-5. CalculationsHGA Gain dBW Total WattsAfter R/T 600 bps(Watts)AfterR/T10.5Kbps(Watts)12 23.3 214.8 210.9 105.2Table 1-6. Total Number of Calls with Aero--H+ (Spot beam operation) and 10.5 KbpsPacket Data RateM4 HSD Channels 8400 Voice Channels 21000 Voice Channels15/6 (Note) 0121NOTE: MCS 6000 = 5, MCS 7000 = 6
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 1--5Table 1-7. Total Number of Calls with Aero--H+ (Spot beam operation) and 600 bps PacketData RateM4 HSD Channels 8400 Voice Channels 21000 Voice Channels15/6 (Note) 1105NOTE: MCS 6000 = 5, MCS 7000 = 6Table 1-8. Total Number of Calls with Aero--H+ (Global beam operation) and 10.5 KbpsPacket Data RateM4 HSD Channels 8400 Voice Channels 21000 Voice Channels1 0 1/2Table 1-9. Total Number of Calls with Aero--H+ (Global beam operation) and 600 bpsPacket Data RateM4 HSD Channels 8400 Voice Channels 21000 Voice Channels105(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 powercombiner with the HS--600 installation. It is essential that a 12 dB antenna isused to be able to support more than one Aero voice channel as well as asimultaneous Aero M4 HSD.E. FCC Compliance(1) This device complies with part 15 of the FCC rules. Operation is subject to thefollowing two conditions:•This device may not cause harmful interference.•This device must accept any interference received, including interference that maycause undesired operation.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 1--62. System ComponentsA. General(1) Table 1-10 gives the component part numbers supplied by Honeywell. Table 1-11gives components that are necessary, but are not supplied by Honeywell.Table 1-10. Components Supplied by HoneywellComponent Model No. Honeywell Part No.High Speed Data Unit HS--600 7519300--901High Speed Combiner Assembly -- 7519340--901RF Power Splitter -- 7519349--1High 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 beused with the HS--600 system.Table 1-11. Components/Parts Not Supplied by HoneywellComponent/Part CommentsHSU 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 1--73. Component DescriptionsA. HS--600 High Speed Data Unit (HSU)(1) The HSU is designed to perform reliably under field conditions and provide ease ofmaintenance when required. The HSU has a modular design to permit easyreplacement of each circuit card assembly (CCA). All CCAs are built to standards thatqualify them for both airline and business aircraft usage.(2) The HSU is packaged as a 4 modular concept unit (4--MCU). The mechanical chassisis constructed of aluminum alloy sheet metal. The HSU requires external cooling airin accordance with ARINC 600 or ARINC 404 to maintain the highest possiblemean--time--between--failures (MTBF). In installations where this is not available, amounting tray with an integral fan is required. Refer to Table 1-15. The HSU is shownin Figure 1-2.(3) Table 1-12 gives the leading particulars for the HSU and Table 1-13 gives theDO--160D categories that this equipment meets or exceeds.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 1--8Figure 1-2. HS--600 HSU
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 1--9Table 1-12. HS--600 Leading ParticularsCharacteristic SpecificationDimensions (maximum):•Length ................................•Width .................................•Height ................................7.64 in. (194.06 mm)4.90 in. (124.46 mm)15.26 in. (387.60 mm)Weight (maximum) ....................... 11.84lb(5.37kg)Power requirements (AC) (Note):•Nominal ............................... 115 V rms, 400 Hz•Maximum ............................. 134 V rms, 480 Hz•Minimum .............................. 97 V rms, 320 HzPower requirements (DC) Note):•Nominal ............................... 27.5 V dc•Maximum ............................. 32.2 V dc•Minimum .............................. 20.5 V dcPowerConsumption ...................... 25 W nominal, 40 W maximumCooling Requirements .................... Select tray from Table 1-15Connector P1 (Rear) ...................... Radiall Part No. 620--600--237Mating Connector (P1) .................... Radiall Part No. 620--600--238•22AWGContacts ...................... Radiall Part No. 620--200•20AWGContacts ...................... Radiall Part No. 620--310•16AWGContacts ...................... Radiall Part No. 620--330•12AWGContacts ...................... Radiall Part No. 620--340•Size5CoaxContacts ................... Radiall Part No. 620--021Mounting ................................ Tray, ARINC 600 4--MCU SizeCircuit Breaker Ratings:•115VacCircuitBreaker ................ 2 Amp typical•28VdcCircuitBreaker ................. 7.5 Amp typicalUserInterface(ISDNS/T) ................. ITU--T 1.430 (S/T interface)DSS1/EuroISDNEnvironmental ........................... Unit must be installed inside pressurized bulkhead (cabin).
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 1--10Table 1-13. DO--160D Environmental CategoriesDescription CategoryTemperature and Altitude XXIn--Flight Loss of Cooling XTemperature Variation XHumidity XShock BVibration SB2Explosion Proofness XWaterproofness XFluids Susceptibility XSand and Dust XFungus Resistance XSalt Spray XMagnetic Effect XPower Input XVoltage Spike XAudio Frequency Susceptibility XInduced Signal Susceptibility XRadio Frequency (RF) Susceptibility XXXEmission of RF Energy MLightning Indirect Effects XXXXLightning Direct Effects XIcing XElectrostatic Discharge (ESD) X
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 1--11(4) Table 1-14 gives a description of the HSU front panel lights during various HSUconditions. The PUSH TO TEST switch on the front panel of the HSU is notoperational.Table 1-14. HSU Front Panel Light DescriptionCondition DescriptionPower 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 30seconds 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 onthis time division multiplex (TDM) channel, the green PASS light flashes.The light flashes for each correctly received signal unit (SU). This shouldoccur within 2 minutes of power up, if the SDU is logged on, or within 30seconds 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 timegoes on; it could even stop flashing with the light on or off. However, duringan HSD call, SUs are received at a high rate, so the green PASS light willflash rapidly, appearing to be almost steady on.Failure The FAIL light will be on if any error occurs.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 1--12B. High Speed Combiner Assembly(1) The high speed combiner assembly combines the signals from both HPAs which arethen sent to the DLNA. Figure 1-3 shows the high speed combiner assembly.Figure 1-3. High Speed Combiner Assembly
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 1--13C. RF Power Splitter(1) The RF power splitter divides the signal from the DLNA which is then sent to the SDUand HSU. The unit weight is 2.5 oz. (70.87 grams). Figure 1-4 shows the RF powersplitter.Figure 1-4. RF Power SplitterD. HSU Mounting Tray(1) The HS--600 HSU ARINC 600 connector, contacts, and mounting trays can bepurchased from ECS or EMTEQ. The addresses for ECS and EMTEQ are as follows:Electronic Cable Specialists5300 W. Franklin DriveFranklin, WI 53132U.S.A.Telephone: (414) 421--5300Fax: (414) 421--5301EMTEQS84 W. 18693 Enterprise DriveMuskego, WI 53150U.S.A.Telephone: (262) 679--6170 / 1--888--679--6170
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 1--14(2) Table 1-15 gives a list of HSU mounting trays available through ECS. ContactEMTEQ for a list of HSU mounting trays available.Table 1-15. HSU Mounting TraysECS Part No. Description Voltage6050--101 4 MCU S/S tray with bottom fan 115 V ac6049--101 4 MCU S/S tray with right side fan 115 V ac6049--102 4 MCU S/S tray with left side fan 115 V ac6083--102 4MCUS/Ltraywithrearfan 115 V ac6050--102 4 MCU S/S tray with bottom fan 28 V dc200--89891--101 4 MCU S/S tray with left side fan 28 V dc200--89892--101 4 MCU S/S tray with right side fan 28 V dc6083--103 4MCUS/Ltraywithrearfan 28 V dc6292--101 8 MCU S/S standard tray 115 V ac6288--101 8MCUS/Strayw/bottomfan 115 V ac6290--101 8 MCU S/S tray w/left side fan 115 V ac6284--101 8 MCU S/S tray w/right side fan 115 V ac6286--101 8 MCU S/L standard tray 115 V ac
MECHANICAL INSTALLATION
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 2--1SECTION 2MECHANICAL INSTALLATION1. OverviewA. 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 dimensionsand 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 theapplicable outline and installation diagram in this section for additional mountinginformation.2. Mechanical Installation DesignA. HS--600 HSU Provisions(1) Mechanical installation data for the HS--600 HSU is shown in Figure 2-1. The HSU ismounted in an ARINC 600 4--MCU mounting tray. The HSU requires external coolingair to maintain the highest possible MTBF. A mounting tray with an integral fan isrequired. Select a mounting tray from Table 1-15. Figure 2-4 shows typical 4--MCUtray assemblies with a fan.(2) The location of the mounting tray allows the interface cabling to other units to be asshort as possible. The location must give protection against rain, condensation,solvents, and hydraulic fluid. The mounting tray must be electrically bonded to theaircraft 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 2--2Blank Page
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 2--3/2--4Figure 2-1 (Sheet 1). HSU Outline and Installation Diagram
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 2--5/2--6Figure 2-1 (Sheet 2). HSU Outline and Installation Diagram
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 2--7/2--8Figure 2-2. High Speed Combiner Outline and Installation Diagram
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 2--9Figure 2-3. RF Power Splitter Outline Diagram
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 2--10Figure 2-4. Typical Dimensions for 4--MCU Tray Assemblies
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 2--11Figure 2-5. Typical Dimensions for 8--MCU Tray Assemblies
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 2--12Blank Page
ELECTRICALINSTALLATION
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 3--1SECTION 3ELECTRICAL INSTALLATION1. OverviewA. General(1) This section gives electrical installation procedures, power distribution, andinterconnect information for the HSU, combiner, and splitter.(2) Procedures for proper shield, power, and signal grounding are also provided in thissection. 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 theelectrical installation.2. Electrical Installation ProcedureA. General(1) The information necessary to provide the electrical interconnects is contained in thefollowing 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 harmonicdistortion of 5%. Under all load conditions, amplitude modulation of the power supplywill not exceed 2% at any frequency. (Percent modulation is defined as one--half ofthe peak--to--peak modulation envelope divided by the carrier amplitude andmultiplied by 100.)(2) DC Power -- The aircraft dc power supply must be 28 V dc (nominal). The normalminimum 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 isimportant in this installation. The potential is the difference between the power pinsand power ground pins at the line replaceable unit (LRU). Excessive voltage drops inthe power wire(s) and power ground wire(s) cause one or more of the followingconditions:•The LRU draws additional current from the aircraft supply system.•Since the LRU is drawing more current, it produces more heat and more heatcauses a lower LRU MTBF.(4) The recommended maximum total combined voltage drop (voltage drop of the powerwire[s] plus voltage drop of the power ground wire[s]) is 1.0 V. Voltage drop is afunction of current and resistance (resistance in this case is a function of wire gaugeand wire length). See Figure 3-1 for determining proper wire gauge for LRU powerand power ground wires.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 3--2Figure 3-1. Electric Cable ChartC. Ground Requirements(1) General(a) Proper grounding is a key factor in ensuring proper system operation undernormal conditions, high intensity radiated electromagnetic frequencies (HIRF),and lightning environments. You must obey this section to satisfy theserequirements.NOTE: HIRF and lightning requirements dictate that the shielded wires meetthe requirements of paragraph 2.C.(3). Installation of this system intoaircraft manufactured prior to the FAA requirements adheres to thesepractices whenever feasible.(2) Chassis Grounding(a) All rack mount/remote mount units are electrically bonded to the airframe. This isdone by making sure the mating surfaces between the LRU mounting tray (orLRU mounting feet if a tray is not used) provide a low impedance (< 0.1 Ω)electrical path.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 3--3(b) The mating surfaces must be free of all paint and other non--conductiveelements and are burnished to ensure a good bond. If the aircraft mating surfaceis not conductive, a bonding strap of a least 1/4--inch wide (preferably 1/2--inchwide) tin coated copper braid can be used between the LRU mounting tray (orLRU 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 iscalled multi--point grounding and is specified to minimize the adverse effects ofHIRF 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 andFigure 3-3. The shield grounding method for rack mount units is detailed inFigure 3-4. This is the preferred shield grounding method for the HSU rackmount unit.Figure 3-2. Example 1, Multi--point Shield GroundFigure 3-3. Example 2, Multi--point Shield Ground
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 3--4Figure 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; allsignal grounds are tied together; and all lighting grounds are tied together. DCpower, ac power, signal and light ground groups are then tied together at a singlepoint and connected to the airframe. Figure 3-5 shows this aircraft groundingmethod.NOTE: It is very important this grounding technique be adhered to. Do not tiethe various ground wires to multiple aircraft frame points and depend onthe aircraft structure to supply a low impedance path for the individualgrounds. Only chassis grounds and shield grounds are grounded atmultiple points in the aircraft.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 3--5Figure 3-5. Aircraft Grounding(b) Because signal grounds are low currents, multiple signal grounds can beconnected to remote aircraft terminal blocks other than the central groundingblocks as long as these remote terminal blocks are isolated from ground. Thevarious remote signal ground blocks must all be grounded only at the aircraftcentral grounding point. If 10 signal grounds are connected to a remote terminalblock, a minimum of one grounding wire must be run from this terminal block tothe aircraft central grounding point.3. Electrical InstallationA. HS--600 HSU(1) The HSU rear ARINC 600 connector layout is shown in Figure 3-6. The contactarrangement for the various connector plugs are given in Table 3-1, Table 3-2, andFigure 3-7. Figure 3-8 shows the connector pin layout for the DATA LOADERconnector located on the front of the HSU. The system interface is shown inFigure 3-9. See Figure 3-10 for the HSU interconnect information.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 3--6Figure 3-6. HSU ARINC 600 Connector (P1) Pin Layout
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 3--7Table 3-1. Contact Arrangements for P1--A Top Insert, HSU ARINC 600 ConnectorA B C D E F G H J K1RSVDAPMPOWERRSVDAPMGNDRSVDAPMENABLE1#RSVDAPMENABLE2#RSVDAPMOUT CLKRSVDPOTSRINGASYNCCTSRSVDAPMOUTDATARSVDAPM INDATARSVDAPM WRPROT 1#2RSVDAPM WRPROT 2#RSVDAPMRSVDRSVDPOTSTIPASYNCTXD10BTRX--ASYNCDCDASYNCCTS SIGGNDISDNS/TRX+10BTRX+RSVDSPARE257 GND3DISCSPARE ADISC TXINHRSVDSPARED/L 18RSVDSPARED/L 17RSVDSPARED/L 16RSVDSPARED/L 15RSVDSPARE174RSVDSPARE258CHASSISGND GC2ISDNS/TTX+4CHASSISGND GC10ASYNCRI SIGGNDASYNCDCD SIGGNDASYNCTXD SIGGND10BTTX--ASYNCRIHTCETXDDISC DMRST*ISDNS/TTX--10BTTX+5DISCSPARE BASYNCDTRCHASSISGND GC3ISDNS/TRX--HTCETXD SIGGNDASYNCRTSHTCERXD SIGGNDHTCERXDRSVDSPARE198ISDNUTIP6ASYNCRXD SIGGNDASYNCDTR SIGGNDASYNCDSRRSVDSPARE176RSVDSPARE175MAINT232 RXDMAINT232 TXDMAINT232 TXDSIG GNDMAINT232 RXDSIG GNDCHASSISGND GC17ASYNCRXDISDNURINGASYNCDSR SIGGNDASYNCRTS SIGGNDRSVDSPARE199RSVDSPARE212RSVDSPARE103RSVDSPARE115CHASSISGNDRSVDVHFKEYLINEGND8RSVDSPARELO 26RSVDSPAREHI 26RSVDSPARELO 27RSVDSPAREHI 27RSVDSPAREHI 11RSVDSPARELO 11RSVDSPARE36RSVDSPARE85RSVDSPAREHI 4RSVDSPARELO 49RSVDVHFAUDIOOUT HIRSVDVHFAUDIOOUT LORSVDVHFAUDIOIN HIRSVDVHFAUDIOIN LOWRSVDSPAREHI 13RSVDSPARELO 13RSVDSPARE161RSVDSPARE162RSVDSPAREHI 9RSVDSPARELO 910 RSVDSPARE29RSVDSPARE78RSVDSPARE19RSVDSPARE68RSVDSPARE43RSVDSPARE92RSVDSPARE107RSVDSPARE120RSVDSPAREHI 1RSVDSPARELO 111 RSVDSPAREHI 7RSVDSPARELO 7RSVDSPARE197CHASSISGNDRSVDSPAREHI 8RSVDSPARELO 8RSVDSPAREHI 6RSVDSPARELO 6RSVDSPARE265CHASSISGND12 RESVDSPARE266RSVDSPARE110RSVDSPARE123RSVDSPARE34RSVDSPARE83RSVDSPARE202RSVDSPARE201RSVDSPARE203RSVDSPARE204CHASSISGND13 RSVDSPAREHI 5RSVDSPARELO 5RSVDSPARE207RSVDSPAREHI 14RSVDSPARELO 14RSVDSPAREHI 12RSVDSPARELO 12RSVDSPARE105RSVDSPARE118RSVDSPARE26714 RSVDSPARE39RSVDSPARE88RSVDSPARE40RSVDSPARE89RSVDSPARE195RSVDSPARE196RSVDSPARE268RSVDSPARE23RSVDSPARE72RSVDSPARE18615 RSVDSPARE177RSVDSPARE178RSVDSPARE179RSVDSPARE180RSVDSPARE181RSVDSPARE182RSVDSPARE183RSVDSPARE184RSVDSPARE185CHASSISGND
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 3--8Table 3-2.Contact Arrangements for P1--B Top Insert, HSU ARINC 600 ConnectorA B C D E F G H J K1RSVDSPARE229RSVDSPARE230RSVDSPARE231RSVDSPARE232RSVDSPARE233RSVDSPARE234RSVDSPARE235RSVDSPARE236RSVDSPARE237CHASSISGND2RSVDSPARE187RSVDSPARE188RSVDSPARE189RSVDSPARE190RSVDSPARE191RSVDSPARE192RSVDSPARE193RSVDSPARE194RSVDSPARE238RSVDSPARE2393RSVDSPARELO 24RSVDSPAREHI 24RSVDSPARELO 25RSVDSPAREHI 25RSVDSPAREHI 17RSVDSPARELO 17RSVDSPARELO 28RSVDSPAREHI 28RSVDSPARELO 29RSVDSPAREHI 294RSVDSPARE240RSVDSPARE241RSVDSPARE46RSVDSPARE95RSVDSPARE242RSVDSPARE243RSVDSPARE244 GNDRSVDSPARE245RSVDSPARE246RSVDSPARE247 GND5RSVDSPARE44RSVDSPARE93RSVDSPARE248CHASSISGND RSVDSPARE24RSVDSPARE73RSVDSPARE248RSVDSPARE250RSVDSPARE251RSVDSPARE252 GND6RSVDSPARE25RSVDSPARE74RSVDSPAREHI 3RSVDSPARELO 3RSVDSPARE31RSVDSPARE80RSVDSPAREHI 18RSVDSPARELO 18RSVDSPARE41RSVDSPARE907RSVDSPAREHI 19RSVDSPARELO 19RSVDSPARE32RSVDSPARE81RSVDSPARE253RSVDSPAREHI 2RSVDSPARELO 2CHASSISGND RSVDSPARE15RSVDSPARE648RSVDSPARE42RSVDSPARE91RSVDSPARE27RSVDSPARE76RSVDSPARE47RSVDSPARE96RSVDSPARE38RSVDSPARE87RSVDSPARE35RSVDSPARE849RSVDSPAREHI 15RSVDSPARELO 15RSVDSPARE173RSVDSPARE200RSVDSPAREHI 16RSVDSPARE163RSVDSPARE164RSVDSPARELO 16RSVDSPARE206RSVDSPARE20810 RSVDSPARE33RSVDSPARE82RSVDSPARE37RSVDSPARE86RSVDSPARE48RSVDSPARE97RSVDSPARE20RSVDSPARE69RSVDSPARE106RSVDSPARE11911 RSVDSPARE108RSVDSPARE121RSVDSPARE9RSVDSPARE58RSVDSPARE10RSVDSPARE59RSVDSPARED/L 36RSVDSPARED/L 35RSVDSPARED/L 30RSVDSPARED/L 2912 RSVDSPARE104RSVDSPARE117RSVDSPARE7RSVDSPARE56RSVDSPARE101RSVDSPARE113RSVDSPARE8RSVDSPARE57RSVDSPARE3RSVDSPARE5213 RSVDSPARE28RSVDSPARE27RSVDSPARE23RSVDSPARE22CHASSISGND RSVDSPARE254RSVDSPARE4RSVDSPARE53RSVDSPARE14RSVDSPARE6314 RSVDSPARE2RSVDSPARE51RSVDSPARE12RSVDSPARE61RSVDSPARE1RSVDSPARE50RSVDSPARE6RSVDSPARE55RSVDSPARE13RSVDSPARE6215 RSVDSPARE255RSVDSPARE256RSVDSPARE109RSVDSPARE122RSVDSPARE99RSVDSPARE111RSVDSPARE102RSVDSPARE114RSVDSPARE5RSVDSPARE54
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 3--9Figure 3-7. Contact Arrangements for P1--C Bottom Insert, HSU ARINC 600 ConnectorFigure 3-8. HSU Data Loader Connector (J1) Pin Layout
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 3--10Figure 3-9. RF System Interface
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 3--11/3--12Figure 3-10. High Speed Data System Interconnect Diagram
INSTALLATION CHECK
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 4--1SECTION 4INSTALLATION CHECK1. OverviewA. General(1) The procedures that follow are designed to check for the satisfactory installation ofthe HS--600 HSD system prior to LRU installation.2. Installation CheckoutA. General(1) The HSD system aircraft installation checkout should include, but is not limited to, thefollowing 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 theantenna RF port (J2).(b) Enter this value into parameter No. 5 through the HS--600 maintenance port. Dono 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 thevalue through the SDU CMT using the keystrokes listed below. If the loss is morethan 1 dB different from the HS--600 HPA to antenna loss, measure the loss firstbefore 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 4--2C. Power Checks(1) Check the pins listed in Table 4-1.Table 4-1. Power ChecksLRU Connector Pin SignalHS--600 HSU BP1 115 V ac (High)BP7 115 V ac (Low)BP2 28 V dc (High)BP3 28 V dc (Low)HSD System HPA (Note) BP1 115 V ac (High)BP7 115 V ac (Low)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 andFigure 4-2 shows the transmit (TX) path loss. These losses are achieved by acombination of RF coaxial cable losses and installed RF attenuators (the latter, ifrequired).Table 4-2. RF ChecksFrom LRU Connector Pin To LRU Connector PinRX Splitter RX IN DLNA J2 (RX OUT)RX OUT MCS--3000 SDU orMCS--4000 SDU orMCS--7000 SDUBP13 (RX IN)RX OUT MCS--6000 RFU TP1C (RX IN)RX OUT RF Attenuator INRF Attenuator OUT HS--600 HSU BP12 (RX IN)Combiner TX OUT DLNA J1 (TX IN)TX IN HSD System HPA MP1C (RX OUT)TX IN SATCOM System HPA MP1C (RX OUT)HS--600 HSU BP13 (TX OUT) RF Attenuator INRF Attenuator OUT HSD System HPA TP1C (RF IN)
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 4--3Figure 4-1. RX Path LossFigure 4-2. TX Path Loss
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 4--4Blank Page
ADJUSTMENT/TEST
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 5--1SECTION 5ADJUSTMENT/TEST1. OverviewA. General(1) This section provides instructions for adjusting/testing the HS--600 HSD system.2. DetailsA. 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 isa 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•1stopbit•Turn caps lock ON.B. Software(1) The software can be any communications package that can send and receive ASCIIat 115,200 baud rate, 8 bits with no parity bit, and 1 stop bit. Among the programsthat 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 cableconnector that attaches to the front of the SDU is a 53--pin male connector. The cableconnector that attaches to the PC is a 9--pin female sub--D connector. Refer toFigure 5-1.Table 5-1. SDU to PC Wire ListFrom SDU Front Connector Pin To PC Connector Pin42 343 249 5
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 5--2Figure 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 inTable 5-2.Table 5-2. HSU to RS--232 Maintenance Port Wire ListFrom HSU Connector PinTo RS--232 Maintenance Port 9--Pin FemaleD--Type Connector PinTP6G 3TP6F 2TP6J, TP6H 5(9) Connect a cable from the RS--232 maintenance port to the PC as shown inFigure 5-2. The cable connector that attaches to the HSU RS--232 maintenance portis a 9--pin male sub--D connector. The cable connector that attaches to the PC is a9--pin female sub--D connector.Figure 5-2. HSU RS--232 Maintenance Cable
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 5--3(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 maintenanceport following a power cycle. The information assumes that the IRS has aligned andthe multi--channel SATCOM has logged on.Table 5-3. Typical HS--600 Maintenance Port Information************** M4--IDUBOOTHEADER ************(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 0800.270:NS--MNS |MNS_CONFIG_CO |ff:ff: 0#270: 02 02 53 01 00 01 08 02 08 0800.280:SM --CC |SM_CONFIG_RQ |ff:ff:ff#264: 00 00 00 01 00 41 61 10 00 8000.290:CC --SM |SM_CONFIG_CO |ff:ff:ff#264:Config CC OK 02 00 43 01 00 4100.290:SM --APP|SM_CONFIG_RQ |ff:ff:ff#0:
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 5--4Table 5-3. Typical HS--600 Maintenance Port Information (cont)Glocom Multi Channel M4 Terminal IDU software start up...IDU SW Version: A1.00 04/05/2002Initializing channel 0...copy bulletin board from flash memory ok, issue no is 23Initializing channel 1...copy bulletin board from flash memory ok, issue no is 23!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!Waiting for LOG ON message from HTCE!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!Power Control: PH(0) = 15.0EIRP(0) = 25.0PM(0) = 9.5GH(0) = 58.0Obo(0) = 2.0Set 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
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 5--5Table 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 ------>1CHNL 0(T=14233) ,TDM Rx stopped!CHNL 0 Set Tx channel to 2AB4.CHNL 0 : Rx is 2ab4CHNL 0(T=14233) ,STATE CHANGE FROM 1 ------>2CHNL 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 23CHNL 0(T=14300) ,STATE CHANGE FROM 2 ------>3CHNL 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=--112.003326CHNL 0 SBS ID = 6CHNL 0(T=14303) ,SBS finished!!CHNL 0 : Rx is 24ccCHNL 0(T=14304) ,STATE CHANGE FROM 3 ------>6CHNL 0(T=14304) ,Start ocean region registration...CHNL 0(T=14306) ,get sync on NCRA channel, continue ORR...Chl 0 wait timer TM081 for 2630CHNL 0(T=14569) ,TM081 timer out !CHNL 0 MESRR Tx: 249CCHNL 0 burst backoff 16 dBmCHNL 0 PwrCtrl cmd: 29 00 A0 00 00CHNL 0 Set Tx channel to 249C.CHNL 0 Tell DSP Tx idle channel is 2AB4.CHNL 0(T=14569) ,send orr burstCHNL 0 : Rx is 2ab4CHNL 0(T=14780) ,STATE CHANGE FROM 6 ------>4CHNL 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 2ab4CHNL 0(T=14780) ,STATE CHANGE FROM 4 ------>2CHNL 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”
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 5--6E. Maintenance Menu Items(1) The maintenance menu items given in Table 5-4 can be accessed through themaintenance port by pressing the ENTER key after the HS--600 system has bootedup. (See paragraph 2.D. in this section.)NOTE: ItemslistedinTable5-4areforreferenceonlyandwillbesetbythemanufacturer.NOTE: Changes to the parameters listed in Table 5-4 should only be accomplishedby 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: 1P(tx) Initial EIRP, range 20 to 25dBW in 0.5dBW steps: 25.0HzPlease enter new value between 20.0 to 25.0):Keep current value!Enter your selection: 2Reference oscillator correction factorrange +/--2200Hz, in 1Hz step: --125HzPlease enter new value between --2200 to 2200(+/--XXXX):Keep current value!Enter your selection: 3Transmit 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 5--7Table 5-4. Maintenance Menu Items (cont)Enter your selection: 4ISE MUT--TO--HPA output gainrange 36 to 42 dB, in 1 dB steps: 40HzPlease enter new value between 36 to 42:Keep current value!Enter your selection: 5HPA output to antenna input loss,range 1--6 dB, in 1dB steps: 2HzPlease enter new value between 1 to 6:Keep current value!Enter your selection: 6Minimum usable reported antenna gain below which the ISEceases operation of the HSD channelrange 7 to 12 dB, in 1dB steps: 7HzPlease enter new value between 7 to 12:Keep current value!Enter your selection: 7Maximum allowed HPA average output power,range 20 to 60W, or 13 to 18 dBW, in 0.5dB steps: 17.0HzPlease enter new value between 13.0 to 18.0):Keep current value!Enter your selection: 8Enabled Bearer Service Interface, 0 for ISDN S/T and 1 for PCM: 0HzPlease enter new value between 0 to 1:Keep current value!Enter your selection: 9Min. frame number for ack TX port: 3HzPlease 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: NPlease enter your new character (A--B):Keep current value!
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 5--8Table 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.****************MainMenu*******************1.Protocol Mode2.Manual Mode3.Change PasswordEnter your selection: 1NOTE: Press <ESC><ESC> or power cycle to exit from this menu.******************Menuinprotocolmode**************************1.Event LogESC. ExitEnter your selection:******************Menuinprotocolmode**************************1.Event LogESC. ExitEnter your selection: 1***************** Event Log Menu *********************1.Display last 20 Event Log records2.Display specified range of Event Log records3.Display all Event Log recordsV.Verify a specified Event Log Record in Hex formatC.Clear all Event Log recordsESC. ExitEnter your selection:******************Menuinprotocolmode**************************1.Event LogESC. ExitEnter your selection:
FAULT ISOLATION
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 6--1SECTION 6FAULT ISOLATION1. OverviewA. General(1) To be supplied.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 6--2Blank Page
MAINTENANCEPRACTICES
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 7--1SECTION 7MAINTENANCE PRACTICES1. OverviewA. General(1) This section provides instructions for removing, reinstalling, and adjusting theHS--600 HSU, combiner, and/or splitter that has been previously installed by theaircraft manufacturer or completion center. Adjustment information is called out asrequired.CAUTION: SHOULD ANY INSTALLATION CRITICAL CASES ARISE WITH THEREINSTALLATION OF ANY UNIT, YOU MUST COMPLY 100 PERCENTWITH THE INSTRUCTION.CAUTION: TO PREVENT DAMAGE TO EQUIPMENT, TURN AIRCRAFT POWER OFFWHEN REMOVING OR INSTALLING LRUS.B. Equipment and Materials(1) No additional special equipment or materials, other than those commonly used in theshop, are required to install the units in existing trays and clamps, and adjust thesystem. Do not over tighten mounting screws. Where torque values are not given, itis acceptable to finger tighten the mounting screws.2. Procedure for the HS--600 HSUA. 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 counterclockwisedirection.(c) Slowly pull forward on the unit handle to separate the unit and tray connectorsand 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 thepins from damage.(e) Place the HSU in a protective static--resistant bag and protective carrying case.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 7--2(2) Reinstall the HSU.(a) Remove the HSU from the protective carrying case and protectivestatic--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 NOTFORCE FIT. IF MATING IS DIFFICULT, REMOVE THE UNIT ANDCHECK FOR CONNECTOR PINS THAT CAN BE BENT OR OUT OFALIGNMENT. ALSO VISUALLY CHECK THE ALIGNMENT OF THERECEPTACLE ON THE MOUNTING TRAY.(d) Gently slide the unit backwards until its connectors are fully engaged with themating connectors of the mounting tray.(e) Put the holddown clamps in place and tighten the knobs in a clockwise directionuntil 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 andstart 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/SplitterA. Removal and Reinstallation Procedures(1) Remove the combiner.(a) Remove power from the HSU. Circuit breakers for the HSU are typically locatedon the flight deck.(b) Locate the combiner.(c) Disconnect the aircraft connectors from the combiner and place protective coverson the connectors.(d) Remove the six screws holding the combiner in position.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 7--3(2) Reinstall the combiner.(a) Attach the combiner using six screws.(b) Remove the protective covers from the connectors and install the aircraftconnectors 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 locatedon the flight deck.(b) Locate the splitter.(c) Disconnect the aircraft connectors from the splitter and place protective coverson 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 aircraftconnectors 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page 7--44. Instructions for Continued Airworthiness, Code of Federal RegulationCFR 91.213A. General(1) Maintenance requirements and instructions for continued airworthiness of theHS--600 HSU components are contained in the following paragraphs:(2) Installation of the HSU on an aircraft by Supplemental Type Certificate or Form 337obligates the aircraft operator to include the maintenance information provided by thismanual in the operator’s Aircraft Maintenance Manual and the operator’s AircraftScheduled 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 manualshould be placed into the aircraft operator’s appropriate aircraft Illustrated PartsCatalog (IPC).(3) Wiring diagram information contained in this manual should be placed into the aircraftoperator’s appropriate aircraft Wiring Diagram Manuals.(4) The high speed data system components are considered on--condition units and noadditional maintenance is required other than a check for security and operation atnormal inspection intervals.(5) If a system component is inoperative, remove unit, secure cables and wiring, collarapplicable switches and circuit breakers, and placard them inoperative. Reviseequipment list and weight and balance as applicable prior to flight and make a logbook entry that unit was removed. Refer to section 91.213 of the CFR or the aircraft’sminimum equipment list (MEL).(6) The HSU components can be repaired only at a factory authorized repair center or anappropriately rated FAA Part 145 repair station.(7) Once repaired, reinstall the LRU in the aircraft in accordance with the original Form337 approved data or instructions in this manual. Do a return--to--service test of thesystem and approve it for return to service with a log book entry required by section43.9 of the FAR.(8) Scheduled Maintenance Program tasks to be added to the aircraft operator’sappropriate 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 todetermine system condition and/or latent failures): None Required
APPENDIX A
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page A--1APPENDIX AM4 CALL CAUSE CODE LIST1. OverviewA. General(1) The following list of cause codes in Table A--1 describes the various conditions of afailed M4 terminal call.Table A--1. Call Cause Code ListCause Code Description Note0001 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 theBulletin 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 theNCSA/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.Mobile Earth Station (MES) is clearing the call as instructed by the relevant MES terminalequipment (i.e., normal clearing due to MES terminal “on--hook” etc.).1.1011 MES Busy.MES is rejecting the call because the specified MES terminal number is currently busy, andMES has not been authorized to divert calls which are addressed to that number.1.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page A--2Table A--1. Call Cause Code List (cont)Cause Code NoteDescription1012 MES is clearing the fixed--originated call because subsequent to the acceptance of the calland 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 AnswerMES is clearing the call because appropriate “off--hook” signaling has not been receivedfrom the addressed MES terminal (including any authorized diversions) within the allowedtime limit.1.1081 Call Failed, MES Terminal # Not InstalledMES is rejecting the call because the specified MES terminal number has not beeninstalled, and MES has not been authorized to divert calls which are addressed to thatnumber.1.1091 Call Failed, MES Terminal # out of ServiceMES is rejecting the call because the specified MES terminal number is currently out ofservice, and MES has not been authorized to divert calls which are addressed to thatnumber.1.1092 MES is clearing the fixed--originated call because subsequent to the acceptance of the calland the signaling of the identity of the mobile terminal to which the call will actually berouted, that terminal has become out--of--service and therefore cannot be rung.1.1141 Call Cleared, pre--empted at MESMES clear: pre--emption for higher priority call.1.1142 Call Refused due to Distress Call from MESMES clear: (Fixed) MES has initiated a distress call.1.1143 Call Cleared, pre--empted at MESFixed--originated call cleared by MES due to SATCOM reporting that it is no longer loggedon.1.1144 Attempted Call pre--empted by MES DistressMES clear: (mobile) MES has initiated a distress call.1.1145 Call Cleared, pre--empted by MESMobile--originated call cleared by MES due to SATCOM reporting that it is no longer loggedon.1.1146 Attempted Call Abandoned by MES TerminalMES is prematurely clearing the mobile--originated call which is in the process of beingestablished because the MES user has abandoned the call (by placing, the originatingterminal “on--hook).1.11A0 LES is clearing the call because the credit card being used is not valid (at this LES) for callsto the country indicated in the “Service Address’ information received from the MES.1.11D1 Call Failed, Request Data InvalidLES 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 currentlydefined in the SDM, mutually contradictory, or not applicable to a MES--originated call.)1.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page A--3Table A--1. Call Cause Code List (cont)Cause Code NoteDescription11D2 Call Failed, Insufficient Digits in Service AddressLES is clearing the call because the “Service Address” information received from the MES isinvalid (e.g., less than 2 digits). If the customer is dialing a valid phone number or prefixcode, verify that the MES has a corresponding Inmarsat mobile number (IMN)s in the LESaccess control and signalling equipment (ACSE) database.1.11D3 Call Failed, Invalid Service AddressLES is clearing the call because the “Service Address” information received from the MES isa 2--digit address which is either undefined or which is currently unavailable at this LES.1.11D4 LES is clearing the call because the “credit card data” information received from the MES isinvalid. (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 MEScontains 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 identificationnumber (PID) information in the fixed/MES--originated (PID) and PID/MES RegistrationTables 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 orsafety access request is not 4.8 kbps AMBE telephony.1.11D8 LES is clearing the call because the service address received from the MES requestingdistress, 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 notconsidered (at this LES) to be valid.1.11E1 LES is clearing the call because it has been determined that an excessive number ofconsecutive 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 thenext beam.1.1261 MES ack: received a simplex call (unstable). 1.1262 Call Cleared, MES Timeout Distress TestMES clear: distress test call has not been cleared in 120s.1.1281 Call Failed, MES Cannot AcceptMES is rejecting the call because the MES is not equipped to provide the specified service.1.1291 Call Failed, MES Cannot Accept at PresentMES is rejecting the call because although it is equipped to provide the specified service, itis not currently able to do so.1.12B1 Call Cleared by MES for Unspecified ReasonMES is rejecting or clearing the call for a reason which is not covered by any of the currentlydefined “Cause” events.1.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page A--4Table A--1. Call Cause Code List (cont)Cause Code NoteDescription12C1 Call Faded, No Scrambling Vector AckMES clear: Scrambling Vector Ack (95) not received by the MES.1.12C2 MES is clearing the call because a “Credit Card Valid” message (type A7) has not beenreceived by the MES within the allowed time limit.1.12C3 Call Failed, MES Timeout, No Terrestrial AnswerMES is clearing the call because an “LES Connect” message (type 8C) has not beenreceived by the MES within the allowed time limit.1.12C4 MES is clearing the call because the “authentication query” ISU message (type B4) and/or the“authentication query” SSU message (type B5) have not been received by the MES within theallowed time limit.1., 2.,13., 14.,15.12C5 MES is clearing the call because an expected supplementary services SU(s) has (have) notbeen received by the MES within the allowed time limit.1.12C6 MES is clearing the call because the “supplementary services interrogation” ISU (type B2H),and/or ”subscriber digits” SSU (type AD H) messages have not been received by the MESwithin the allowed time limit.1.12C7 MES is clearing the call because a “SCPC channel release” SU (type 8AH) has not beenreceived by the MES, in response to the transmission of a “notification acknowledge”message (type BAH) during the supplementary services call diversion information retrievalprocess, within the allowed time limit.1.12C8 (Spot Beam Handover): MES is clearing the call session in the next beam because the MESdid not detect the LESH carrier on the new frequency.1.12D1 Call Failed, Spot Beam Data InvalidLES is rejecting the call because the “spot beam ID” information received from the MES isinvalid, i.e., ID is not allocated on the satellite in use.1.12D2 Call Failed, Invalid Scrambling Vector (LES is clearing the call because the “ScramblingVector” 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 tostore the short message.1.1361 Call Cleared by MES; Cable UnwrapMES is clearing the call because the above--decks equipment is about to “cable unwrap”.1.1362 Call Cleared, Long Interruption ReceptionMES is clearing the call because a long--term interruption (16 sec) in reception of LEScarrier has occurred. The definition of a “long--term interruption” depends upon the servicetype.1., 3.1363 Call Cleared, MES Antenna Repointed(WS clear: switching ocean regions)A secondary functional center of Multi--channel MES is clearing the call because theprimary functional center has commanded the above--decks equipment to repoint to adifferent ocean region.1.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page A--5Table A--1. Call Cause Code List (cont)Cause Code NoteDescription1391 Aero Class MES only: MES is clearing the call because the call has lasted more than 700km in linear travelled distance.1.1392 Aeronautical Class MES only: MES is clearing the call because it has moved out of spotbeam coverage.1.1393 Aeronautical Class MES only: MES in “cooperative mode” is clearing the call because of apreemption request from the master entity. Call cleared by MES due to reported antennagain falling below the antenna gain threshold setting (Maintenance parameter #6) for morethan 10 seconds.1.1393 Call cleared by the MES due to the reported antenna gain falling below the antenna gainthreshold setting (maintenance parameter #6).1.1451 Call Failed, Terrestrial Circuits CongestedLES is rejecting the call because an appropriate terrestrial circuit is not currently available atthis specific LES.1.1452 Call Failed, LES CongestedLES is rejecting the call because an appropriate channel unit and associated terrestrialcircuit are currently not available at this LES.1.1502 (Spot Beam Handover): LES is ready to make the transition from the current beam to thenext 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 ChannelLES is rejecting the call because an appropriate satellite channel is not currently available atthis specific LES.1.1552 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 LESLES is rejecting the call because the requested service is not provided by this specific LES.1.1591 LES is rejecting the call because the requested service is temporarily not available at thisspecific LES.1.1592 LES is clearing the call because the specified credit card type is not currently supported bythis 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.If the customer’s ISP or AA are authorized through this LES, verify that the MES ID hascorresponding IMNs in the LES ACSE database.If the call setup proceeds to the point where the ACSE passes the call to the switch, checkto see 1) if the area code is invalid, 2) if a valid area code is missing in the switch, 3)checkto see if the ACSE passes the correct ICD message including the IMN (not all 9’s) to theswitch.1., 4.15A2 LES is rejecting the call because the specified MES is not authorized to use specificrequested service via this specific LES.1.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page A--6Table A--1. Call Cause Code List (cont)Cause Code NoteDescription15A3 LES is clearing the call because the “credit card data” information received from the MEShas been rejected by the credit card authorization process.1.15A4 LES is clearing the call because the data received from the MES in the “AuthenticationReply” 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 thisspecific LES.1.15A6 LES is rejecting the call because the specified PID is not authorized to use specificrequested service via this specific LES. (User not authorized/barred for service in the LESdatabase.)1.15A7 LES is clearing the call because the service address received from the MES is notauthorized for the requested priority.1.15B1 Call Cleared by LES for Unspecified ReasonsLES is rejecting or clearing the call for a reason which is not covered by any of the currentlydefined “Cause” events.1.15C1 Call Failed, LES Timeout, No AssignmentLES is rejecting the call because an appropriate “Channel Assignment” message has notbeen received from the NCS by the LES within the allowed time limit.1.15C2 LES is clearing the call because the “Service Address” information has not been receivedby the LES from MES within the allowed time limit.1.15C3 Call Failed, LES Timeout, No Scrambling VectorLES is clearing the call because a “Scrambling Vector” message (type 8D) has not beenreceived by the LES from the MES within the allowed time limit.1.15C4 Call Failed, No Service Address or VectorLES 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 withinthe allowed time limit.1.15C5 LES is clearing the call because the complete “credit card data” information has not beenreceived by the LES within the allowed time limit.1.15C6 Call Failed, LES Timeout, No Return Carrier IDLES is clearing the call because the Return Carrier Identifier (8B) was not received.1.15C7 LES is clearing the call because an “MES Connect” message (type 99) has not beenreceived 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 beenreceived by the LES within the allowed frame limit.1., 6.15CA LES is clearing the call because a “notification acknowledge” message (type BAH) has notbeen received by the LES within the allowed time limit.1.15CB LES is clearing the call because the request sequence number contained in the received“notification acknowledge”message (type BA) is not valid (i.e. eithernot ‘0’ or not the next valuein the sequence).1.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page A--7Table A--1. Call Cause Code List (cont)Cause Code NoteDescription15CC Aeronautical Class MES only: (Spot Beam Handover): LES is terminating the procedurebecause 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 MESdid not indicate that it was ready to make the transition (possibly because the MES did notreceive the Channel Assignment).1.15D1 LES is rejecting the call because the “Channel Assignment” message received from theNCS contains inappropriate or conflicting information.1.15D2 LES is clearing this MES ID and channel number in the busy lists at LES and NCS becausea new call to/from this MES is being set--up (and thus any previous call to/from this MEScleared).1.15E1 Call Cleared, MES still Transmitting FaultLES is attempting to clear an MES which has sent an SCPC channel release message butis found still to be transmitting 5.12 sec later.1.1651 Call Failed, LES Congested, No Channel UnitLES is rejecting the call because an appropriate channel unit is not currently available atthis specific LES.1.1661 Call Failed, Long Interruption in ReceptionLES is clearing the call because of an interruption in reception of the MES carrier exceedingthe allowed time limit of 62 seconds.1.16C1 LES clear: SEST carrier not received. 1.16C2 LES is clearing the call because an appropriate SCPC MES carrier has not been receivedby 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 didnot detect the MESH carrier on the new frequency1.1790 LES is clearing the call because of a malfunction in the credit card validity checkingdatabase or in the communications links.1.1791 LES is clearing the call because of a malfunction in the authentication checking database orin 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. 1., 7., 8.1852 NCS is rejecting the call because no SCPC channel exists at the NCS which matches thecontents of the Channel Parameters, Service Nature, Service Type, MES Category, Spot BeamID and Priority fields contained in the Request for Channel Assignment.1., 9.,10., 11.,12.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page A--8Table A--1. Call Cause Code List (cont)Cause Code NoteDescription1853 NCS is rejecting the call because no SCPC channel is currently available for the specifiedleasemarked MES.Contact the NCS to verify that the MES has frequencies in a lease pool available or requestthatthe MES ID be removed from the leasemark pool.1.1854 NCS is rejecting the call because the MES is outside the spot beam coverage area. 1.1855 NCS is rejecting the call because an appropriate SCPC channel is not currently available andchannel pre--emption failed.1.1856 NCS is rejecting the call because the requested spot beam indicates failed spot beam selection(“FF” ) and an appropriate global SCPC channel is not currently available.1.1857 (Spot Beam Handover) NCS is rejecting the Handover Request because an appropriate SCPCchannel is not available in the next beam.1.18A1 NCS is rejecting the call because the specified MES ID was not found in the “Forward andReturn MES ID” cross--reference table.1.18A2 NCS is rejecting the call because the specified MES is not authorized for any service (exceptfor Distress calls) at the NCS.1.18A3 NCS is rejecting the call because the specified LES is not authorized for the requested serviceat the NCS.1.18A4 Reserved. 1.18B1 NCS is rejecting or clearing the call for a reason which is not covered by any of the currentlydefined “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 (inreaction 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( i.e. no response within the allowed time limit).1.18D1 NCS is rejecting the call because the Request for Call Announcement or Request for ChannelAssignment contains invalid or inappropriate information.1.18E1 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 “callannouncement” addressed to that MES.1.18E2 NCS is rejecting the call because the specified MES is busy with an IPDS call through thesame 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 relevantterrestrial circuit (i.e., normal clearing).1.1F11 LES is clearing the call because the terrestrial called party is engaged (busy). 1.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page A--9Table A--1. Call Cause Code List (cont)Cause Code NoteDescription1F21 Call Failed, LES Timeout, No AnswerLES is clearing the call because appropriate “off--hook” signaling from the terrestrial calledparty has not been received by the LES within the allowed time limit.1.1F61 Call Failed, Terrestrial Circuit FailureLES is clearing the call because of the detection of a failure in the relevant terrestrial circuit.1.1F62 Call Failed, Early Clear Terrestrial CircuitLES is clearing the call before the “MES Connect”.1.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. Theuser must wait at least 20 seconds before making a mobile--originated call. Ask the customer to be patient and tryagain.3. If this cause code occurs during call setup, there could be a problem with a particular LES channel unit. Thechannel unit may need to be reset. This cause code may also occur after the call has been connected. Thisproblem 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. Forfixed--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 orunavailable.8. Frequencies/channels at the NCS for a particular spot beam and for a specific service could be blocked orunavailable/not assigned or congested.9. Verify that the LES is enabled for the particular service at the NCS10. Verify that the MES/LES is lease--marked if appropriate11. Verify that the Aero--HSD/F MES is using the new generation of signaling units12. 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page A--10Blank Page
APPENDIX B
SYSTEM DESCRIPTION AND INSTALLATION MANUALHS--600 High Speed Data System23--20--3130 May 2002Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.Page B--1APPENDIX BINMARSAT REGISTRATION FORM1. OverviewA. General(1) This appendix provides an example of the Inmarsat registration form required toactivate the HSD system.
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