Page 1 AVIATOR 700/700D Installation & maintenance manual...
Page 3 AVIATOR 700/700D Installation & maintenance manual Document number: 98-124743-G Release date: 15 October 2018...
Page 4: Trademark Acknowledgements
This manual and the drawings and wiring diagrams contained herein may not be used as a substitute for an STC package. The newest versions of Cobham SATCOM user and installation manuals as well as outline drawings can be downloaded from www.cobham.com/satcom, Cobham SYNC Partner Portal. Some material and features are for partners only and can only be accessed after login with a password.
Page 5: Record Of Revisions
The following figures have been edited: 2-5, 5-1, 6-7, 6-43, 6-45, 6- 25 March 2010 53 and 6-55. Table 2-4 added. Section 6.10.8 Remote management added. The AVIATOR 700 replaces the earlier Thrane & Thrane Aero-SB 28 January The Aero-SDU Configuration Program replaces the earlier HSD+SB+ 2011 Configuration Program....
Page 6 The manual has been rebranded to Cobham layout. 10 August 2016 Section, table and figure numbers refer to the numbers in the present updated version. The following sections have been edited: 2.1.1, 2.1.2, 2.2.2, 3.1, 3.12, 5.1.1, 5.2.6, 5.6.1, 6.2.1, 6.4.2, 6.6.2, 6.7.8, 6.7.14, 6.8.10, 6.11.1, 8.1.1, 8.2.2, 8.3, 8.4.7, 8.6, C.3.1...
Page 7: Table Of Contents
About this manual Purpose .............................1-1 Organization .........................1-1 Related documentation ....................1-2 Precautions: Warnings, Cautions and Notes ..........1-2 Chapter 2 Introduction to the AVIATOR 700 General description ......................2-1 2.1.1 The AVIATOR 700 system ....................2-1 2.1.2 AVIATOR 700 features ....................2-10 Application ......................... 2-11 2.2.1...
Page 8 Connection with SDU ....................4-24 4.5.2 Connection with HPA ..................... 4-25 4.5.3 Connection with SBU ..................... 4-25 Chapter 5 Installation General installation information ................5-1 5.1.1 Overview ..........................5-1 5.1.2 Minimum system components ..................5-2 5.1.3 To upgrade your installation from Aero-HSD to AVIATOR 700 ....5-4 98-124743-G...
Page 9 Recommended cables for RS-422 SBU control interface ......5-84 5.4.7 Recommended cables for Ethernet ................. 5-84 5.4.8 Cables for Discrete Signals ..................5-84 Verifying the installation ..................5-85 Activation of airtime services ................5-85 5.6.1 The 3 ID numbers for the AVIATOR 700 system ..........5-85 98-124743-G...
Page 10 Table of contents Chapter 6 Configuration of the AVIATOR 700 system Configure the basic system ..................6-2 Aero-SDU Configuration Program for the SDU .........6-2 6.2.1 Install the Aero-SDU Configuration Program ............6-3 6.2.2 To use the Aero-SDU Configuration Program ............6-4 6.2.3 Basic configuration of the SDU ................. 6-10 6.2.4...
Page 11 6.11 Configuration of 3rd party phone systems ..........6-95 6.11.1 Sigma setup ........................6-95 6.11.2 ICG DECT Cordless Handset setup ................6-95 6.11.3 Iridium Communication System, ICS-200 ............6-96 6.12 AVIATOR 700 system ready for use ............6-100 Chapter 7 Check procedures Basic check flow ........................7-1 7.1.1 Check procedures .......................7-1...
Page 12 Table of contents Interference Test ......................7-6 7.4.1 Introduction ..........................7-6 7.4.2 Test ............................7-6 Functional Test, Airborne ..................7-7 Chapter 8 Maintenance and troubleshooting Continued Airworthiness ....................8-1 8.1.1 General .............................8-1 8.1.2 Instructions ..........................8-1 Get support: Service log and HELPDESK ............8-5 8.2.1 Airtime support ........................8-5 8.2.2 System support ........................8-5 8.2.3...
Page 13 SDU software update to version 1.14 or higher ..........C-5 C.3.2 Read the configuration from the SDU ..............C-6 C.3.3 Select the correct product: AVIATOR 700 .............C-6 C.3.4 Update the cable loss ......................C-7 C.3.5 Update the GES list with I-4 satellites ...............C-7 C.3.6...
Page 14 Table of contents Appendix D System messages Types of messages ......................D-1 Cause Codes ........................D-2 D.2.1 H+ Cause Codes ........................D-2 D.2.2 MPDS Cause Codes ......................D-6 D.2.3 ISDN Cause Codes ......................D-8 BITE Error codes ......................D-15 D.3.1 Definition of severity levels ..................D-15 D.3.2 List of BITE codes ......................D-16 List of SBU events ......................D-28...
Page 15: List Of Figures
About this manual Chapter 2 Introduction to the AVIATOR 700 Figure 2-1: Communication devices for the AVIATOR 700 system (example for a Level E system)2-3 Figure 2-2: Satellite coverage of data and voice services..................2-5 Figure 2-3: SwiftBroadband and classic aeronautical services coverage on I4 satellite......2-6 Figure 2-4: Swift64 and classic aeronautical services coverage on I3 satellite ..........
Page 16 Figure 4-12: 2-Wire Cradle connector (DB9M). View: Solder side ..............4-22 Chapter 5 Installation Figure 5-1: AVIATOR 700 minimum system........................ 5-3 Figure 5-2: Mounting the Rx Power Splitter......................... 5-6 Figure 5-3: Mounting two WLAN antennas for optimum performance............5-8 Figure 5-4: Wiring SDU power supply ..........................
Page 17 TT 37-112940 maintenance cable for front connector on SDU and PC......5-77 Figure 5-36: Wiring maintenance handset ........................5-78 Chapter 6 Configuration of the AVIATOR 700 system Figure 6-1: Line of sight when communicating with the satellite..............6-1 Figure 6-2: Configuration tools for SDU and SBU.....................
Page 18 List of figures Figure 6-32: Web interface: Settings, Common, Closed user group..............6-43 Figure 6-33: Web interface: Settings, IP handsets ....................6-45 Figure 6-34: Web interface: Settings, IP handsets, Call settings ................ 6-46 Figure 6-35: Web interface: Settings, Discrete I/O ....................6-48 Figure 6-36: Web interface: Settings, System Type....................
Page 19 Figure 6-78: Web interface: Settings, IP handsets, Call settings (example, Multi-voice) ....... 6-93 Figure 6-79: Web interface: Site map..........................6-94 Figure 6-80: AVIATOR 700 system ready for use ....................6-100 Chapter 7 Check procedures Chapter 8 Maintenance and troubleshooting Figure 8-1: Support tools: Service log and Helpdesk....................
Page 20 List of figures Figure C-9: Upgrading HSD to AVIATOR 700, step 7/7 ..................C-8 Appendix D System messages Appendix E WLAN country codes Appendix F Terminal commands Figure F-1: How to change shells............................F-1 Figure F-2: Troubleshooting SDU, Call Log command: call -p ................F-6...
Page 21 List of tables Chapter 1 About this manual Table 1-1: List of Related Documentation........................1-2 Chapter 2 Introduction to the AVIATOR 700 Table 2-1: Part numbers..............................2-12 Table 2-2: Part numbers for configuration modules and options ..............2-13 Table 2-3: Part numbers for Klixon circuit breaker ....................
Page 22 List of tables Table 5-9: Pins for SBU power supply......................... 5-15 Table 5-10: Requirements to SBU power cables ...................... 5-16 Table 5-11: SBU Pins for AMT-50 antenna subsystem..................5-18 Table 5-12: SDU Pins for AMT-50 antenna subsystem..................5-18 Table 5-13: HPA Pins for ARINC 741 antenna system ..................
Page 23 Table 5-64: Allowed lengths for WLAN cables ......................5-83 Table 5-65: ID numbers in the Inmarsat network....................5-85 Chapter 6 Configuration of the AVIATOR 700 system Table 6-1: Configuration related menu commands ....................6-6 Table 6-2: Menu commands for configuration data transfer................6-12 Table 6-3: Web interface: Icons ............................
Page 24 Environmental Qualification Form for 2-Wire Handset and Cradle........B-13 Appendix C Upgrade from Aero-HSD+ to AVIATOR 700 Table C-1: Items needed for upgrading to AVIATOR 700 Level E or AVIATOR 700D (Level D) ..C-1 Table C-2: Items needed for upgrading for different antenna types .............C-1 Table C-3: Upgrade to AVIATOR 700, mounting and wiring considerations..........C-2...
Page 25: Appendix F Terminal Commands
List of tables Appendix F Terminal commands Table F-1: “list” Commands..............................F-3 Table F-2: “slog” Commands .............................. F-4 Table F-3: “call_log” Commands............................F-6 Table F-4: “flight” Commands............................F-7 Table F-5: Status ARINC driver, overview ........................F-10 Table F-6: Purpose of the states for receivers ......................F-10 Table F-7: Purpose of the states for the antenna modem.................F-10 Table F-8:...
Page 26 List of tables xxiv 98-124743-G...
Page 27: Chapter 1 About This Manual
• Configuration An introduction to the Aero-SDU Configuration Program and the SwiftBroadband Unit’s web interface, and a description of how to configure the AVIATOR 700 system. A short description of how to configure some of the 3rd party handsets. • Check Procedures. An overview of the recommended check procedures and checklists.
Page 28: Related Documentation
98-129600 AVIATOR Wireless Handset and Cradle Installation & Maintenance Manual 98-132721 Swift64 and H+ Data Service, Supplement to AVIATOR 700 and Aero- HSD+ User Manual (available for download) 95-160581 Vendor Service Information Letter: Service migration from Inmarsat I- 3 to I-4 satellite constellation (available for download)
Page 29: Introduction To The Aviator 700
Cobham. The AVIATOR 700 system is available in two versions: Note • AVIATOR 700 approved to RTCA specification DO- 178B level E and DO-254 level E • AVIATOR 700D approved to RTCA specification DO-178B level D and DO-254 level D.
Page 30 (HPA) must all be level D approved. No mismatch is allowed. Non-Safety interfaces for AVIATOR 700 (Level E) The following interfaces in the AVIATOR 700 system are strictly for non-safety usage: • Cockpit voice • ACARS/AFIS/CMU (information and management systems) •...
Page 31 Services on page 2- The AVIATOR 700 system provides a wide range of user interfaces: several 4-wire and 2- wire interfaces, ISDN, WLAN and Ethernet interfaces available on the SDU and SBU.
Page 32 See also the I3 to I4 Satellite Service Migration - Service Information Letter on the Cobham SYNC Partner Portal. After migration, I3 will still remain in the AVIATOR 700 user interface as virtual satellites. Chapter 2: Introduction to the AVIATOR 700 98-124743-G...
Page 33: Figure 2-2: Satellite Coverage Of Data And Voice Services
3.1 kHz audio, it accommodates simultaneous voice and data. You can use the AVIATOR 700 cabin installation for IP background data, IP data streaming at 8/16/32/64/128 kbps and X-stream full-channel streaming > 250 kbps, and standard AMBE 2 voice.
Page 34: Figure 2-3: Swiftbroadband And Classic Aeronautical Services Coverage On I4 Satellite
Atlantic Ocean Region-East Indian Ocean Region conditions. Classic Aero and Swift 64 coverage December 2015. Figure 2-4: Swift64 and classic aeronautical services coverage on I3 satellite Chapter 2: Introduction to the AVIATOR 700 98-124743-G...
Page 35: Figure 2-5: Pbx Functionality In Sdu And Sbu
General description PBX telephone exchange The AVIATOR 700 system has two built-in PBX units: One in the SDU and one in the SBU, making the AVIATOR 700 capable of connecting in total four 4-wire handsets and four 2- wire devices.
Page 36 SBU. The SDU to SBU Software Interface is pre-configured at the factory when ordering the basic AVIATOR 700 system. Satcom antenna systems The AVIATOR 700 system can be used with a wide range of satcom antennas. An AVIATOR 700 system must only be used with satcom antennas that have received type approval by Inmarsat.
Page 37 He can also read status messages of the AVIATOR 700 system in the MCDU display. 1. Supported from software version 1.07 for AVIATOR 700 (Level E) and 2.01 for AVIATOR 700D (Level D). 98-124743-G...
Page 38: Aviator 700 Features
General description 2.1.2 AVIATOR 700 features The AVIATOR 700 system has the following features:  Unique multi-channel solution, combining the Inmarsat Aero-H+, Swift64 and SwiftBroadband services with the following channels available: • one spot beam SwiftBroadband channel, providing access to the BGAN system with data rates up to 432 kbps.
Page 39: Software Versions
Application Software versions The AVIATOR 700 is shipped with the following software versions (at the time of writing): For Level E: SBU software version 1.09 SDU software version 1.15. For Level D: SBU software version 2.02 SDU software version 2.01 Application 2.2.1...
Page 40: Part Numbers
Application 2.2.2 Part numbers Applicable part numbers This installation manual is for the AVIATOR 700 system and is applicable to the part numbers in the following tables. Part number Unit description 405035A Satellite Data Unit (SDU) [without CM] AVIATOR 700...
Page 41: Table 2-2: Part Numbers For Configuration Modules And Options
CM for SBU with A700 key, Router, WiFi, Multi voice, ACARS+SB- Safety (ICAO) voice option(s) Table 2-2: Part numbers for configuration modules and options a. By default, SB-Safety voice is not supported by the AVIATOR 700 system. If SB-Safety voice is required, contact your sales representative. 98-124743-G...
Page 42: Table 2-3: Part Numbers For Klixon Circuit Breaker
32C2. DPX2NA-67322-606 Required Connector Kit for SBU tray: ITT Cannon Connector, Dual Plug, contact arrangement top: 33C4, bottom: 33C4. (old number: DPX2NA-67322-500) Table 2-4: Part numbers for trays and connectors 2-14 Chapter 2: Introduction to the AVIATOR 700 98-124743-G...
Page 43: Table 2-5: Installation Kits, Contact Information
Home page: www.CarlisleIT.com Table 2-5: Installation kits, contact information ECS offers two installation kits, one for AVIATOR 700 (ECS part number: 120-14973-101) and one for the SBU (ECS part number: 120-14973-102). Upgrade from HSD Item in installation kit AVIATOR 700 to AVIATOR 700 ARINC connector, SBU ...
Page 44: System Block Diagrams
AVIATOR 700 system. In order to use the satcom antenna with the AVIATOR 700 system, the specific antenna type and the AVIATOR 700 system must be Type Approved by Inmarsat as a combined system.
Page 45: Arinc 741 Compatible High Gain Antenna
The AVIATOR 700 system supports ARINC 741 compatible antenna systems, such as a HGA-6000 antenna or an HGA-7000 antenna with an HGA-7000 BSU. In an AVIATOR 700 system, there are extra requirements to the DLNA. For further Note information, see Selection of DLNA on page 2-16.
Page 46: Figure 2-7: System Configuration With Hga 7000
System block diagrams You can also configure the system with AHRS/GPS. Figure 2-7: System Configuration with HGA 7000 2-18 Chapter 2: Introduction to the AVIATOR 700 98-124743-G...
Page 47: Dual Side Panel Antenna System
An ARINC 741 dual side panel antenna system may be installed, in order to improve the view to the satellite. In an AVIATOR 700 system, there are extra requirements to the DLNA. For further Note information, see Selection of DLNA on page 2-16.
Page 48: Arinc 781 Compatible High Gain Antenna
2.3.4 ARINC 781 compatible High Gain Antenna The AVIATOR 700 system supports ARINC 781 compatible antenna systems. In an AVIATOR 700 system, there are extra requirements to the DLNA. For further Note information, see Selection of DLNA on page 5-16.
Page 49: User Interfaces
System block diagrams 2.3.5 User interfaces The AVIATOR 700 system has the following user interfaces: Interfaces SDU SBU 4-wire PBX interfaces This interface can be used e.g. for the TT-5620A 4-Wire Handset and TT-5622A 4-Wire Cradle. For additional information on the use of the 4-wire interfaces see Wiring telephone systems on page 5-46.
Page 50: Figure 2-10: System Configuration Showing The User Interfaces
System block diagrams The following figure shows most of the possible user interfaces. Figure 2-10: System Configuration showing the user interfaces 2-22 Chapter 2: Introduction to the AVIATOR 700 98-124743-G...
Page 51: Operation Overview
Operation overview 2.4.1 Configuration There are two configuration tools for the AVIATOR 700 system: • Aero-SDU Configuration Program for the SDU The configuration tool for the SDU is the Aero-SDU Configuration Program. It is launched from a standard PC connected to the front connector of the SDU (RS232) with the maintenance cable (see Figure 5-35: TT 37-112940 maintenance cable for front connector on SDU and PC).
Page 52: Operation
2.4.2 Operation The core components of the AVIATOR 700 System are the SDU with the classic aero services and the SBU providing SwiftBroadband services. These two units share the same satcom antenna and HPA. When installing the system you must bear in mind at which unit the handsets and PC equipment are connected, so you prepare the installation for the future use of various handsets and computers in the cabin.
Page 53: Chapter 3 Equipment Drawings
The drawings in this manual are for reference only. If you have access to the Important partner platform Cobham SYNC, you can get copies of the outline drawings at: https://sync.cobham.com/satcom/support/downloads. You can download the drawings as PDF files. There are also 3D models of selected units.
Page 54: Tt-5035A Satellite Data Unit
TT-5035A Satellite Data Unit TT-5035A Satellite Data Unit Figure 3-1: Outline Drawing: Satellite Data Unit Chapter 3: Equipment drawings 98-124743-G...
Page 55: Tt-5035A-001 Configuration Module (Inserted In The Sdu)
TT-5035A Satellite Data Unit 3.2.1 TT-5035A-001 Configuration Module (inserted in the SDU) Figure 3-2: Outline Drawing: Configuration Module 98-124743-G Chapter 3: Equipment drawings...
Page 56: Tt-5014A High Power Amplifier
TT-5014A High Power Amplifier TT-5014A High Power Amplifier Figure 3-3: Outline Drawing: High Power Amplifier Chapter 3: Equipment drawings 98-124743-G...
Page 57: Tt-5040A Sbu
TT-5040A SBU TT-5040A SBU Figure 3-4: Outline drawing: TT-5040A SBU 98-124743-G Chapter 3: Equipment drawings...
Page 58: Tt-5040A-001 Cm (Inserted In The Sbu)
TT-5040A SBU 3.4.1 TT-5040A-001 CM (inserted in the SBU) Figure 3-5: Outline drawing: TT-5040A-001 CM, inserted in the SBU Chapter 3: Equipment drawings 98-124743-G...
Page 59: Tt-5038A-002 Tx Coupler
TT-5038A-002 Tx Coupler TT-5038A-002 Tx Coupler Figure 3-6: Outline Drawing: Tx Coupler 98-124743-G Chapter 3: Equipment drawings...
Page 60: Tt-5038A-003 Rx Power Splitter
TT-5038A-003 Rx Power Splitter TT-5038A-003 Rx Power Splitter If the Rx Power Splitter is to be mounted on a flat surface, mount it on a 3 mm Note mounting plate to provide enough space for mounting of the connectors. For further information see Rx Power Splitter on page 5-5.
Page 61: Tt-5013A Dlna Type F
Dimentions are in inches/[mm] A=10.350 [262.90] Tolerances: ± 0.020/[0.5] B= 9.550 [242.57] Unless otherwise stated. Placement of C= 8.464 [215.00] Thrane (Cobham) S/N Label D= 7.764 [197.20] E= 9.852 [250.24] F=11.099±0.04 [281.51]±0.013 G= 3.960 [100.50] H= 2.000 [50.79] MAX J= 2.180 [55.30] K= 0.860 [21.90]...
Page 62: Tt-5620A 4-Wire Handset
TT-5620A 4-Wire Handset TT-5620A 4-Wire Handset Figure 3-9: Outline Drawing: 4-Wire Handset 3-10 Chapter 3: Equipment drawings 98-124743-G...
Page 63: Tt-5622A 4-Wire Cradle
TT-5622A 4-Wire Cradle TT-5622A 4-Wire Cradle Figure 3-10: Outline Drawing: 4-Wire Cradle 98-124743-G Chapter 3: Equipment drawings 3-11...
Page 64: Tt-5621B 2-Wire Handset
TT-5621B 2-Wire Handset 3.10 TT-5621B 2-Wire Handset Figure 3-11: Outline drawing: TT-5621B 2-Wire Handset 3-12 Chapter 3: Equipment drawings 98-124743-G...
Page 65: Tt-5622B 2-Wire Cradle
TT-5622B 2-Wire Cradle 3.11 TT-5622B 2-Wire Cradle Figure 3-12: Outline drawing: TT-5622B 2-Wire Cradle 98-124743-G Chapter 3: Equipment drawings 3-13...
Page 66: Sbu Trays
SBU trays 3.12 SBU trays The comment OBSOLETE refers to the -102 assembly. Note Figure 3-13: Outline drawing: SBU tray: ECS PO299-101 3-14 Chapter 3: Equipment drawings 98-124743-G...
Page 67: Figure 3-14: Outline Drawing: Sbu Tray: Emteq Mt4-2346-101
SBU trays Figure 3-14: Outline drawing: SBU tray: EMTEQ MT4-2346-101 (page 1) 98-124743-G Chapter 3: Equipment drawings 3-15...
Page 68: Figure 3-15: Outline Drawing: Sbu Tray: Emteq Mt4-2346-101
SBU trays Figure 3-15: Outline drawing: SBU tray: EMTEQ MT4-2346-101 (page 2) 3-16 Chapter 3: Equipment drawings 98-124743-G...
Page 69: Sdu And Hpa Tray
SBU trays 3.12.1 SDU and HPA tray Figure 3-16: Outline Drawing: Tray for SDU and HPA. 98-124743-G Chapter 3: Equipment drawings 3-17...
Page 70: Sdu Tray Connector
SDU tray connector 3.13 SDU tray connector For correct index pin codes for the SDU see Figure 4-2 on page 4-4. Figure 3-17: SDU Tray Connector: ITT Canon DPX2NA-67322-605 3-18 Chapter 3: Equipment drawings 98-124743-G...
Page 71: Hpa Tray Connector
HPA tray connector 3.14 HPA tray connector For correct index pin codes for the HPA see Figure 4-3 on page 4-10. Figure 3-18: HPA Tray Connector 98-124743-G Chapter 3: Equipment drawings 3-19...
Page 72: Sbu Tray Connector
SBU tray connector 3.15 SBU tray connector For correct index pin codes for the SBU see Figure 4-5 on page 4-14. Figure 3-19: Outline drawing: SBU tray connector: ITT Cannon DPX2NA-67322-606 3-20 Chapter 3: Equipment drawings 98-124743-G...
Page 73: Contact Assembly: Quadrax Pin Size 5 Special
Contact Assembly: Quadrax Pin size 5 special 3.16 Contact Assembly: Quadrax Pin size 5 special Figure 3-20: Contact Assembly: Quadrax Pin size 5 special: ITT Cannon 244-0011-001 98-124743-G Chapter 3: Equipment drawings 3-21...
Page 74 Contact Assembly: Quadrax Pin size 5 special Figure 3-20: Contact Assembly: Quadrax Pin size 5 special: ITT Cannon 244-0011-001 (Continued) 3-22 Chapter 3: Equipment drawings 98-124743-G...
Page 75: Tt-5040A-004 Wlan Antenna
TT-5040A-004 WLAN antenna 3.17 TT-5040A-004 WLAN antenna Original Manufacturer P/N: VT Miltope 901167-2. Measures are in inches. Figure 3-21: Outline drawing: TT-5040A-004 WLAN antenna 98-124743-G Chapter 3: Equipment drawings 3-23...
Page 76 TT-5040A-004 WLAN antenna 3-24 Chapter 3: Equipment drawings 98-124743-G...
Page 77: Chapter 4 Connectors And Pin-Out
Chapter 4 Connectors and pin-out This chapter has the following sections: • TT-5035A Satellite Data Unit • TT-5014A High Power Amplifier • TT-5040A SBU • Cradle connectors for handsets • Mating connectors in aircraft TT-5035A Satellite Data Unit 4.1.1 Connectors on SDU There are three connectors on the SDU: •...
Page 78: Sdu Maintenance Front Connector
TT-5035A Satellite Data Unit 4.1.2 SDU Maintenance front connector Connector drawing Figure 4-1: SDU Front Connector, Face View of Engaging End. (DB15F) Functions The front connector is a 15 pin Female Sub-D Filter connector, and contains the following interfaces: • EIA/TIA-232-E PC port to connect to PC with Aero-SDU Configuration Program •...
Page 79: Table 4-1: Pin-Out For Sdu Front Connector
TT-5035A Satellite Data Unit Pin-out for SDU front connector Pin. No. Pin Name Maintenance Handset Audio In Hi Maintenance Handset Audio In Lo Maintenance Handset Audio Out Hi Maintenance Handset Audio Out Lo Signal Ground SGND Maintenance Handset RS-485 Data A Maintenance Handset RS-485 Data B +12 V DC/120 mA GND, Power Return (for +12 V DC)
Page 80: Sdu Rear Receptacle
TT-5035A Satellite Data Unit 4.1.3 SDU rear receptacle Connector drawing Figure 4-2: SDU Rear Receptacle and Mating Plug in Tray, Engaging End Functions, top plug The Top Plug (TP) connects the following signals: Power, RF Interfaces and Antenna Modem: • +28 V DC Power + chassis ground •...
Page 81 TT-5035A Satellite Data Unit Functions, bottom plug The Bottom Plug (BP) connects the following signals: Aircraft Avionics Interfaces: • 24 bit discrete hardwire strapped ICAO address • Two high speed ARINC 429 Inertial Reference System (IRS) or • Two high or low speed ARINC 429 Attitude and Heading Reference System (AHRS) •...
Page 82: Table 4-2: Pin-Out For Sdu Rear Receptacle (Top Plug)
TT-5035A Satellite Data Unit Pin-out for SDU rear receptacle (top plug) Pin No. Pin Name Pin No. Pin Name Handset #1 Audio Out Hi /  TP12 TP A1 RF Rx input from power splitter Cockpit Voice Audio #1 Out Hi TP A2 RF Tx output to coupler (Coax) Handset #1 Audio Out Lo / ...
Page 83 TT-5035A Satellite Data Unit Pin-out for SDU rear receptacle (bottom plug) Pin No. Pin Name Pin No. Pin Name BP27 Data from primary IRS 429 B / Data ICAO Address Bit #1 (MSB) from primary AHRS 429 B ICAO Address Bit #2 BP28 Data from second IRS 429 A / Data ICAO Address Bit #3...
Page 84 TT-5035A Satellite Data Unit Pin No. Pin Name Pin No. Pin Name Data bus output to SBU;  BP70 BP46 Data bus from MCDU #1 429 A Output B, RS-422 BP47 Data bus from MCDU #1 429 B BP71 Data bus output to SBU; BP48 Data bus to MCDU #1 &...
Page 85: Table 4-3: Pin-Out For Sdu Rear Receptacle (Bottom Plug)
TT-5035A Satellite Data Unit Pin No. Pin Name Pin No. Pin Name 4-Wire Handset #2  BP96 BP87 WH-10/MagnaStar Ringer Output B2 or RS-485 Data A ICS-200 Hook Switch Output #2 or CP Voice Call Light Output #2 (Discrete 4-Wire Handset #2  BP97 RS-485 Data B BP88...
Page 86: Tt-5014A High Power Amplifier
TT-5014A High Power Amplifier TT-5014A High Power Amplifier 4.2.1 HPA rear receptacle The HPA has one connector: An ARINC 404, shell size 2, rear receptacle, used for connection to the antenna system and the SDU. Connector drawing Mating Plug in Tray HPA Rear Receptacle Top plug (TP) Index pin code 08...
Page 87: Table 4-4: Pin-Out For Hpa Receptacle (Top Plug)
TT-5014A High Power Amplifier Pin-out for HPA receptacle Top Pin Pin Name RF Tx output to DLNA RF Tx input from coupler Table 4-4: Pin-out for HPA Receptacle (Top Plug) Bottom Bottom Pin Name Pin Name BP17 HPA Mute 1 A BP A1 +28 V DC Power BP18...
Page 88: Tt-5040A Sbu
Connector functions The front Maintenance interface is 10/100BaseT Ethernet, IEEE802.3. Use this interface for the following purposes: • AVIATOR 700 system configuration • Maintenance • System software upgrade For systems without the Built-in Router option enabled, i.e. the basic version...
Page 89: Table 4-6: Pin-Out For Sbu Maintenance Connector (Standard Ethernet)
TT-5040A SBU Use a standard straight network cable. For instructions how to configure the AVIATOR 700 system see SBU Configuration tasks on page 6-13. Pin-out for SBU Maintenance connector Pin no. Pin Name TxD+ input TxD- input RxD+ output Not Used...
Page 90: Sbu Rear Receptacle
TT-5040A SBU 4.3.3 SBU rear receptacle Connector drawing The following drawing shows the SBU rear receptacle and mating plug. Figure 4-5: SBU rear receptacle, engaging end (Index code: 19) 4-14 Chapter 4: Connectors and pin-out 98-124743-G...
Page 91: Figure 4-6: Sbu Rear Receptacle With Pin Functions
TT-5040A SBU Connector drawing with functions The following drawing shows the SBU rear receptacle with pin functions. For wiring details of this interface see Electrical installation and wiring on page 5-9. Figure 4-6: SBU rear receptacle with pin functions 98-124743-G Chapter 4: Connectors and pin-out 4-15...
Page 92 TT-5040A SBU Connector functions, top plug The top plug of the SBU rear receptacle connects the following signals: Power & RF Interfaces: • +28 V DC and GND, Power return • RF Tx signal to 405038A-002 HSU Tx Coupler • RF Rx signal from 405038A-003 HSU Rx Power Splitter •...
Page 93: Table 4-7: Pin-Out For Sbu Rear Receptacle, Top Plug
TT-5040A SBU Pin-out for SBU rear receptacle (top plug) Function Function TP14 Spare I/O, (Discrete I/O) TP A1 RF TX output to 405038A-002 HSU TX Coupler ISDN #2 Tx+ (c) output (TE)  TP15 Do not connect! TP A2 WLAN antenna #2 (coax) ISDN #2 Rx+ (d) input (TE) ...
Page 94: Table 4-8: Pin-Out For Sbu Rear Receptacle, Bottom Plug
TT-5040A SBU Pin-out for SBU rear receptacle (bottom plug) Pin no. Pin name Pin no. Pin name Data from secondary ARINC429 BP A1.1 Tx+ 10/100BaseT Ethernet #1 (Quadrax navigational input, A pin 1, Input) Data from primary ARINC429 BP A1.2 Rx+ 10/100BaseT Ethernet #1 (Quadrax navigational input, B pin 2, Output) Data from BSU or CMU, reserved,...
Page 95: Cradle Connectors For Handsets
Cradle connectors for handsets Cradle connectors for handsets For details on AVIATOR Wireless Handset cradle connectors, see AVIATOR Wireless Handset and Cradle Installation & Maintenance Manual, 98-129600. 4.4.1 Connectors on 4-Wire Cradle There are four connectors on the 4-Wire Cradle, two on the side of the cradle and two at the end: 4-Wire Handset connection SDU connection...
Page 96: 4-Wire Connector To Sdu
Cradle connectors for handsets 4.4.2 4-wire connector to SDU Connector drawing Figure 4-9: 4-Wire Cradle Connector (DB15M). View: Solder Side Functions The 15 pin Sub-D male connector on the short cable at the end of the 4-Wire Cradle connects the following signals on the SDU: Handset interface (analog): •...
Page 97: Table 4-9: Pin-Out For 15 Pin Sub-D Male Connector On Short Cable In 4-Wire Cradle
Cradle connectors for handsets Pin-out for DB15 connector The 4-Wire Cradle connector for connection to the SDU has the following pin-out: Function Function 2-Wire Tip (Fax/PC_modem/Auxiliary) 2-Wire Ring RS-485 Data A (Fax/PC_modem/Auxiliary) RS-485 Data B +28 V DC SDU Audio out + GND, Power Return SDU Audio out - SDU Audio in +...
Page 98: Connectors On 2-Wire Cradle
Cradle connectors for handsets 4.4.3 Connectors on 2-Wire Cradle There are three connectors on the 2-Wire Cradle, one at the side and two at the end: 2-Wire Handset connection SDU connection Figure 4-10: 2-Wire Cradle connectors, end view of cradle 2-Wire Voice/Fax/Modem/secure voice connection Figure 4-11: TT-5622B 2-Wire Cradle connectors, side view of cradle 4.4.4...
Page 99: Table 4-10: Pin-Out For 9 Pin Sub-D Male Connector In Tt-5622B 2-Wire Cradle
Cradle connectors for handsets Connector functions The 9 pin Sub-D male connector on the short cable at the end of the 2-Wire Cradle connects the following signals on the SDU or SBU: • Analogue 2-wire standard POTS interface for Voice/Fax/Modem/secure voice. Pin-out for 2-Wire Cradle connector to SBU The 2-Wire Cradle connector to connect to the SDU has the following pin-out: Function...
Page 100: Mating Connectors In Aircraft
Mating connectors in aircraft Mating connectors in aircraft 4.5.1 Connection with SDU The installation requires the following mating connectors in the aircraft. Note that the SDU tray holds the mating connector for the SDU rear connector. Connector Mating Connector Type Front Panel 15 pin SUB-D male Connector...
Page 101: Connection With Hpa
Mating connectors in aircraft 4.5.2 Connection with HPA The installation tray for the HPA is equipped with the following connector: Connector Mating Connector Type Rear ARINC 404 shell size 2 plug with the following contact arrangements: Connector Insert A (Top Plug): MC2 •...
Page 102 Mating connectors in aircraft 4-26 Chapter 4: Connectors and pin-out 98-124743-G...
Page 103: Chapter 5 Installation
This manual and the drawings and wiring diagrams contained herein may not be used as a substitute for an STC. To ensure optimal performance from the AVIATOR 700 system, you must Note maintain strict adherence to the installation guidelines in this chapter.
Page 104: Minimum System Components
• one antenna system with DNLA type F. As antenna system, use either an ARINC 741 or ARINC 781 compatible system or an HGA-6000, HGA-6500 or HGA-7000 antenna system. The following drawing shows the minimum installation required in the AVIATOR 700 system. Chapter 5: Installation...
Page 105: Figure 5-1: Aviator 700 Minimum System
Electrical installation and wiring on page 5-9 and onwards. Figure 5-1: AVIATOR 700 minimum system For navigational input we recommend to use input from an IRS/AHRS navigation system. This example includes an ARINC 741 antenna system, but the antenna system Note may as well be e.g.
Page 106: To Upgrade Your Installation From Aero-Hsd + To Aviator 700
To upgrade your installation from Aero-HSD to AVIATOR 700 The Aero-HSD+ system can be upgraded to an AVIATOR 700 system. To make the upgrade you replace the HSU with an SBU. The upgrade procedure is described in detail in the appendix Upgrade from Aero-HSD+ to AVIATOR 700 on page C-1.
Page 107: Mounting Considerations
Overview For optimum system performance, some guidelines on where to install or mount the components of the AVIATOR 700 system must be followed. Mounting and placement details are included in this section. For information on requirements to cables, see the individual sections in Electrical installation and wiring on page 5-9.
Page 108: Hpa
5-24. 5.2.6 Satcom antenna In order to steer the satcom antenna towards the satellite, the AVIATOR 700 system needs to know the position and attitude of the aircraft. Several methods are available to achieve this. About satcom antenna steering •...
Page 109: General Mounting Considerations
Mounting considerations Satcom antenna types supported For a list of Cobham antenna types supported in the AVIATOR 700 system see Satcom antenna systems on page 2-8. An AVIATOR 700 system must only be used with satcom antennas that have received type approval by Inmarsat.
Page 110: Wlan Antennas
5.2.7 WLAN antennas The recommended WLAN antenna to use with the AVIATOR 700 system is the TT5040A-004 Wireless Antenna. The WLAN antenna is PMA approved by VT Miltope (P/N 901167-2). You may also use other WLAN antennas approved for aeronautical use.
Page 111: Electrical Installation And Wiring
Electrical installation and wiring Electrical installation and wiring 5.3.1 Wiring symbols Throughout the wiring section these common symbols are used: Coax Shield Ground (fuselage) Twisted Twisted and shielded Table 5-2: Wiring symbols Each wiring drawing in this chapter only shows the connections referred to in Important that particular section.
Page 112: Wiring Sdu To Sbu
Electrical installation and wiring 5.3.2 Wiring SDU to SBU SDU pin SBU pin Description with reference to SDU BP56 SBU Enable BP73 TP20 Data bus input from SBU; Input A, RS422 BP72 TP19 Data bus input from SBU; Input B, RS422 BP71 TP22 Data bus output to SBU;...
Page 113: Table 5-4: Pins For Sdu Power Supply
Electrical installation and wiring Pins for SDU power supply The following list shows the pins used for the SDU power supply. SDU pin Name Description +28 V DC Power +28 V DC Power input from Aircraft power bus. GND, Power Return Aircraft Ground connection Chassis Ground and ...
Page 114: Figure 5-5: Wiring Hpa Power Supply
Electrical installation and wiring Cable requirements, SDU power supply Cable Max. Resistance Other Requirements [1] 200 m, (+28 V DC) incl. circuit breaker [2] 25 m The cable should be as short as possible. (GND, Power Return) [3] 25 m Connect directly to aircraft chassis.
Page 115: Table 5-6: Pins For Hpa Power Supply
Electrical installation and wiring Pins for HPA power supply The following list shows the pins used for the HPA power supply. HPA pin Name Description BP A1 +28 V DC Power +28 V DC Power input from Aircraft power bus. BP A2 GND, Power Return Aircraft ground connection.
Page 116: Figure 5-6: Wiring Sbu Power Supply
Figure 5-6: Wiring SBU power supply SBU maximum power consumption In the AVIATOR 700 system the SBU does not supply power for neither the HPA nor external satcom antennas. See Table A-3 on page A-6 for the total power consumption of the SBU (including CM).
Page 117: Table 5-9: Pins For Sbu Power Supply
Electrical installation and wiring Pins for SBU power supply The following list shows the pins used for the SBU power supply. SBU pin Name Description +28 V DC Power +28 V DC Power input from Aircraft power bus. GND, Power Return Aircraft Ground connection Chassis Ground Chassis connection, connected to installation tray...
Page 118: Wiring The Satcom Antenna
Aero-SDU Configuration Program and Configure RF settings of the SBU on page 6-50. Selection of DLNA Use the 405013A DLNA Type F. The DLNA used in the AVIATOR 700 system must contain improved Tx- Important filtering for protection of the GNSS and Iridium band. 5-16...
Page 119: Figure 5-7: Wiring Amt-50 Subsystem
An example of an ARINC 741 antenna system is the AMT-50 system. The following drawing shows the wiring for an AVIATOR 700 system using an AMT-50 antenna. In an AVIATOR 700 system, the DLNA must be ARINC 781 Type F compatible and Note contain extra TX-filtering for protection of the GNSS and Iridium band.
Page 120: Table 5-11: Sbu Pins For Amt-50 Antenna Subsystem
Electrical installation and wiring Pins for ARINC 741 antenna system The following lists show the SBU, SDU and HPA pins in the AVIATOR 700 system used for connecting an ARINC 741 antenna system. SBU pin Description TP A1 RF Tx output to Tx Coupler (HSU port)
Page 121: Table 5-13: Hpa Pins For Arinc 741 Antenna System
Electrical installation and wiring HPA pin Description RF Tx output to DLNA RF Tx input from Tx Coupler Remote nOn/Off input from SDU A429 Tx A output to ACU/BSU A429 Tx B output to ACU/BSU BP13 A429 Rx1 A input from ACU/BSU BP14 A429 Rx1 B input from ACU/BSU BP25...
Page 122: Table 5-14: Requirements To Rf Cables, Arinc 741 Antenna Systems
Electrical installation and wiring RF cable requirements, ARINC 741 antenna system Cable Min. Cable Loss @1.6 GHz Max. Cable Loss@1.6 GHz W3 0 dB 0.3 dB (DLNA to Antenna) W3 + DLNA loss + W4 0 dB Total: 2.6 dB W5a + Splitter loss + W5b 6 dB 29 dB W5a + Splitter loss + W5c 6 dB...
Page 123: Figure 5-8: Wiring Arinc 741 Dual Side Panel Antenna System
Electrical installation and wiring Wiring ARINC 741 dual side panel antenna system The following drawing shows the wiring of an ARINC 741 dual side panel antenna system. Figure 5-8: Wiring ARINC 741 dual side panel antenna system Remember to select ARINC741 Dual Panel Antenna in the Configuration Important program under Installation >...
Page 124: Table 5-15: Hpa Pins For Dual Side Panel Antenna System
Electrical installation and wiring Pins for Dual Side Panel antenna system The following list shows the pins in the AVIATOR 700 system used for connecting a Dual Side Panel antenna system. HPA pin Name/Description RF Tx output to HPR RF Tx input from SDU...
Page 125: Table 5-16: Sdu Pins For Dual Side Panel Antenna System
Electrical installation and wiring SDU pin Name/Description TP A1 RF Rx input from RX Power Splitter (SDU port) TP A2 RF Tx output to Tx Coupler (SDU port) BP56 SBU Enable output (active low) BP57 HPA remote nOn/Off output BP70 Data bus output to SBU;...
Page 126: Figure 5-9: Wiring Arinc 781 Antenna System
Electrical installation and wiring Wiring ARINC 781 antenna systems The following drawing shows the wiring for an AVIATOR 700 system using an ARINC 781 antenna system. Requirements to the cables are stated on the drawing and in the next section RF cable requirements, ARINC 781 antenna systems.
Page 127: Table 5-18: Sbu Pins For Arinc 781 Antenna System
Electrical installation and wiring Pins for ARINC 781 antenna system The following lists show the SBU, SDU and HPA pins in the AVIATOR 700 system used for connecting an ARINC 781 antenna system. SBU pin Description TP A1 RF Tx output to Tx Coupler (SBU port)
Page 128: Table 5-20: Hpa Pins For Arinc 781 Antenna System
Electrical installation and wiring HPA pin Description RF Tx output to DLNA RF Tx input from Tx Coupler (HPA port) Remote nOn/Off input from SDU A429 Tx A output to ARINC 781 antenna A429 Tx B output to ARINC 781 antenna BP13 A429 Rx1 A input from ARINC 781 antenna BP14...
Page 129: Figure 5-10: Wiring Hga-7000 Antenna System
Electrical installation and wiring Wiring HGA 7000 antenna system Figure 5-10: Wiring HGA-7000 antenna system 98-124743-G Chapter 5: Installation 5-27...
Page 130: Table 5-21: Sbu Pins For Hga 7000 Antenna System
Electrical installation and wiring Pins for HGA-7000 antenna system The following lists show the SBU, SDU and HPA pins in the AVIATOR 700 system used for connecting an HGA 7000 antenna system. SBU pin Description TP A1 RF Tx output to Tx Coupler (SBU port)
Page 131: Table 5-23: Hpa Pins For Hga 7000 Antenna System
Electrical installation and wiring HPA pin Description RF Tx output to DLNA RF Tx input from Tx Coupler (HPA port) Remote nOn/Off input from SDU A429 Tx A output to ARINC 781 antenna A429 Tx B output to ARINC 781 antenna BP13 A429 Rx1 A input from ARINC 781 antenna BP14...
Page 132: Table 5-24: Requirements To Rf Cables, Arinc 781 Antenna Systems
Electrical installation and wiring RF cable requirements, ARINC 781 antenna systems Cable Min. Cable Loss @1.6 GHz Max. Cable Loss@1.6 GHz W3 0 dB 0.3 dB (DLNA to Antenna) W3 + DLNA loss + W4 0 dB Total: 2.6 dB W5a + Splitter loss + W5b 6 dB 29 dB W5a + Splitter loss + W5c 6 dB...
Page 133: Wiring Arinc 429 Interfaces
Electrical installation and wiring 5.3.5 Wiring ARINC 429 interfaces The source for navigational data over ARINC 429 can be either an IRS, AHRS or Note another navigational input compatible with the requirements in this section. Wiring an ARINC 429 source system The SDU has two ARINC 429 input interfaces for 2 NAV sources.
Page 134: Table 5-25: Sdu Pins For Irs And Ahars
Electrical installation and wiring Pins for AHRS/IRS for SDU The following list shows the pins used for AHRS or IRS: SDU Pin Name/Description BP26 Data from primary IRS 429 A /Data from primary AHRS 429 A BP27 Data from primary IRS 429 B /Data from primary AHRS 429 B BP28 Data from secondary IRS 429 A /Data from secondary AHRS 429 A BP29...
Page 135: Table 5-27: Arinc Data Format For Irs
1 Hz Table 5-27: ARINC data format for IRS a. The labels marked optional do not have an effect on the operation of the AVIATOR 700 system, but may increase precision in the antenna pointing and time management. ARINC data format for AHRS...
Page 136: Figure 5-13: Wiring Acars/Afis/Cmu
Electrical installation and wiring Wiring ACARS/AFIS/CMU The SDU has ARINC 429 interfaces for 2 high or low speed (HS/LS) ACARS/AFIS/CMU including one output port and 2 input ports. The following drawing shows the wiring of ACARS/AFIS/CMU. Requirements to the cables are stated in the section Cable requirements, ARINC 429 on page 5-35.
Page 137: Figure 5-14: Wiring Mcdu
Electrical installation and wiring Wiring MCDU The SDU has interfaces prepared for two high or low speed ARINC 429 interfaces for communication with MCDU #1 and MCDU #2. One common output and two inputs. The following drawing shows the wiring of MCDU. Requirements to the cables are stated in the section Cable requirements, ARINC 429 on page 5-35.
Page 138: Wiring Gps Interface
Electrical installation and wiring 5.3.6 Wiring GPS interface Wiring the GPS antenna The following figure shows the wiring of the GPS interface when using a power splitter. You can use the power splitter shown in TT-5038A-003 Rx Power Splitter on page 3-8. Figure 5-15: Wiring GPS Interface with Power Splitter Pins for input from the GPS antenna SBU pin Name/description...
Page 139: Wiring Icao Address
24 discrete inputs on the SDU). The strapped ICAO address is compared to the ICAO address entered in the Configuration Module of the SDU. If they do not match, the AVIATOR 700 system suspends all RF communication.
Page 140 When the system is powered, the SDU reads the strapped ICAO address from the SDU rack connector and compares it to the ICAO address entered in the Configuration Module. If the SDU does not detect or recognize the strapped ICAO address, the AVIATOR 700 system suspends all RF communication until the error is corrected.
Page 141: Wiring Ethernet At The Sbu
Electrical installation and wiring 5.3.8 Wiring Ethernet at the SBU Overview The SBU has six 10/100BaseT Ethernet interfaces, plus the interface on the front of the SBU described in Wiring the maintenance interfaces and Reset on page 5-75. The following drawing shows the wiring of the rear SBU Ethernet interfaces. Figure 5-18: Wiring Ethernet The RJ45 Ethernet interfaces match a standard straight network cable.
Page 142: Table 5-32: Sbu Pins For 10/100Baset Ethernet
Electrical installation and wiring Pins for 10/100BaseT Ethernet The following list shows the pins used for the Ethernet interface. SBU pin Name Description RJ45 pin (F) Name BP A1.1 Tx+ 10/100BaseT Ethernet #1 Input TxD+ BP A1.2 Rx+ 10/100BaseT Ethernet #1 Output RxD+ BP A1.3...
Page 143: Figure 5-19: Ethernet Pin Configuration For Sbu
Electrical installation and wiring SBU pin Name Description RJ45 pin (F) Name BP26 Rx+ 10/100BaseT Ethernet #5 Output RxD+ BP27 Common Signal GND for Ethernet GND Shield BP28 Tx+ 10/100BaseT Ethernet #6 Input TxD+ BP29 Rx+ 10/100BaseT Ethernet #6 Output RxD+ Table 5-32: SBU Pins for 10/100BaseT Ethernet (Continued) Wiring of RJ45 connector to Quadrax connector...
Page 144: Wiring Wlan Antenna Interface
Electrical installation and wiring 5.3.9 Wiring WLAN antenna interface Before wiring the WLAN antenna interface make sure that your system has the Built-in Wireless Option 405040A-003. Overview The following drawing shows the wiring of the SBU WLAN antenna interfaces. Figure 5-20: Wiring WLAN antenna interfaces #1 and #2 If you have installed the wireless option 405040A-003, and TP5 (WLAN enable) is Note not connected to Ground at startup, the Pass/Fail LED of the SBU will be flashing...
Page 145: Table 5-34: Wlan Antenna Configuration
Electrical installation and wiring Not all countries allow full use of all channels. Also, some countries do not allow operation according to the 802.11g standard. Therefore the WLAN interface must be set up to the right country code. For further information, see WLAN country codes on page E-1. The maximum EIRP output level for WLAN 802.11b and 802.11g is 100 mW for indoors use.
Page 146: Wiring Isdn
Wiring ISDN Wiring drawing Figure 5-21: Wiring ISDN Note that even though the AVIATOR 700 system supports connection of several ISDN devices, the satellite channel only supports transmission on one ISDN channel. Pins for ISDN The following lists show the pins used for the ISDN interfaces on the SBU and the SDU.
Page 147: Figure 5-22: Isdn Rj45 Connector
Electrical installation and wiring SDU pin Name/Description BP67 ISDN Tx+ output (d) BP68 ISDN Tx- output (e) BP66 ISDN Rx+ input (c) BP69 ISDN Rx- input (f) Table 5-37: SDU pins for ISDN Description of SBU and SDU ISDN interface The SBU and SDU have one ISDN interface each.
Page 148: Wiring Telephone Systems
Wiring telephone systems Built-in Private Branch Exchange (PBX) The AVIATOR 700 system has two built-in PBX systems: one in the SDU and one in the SBU. • The PBX of the SDU controls four 4-wire audio interfaces, two 2-wire POTS interfaces and one ISDN interface.
Page 149: Isdn Interface
The maximum number of telephones on each 2-wire POTS interface is:  Two TT-5621B 2-Wire Handset / TT-5622B 2-Wire Cradle or two Sigma phones. The AVIATOR 700 system supports 3 external call at a time: 2 calls on H , 1 call on SwiftBroadband.
Page 150: Figure 5-23: Handset Interfaces, Possible Combinations Of Connected Devices
Electrical installation and wiring Configuration of wired handset interfaces The following drawing shows the possible combinations of devices connected to the handset interfaces. Figure 5-23: Handset interfaces, possible combinations of connected devices. 5-48 Chapter 5: Installation 98-124743-G...
Page 151: Figure 5-24: Wiring T&T 4-Wire Handset Systems
Electrical installation and wiring Wiring 4-Wire Handsets The following drawing shows the wiring of the TT-5622A/TT-5620A 4-Wire Handsets. Figure 5-24: Wiring T&T 4-Wire Handset systems 98-124743-G Chapter 5: Installation 5-49...
Page 152: Table 5-38: Sdu Pins For 4-Wire Interface
Electrical installation and wiring SDU pins for 4-wire interfaces Pin no. Name/Description TP10 Handset #1 Audio In Hi / Cockpit Voice Audio #1 In Hi TP11 Handset #1 Audio In Lo / Cockpit Voice Audio #1 In Lo TP12 Handset #1 Audio Out Hi / Cockpit Voice Audio #1 Out Hi TP13 Handset #1 Audio Out Lo / Cockpit Voice Audio #1 Out Lo BP94...
Page 153: Figure 5-25: Wiring T&T 2-Wire Handset Systems
Electrical installation and wiring Description of 4-wire interfaces The SDU has four 4-wire analog interfaces for the TT-5620A/ TT-5622A Thrane & Thrane aeronautical handset system on the rear connector. The handsets use an RS-485 data bus for on/off hook signalling, display control, keyboard control, background light, etc. AVIATOR 700D: For safety reasons do not install the 4-wire handset in the Important cabin, see also Mounting considerations, SDU on page 5-5.
Page 154: Table 5-39: Sdu Pins For 2-Wire Interface
Electrical installation and wiring Pins for 2-wire interfaces The below lists show the pins used for the 2-wire interfaces of the SDU and the SBU. SDU pin Name/Description 2-Wire Voice/Fax/Modem #1 (Ring) 2-Wire Voice/Fax/Modem #2 (Ring) 2-Wire Voice/Fax/Modem #2(Tip) TP19 2-Wire Voice/Fax/Modem #1 (Tip) Table 5-39: SDU pins for 2-wire interface SBU pin Name/Description...
Page 155: Wiring Wh-10 Handsets
Electrical installation and wiring 5.3.12 Wiring WH-10 handsets Overview The following drawing shows the wiring of WH-10 handsets. Figure 5-26: Wiring WH-10 handsets 98-124743-G Chapter 5: Installation 5-53...
Page 156: Table 5-41: Sdu Pins For Wh-10 Interface
Electrical installation and wiring WH-10 pins The below list shows the pins used for the WH-10 interfaces on the SDU. Pin no. Name/Description Chassis Ground and Handset Power Return +28 V DC/600 mA Handset Supply TP10 Handset #1 Audio In Hi / Cockpit Voice Audio #1 In Hi TP11 Handset #1 Audio In Lo / Cockpit Voice Audio #1 In Lo TP12...
Page 157: Discretes For Wh-10 Handset Systems
Electrical installation and wiring Description of WH-10 interfaces Up to three WH-10 systems can be connected to the AVIATOR 700 system, using the interfaces #1, #2 or #3. The 4-wire handset system #1, #2 and #3 interfaces are used for either the 4-Wire Note Handset system, MagnaStar, ICS-200, 2.4GHz Cordless or WH-10 phones, as...
Page 158: Wiring Ics-200 Telephone System
Electrical installation and wiring 5.3.14 Wiring ICS-200 telephone system When simultaneously operating the AVIATOR 700 over the Inmarsat network Important and the ICS-200 there is a potential risk of interference. Overview The following drawing shows the wiring of the ICS-200 telephone system.
Page 159: Table 5-43: Sdu Pins For Ics-200 Interface
Electrical installation and wiring Pins on SDU for ICS-200 telephone system The below list shows the pins used for the ICS-200 interface on the SDU. Pin no. Name/Description TP10 Handset #1 Audio In Hi TP11 Handset #1 Audio In Lo TP12 Handset #1 Audio Out Hi TP13...
Page 160 The Iridium Communication System ICS-200 can be connected to the SDU, providing the possibility of routing calls from the AVIATOR 700 system to the Iridium satellite network. The 4-wire handset system #1, #2 and #3 interfaces are used for either the 4-Wire Note Handset system, MagnaStar, ICS-200, 2.4GHz Cordless or WH-10 phones, as...
Page 161: Wiring 2.4Ghz Cordless (4-Wire) Phone
Electrical installation and wiring 5.3.15 Wiring 2.4GHz Cordless (4-wire) phone Overview The following drawing shows the wiring of 2.4GHz Cordless 4-wire phones. Figure 5-28: Wiring 2.4GHz Cordless 4-wire phones The power for the 2.4GHz Cordless base unit must be supplied from an external Note power supply.
Page 162: Table 5-44: Sdu Pins For 2.4Ghz Cordless (Wh-10) Interface
Electrical installation and wiring Pins for 2.4GHz Cordless (WH-10) interfaces The below list shows the pins used for the 2.4GHz Cordless (WH-10) interfaces on the SDU. Pin no. Name/Description TP10 Handset #1 Audio In Hi TP11 Handset #1 Audio In Lo TP12 Handset #1 Audio Out Hi TP13...
Page 163 Electrical installation and wiring Description of 2.4GHz Cordless interfaces Up to three 2.4GHz Cordless Handsets can be connected to the AVIATOR 700 system, using the interfaces #1, #2 or #3. The 4-wire handset system #1, #2 and #3 interfaces are used for either the 4-Wire Note Handset System, MagnaStar, 2.4GHz Cordless or WH-10 phones, as configurations...
Page 164: Wiring Sigma 7 (2-Wire) Handsets
Electrical installation and wiring 5.3.16 Wiring Sigma (2-wire) handsets One to four Sigma handsets can be connected to the 2-wire interfaces of the AVIATOR 700 system. The following drawing shows the wiring of Sigma handsets. Figure 5-29: Wiring Sigma handsets The above wiring shows the connection for the non-backlit Sigma handset.
Page 165: Wiring Icg Dect Cordless Handset (2-Wire) Phone
Wiring ICG DECT Cordless Handset (2-wire) phone One to four ICG DECT Cordless Handset phones can be connected to the 2-wire interfaces of the AVIATOR 700 system. The following drawing shows the wiring of ICG DECT Cordless Handset 2-wire phones.
Page 166: Wiring Discretes
Electrical installation and wiring 5.3.18 Wiring discretes Discrete annunciators, Chime/Lamps Inhibit and WOW The following drawing shows the wiring of discrete annunciators, Chime/Lamps Inhibit and Weight-on-Wheels (WOW). Figure 5-31: Wiring discrete annunciators and Weight-on-Wheels Pins for discrete annunciators The following list shows the pins used for discrete annunciators: Specification of discrete SDU Pin Name/Description...
Page 167: Table 5-46: Sbu Pins For Discrete Annunciators
Electrical installation and wiring SBU pin Name and description Discrete type TP27 Annunciator #3 “Service available” (Discrete I/O) Output: Lamp Driver TP28 Annunciator #1 “Incoming call” (Discrete I/O) Output: Lamp Driver TP29 Annunciator #2 “SBU failed” (Discrete I/O) Output: Lamp Driver Annunciator #4 “Message received”...
Page 168: Table 5-47: Sdu Pin For Chime/Lamps Inhibit Input
Electrical installation and wiring Pins for Chime/Lamps Inhibit input Pins used for the Chime/Lamps Inhibit input: SDU Pin Name/Description Specification of discrete type BP88 Chime/Lamps Inhibit Input Input: WOW (active low) Table 5-47: SDU Pin for Chime/Lamps Inhibit input a. The discrete interfaces are described in Description of the discrete types on page 5-67. SBU pin Name/description Specification of discrete type...
Page 169: Table 5-50: Sbu Pins For Discrete Inputs
Electrical installation and wiring Pins for non-configurable discrete inputs on the SBU The SBU has two non-configurable discrete inputs: one for SBU nON, one for WLAN Enable. The below table shows the pin-out for the discrete inputs: SBU pin Name/description SBU nON input WLAN Enable input Table 5-50: SBU pins for discrete inputs...
Page 170: Wiring Cockpit Voice Interface
Electrical installation and wiring 5.3.19 Wiring Cockpit Voice interface Introduction The Cockpit Voice interface must be wired to the Audio Management System (AMS) and an Audio Control Panel (ACP) or similar. Figure 5-32: shows a typical Cockpit Voice installation. Pay attention to the drawing notes: NOTES: [1] The balanced audio outputs from the SDU (TP10, TP11, TP17 and TP18) are not transformer coupled.
Page 171 Electrical installation and wiring Typical Cockpit Voice installation Figure 5-32: Typical Cockpit Voice installation 98-124743-G Chapter 5: Installation 5-69...
Page 172 Electrical installation and wiring Cockpit Voice with unbalanced AMS audio interface Figure 5-33: Typical Cockpit Voice installation with unbalanced AMS audio interface 5-70 Chapter 5: Installation 98-124743-G...
Page 173: Table 5-53: Universal Interface Amplifier Model 270-16 Settings
Electrical installation and wiring NAT, Universal Interface Amplifier model 270-16 settings Switch/Jumper/ NAT, Universal Interface Amplifier model 270-16 settings Adjustment ID 9V bias, MS3 The SDU does not provide microphone DC power. If the microphone needs DC-power, and if the AMS does not provide DC power this switch shall be set to "9V bias".
Page 174: Table 5-54: Universal Interface Amplifier Model Aa34-300 Settings
Electrical installation and wiring NAT, Universal Interface Amplifier model AA34-300 settings Switch/Jumper/ NAT, Universal Interface Amplifier model AA34-300 settings Adjustment ID Microphone DC bias, S1 The SDU does not provide microphone DC power. If the microphone needs DC-power, and if the AMS does not provide DC power this switch shall be set to "closed".
Page 175: Table 5-55: Sdu Pins For Cockpit Voice Interface
Electrical installation and wiring SDU pins for Cockpit Voice SDU Pin Name/Description Specification BP52 CP Voice Chime Signal Contact #1; Relay type, forms a circuit closure Current from Chime between BP52 and BP53 BP53 CP Voice Chime Signal Contact #2; Relay type, forms a circuit closure Current to Chime between BP52 and BP53...
Page 176 Electrical installation and wiring Description of the Cockpit Voice interface CP Voice Chime Signal Contact #1/#2 (BP52, BP53) The solid state relay drives a chime, that is sounded on incoming calls (ground-to-air call), and per configuration on outgoing calls (air-to-ground calls), when the line is connected and ready (single stroke or multi stroke chime).
Page 177: Wiring The Maintenance Interfaces And Reset
Electrical installation and wiring 5.3.20 Wiring the maintenance interfaces and Reset Make sure that there is no cable connected to the SDU or SBU Maintenance Important connector when the aircraft is airborne. Maintenance PC, CM Write Enable, SDU Reset and ATE The following drawing shows the wiring of: •...
Page 178: Table 5-56: Sdu Pins For Rs-232 Pc Interface
Electrical installation and wiring Pins for SDU RS-232 Maintenance PC interface and CM Write Enable (SDU) The following list shows the SDU pins used for RS-232 PC interface and for CM Write Enable. Both interfaces are included in the TT 37-112940 data cable described at the end of this section.
Page 179: Table 5-57: Sbu Pins For Maintenance Interface
Electrical installation and wiring The following drawing shows the wiring of the maintenance cable for the SDU front connector. Figure 5-35: TT 37-112940 maintenance cable for front connector on SDU and PC Pins for the Maintenance interface on SBU The following list shows the pins used for the Maintenance interface on the SBU. SBU pin Name/Description TxD+...
Page 180 Electrical installation and wiring Reset The SDU has a discrete input (BP77) on the rear connector, which can be used for SDU hardware reset. The specification complies with the discrete WOW input. You only need to connect this input if you have special requirements to the reset Note function.
Page 181: Table 5-58: Sdu Pins For Maintenance Handset Interface
Electrical installation and wiring Pins for Maintenance handset interface The following list shows the pins used for maintenance handset interface. SDU Pin Function: Handset Interface Maintenance Handset Audio In Hi Maintenance Handset Audio In Lo Maintenance Handset Audio Out Hi Maintenance Handset Audio Out Lo Maintenance Handset RS-485 Data A Maintenance Handset RS-485 Data B...
Page 182: Recommended Cables
Recommended cables Recommended cables 5.4.1 Introduction This section lists recommended cables and allowed cable lengths for the cables in the AVIATOR 700 system. For specific requirements to the cables, see the applicable section in Important 5.3 Electrical installation and wiring. 5.4.2...
Page 183: Table 5-60: Allowed Lengths For Hpa Power Cables
Recommended cables Allowed cable lengths, HPA The following table shows the allowed HPA cable lengths for selected AWG types. If other AWG types are used, make sure the contact type supports the AWG type. It is generally recommended to keep cable lengths as short as possible, specially Note on cables for Chassis.
Page 184: Recommended Power Cables
Recommended cables Allowed cable lengths, SBU The following table shows the allowed SBU cable lengths for selected AWG types. If other AWG types are used, make sure the contact type supports the AWG type. It is generally recommended to keep cable lengths as short as possible, specially Note on cables for Chassis GND.
Page 185: Recommended Rf Cables
Recommended cables 5.4.4 Recommended RF cables The following cable types are recommended for the RF cables. Contact your cable supplier for other cable types. Equivalent cable types, which meet the requirements, may also be used. Note CABLE TYPE SPECIFICATIONS Attenuation  Size 5 Diameter...
Page 186: Recommended Cables For Arinc 429
Recommended cables Cable from SBU to WLAN antenna W5 and W6 Cable Maximum Size 5 Attenuation Part number diameter cable contact (dB/100 ft) (mm/in.) length part number ECS 311501 5.82/0.229 10.7 dB 46 ft (14 m) P922 EMTEQ PFLX195-500 5.08/0.2 16.81 30 ft (9 m) A45195-1...
Page 187: Verifying The Installation
5.6.1 The 3 ID numbers for the AVIATOR 700 system The AVIATOR 700 system is a hybrid system with 3 individual parts. Each part uses different Inmarsat services and therefore has its own ID number in the Inmarsat network. Format...
Page 188 Cobham and is printed on the label of the SDU configuration module (CM). Note the CM has 2 ISN. Make sure to use the one marked SDU ISN for AVIATOR 700. The ISN can also be seen in the Aero-SDU Configuration Program under the Commissioning IDs.
Page 189: Service Providers
Activation of airtime services Service providers You find a list of Service providers on Inmarsat’s web site, Partner search (http://www.inmarsat.com/partners/search-for-partner/). 98-124743-G Chapter 5: Installation 5-87...
Page 190 Activation of airtime services 5-88 Chapter 5: Installation 98-124743-G...

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