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COMPONENT MAINTENANCE MANUAL

AIRBUS IRIDIUM SATCOM SYSTEM

AIRBUS IRIDIUM SATCOM SYSTEM

IRIDIUM SATCOM SYSTEM

PART NUMBERS

SDU - 228E5733-00

SCM - 418E5733-00

COMPONENT MAINTENANCE MANUAL

WITH

ILLUSTRATED PARTS LIST

P/N: 165E5733-10

IN ACCORDANCE WITH

TSO C-159a

VENDOR CODE: 06141

23-28-01

Revision 1
Jan. 21/14

Summary of Contents for SDU L-3

Page 1: ...Iridium Iridium Welcome Welcome Package Package Package Package Airbus Iridium SATCOM System...

Page 2: ...The AFIRS 228 SDU includes telecom functions integrated into the cockpit audio system for the flight crew and separate calling capability through conventional two wire tip and ring telephony devices...

Page 3: ...ut L 3 products please visit the company s website at http www l 3ar com This Welcome Package includes the following useful information for you to obtain support for effective operation of your Iridiu...

Page 4: ...these documents may not be the latest up to date revisions Please check the L 3 Customer Support website for the latest update available at http www l 3ar com customer index htm Documents Welcome Let...

Page 5: ...li l 3com com Technical Technical Mike Phillips Documentation Documentation For access to Technical documentation please log on to Website http www l 3ar com customer technical htm For specific reques...

Page 6: ...ervice facility will be established later in 2014 Until such time all Iridium repairs will be performed at L 3 Factory Address L 3 Communications Aviation Recorders 100 Cattlemen Rd Sarasota Florida 3...

Page 7: ...Iridium SATCOM System L 3 Aviation Recorders Proprietary 165E5733 01 Rev 02 7 March 2014 Page 1 Airbus Iridium SATCOM System Quick Start Guide SDU L 3 part number 228E5733 00 SCM L 3 part number 418E5...

Page 8: ...ft s Air Traffic Service Unit ATSU and the other prioritized for voice via a certified terrestrial service provider The Automated Flight Information Reporting System AFIRS provides a satellite voice a...

Page 9: ...atellite Data Unit SDU 2 SDU Configuration Module SCM The SCM is housed in a small enclosure which is designed to be mounted within 24 of the SDU rear connector The SCM and antenna connect directly to...

Page 10: ...the front panel of the SDU IMPORTANT READ BEFORE CONFIGURING SATCOM SYSTEM The MUI only accepts English language characters and numbers The aircraft s status must be deemed On Ground to access Mainte...

Page 11: ...rders Proprietary 165E5733 01 Rev 02 7 March 2014 Page 5 1 Install SIM Card 1 Remove the four screws from the plate on the SCM 2 Remove the plate on the SCM to reveal the SIM enclosure 3 Slide the SIM...

Page 12: ...lide the SIM card in the slot It will fit only one way do not force 6 Close the SIM Enclosure and slide to the left to lock The SIM Card is now installed 7 Replace the plate 8 Replace the four screws...

Page 13: ...ommended 3 Confirm that the green link light is illuminated The light can be steady or flashing flashing means that data is being transmitted 4 Set the laptop network adapter to the following IP 192 1...

Page 14: ...w connected to the Airbus Iridium SATCOM System MUI Home Page type the following in the Login fields Default User Name AFIRSMAINT Default Password 228MAINT 2 Click Login 3 Click Enter Maintenance Mode...

Page 15: ...s from cockpit can be placed manually No Calls from cockpit can only be placed from address book Low Priority Calls Yes Low priority calls can be received made from cockpit No Low priority calls canno...

Page 16: ...e no list numbers in the adb csv file to identify individual entries Important The template adb csv entries must adhere to the parameters exactly Address Book Parameters Phone Number Up to 18 digits A...

Page 17: ...message displays prompting for confirmation to exit Maintenance Mode 14 Click OK The system saves changes reboots and returns to Operational Mode 15 Proceed to Enter Administrator Role below 7 Enter...

Page 18: ...ha numeric characters Password 4 20 upper case alpha numeric characters Security Level Data Collector default Maintenance Administrator Roles Privileges Modifications Software Data Loading Upload ORT...

Page 19: ...a backup UAT file that you could upload in the event that the system file should fail 1 On the Home Page type the following in the Login fields Default User Name AFIRSADMIN Default Password ADMIN228 2...

Page 20: ...Manual a Call from Landline Phone to Iridium SATCOM Phone NON ATS Air Traffic Service SIM 1 Call Iridium Call Service U S 1 480 768 2500 Non U S 001 480 768 2500 2 Enter Iridium 12 digit phone number...

Page 21: ...Page 15 b Call from Iridium SATCOM Phone to Landline Phone Manual 1 Select Manual Dial from the MCDU screen 2 Punch in the phone number and select the button directly next to the open field to popula...

Page 22: ...Call from Iridium SATCOM Phone to Landline Phone Directory IMPORTANT If manual dialing has been disabled the ability to use dual tone multi frequency signaling DTMF will also be disabled This means th...

Page 23: ...3 Locate the number to call 4 Initiate the call 2 Send Data Message from Iridium SATCOM 1 Go to the MCDU 2 Choose a free text and send a test message to Dispatch or Maintenance The system will automa...

Page 24: ...t Fault Event Never Red GPS Link Internal GPS Active Parameter Set to Inactive Operational Mode No Failure Fault Fault Event Never Red Ethernet Link for each port Not Used or Fault Steady Link OK Flas...

Page 25: ...red in the SC The SCM Compatibility Fault cannot be cleared once raised No N A N A Transition to Configuration Invalid State Verify software load in MUI Fault Light Discrete Output ON OFF L 3 Iridium...

Page 26: ...s below 18 0 V or above 32 2 V The Alternate Power Status will be cleared if the voltage at the Alternate Input is within an inclusive range of 18 0 V to 32 2 V Yes OK OK Check input voltage Comment L...

Page 27: ...f the system exits the System Low Yes OK OK Temperature is below 15 C NVM FAIL ISVM Elevated The System High Temperature Status The System High Yes OK OK Temperature is Comment L 3 Iridium SATCOM Syst...

Page 28: ...n with the ISVM AT port Yes FAIL OK Link should reestablish within a few minutes If link does not reestablish within 20 minute period replace SDU ISDM FAIL ISDM Communication Failure The Iridium Satel...

Page 29: ...is received for 4 seconds in a row over the port for which the Yes OK OK Verify ACARS 1 receiver data ACARS2 RX INACT ACARS 2 Receiver Port Inactive Fault The ACARS 2 Receiver Port Inactive Fault will...

Page 30: ...ved a recognized label with correct parity for 4 seconds in a row the port for which the MCDU 1 Receiver Port Inactive Fault was raised 3 A429 TXn FAIL n Port Number ARINC 429 Transmitter Port Loopbac...

Page 31: ...lt will be raised for any active RS 232 422 Serial Port for which a received data error is reported A raised RS 232 422 Receiver Fault will be cleared if the data is received without error over the po...

Page 32: ...te period replace Status Receiver reports no navigation solution for 5 seconds in a row reports a navigation solution for 5 seconds in a row minute period replace SDU If still present verify Iridium G...

Page 33: ...e of the system You may select any valid Iridium Service provider Our recommendation is to contact our partner FLYHT Aerospace Solutions Ltd complete the following activation form and send to FLYHT fo...

Page 34: ...Serial Number 3 Please select one of the following satcom voice service plan options AFIRS Global Voice Data Plan NON ATS Rate Billing Intervals Air to Ground 1 45 min USD 20 seconds Ground to Air 1 4...

Page 35: ...note you will require a separate agreement with your selected ACARS satcom data service provider 5 Contact information Primary contact Billing Contact if different Company Name Address email Phone The...

Page 36: ...the collection shall be deemed the date of payment Any check received from Buyer may be applied by Seller against any obligation owing from Buyer to Seller regardless of any statement appearing in or...

Page 37: ...vice based upon information supplied I understand that our company is responsible for all charges and services up till the date our account is properly cancelled through FLYHT and the Iridium network...

Page 38: ...Proprietary 100 Cattlemen Road Sarasota FL 34232 Installation Manual Airbus Iridium SATCOM System SDU L 3 part number 228E5733 00 SCM L 3 part number 418E5733 00 Publication Number 165E5733 00 Issue...

Page 39: ...rohibited without the prior written consent of the U S Department of Commerce HTSUS Schedule B 85439 09 000 This manual contains date sensitive information To verify the latest revision level of this...

Page 40: ...Sarasota FL 34232 Record of Revisions Rev Issue Date Description Pages By 00 01 November 2013 Initial issue All CM 01 15 December 2013 Corrected SDU SCM Top Level Part Numbers All CM SC 02 21 January...

Page 41: ...s 20 3 1 Satellite Data Unit SDU 20 3 1 1 General 21 3 1 2 Mechanical Specifications 21 3 1 3 Environmental Specifications Airbus Iridium SATCOM System 22 3 2 SDU Configuration Module SCM 22 3 2 1 Gen...

Page 42: ...SDU to Airbus CFDS 35 4 Installation Considerations 36 4 1 Satellite Data Unit SDU 36 4 2 SDU Configuration Module SCM 37 4 3 Iridium Antenna System 37 4 3 1 Antenna 37 4 3 2 Antenna Mounting 39 4 3 3...

Page 43: ...T 68 7 3 4 User Access Table UAT Parameters 68 7 4 Upgrading Airubs Iridium SATCOM System Software 70 7 4 1 Upgrade Materials 70 7 4 2 Upgrade Procedure 70 7 5 Exiting Maintenance Mode 73 8 Maintenanc...

Page 44: ...thernet Interface 48 Figure 6 7 Discrete Input Interfaces 50 Figure 6 8 Latched ACP Audio Interface 51 Figure 7 1 Maintenance Port Location 52 Figure 7 2 Home Page General Tab 54 Figure 7 3 Faults Pag...

Page 45: ...3 5 ARINC 429 Receiver Protocols CFDS 33 Table 3 6 ARINC 429 Receiver Protocols MCDU 33 Table 3 7 ARINC 429 Receiver Port Monitoring 34 Table 3 8 ARINC 429 Transmitter Protocols SDU ATSU FWC 34 Table...

Page 46: ...l Designation This manual covers model designation Airbus Iridium SATCOM System 1 2 1 Airbus Iridium SATCOM System The Airbus Iridium SATCOM System will be certified to TSO C 159a for voice and data s...

Page 47: ...System 14 ARINC 758 2 Communications Management Unit CMU Mark 2 15 ARINC 761 4 Second Generation Aviation Satellite Communication System Aircraft Installation Provisions 16 FAA TSO C 159a Technical St...

Page 48: ...quirements 31 ABD0100 1 7E Mechanical Requirements 32 ABD0100 1 8E Electrical and Installation Requirements 33 ABD0100 1 9H Electronic Equipment Design and Parts Requirements 34 ABD0100 1 10G Software...

Page 49: ...ce Process 52 ABD0100 3 0H Documentation Requirements 53 ABD0012G Supplies Tool and Test Equipment 54 ABD0031F Fire Smoke Toxicity 55 ABD0024E Aircraft MFR Tools and test equipment 56 ABD0046D Units o...

Page 50: ...em Airbus CNSSA Core Non Safety Services Application CTS Clear To Send DITS Digital Information Transfer System DTP Date Time Position EFB Electronic Flight Bag EIA Electronics Industry Association EL...

Page 51: ...n LGCIU Landing Gear Control Interface Unit LED Light Emitting Diode LRU Line Replaceable Unit LSK Line Select Key MCDU Multi Purpose Control and Display Unit MOPS Minimum Operational Performance Spec...

Page 52: ...le SDI Source Destination Identifier SDU Satellite Data Unit SIM Subscriber Identity Module SSA Safety Service Application SSM Signed Status Matrix SW Software TIA Telecommunications Industry Associat...

Page 53: ...nd ARINC 739A Multi Purpose Control and Display Units MCDUs in the cockpit as well as providing 3 extension Public Branch Exchange PBX capability for up to 2 handsets in the cabin Figure 2 1 Airbus Ir...

Page 54: ...hich are listed below and described in detail in this section Audio System Interface 1 ARINC 429 Transmitters 6 and Receivers 16 RS 232 422 Serial Ports 4 Ethernet Ports 4 Discrete Outputs 8 and Input...

Page 55: ...DO 214 Audio Integrating System e g Audio Panel in the aircraft Software selectable discrete inputs and outputs can be configured to support this interface e g Mic On Chime Chime Reset End Call functi...

Page 56: ...trol and display interactions particularly for voice functions Discrete inputs can also be used to determine the states of various aircraft systems when this information is not available on a databus...

Page 57: ...ection describes the mechanical and environmental specifications of the components of the Airbus Iridium SATCOM System 3 1 Satellite Data Unit SDU This section describes the mechanical and environment...

Page 58: ...ich is designed to be mounted in a standard ARINC 600 mounting tray See Figure 3 2 for an outline of this component Figure 3 2 SDU Outline Drawing dimensions in millimeters and inches 3 1 2 Mechanical...

Page 59: ...or environmental testing conditions categories and descriptions of the conducted tests of the SDU Note DO 160G Categories for the Airbus Iridium SATCOM System are as specified by the design Qualificat...

Page 60: ...600 mounting tray used for the SDU See Figure 3 4 for an outline of this component Figure 3 4 SCM Outline Drawing dimensions in millimeters and inches 3 2 2 Mechanical Specifications Dimensions 1 00...

Page 61: ...24 Figure 3 5 SCM Oblique View Note 1 Resistance between mounting plate and module not to exceed 20 milli ohms Also resistance between mounting plate and aircraft structure not to exceed 20 milli ohms...

Page 62: ...for environmental testing conditions categories and descriptions of the conducted tests of the SCM 3 3 Airbus Iridium SATCOM System Satellite Antenna The antenna is a Commercial Off the Shelf COTS un...

Page 63: ...al cable please see Section 4 3 4 which provides recommended coaxial cable types to be used which meet the Airbus Iridium SATCOM System requirements Figure 3 8 illustrates the Iridium antenna coaxial...

Page 64: ...t 3B Tx Ethernet 3B Rx 2 Ethernet 1A Rx Ethernet 1A Tx O Ethernet 2B Rx Ethernet 2B Tx O O Ethernet 3B Rx Ethernet 3B Tx 3 O O O O O O O O O O 4 O O O O O O O O O O 5 Ethernet 4B Tx Ethernet 4B Rx O O...

Page 65: ...RS232 Com No 4 RS232 Com 8 No 8 Discrete Input No 2 Discrete Output No 12 A429Rx A No 12 A429Rx B No 3 Discrete Output No 9 Discrete Input No 4 Discrete Output No 10 Discrete Input No 13 A429Rx A No...

Page 66: ...r Ground 4 20 Not Used 5 20 Not Used 6 20 Not Used 7 12 Not Used 8 12 Chassis Ground 9 16 Not Used 10 16 Not Used 11 16 Not Used 12 5 Not Used 13 5 Iridium GPS Antenna Figure 3 9 SDU Connector Map 3 5...

Page 67: ...M SDI Data Definition Software Selectable Protocols 3 5 5 Ethernet Quantity 4 Format 802 3 10BASE T 100BASE TX half and full duplex modes auto negotiated ARINC 664P2 Physical Layer 3 5 6 Discrete Inpu...

Page 68: ...output is either high impedance to ground Open or low impedance to ground Closed Each configurable discrete output is individually software configurable for the following Logic Assignment Active Low...

Page 69: ...op or Personal Computer with a standard web browser 3 7 SDU Configuration Module SCM The SCM and antenna connect directly to the SDU The SDU is the heart of the system and provides all of the interfac...

Page 70: ...Command ISO 5 120 ms 233 Flight Number 1 2 ISO 5 4 s 234 Flight Number 3 4 ISO 5 4 s 235 Flight Number 5 6 ISO 5 4 s 236 Flight Number 7 8 ISO 5 4 s 260 BCD Date YY MM DD BCD 1 s 301 Aircraft Identif...

Page 71: ...4 consecutive samples fail Table 3 7 ARINC 429 Receiver Port Monitoring Receiver Activity Label Min Update Rate ATSU FWC 270 1 Hz ARINC 739A MCDU 270 377 1 Hz Airbus CFDS 125 260 1 Hz 3 10 ARINC 429 T...

Page 72: ...er BCD 1 s 220 MCDU Address Label for MCDU 1 221 MCDU Address Label for MCDU 2 222 MCDU Address Label for MCDU 3 Table 3 10 ARINC 429 Transmitter Protocols SDU CFDS 3 10 3 From SDU to Airbus CFDS Dest...

Page 73: ...igure 4 1 shows a typical ARINC 600 2MCU tray used for the SDU Figure 4 1 2MCU Mounting Tray While the SDU does not require forced air cooling every attempt should be made to place the SDU in a benign...

Page 74: ...nith therefore the maximum attenuation in the rest of the antenna system must be less than 3 dB If an antenna with a different gain is selected the maximum loss of the rest of the antenna system must...

Page 75: ...60068 ISO 2669 and the applicable ABDs unless otherwise noted Temperature 55 C 67 F to 85 C 185 F Altitude 100 to 55 000 FT Vibration 10 G s DO 160D E F2 AB Electrical Specifications Frequency 1616 0...

Page 76: ...frequency range from 1565 MHz to 1626 5 MHz for Iridium transmit receive operations and GPS reception It is a low loss aircraft grade cable that will be mounted in the aircraft fuselage This cable pro...

Page 77: ...3 9 95 m 392 0 inches Diameter 8 1 mm 0 317 inches Manufacturer s Specification Reference Number Drawing 024E5733 00 Revision B Iridium Antenna Coax Cable see Figure 4 4 Iridium SATCOM System Supplier...

Page 78: ...required as part of a typical Airbus Iridium SATCOM System installation Note The system integrator is responsible to ensure that all installation materials used meet the regulatory requirements for th...

Page 79: ...Keep shield drains and unshielded conductor lengths as short as practicable 3 6 2 Primary Power Antenna and SCM The primary power antenna and SCM connections shown in Figure 6 1 are required for all A...

Page 80: ...er ports None ACARS 1 ACARS 2 Airbus CFDS A739 MCDU 1 A739 MCDU 2 A739 MCDU 3 When an input is not connected to an active system e g no connection or wiring provisions only are installed the port shou...

Page 81: ...Rev 02 21 January 2014 Page 44 6 4 MCDU If an ARINC 739A MCDU is installed MCDU 1 should be connected to ARINC 429 Tx 1 and ARINC 429 Rx 1 For MCDU 2 and 3 ARINC 429 Rx ports 2 and 3 are used as shown...

Page 82: ...erface provides safety services data functionality for the Airbus Iridium SATCOM System It is recommended that if the ACARS ATSU ARINC 429 Rx connection will not be utilized that the wires be capped a...

Page 83: ...d events Date time and position information is provided by the system s internal GPS 6 8 RS 232 422 Databus The Airbus Iridium SATCOM System has four serial ports transmit and receive Each port is sof...

Page 84: ...struction but a twisted pair cable construction can generally also be used For star quad cables the conductor lay order should be maintained without crossing the conductors when terminating For twiste...

Page 85: ...l Interface Unit LGCIU1 input When there is only one LGCIU input i e the LGCIU2 function is not assigned to a Discrete Input see 6 10 2 and the LGCIU1 input transitions to the active state the system...

Page 86: ...U input Only Discrete Inputs Din 2 through Din 15 are software configurable Discrete Input No 16 Din 16 is dedicated as aircraft on ground LGCIU HPP None When an input is not connected to an active sy...

Page 87: ...utput it is no longer available for assignment to any of the other outputs 6 12 SATCOM This section describes the interface and integration requirements for the Airbus Iridium SATCOM System with an Au...

Page 88: ...ing lights When an incoming voice call is ringing the Call Light output will transition to the active state either in a steady state or flashing at approximately a 1 Hz rate When the incoming call is...

Page 89: ...to the Maintenance Port and access the Maintenance User Interface MUI It also provides general information on the steps required to configure and update the Airbus Iridium SATCOM System The Airbus Iri...

Page 90: ...e other end of the Ethernet cable to a laptop that is running a web browser Note It is recommended to use Mozilla Firefox as the Internet browser with the SDU The laptop network adapter must be set to...

Page 91: ...ord required The General tab page displays UTC Date and Time This is correlated to a GPS clock if ICT parameter Internal GPS Active If no link is available i e during startup a default date is display...

Page 92: ...The status of a configured function is either ACTIVE green or FAULT red The ARINC 717 RX configuration is currently not used The DISCRETE IN tab displays the state of the 16 Discrete Inputs The state...

Page 93: ...Rev 02 21 January 2014 Page 56 7 1 3 Part Numbers Page The Part Numbers page provides the status of the software Figure 7 5 and hardware configuration Figure 7 6 of the Airbus Iridium SATCOM System F...

Page 94: ...ntenance Mode provides the Upgrades page to the Maintenance User and Administrator User In addition the Maintenance User is allowed to modify 5 parameters in the ORT page The Administrator User is all...

Page 95: ...nce Mode disables all MCDU functions Figure 7 8 Maintenance Mode Initial Display Screen To exit Maintenance Mode Upon completion of uploading of data or software files or modifying parameters click Ex...

Page 96: ...10 System Restart Screen Note Exiting Maintenance Mode enables all MCDU functions If the aircraft status changes to In Air while in Maintenance Mode the system will reboot automatically and return to...

Page 97: ...pload step the blue progress bars turn green The uploaded data files display a CRC code the uploaded software file displays the part number of the software Non compatible files will be rejected and an...

Page 98: ...aircraft and or operator requirements 8 Administrator User can modify any UAT parameter a Click UAT User Access Table to configure user access privileges 9 Click Exit Maintenance Mode for changes to...

Page 99: ...DM IMEI Status LEDs System GPS ISVM ISDM ARINC 429 Rx Channels Status Active Inactive Discrete Inputs Status Active Inactive Fault Status Part Numbers ICT P N ORT P N ISVM F W Ver ISDM F W Ver S W P N...

Page 100: ...Roles Download Privileges Logs Configurations Failures In Air Faults On Ground Faults Status Link Changes Debug ICT ORT ADB Address Book UAT User Access Table Guest no login required No No No No No No...

Page 101: ...s Modifications Software Data Loading Upload ORT Parameters ICT Parameters Address Book UAT User Access Table S W Upgrades ICT ORT Complete ADB Address Book UAT User Access Table Guest no login requir...

Page 102: ...ile to upload 4 UAT parameters for user roles 7 3 1 Address Book The Address Book can be uploaded as a comma separated values file adb csv by the Maintenance User or Administrator User after login wit...

Page 103: ...are Emergency Safety Non Safety and Public Protected YES indicates that the Address Book entry is protected from being modified NO indicates that the Address Book entry is not protected and can be mo...

Page 104: ...e User 2 Click Enter Maintenance Mode Note The aircraft status must be On Ground to be able to Enter Maintenance Mode 3 Click the ORT link on the left hand side of the screen to open the ORT page 4 AI...

Page 105: ...S the Iridium SIM card installed in the SCM must be ATS enabled If set to NO the Iridium SIM card installed in the SCM is not ATS enabled 7 3 3 Installation Configuration Table ICT The Installation Co...

Page 106: ...en to open the UAT page 4 USER NAME From 4 to 20 upper case alphanumeric characters 5 PASSWORD From 4 to 20 upper case alphanumeric characters 6 SECURITY LEVEL Select either DATA COLLECTOR default or...

Page 107: ...d straight through Ethernet patch cable The software release folder that contains the upgrade file upgrade tgz The software release notes to identify any changes to functionality or special upload ins...

Page 108: ...the upgrade process 4 Click Apply to verify and load the software into non volatile memory Blue progress bars indicate the status of the software file being installed on the SDU When the software veri...

Page 109: ...de click Exit Maintenance Mode at the top right corner of the MUI screen A confirmation message displays prompting to confirm that you want to exit Maintenance Mode see Figure 7 17 Figure 7 17 Exit Ma...

Page 110: ...the software version and part number as noted in the release notes or upgrade instructions d Enter User Name and Password Maintenance User and click Login e Maintenance User Click ORT and review the O...

Page 111: ...Screen 5 Once the system reboots to Operational Mode verify your changes and confirm that the correct software and data files have been installed 6 Click the Part Numbers page and review the Software...

Page 112: ...e Airbus Iridium SATCOM System 6 If installed the cockpit FAULT indication should be illuminated when power is not applied to the system 7 Set the system circuit breaker for the Main power source The...

Page 113: ...s connected to the databus ports being tested are operational and transmitting on the databus 3 Confirm that the ARINC 429 Rx 1 16 channels used are shown as ACTIVE 8 1 2 3 MCDU Tests Confirm SATCOM f...

Page 114: ...each discrete output configured and connected 1 8 confirm the correct state is detected as follows 1 Manipulate the system providing the discrete output as required to indicate the output active state...

Page 115: ...is ATS enabled place a ground to air call While the call is in progress place a higher priority ground to air call Confirm that the existing call is terminated and preempted by a call of higher priori...

Page 116: ...Airbus Iridium SATCOM System 165E5733 00 L 3 Aviation Recorders Proprietary Issue Rev 02 21 January 2014 Page 79 Appendix A Wiring Diagram follows on next 3 pages...

Page 117: ...Airbus Iridium SATCOM System 165E5733 00 L 3 Aviation Recorders Proprietary Issue Rev 02 21 January 2014 Page 80...

Page 118: ...Airbus Iridium SATCOM System 165E5733 00 L 3 Aviation Recorders Proprietary Issue Rev 02 21 January 2014 Page 81...

Page 119: ...Airbus Iridium SATCOM System 165E5733 00 L 3 Aviation Recorders Proprietary Issue Rev 02 21 January 2014 Page 82...

Page 120: ...RT Worksheet ORT Group ORT Parameter Name Value Air to Ground Calls Call Progress Tones NORTH AMERICAN EUROPEAN Allow Manual Dialing Extension 1 YES NO Other Call Parameters Allow Low Priority Calls i...

Page 121: ...Airbus Iridium SATCOM System 165E5733 00 L 3 Aviation Recorders Proprietary Issue Rev 02 21 January 2014 Page 84 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 122: ...rders Proprietary Issue Rev 02 21 January 2014 Page 85 Appendix C Environmental Qualification Forms The following forms are provided for the Airbus Iridium SATCOM System SDU and Airbus Iridium SATCOM...

Page 123: ...3041 TSO Number Manufacturer s Specification and or Other Applicable Specifications Aviation Recorders QTP 905 E5750 34 Airbus Purchaser Technical Specification X2328SP1010161 Airbus ABD0100 1 2 Airbu...

Page 124: ...Equipment tested to Category B Humidity DO 160G Section 6 0 IAW ABD100 1 2 G Equipment tested to Category A Standard Operational Shocks DO 160G Section 7 0 IAW ABD100 1 2 G Equipment tested to Categor...

Page 125: ...ualified to Category D Fungus Resistance DO 160G Section 13 0 and IAW ABD100 1 2 G Section 1 11 Equipment qualified to Category F Magnetic Effect DO 160G Section 15 0 IAW ABD100 1 2 G Section 3 4 1 Eq...

Page 126: ...ion 3 4 4 19 3 1 19 3 3 19 3 4 19 3 5 Equipment tested to Category ZW Equipment Cables Cables Cables Electrostatic Discharge IAW ABD100 1 2 G Section 3 5 Equipment tested Category B Flammability Smoke...

Page 127: ...viation Recorders Proprietary Issue Rev 02 21 January 2014 Page 90 L 3 Aviation Recorders 100 Cattlemen Road Sarasota FL 34232 Telephone 1 941 371 0811 Fax 1 941 377 5591 E mail support DLAR aviationp...

Page 128: ...YSTEM AIRBUS IRIDIUM SATCOM SYSTEM IRIDIUM SATCOM SYSTEM PART NUMBERS SDU 228E5733 00 SCM 418E5733 00 COMPONENT MAINTENANCE MANUAL WITH ILLUSTRATED PARTS LIST P N 165E5733 10 IN ACCORDANCE WITH TSO C...

Page 129: ...onsent of the U S Department of Commerce HTSUS Schedule B 85439 09 000 This manual contains date sensitive information To verify the latest revision level of this manual check the Publications Index l...

Page 130: ...f personsworkingwithstaticsensitivedevices Whenhandlingor servicingequipment containingstaticsensitivedevices adequateprecautionsmust be takentoprevent devicedamageor destruction Onlythosewhoarethorou...

Page 131: ...AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM THIS PAGE IS INTENTIONALLY LEFT BLANK Title Page iv Jan 21 14 23 28 01...

Page 132: ...AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM SERVICE BULLETIN LIST SERVICE BULLETIN DATE EFFECTIVITY DESCRIPTION Service Bulletin Page v Jan 21 14 23 28 01...

Page 133: ...AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM THIS PAGE IS INTENTIONALLY LEFT BLANK Service Bulletin Page vi Jan 21 14 23 28 01...

Page 134: ...IRIDIUM SATCOM SYSTEM RECORD OF CHANGES Issue Revision Date of Change Comments Initial 00 Dec 15 13 Initial issue of AB Iridium SATACOM CMM Includes all sections per ATA100 1 Jan 21 14 Corrected part...

Page 135: ...AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM THIS PAGE IS INTENTIONALLY LEFT BLANK 23 28 01 Record of Changes Page viii Jan 21 14...

Page 136: ...RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM RECORD OF REVISIONS REV NO INSERTION DATE BY REV NO INSERTION DATE BY REV NO INSERTION DATE BY 23 28 01 Record of Revisions Page ix...

Page 137: ...AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM THIS PAGE IS INTENTIONALLY LEFT BLANK 23 28 01 Record of Revisions Page x Jan 21 14...

Page 138: ...of Effective Pages xi Jan 21 14 xii Jan 21 14 Table of Contents xiii Jan 21 14 xiv Jan 21 14 xv Jan 21 14 xvi Jan 21 14 Introduction 1 Jan 21 14 2 Jan 21 14 3 Jan 21 14 4 Jan 21 14 5 Jan 21 14 6 Jan 2...

Page 139: ...14 602 Jan 21 14 Assembly 701 Jan 21 14 702 Jan 21 14 Fits and Clearances 801 Jan 21 14 802 Jan 21 14 803 Jan 21 14 804 Jan 21 14 805 Jan 21 14 806 Jan 21 14 807 Jan 21 14 808 Jan 21 14 Special Tools...

Page 140: ...B DESCRIPTION AND OPERATION 7 C TESTING AND TROUBLESHOOTING 7 D DISASSEMBLY 7 E CLEANING 7 F CHECK 7 G REPAIR 7 H ASSEMBLY 8 I FITS AND CLEARANCES 8 J SPECIAL TOOLS FIXTURES AND EQUIPMENT 8 K ILLUSTR...

Page 141: ...701 FITS AND CLEARANCES SUBJECT DESCRIPTION PAGE 1 GENERAL 801 2 EQUIPMENT SPECIFICATIONS 801 A SATELLITE DATA UNIT SDU 801 B SDU CONFIGURATION MODULE SCM 803 C IRIDIUM ANTENNA SYSTEM 804 D COAXIAL AN...

Page 142: ...28E5733 00 3 Figure 4 SDU Configuration Module SCM Assembly Drawing Part Number 418E5733 00 4 Figure 5 Airbus Iridium SATCOM System Antenna Drawing Part Number 009E5733 00 5 Figure 801 SDU Outline Dra...

Page 143: ...AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM THIS PAGE IS INTENTIONALLY LEFT BLANK 23 28 01 Table of Contents Page xvi Jan 21 14...

Page 144: ...ble assembly are considered Level 1 maintenance line replaceable units and are not field repairable No periodic adjustments calibration or maintenance is required to maintain this system The Airbus Ir...

Page 145: ...ware FWC Flight Warning Computer GAMA General Aviation Manufacturers Association GFI General Format Identifier GPS Global Positioning System GSE Ground Service Equipment HBP Harvard Bi Phase HYB Hybri...

Page 146: ...User Interface N C Normally Closed NGSS Next Generation Satellite Systems N O Normally Open ORT Owner Requirements Table PBX Public Branch Exchange PC Personal Computer P N Part Number PSTN Public Sw...

Page 147: ...TSO Technical Standard Order UAT User Access Table UTC Coordinated Universal Time VAC Volts Alternating Current VDC Volts Direct Current WPS Words Per Second 3 DOCUMENT REQUIREMENTS The following equ...

Page 148: ...dvanced Flight Management Computer System ARINC 717 14 Flight Data Acquisition and Recording System ARINC 718 4 Mark 3 Air Traffic Control Transponder ATCRBS MODE S ARINC 718A 2 Mark 4 Air Traffic Con...

Page 149: ...cialized factory equipment training and techniques These assemblies are not field repairable while the unit is under the warranty period As a result during the unit s warranty period the Airbus Iridiu...

Page 150: ...he unit its interconnections and functionality C TESTING AND TROUBLESHOOTING This section is not applicable under the Level 1 maintenance philosophy for the SDU and SCM units These units are not field...

Page 151: ...r this unit The unit is not field repairable and as such must be returned to the factory for testing and repair should an LRU fail K ILLUSTRATED PARTS LIST This section provides only top level drawing...

Page 152: ...ponding satellites channel management and switching and interconnections with the aircraft and their attached avionics The Airbus Iridium SATCOM System provides multiple voice and data communications...

Page 153: ...s between the aircraft s Air Traffic Service Unit ATSU and a safety services certified terrestrial service provider AFIRS Antenna Iridium and GPS Satellite Data Unit SDU To Aircraft Interfaces Satelli...

Page 154: ...embly Optional components include Cabin Handset s Wired or Cordless A SATELLITE DATA UNIT SDU Refer to Figure 3 The SDU is an ARINC 600 2MCU electronic enclosure that resides in the aircraft s equipme...

Page 155: ...nted near the SDU It uses an EEPROM to store a copy of the aircraft personality information The SCM also contains the Iridium SIM card which provides access to the Iridium satellite network for the vo...

Page 156: ...bined Iridium GPS Antenna The antenna system is comprised of all the components from the rear interface connector up to and including the antenna The total gain of the antenna system must be greater t...

Page 157: ...AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM THIS PAGE IS INTENTIONALLY LEFT BLANK Description and Operation Page 6 Jan 21 14 23 28 01...

Page 158: ...Data Unit p n 228E5733 00 and SDU Configuration Module p n 418E5733 00 have been designated as Level 1 non field repairable Line Replaceable Units These Airbus Iridium System units should be returned...

Page 159: ...AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM THIS PAGE IS INTENTIONALLY LEFT BLANK 23 28 01 Testing Fault Isolation Page 102 Jan 21 14...

Page 160: ...ata Unit p n 228E5733 00 and SDU Configuration Module p n 418E5733 00 have been designated as Level 1 non field repairable Line Replaceable Units These Airbus Iridium System units must be returned to...

Page 161: ...AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM THIS PAGE IS INTENTIONALLY LEFT BLANK Disassembly Page 302 Jan 21 14 23 28 01...

Page 162: ...ta Unit p n 228E5733 00 and SDU Configuration Module p n 418E5733 00 have been designated as Level 1 non field repairable Line Replaceable Units These Airbus Iridium System units should be returned to...

Page 163: ...AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM THIS PAGE IS INTENTIONALLY LEFT BLANK Cleaning Page 402 Jan 21 14 23 28 01...

Page 164: ...ta Unit p n 228E5733 00 and SDU Configuration Module p n 418E5733 00 have been designated as Level 1 non field repairable Line Replaceable Units These Airbus Iridium System units should be returned to...

Page 165: ...AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM THIS PAGE IS INTENTIONALLY LEFT BLANK Check Page 502 Jan 21 14 23 28 01...

Page 166: ...ts that make extensive use of surface mount technology SMT The repair of circuit card assemblies CCAs containing SMT components requires specialized factory equipment training and techniques therefore...

Page 167: ...AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM THIS PAGE IS INTENTIONALLY LEFT BLANK Repair Page 602 Jan 21 14 23 28 01...

Page 168: ...atellite Data Unit p n 228E5733 00 and SDU Configuration Module p n 418E5733 00 have been designated Level 1 non field repairable Line Replaceable Units These Airbus Iridium System units must be retur...

Page 169: ...AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM THIS PAGE IS INTENTIONALLY LEFT BLANK Assembly Page 702 Jan 21 14 23 28 01...

Page 170: ...pe recorder units 2 EQUIPMENT SPECIFICATIONS This section describes the mechanical specifications of the components of the Airbus Iridium SATCOM System A SATELLITE DATA UNIT SDU This paragraph describ...

Page 171: ...olyurethane Finish Mounting ARINC 600 2MCU Mounting Tray Rear Mating Connector Size 2 ARINC 600 Receptacle Radiall P N NSXN2P201S0004 Maintenance Connector RJ45 8P8C Modular Connector Jack Flash Card...

Page 172: ...ions Figure 802 SCM Outline Drawing dimensions in millimeters and inches 2 SCM Specifications Dimensions 1 00 x 2 00 x 4 69 25 4mm x 50 8mm x 119 1mm Weight 0 4 lbs 0 18 kg Max Material Finish Aluminu...

Page 173: ...graph describes the mechanical specifications of the Iridium Antenna Refer to Figure 803 for the Outline Dimension drawing of this component 1 Iridium Antenna Outline Dimensions Figure 803 Iridium Ant...

Page 174: ...mm 0 66 inches Diameter 89 mm 3 5 inches Manufacturer s Specification Reference Number Drawing 009E5733 00 Revision Iridium Antenna Passive 1565 1626 5 MHz RHCP refer to Figure 5 Iridium SATCOM System...

Page 175: ...ception It is a low loss aircraft grade cable that will be mounted in the aircraft fuselage This cable provides the interconnection between the Iridium SATCOM System Satellite Data Unit and the Iridiu...

Page 176: ...mm 0 317 inches Manufacturer s Specification Reference Number Drawing 024E5733 00 Revision B Iridium Antenna Coax Cable see Figure 804 Iridium SATCOM System Supplier Equipment Specification Document N...

Page 177: ...AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM THIS PAGE IS INTENTIONALLY LEFT BLANK Description and Operation Page 808 Jan 21 14 23 28 01...

Page 178: ...been designated as Level 1 non field repairable Line Replaceable Units There are no special tools fixtures and test equipment for Level 1 maintenance for the Airbus Iridium System units These units mu...

Page 179: ...AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM THIS PAGE IS INTENTIONALLY LEFT BLANK Special Tools and Test Equipment Page 902 Jan 21 14 23 28 01...

Page 180: ...228E5733 00 and SDU Configuration Module p n 418E5733 00 have been designated as Level 1 non field repairable Line Replaceable Units The Airbus Iridium System units should be returned to L 3 Communica...

Page 181: ...AVIATION RECORDERS COMPONENT MAINTENANCE MANUAL AIRBUS IRIDIUM SATCOM SYSTEM THIS PAGE IS INTENTIONALLY LEFT BLANK Illustrated Parts List Page 1002 Jan 21 14 23 28 01...

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