Raytheon IIS ARTU Air-Ground Radio System User Manual installation manual part six

Raytheon Company Air-Ground Radio System installation manual part six

EXHIBfi' CC-2000 DIGITAL AIRBORNE TELEPHONE SYSTEMFCC ID: CDG-ARTUMAGNASTARMagnaStar Aircraft Configuration SettingsAircraft Tail Number Date:Svstem Confil!uration Settinl!s:Maintenance Pa88code:Billing Node:Aircraft Aircall NUmber:Direct Call pickup:Aircraft Satcom Terminal ID:Call waiting:Node (AItJ):Satcom ~edance (AItJ):Satcom Node (ArO):Aero-I Satcom Dialing:Aero-B+ Satcom Dialing:Auto Link SwitchzDialing Plan:'800 MOD" Call Randoff Mode:9600 MODBM Call Bandoff Mode:CAS Service Indicator:Auxilary Call Alerter Cadence:PC Station uplink Call Mode:Programm8d Speed Dial Humber8 zHI' Decay SettingzHI' Sen.e Setting:HP Label:HP P'1'T:Direct I Credit Card PIN:Y/R-Y/NSatc~ I GroundCellBighl LowBand.et I PBXBnabled/Di8ahledBnabled/DiabledBnab1ed/Di8ahledUS-Canada I MexicoBDabled/Di8ab1edBDabled/DiabledAir-Ground/Satc~/QrouDdCe110113456789Voice/FAX/TDDY I N-8Dabled/ Di .&bledHandset Confi2uration Settin2s:Hand..t location: - -Inplane Number Assigned a 0 1 2 3 4 5 6 7 8 9Inplane Label: -Station Aircall Numbera Station Aircall pin:Ring Handset w/Aircraft AircallaLinka Air-Oround/Satc~Satc~ Station Terainal IDa - --Ring Handset w/Aircraft Satc~ Term. ID: TINStation Type: Cockpit/Cabin/Pax/Mod../TDD/PCStation Baud Rate: 4800bp. I 9600bp.Hand.et Ringera BDabl84 I Di.abl84Hand..t Alerter Gain:Hand..t RJ-ll GainaHand..t Coar.. Speaker Gain a ._-Handset pine Speaker GainaHand..t Voice Sidetone GainaHand..t D'l'KP Oain: - --Hand..t DTNP IIoni tor Scale aHand..t DTNP Moni tor Sen.e a .Hand..t Coar.. Microphone Tx Gaina ---Hand..t pine Microphone Tz Gaina --Auxiliary Call Alerter: 012 3 4 567 8 9Call In progre.. Indicator a ~l84/Di.abl84Inplane LBD Blink Rateauplink LBO Blink Rate:Y/RHand..t location:Inplane II'W8b8r A8.igne4a 0 1 2 J 6 5 , 7 8 9Inplane Label:Station Aircall II'W8b8raStation Aircall pin a Ring Handset -/Aircraft Aircalla T/RLiDJr.: Air-Ground/ satc~Satcom Station Ter8dnal %DaRing Handset -/Aircraft Satc~ Te~. %Da Y/RStation Type: Cockpit/Cabin/rax/~eaJTDD/PCStation Baud Rate: 6800bp. /9600bp.Hand..t Ringer: BDabled / Di8able4Hand..t Alert.r Gain:Hand..t RJ-11 Gaina -Hand..t Coar.. Speaker GainaHand..t Fine Speaker Gain: . ~~ ~Band..t voice sid.tone Gaina ,Hand..t D'rIIJ' Gain: -Hand..t DTMF Noni tor Scale aBand..t D'rIIJ' Noni tor Seu.e aHand..t Coar.. Microphone '1'X Gaina ,Hand..t Fine Kicrophone '1'x GainaAuxiliary Call Al.rter: 012 3 6 5 , 7 8 9Call In Progr... Indicator a BDable4/Di8able4Inplane LBD BliDJr. Rat.aUpliDJr. LBD BliDJr. Rate:Speed Diu' " .i 1 .!C:;i" Speed D a ~~: i~~cSpeed Dial' ::~"Speed Dial' c',...",,'Speed Dial' ~

$FCC ill: COG-ARTUMAGNASTAREXHIBITCC-2000 DIGITAL AIRBORNE TELEPHONE SYSTEMMagnaStar Aircraft Configuration SettingsAircraft Tail Number Date:0123~56789Y/R-BaDd.et location: Inplane Humber Aa.igDed: 0 1 2 3 4 5 I 7 8 tInplane Label:Station Aircall Ru8b8r:_-Station Aircall pin: --Ring BaDd.et -/Aircraft Aircall: T/RLink: Air-Ground/ SatcoaSatcoa Station Ter8inal ID:Ring Handset _/Aircraft Satcom T8%m. ID: T/RStation TYPe: Cockpi t/Cabin/Pax/MOd../TDD/PCStation Baud Rate: 4800bp. / 'IOObp.BaDd.et Ringer: BDabled / Di.abledHand.et Alerter Gain:Hand.et RJ-ll Gain:Hand.et Coar.e Speaker Gain:Hand.et Fine Speaker Gain: ; .'Hand.et voice Sidetone Gain: . ~_.,Handset DTIIP Gain:Hand.et DTIIP Honi tor Scale:Hand.et DTIIP Honi tor Senae:Hand.et Coar.e Microphone Tx Gain: ---Hand.et pine Kicrophone Tx Gain: --Auxiliary Call Alerter: 0 1 2 3 4 5 I 7 8 ,Call In progre.. Indicator: BDabled/Di.abledInplane LBD Blink Rate:Uplink LED Blink Rate:Band..t location:Inplan. IfUmb8r A8.ignedaInplan. Labela ~Station Aircall Rumb8r:Station Aircall pinaRing Band.et -/Aircraft AircallaLink: Air-QrouDdISatc~Sat com Station T.rminal ID: -Ring Bands.t -/Aircraft Satcom T.rm. ID: TINStation TYPe: Cockpit/Cabin/Fax/Mod../TDD/PCStation Baud Rate: t800bp. I '600bp.Band..t Ring.r: Bnabled I Di.abledBand..t Alert.r Gain:Band..t RJ-ll Gain: -Band..t Coar.. Speak.r Gain: Band..t Fin. Speak.r Gain a ::,.;~-;;-Band..t Voice Sid.tone Gaina ~Band..t DTIIF Gain: ",-,. :;.,Band..t D'l'KF ~ni tor Scal. aBand..t DTIIF ~ni tor Sen..aBands.t Coar.. Microphone Tx GaiDa ---Bands.t FiD. Microphone Tx GaiDa Auxiliary Call Al.rt..r: 0 1 2 3 t 5 , 7 8 9Call In progr.ss Indicatora BDabled/Di.abledInplan. LBD Blink Rate:Uplink LED Blink Rat.: ---0123'5678.9 Band..t location:Inplan. NUmber Aa.ignedl 0 ~ 2 J '5 , 7 . 9Inplane Label: -Station Aircall -.her: -Station Aircall pillaRing Hand..t -/Aircraft Aircalll Y/RLink: Air-Qround/Satc~Satcom Station Ter8dnal ID: -Ring Band..t _/Aircraft Satcoa T.:m. ID: Y/RStation Typ.1 Cockpit/Cabin/Fax/Modem/TDD/PCStation Baud Rat.1 4.00bp. / 9600bp.BaDd..t Ring.r: Bnabled / Di.abledBand..t Al.rt.r Gain IHand..t RJ-ll GainlHand..t Coar.. Speaker GainlHand..t Fin. Speak.r Gain I ;iBand..t Voice Sid.tone Gainl ..,Band..t I)'1'Np Gain: -Hand..t ~ ~nitor Scal.1Hand..t DTKr Moni tor S.n..1Band..t Coar.. Microphon. TX GainlBaDd..t pin. Microphone TX GainlAuxiliary Call Al.rt.r: 0 ~ 2 3 4 5 6 7 . 9Call In progr... Indicator I Bnabled/Di.abledInplan. LBD Blink Rat.1Uplink LED Blink Rat.: -Hand.et location: -Inplane B\uaber Aa.igned IInplane LabellStation Aircall RU8b8r:Station Aircall Pinl -Ring Hand.et -/Aircraft Aircalll T/BLinkl Air-around/8at~Satc08 Station Ter8dnal ZDIRing Hand.et -/Aircraft Satcam T8~. ID: TINStation Type: Cockpit/Cabin/Pax/Nodea/TDD/PCStation Baud Ratel tBOObp. / ,'OObp.Hand.et Ringer: BDabled I Di.abledHand.et Alerter aain IHand.et RJ-ll Gain: -Hand.et Coar.e Speaker Gain: .Hand.et Fine Speaker (Jainl 2C~~Hand.et voice Sidetone Gain: --Hand.et DTIII' aain:Hand.et DTIII' Monitor ScalelHand.et DTIII' Moni tor Sen.elHand.et Coar.e Microphone TX Gain I ~Hand.et Fine Microphone TX GaiDI Auxiliary Call Alerter: 0 1 2 3 , 5 , 7 B ,Call In Progre.. Indicator: BDabled/Di.abledInplane LED Blink Rate:Uplink LED Blink Rate: -$

$FCC ID: CDG-ARTUMAGNASTAREXHlBlTCC-2000 DIGITAL AI RBORNE TELEPHONE SYSTEM0123456789Band.et location: -Inplane Rumber Aa.ignedlInplane Labell - -Station Aircall R\l8ber1Station Aircall pinsRing Band.et -/Aircraft Aircalll T/RLink I Air-GrouDd/Satc~Satcom Station Terminal ID:Ring Band.et -/Aircraft Satcom Te~. ID: T/RStation Type: Cockpit/Cabin/Fax/Nodea/TDD/PCStation Baud Ratel j800bp. l'fOObp.Band..t Ring.r: 8Dabled I DiaabledBand..t Al.rt.r Gain:Band..t RJ-ll Gain IBand..t Coar.. Speak.r ~iD 1 -Band..t Fine Speak.r ~inl ~,,: ,Band..t Voice sid.tone ~iDl I'~Band..t D'1'IIF ~in:Band..t DTKF Monitor Scal.:Band..t D'1'IIF Moni tor Sen..1BaDd..t Coar.. Microphone TX ~inl --Band..t Fine Microphon. Tx ~inlAuxiliary Call Al.rter: 0 1 2 3 j 5 f 7 8 ,Call In progr... Indicator: 8Dabled/Di.abledInplane LBD Blink RatelUplink LED Blink Rat.: -BaD4..t location: - -Inplane Number A8.ignedl 0 1 2 3 6 5 6 7 8 9Inplane LabellStation Aircall RU8b8r1Station Aircall pin: .Ring BaD4..t w/Aircraft Aircalll Y/RLink: Air-GroUDd/Satc~Satcom Station T.rBdnal ID: -Ring Band..t w/Aircraft Satc08 T8~. ID: Y I.Station Type: Cockpit/Cabin/rax/Modea/TDD/PCStation Baud Ratel 4800bp. 19600bp.BaD4..t Ring.r I 8Dabled 1 Di.abledBand..t Alert.r Gainl -BaDd.et RJ-ll GainlBaD4..t Coar.. Speaker QainlBand..t riDe Speak.r Qain: 10.';'Band.et Voice Sid.ton. Qainl ~--Band.et D'1'IIF Gain IBand..t D'1'IIF Monitor Scal.1 -Band.et DTKr Monitor S8D8.1BaD4..t Coar.. Microphone TX Gainl --Band..t riDe Microphon. TX Gainl Auxiliary Call Al.rterl 0 1 2 3 6 5 6 7 8 9Call In Progr... Indicator: BDabled/Di.abledInplan8 LSD Blink Rate I -Uplink LSD Blink Rat.:0123456789y,.Band.et location: - -Inplane NwDber Aa.igD,ed1 0 1 2 J, & 5 I' 7 8 9Inplane LabellStation Aircall .u.berl -Station Aircall PinlRing Band.et w/Aircra~t Aircalll T/RLinkl Air-GroW1d/Satc~Satcom Station TermiDal IDIRing BaD4.et w/Aircraft Satc~~. ID: TISStation TYPe: Cockpit/Cabin/raz/~~~/TDD/PCStation Baud Ratel 4800bp. 191'OObp.Band.et Ringer: BDable4 I Di.able4Band.et Alerter Gain:Band.et RJ-ll GainlBand.et Coar.e Speaker Gain I -Band.et Pine Speaker Gainl -- --"Band.et voice sidetone Gainl -Band.et D'1'KF Gain I -Band.et DTMF Monitor Scale IBaD4.et DTHF Moni tor Sen.elBand.et Coar.e Kicropbone TZ Gainl ---Band.et pine Micropbone TZ Gainl ---Auxiliary Call Alerterl 0 1 2 3 4 5 I' 7 8 9Call In Progre.. Indicator: BDable4/Di.abledInplane LSD Blink Ratel -Uplink LSD Blink Rate: -Band..t location:Inplane Number A..igne4aInplane Labela ~-Station Aircall RU8b8ra . -"Station Aircall pina 'cot'Ring BaDc!.et -/Aircraft Aircalla -"Link a Ai r-Ground I Satc~Satcom Station TerBdnal ID:Ring BaDc!..t -/Aircraft Satc~ T.Em. XD: Y/SStation Type: Cockpi t/Cabin/Paz/Mod../TDD/PCStation Baud Rat.a j800bp. I'SOObp.BaDc!..t Ring.r: BDablec! I Di.ablec!BaDd..t Al.rt.r Gain:Ban4..t RJ-ll Gain aBaDc!..t Coar.. Speaker GainaBaD4..t pine Speak.r Gaina ."~'j.-~cBan4..t Voice Sid.ton. Gaina - :":';;;:iiBaDd..t D'1'IIF Gain: '0' ,"'C:Band..t D'1'IIF Koni tor Scale:BaDd..t DTKF Koni tor Sen..: -Band..t Coar.. Microphone '1'z GaiDa -BaDd..t Pine Microphon. '1'z Gaina ---Auxiliary Call Al.rtera 0 1 2 3 . 5 S 7 8 ,Call Xn Progr... Indicator: 8Dablec!/Di.ablec!Inplane LED Blink Rate:uplink ~D Blink Rat.a$

$EXHIBrrcC-2000 DIGITAL AIRBORNE TELEPHONE SYSTEMFCC ID: CDG-ARTUMAGNASTARMMT SOFTWARE LOADING8.0This section covers loading of MMT software onto the MMT host computer.The host computer must be a 386 or faster IBM compatible computer with 4 Megabytes of RAM.a 3.5" high density floppy drive. and at least 1 Megabyte of memory available for use on the harddrive. For the MMT software to run property it is important that the C: partition is no larger than1.5 Gigabytes and be designated FAT or FAT 16. The MMT software must be executed fromDOS and cannot be run from Windows or a Windows DOS shell. A RS-232C serial port andserial cable (PIN 422632-801) are necessary for connection to the MagnaStar C-2000 system.Execution of the MagnaStar Maintenance Terminal (MMT) software can only occur after it isloaded in the host computer memory. This loading process will only be required to be performedthe first time the MMT software is to be used or if an updated version is required. The hostcomputer when loaded with the MagnaStar Maintenance Terminal software will be referred to asthe MMT. Loading of the MMT software will automatically start the execution of the MMT afterthe completion of the software download to the computer's memory. The following steps are tobe used if the MMT software has not been loaded into the host computers memory or if anupdated version is to be loaded:Power up the computer and wait for the computer to complete the boot process. Afterthe computer has completed the boot sequence, insert the 3.5- MagnaStar MaintenanceTerminal (MMT) software disk in the appropriate drive (A or B) of the computer.If you placed the diskette in the A drive use the following commands: From the rootdirectory type "A:\MMT COPY" . then press "ENTER" to execute this command.C:>A:\MMT COpy IENTERIIf you placed the diskette in the B drive use the following commands: From the rootdirectory type "B:\MMT COpy B" , then press "ENTER" to execute this command.C:>B:\MMT COpy B I ENTERIThe "MMT COPY" command will automatically load all the software files and create thenecessary directories required to operate the MMT software. This command will alsostart the execution of the MMT software.RevB8-$

FCC ID: CDG-ARTU EXHIBIT CMAGNASTAR C-2000 DIGITAL AIRBORNE TELEPHONE SYSTEMEQUIPMENT TROUBLESHOOTING PROCEDURES...9-1...9-1...9-19-2...9-3...9-5...9-6...9-7...9-9.9-11.9-12.9-13.9-14.9-15.9-16.9-16.9-17.9-17.9-18.9-18.9-20.9-22.9-23.9-26.9-279-279-29.9-309-309-329.0 EQUIPMENT TROUBLESHOOTING PROCEDURES ,..9.1 TROUBLESHOOTING PROCEDURE FOR MMT INST ALLA TION TUTORIAL9.1.1 C-2000 SYSTEM POWER UP 9.1.2 MMT COMMUNICATION VERIFICATION 9.1.3 START ARTU OPERATIONAL SOFTWARE 9.1.4 LOCKED OFF-LINE STATE 9.1.5 ARTU MOUNTING TRAY FAN TEST 9.1.6 ARTU TRANSMI1TER OUTPUT POWER 9.1.7 ARTU RECEIVE SIGNAL STRENGTH MEASUREMENT 9.1.8 HANDSET / LAN TEST """""""".'.."""""""'"9.1.9 RESET MAINTENANCE ACCESS PASSCODE 9.1.10 UNLOCKED ONLINE STATE 9.1.11 RSS MEASUREMENT USING GENSTARGROUND STATION 9.1.12 MMTI TROUBLESHOOT CONCLUSION 9.1 Additioul MMTI Troubleshoot Informatio. 9.2.1 Data Cable Pull Check .""' """"'.".""'.' """"""'" 9.2.2 Fault Counter Check 9.2.3 Flight Test Log 9.2.4 L-Band Interference Tests 9.2.5 CEPT -EI Communication Verification 9.3 MMTI Commanded Mode "" """""""""."""..""9.3.1 MMTI Commanded Mode - C-2000 MMT Boot Menu 9.3.2 MMTI Commanded Mode - C-2(xx) MMT Radio Configuration Menu 9.3.3 MMTI Commanded Mode - C-2(xx) MMT Radio Installation/Test Menu 9.3.3.1 C-2000 MMT Commanded BIT Menu 9.3.3.2 C-2(xx) MMT RF Test Menu """ '."..".'."' ' ""' "".." 9.3.3.3 C-2(xx) MMT Handset Test Menu 9.3.3.4 C-2(xx) MMT Radio Maintenance Operations Menu 9.3.3.4.1 C-2000 MMT Debug Menu. , 9.4 HaDdIet Text MeuagesRevS9-i

FCC ID: CDG-ARTU EXHIBIT CMAGNAST AR C-2000 DIGITAL AIRBORNE TELEPHONE SYSTEM9.1.2 MMT COMMUNICATION VERIFICATIONThe MMT Communications Verification test assures that the MMT software is properly communicatingwith the ARTU by checking the version of software that is loaded in the ARTU.Symptom: "ERROR=> MMT communications failure - timed out"The ARTU and the MMT are not communicating when this information is displayed in the RadioResponses window. Check the MMT cable connection between the MMT computer and theARTU. Check for a damaged connector on RS-232 serial communications port of the computer.After checking these interface connections press "R" to repeat the test. If the same error isdisplayed. cycle power on the computer. If the same error message is displayed after cyclingpower on the computer then replace the ARTU.Symptom: "Radio software executing in unlocked online state"This message will be displayed on the screen if the ARTU was powered up before the computerwith the MMT software running was connected to the ARTU. Remove power to the ARTU forgreater than 20 seconds. Apply power to the ARTU and press "R" to repeat the test.+ V..OA MNT R6dio Re8PQna +, I, ,: Power-up Status: 80376 Kicroproc...or 01, BRAN OK. :: ARTC code pile ARTCC40B.HBX Ver 0.0 net. 0./06/00 1.:25 Bank 2 CRC:4CB8:: DBP code Pile MDSPC.OB.HEX Ver 0.0 Dat. 03/27/00 12:13 B8Dk 4 cac:1298:: BIT code Pile MBITC.OA.HBX Ver 0.0 net. 05/18/99 16:03 Bank 1 CRC:209C:: Boot code Pile ~31C.HBX Ver 0.0 Date 0./2./96 14:27 B8Dk 1 CRC:B818:: R6dio software is not executing.+ ++ MMT Tutorial ~--~'DSlA103 .": Sy8ptom: "ERROR-> MNT cO8mUnications failure - ti-.d out." 1: a) Check that the MNT cable i. properly connected to the AR'I'U. ~: b) Pr..s "R" to repeat test step. J: c) If the error -ssage still appears, then cycle power on the coqlUter J: and start again. :: d) If error -.sage still appears, turn power off to the AR'I'U for more:: than ten seconds. Apply ~r to the AR'ro. Does the pault indicator on :: the front of the AR'I'U illuminate for appr_~tely one .!nut. or 8Ore? :: If it does, cbeck for a bad MNT cable or bad C(»I port on the c~ter. :: e) If the fault indicator does not illuminate, tben replace the ARTU. :,(a.8tuzn ,Figure 9.1.2. MMT Communications Verification MMTI Troubleshoot Screen.9-2 RevB

FCC ID: CDG-ARTU EXHIBIT CMAGNASTAR C-2000 DIGITAL AIRBORNE TELEPHONE SYSTEM9.1.3 START ARTU OPERATIONAL SOFTWAREWhen the ARTU is powered up with an MMT connected, the ARTU software will not execute and will bein what is termed a "boot" mode. When commanded by the MMT, the ARTU will start the operationalsoftware. The first step in starting the operational is for the ARTU to run Built-In-Test (BIT). The normalBIT process begins by turning "ON" the ARTU Fault indicator. The MMT will indicate that the ARTU hasstarted software execution which is displayed in the Radio Responses window. The ARTU then begins anFEPROM test which takes approximately 15-20 seconds to complete. Owing this time there will be no newmessages displayed in the Radio Responses window. BIT test result information will be reported in theRadio Responses window. Depending on how long the ARTU has been powered prior to executing power-up BIT, the screen may pause in the middle of the tests. This pause is to allow the ARTU oscillator towarm-up. This can take one to five minutes. After this pause, BIT will complete.Symptom: Radio Responses window does not display test results.If the Radio Responses window does not appear to change, the user should look to see if the redFault light is illuminated. If the red Fault light is not illuminated then press "R" to repeat the test.Symptom: ARTU fails power-up BIT.If the ARTU fails a BIT test, note which test has failed and replace the ARTU.After power up BIT has completed, it is possible to review the BIT test data by sending thefollowing MMT commands:Press "FI ", ; scrolls screen to commanded mode menuspress "2" and then press ENTER, ; selects Radio Test Menupress "2" and then press ENTER, ; selects Commanded Bit Menupress "0" and then press ENTER. ; selects view BIT resultsPressing "N" for next, or "P" for previous, will scroll the user through the BIT test results.Symptom: ARTU appears to pause during BIT for longer than ten minutes.BIT will begin testing and stop during the middle of the tests to wait for the OCXO frequencyreference to warm up. BIT testing will stop at the "QUERY AMX" test. Ifafter stopping at the"QUERY AM)(" test, the MMT BIT test times out after ten minutes and the RED Fault indicatoris still illuminated, then the ARTU has faulted. Replace the ARTU and note that the ARTU hasfailed for OCXO warm up.Symptom: BIT test appears to repeat.If the BIT test appears to be repeating over and over then one of two conditions is occurring. One,the voltage at the ARTU is dropping below +20.5 volts DC during the power up BIT. Measure thevoltage at the radio interface with ARTU attached. If the voltage drops below +20.5 VDC, checkthe gauge of wire used for the power cable to insure that it is of sufficient size to minimize thevoltage drop from the circuit breaker to the ARTU. The second condition is current limiting. Ifthe power system cannot support a 3-5 ampere current surge while maintaining a stable voltagethen the ARTU will repeat BIT.9-3 RevB

FCC 10: CDG-ARTU EXHIBIT CMAGNASTAR C-2000 DIGITAL AIRBORNE TELEPHONE SYSTEM+ V4. OA NNT Radio Response +I II I: Power-up Statu8, 80376 Kicroproc...or OK. SRAH ox. :: ARTC code Pile ARTCC4OB.HIX Ver 0.0 Date 04/06/00 14,25 BaDk 1 CRC,~:: DSP code Pile KDSPC40A.HIX Ver 0.0 Date 03/27/00 12,13 BaDk 2 CRC,1298:: BIT code pile MBITC40A.HIX Ver 0.0 Date 05/18/99 16,03 BaDk 1 CRC,209C:: Boot code Pile ~31C.HBX Ver 0.0 Date 04/24/'6 14,27 BaDk 1 CRC,B8& :: Radio sottware is not executing.+ ++ V1A NNT Tutorial +: IJfS1A104 1: This test step is info~tional only. :: Pressing .C' will start Built-In-Test (BIT). The no~l BIT process begina 1: by turning .(»t. the ARro pault indicator. The ~ will indicate in that the :: AR'1'U baa started sott~e execution which is displayed in the Radio :: Respon... window. The AR'1'U then begins an PBPftCIf test which takes :: approximately 15-20 seconds. During this time there will be no new ..ssages :: di8Played in the Radio Responses window. BIT test result into~tion will:: be reported in the Radio Responses window. Depending on how long the ARTU :: baa been powered prior to executing power-up BIT. the screen may paU8e in :: the middle ot the tests. This paU8e is to allow the ARTU 08cillator to :: _ra-up. This can take one to five IBinutes. After this paU8e. BIT will :: complete. :: (R)eturn, - :+ +Figure 9.l.3.A. Start ARTU Operational Software MMTI Troubleshoot Screen.V4. OA MMT Radio Responses: WAITDfG FOR POWER-UP BIT RESULTS «5 IIIMnE DELAY:: Press 'B8c' to Terminate Wait: Radio software starting execution.: The KIlT baa been reconfigured for CON Port 1 at 9.6 kbs.'IR S'.'O S c ;' f', ,C',: S~t_: Radio ~SP0D8es window does not change. ';;';;~: al Did you W8~t for the PZPROM test to cO8plete. if 80 Pr88s "R" for,:,~: rete.t. "};: bl Did the ARro fault light illlainate? cf: Sy8ptoa: ARro fails power-up BIT. :: al Determine the Brr fault and record for repair information. See :: KagnaStar Inatallation Manual for steps required to view fault :: information. Replace faulted ARTU. :: Symptom: ARro appears to pause during Brr for l~ger than ten ainutes. :: al If the BIT testing stops at the "TEST AKX" test step for longer than :: ten ainute. at ro- t~rature then note that the ARTU baa failed :: OCXO ~-up. Replace the failed ARTU. :: (Rleturn: - I+ +Figure 9.1.3.8. Start ARTU Operational Software MMTI Troubleshoot Screen.9-4 RevB

FCC 10: CDG-ARTU EXHIBIT CMAGNAST AR C-2000 DIGITAL AIRBORNE TELEPHONE SYSTEM9.1.4 LOCKED OFF-LINE STATEFor the MMT to command certain tests for the installation checkout, the ARTU software must be placed ina mode which will allow the ARTU the flexibility to perform these tests. This mode of operation is calledthe "Locked OFF-Line State". This test step is a mode change only. Failure of this mode change will onlyoccur iftbe MMT is not communicating with the ARTU.It should be noted that while the ARTU is in this mode, the Handset screen may go blank and will notrespond to keypad inputs.Symptom: ERROR=> MMT communications failure - timed out.If this message is displaycd in thc Radio Responses window then check the cabling between thcARTU and the MMT. If the cabling is correct then press "R" to repeat the test.V4.0A MMT Radio Re~Radio 8oftw8re executing in locked offline state.+ + VlA ~ Tutorial':DlS1A1O6,,: Syq>toa: ERROR-> I8rr c~icati0D8 failure - tiJ: a) Check the I8rr cable connecti_.: b) Press .R. for repeat.Figure 9.].4. Locked Off-Line State MMT] Troubleshoot Screen.9-5 RevB

FCC 10: CDG-ARTU EXHIBIT CMAGNASTAR C-2000 DIGITAL AIRBORNE TELEPHONE SYSTEM9.1.5 ARTU MOUNTING TRAY FAN TESTUnder normal operational conditions, the ARTU Mounting Tray Fan is activated by a switch in the ARTUwhich is under software control. The ARTU monitors a temperature sensor located in the ARTU and isprogrammed to turn on the Fan when the temperature is at approximately room temperature. The ARTUMounting Tray Fan test will command the ARTU to turn the fan "ON" to check operation.Symptom: The ARTU Mounting Tray Fan is not operational.If the ARTU Mounting Tray Fan is not operational, the problem can be caused by the ARTU,wiring to the ARTU Mounting Tray or the Mounting Tray Fan itself. Several steps wi)] berequired to detennine the cause of failure. These steps may also vary depending on whichassembly of the ARTU mounting Tray assembly that is used in the aircraft.For -801 Tra~: Remove power from system Remove the power connector from ARTU J2connector interface and ground pin P I-F of the ARTU Power cable. Apply power to the system.If the fan operates, perform a continuity check on the ARTU Tray - ARTU Power cable interface.If the wiring is correct, replace the ARTU. If the fan does not operate, replace the ARTUMounting Tray.For -802 Trax: Remove the PI connector from the ARTU Mounting Tray. With power removed,grotmd pin Jl-9 on the ARTU Tray. Apply power to the system. If the fan does not operate,replace the ARTU Mounting Tray. If the fan operates, perform a continuity check on the 802ARTU Tray - ARTU Power cable. If the wiring is correct, replace the ARTU. Ifnot replacecable.V4.0A 8'l' Radio Response.C-2000 report8 engineering teat FAN CONTROL performed+ ++ VlA MNT Tutorial +:IRS1A101 :: SYJI4>tca: Pen do.. DOt operate. :: por -801 Tray: ~e power from syst_. R~ J2 connector fr.. ARTU end :: ground pin Pl-P of the ARTU Power cable. Apply ~r to the ayst_. If :: the fen operate8. replace the ARTU. If the fan does not operate. replace:: the ARTU Mounting Tray. :: For -802 Tray: a..ove the Pl connector from the ARTU Mounting Tray. with :: power r~ed. gr~ pin Jl-' on the ARTU Tray. Apply power to the :: syst_. If the fen ~ DOt operate. replace the ARTU Mounting Tray. If :: the fan operatH. perfora . continuity on the 802 ARTU Tray - ARTU :: Power cable. If the continuity is correct. replace the ARTU. If not :: replace cable. :~Figure 9.1.5. ARTU Mounting Tray Fan MMTI Troubleshoot Scret9-6 RevB

FCC 10: CDG-ARTU EXHIBIT CMAGNASTAR C-2000 DIGITAL AIRBORNE TELEPHONE SYSTEM9.1.6 ARTU TRANSMITTER OUTPUT POWERDuring the ARTU Transmitter Output Power test, the ARTU will transmit a CW signal at a frequency of894.9495 MHz. The power level transmitted by the ARTU will be 10 watts minimum. Measurement ofthe transmitted signal should be made as close to the Antenna as possible to check the functionality of thegreatest number of the C-2000 components. The insertion loss of components in addition to the ARTUmust be accounted for when measuring the output power of the C-2000 system. The maximum total cableloss that can be used with the C-2000 system is specified at 3 dB. The maximum specified insertion loss ofthe Duplexer is 1.4 dB. If power is measured at the Antenna connector, the minimum power measuredshould be no less than 4 watts.It should be noted that the power meter or thru-line wattmeter used for this test must be capable ofwithstanding 16 Watts of RF energy and must be capable of operating at frequency of I Ohz for correctresults.Symptom: The MMTI appears stuck.Wait for the MMTI to properly execute commands to ARTU (5-10 sec). Commands to the ARTUvia the MMTI may take from 5 to 10 seconds to execute during which time the MMTI screens willappear to change and then stop before completing.Symptom: Low output power / No output power.If power measurements at the Antenna connector are low, it will be necessary to determine whichcomponent is responsible for the excessive loss by process of elimination. First, measure theoutput power directly out of the ARTU. If the power measurement is incorrect replace the ARTU.If the power measurement is correct, measure the output at the end of the transmit cable. If thepower measurements is incorrect, replace the transmit cable. If the power measurement is correct,measure the power at the Antenna output of the Duplexer. If the power measurement is incorrect,replace the Duplexer.V.. OA MMT Radio Respons ''ing teat FAN CONTROL perfo~d.:::::::::: ~ - ~- ~~;w::::7J;~~DfSlAl08This t..t step is inatructional only.During the next test step the ARTU will transmit a CW signal at a powerlevel of +40 to +42 dBm. The Duplexer is specified for a n8Xi.u. lossof 1.4 dB. The 8aXimu8 syat.. C8ble loas for the RP cables is specifiedat 3 dB. The ~r _ter should measure greater than +36 dBm when allthe above factors are taken into account.[aleturnFigure 9.1.6.A. ARTU Transmitter Output Power MMTI Troubleshoot Screen.,,"1 RevS

FCC ill: CDG-ARTU EXHmrr CMAGNAST AR C-2000 DIGITAL AIRBORNE TELEPHONE SYSTEM+ ~.~ MMT Radio R88p0D8" ti C-2000 reports eagiDeeriDQ teat ~ INITIAL PA ~ perfo~.,DS1Al09 , v4~,I :: ~t~: 81'1 aR>ear. .tuck. :: Wait for tha *1'I to properly .-cute c~ to AR'fU (5-10 Me). :: t: ~t08: Low output power / No output power. T: H.-ure the output p~r directly out of the AR'ro. If the power r: me&8Ur..-Dt i. incorrect replace the AR'ro. If the power 8ea8Ur888Dt i. 1: correct. -=e the output at the end of the tran~t cable. If the .f: power _.ur-ts is incorrect. replace the tr~t cable. If the ~ :: -..ur~t i. correct. _sure the power at the Antenna output of the :: Duplex8r. If the power 88a8Ur8ment is incorrect. replace the Duplexer. t, .., .: (R)eturn: - :+ +Figure 9.1.6.8. ARTU Transmitter Output Power MMTI Troubleshoot Screen.7 Vt.OA MItT Radio Resp0n8 "~::.~ 7! C-2000 reporta engineeriD9 teat STOP TRANSMIT perfor8ed. ::i :,DlS1Al10 c c" -1, .., ,: ~t_: ARTU does not stop tran8lRitting. l: If the ARTIS does not stop transmitting check that the ~ ~. 1. '1: properly eonneeted. If the cable is properly connected. pr..s "R- for 1: repeat. :~Figure 9.1.6.C. ARTU Transmitter Output Power MMTI Troubleshoot Screen.9-8 RevB

FCC ID: CDG-ARTU EXHIBIT CMAGNASTAR C-2000 DIGITAL AIRBORNE TELEPHONE SYSTEM9.1.7 ARTU RECEIVE SIGNAL STRENGTH MEASUREMENTThe ARTU Receive Signal Strength measurement test will verify the complete RF portion of the C-2000system. This test will require the use of a MagnaStar Loop-Around test box. During this test a 16 QAMsignal is transmitted by the ARTU. With the MagnaStar Loop-Around test box connected to the Antenna,the signal is coupled into the Loop-Around test box where it is mixed by 45 MHz and coupled back into theAntenna. A receive signal strength measurement using the ARTU checks out both the TSC and Pilotreceive channels of the ARTU as well all the components between the ARTU and the Antenna. Thefrequency of the transmitted signal is 894.9495 MHz.This test is to check for gross loss problems in the RF cables and associated hardware and is not intended tobe a calibrated test measurement. Typically the value should be measured at - 103 dBm +/- 6 dB withnominally valued components. Because the TSC and Pilot channels are separate receivers, variationsbetween measurements are possible. If, however, there is a delta between the two receivers of greater than10 dB, the ARTU is to be rejected.The Loop-Around test box is powered by a 9 volt battery. The battery voltage must be greater than 6.0volts to operate and provide the expected perfonnance results. The Loop-Around test box provides thecapability to check the battery to ensure that the voltage is correct. The Loop-Around test box attenuatorsetting should be set to the "ON" position for the first part of this test. Switching the attenuator to the"OFF" position should change the receive signal strength by approximately 30 dB.Symptom: Reading between the TXRX and RX receivers greater than 10 dB.If the delta between the TXRX (TSC) and RX (Pilot) receivers is greatertban 10 dB, repeat thetest. If after repeating the test the same results occur then replace the ARTU.Symptom: RSS readings on both the TXRX and RX channels less than -109 dBm (-103 dBm - 6 dB)If the RSS readings are less than -109 dBm then the lossy component needs to be located. If theARTU Transmitter Output Power test has been successfully completed then the problem is eitherthe Antenna, Duplexer, Receive cable or ARTU. If the ARTU has successfully passed BIT, thenthe most likely candidates are the Antenna, Duplexer or the receive cable. With the properadapters, cable loss should be measured for the ARTU receive cable. Elimination of the receivecable as the problem leaves the Duplexer and Antenna. With the proper adapters and a 30 dB/25Watt pad, the antenna cable can be directly attached to the Loop-Around test box bypassing theAntenna. If the loss problem still exists after bypassing the Antenna, replace the Duplexer., V4. OA 10ft' Radio ReSPO8'8M+ ~ ++ VlA IGrr TutorW;' +'mS1A200 II I: This test step i8 instructional only. :I ,I I: In preparation for measuring the syst.. receive 8ignal strength. the :: loop around test box -.t be configured and properly placed for expected :: results. Perfora a battery check prior to use by turning .ON. the loop :: around test box and pressing the -.ntary battery check _itch. 'ft1e :: indicator light vill illU8inate if the battary is within operational :: require8eDts. set the attenuator svitch to the .ON. position. Place the :: cable clip-on cla.p on the center of the blade antenna for best results. :(a}~.-Figure 9. 7 A. ARTU Receive Signal Strength Measurement MMTI Troubleshoot Screen.' V4.0A MMT Radio Responses.2000 ~rta .tatu. update ENABLED.9-9 RevB

$FCC ill: CDG-ARTU EXHIBIT CMAGNASTAR C-2000 DIGITAL AIRBORNE TELEPHONE SYSTEMPr'-' F2 to View Status Display+ ++ VlA I8rr Tutorial :mSlA20l :: SY8f{)tom, us Value alUch lower than ~kings on Loop-Around Teat Box. :: a) Are the ON/OFF and Attenuator awitches in the correct po8ition? :: Is the battery voltage greater than 6 volts? :: b) .ove ~e Loop-Around Test Cable connection plac_t on the Ant~a. :: c) Replace cables or C-2000 RP components one at a time to isolate the :: faulted unit. :I I. I: ~t_, RSS value difference bet_en the TXRX and RX is gre.ter than 10 dB. :: If values of the US readings bet_en the TSC (TXRX) and the Pilot (RX) :: receivers is greater than 10 dB replace the ARTU. :._"'~~:_:Figure 9.1.7B. ARTU Receive Signal Strength Measurement MMTI Troubleshoot Screen.9-10 RevB$

Raytheon IIS ARTU Air-Ground Radio System User Manual installation manual part six

Raytheon Company Air-Ground Radio System installation manual part six

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