Axess Ready CM-111520-RT-AR Instructions d'exploitation

TM 11–5865–229–12OPERATOR’S AND AVIATION UNITMAINTENANCE MANUALCOUNTERMEASURES SETAN/ALQ-162(V)2(NSN 5865-01-187-4729)EQUIPMENTDESCRIPTIONIOPERATINGIN

TM 11-5865-229-12TYPICAL LOCATION OF CM SET LRUs1-0

By Order of the Secretary of the Army:CARL E. VUONOGeneral, United States ArmyChief of StaffOfficial:THOMAS F. SIKORABrigadier General United States A

TM 11-5865-229-12USE OF METRIC MEASURING SYSTEMIn this manual, you’ll find weights and measurements given in American Standard units with the same mea

PIN: 049644-000

This fine document...Was brought to you by me: Liberated Manuals -- free army and government manualsWhy do I do it? I am tired of sleazy CD-ROM sell

TM 11-5865-229-12CHAPTER 1INTRODUCTIONSECTION IGENERAL INFORMATIONSECTION CONTENTSSCOPE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

TM 11-5865-229-121-6 REPORTING EQUIPMENT IMPROVEMENT RECOMMENDATIONS (EIR).If your equipment needs improvement, let us know. Send us an EIR. You, the

TM 11-5865-229-12SECTION IIEQUIPMENT DESCRIPTIONSECTION CONTENTSPAGEEQUIPMENT CHARACTERISTICS, CAPABILITIES, AND FEATURES ...

TM 11-5865-229-121-9 LOCATION AND DESCRIPTION OF MAJOR COMPONENTS.The typical location of each line replaceable Unit (LRU) of the CM Set is shown belo

TM 11-5865-229-121-10 EQUIPMENT DATA.POWER SOURCE. . . . . . . . . . 115 Vac, 400 Hz, 3-phase28 VdcDISSIPATED POWER . . . . 426 wattsCCUHEIGHT. . . .

TM 11-5865-229-12CHAPTER 2OPERATING INSTRUCTIONSSECTION IDESCRIPTION AND USE OF OPERATOR’SCONTROLS AND INDICATORSSECTION CONTENTSPAGECCU CONTROLS AND

TM 11-5865-229-122-2 RT CONNECTORS AND INDICATORS.2-2

TM 11-5865-229-12SECTION IIOPERATION UNDER USUAL CONDITIONSSECTION CONTENTSPAGEGENERAL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

TM 11-5865-229-12Turn aircraft console light control fully clockwise. Refer to aircraft manual for control location.Put on aircraft headset and turn C

TM 11-5865-229-12When the CCU mode switch is in the OPR position, the system is radiating RF energy. All personnelshall stay at least 6 feet away from

TM 11-5865-229-12CHAPTER 3AVIATION UNIT MAINTENANCEINSTRUCTIONSSECTION IREPAIR PARTS; SPECIAL TOOLS; TEST, MEASUREMENT,AND DIAGNOSTIC EQUIPMENT (TMDE)

TM 11-5865-229-12SECTIONSERVICE UPONIIRECEIPTSECTION CONTENTSPAGESERVICE UPON RECEIPT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

TM 11-5865-229-12SECTION IllAVIATION UNIT PREVENTIVE MAINTENANCECHECKS AND SERVICESSECTION CONTENTSPAGEGENERAL. . . . . . . . . . . . . . . . . . . .

TM 11-5865-229-12SECTION IVTROUBLESHOOTING PROCEDURESSECTION CONTENTSPAGEGENERAL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

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TM 11-5865-229-12WARNINGHIGH VOLTAGE IS USED IN THE OPERATION OF THISEQUIPMENT. DEATH ON CONTACT MAY RESULT IFPERSONNEL FAIL TO OBSERVE SAFETY PRECAUT

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TM 11-5865-229-12SECTION VMAINTENANCE PROCEDURESSECTION CONTENTSPAGEINTRODUCTION. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

TM 11-5865-229-12Locate CCU in crew compartment. Refer to aircraft manual for location.Make sure system power is off. Refer to aircraft manual for ins

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TM 11-5865-229-12Do not disconnect CCU ground cable before disconnecting J1 and J2 on the CCU. An ungroundedCCU can present a shock hazard if the syst

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TM 11-5865-229-12SAFETY STEPS TO FOLLOW IF SOMEONE IS THEVICTIM OF ELECTRICAL SHOCK.DO NOT TRY TO PULL OR GRAB THE INDIVIDUAL.IF POSSIBLE, TURN OFF T

TM 11-5865-229-123-12 RT REMOVAL AND INSTALLATION.a. Tools and Materials Required.Tool Kit, Electronic Equipment TK-101/GFlashlightTorque Wrench, Pre

TM 11-5865-229-12Always turn system power off beforedisconnecting RT cables. If power isleft on, you could be injured or killedby high voltage in the

TM 11-5865-229-12c. RT Installation.Perform the following procedure to install the RT in the aircraft.Carefully slide RT into mounting rack. Align gu

TM 11-5865-229-12Always turn system power off before connecting RT cables. If power is left on, you could be injuredor killed by high voltage in the p

TM 11-5865-229-123-13 ANTENNA REMOVAL AND INSTALLATION.This paragraph contains removal and installation instructions for antennas installed with flexi

TM 11-5865-229-12Remove coaxial cable from adapter by turning connector counterclockwise and removing cable.Remove adapter from antenna by removing fo

TM 11-5865-229-12Cap open waveguide sections to prevent foreign particles from entering.c. Antenna Installation (Flexible Coaxial Cable Installations)

TM 11-5865-229-12Attach adapter to replacement antenna by securing four internal hex cap screws.NOTEMake sure preformederly seated.gasket is prop-Atta

TM 11-5865-229-12Carefully insert replacement antenna, with coaxial cable attached, into the aircraft.NOTEMake sure the UP label onantenna mounting fl

TM 11-5865-229-12d. Forward Antenna Removal (EH-60A).Perform the following procedure to remove forward antennafrom the aircraft.Turn system power off.

TM 11-5865-229-12CAUTIONTHIS EQUIPMENT CONTAINS PARTSAND ASSEMBLIES SENSITIVE TODAMAGE BY ELECTROSTATIC DISCHARGE (ESD).USE ESD PRECAUTIONARY PROCEDUR

TM 11-5865-229-12Using ball point hex driver, remove four internal hex cap screws from waveguide flange.Carefully remove antenna from aircraft.If pref

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TM 11-5865-229-123-14 PROGRAM MODULE ASSEMBLY REMOVAL AND INSTALLATION.The program module assembly, located on the front of the RT, contains a threat

TM 11-5865-229-12NOTEThe RT and program module assembly are classified CONFIDENTIAL. Control all classifiedequipment in accordance with appropriate go

TM 11-5865-229-12c. Program Module Assembly Removal.Perform the following procedure to remove the programmodule assembly from the RT. The program m

TM 11–5865-229-12d. Changing RT Mode. Perform the following procedure to change the RT mode.NOTEIf you have not been directed to change the RT mode, p

TM 11-5865-229-12e. Program Module Assembly Installation.Perform the following procedure to install the programmodule assembly in the RT.Leave replace

TM 11-5865-229-12b. Knob Replacement.Perform the following procedure to replace CCU knobs.Make sure system power is off. Refer to aircraft manual for

TM 11-5865-229-12Make sure system power is off. Refer to aircraft manual for instructions.Gently pry the lamp assembly outof the switch with a common–

TM 11-5865-229-12SECTION VIPREPARATION FOR STORAGE OR SHIPMENTSECTION CONTENTSPAGESECURITY PROCEDURES. . . . . . . . . . . . . . . . . . . . . . . .

TM 11-5865-229-12APPENDIX AREFERENCESA-1 SCOPE.This appendix lists all forms, field manuals, technical manuals and miscellaneous publications referenc

TM 11-5865-229-12Supplement, Aviation Unit and Intermediate Maintenance, Avionics Mainte-nance Task Manual, UH-60A and EH-60A Helicopters. . . . . . .

TM 11-5865-229-12APPENDIX BMAINTENANCE ALLOCATION CHARTSECTION IINTRODUCTIONB-1 MAINTENANCE ALLOCATION CHART.a. This Maintenance Allocation Chart (MAC

Technical ManualNo. 11-5865-229-12TM 11-5865-229-12HEADQUARTERSDEPARTMENT OF THE ARMYWashington, DC, 30 November 1990Operator’s and Aviation UnitMaint

TM 11-5865-229-12depot maintenance.) AVIM may perform all maintenance functions authorized to be done at AVUM. Repair ofequipment for return to user w

TM 11-5865-229-12b. Only the lowest category of maintenance authorized to perform a maintenance function is indicated.If the lowest maintenance catego

TM 11-5865-229-12j. Overhaul. The act of disassemblingequipment units down to all removable parts, cleaning, criticallyinspecting, repairing, restorin

TM 11-5865-229-12SECTION IIMAINTENANCE ALLOCATION CHARTFORCOUNTERMEASURES SET AN/ALQ-162(V)2(1)(2)(3)(4)(5)(6)Group Maintenance,Maintenance CategoryTo

TM 11-5865-229-12(1)GroupNumber0101020101020101010202010102020101010203010103010104010105(2)Component/AssemblyRF Module Assy1A1A4High Level Mixer Assy

TM 11-5865-229-12(1)(2)(3)(4)(5)(6)GroupMaintenanceMaintenance CategoryTool &NumberComponent/AssemblyFunction AVUMAVIM Depot EquipmentRemarks01010

TM 11-5865-229-12(1)GroupNumber01011201020104010201050102010501010201060102010601010201060101010202010202010103B-8(2)Component/AssemblyCCA, Transforme

TM 11-5865-229-12(1)(2)(3)(4) (5) (6)GroupMaintenanceMaintenance CategoryTool &NumberComponent/Assembly FunctionAVUM AVIMDepot EquipmentRemarks010

TM 11-5865-229-12(1)(2)(3)(4) (5) (6)GroupMaintenance .Maintenance CategoryTool &Number Component/Assembly Function AVUM AVIM Depot EquipmentRemar

TM 11-5865-229-12SECTION IllTOOLS AND TEST EQUIPMENT REQUIREMENTSToolor TestEquipmentReferenceMaintenance National/NATOCodeCategory NomenclatureStock

TM 11-5865-229-12IIITools and Test Equipment Requirements. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

TM 11-5865-229–12Toolor TestEquipmentReferenceMaintenanceNational/NATOCode CategoryNomenclatureStock NumberTool Number23OOpen End Wrench Head,OP-1049/

TM 11-5865-229-12Toolor TestEquipmentReferenceCode4445464748495051525354555657585960616263MaintenanceCategoryDDDDDDDDDDDDDDDDDDOO, DNomenclatureTest F

TM 11-5865-229-12Toolor TestEquipmentReferenceCode646566676869707172737475MaintenanceCategoryO, DDDO, DDDODDDDDNomenclatureTool Kit, ElectronicEquipme

TM 11-5865-229-12SECTION IVREMARKSReference CodeRemarks/NotesAOperator Initiated Built-In Test (BIT) and System Operational Test.B Repair is limited t

TM 11-5865-229-12APPENDIX CEXPENDABLE SUPPLIES AND MATERIALSSECTION IINTRODUCTIONC-1 SCOPE.This appendix lists expendable supplies and materials you w

TM 11-5865-229-12SECTION IIEXPENDABLE SUPPLIES AND MATERIALS LIST(1)(2) (3)(4) (5)NationalItemStockNumber Level NumberDescriptionU/M1O8105-01-120-3377

TM 11-5865-229-12GLOSSARYLIST OF ABBREVIATIONSac. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

TM 11-5865-229-12INDEXAAbbreviations, list of. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

TM 11-5865-229-12HOW TO USE THIS MANUALThis manual provides instructions for operating and maintaining the AN/ALQ-162(V)2 Countermeasures (CM)Set at t

TM 11-5865-229-12INDEX — CONTINUEDE— CONTINUEDdescription. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

TM 11-5865-229-12INDEX — CONTINUEDL— CONTINUEDLocation and description of major components. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

TM 11-5865-229-12RecommendedReferences ...INDEX— CONTINUEDRimprovement. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .