Honeywell KHF1050 High Frequency Communications Transceiver User Manual 006 10640 0000

Honeywell International Inc. High Frequency Communications Transceiver 006 10640 0000

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KHF1050 User Manual

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SYSTEM INSTALLATIONMANUALKHF 1050HF COMMUNICATION SYSTEMMANUAL NUMBER 006-10640-0000REVISION 0, March 2003Preliminary - Subject to Change Without Notice

WARNINGPRIOR THE EXPORT OF THIS DOCUMENT, REVIEW FOR EXPORT LICENSE REQUIREMENT IS NEEDED.COPYRIGHT NOTICE ©2003 Honeywell International Inc.REPRODUCTION OF THIS PUBLICATION OR ANY PORTION THEREOF BY ANY MEANSWITHOUT THE EXPRESS WRITTEN PERMISSION OF HONEYWELL IS PROHIBITED. FORFURTHER INFORMATION CONTACT THE MANAGER, TECHNICAL PUBLICATIONS,HONEYWELL, ONE TECHNOLOGY CENTER, 23500 WEST 105TH STREET OLATHE KS66061 TELEPHONE: (913) 782-0400.Preliminary - Subject to Change Without Notice

NRevision 0 T-110640I00.SLK Mar/200323-10-09System Installation ManualP/N 006-10640-0000KHF 1050HF Communication System(Also known as Primus HF 1050)KAC 1052 Antenna CouplerKPA 1052 Power AmplifierKRX 1053 Receiver/ExciterCompatible HF Control UnitsPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALREVISION HISTORYRevision 0 RH-110640I00.SLK 23-10-09 Mar/2003KHF 1050SYSTEM INSTALLATION MANUAL23-10-09-----------------------------------------------------------------PART NUMBER REV DATE DESCRIPTION006-10640-0000 0 Mar/2003 Original issue.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALREVISION HISTORYRevision 0 RH-210640I00.SLK 23-10-09 Mar/2003KHF 1050SYSTEM INSTALLATION MANUAL23-10-09-----------------------------------------------------------------PART NUMBER REV DATE DESCRIPTIONPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRECORD OF REVISIONSRevision 0 RR-110640I00.SLK 23-10-09 Mar/2003REV.NO. REVISIONDATE DATEINSERTED BY REV.NO. REVISIONDATE DATEINSERTED BYPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRECORD OF REVISIONSRevision 0 RR-210640I00.SLK 23-10-09 Mar/2003REV.NO. REVISIONDATE DATEINSERTED BY REV.NO. REVISIONDATE DATEINSERTED BYPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALCOMMENTARY: LEP TO BE UPDATED UPON COMPLETION OF MANUALLIST OF EFFECTIVE PAGESSUBJECT PAGE DATE SUBJECT PAGE DATEF INDICATES FOLDOUT PAGES - PRINT ONE SIDE ONLYRevision 0 LEP-110640I00.SLK 23-10-09 Mar/2003Title T-1 Mar/2003T-2 Mar/2003Revision RH-1 Mar/2003History RH-2 Mar/2003Record of RR-1 Mar/2003Revisions RR-2 Mar/2003List of Effective Pages LEP-1 Mar/2003LEP-2 Mar/2003Table of Contents TC-1 Mar/2003TC-2 Mar/2003Introduction INTRO-1 Mar/2003INTRO-2 Mar/2003Glossary G-1 Mar/2003G-2 Mar/2003G-3 Mar/2003G-4 Mar/2003Description and 1 Mar/2003Operation 2 Mar/20033 Mar/20034 Mar/20035 Mar/20036 Mar/20037 Mar/20038 Mar/20039 Mar/200310 Mar/200311 Mar/200312 Mar/200313 Mar/200314 Mar/200315 Mar/200316 Mar/2003Testing and 1001 Mar/2003Fault Isolation 1002 Mar/2003Installation and 2001 Mar/2003Maintenance 2002 Mar/20032003 Mar/20032004 Mar/20032005 Mar/20032006 Mar/20032007 Mar/20032008 Mar/20032009 Mar/20032010 Mar/20032011 Mar/20032012 Mar/20032013 Mar/20032014 Mar/20032015 Mar/20032016 Mar/20032017 Mar/20032018 Mar/20032019 Mar/20032020 Mar/20032021 Mar/20032022 Mar/20032023 Mar/20032024 Mar/20032025 Mar/20032026 Mar/20032027 Mar/20032028 Mar/20032029 Mar/20032030 Mar/20032031 Mar/2003Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALCOMMENTARY: LEP TO BE UPDATED UPON COMPLETION OF MANUALLIST OF EFFECTIVE PAGESSUBJECT PAGE DATE SUBJECT PAGE DATEF INDICATES FOLDOUT PAGES - PRINT ONE SIDE ONLYRevision 0 LEP-210640I00.SLK 23-10-09 Mar/2003F 2125 Mar/20032126 BlankPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALCOMMENTARY: TOC TO BE UPDATED UPON COMPLETION OF MANUALTABLE OF CONTENTSRevision 0 TC-110640I00.SLK 23-10-09 Mar/2003INTRODUCTIONSECTION PAGE1. General INTRO-12. Layout of Material INTRO-13. Revision Service INTRO-1DESCRIPTION AND OPERATIONSECTION PAGE1. System Description 1A. System Overview 3B. System Component Descriptions 4C. Component Installation Kits 5D. Equipment Required But Not Supplied 6E. Optional (Non-Essential) Aircraft Equipment 8F. Related Publications 82. Component Configurations 9A. KAC 1052 Antenna Coupler Configurations 9B. KPA 1052 Power Amplifier Configurations 9C. KRX 1053 Receiver/Exciter Configurations 9D. RM-855 Radio Management Unit Configurations 9E. MCDU Multifunction Control and Display Unit Configurations 9F. PS440 Control Display Unit Configurations 9G. ???? Antenna Configurations 9H. Long Wire HF Antenna Configurations 93. System Leading Particulars 10A. General Specifications 10B. System Operating Modes 10C. Component Leading Particulars 134. System Function 15A. System Functional Overview 15B. Dual System 165. Component Functions 16A. RM-855 Radio Management Unit Function 16B. MCDU Multfunction Control and Display Unit Function 16C. PS440 Control Display Unit Function 166. System Inputs/Outputs 17A. Input/Output Signals 17TABLE PAGECOMMENTARY: ALL SECTION TABLES TO BE LISTED HERE AS THEY ARE INSERTED.FIGURE PAGECOMMENTARY: ALL SECTION FIGURES TO BE LISTED HERE AS THEY ARE INSERTEDPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALCOMMENTARY: TOC TO BE UPDATED UPON COMPLETION OF MANUALTABLE OF CONTENTSRevision 0 TC-210640I00.SLK 23-10-09 Mar/2003TESTING AND FAULT ISOLATIONSECTION PAGE1. Fault Isolation 10012. System Performance Check 1002A. Preliminary Check 1002B. Receiver Performance Check 1002C. Transmitter Performance Check 1002INSTALLATION AND MAINTENANCESECTION PAGE1. General Coverage 20012. Unpacking 20013. Pre-installation Testing 20014. Equipment Changes and Markings 20025. Installation Planning 2002A. General Considerations 2002B. Location of Equipment 2002C. Interwiring and Cable Fabrication 2017D. Strapping Options 20526. Equipment Installation 2055A. Bonding Connections 2055B. KCU 951 Control Unit Installation 2056C. KFS 594 Miniature Control Unit Installation 2056D. KA 594 Bus Adapter Installation 2056E. KCU 1051 Control Display Unit Installation 2056F. KAC 952 Power Amplifier/Antenna Coupler Installation 2057G. KTR 953 Receiver/Exciter Installation 2061H. Antenna Installation 2062I. KA 161 External Capacitor Installation 2063J. KA 158 Bridging Amplifier Installation 2064K. KA 160 Dual Antenna Adapter Installation 2064L. KA 162 Dual External Capacitor Installation 20657. Inspection, System Checkout, and Flight Test Procedures 2065A. Inspection 2065B. System Checkout 2068C. Flight Test 20688. Removal and Re-installation 2069A. KCU 951 Control Unit Removal and Re-installation 2069B. KFS 594 Miniature Control Unit Removal and Re-installation2069C. KA 594 Bus Adapter Removal and Re-installation 2069D. KCU 1051 Control Display Unit Removal and Re-installation 2069E. KAC 952 Power Amplifier/Antenna Coupler Removal 2070F. KTR 953 Receiver/Exciter Removal and Re-installation 2070G. KA 98 Antenna Removal and Re-installation 2071H. KA 161 External Capacitor Removal and Re-installation 2072I. KA 158 Bridging Amplifier Removal and Re-installation 2073J. KA 160 Dual Antenna Adapter Removal and Re-installation 2074K. KA 162 Dual External Capacitor Removal and Re-installation2074Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALCOMMENTARY: TOC TO BE UPDATED UPON COMPLETION OF MANUALTABLE OF CONTENTSRevision 0 TC-310640I00.SLK 23-10-09 Mar/20039. Maintenance Procedures 2075A. In-Aircraft Adjustments 2075B. System Protection 2075C. Lubrication 2076D. Cleaning 207610. System Maintenance Programs 2076A. System Maintenance Recommendations 2076B. Field Alignment of KTR 953 Receiver/Exciter (-51, -53) 2076TABLE PAGECOMMENTARY: ALL SECTION TABLES TO BE LISTED HERE AS THEY ARE INSERTED.FIGURE PAGECOMMENTARY: ALL SECTION FIGURES TO BE LISTED HERE AS THEY ARE INSERTEDPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALCOMMENTARY: TOC TO BE UPDATED UPON COMPLETION OF MANUALTABLE OF CONTENTSRevision 0 TC-410640I00.SLK 23-10-09 Mar/2003Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 INTRO-110640I00.SLK Mar/200323-10-09INTRODUCTION1. GeneralThis manual provides description and operation, testing, fault isolation, installation, maintenance, and flightline checkout procedures for the KHF 1050 HF Communication System.2. Layout of ManualSection 1 Description and OperationSection 1000 Testing and Fault IsolationSection 2000 Installation and MaintenanceRefer to the Table of Contents for the location of applicable information.Weights and measurements in the manual are in English units, unless otherwise stated.3. Revision ServiceThe manual will be revised as necessary to reflect current information. Service Bulletins may be issued separately, and will be incorporated in the manual as appropriate.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 INTRO-210640I00.SLK Mar/200323-10-09Blank PagePreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 G-110640I00.SLK Mar/200323-10-09Glossary of Terms and AbbreviationsA/C AircraftAGC Automatic Gain ControlAME Amplitude Modulation EquivalentARM The ready to operate status of a function/device.CFR ClarifierCLK ClockCOMP CompatibleCPLR CouplerGND GroundHF High FrequencyLCD Liquid Crystal DisplayLSB Lower Side BandMCDU Multifunction Control and Display UnitMIC MicrophoneNVG Night Vision GogglesORTHOGONAL Intersecting at right angles.PA Power AmplifierPROC Processing, ProcessorPEP Peak Envelope PowerPTT Push To TalkPWR PowerRC Reduced CarrierRCVR ReceiverRDY ReadyREF ReferenceRF Radio FrequencyPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 G-210640I00.SLK Mar/200323-10-09RMU Radio Management UnitRTCA Radio Technical Commission for AeronauticsRTN ReturnRX ReceiveSELCAL SELective CALlingSELECTIVITY The ability of a receiver to differentiate desired RF signals from undesired signals and other disturbances within specified frequency and dB limits.SENSITIVITY The ability of a receiver to detect and demodulate desired signals at specified minimum RF levels.SIDETONE The small portion of the transmitter signal that is fed back to the receiver’s audio circuit.SIG SignalSQUELCH The ability to disable the demodulated output of a radio receiver until a preset level of RF input is received. The level of received RF signal required to break squelch is determined by the squelch control setting.SSB Single Side BandSYN Synthesize(r), Synchronize(r)TCXO Temperature compensated crystal oscillatorTRANLINE Transmission LineTX TransmitUSB Upper Side BandVOL VolumeVSWR Voltage Standing Wave RatioXCTR Exciter (low level signal source that drives power amplified transmitted signal).XMT TransmitXMTR TransmitterGlossary of Terms and AbbreviationsPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 110640I00.SLK Mar/200323-10-09DESCRIPTION AND OPERATION1. System DescriptionA basic KHF 1050 HF Communication System consists of three individual units: KAC 1052 Antenna Coupler, KPA 1052 Power Amplifier, and KRX 1053 Receiver/Exciter. A compatible control unit is also required. Control units compatible with the system include the Gables PS440, Honeywell MCDU Multifunction Control and Display Unit and Honeywell RM-855 Radio Management Unit.NOTE: For complete installation information on the Gables PS440 refer to the PS440 Control Display Unit Installation Manual P/N 006-10655-0000.For complete installation information on the MCDU Multfuntion Control and Display Unit refer to the MCDU Installation Manual P/N XXXX.For complete installation information on the RM-855 Radio Management Unit refer to the RM-855 Installation Manual P/N XXXX.Typical SystemFigure 1Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 210640I00.SLK Mar/200323-10-09PS440 Control Display UnitFigure 2MCDU Multfunction Control and Display UnitFigure 3Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 310640I00.SLK Mar/200323-10-09RM-855 Radio Management UnitFigure 41.A. System OverviewThe KHF 1050 HF voice and data communication system is a solid state design with 200 watts (PEP) of output power, operating at 28 Vdc. Frequency of operaton ranges between 2.0 and 29.9999 MHz with 100 Hz resolution. Systems may be strapped to set the upper frequency limit to 22.9999 MHz.NOTE: Operations are limited to 25 MHz for aircraft installation by aeronautical mobile band frequency limits.A configuration is called a “dual system” when two KHF 1050 HF systems are installed in the same aircraft to share one antenna. Both systems may receive simultaneously, but only one system is chosen to transmit at any one time. An auto select transmit scheme determines which system is selected to transmit.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 410640I00.SLK Mar/200323-10-09In an auto select configuration, the first system (System 1 or System 2) to be keyed is selected to transmit, and transmission from the other system is inhibited until the first system has stopped transmitting.The RM-855 Radio Management Unit, the MDCU Multifunction Control Display Unit, or the PS440 Stand-Alone HF Controller determines the frequency and mode of operation of the system and displays that information to the pilot.Receiver and low level transmitter signals are located in the KRX 1053 Receiver/Exciter. The KRX 1053 Receiver/Exciter employs an oven controlled oscillator, which requires a short warm-up period to generate the frequency reference required for the synthesizer.The KAC 1052 Power Amplifier amplifies the excitation signal from the KRX 1053 Receiver/Exciter to 200 watts PEP, or 50 watts of carrier power in AM. The amplified signal is routed to the KAC 1052 Antenna Coupler, which matches the various impedances of the antenna to the 50 ohm output of the transmitter. In receive function, signals from the antenna pass through the KAC 1052 Antenna Coupler to the KRX 1053 Receiver/Exciter.The KHF 1050 can be installed as a single or dual HF system. In a dual system when one system is transmitting, receive on the other system is disbled. The single antenna in a dual system can be tuned to only one frequency at any given time. If the two systems are tuned to different frequencies, the strongest reception is realized on the primary system, which is tuned to the same frequency as the antenna. The primary system is defined as the system that was last used for transmission in auto-select configuration. The secondary system would employ an internal bridging amplifier to improve reception. No external accessories ae required for dual system operation for the KHF 1050.When two independent HF systems employing two separate antennas are used on one aircraft, it is important to maximize separation between the antennas. A minimum of 6 ft. (2 m.) separation is recommended and the antennas should be configured as orthogonally as possible.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 510640I00.SLK Mar/200323-10-09WARNING: IN A DUAL KHF 1050 INSTALLATION, PERMANENT DAMAGE WILL OCCUR TO THE SYSTEM IF EITHER THE RF OR DC CABLES ARE NOT CONNECTED PROPERLY BETWEEN HF1 AND HF2. IT IS RECOMMENDED THAT HF1 CABLES BE COLOR CODED RED AND HF2 CABLES BE COLOR CODED GREEN.Several operating mode options are available for the KHF 1050 HF system to meet particular operational needs.USB (upper sideband A3J) AME (amplitude modulation equivalent A3H) are standard modes of operation permitted on all system configurations.LSB (lower sideband A3J) operation is not permitted for stations operating under Part 87 FCC (USA) regulations. LSB may be enabled for use in regions or applications where its use is authorized.A seldom used mode A3A (USB reduced carrier) if available for use in locations that may utilize the mode.Table 23, Modes of Operation, lists the modes of operation applicable to the PS440, MCDU, and RM-855 controllers.The system is capable of operating in a channel (frequency preset) mode or a direct frequency mode. A microcomputer within the system provides the following functions:• controls the non-volatile storage of frequency, mode and channel data• controls a multiplexed eight-digit frequency display• provides synthesizer serial data tuning information• provides tune and transmit mode control logic• provides band switching information• preset antenna tune• built-in test with fault displayDashed lines and shaded boxes in the block diagram, Figure 5, indicate for future use.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 610640I00.SLK Mar/200323-10-09Typical System Block DiagramFigure 5Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 710640I00.SLK Mar/200323-10-09This version of the block diagram does not attempt to show the interconnectins between the receiver/exciter, the power amplifier, and the antenna coupler.This version of the block diagram corresponds to the content of Technical Specification Rev C, January, 2002.1.B. System Component DescriptionsThe required and optional equipment of a KHF 1050 HF Communication System is listed below:• KAC 1052 Antenna Coupler (required)• KPA 1052 Power Amplifier (required)• KRX 1053 Receiver/Exciter (required)• Compatible HF Control Display Unit (required)• Mounting Tray Hardware (optional)1.B.(1) KAC 1052 Antenna Coupler(P/N 064-01074-0001)Under microprocessor control, the KAC 1052 antenna coupler selects tuning network configurations, impedance transformations and binary capacitance and inductance to produce a VSWR of 2.5:1 or less upon initial tune. The VSWR may then deteriorate to 3:1 before the coupler will retune when transmit is next initiated.1.B.(2) KPA 1052 Power Amplifier(P/N 064-01072-0101)The KPA 1052 is a high frequency power amplifier. From 2.0 to 29.999MHz, the power amplifier is capable of linear amplification of a 0dBm signal to a 200 Watt output level at 50 ohms input and output impedance.1.B.(3) KRX 1053 Receiver/Exciter(P/N 064-01073-0101)The KRX 1053 is a high frequency receiver/exciter that is designed to operate from 2.0 to 29.999MHz synthesized in 100Hz steps. The unit will operate Amplitude Modulation Equivalent, Upper and Lower Sideband modes and Required-Carrier mode.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 810640I00.SLK Mar/200323-10-091.B.(4) Gables PS440 Control Display Unit(P/N 071-01605-0101, -0201, -1101, -1201, -2101)The PS440 stand-alone HF COMM Control Panel is designed to provide control of a single or dual HF COMM radio system. Full operational control of the HF system is accomplished via a dedicated low speed, digital ARINC 429 bus.1.B.(5) MCDU Multfunction Control and Display Unit(P/N 7025725-901, -910, -920, -930, -940)This multi-function radio controller provides control of all the functions of the KHF 1050 system via ARINC 429. Frequency, channel, squelch type and level, emission type and power level are selected from the MCDU.1.B.(6) RM-855 Radio Management Unit(P/N 7013270-967/968)The RM-855 displays frequency, mode and maintenance information. Via the ARINC 429 bus it provides frequency, channel, transmitter power and squelch level selection. It also has fault monitoring and fault annunciation.1.C. Component Installation KitsCOMMENTARY: THE FOLLOWING INSTALLATION KIT INFORMATION IS PRELIMINARY, PENDING CHANGE ORDER RELEASE.1.C.(1) KAC 1052 Antenna Coupler Installation KitsKAC 1052 Single Vertical Installation Kit(P/N:050-03658-0000)Table 1Part Number Description UM Qty030-00005-0000 CONN BNC UG 99C/U EA 1030-01157-0011 SOCKET CRMP 20G EA 37030-03517-0004 CONN, D-SUB, RECPT, CRMP, HOOD, 37 POS EA 1047-06261-0036 GROUND STRAP EA 1057-05944-0027 VERT TSO KIT LABEL, KAC 1052 EA 1071-00200-0000 VERT TRAY ASSEMBLY KAC 1052 EA 1Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 910640I00.SLK Mar/200323-10-09KAC 1052 Single Vertical Installation Kit (tray only)(P/N:050-03658-0001)Table 2KAC 1052 Single Vertical Install Kit (connectors only)(P/N:050-03658-0002)Table 3KAC 1052 Single Horizontal Installation Kit(P/N:050-03660-0000)Table 4Part Number Description UM Qty057-05944-0034 VERT TSO KIT LABEL, KAC 1052 EA 1071-00200-0000 VERT TRAY ASSEMBLY, KAC 1052 EA 1Part Number Description UM Qty030-00005-0000 CONN BNC UG 88C/U EA 1030-01157-0011 SOCKET CRMP 20G EA 37030-03517-0004 CONN, D-SUB, RECPT, CRMP, HOOD,37 POS EA 1057-05944-0036 TSO KIT LABEL EA 1Part Number Description UM Qty030-00005-0000 CONN BNC UG 88C/U EA 1030-01157-0011 SOCKET CRMP 20G EA 37030-03517-0004 CONN, D-SUB, RECPT, CRMP, HOOD,37 POS EA 1047-06261-0036 GROUND STRAP EA 1047-12728-0001 KAC 1052 GROUND STRAP EA 1057-05944-0029 HORIZ TSO KIT LABEL, KAC 1052 EA 1071-00202-0000 HORIZ TRAY ASSEMBLY, KAC 1052 EA 1155-02988-0015 HN CABLE EA 1Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 1010640I00.SLK Mar/200323-10-09KAC 1052 Dual Vertical Installation Kit(P/N:050-03661-0000)Table 5KAC 1052 Dual Vertical Installation Kit (tray only)(P/N:050-03661-0001)Table 6KAC 1052 Dual Vertical Installation Kit (connectors only)(P/N:050-03661-0002)Table 7Part Number Description UM Qty030-00005-0000 CONN BNC UG 88C/U EA 2030-01157-0011 SOCKET CRMP 20G EA 74030-03517-0004 CONN, D-SUB, RECPT, CRMP, HOOD, 37 POS EA 2047-06261-0036 GROUND STRAP EA 2057-05944-0030 DUAL VERT KAC 1052 TSO KIT LABEL EA 1071-00200-0000 VERT TRAY ASSEMBLY KAC 1052 EA 2Part Number Description UM Qty057-05944-0035 DUAL VERT TSO KIT LABEL, KAC 1052 EA 1071-00200-0000 VERT TRAY ASSEMBLY, KAC 1052 EA 2Part Number Description UM Qty030-00005-0000 CONN BNC UG 88C/U EA 2030-01157-0011 SOCKET CRMP 20G EA 74030-03517-0004 CONN, D-SUB, RECPT, CRMP, HOOD,37 POS EA 2057-05944-0039 TSO KIT LABEL EA 1Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 1110640I00.SLK Mar/200323-10-091.C.(2) KPA 1052 Power Amplifier Installation KitsKPA 1052 Single Horizontal Installation Kit(P/N:050-03629-0000)Table 8KPA 1052 Installation Kit (tray only)(P/N:050-03629-0001)Table 9KPA 1052 Installation Kit (connectors only)(P/N:050-03629-0002)Table 10Part Number Description UM Qty030-00005-0000 CONN BNC UG 88C/U EA 2030-01157-0011 SOCKET CRMP 20G EA 25030-01466-0002 CONN, D-SUB, CONTACT, CRMP, PWR, SIZE 8 EA 2030-03516-0001 CONN, D-SUB, RECPT, COMBO-27W2, CRMP EA 1057-05944-0022 TSO KIT LABEL EA 1071-00185-0000 TRAY ASSEMBLY EA 1Part Number Description UM Qty057-05944-0033 KSO KIT LABEL, KPA 1052 EA 1071-00185-0000 TRAY ASSEMBLY EA 1Part Number Description UM Qty030-00005-0000 CONN BNC UG88C/U EA 2030-01157-0011 SOCKET CRMP 20G EA 25030-01466-0002 CONN, D-SUB, ACCESSORY, CONTACT, CRMP, PWREA 2030-03516-0001 CONN, D-SUB, RECPT, COMBO - 27W2, CRIMP, HOOD, V-LOCEA 1057-05944-0037 TSO KIT LABEL EA 1Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 1210640I00.SLK Mar/200323-10-091.C.(3) KRX 1053 Receiver/Exciter Installation KitsKRX 1053 Installation Kit(P/N 050-03628-0000)Table 11KRX 1053 Installation Kit (tray only)P/N 050-03628-0001Table 12KRX 1053 Installation Kit (connectors only)P/N 050-03628-0002Table 13Part Number Description UM Qty030-00005-0000 CONN BNC UG 88C/U EA 1030-01451-0000 CONTACT SOCKET EA 104030-03518-0001 CONN, D-SUB, RECPT, HI-DENS, W/HOOD, 104 POSEA 1057-05944-0021 TSO KIT LABEL EA 1071-00184-0000 TRAY ASSEMBLY EA 1Part Number Description UM Qty057-05944-0032 TSO KIT LABEL EA 1071-00184-0000 TRAY ASSEMBLY EA 1Part Number Description UM Qty030-00005-0000 CONN BNC UG88C/U EA 1030-01466-0001 CONN D-SUB,ACCESSORY, CONTACT 22AWG, CRMP, FEMALEEA 104030-03518-0001 CON, D-SUB, ACCESSORY, HOOD, 104 POS EA 1057-05944-0038 TSO KIT LABEL EA 1Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 1310640I00.SLK Mar/200323-10-09Long-Wire Antenna Installation Kit(P/N:071-01214-0001)Table 141.D. Equipment Required But Not SuppliedPart Number Description UM Qty3280 VERTICAL FIN ANCHOR KIT EA 15 ARM 200-6LV VERTICAL FIN “V” TENSION KIT EA 150 ARM 300-205 ANTI-PRECIPITATION ANTENNA WIRE FT 4525 ARM 300-20E 30° FEED-THROUGH INSULATOR EA 150 ARM 300-250 WIRE RELEASE TOOL EA 1FORM #101 INSTALLATION INSTRUCTIONS EA 116390 FEED-THROUGH ASSEMBLY EA 1Equipment Required But Not SuppliedAIRCRAFT EQUIPMENT DESCRIPTIONPower 28 Vdc Primary power source.Lighting Bus 5 Vac, 5 Vdc or 28 Vdc Panel lighting power source for control units, according to version installed.Microphone Noise cancelling, 150 ohms nominal, pre-amplified.Headphones Approx. 600 ohms.Selective Calling DecoderAVTGARequired if SELCAL operation is desired. Ground Strap 047-06261-0036 36” lengthLong Wire HF Antenna Long Wire HF Antenna Kit available as P/N 071-01214-0000.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 1410640I00.SLK Mar/200323-10-09Grounded Tranline Grounded tranline: Towel bar with 1 inch diameter recommended. Contact:Trivec-Avant Corp.17831 Jamestown Ln.Huntington Beach, CA 92647714-841-4976WIRE: Available as:RG 400 Double shielded coax P/N 024-00075-0000RG 142B/U Double shielded coax P/N 024-00002-000024 AWG Single conductor P/N 025-00029-000920 AWG Single conductor P/N 025-00031-000016 AWG Single conductor P/N 025-00031-000324 AWG Single conductor with shield and jacket P/N 025-05018-000018 AWG Single conductor with shield and jacket P/N 025-05019-000024 AWG Two conductor with shield and jacket P/N 025-05020-000024 AWG Three conductor with shield and jacket P/N 025-05023-0000CABLE:AN-22a 755 Nominal Circular Mil Area*0.090 inches Max. Overall Diameter16.45 ohms Max. per 1000 feet @ 20°C8 amps Max. Cont. Current Rating**5 amps Max. Cont. Current Rating***AN-20 1,200 Nominal Circular Mil Area*0.100 inches Max. Overall Diameter10.25 ohms Max. per 1000 feet @ 20°C11 amps Max. Cont. Current Rating**7.5 amps Max. Cont. Current Rating***Equipment Required But Not SuppliedAIRCRAFT EQUIPMENT DESCRIPTIONPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 1510640I00.SLK Mar/200323-10-09AN-18 1,909 Nominal Circular Mil Area*0.115 inches Max. Overall Diameter6.44 ohms Max. per 1000 feet @ 20°C16 amps Max. Cont. Current Rating**10 amps Max. Cont. Current Rating***AN-16 2,409 Nominal Circular Mil Area0.130 inches Max. Overall Diameter4.76 ohms Max. per 1000 feet @ 20°C22 amps Max. Cont. Current Rating**13 amps Max. Cont. Current Rating***AN-14 3,830 Nominal Circular Mil Area0.150 inches Max. Overall Diameter2.99 ohms Max. per 1000 feet @ 20°C32 amps Max. Cont. Current Rating**17 amps Max. Cont. Current Rating***AN-12 6,088 Nominal Circular Mil Area0.170 inches Max. Overall Diameter1.88 ohms Max. per 1000 feet @ 20°C41 amps Max. Cont. Current Rating**23 amps Max. Cont. Current Rating***High Voltage HN Cables:155-02988-2215 Designed for single 1050 installation. Length is 15” 38.1 cm). Both connectors are straight. 155-02989-0001 Designed for dual 1050 installation. Total length is 16” (40.64 cm). Common leg is 6” (15.24 cm). Each separate leg is 10” (25.4 cm). All three connectors are straight.155-02988-0121 Designed for single 1050 installaton. 21” (53.34 cm) length center, both connectors right angle, 180 degree indexing (one connector up, one down).Equipment Required But Not SuppliedAIRCRAFT EQUIPMENT DESCRIPTIONPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 1610640I00.SLK Mar/200323-10-09Equipment Required But Not SuppliedTable 15WARNING: THE HIGH VOLTAGE HN CABLES ARE SPECIFICALLY DESIGNED TO WITHSTAND THE HIGH VOLTAGE GENERATED BY THE KHF 1050 SYSTEM. THEY CAN NOT BE REPLACED BY CABLES THAT HAVE NOT BEEN TESTED TO THESE HIGH VOLTAGES AT ALTITUDE. THESE CABLES SHOULD BE PURCHASED DIRECTLY FROM HONEYWELL, OR FROM THE QUALIFIED VENDOR (CANTON CONNECTOR CORP, 26 WAPPING ROAD, KINGSTON, MA, 02364, 781-585-4315).1.E. Related PublicationsRelated PublicationsTable 16155-02988-0015 Designed for single 1050 installation. Length is 15” (38.1 cm). Both connectors are right angle with the same orientation.Miscellaneous installation hardwaremounting bracketswirecablesnutsboltsPart Number Description006-15640-0000 KAC 1052 Antenna Coupler Maintenance Manual006-15641-0000 KPA 1052 Power Amplifier Maintenance Manual006-15642-0000 KRX 1053 Receiver/Exciter Maintenance Manual006-15655-0000 PS440 Control Display Unit Maintenance ManualA09-3642 MCDU Multfunction Control and Display UnitMainenance Manual???? RM-855 Radio Management Unit Maintenance ManualEquipment Required But Not SuppliedAIRCRAFT EQUIPMENT DESCRIPTIONPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 1710640I00.SLK Mar/200323-10-09NOTE: An Aircraft Station License is required for KHF 1050 HF system equipment. Forms (FCC Form 404, New Aircraft Station License, or FCC 405A, Renewal of Aircraft Station License) can be obtained from the nearest FCC Field Office.2. Component ConfigurationsSystem component configurations are listed in this section. The overall configuration of a KHF 1050 HF system is dependent on the component versions installed in the aircraft.2.A. KAC 1052 Antenna Coupler Unit ConfigurationsKAC 1052 ConfigurationsTable 172.B. KPA 1052 Power Amplifier ConfigurationsKPA 1052 ConfigurationsTable 182.C. KRX 1053 Receiver/Exciter ConfigurationsKRX 1053 ConfigurationsTable 19PART NUMBER VERSION DESCRIPTON064-01074 -0101 Antenna Coupler - standardPART NUMBER VERSION DESCRIPTION064-01072 -0101 Power Amplifier - standardPART NUMBER VERSION DESCRIPTION064-01073 -0101 Receiver/Exciter - standardPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 1810640I00.SLK Mar/200323-10-092.D. PS440 Control Display Unit ConfigurationsPS440 ConfigurationsTable 202.E. MCDU Multfunction Control and Display Unit ConfigurationsMCDU ConfigurationsTable 212.F. RM-855 Radio Management Unit ConfigurationsRM-855 ConfigurationsTable 22PART NUMBER VERSION BEZEL LCD BACKLIGHTING071-01605 -0101 Gray White071-01605 -0201 Black White071-01605 -1101 Gray Amber071-01605 -1201 Black Amber071-01605 -2101 Gray NVIS071-01605 -2201 Black NVISPART NUMBER VERSION USER7025725 -901 Hawker Horizon7025725 -910 Planeview GV, Cessna Sovereign7025725 -920 (no user at present)7025725 -930 Embraer ERJ 1707025725 -940 Agusta AB139PART NUMBER VERSION FEATURES BEZEL7013270 -967 Radio Management Unit - HF Gray7013270 -968 Radio Management Unit - HF BlackPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 1910640I00.SLK Mar/200323-10-093. System Leading Particulars3.A. General SpecificationsThe KHF 1050 HF System is a solid state design with 200 watts PEP of output power, supplied by 28 VDC, with an operational frequency range of 2.0 to 29.9999 MHz with 100kHz resolution. The KHF 1050 HF System has been type accepted by the FCC and TSO approved.3.B. System Operating Modes3.B.(1) Emission ModesSeveral operating mode options are available for the KHF 1050 HF system to meet particular operational needs.USB (upper sideband, A3J) AME (amplitude modulation equivalent A3H) are standard modes of operation permitted on all system configurations.LSB (lower sideband, A3J) operation is not permitted for stations operating under Part 87 FCC (USA) regulations. LSB may be enabled for use in regions or applications where its use is authorized.AM or AME (amplitude modulation equivalent, A3H) may be used in some areas that lack single-sideband (SSB) capabilities. AME is a form of amplitude modulation that is more efficient than full AM, yet compatible with AM systems.USB Data and LSB Data are the same as the above-mentioned USB and LSB modes, except receiver audio and transmitter audio are connectedto a data-modem rather than to a speaker or microphone.A seldom used mode A3A (USB reduced carrier) is available for use in locations that may utilize the mode.Table 25, Modes of Operation, lists the modes of operation applicable to the PS440, MCDU and RM-855.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2010640I00.SLK Mar/200323-10-09Modes of OperationTable 233.B.(2) 23 MHz Limit ModeThe KHF 1050 HF system can be strapped to limit the frequency of operation to an upper limit of 22.9999 MHz for certification in countries that may require such an upper frequency limit.3.B.(3) Channel ModeWhen operating in the channel mode the KHF 1050 HF system can operate as a simplex, semi-simplex, or receive only communication system. Transmit and receive frequencies are selected by selecting a pre-programmed channel.3.B.(4) Direct Frequency ModeWhen operating in the direct frequency mode the KHF 1050 HF system can operate as a simple communication system only. Transmit and receive frequency is determined by the selected frequency, which is entered directly on the control unit.MODE OF OPERATION DESIGNATOR CONTROL UNIT DESIGNATORTECHNICALALTERNATE PS440 MCDU RM-855OLD NEWA3H H3E AME AM Equivalent AM AM AMA3A R3E AM Reduced Carrier RC RCA3J J3E USB Upper Sideband UV UV UVA3J J3E LSB Lower Sideband LV LV LVA7J J2D USB Data Upper Sideband Data UD UD UDA7J J2D LSB Data Lower Sideband Data LD LD LDH2D AM Data Amplitude Modulation Data AM AM AMPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2110640I00.SLK Mar/200323-10-093.B.(5) Data ModeWhen the KRX 1053 Receiver/Exciter is operating in the DATA mode, interface with data modems or secure voice systems is enabled. The external modem inputs and external modem outputs are available to bypass squelch and compression functions in the KRX 1053. These levels are controlled by field adjustments.A 4 dB variation is possible in the audio response when operating in the data mode.Audio modulation from the modem is applied to the EXTERNAL MODEM AUDIO INPUT. When the DATA KEYLINE is grounded, the transmitter modulation is derived from the DATA AUDIO INPUT rather than from the microphone.3.B.(6) SELCAL ModeNOTE: SELCAL mode requires a SELCAL decoder, not supplied.SELCAL (SELective CALling) may be used to relieve background noises during flight. The volume may be turned down completely while the system maintains a watch for a SELCAL coded audio signal.When a decoded SELCAL signal is received, a call waiting is indicated. The SELCAL decoder generates an audio alert for the crew.The SELCAL AUDIO OUTPUT is connected to the external SELCAL decoder. Regardless of the operating mode selected by the pilot, the SELCAL AUDIO OUTPUT is derived from an AM receiver inside the KRX 1053.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2210640I00.SLK Mar/200323-10-093.C. Component Leading ParticularsLeading particulars for components of the KHF 1050 HF system are listed below.3.C.(1) KAC 1052 Antenna Coupler, Leading ParticularsKAC 1052 Leading ParticularsTable 243.C.(2) KPA 1052 Power Amplifier, Leading ParticularsKPA 1052 Leading ParticularsTable 253.C.(3) KRX 1053 Receiver/Exciter, Leading ParticularsKRX 1053 Leading ParticularsTable 26CHARACTERISTIC DESCRIPTIONWeight: Refer to Figure 2028 (P/N 155-01774-2028)Dimensions: Refer to Figure2028 (P/N 155-01774-2028)Connector: Refer to figure 2009 (J10521) and table 2001.CHARACTERISTIC DESCRIPTIONWeight: Refer to figure2031 (P/N 155-01450-0000) Dimensions: Refer to figure2031 (P/N 155-01450-0000) Connector: Refer to figure 2010 (J10524) and table 2002.CHARACTERISTIC DESCRIPTIONWeight: Refer to Figure 2032 (P/N 155-01751-0000)Dimensions: Refer to Figure 2032 (P/N 155-01751-0000)Connector: Refer to figure 2011 (J10531) and table 2003.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2310640I00.SLK Mar/200323-10-093.C.(4) PS440 Control Display Unit, Leading ParticularsNOTE: Refer to the PS440 Control Display Unit Component Maintenance Manual P/N 006-15655-XXXX for more description of the PS440.PS440 Leading ParticularsTable 273.C.(5) MCDU Multifuction Control and Display Unit, Leading ParticularsNOTE: Refer to the MCDU Multifunction Control and Display Unit Maintenance Manual P/N A09-3642 for more description of the MCDU.MCDU Leading ParticularsTable 28CHARACTERISTIC DESCRIPTIONWeight: Refer to Figure 2022 (P/N ???)Dimensions: Refer to Figure 2022 (P/N ???)Connector: Refer to figure 2011 (J1) and table 2004.CHARACTERISTIC DESCRIPTIONWeight: Refer to figure 2023 (P/N 7025726-930)Dimensions: Refer to figure 2023 (P/N 7025726-930)Connector: Refer to figure 2016 (J???) and table 2007.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2410640I00.SLK Mar/200323-10-093.C.(6) RM-855 Radio Management Unit, Leading ParticularsNOTE: Refer to the RM-855 Radio Management Unit Component Maintenance Manual P/N ??? for more description of the RM-855.RM-855 Leading ParticularsTable 294. System Function4.A. System Functional OverviewThe KHF 1050 HF Communication System supports a wide variety of communication requirements. The major components of the KHF 1050 HF system are listed below:yKAC 1052 Antenna CoupleryKPA 1052 Power AmplifieryKRX 1053 Receiver/ExciteryCompatible Control Display UnitThe basic KHF 1050 HF system is a mobile communication system for aircraft. It operates in a frequency range between 2.0 and 29.9999 MHz offering several different emission modes to provide voice communication.By including the appropriate components in an installation, the KHF 1050 HF system capabilities can be increased to allow the system to support Data, SELCAL, and Secure Voice communication.4.A.(1) System Power UPCOMMENTARY: INSERT POWER-UP DESCRIPTION HERE.CHARACTERISTIC DESCRIPTIONWeight: Refer to figure 2026 (P/N 7013270)Dimensions: Refer to figure 2026 (P/N 7013270)Connector: Refer to figure 2016 (J???) and table 2007.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2510640I00.SLK Mar/200323-10-094.A.(2) Channel OperationCOMMENTARY: INSERT CHANNEL OPERATION DESCRIPTION HERE.4.A.(3) Direct Frequency ModeCOMMENTARY: INSERT DIRECT FREQUENCY MODE OPERATION HERE.4.B. Dual SystemCOMMENTARY: INSERT ANY DUAL SYSTEM FUNCTIONALITY INFO HERE.5. Component Functions5.A. PS440 Control Display Unit Unit FunctionSee Pilots Guide P/N 006-18289-0000 for PS440 Control Display Unit operation.5.B. MCDU Multfunction Control and Display Unit FunctionSee Pilots Guide P/N XXXX for MCDU Multfunction Control and Display Unit operation.5.C. RM-855 Radio Management Unit FunctionSee Pilots Guide P/N XXXX for RM-855 Radio Management Unit operation.6. System Inputs/Outputs6.A. Input/Output SignalsSee Paragraph 5.C.(5) in the Installation and Maintenance section of this book.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 100110640I00.SLK Mar/200323-10-09TESTING AND FAULT ISOLATION1. Fault IsolationFault isolation locates the source of system failure at the black box or aircraft wiring level. Fault isolation is typically performed on the ground in response to failures indicated during post-installation checkout, preflight testing, or flight operation.Perform the System Performance Check (Paragraph 2.) and refer to the Fault Isolation Checklist (Paragraph 3.) for fault isolation in the KHF 1050 HF system.2. System Performance CheckThe system check detects problems in the installation that may cause the HF system to fail, to degrade performance, or cause damage to the HF system, such as:yIntermittent or improperly connected cables or connectors.yDefective units.yPoorly regulated aircraft DC power.yPoor grounding of KHF 1050 HF system or poor aircraft bonding.yAudio ground loops.yRF interference.CAUTION: POWER CARTS MAY REGULATE POORLY WHEN SUBJECTED TO STRONG RF FIELDS. IF MORE THAN 20% FLUCTUATIONS IN POWER CART VOLTAGES ARE NOTED WHEN TRANSMITTING, DO NOT CONTINUE TESTING WITH POWER CART.CAUTION: SOME INTERMITTENT CONDITIONS MAY CAUSE OUTPUT TRANSISTORS TO FAIL, THEREFORE TRANSMIT ONLY AFTER OTHER CHECKS HAVE SUCCESSFULLY COMPLETED.Perform the steps in the stated sequence.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 100210640I00.SLK Mar/200323-10-092.A. Preliminary Check1. Prior to turning the system on, ensure that all connectors are properly seated in their proper location.2. Turn the system on. As the system turns on it performs a brief self-test.Normally, after a few seconds, the HF controller (or HF window of a multi-function controller) will show an HF operating frequency, mode of operation and other operating parameters. Refer to the operating manual for the specific controller for specific operation and the information available on the display.3. Push the TEST button on the controller to perform a system test. The pilot-activated self-test takes approximately 15 seconds to complete.4. KXR 1053 Receiver/Exciter Built-In-TestThe receiver/exciter design incorporates provisions for monitoring its own operation to detect any condition or occurrence that the operator (a flight crew member) might observe and interpret as a reason for requesting a maintenance action.These maintenance observations are stored in non-volatile memory within the receiver/exciter so they can be retrieved with appropriate test equipment.If a sufficiently serious fault is detected, the “receiver/exciter status” bit of the Maintenance Status message, label 351, is set to indicate a fault.The maintenance data collection provision includes the following three types of monitoring: Power-On, Continuous Monitoring and Initiated Tests. The BITE tests that shall be performed at system turn-on, at pilot activated, or continuously are summarized in Table 1001. The table shows which tests are performed for each of the three types of monitoring.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 100310640I00.SLK Mar/200323-10-09RX/EX BITE MatrixTable 1001FUNCTION TURN ON PILOT CONT Label 351Discrete Line Check X 29Flash ROM Checksum X 29DSP ROM X X 29DSP RAM X X 29DSP CLOCK (60MHz) X X 29RF Board XMT Operation X X 29RF Board RCV Operation X X 29RF Board DSP Clock (60MHz) X X 2915V Power Line X X 299V Power Line X X 293.3V Power Line X X 29PRIMARY Power Fail(28V Power Line Voltage)XXX29Rx/Ex Internal Temperature X 29PA OK/NG X X X 18ACP OK/NG X X X 28Rx/Ex - CPLR Serial Communication X X 29ACP WARN X 15ACP Tune Fail X 28 Note 1Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 100410640I00.SLK Mar/200323-10-095. KPA 1052 Power Amplifier Built-In-TestThe power amplifier design incorporates provisions for monitoring its own operation to detect any condition or occurrence that the operator (a flight crew member) might observe and interpret as a reason for requesting a maintenance action.The maintenance data collection provision includes the following three types of monitoring: Power-On Test, Conditions Monitoring and Initiated test, as defined below.PA Alarm 1 - This alarm will be generated whenever the SWR at the input to the antenna coupler is too high. The antenna coupler will try to retune to lower SWR during transmit mode.PA Alarm 2 - This alarm will be generated whenever an invalid band error request occurs, a higher than normal SWR within the PA is generated, a higher than normal output power occurs, an over-temperature condition exists, or the PA has no output power. This alarm inhibits all transmissions.The BITE tests that shall be performed at system turn-on, at pilot activated or continuously are summarized in Table 1002.PA BITE MatrixTable 1002FUNCTION POWER ON PILOT CONTLabel 351 Bit Note 1Load SWR (PA ALM#1) During Tx Only X 18Temperature (PA ALM#2) X 18Transmitter Power at 50 W(With KAC 1052 in the system)XX 18Note1: PA ALM#1 and PA ALM#2 are sent to the KAC 1052 with discrete lines. The KAC 1052 then sends the PA Alarm data to the KRX 1053. Label 351 information is actually sent by the KRX 1053.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 100510640I00.SLK Mar/200323-10-096. KAC 1052 Antenna Coupler Built-In-TestThe antenna coupler design incorporates provisions for monitoring its own operation to detect any condition or occurrence that the operator (a flight crew member) might observe and interpret as a reason for requesting a maintenance action.These maintenance observations are stored in non-volatile memory within the antenna coupler so they can be retrieved with appropriate test equipment.If the maintenance observation is serious enough to indicate Antenna Coupler failure, the failure shall be communicated to the receiver/exciter for reporting to the HF controller.The BITE tests that shall be performed at system turn-on, at pilot activation or continuously are summarized in Table 1003.FUNCTIONPOWERON PILOT CONTLabel 351 Bit Note 1Internal memory X 2812V Power Line 285V Power Line X 28Bridge amplifier output voltage X 28Low pressure alarm signal (PRESS ALM) X X 15Leak pressure warning level(Temp, Press)X X 15 & 28RF power level and Power Sensor X 28PA alarm #1 signal (PA ALM#1)During Tx OnlyXX 18PA alarm #2 signal (PA ALM#2) X X 18VSWR sensor X 28Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 100610640I00.SLK Mar/200323-10-09Antenna Coupler BITE MatrixTablE 10037. In the event that a problem is detected during either the turn-on test or the pilot-activated self-test, an error message will appear on the controller. The error message may indicate a failure of one or more of the following:• Controller• Receiver/Exciter• Power Amplifier• Antenna CouplerRefer to Section 3, Fault Isolation Checklist.2.B. Receiver Performance Check1. If an operating frequency is properly displayed on the controller, listen to the speaker or headphones. Ensure that the aircraft audio panel is properly set to select the HP audio.2. Select the USB Voice (UV) mode, SBH type squelch. (SBH is the default squelch type. If using an RM855, only the SB type is available.) Adjust the squelch level to OFF. Adjust the volume control on the PS440 controller, and/or the volume control on the audio panel. Depending on the frequency or channel selected, a signal may be heard - or perhaps just atmospheric static.NOTE: If the aircraft is located in a metal hangar, both signals and noise may be weak. It is advisable to have the aircraft outside the hangar to perform the receiver or transmitter tests.Select a channel with a known usable signal. One possibility is one of the time-and-frequency standard stations operating on frequencies of 2500.0 MHz, 5000.0 MHz, 10000.0 kHz, 15000.0 kHz or 20000.0 kHz.Impedance sensors X 28Note 1: The Label 351 information is actually sent by the KRX 1053 in response to RS-422 serial data sent by the KAC 1052 to the KRX 1053.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 100710640I00.SLK Mar/200323-10-09These stations are located in Fort Collins, Colorado and Kekaha, Hawaii. Consult the HF frequency propagation chart in Table 2001 for an overview of the frequency to use for a particular time of day and distance from the transmitter. These stations transmit in the AM mode. However, they can be received by the KHF 1050 System in the USB Voice (UV), LSB Voice (LV), AM or Reduce-Carrier (RC) modes.If a signal can not be heard,check the connetion to the antenna, the antenna itself and ensure that all coaxial cables that interconnect the KHF 1050 System are properly connected.4. Adjust the squelch level as needed to LOW, MED or MAX to achieve the minimum level required to suppress the receiver noise with no signal present.2.C. Transmitter Performance Check1. Select the HF positon on the audio panel microphone switch.CAUTION: VERIFY THAT NO ONE IS STANDING ON THE GROUND NEAR THE AIRCRAFT OR TOUCHING THE AIRCRAFT. WITH MANY TYPES OF AIRCRAFT HF ANTENNAS, THE ENTIRE AIRFRAME BECOMES PART OF THE ANTENNA. ANYONE STANDING ON THE GROUND COULD RECEIVE AN ELECTRICAL SHOCK IF TOUCHING THE AIRCRAFT, OR IF ENTERING OR EXITING THE AIRCRAFT DURING A TRANSMISSION BY THE KHF 1050 SYSTEM. DO NOT OPERATE THE HF SYSTEM WHILE THE AIRCRAFT IS BEING FUELED.2. Select a channel on which the aircraft is authorized to transmit, with the apropriate mode of operation, which is typically USB Voice (UV). Momentarily press the PTT switch to start the antenna tuing process.Assuming the KAC 1052 Antenna Coupler has not previously been on this frequency, the antenna coupler will begin to tune to the antenna and the controller display will begin to indicate that tuning is taking place. Refer to the controller information for the details of how tuning is annunciated by the particular controller being used.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 100810640I00.SLK Mar/200323-10-09In the event that the operating frequency selected had previously been tuned by the KAC 1052 Antenna Coupler, the antenna coupler will utilize stored tune information and match to the antenna in less than 50msec. However, changes in antenna impedance can occasionally result in the KAC 1052 needing to retune on a previously tuned frequency.3. Upon completion of the tune cycle, the tune indication will disappear and the display will return to a normal recieve window. The receiver audio will likely be stronger than it was prior to tuning the antenna and it may be necessary to readjust the squelch if there is significant noise on the channel. The system is now ready to transmit voice communications.4. In order to ensure good audio quality of the transmitted signal, a microphone-ground-loop test is recommended. To check for microphone ground loops, select the AM mode on an unused frequency. Key the system with no modulation, preferably covering the microphone element with your hand. Listen for any squeal or popping sound in the speaker or headphones. A squeal or popping sound tends to indicate that a microphone ground loop exists. Microphone ground loops will result in distorted audio. Such a ground loop is usually the result of the microphone audio low line being tied to airframe ground at multiple points.5. Listen to the sidetone in the headphones or speaker while transmitting, both in USB Voice (UV) and in AM. A raspy sound may indicate that RF interference is feeding back into the HF or audio system.6. While transmitting a voice test message in USB Voice (UV), observe other electrical equipment in the aircraft and note any interference observed that correlates to the HF transmission.7. Voice communications should be established with a ground station or another aircraft. See Section 7.B.(4)(b).Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 100910640I00.SLK Mar/200323-10-093. Fault Isolation ChecklistFault Isolation ChecklistTable 1004FAULT ACTIONTurn-On or Pilot-Activated Self-Test Fault:1.2.3.Check the connections to each unit having an associated error condition.Verify that 28 VDC power is being applied to each unit and that the voltage is steady.Ensure the integrity of each coaxial cable in the system and verify that each is connected to the proper connectors.Tuning Fault: 1.2.3.4.5.Press PTT switch to retune antenna.If unit fails to retune, select a different frequency and try to retune the antenna at the new frequency.Turn the KHF 1050 system off and check the coaxial cable connections between the KAC 1052 and the antenna feedpoint.Ensure that there is no evidence of arcing in the connectors, antenna feed-through insulator or at the antenna.Check the antenna. If it is a grounded antenna, verify that the DC resistance to ground is very low. If it is an open wire antenna, verify that the resistance to ground is very high.Refer to the bonding information in Section 6A.Contact Honewell Product Support for further assistance.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 200110640I00.SLK Mar/200323-10-09INSTALLATION AND MAINTENANCE1. General CoverageThis section provides service personnel with installation and maintenance information pertaining to the following KHF 1050 HF Communication System components:yKAC 1052 Antenna CoupleryKPA 1052 Power AmplifieryKRX 1053 Receiver/ExciterNOTE: For installation and maintenance information on the Gables PS440 refer to the PS440 Control Display Unit Installation Manual P/N 006-10655-XXXX.For installation and maintenance information on the MCDU Multifunction Control and Display Unit refer to the MCDU Installation Manual P/N XXXX.For installation and maintenance information on the RM-855 Radio Management Unit refer to the RM-855 Installation Manual P/N XXXX.2. UnpackingUse care when unpacking KHF 1050 HF system components. Open shipping cartons and carefully remove all items. Check that all items on the packing list are included. Visually inspect each component for damage incurred during shipment: dents, deep abrasions, chipped paint, etc. If any component is damaged, notify the transportation carrier immediately.3. Pre-installation TestingAll components of the KHF 1050 HF system have been adjusted and tested before shipment and pre-installation testing is not required. If pre-installation bench testing of any unit is desired, refer to bench test section of the applicable maintenance manual. Refer to DESCRIPTION AND OPERATION, section 1.F., for a list of related maintenance manuals.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 200210640I00.SLK Mar/200323-10-094. Equipment Changes and MarkingsA standardized marking system identifies equipment with incorporated modifications. Refer to the Publication Index for a list of Service Bulletins affecting the various units in the KHF 1050 HF system.5. Installation Planning5.A General ConsiderationsGeneral information for installation of the KHF 1050 HF system, instructions for location of system components, interwiring and cable fabrication, and mode strapping options are provided in the following paragraphs. Interconnect diagrams at the end of this section show the interconnection of various system components.The KHF 1050 HF system should be installed in the aircraft in a manner consistent with acceptable workmanship and engineering practices and according to instructions set forth in this publication.The installer should make a thorough visual inspection and perform the post-installation and operational checks of the system to ensure that the system has been properly and safely installed in the aircraft.CAUTION: AFTER INSTALLATION OF THE CABLING AND BEFORE INSTALLATION OF THE EQUIPMENT, SUPPLY AIRCRAFT PRIMARY POWER TO THE CABLES AND CHECK THAT POWER IS APPLIED ONLY TO THE UNIT CONNECTOR PINS SPECIFIED IN THE INTERWIRING DIAGRAMS.5.B. Location of Equipment5.B.(1) KAC 1052 Antenna Coupler Mounting LocationRefer to Figure 2028 for mounting dimensions.The location of the KAC 1052 Antenna Coupler is critical. It must be located very close to the feedpoint of the antenna or the antenna feed-through insulator. In order to maximize the efficiency of the HF system, it is desireable to keep the length of the feedline less than 12 inches, if possible. The feedline should not exceed 24 inches, including the connector length.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 200310640I00.SLK Mar/200323-10-09NOTE: Due to the high level of RF voltage the KHF 1050 system is capable of generating, only a specially fabricated Honeywell feedline may be used. Refer to Section 1.C.(1) for appropriate part numbers.The KAC 1052 must be mounted in a location that will allow it to be well bonded to the airframe. See Section 6A for bonding considerations.For best reliability, the KAC 1052 should be mounted such that it is not subjected to excessive vibration or heat.The KAC 1052 can be mounted to either vertically or horizontally on a horizontal surface.5.B.(2) KPA 1052 Power Amplifier Mounting LocationRefer to Figure 2031 for mounting dimensions.The location of the KPA 1052 is generally not critical. It is recommended that it be mounted near the KAC 1052, to minimize loss in the coaxial cable interconnecting the KPA 1052 and the KAC 1052.The cable length between the KPA 1052 and the KAC 1052 should not exceed 50 feet.For best reliability, the KAC 1052 should be mounted such that it is not subjected to excessive vibration or heat.The KAC 1052 can be mounted to either a vertical or horizontal surface.5.B.(3) KRX 1053 Receiver/Exciter Mounting LocationRefer to Figure 2032 for mounting dimensions.Mount the KRX 1053 so that the connection between the KRX 1053 and the KAC 1052 does not exceed 50 feet. The KRX 1053 is typically mounted vertically on a horizontal surface.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 200410640I00.SLK Mar/200323-10-095.B.(4) Control Display Unit Mounting LocationRefer to Figures 2022, 2023 and 2026 for mounting dimensions.Refer to the installation manual for the PS440 Control Display Unit, P/N 006-10655-XXXX, for PS440 mounting instructions.Refer to the installation manual for the MCDU, P/N XXXX, for MCDU mounting instructions.Refer to the installation manual for the RM-855, P/N XXXX, for RM-855 mounting instructions.5.B.(5) Antenna LocationThe antenna is a primary factor for maximum performance of the KHF 1050 HF system. While numerous options are available in the choice of antenna configurations, some configurations are better suited for a particular installation than others. Commonly used aircraft HF antennas will generally fall into one of four categories:y"V" (Referring to the V shape formed by the antenna wire) and Long wire antenna.yShort grounded wire antenna.yShunt antenna.Characteristics of these commonly used antennas and the compromise associated with each type are described below, so the installer can select the antenna that is best suited to a particular aircraft and type of operation. All antennas should be installed in a manner that does not jeopardize the safe operation of the aircraft.5.B.(6)(a) "V" and Long Wire Antenna Mounting LocationBecause of their generally good performance, consideration should be given to the use of "V" and long wire antennas on all installations, except very high speed fixed wing aircraft and helicopters. Wire antennas are not recommended for use on helicopters, due to safety concerns in the event of an antenna wire breakage.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 200510640I00.SLK Mar/200323-10-09"V" and long wire antenna performance will be enhanced by striving to meet the following criteria:yMaximize the length of wire (up to approximately 60 feet or 18 m.). The total length of the antenna should be at least 25 feet (7.6 m).yMaximize the separation between the antenna wire and the aircraft structure. This is usually achieved by attaching the tensioner as high as possible on vertical stabilizers.5.B.(6)(a)1 Wing Tip “V” Antenna Mounting LocationThe wing type “V” is one of the most effective HF antennas which can be utilized on an aircraft. It is well suited for slow and moderate speed aircraft which require optimum HF communication and performance. It will exhibit a rather omnidirectional radiation pattern and provide good efficiency at all frequencies. It has the disadvantages of having high drag, and on low wing aircraft is prone to being walked into. The length of a wing tip “V” antenna is usually 30 to 45 feet (9.2 to 13.7 m).Typical Wing Tip “V” AntennaFigure 2001Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 200610640I00.SLK Mar/200323-10-095.B.(6)(a)2 Inverted “V” Antenna Mounting LocationThe inverted “V” antenna is recommended when a wing “V” is not practical and the antenna coupler is to be mounted in the aft position of the aircraft. The inverted “V” antenna will produce maximum signal strength off the side of the aircraft and will produce a moderate amount of drag.The vertical fin anchor should be located as high as possible on the vertical stabilizer. The feedthru insulator should be located approximately 3 feet (0.9 m) forward of the base of the vertical stabilizers and near the centerline of the top of the aircraft.Typical Inverted “V” AntennaFigure 20025.B.(6)(b) Long Wire Antenna Mounting LocationThe long wire antenna is used when the KAC 1052 Antenna Coupler is located in the forward part of the aircraft. It will provide maximum signal radiation off the sides of the aircraft. Significant nulls in signal strength may be noted off the nose and tail of the aircraft.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 200710640I00.SLK Mar/200323-10-09Typical Long Wire AntennaFigure 20035.B.(6)(c) Short Grounded Wire Antenna Mounting LocationShort grounded wire antennas may be utilized on higher speed and/or high altitude aircraft. These short wire antennas have a minimum drag and do not develop as high of RF voltages as do the longer wire antennas, making them suitable for operations up to 55,000 feet. However the efficiency of the short antenna will be lower, especially at the low frequencies.Typical short wire antenna lengths are approximately 8 feet (2.4 m) to 18 feet (5.5 m). The large antenna currents require the use of a wire with low RF resistance (i.e., large diameter and highly conductive surface) to reduce the power losses in the wire. The feedline and the antenna grounding must have very low RF resistance. Only a tensioner with an attached ground wire should be used to terminate the antenna.5.B.(6)(c)1 Short Wire to Vertical Stabilizer Antenna Mounting LocationThe most common form of short grounded wire antennas ahve the feedthru insulator mounted on the upper aft part of the fuselage, as far forward of the vertical stabilizer as is practical. The antenna wire runs from this feedthru to the tip of the vertical stabilizer. It is important to ground this wire as high as possible on the vertical stabilizer to maximize the efficiency and to reduce the nulls in the pattern. This antenna will generally exhibit maximum radiation off the side of the aircraft.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 200810640I00.SLK Mar/200323-10-09Typical Short Wire to Vertical Stabilizer AntennaFigure 20045.B.(6)(c)2 Short Wire to Wing or Horizontal Stabilizer Antenna Mounting LocationIn installations where the short wire to the vertical stabilizer may not be practical, consideration may be given to a short grounded wire to the wing or horizontal stabilizer. While such antennas produce only minimum drag, they will tend to be directional off the side of the aircraft. These antennas are also prone to being walked into. Maximum separation between the wire and the aircraft structure is important, as is maximizing the length of the wire.Typical Short Wire to Wing AntennaFigure 2005Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 200910640I00.SLK Mar/200323-10-09Typical Short Wire to Horizontal Stabilizer AntennaFigure 20065.B.(6)(d) Shunt Antenna Mounting LocationTwo types of shunt antennas are commonly used. The most preferable type, on a fixed wing aircraft, is designed by the airframe manufacturer as a part of the airframe structure. It is most often an electrically isolated section of the leading edge of the vertical stabilizer, grounded at the top. The other type of shunt antenna is often referred to as a "tranline" or "towel bar", which is simply a rod or tube run external to a section of the airframe and grounded.Shunt antennas are suitable for high altitude aircraft because they do not develop extremely high voltage but do not develop extremely high RF current (up to 50 amps).5.B.(6)(d)1 Leading Edge of Vertical Stabilizer Antenna Mounting LocationA shunt antenna that is built into the leading edge of the vertical stabilizers has become popular on many jet aircraft. Such an antenna provides no drag, exhibits a rather omnidirectional radiation pattern and if well bonded can provide moderate to good efficiencies. Good bonding of the antenna and the KAC 1052 Antenna Coupler is essential.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 201010640I00.SLK Mar/200323-10-09A large diameter feedline exhibiting extremely low RF resistance must be used between the KAC 1052 Antenna Coupler and the antenna.Typical Shunt Leading Edge AntennaFigure 20075.B.(6)(d)2 Shorted Tranline or Towel Bar Antenna Mounting LocationGrounded transline (transmission line), often referred to as “towel bar” antennas because their shape resembles a towel bar, are best suited for helicopter applications. They can be attached parallel to the tailboom and fed on the forward end. These antennas provide minimum drag but suffer from poor efficiencies, especially at low frequencies. Loss with this type of antenna can be minimized by observing the following criteria:• Space the antenna as far off the airframe as possible. 18 inches (0.46 m) is preferred, with spacing of less than 9 inches (23 cm) being acceptable.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 201110640I00.SLK Mar/200323-10-09• The antenna diameter should be a minimum of 1 inch (2.54 cm) and constructed out of a highly conductive material. Copper or aluminum is generally used, with silver plating being recommended. Stainless steel should be avoided due to its high resistance. This antenna should be a continuous piece (non-spliced) and should be well bonded at both ends.• A minimum antenna length of 12 feet (3.7 m) should be used. The feedline coax length should be limited to 6 inches (15 cm).• It is preferable to attach the antenna to a protruding surface, such as a tail boom or a stabilizer element. Attaching to a wide section of the fuselage will generally give poor performance.Typical Shorted Tranline or Towel Bar AntennaFigure 20085.C. Interwiring and Cable Fabrication5.C.(1) Fabrication and RoutingFigure 2033 provides a KHF 1050 HF Communication System interconnect summary.Cabling must be fabricated according to the interwiring diagrams. The length of the wires to parallel pins should be approximately the same length, for best current distribution.Wires for optional functions are shown on the interwiring diagrams. The actual use of these wires will depend upon the installation, customer requirements and capability of the units installed.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 201210640I00.SLK Mar/200323-10-09When the cables are installed in the aircraft, they must be supported firmly enough to prevent movement and should be carefully protected against chafing. Additional protection should also be provided in all locations where the cables may be subject to abuse.In wire bundles, the cabling should not be tied tightly together as this tends to increase the possibility of noise pickup and similar interference. When routing cables through the airframe, the cables should cross high-level lines at a right angle.Wiring harness and antenna cable should be routed in such a manner that they do not adversely affect the operation of the shock mounts.The installer must be knowledgeable of any system variation peculiar to the installation such as strapping requirements described in section 5.D. Furthermore, the installer should use ARINC Characteristic 735 as a guide and reference throughout the fabrication and installation of the cabling in the aircraft.5.C.(2) Interface Capability and RequirementsAll RF coaxes must be double shielded.In systems that employ speech processing, special care should be taken in the routing of the microphone input line. This line is susceptible to noise. It should not be routed in the same harness containing high current lines.5.C.(3) Primary Power and Circuit Breaker RequirementsAll units in the KHF 1050 system should be protected by circuit breakers in the positive primary power lines. The KPA 1052 should use an individually dedicated 30 amp slow-acting circuit breaker. The KAC 1052 and KRX 1053 can share a common 5 amp circuit breaker, or be individually protected by 5 amp circuit breakers for each. If a PS440 controller is used in the system, it can share a circuit breaker with the KRX 1053. An MCDU or an RM-855 must not share a circuit breaker with any HF system component.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 201310640I00.SLK Mar/200323-10-095.C.(4) Antenna Cable TypeThe cable connecting the KAC 1052 antenna output (J10528) to the antenna or antenna feed-through must be a specially fabricated feedline supplied by Honeywell. Due to the high level of RF voltage the KHF 1050 system is capable of generating, substitute cables must not be used. Refer to Section 1.C.(1) for appropriate part numbers for the Honeywell supplied HN-to-HN feedline assemblies.5.C.(5) ConnectorsMating connectors for the KHF 1050 HF system components are identified on the appropriate outline drawing. Associated connector installation kits are specified in DESCRIPTION AND OPERATION section of this manual. Crimping, insertion, extraction tools are identified in section 5.C.(6).5.C.(5)(a) KAC 1052 Antenna Coupler ConnectorKAC 1052 Antenna Coupler Connector (J10521) Pin ConfigurationFigure 2009KAC 1052 CONNECTOR PIN DEFINITIONSPIN SIGNAL NAME DESCRIPTION1 PRI PWR RTN PRIMARY POWER RETURN2 PWR CONT RTN POWER ON/OFF CONTROL RETURN3 STRP A STRAP A4 STRP COM STRAP COMMON6 RCA CPLR TXD BUS +7 CRA CPLR RXD BUS +8 BUS COM BUS COMMON9 EXCTR INHB + EXCTR INHIBITION +Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 201410640I00.SLK Mar/200323-10-0910 TUN FAIL + TUNE FAIL +11 RC COM PHOTO-COUPLER COMMON SOURCE12 EXCTR TUN REQ - EXCTR TUNE REQUEST -13 FG FRAME GROUND14 APC H APC HIGH15 PA INHB+ PA INHIBITION +16 PA SI PA SERIAL DATA17 PA SCK PA SERIAL CLOCK18 PA RCK PA SERIAL STROBE19 PA RST PA RESET20 +27.5V PRI PWR +27.5 VDC PRIMARY POWER21 PWR CONT POWER ON/OFF CONTROL22 STRP B STRAP B24 RCB CPLR TXD BUS -25 CRB PHOTO-COUPLER COMMON SOURCE26 EXCTR COM EXCTR COMMON27 MATCH ON - MATCHING CIRCUIT ON -28 BRDG ON + BRIDGING AMPLIFIER ON +29 CR COM PHOTO-COUPLER COMMON SOURCE30 BFRD KEY - BUFFERED KEY -31 FG FRAME GROUND32 CP COM PHOTO-COUPLER COMMON SOURCE33 PA BFRD KEY - PA BUFFERED KEY -34 PA ALM + #1 PA ALARM + #135 PA ALM + #2 PA ALARM + #236 PC COM PHOTO-COUPLER COMMON SOURCEKAC 1052 CONNECTOR PIN DEFINITIONSPIN SIGNAL NAME DESCRIPTIONPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 201510640I00.SLK Mar/200323-10-09KAC 1052 Antenna Coupler Connector (J10521) Pin DefinitionsTable 20015.C.(5)(b) KPA 1052 Power Amplifier ConnectorKPA 1052 Power Amplifier Connector (J10524) Pin ConfigurationFigure 201037 APC L APC LOWKPA 1052 CONNECTOR PIN DEFINITIONSPIN SIGNAL NAME DESCRIPTIONA1 +27.5V PRI PWR +27.5 VDC PRIMARY POWERA2 PRI PWR RTN PRIMARY POWER RETURN4 FG FRAME GROUND5 PA SI PA SERIAL DATA6 PA RCK PA SERIAL STROBE7 PA ALM + #1 PA ALARM + #18 PA RST PA RESET9 APC H APC HIGH10 APCL APC LOW11 PWR CONT RTN POWER ON/OFF CONTROL RETURN17 CP COM PHOTO-COUPLER COMMON SOURCE18 PA SCK PA SERIAL CLOCK19 PA INHB+ PA INHIBITIION +KAC 1052 CONNECTOR PIN DEFINITIONSPIN SIGNAL NAME DESCRIPTIONPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 201610640I00.SLK Mar/200323-10-09KPA 1052 Power Amplifier Connector (J10524) Pin DefinitionsTable 20025.C.(5)(c) KRX 1053 Receiver/Exciter ConnectorKRX 1053 Receiver/Exciter Connector (J10531) Pin ConfigurationFigure 201120 PA ALM + #2 PA ALARM + #221 PC COM PHOTO-COUPLER COMMON SOURCE22 PA BFRD KEY - PA BUFFERED KEY -23 PWR CONT POWER ON/OFF CONTROLKRX 1053 CONNECTOR PIN DEFINITIONSPIN SIGNAL NAME I/O DESCRIPTION1 PWR CONT RTN I POWER ON/OFF CONTROL RETURN2 A615 DATA LDR INP#2(A) I A615 DATA LOADER INPUT #2 (A)3 A615 DATA LDR OUT#2(A) O A615 DATA LOADER OUTPUT #2 (A)4 CMU OUT(A) O CMU OUTPUT (A)5 CMC INP(A) I CMC INPUT (A)6 CMC OUT(A) O CMC OUTPUT (A)7 A615 DATA LDR OUT#1(A) O A615 DATA LOADER #1 (A)8 HF CONT INP #2(A) I HF CONTROLLER INPUT #2(A)KPA 1052 CONNECTOR PIN DEFINITIONSPIN SIGNAL NAME DESCRIPTIONPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 201710640I00.SLK Mar/200323-10-099 HF CONT INP #1(A) I HF CONTROLLER INPUT #1(A)10 SPARE11 RCB O CPLR RXD BUS -12 BUFFERED KEY O BUFFERED KEY -13 KEY EVENT O KEY EVENT14 EXCTR TUNE REQUEST - I EXCTR TUNE REQUEST -15 TUNE MODE I CONTINUOUS/BURST TUNING MODE16 VO PTT H I VOICE PUSH-TO-TALK HIGH17 SW LD#1 I SOFTWARE LOAD #118 AGC TEST O AGC TEST19 SELCAL AUD H I SELCAL AUDIO HIGH20 EXT MODEM AUD H O EXTERNAL MODEM AUDIO HIGH21 MIC AUD H I MIC AUDIO HIGH22 +27.5V PRI PWR I +27.5 VDC PRIMARY POWER23 PWR CONT I POWER ON/OFF CONTROL24 A615 DATA LDR OUT#2(B) O A615 DATA LOADER OUTPUT #2 (B)25 CMU INP(A) I CMU INPUT (A)26 GENL PRP BUS INP(A) I GENERAL PURPOSE BUS INPUT (A)27 CMC OUT(B) O CMC OUTPUT (B)28 A615 DATA LDR INP#1(A) I A615 DATA LOADER INPUT #1 (A)29 HF TUNE/M STAT(A) O HF TUNING/MODE STATUS (A)30 HF CONT INP #1(B) I HF CONTROLLER INPUT #1 (B)31 SPARE32 RCA O CPLR TXD BUS +33 TXD(OUT) O RS232 MAINT MODE TXD BUS (OUT)34 MATCH ON - O MATCHING CIRCUIT ON -KRX 1053 CONNECTOR PIN DEFINITIONSPIN SIGNAL NAME I/O DESCRIPTIONPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 201810640I00.SLK Mar/200323-10-0935 RC COM PHOTO-COUPLER COMMON SOURCE36 STUCK MIC PTCT I STUCK MIC PROTECTION37 OTHER SIDE PTT I OTHER SIDE PTT38 EXT DATA KEYLINE H I EXTERNAL DATA KEYLINE HIGH39 I40 RCV AUD/SIDETN H O RECEIVE AUDIO/SIDETONE HIGH41 EXT MODEM AUD OUT L O EXT MODEM AUDIO OUTPUT LOW42 EXT MODEM AUD INP H I EXT MODEM AUDIO INPUT HIGH43 +27.5V PRI PWR I +27.4 VDC PRIMARY POWER44 A615 DATA LDR INP#2(B) I A615 DATA LOADER INPUT #2 (B)45 CMU INP(B) I CMU INPUT (B)46 CMU OUT(B) O CMU OUTPUT (B)47 CMC INP(B) I CMC INPUT (B)48 A615 DATA LDR INP#1(B) I A615 DATA LOADER INPUT #1 (B)49 A615 DATA LDR OUT#1(B) O A615 DATA LOADER OUTPUT #1 (B)50 HF CONT INP #2(B) I HF CONTROLLER INPUT #2 (B)51 SPARE52 SPARE53 CRA I CPLR RXD BUS +54 BRDG ON + O BRIDGING AMPLIFER ON +55 EXCTR INHB + I EXCTR INHIBITION +56 DATA XMT INHB I DATA TRANSMIT INHIBIT57 CONT SEL I CONTROLLER SELECT58 VO PTT L I VOICE PUSH-TO-TALK LOW59 DATA CAPBLTY INSTL DATA CAPABILITY INSTALLED60 SPAREKRX 1053 CONNECTOR PIN DEFINITIONSPIN SIGNAL NAME I/O DESCRIPTIONPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 201910640I00.SLK Mar/200323-10-0961 SELCAL AUD L O SELCAL AUDIO LOW62 EXT MODEM AUD INP L I EXT MODEM AUDIO INPUT LOW63 MIC AUD L I MIC AUDIO LOW64 PRI PWR RTN I PRIMARY POWER RETURN65 SPARE66 DATA BUS SHLD GND GND DATA BUS SHIELD GROUND67 DATA BUS SHLD GND GND DATA BUS SHIELD GROUND68 GENL PRP BUS I GENERAL PURPOSE BUS INPUT (B)69 DATA BUS SHLD GND GND DATA BUS SHIELD GND70 DATA BUS SHLD GND GND DATA BUS SHIELD GND71 HF TUNE/M STAT(B) O HF TUNING/MODE STATUS (B)72 DATA BUS SHLD GND GND DATA BUS SHIELD GROUND73 SPARE74 CRB I CPLR RXD BUS -75 RXD(IN) I RS232 MAINTENANCE MODE 76 CR COM PHOTO-COUPLER COMMON SOURCE77 TUN FAIL + I TUN FAIL +78 I79 R SIDE I RIGHT SIDE80 EXT DATA KEYLINE L I EXTERNALDATA KEYLINE LOW81 I82 RCV AUD/SIDETN L O RECEIVE AUDIO/SIDETONE LOW83 ANLG SHLD GND GND ANALOG SHIELD GROUND84 ANLG SHLD GND GND ANALOG SHIELD GROUND85 PRI PWR RTN I PRIMARY POWER RETURN86 DATA BUS SHLD GND GND DATA BUS SHIELD GROUNDKRX 1053 CONNECTOR PIN DEFINITIONSPIN SIGNAL NAME I/O DESCRIPTIONPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 202010640I00.SLK Mar/200323-10-09KRX 1053 Receiver/Exciter Connector (J10531) Pin DefinitionsTable 200387 DATA BUS SHLD GND GND DATA BUS SHIELD GROUND88 DATA BUS SHLD GND GND DATA BUS SHIELD GROUND89 DATA BUS SHLD GND GND DATA BUS SHIELD GROUND90 DATA BUS SHLD GND GND DATA BUS SHIELD GROUND91 DATA BUS SHLD GND GND DATA BUS SHIELD GROUND92 DATA BUS SHLD GND GND DATA BUS SHIELD GROUND93 FG GND FIELD GROUND94 DATA BUS SHLD GND GND DATA BUS SHIELD GND95 BUS COM GND BUS COMMON96 GND GND GND97 EXCTR COM GND EXCITER COMMON98 L SIDE I LEFT SIDE99 GND GND DISCRETE SIGNAL GROUND100 NAR/W FREQ RNG I NARROW/WIDE FREQ RANGE101 FG GND FRAME GROUND102 ANLG SHLD GND GND ANALOG SHIELD GROUND103 ANLG SHLD GND GND ANALOG SHIELD GROUND104 ANLG SHLD GND GND ANALOG SHIELD GROUNDKRX 1053 CONNECTOR PIN DEFINITIONSPIN SIGNAL NAME I/O DESCRIPTIONPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 202110640I00.SLK Mar/200323-10-095.C.(5)(d) PS440 Control Display Unit ConnectorPS440 Control Display Unit Connector (J1) Pin ConfigurationFigure 2012PS440 CONNECTOR PIN DEFINITIONSPIN PIN FUNCTION1 A 28 VDC In2 B DC Ground3 C Chassis Ground4 D Spare5 E Reserved6 F Spare7 G Spare8 H Spare9 J Spare10 K Spare11 L Spare12 M AM Inhibit In13 N Spare14 P Freq Range In15 R SparePreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 202210640I00.SLK Mar/200323-10-0916 S Spare17 T HF On/Off Out18 U Spare19 V ARINC 429 Out A20 W Spare21 X Reserved22 Y 28 VDC Dimming Bus23 Z ARINC 429 In #1A24 a Test Out25 b Reserved26 c Spare27 d Spare28 e Spare29 f Spare30 g Spare31 h Spare32 i Spare33 j Spare34 k Spare35 m Reserved (ALE Inhibit In)36 n LSB Voice and Data Inhibit In37 p FCDE Enable In38 q Spare In39 r ARINC 429 Out B40 s Spare41 t ReservedPS440 CONNECTOR PIN DEFINITIONSPIN PIN FUNCTIONPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 202310640I00.SLK Mar/200323-10-09PS440 Control Display Unit Connector (J1) Pin DefinitionsTable 20045.C.(5)(e) MCDU Multifunction Control and Display Unit ConnectorsFor MCDU Multifunction Contol and Display Unit connection information, refer to Installation Manual P/N: XXXX.42 u ARINC 429 In #1B43 v Spare44 w Spare45 x Spare46 y Spare47 z Spare48 AA HFDL Inhibit In49 BB SDI Config In50 CC Reduced Carrier Inhibit In51 DD 0.1 kHz Enable In52 EE Spare Out #153 FF Spare54 GG 5 VDC / AC Lighting High55 HH Spare56 JJ Spare57 KK Spare58 LL Spare Out #259 MM HF Datalink Out60 NN Lighting Lo61 PP USB Data Inhibit InPS440 CONNECTOR PIN DEFINITIONSPIN PIN FUNCTIONPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 202410640I00.SLK Mar/200323-10-095.C.(5)(f) RM-855 Radio Management Unit ConnectorRM-855 Radio Management Unit Connector (J????) Pin ConfigurationFigure 2016RM-855 CONNECTOR PIN DEFINITIONSPIN FUNCTION CONNECT TOX LRU IDENT OPEN - PILOT SIDE HF (ARINC SDI = 01B)GROUND - COPILOT SIDE HF (ARINC SDI = 10B)eSTRAP COMMON JUMPER TO X FOR GROUNDk(-) 429 RXA RMU1 429 TXS (+) 429 RXAR (-) 429 RXB RMU2 429 TXP (+) 429 RXBD (-) 429 RXC FMS 429 RXE (+) 429 RXCAA (-) 429 TXA HF1 - HF1 RMU 429 RXHF2 - HF2 RMU 429 RXm(+) 429 TXACC (-) 429 TXB FMS 429 RXBB (+) 429 TXBrA/B SELECT LEAVE OPENPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 202510640I00.SLK Mar/200323-10-09RM-855 Radio Management Unit Connector (J????) Pin DefinitionsTable 2007sC SELECT LEAVE OPENY BURST ENABLE JUMPER TO e - ARINC 429 BURST ENABLEqSTOP SCAN JUMPER TO u - STOP SCAN ENABLEuRETRANSMIT JUMPER TO q - STOP SCAN ENABLERM-855 CONNECTOR PIN DEFINITIONSPIN FUNCTION CONNECT TOPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 202610640I00.SLK Mar/200323-10-095.C.(5)(f) BNC Connector Assembly (P/N 030-00005-0001)BNC Connector Assembly ProcedureFigure 2017Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 202710640I00.SLK Mar/200323-10-095.C.(6) Connector Pin ToolsThe crimping tool and associated positioner used during the fabrication of cables are identified in figure 2018.The insertion and extraction tools used during the fabrication of cables are identified in figure 2019.Crinping ToolFigure 2018Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 202810640I00.SLK Mar/200323-10-09Insertion and Extraction ToolsFigure 2019Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 202910640I00.SLK Mar/200323-10-095.D. Strapping Options5.D.(1) KRX 1053 Receiver/Exciter Strapping OptionsRefer to Table 2008 for KRX 1053 strapping options.5.D.(1)(a) Power ON/OFF Control - (J10531-23) PWR CONTAn external controller turns on the KRX 1053 Receiver/Exciter by asserting the POWER ON/OFF CONTROL discrete input. In an installation in which LRU power is to be controlled by a radio master switch or relay, this input may be permanently strapped to ground.This input is continuously read.5.D.(1)(b) Controller Select - (J10531-57) CONT SELWhen the TUNING MODE discrete input is not assorted, the CONTROLLER SELECT discrete determines which HF controller input is active.NOTE:Asserted = GND, Not Asserted = OPENThe KRX 1053 Reciever/Exciter accepts tuning and control data from the HF CONTROLLER INPUT #1 when the CONTROLLER SELECT and TUNING MODE discrete inputs are not asserted.The KRX 1053 Receiver/Exciter accepts tuning and control data from the HF CONTROLLER INPUT #2 when the CONTROLLER SELECT discrete input is asserted and the TUNING MODE discrete input is not asserted.This input is continuously read.5.D.(1)(c) Burst/Continuous Tuning Mode - (J10531-15) TUNE MODEWhen the BURST/CONTINUOUS TUNING MODE discrete input is not asserted, the KRX 1053 Receiver/Exciter operates with continuous tuning and mode control data and the CONTROLLER SELECT discrete input determines the active controller input.When the BURST/CONTINUOUS TUNING MODE discrete input is asserted, the KRX 1053 Receiver/Exciter operates by receiving bursts of tuning data.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 203010640I00.SLK Mar/200323-10-09In a system consisting of two external HF controllers, with one controller connected to HF CONTROLLER INPUT #1 data bus and the other connected to HF CONTROLLER INPUT #2 data bus, this tuning and control mode allows the receiver/exciter to automatically accept tuning/control data bursts from either controller.In either the BURST or CONTINUOUS mode, the receiver/exciter sends continuous data to the controller.The KRX 1053 Receiver/Exciter processor samples the state of this discrete input only at initial power application. The state of this discrete is assumed to not change during operation.5.D.(1)(d) Key Event - (J10531-13) KEY EVENTThe KRX 1053 Receiver/Exciter asserts the KEY EVENT discrete output when the transmitter is activated by any activation method.This output may be used by external equipment, such as a flight recorder, to sense when the HF system is transmitting.5.D.(1)(e) Left Side (J10531-98) L SIDE and Right Side (J10531-13)When the LEFT SIDE discrete input is asserted and the RIGHT SIDE descrete input is not asserted, the KRX 1053 Receiver/Exciter accepts ARINC 429 data in which the SDI field is set to 10B, 00B, or 11B. (SDI field 00B identifies an “all call” message and SDI field 11B identifies a “tune both” message.)Additionally, the KRX 1053 Receiver/Exciter sets the SDI field of all ARINC 429 transmitted messages to 01B (bit 9 = 1, bit 10 = 0). This condition identifies the system as HF #1.When the RIGHT SIDE discrete input is asserted and the LEFT SIDE discrete input is not asserted, the KRX 1050 Receiver/Exciter accepts ARINC 429 data in which the SDI field is set to 10B, 00B, or 11B.(SDI field 00B identifies an “all call” message and SDI field 11B identifies a “tune both” message.)Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 203110640I00.SLK Mar/200323-10-09Additionally, the KRX 1053 Receiver/Exciter sets the SDI field of all ARINC 429 transmitted messages to 10B (bit 9 = 0, bit 10 = 1). This condition identifies the system as HF #2.When neither the LEFT SIDE discrete input nor the RIGHT SIDE discrete input is asserted, or when both the LEFT SIDE and RIGHT SIDE discrete inputs are asserted:• The KRX 1053 Receiver/Exciter does not accept ARINC 429 data.• The KRX 1053 Receiver/Exciter sets the SDI field of all ARINC 429 transmitted messages to 00B, and it sets bits 30 and 31 (status field) of all messages except that with label 351 to 11B, indicating an invalid condition shall set bits 30 and 31 (status field) of the label 351 Maintenance Status message to 00B, indicating a fault condition. It is intended that at least one of these discrete inputs, but not both, be asserted.The KRX 1053 Receiver/Exciter processor samples the state of these discrete inputs only at initial power application. The state of these discretes are assumed to not change during operation.5.D.(1)(f) Narrow/Wide Freq Range - (J10531-100) NAR/W FREQ RNGWhen the NARROW/WIDE FREQ RANGE discrete input is asserted, the KRX 1053 Receiver/Exciter restricts operations to the frequency range from 2.0000 MHz through 22.9999 MHz, and clears bit 18 of the Receiver/Exciter Output Label 037, Word ID #1 (Control Status) word to logic 0.When the NARROW/WIDE FREQ RANGE discrete input is not asserted, the KRX 1053 Receiver/Exciter operates over the full frequency range from 2.0000 MHz through 29.9999 Mhz.If the NARROW/WIDE FREQ RANGE discrete input is asserted and the HF controller commands a transmit or receive frequency below 2.0000 MHz or above 22.9999 MHz, the receiver/exciter sets bits 30 and 31 of all transmitted Frequency/Control Status words (label 037) to 11B, indicating an invalid condition.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 203210640I00.SLK Mar/200323-10-09The KRX 1053 Receiver/Exciter processor samples the state of this discrete input only at initial power application. The state of this discrete is assumed not to change during operation.5.D.(1)(g) Maintenance Test- (J10531-78) MAINT TESThen the MAINTENANCE TEST discrete input is asserted, the KRX 1053 Receiver/Exciter RS-232 Maintenance port accepts test modes including the generation of a two-tone PEP test signal.This input is continuously read.5.D.(1)(h) Stuck MIC Protection- (J10531-36) STUCK MIC PTCTWhen the STUCK MIC PROTECTION discrete input is asserted, the receiver/exciter stops transmitting after a transmission duration equal to a constant set in non-volatile memory during manufacturing test or service center test.• This time duration can be set to a value between 30 seconds and 240 seconds. The default time is 120 seconds.• The KRX 1053 Receiver/Exciter processor samples the state of this discrete input only at initial power application. The state of this discrete is assumed to not change during operation.5.D.(1)(i) External Data Keyline HI (J10531-38) EXT DATA KEYLINE HWhen the external resistance between the EXTERNAL DATA KEYLINE HI and LO pins is ten ohms or less, the KRX 1053 Receiver/Exciter activates the transmitter and uses the audio at the EXTERNAL MODEM AUDIO INPUT as the modulation source.The KRX 1053 Receiver/Exciter drives a current of at least ten milliamps through any resistance of ten ohms or less between the EXTERNAL DATA KEYLINE HI and LO pins.The EXTERNAL DATA KEYLINE LO pin may be connected externally to airframe ground in some installations.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 203310640I00.SLK Mar/200323-10-09The KRX 1053 Receiver/Exciter interprets a resistance of ten ohms or less between the EXTERNAL DATA KEYLINE HI and LO pins as a command to transmit, whether the LO pin is grounded or left floating.This input is continuously read.5.D.(1)(j) External Modem Audio Input High/Low- (J10531-42/62) EXT MODEM AUD INP H/LThe audio signal level is typically 0.775 VRMS across 600 ohms.The KRX 1053 Receiver/Exciter presents a balanced, floating 600 ohm load to this signal.This input does ot present direct-current bias to the signal source.There is no audio clipping or compression associated with this input at levels below 1.55 VRMS when adjusted as in paragraph one above.This input is factory adjusted so that at standard temperature and primary power voltage, a 1 kHz modem input signal of 0.775 VRMS yields full Data USB output power from the KRX 1053 Receiver/Exciter and an input of 0.39 V yields 6 dB +/-0.5 dB more output power than that obtained with 0.775 V of input signal.5.D.(1)(k) Voice Push-To-Talk HI- (J10531-16) VO PTT HWhen the external resistance between the VOICE PUSH-TO-TALK HI and LO pins is ten ohms or less, the KRX 1053 Receiver/Exciter activates the transmitter and uses the audio at the MIC AUDIO INPUT as the modulation source.The KRX 1053 Receiver/Exciter drives a current of at least ten milliamps through any resistance of ten ohms or less between the VOICE PUSH-TO-TALK HI and LO pins.The KRX 1053 Receiver/Exciter interprets a resistance of ten ohms or less between the VOICE PUSH-TO-TALK HI and LO pins as a command to transmit, whether the LO pin is grounded or left floating.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 203410640I00.SLK Mar/200323-10-09This input is continuously read.NOTE: The VOICE PUSH-TO-TALK LO pin may be connected externally to airframe ground in some installations.5.D.(1)(l) Other Side PPT- (J10531-37) OTHER SIDE PTTWhen asserted, the OTHER SIDE PTT input prevents the system from transmitting.This input is continuously read.In a dual system installation, when this input is connected to the KEY EVENT output of the KRX 1053 Receiver/Exciter in the opposite system, it prevents this system from transmitting whenever the KEY EVENT of the other system is asserted.When asserted, bit 18 of message (Output label 037), word ID #1 “Other side keyed” is set to 0.The OTHER SIDE PTT and the KEY EVENT discrete inputs/outputs function as an “interlock” to ensure that both systems can not transmit at the same time. Such an interlock function is required when two HF systems share a common antenna on an aircraft.Example: If the co-pilot is transmitting (or tuning the antenna) on the right-side HF system, the pilot will not be able to key the left-side system until the right-side system returns to the receive mode. Once the right-side system has returned to receive mode, the pilot will be able to immediately transmit (or tune the antenna) on the left-side system.Unit/Pin Function Strapping Comment76J1-23 Power On/OffMAU/MCDU May be grounded for KHF 1050 System to be be always on.76J1-15 Tuning Mode Ground Accepts burst ARINC 429 input.76J1-36 Stuck MIC TBD Ground to limit transmission to 30 second default.76J1-57 Controller SelectOpen N/A with Burst Tuning Control.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 203510640I00.SLK Mar/200323-10-09KRX 1053 Receiver/Exciter StrapsTable 2008KRX 1053 Logic Inputs and OutputsTable 200976J1-79 Right Side Side DepenentGround if right-side system. Open if a single KHF 1050 installation.76J1-98 Left Side Side DependentGround if left-side system. Open if a single KHF 1050 installation.76J1-100 Narrow/Wide Open Allows 2.0000 to 29.9999 MHz operation.Unit/Pin Function Strapping Comment76J1-16 Voice PTTTo Audio Panel May be pulled to aircraft ground or 76J1-58.76J1-38 External Data KeylineOpen Used only for data transmission. May be pulled to aircraft ground or 76J1-60.76J1-13 Key EventOpen in a single KHF 1050 installationMay also be used to suppress other equipment in the aircraft during HF transmission.76J1-37 Other Side PTTOpen in a single KHF 1050 installationIn a dual KHF 1050 installation, connect to the keyline of the other system.Unit/Pin Function Strapping CommentPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 203610640I00.SLK Mar/200323-10-096. Equipment Installation6.A Bonding Connections6.A.(1) Antenna Coupler Bonding ConnectionsThe importance of properly bonding the KAC 1052 Antenna Coupler to the airframe can not be over emphasized.Good RF bonding of the KAC 1052 Antenna Coupler to the aircraft fuselage is essential in achieving maximum efficiency from the system and minimizing interference with other systems in the aircraft.The primary bonding path is through a ground strap from a ground post on the KAC 1052 to a point on the airframe near the antenna feed point. More than one ground strap can be used. Additional grounding is achieved via the KAC 1052 mounting tray and mounting shelf. The shield of the coax also contributes to the overall bond of the KAC 1052 to the airframe.6.A.(2) Bonding Strap ConsiderationsMake bonding straps as short as practical and installed in such a manner that the resistance of each connection does not exceed 0.003 ohms. The straps must not interfere with moveable aircraft elements, such as surface controls, nor should the movements of these elements result in damage to the bonding straps.The bonding strap should be made of a solid conductive material rather than braid. Strap thickness should be 0.010 inches or greater. A one inch wide silver plated copper strap, available from Honeywell, is recommended. P/N 047-06261-0036 is a 36 inch length of the strap.6.A.(3) Bonding Connection and Corrosion Prevention TechniquesBecause the mounting surfaces are an important part of the ground system, bonding between these surfaces requires special attention.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 203710640I00.SLK Mar/200323-10-09NOTE: All nonconductive finishes such as paint, anodizing films, or zinc chromate, must be totally removed from the entire mating surface before assembly. Techniques such as spot-facing or cleaning only small area of the mating surfaces do not provide adequate RF bonding.Ground strap connections must be totally free of any non-conductive finishes.Corrosion resistance for aluminum mating surfaces should be achieved by cleaning the aluminum surfaces with Alumiprep #33 (P/N 016-01127-0000), and then applying Alodine #1001 (P/N 016-01128-0000). Alodine #1001 (as well as Alodine #600) provides good electrical conductivity, other Alodine coatings should be avoided.Only after the shelves are assembled and mounted, and ground straps installed, may nonconductive or poorly conductive protective finishes, such as zinc chromate be applied. Periodic inspection should be made of all bonds to ensure that corrosion is not occurring. Any observed corrosion should be cleaned off.6.B. KAC 1052 Antenna Coupler Installation6.B.(1)Select a mounting location for the KAC 1052 Antenna Coupler, referring to Section 5.B.(1).6.B.(2)Power RequirementsThe KAC 1052 Antenna Coupler will operate from a 28 Vdc power supply. The unit must be connected to the aircraft power supply with a circuit breaker with not less than 25 Amp rating.6.B.(3) Grounding RequirementsNOTE: The importance of properly bonding the KAC 1052 Antenna coupler to the airframe can not be over emphasized.NOTE: Except for the ground provided by the feedline coax shield, bonding should not be done with braided wire but with solid conductive straps, typically one inch wide.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 203810640I00.SLK Mar/200323-10-09Good RF bonding of the KAC 1052 Antenna Coupler to the aircraft fuselage is basic in achieving maximum efficiency from the system and eliminating any possible intereference to other systems in the aircraft. See Section 6.A for bonding considerations.6.B.(4) After a location has been selected, remove the mounting tray from the four shock mounts.6.B.(5) Place each shock mount dead center over each center tap position.6.B.(6) Drill four #8 holes per each shock mount.6.B.(7) Thoroughly clean the mounting surface where the bonding straps will be attached. If the surface is aluminum, apply Alodine #1001 per Section 6.A.(1).6.B.(8) Mount the shock mounts to the mounting surface with four each # 8-32 fasteners and lock nuts, installing the ground straps under the appropriate shock mounts.6.B.(9) Attach the mounting tray to the four shock mounts, installing the two tray ground straps.6.B.(10) With the mounting tray secured, locate a point on the airframe structure near the antenna feedthru for attaching a unit to airframe ground strap. Drill two #6 holes, clean and apply Alodine per section 6.A.(1). Connect a ground strap between this point and the KAC 1052 Antenna Coupler ground stud.NOTE: This strap shold not be braided wire, but a solid strap.6.B.11 Place the KAC 1052 Antenna Coupler unit into the mounting tray and secure it in place with two knurled knobs. Provisions for safety wire installation is provided, if desired.6.C. KPA 1052 Power Amplifier Installation6.C.(1)Select a mounting location for the KPA 1052 Power Amplifier, referring to Section 5.B.(2).6.C.(2)Power RequirementsThe KPA 1052 Power Amplifier will operate from a 28 Vdc power supply. The unit must be connected to the aircraft Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 203910640I00.SLK Mar/200323-10-09power supply with a circuit breaker with not less than 25 Amp rating.6.C.(3) Grounding RequirementsExcept for the ground provided by the feedline coax shield, bonding should not be done with braided wire but with solid conductive straps, typically one inch wide.6.C.(4) After a location has been selected, remove the mounting tray from the four shock mounts.6.C.(5) Place each shock mount dead center over each center tap position.6.C.(6) Drill four #8 holes per each shock mount.6.C.(7) Thoroughly clean the mounting surface where the bonding straps will be attached. If the surface is aluminum, apply Alodine #1001 per Section 6.A.(1).6.C.(8) Mount the shock mounts to the mounting surface with four each # 8-32 fasteners and lock nuts, installing the ground straps under the appropriate shock mounts.6.C.(9) Attach the mounting tray to the four shock mounts, installing the two tray ground straps.6.C.(10) With the mounting tray secured, locate a point on the airframe structure near the antenna feedthru for attaching a unit to airframe ground strap. Drill two #6 holes, clean and apply Alodine per section 6.A.(1). Connect a ground strap between this point and the KPA 1052 Power Amplifier.NOTE: This strap shold not be braided wire, but a solid strap.6.C.(11) Place the KPA 1052 Power Amplifier unit into the mounting tray and secure it in place with two knurled knobs. Provisions for safety wire installation is provided, if desired.6.D. KRX 1053 Receiver/Exciter Installation6.D.(1) Select a mounting location, referring to Section 5.B.(3).6.D.(2) After a location has been selected, remove the mounting tray from the four shock mounts.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 204010640I00.SLK Mar/200323-10-096.D.(3) With the shock mounts removed and the tray laying flat against the mounting structure, center tap four positions at which the shock mounts will mount to the tray.6.D.(4) Place each shock mount dead center over each center tap position.6.D.(5) Drill two #6 holes per each shock mount.6.D.(6) Clean and Alodine the mounting surface where the ground strap will be attached. See Section 6.A.(1).6.D.(7) Mount the shocks mounts with two each #6-32 fasteners and lock-nuts, installing the ground strap under the appropriate shock mount.6.D.(8) Attach the mounting tray to the four shock mounts, installing the ground strap.6.D.(9) Slide the KRX 1053 Receiver/Exciter into the mounting tray. Secure the KRX 1053 Receiver/Exciter into place on the mounting tray with the fluted knob. Provisions for safety wire installation is provided, if desired.6.E. Compatible Control Display Unit InstallationFor installation information on the PS440, refer to the PS440 Control Display Unit Installation Manual P/N 006-10655-XXXX.For installation information on the MCDU Multifunction Contol and Display Unit, refer to Installation Manual P/N: XXXX.For installation information on the RM-855 Radio Management Unit, refer to Installation Manual P/N: XXXX.6.F. Antenna Installation6.F.(1) Selecting an Antenna Configuration.While numerous options are available in the choice of antenna configurations, some configurations will be better suited for a particular installation than others. Refer to section 5.B.(7) when selecting an antenna configuration.6.F.(2) Refer to section 6.A.(1) for special bonding consideration when installing an antenna configuration.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 204110640I00.SLK Mar/200323-10-097. Inspection, System Checkout, and Flight Test Procedures7.A. InspectionTable 2010 is a visual inspection/check procedure that should be performed after the system installation as part of a system checkout. In addition, the procedure can be used as periodic maintenance inspection check.Visual Inspection ProcedureTable 20107.B. System Checkout 7.B.(1) GeneralThe KHF 1050 HF Communication System requires three stages of post-installation testing to ensure proper operation: (1) A system interwiring check is performed before installation of system components and before power is applied, to verify that all aircraft and HF system interconnections are correct. Continuity of power pins is double-checked. (2) After system components are installed, a visual inspection of the equipment and connections is made. (3) The post-installation test applies power to system components and checks out system functions.EQUIPMENT INSPECTION/CHECK PROCEDUREKAC 1052 1.2.Verify that all connections to the KAC 1052 are secure.Verify that the ground strap is connected to the ground post.KPA 1052 1.2.Verify that all connections to the KPA 1052 are secure.Verify that all coaxial cables are properly connected to the KRX 1053 and the KAC 1052.KRX 1053 1.2.Verify that all connections to the KAC 1052 are secure.Verify that the controller connector is secure.Antenna Verify that the antenna HN connector is securely tightened.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 204210640I00.SLK Mar/200323-10-097.B.(2) System Interwiring Check7.B.(2)(a) Check that all cables and interwiring are installed according to the interwiring and cable fabrication instructions (section 5.C).7.B.(2)(b) Check that all functions are properly strapped to reflect the aircraft system configuration (section 5.D).7.B.(2)(c) Double-check continuity of all power pins.7.B.(3) Visual InspectionPerform the visual inspection/check procedure (Table 2010).7.B.(4) Post-Installation Test7.B.(4)(a) Perform the System Performance Check in FAULT ISOLATION, Section 2.7.B.(4)(b) Establish communications with another HF station in each of the six communication bands (see Table 2011). Request a signal/audio quality report.7.C. Flight Test While in flight, establish communications with another HF station. It is important that the frequencies selected be apropriate for the distance between the aircraft and the other station (see Table 2011). Request a signal and audio quality report, preferably on several different operating frequencies.Frequency Band(MHz)Daytime Distance(miles)Nighttime Distance(miles)2.8 up to 100 up to 4004.4 up to 200 up to 10005.5 up to 300 100 to 12006.5 100 to 600 200 to 1500 or greater8.8 200 to 800 400 to 1500 or greater*Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 204310640I00.SLK Mar/200323-10-09Typical HF Signal Propagation Distance for Common Aviation BandsTable 20118. Removal and Re-installationCAUTION: Remove all power before performing removal and re-installation procedures.8.A. KAC 1052 Antenna Coupler Removal and Re-installation8.A.(1) KAC 1052 Antenna Coupler Removal8.A.(1)(a) Detach cables from connector J10521.8.A.(1)(b) Remove nut and washer on the GND post. Detach ground strap. Replace nut and washer on the GND post.8.A.(1)(c) Loosen retaining screw clamp loacted at the front of the KAC 1052 Antenna Coupler. Remove unit from rack.8.A.(2) KAC 1052 Antenna Coupler Re-installation8.A.(2)(a) Slide the KAC 1052 Power Amplifier gently into the mounting rack.8.A.(2)(b) Engage and tighten retaining screw clamps to secure unit.10.0 300 to 1000 500 to 1800 or greater*11.1 400 to 1200 600 to 1800 or greater*13.3 600 to 1500 or greater often unusable17.9 700 to 1800 or greater* often unusable21.9 900 to 1800 or greater* often unusableNOTE: HF propagation is dependent on the condition of the ionisphere. Occasionally, distances significantly different than those indicated above may be realized.* At at times, communication may not be possible on this band during this time.Frequency Band(MHz)Daytime Distance(miles)Nighttime Distance(miles)Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 204410640I00.SLK Mar/200323-10-098.A.(2)(c) Reconnect appropriate cables to connector J10521.8.B. KPA 1052 Power Amplifier Removal and Re-installation8.B.(1) KPA 1052 Power Amplifier Removal8.B.(1)(a) Detach cables from connector J10524.8.B.(1)(b) Remove nut and washer on the GND post. Detach ground strap. Replace nut and washer on the GND post.8.B.(1)(c) Loosen retaining screw clamp loacted at the front of the KPA 1052 Power Amplifier. Remove unit from rack.8.B.(2) KPA 1052 Power Amplifier Re-installation8.B.(2)(a) Slide the KPA 1052 Power Amplifier gently into the mounting rack.8.B.(2)(b) Engage and tighten retaining screw clamps to secure unit.8.B.(2)(c) Reconnect appropriate cables to connector J10524.8.C. KRX 1053 Receiver/Exciter Removal and Re-installation8.C.(1) KRX 1053 Receiver/Exciter Removal8.C.(1)(a) Detach cables from connector J10531.8.C.(1)(b) Loosen retaining screw clamp located at the front of the KRX 1053 Receiver/Exciter. Remove unit from mounting rack.8.C.(2) KRX 1053 Receiver/Exciter Re-installation8.C.(2)(a) Slide the KRX 1053 Receiver/Exciter gently into the mounting tray.8.C.(2)(b) Engage and tighten retaining screw clamps to secure unit.8.C.(2)(c) Reconnect appropriate cables to connector J10531.8.D. Control Unit Removal and Re-installationPreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 204510640I00.SLK Mar/200323-10-09Refer to the installation manual for the PS440 Control Display Unit, P/N 006-10655-XXXX, for PS440 removal and re-installaton instructions.Refer to the installation manual for the MCDU, P/N XXXX, for MCDU removal and re-installation instructions.Refer to the installation manual for the RM-855, P/N XXXX, for RM-855 removal and re-installation instructions.9. Maintenance Procedures9.A. In-Aircraft Adjustments9.A.(1) GeneralAll alignment and adjustment procedures are accomplished during bench maintenance. When unit performance indicates an adjustment or an alignment is required technician should remove the unit from the aircraft, then reference should be made to the related Maintenance Manual.9.A.(2) Audio LevelsThe audio inputs and outputs of the KRX 1053 are factory adjusted to the following levels:• Receiver/Sidetone: 7.75 Vrms into 600 ohms at maximum volume• Data Input: 0.775 Vrms across 600 ohms• Microphone Input: 200 mVrms to 2 Vrms (typical) into 150 ohms• Data Output: 1.775 Vrms into 600 ohms• SELCAL Output: 0.775 Vrms into 600 ohmsIf necessary, these levels may be adjusted for compatibility with other aircraft systems. To access the adjustments, loosen the two Dzues fasteners on the top of the unit and remove the dust cover. Refer to Figure 2020 for adjustment locations. Replace and secure the dust cover once the adjustment is complete.9.B. System ProtectionThe KHF 1050 system is primarily protected by circuit breakers located at the circuit breaker panel in the aircraft. The KPA 1052 contains an internal fuse for additional protection.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 204610640I00.SLK Mar/200323-10-099.C. LubricationNo lubrication is required. There are no moving parts that require lubrication in the KHF 1050 HF Communication System.9.D. CleaningThe exterior of the units should be wiped with lint-free cloth dampened with the approved cleaning agent, when deemed necessary, depending upon environmental exposure and intensity of use.NOTE: Limit cleaning of equipment interiors to that required at bench overhaul.10. System Maintenance Programs10.A.System Maintenance Recommendations10.A.(1) Perform a system performance check when a component of the system is replaced or installed.10.A.(2) To confirm satisfactory system operation a system performance test may be performed as required.10.A.(3) After major aircraft maintenance cycles a system performance check should be performed.Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 204710640I00.SLK Mar/200323-10-09KRX 1050 AdjustmentsFigure 2020Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 204810640I00.SLK Mar/200323-10-09Blank PagePreliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2049/205010640I00.SLK Mar/200323-20-03COMMENTARY: INSERT OUTLINE DRAWING HERE WHEN AVAILABLE PS440 Control Display Unit Outline and Mounting(Dwg P/N ????)Figure 2022Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2051/205210640I00.SLK Mar/200323-10-09MCDU Multifunction Control and Display Unit Outline and Mounting(Dwg P/N 7025726-930 - Sheet 1 of 3)Figure 2023Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2053/205410640I00.SLK Mar/200323-20-03 MCDU Multfunction Control Display Unit Outline and Mounting(Dwg P/N 7025726-930 - Sheet 2 of 3)Figure 2024Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2055/205610640I00.SLK Mar/200323-10-09MCDU Multifunction Control and Display Unit Outline and Mounting(Dwg P/N 7025726-930 - Sheet 3 of 3)Figure 2025Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2057/205810640I00.SLK Mar/200323-20-03 RM-855 Radio Management Unit Outline and Mounting(Dwg P/N 7013270 sheet 1 of 2)Figure 2026Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2059/206010640I00.SLK Mar/200323-20-03 RM-855 Radio Management Unit Outline and Mounting(Dwg P/N 7013270 sheet 2 of 2)Figure 2927Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2061/206210640I00.SLK Mar/200323-20-03KAC 1052 Antenna Coupler Single Horizontal Outline and Mounting(Dwg P/N 155-01774-0000)Figure 2028Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2063/206410640I00.SLK Mar/200323-20-03KAC 1052 Antenna Coupler Single Vertical Outline and Mounting(Dwg P/N 155-01772-0000)Figure 2029Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2065/206610640I00.SLK Mar/200323-20-03KAC 1052 Antenna Coupler Dual Vertical Outline and Mounting(Dwg P/N 155-01775-0000)Figure 2030Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2067/206810640I00.SLK Mar/200323-20-03KPA 1052 Power Amplifier Outline and Mounting(Dwg P/N 155-01750-0000)Figure 2031Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2069/207010640I00.SLK Mar/200323-20-03KRX 1053 Receiver/Exciter Outline and Mounting(Dwg P/N 155-01751-0000)Figure 2032Preliminary - Subject to Change Without Notice

NKHF 1050 SYSTEM INSTALLATION MANUALRevision 0 Page 2071/207210640I00.SLK Mar/200323-20-03COMMENTARY: INSERT INTERCONNECT DRAWING HERE WHEN AVAILABLEKHF 1050 HF System Interconnect(Dwg P/N 155-01762-0000)Figure 2033Preliminary - Subject to Change Without Notice

COMMENTARY: INSERT KAC 1052 QUALIFICATION FORM HERE WHEN AVAILABLE.Preliminary - Subject to Change Without Notice

COMMENTARY: INSERT KPA 1052 QUALIFICATION FORM HERE WHEN AVAILABLE.Preliminary - Subject to Change Without Notice

COMMENTARY: INSERT KRX 1053 QUALIFICATION FORM HERE WHEN AVAILABLE.Preliminary - Subject to Change Without Notice

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