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SYSTEM INSTALLATION MANUAL

89000016

10. KGX Interface Details (All Models)

A.

Power Input

(1)

Aircraft power is provided to the KGX through the J1 power and I/O connector. The power
supply input can be 10 to 40 VDC. Use a 2-AMP circuit breaker for power supply protection.
Power input resides on the pins shown in Table 1011.

Table 1011. Power Input

Pin

Signal

Electrical

I/O

Description

J1-1

Vin

10 to 40 VDC

Pwr

Aircraft power input

J1-16

Vin

10 to 40 VDC

Pwr

Aircraft power input

J1-17

RTRN

Ground

GND

Aircraft power return

J1-31

RTRN

Ground

GND

Aircraft power return

J1-32

REM ON

1

Open/ground

I

Remote power control (Ground: ON, Open:
OFF)

NOTE:

1

REM ON must be tied to KGX control panel Pin 7 for remote on/off control or tied to ground for the KGX to
power up.

B.

Personality Module

NOTE:

The personality module is installed to simplify KGX service replacement.

(1)

The PM eliminates the need to reconfigure the KGX if replaced with a new unit for any reason
after initial configuration. Installation specific configuration data is stored in the PM as well
as in the KGX. The installation configuration data in the PM (if present) is copied to the
KGX at power-up.

(2)

Both the PM and the KGX configuration data are stored during the installation configuration
process. The PM is optional but simplifies the process to replace a serviced KGX. Refer to
Paragraph 13 in this section for the detailed installation of the PM.

(3)

The KGX control panel (if used in the installation) also contains a back-up copy of the
installation configuration data. If the PM is not installed, the KGX control panel will
automatically reconfigure the KGX if it is replaced in the installation.

(4)

However, if the KGX control panel is replaced in an installation without the PM, the KGX
must be reconfigured.

(5)

The PM connections are on the pins shown in Table 1012.

Table 1012. Personality Module Interface

Pin

Signal

Electrical

I/O

Description

J1-14

Vpm

3.0 to 3.6 VDC

O

Personality module power output

J1-30

GND

Ground

GND

Personality module power return

EFFECTIVITY

ALL

Page 1011

22 Dec 2016

© Honeywell International Inc. Do not copy without express permission of Honeywell.

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Содержание 89000016-130

Страница 1: ...PC31 89000016 150 6PC31 89000016 151 6PC31 Legal Notice Export Control This document contains technical data and is subject to U S export regulations These commodities technology or software were expo...

Страница 2: ...greement related to the operation maintenance or repair of Honeywell aerospace products Honeywell hereby grants you a limited non exclusive license to use these Materials to maintain or repair the sub...

Страница 3: ...verned and construed in accordance with the laws of the State of New York without regard to the conflicts of laws provisions thereof This license sets forth the entire agreement between you and Honeyw...

Страница 4: ...tional Inc All rights reserved Honeywell is a registered trademark of Honeywell International Inc All other marks are owned by their respective companies THIS IS THE CMM FOSI DATE 20101217 Page T 4 22...

Страница 5: ...ith the attached pages Write the revision number revision date and replacement date on the Record of Revisions page The table of highlights tells users what has changed as a result of the revision The...

Страница 6: ...Paragraph 2 B Updated the text in Step 2 All Page 5 Paragraph 2 C Changed TSO C88a to TSO C88b and added ETSO C88a in Step 1 All Page 5 Paragraph 2 C Added a note in Step 4 Updated the nomenclature in...

Страница 7: ...2 Connections to MPI Pinout Updated the text in Steps 8 and 9 and the note associated with Step 9 All Page 1019 Paragraph 12 D Added a reference to the Serial Interface Specifications section in Step...

Страница 8: ...Added Display in ALT mode graphic All Page 3003 Figure 3004 Added Reverse Video Examples when KGX Control Panel is in External Control Mode All Page 3004 Paragraph 2 A Updated Step 4 Deleted Steps 5 a...

Страница 9: ...to include the latest data All Page 3024 Figure 3014 Updated graphic to include the latest data All Page 3025 Figure 3016 Updated graphic to include the latest data All Page 3026 Figure 3017 Updated g...

Страница 10: ...mand All Page 3041 Figure 3045 Added checkpw Command All Page 3041 Figure 3046 Added resetpw Command All Page 3041 Figure 3047 Added maint ascii pw Command All Page 3041 Paragraph 5 A Updated Step 1 a...

Страница 11: ...ord Sensor to the task title All Page 6001 Paragraph 3 A Added default minimum to the first bullet in Step 1 All Page 7001 Paragraph 1 A Changed No 33 comments for item 33 from Installation configurat...

Страница 12: ...SYSTEM INSTALLATION MANUAL 89000016 Blank Page EFFECTIVITY ALL Page TI 8 22 Dec 2016 Honeywell International Inc Do not copy without express permission of Honeywell...

Страница 13: ...mber revision date date put in the manual and your initials in the applicable column NOTE Refer to the Revision History in the TRANSMITTAL INFORMATION section for revision data EFFECTIVITY ALL Page RR...

Страница 14: ...SYSTEM INSTALLATION MANUAL 89000016 Blank Page EFFECTIVITY ALL Page RR 2 22 Dec 2016 Honeywell International Inc Do not copy without express permission of Honeywell...

Страница 15: ...TR may be active incorporated or deleted Active is entered by the holder of the manual Incorporated means a TR has been incorporated into the manual and includes the revision number of the manual when...

Страница 16: ...SYSTEM INSTALLATION MANUAL 89000016 Blank Page EFFECTIVITY ALL Page RTR 2 22 Dec 2016 Honeywell International Inc Do not copy without express permission of Honeywell...

Страница 17: ...in Date Put in Revision Number Title Modification Manual 89000016 34 0001 D201603000071 NAVIGATION KGX 150 130 TRANSCEIVERS AND RECEIVERS AUTOMATIC DEPENDENT SURVEILLANCE BROADCAST ADS B UNIVERSAL ACC...

Страница 18: ...SYSTEM INSTALLATION MANUAL 89000016 Blank Page EFFECTIVITY ALL Page SBL 2 22 Dec 2016 Honeywell International Inc Do not copy without express permission of Honeywell...

Страница 19: ...2 Dec 2016 TC 6 22 Dec 2016 TC 7 22 Dec 2016 TC 8 22 Dec 2016 TC 9 22 Dec 2016 TC 10 22 Dec 2016 TC 11 22 Dec 2016 TC 12 22 Dec 2016 TC 13 22 Dec 2016 TC 14 22 Dec 2016 Introduction INTRO 1 22 Dec 201...

Страница 20: ...24 22 Dec 2016 Configuration Calibration and Checkout 3001 22 Dec 2016 3002 22 Dec 2016 3003 22 Dec 2016 3004 22 Dec 2016 3005 22 Dec 2016 3006 22 Dec 2016 3007 22 Dec 2016 3008 22 Dec 2016 3009 22 De...

Страница 21: ...2016 22 Dec 2016 22 Dec 2016 4003 4004 RTCA DO 160 Environmental Qualification 5001 22 Dec 2016 5002 22 Dec 2016 5003 22 Dec 2016 5004 22 Dec 2016 Serial Interface Specifications 6001 22 Dec 2016 6002...

Страница 22: ...SYSTEM INSTALLATION MANUAL 89000016 Blank Page EFFECTIVITY ALL Page LEP 4 22 Dec 2016 Honeywell International Inc Do not copy without express permission of Honeywell...

Страница 23: ...NTRO 5 3 References INTRO 5 A Honeywell Vendor Publications INTRO 5 B Other Publications INTRO 5 4 Acronyms and Abbreviations INTRO 5 A General INTRO 5 B Service Information Documents INTRO 10 GENERAL...

Страница 24: ...GX Control Panel Cut Out Options 1007 A General 1007 8 Cooling Requirements All Models 1009 A General 1009 9 KGX Electrical Connections All Models 1009 A KGX 150 130 Transceivers and Receivers Interfa...

Страница 25: ...General 1023 B Antenna Power 1024 C Recommended Cable 1024 D SATCOM Compatibility 1024 16 KGX Control Panel Static Pressure Connection 1024 A General 1024 17 Equipment Limitations 1025 A General 1025...

Страница 26: ...tup and Configuration 3004 A General 3004 B Configuration Item Summary 3005 C Serial and ARINC Port Configuration Details 3007 4 Configuration and Setup Using MPI 3017 A General 3017 B KGX Maintenance...

Страница 27: ...RONMENTAL QUALIFICATION 1 KGX UAT DO 160 Qualification 5001 A General 5001 2 KGX Control Panel DO 160 Qualification 5002 A General 5002 SERIAL INTERFACE SPECIFICATIONS 1 General 6001 A Overview 6001 2...

Страница 28: ...ng Equipment 8003 C Equipment Mounting 8003 D Electrical Interface 8004 E Connecting to the WiFi Module 8005 3 RTCA DO 160G Environmental Qualification 8008 A WiFi Module 8008 4 Typical Interconnect D...

Страница 29: ...helton FlightLogic Display GSL 71 Controller No Transponder Interconnect Diagram 2005 2003 Aspen Display and Control GTX 327 Transponder Interconnect Diagram 2007 2004 BendixKing KSN 765 770 Display a...

Страница 30: ...3024 3014 comm Command 3024 3015 control Command 3025 3016 gps Command 3025 3017 info Command 3026 3018 Reset Command 3026 3019 rxstatus Command 3027 3020 cnfg Command 3028 3021 set Command 3029 3022...

Страница 31: ...3050 VFR Squawk Code Display 3043 3051 Call Sign VFR Flight ID Display 3043 3052 Groundspeed Threshold Display 3044 3053 Aircraft Emitter Category Display 3045 3054 Squat Switch Type Display 3045 3055...

Страница 32: ...3078 Alt Encoder Cal Low Altitude 0ft Display 3058 3079 Alt Encoder Cal Mid Altitude FL100 Display 3058 3080 Alt Encoder Cal High Altitude FL300 Display 3058 3081 Pressure Altitude Reported Display 30...

Страница 33: ...1003 1006 TSO C190 KA 96 WAAS GPS Antenna PN 071 01620 0001 1003 1007 Compatible WAAS GPS Receivers 1004 1008 Other Approved WAAS GPS Antennas 1004 1009 FT 9000 RAMP Tester Kit 1005 1010 KGX Interface...

Страница 34: ...08 Serial Port Output Baud Rate Settings 3012 3009 ARINC 429 Port Input Configuration Settings 3012 3010 ARINC Port Input Speed Configuration Settings 3013 3011 GPS 743 Input ARINC Labels 3013 3012 GP...

Страница 35: ...lification 5002 6001 ASCII Message 6001 6002 KGX Message Items 6002 7001 Supported ADS B Parameters 7001 8001 LED Indicators 8001 8002 WiFi Module PN 89000016 002 Technical Characteristics 8002 8003 W...

Страница 36: ...SYSTEM INSTALLATION MANUAL 89000016 Blank Page EFFECTIVITY ALL Page TC 14 22 Dec 2016 Honeywell International Inc Do not copy without express permission of Honeywell...

Страница 37: ...related instruction 5 Warnings and cautions go before the applicable paragraph or step Notes follow the applicable paragraph or step B Observance of Manual Instructions 1 Make sure that you carefully...

Страница 38: ...INSTALLATION MANUAL 89000016 Figure INTRO 1 Sheet 1 of 2 Geometric Tolerance Symbols EFFECTIVITY ALL Page INTRO 2 22 Dec 2016 Honeywell International Inc Do not copy without express permission of Hon...

Страница 39: ...INSTALLATION MANUAL 89000016 Figure INTRO 1 Sheet 2 of 2 Geometric Tolerance Symbols EFFECTIVITY ALL Page INTRO 3 22 Dec 2016 Honeywell International Inc Do not copy without express permission of Hon...

Страница 40: ...99 CONFIGURATION CALIBRATION AND CHECKOUT 3001 thru 3999 TROUBLESHOOTING 4001 thru 4999 RTCA DO 160 ENVIRONMENTAL QUALIFICATION 5001 thru 5999 SERIAL INTERFACE SPECIFICATIONS 6001 thru 6999 ADS B COMP...

Страница 41: ...an National Standards Institute at http www ansi org ASME Y14 38 Abbreviations for Use on Drawings and Related Documents available from the American National Standards Institute at http www ansi org A...

Страница 42: ...ASME American Society of Mechanical Engineers ATA Air Transport Association ATC Air Traffic Control ATCRBS air traffic control radar beacon system AWG American wire gauge BIT built in test bps bits pe...

Страница 43: ...FN function FOM figure of merit G Dest general destination GHz gigahertz gm gram GND ground GNSS global navigation satellite system GPO Government Printing Office GPS global positioning system GUI gra...

Страница 44: ...m millimeter MOPS minimum operational performance standards MPI maintenance port interface MSL mean sea level N S North South NACv navigation accuracy category for velocity NEXRAD next generation rada...

Страница 45: ...rmation SIM system installation manual Spec specification SSI signal strength indication STC supplemental type certificate STX start of text T R transmit receive TA traffic advisory TC type certificat...

Страница 46: ...Information Documents 1 Refer to Table INTRO 2 for other applicable service information documents not listed in the Service Bulletin List Table INTRO 2 Service Information Documents Document Type Doc...

Страница 47: ...and other flight data to other aircraft and ground station equipment through a UAT data link once each second ADS B Out The KGX 150 130 transceivers and receivers receive aircraft position velocity a...

Страница 48: ...ce of a dedicated MPI port This allows traffic and weather data to be shared with a portable electronic device in flight and can be used to simplify system configuration during maintenance activities...

Страница 49: ...quire any connections to a transponder or transponder transmit control and is not required to obtain pressure altitude data from the same altitude sensor used by the transponder GPS data and pressure...

Страница 50: ...500W with GPS ADS B Plus interface or Bendix King KSN 765 770 GPS interface through an RS 232 serial port or an ARINC 743A compatible GPS e g FreeFlight systems 1203 1203C through an ARINC 429 bus c T...

Страница 51: ...tude received directly by the KGX 150T 130T transceivers and outputs the altitude on its RS 232 serial output 2 The KGX control panel has a DB 9 connector for electrical interface and a static pressur...

Страница 52: ...el to the KGX 150 130 transceivers 9 Remote On Off a System on off power is controlled with the mode selection knob 10 Altitude Output a Pressure altitude data is output on an RS 232 serial port D UAT...

Страница 53: ...1 150 and 151 1 Refer to Table 2 for the KGX 150 130 transceivers and receivers leading particulars Table 2 KGX 150 130 Transceivers and Receivers Leading Particulars Characteristic Specification Envi...

Страница 54: ...NC 429 Discrete inputs Input 3 air GND traffic test and anonymous mode Discrete outputs Output 2 transmit suppression and UAT status GPS output KGX 150 series only Output Serial RS 232 or ARINC 429 In...

Страница 55: ...cteristic Specification Power requirements 5 5 to 10 VDC 0 3 AMP MAX at 6 5 VDC powered by the KGX Interfaces Type I O KGX control panel RS 485 I O Altitude output RS 232 output EFFECTIVITY ALL Page 9...

Страница 56: ...SYSTEM INSTALLATION MANUAL 89000016 Blank Page EFFECTIVITY ALL Page 10 22 Dec 2016 Honeywell International Inc Do not copy without express permission of Honeywell...

Страница 57: ...hrough a KGX 150 130 transceiver serial port to control Mode A code and IDENT Mode A C transponders without serial control data out can use the KGX 150 130 transceiver internal Mode A receiver configu...

Страница 58: ...tallation kit is needed order PN 89000016 005 The items included in the KGX control panel installation kit are listed in Table 1003 Table 1003 KGX Control Panel and Installation Kit PN 89000016 001 It...

Страница 59: ...inch 0 5 inch 4 The items included in the optional KA 61 UAT antenna PN 071 00221 0010 are listed in Table 1005 Table 1005 KA 61 UAT Antenna PN 071 00221 0010 PN Qty Description 071 00221 0010 1 L ban...

Страница 60: ...S B Plus Interface 066 01204 0101 066 01204 1101 066 01213 0101 066 01213 1101 BendixKing KSN 765 770 Safety Navigator B List of Other Approved WAAS GPS Antennas 1 The KGX 150 series PN 89000016 150 o...

Страница 61: ...llation of cables and connectors a Select a position in the panel that is not too close to any high external heat source the KGX control panel is not a significant heat source itself b Avoid sharp ben...

Страница 62: ...adequate space for installation of cables and connectors a Select a position in the aircraft that is not too close to any high external heat source the KGX is not a significant heat source itself b Av...

Страница 63: ...either the compact mounting hole or a conventional 2 25 inch 57 mm instrument cut out The compact mounting is a truncated 58 mm opening Note that the mounting screws are not in the same location for...

Страница 64: ...at you must check all dimensions before using it as a template Figure 1003 Sheet 1 of 1 KGX Control Panel Ultra Compact Mounting Hole Cut Out Option Figure 1004 Sheet 1 of 1 KGX Control Panel Standard...

Страница 65: ...und GND KGX control panel power return 3 232 RxD2 RS 232 I Serial Port 2 RS 232 data in 4 232 RxD1 RS 232 I Serial Port 1 RS 232 data in 5 232 TxD1 RS 232 O Serial Port 1 RS 232 data out 6 429 IN 2A A...

Страница 66: ...emote power control Ground ON Open OFF 33 232 TxD2 RS 232 O Serial Port 2 RS 232 data out 34 429 IN 1B ARINC 429 I ARINC 429 input Port 1B 35 429 IN 1A ARINC 429 I ARINC 429 input Port 1A 36 429 IN 2B...

Страница 67: ...onfiguration Installation specific configuration data is stored in the PM as well as in the KGX The installation configuration data in the PM if present is copied to the KGX at power up 2 Both the PM...

Страница 68: ...t condition or no position available GPS status GREEN Flash slow GPS is acquiring satellites and determining position Flash fast GPS reporting a fault condition ON GPS has acquired satellites and is o...

Страница 69: ...3 4 5 and 6 Two ARINC 429 input interfaces 429 IN1 and 429 IN2 One ARINC 429 output interface 429 OUT1 NOTE Refer to Paragraph 3 C in the CONFIGURATION CALIBRATION AND CHECKOUT section for detailed se...

Страница 70: ...rial Port 6 data in NOTE 1 Serial Port 6 can be optionally configured for RS 232 serial interface on Pins J1 8 and J1 38 3 ARINC 429 Ports a Two ARINC 429 input serial interfaces are available on the...

Страница 71: ...ion The air ground discrete is configurable to be either Not connected High when airborne Low ground when airborne b Deleted c Airborne or on ground status affects ADS B message transmission behavior...

Страница 72: ...UAT status output is an active low open collector output capable of sinking a maximum of 100 mA The UAT status output indicates a UAT transmit or receive system failure when continuously grounded UAT...

Страница 73: ...on status information and update system software firmware The MPI must be used by qualified installation personnel to configure and update the system 2 The MPI functionality is provided through serial...

Страница 74: ...are configured and interfaced to other equipment KGX control panel or display the connections to the configured device must be temporarily disconnected to use the port for MPI purposes If the KGX con...

Страница 75: ...485 lines TRxD3 and TRxD3 respectively D Altitude Out 1 The KGX control panel outputs pressure altitude data on an RS 232 serial output pin ALT_OUT at 9600 baud using the Icarus format refer to SERIAL...

Страница 76: ...shows the personality module wire color connections to the DB 44 connector Table 1024 Personality Module Interface Pin Signal Electrical I O Description PM Wire Color J1 14 Vpm 3 0 to 3 6 VDC O Perso...

Страница 77: ...performance of the KGX The following considerations must be taken into account when selecting the antenna location a The antennas must be installed away from any projections the engine s and propelle...

Страница 78: ...e the ground plane must be very large compared to the wavelength of the transmission which is approximately 12 inches 304 8 mm 2 For a composite or fabric skinned aircraft a metallic ground plane must...

Страница 79: ...ble away from away from potential interference sources such as ignition wiring 400 Hz generators fluorescent lighting and electric motors Allow a minimum separation of 12 inches 300 mm from an ADF ant...

Страница 80: ...een shown through testing to be specification compliant for single channel SATCOM compatibility in accordance with RTCA DO 229D 2 Extra care must be exercised when installing GNSS equipment on aircraf...

Страница 81: ...for GPS antennas 3 For a compliant installation in accordance with the TSO and the FAR the KGX installation must meet the following requirements NOTE Certified installations must be approved by a STC...

Страница 82: ...cations 18 Department of Commerce Compliance A General 1 The Department of Commerce Bureau of Export Administration s Revision of the Commodity Control List permits shipment of commercial GPS products...

Страница 83: ...aragraph 6 NOTE Highlighted configuration options represent those that are unique to each aircraft Configuration options must be configured appropriately in accordance with CONFIGURATION CALIBRATION A...

Страница 84: ...SYSTEM INSTALLATION MANUAL 89000016 Blank Page EFFECTIVITY ALL Page 2002 22 Dec 2016 Honeywell International Inc Do not copy without express permission of Honeywell...

Страница 85: ...0016 Figure 2001 Sheet 1 of 1 Garmin GNS 430W 530W Display and GPS GTX 330 Transponder Interconnect Diagram EFFECTIVITY ALL Pages 2003 2004 22 Dec 2016 Honeywell International Inc Do not copy without...

Страница 86: ...16 Figure 2002 Sheet 1 of 1 Chelton FlightLogic Display GSL 71 Controller No Transponder Interconnect Diagram EFFECTIVITY ALL Pages 2005 2006 22 Dec 2016 Honeywell International Inc Do not copy withou...

Страница 87: ...89000016 Figure 2003 Sheet 1 of 1 Aspen Display and Control GTX 327 Transponder Interconnect Diagram EFFECTIVITY ALL Pages 2007 2008 22 Dec 2016 Honeywell International Inc Do not copy without expres...

Страница 88: ...016 Figure 2004 Sheet 1 of 1 BendixKing KSN 765 770 Display and GPS GTX 327 Transponder Interconnect Diagram EFFECTIVITY ALL Pages 2009 2010 22 Dec 2016 Honeywell International Inc Do not copy without...

Страница 89: ...NUAL 89000016 Figure 2005 Sheet 1 of 1 Mode A C Transponder KGX Control Panel Interconnect Diagram EFFECTIVITY ALL Pages 2011 2012 22 Dec 2016 Honeywell International Inc Do not copy without express p...

Страница 90: ...NUAL 89000016 Figure 2006 Sheet 1 of 1 Garmin GNS 480 SL 70 Transponder TCAS Interconnect Diagram EFFECTIVITY ALL Pages 2013 2014 22 Dec 2016 Honeywell International Inc Do not copy without express pe...

Страница 91: ...89000016 Figure 2007 Sheet 1 of 1 Garmin MX 20 Display and Control No Transponder Interconnect Diagram EFFECTIVITY ALL Pages 2015 2016 22 Dec 2016 Honeywell International Inc Do not copy without expre...

Страница 92: ...AL 89000016 Figure 2008 Sheet 1 of 1 Garmin GMX 200 Display GTX 330 Transponder Interconnect Diagram EFFECTIVITY ALL Pages 2017 2018 22 Dec 2016 Honeywell International Inc Do not copy without express...

Страница 93: ...of 1 FreeFlight Systems 1203C Wiring Diagram 4 Equipment Compatibility and Functions A General 1 Refer to Table 2003 for a summary of the ADS B transmit control function capabilities of various potent...

Страница 94: ...X ADS B Controller Garmin GSL 71 X X X X 2 Refer to Table 2004 for the minimum compatible software versions as tested with the KGX series Table 2004 Compatible Software Versions Device Permitted Soft...

Страница 95: ...ater 5 Maintenance Interface Wiring Diagrams A General 1 This paragraph describes the various KGX series configuration and setup options available through the MPI 2 Refer to Table 2005 for a list of t...

Страница 96: ...FOR VISUAL ACQUIRING TRAFFIC AND MANEUVERING THEIR AIRCRAFT IN TRAFFIC WARNING THE KGX SERIES PROVIDES WEATHER INFORMATION THAT CAN BE USED AS AN AID FOR SITUATIONAL AWARENESS ONLY WEATHER INFORMATION...

Страница 97: ...isfactory operation The following table gives guidelines for typical aircraft hook up wire NOTE Different brands can vary Check your supplier for details 4 Refer to Table 2006 for the wiring considera...

Страница 98: ...SYSTEM INSTALLATION MANUAL 89000016 Blank Page EFFECTIVITY ALL Page 2024 22 Dec 2016 Honeywell International Inc Do not copy without express permission of Honeywell...

Страница 99: ...and is continually tested using a PBIT when the system is in operation This method of testing will notify the operator of a failure System software updates are accomplished using the MPI 2 Continued a...

Страница 100: ...de but will be correctly reported in the ADS B message c Refer to Figure 3003 for the KGX 150 130T powered on in the airborne transmission mode with a pressure altitude of flight level 500 feet being...

Страница 101: ...he MSG icon in the center of the LCD to indicate warning messages are present Depending on the nature of the malfunction the KGX may not be transmitting ADS B messages The Warning page is only availab...

Страница 102: ...and then turn on the KGX control panel if installed During initialization the KGX unit performs a comprehensive diagnostics test 3 A system component failure will be annunciated by a Warning Indicati...

Страница 103: ...anel B Configuration Item Summary 1 Refer to Table 3001 for the Serial and ARINC Port Configuration Settings 2 Refer to Table 3002 for the ADS B transmit Configuration Settings 3 Refer to Table 3003 f...

Страница 104: ...nfiguration Settings Configuration Item Default Setting ICAO Address Mode S 0 VFR Call Sign Flight ID GPS SDA Level UNKNOWN GPS NACv Mode UNKNOWN Receiver Configuration UAT Receiver Installed 978 ES10...

Страница 105: ...is not configurable on the KGX control panel 2 Traffic Velocity Validation is not configurable on the KGX control panel 3 Display data output is not configurable on the KGX control panel 5 Refer to P...

Страница 106: ...able in the configured protocol Pressure altitude data output can also be configured to share with a transponder Serial Port 4 is typically used for altitude Input Pressure altitude input is required...

Страница 107: ...has an internal GPS and serial IN 1 is set to GPS Internal and ARINC IN 1 is set to GPS 743 then the KGX will not receive GPS data from the internal GPS f Set only one control input only one altitude...

Страница 108: ...pically configured on Port 1 GPS KSN 4 GPS aviation GPS Input GPS position velocity time and integrity data input Format for the BendixKing KSN 765 770 GPS PXPRESS protocol Typically configured on Por...

Страница 109: ...connection to serial port Alt Encoder Encoded Altitude Altitude Output Altitude data Format for sending altitude to a transponder or display using the protocol in Paragraph 2 Xpndr Monitor XPDR Monit...

Страница 110: ...e correct rate must be selected to match the interfacing equipment s configured or default baud rate 230400 460800 These high baud rates are not normally recommended for RS 232 serial ports 4 ARINC 42...

Страница 111: ...in parenthesis Table 3010 ARINC Port Input Speed Configuration Settings Setting Description Low Low speed ARINC 429 12 5 kBaud High High speed ARINC 429 100 kBaud b The ARINC 429 Input channels accept...

Страница 112: ...2 Table 3013 Transpnder Cntrl Input ARINC Labels Label Description 016 TCAS ATC control squawk code and IDENT only 031 ATCRBS control squawk code and IDENT only 233 Flight ID Characters 1 and 2 234 F...

Страница 113: ...tion to ARINC 429 output port Traffic traffic Display Output Ownship data and traffic intruder data format for displays that receive the ARINC 735 A B traffic labels listed in Table 3020 GPS 743 GPS 2...

Страница 114: ...ble 3020 GPS 743 Output Labels Order Setting Description 3 273 Sensor status 076 Altitude MSL 110 Latitude 111 Longitude 120 Latitude fine 121 Longitude fine 125 UTC 103 Track angle 112 Ground speed 1...

Страница 115: ...uration and setup through the MPI on Serial Port 3 or 5 The MPI connections detailed in Paragraph 10 J can be connected to a PC or Tablet through one of following two devices Off the shelf RS 232 to U...

Страница 116: ...e interfacing directly to the MPI using a terminal interface program on a PC like Tera Term to enter MPI commands Any of the two interface devices mentioned above can be used to interface to the PC EF...

Страница 117: ...8 Bit 1 Bit None NOTE 1 Odd parity is only required if Port 3 is configured to TMAP at 38400 baud If the port has changed from either of these default settings Parity should be set to None 2 MPI WiFi...

Страница 118: ...9000016 Figure 3006 Sheet 1 of 1 Tera Term Terminal Setup Figure 3007 Sheet 1 of 1 Tera Term Serial Port Setup EFFECTIVITY ALL Page 3020 22 Dec 2016 Honeywell International Inc Do not copy without exp...

Страница 119: ...ntenance Interface Diagrams 1 Maintenance Interface Diagrams for configuring the KGX through the MPI are represented in Figure 3009 and Figure 3010 Figure 3009 Sheet 1 of 1 Off the shelf RS 232 to USB...

Страница 120: ...ds Command Description ads Display data from the altitude air data input bit Display built in test status clear Clear the screen comm Display communication port s status continuous control Display con...

Страница 121: ...ration item s value setpw Set MPI access password See Section 6 G cnfg defaults Reset configuration to defaults stop Stop continuous data outputs 2 help or Command a This command displays a list of av...

Страница 122: ...ually displays serial port communication status information Enabled disabled status Receive and transmit byte count and errors b The data is updated once for each second Refer to Figure 3014 for an ex...

Страница 123: ...1 of 1 control Command 7 gps Command a This command displays data which is being received from the GPS input Refer to Figure 3016 Figure 3016 Sheet 1 of 1 gps Command 8 info Command a This command dis...

Страница 124: ...ected Reed Solomon errors RSErr x d The third rxstatus section displays detailed traffic information This information includes total number of traffic targets being tracked and then detailed informati...

Страница 125: ...nd to stop updating rxstatus and return to the prompt Figure 3019 Sheet 1 of 1 rxstatus Command 11 cnfg Command a This command displays configurable information such as the serial port settings protoc...

Страница 126: ...used to modify configuration settings such as ICAO address call sign and serial port function Help on this command is displayed by entering set Example set output is shown in Figure 3021 EFFECTIVITY...

Страница 127: ...his section describes the configuration settings for serial and ARINC port functionality 2 set serial in Command a This command sets the serial port input configuration options Help on this command is...

Страница 128: ...Help on this command is displayed by entering set serial out Refer to Figure 3024 for an example NOTE Refer to Paragraph 3 C Step 3 for information on selecting serial output settings NOTE Serial Por...

Страница 129: ...This command sets the ARINC 429 input configuration for Ports 1 and 2 Refer to Figure 3025 for an example NOTE Refer to Paragraph 3 C Step 4 for information on selecting ARINC input settings EFFECTIVI...

Страница 130: ...ration for Port 1 Note that there is only one ARINC 429 output port Refer to Figure 3026 for an example NOTE Refer to Paragraph 3 C Step 5 for information on selecting ARINC output settings Figure 302...

Страница 131: ...rcraft and is typically the aircraft tail number For example to set the call sign to ABCD1234 enter set call sign ABCD1234 The default call sign is transmitted by a transceiver if a call sign setting...

Страница 132: ...a This command sets the receiver installed options to be transmitted by a transceiver Transceivers must be set to 978 and no1090 It is not necessary to set this for a receiver only Refer to Figure 30...

Страница 133: ...in the air This must be set for all KGX products Refer to Figure 3033 Figure 3033 Sheet 1 of 1 set squat Command 9 set threshold Command a This command sets the groundspeed threshold which is used to...

Страница 134: ...to Figure 3035 Figure 3035 Sheet 1 of 1 set acsize Command 11 set uatant Command a This command sets the UAT antenna configuration This must be set for all KGX products Refer to Figure 3036 Figure 30...

Страница 135: ...d must not be set in receiver only units This should be set to enable if using the external or internal Xpndr Monitor functions Refer to Figure 3038 Figure 3038 Sheet 1 of 1 set modeArx Command 14 set...

Страница 136: ...A Command a This command enables disables the Conflict Situational Awareness CSA bit in the Heartbeat message of the Traffic Alert protocol This parameter defaults to disable and must ONLY be set to e...

Страница 137: ...directional traffic Setting this parameter to disable turns off all DO 317A TSO C195a velocity validation invalidation and passes the track s velocity data to the display as directional traffic This...

Страница 138: ...control panel 2 setpw Command refer to Figure 3044 a This command allows the installer to set a password in order to access the MPI The password goes into effect once the unit is reset and prevents a...

Страница 139: ...the password protection from the MPI and allows normal access 1 Remove power from the KGX 2 Ground Pins J1 12 Anonymous Mode J1 15 Traffic Test J1 27 Air Gnd 3 Apply power to the KGX and turn on by gr...

Страница 140: ...advances to the next configuration item b The following paragraphs detail the setup modes available for configuring the KGX 2 Aircraft Mode S or ICAO Address a The Mode S address is a 24 bit number as...

Страница 141: ...types Type A The characters corresponding to the registration marking of the aircraft Type B The telephony designator of the aircraft operating agency followed by the last four characters of the regi...

Страница 142: ...he CODE knob either clockwise or counterclockwise to display the options above and select the groundspeed threshold Once selected press the ENT key to confirm your selection and move to the next confi...

Страница 143: ...e c Rotate the CODE knob either clockwise or counterclockwise to display the options above and select the correct squat switch type Once selected press the ENT key to confirm your selection and move t...

Страница 144: ...tions from above c Rotate the CODE knob either clockwise or counterclockwise to display the options above and select the correct serial input type Once selected press the ENT key to confirm your selec...

Страница 145: ...guration mode Figure 3056 Sheet 1 of 1 Serial IN Channel X Line Speed Display 10 Serial OUT Channel X Data Type NOTE X Channel number a The KGX can transmit data through two serial channels The follow...

Страница 146: ...ration mode is not displayed and the next configuration mode item is displayed Figure 3057 Sheet 1 of 1 Serial OUT Channel X Data Type Display 11 Serial OUT Channel X Line Speed NOTE X Channel number...

Страница 147: ...he CODE knob either clockwise or counterclockwise to display the options above and select the correct ARINC input type Once selected press the ENT key to confirm your selection and move to the next co...

Страница 148: ...or counterclockwise to display the options above and select the correct ARINC output type Once selected press the ENT key to confirm your selection and move to the next configuration item in the confi...

Страница 149: ...Sheet 1 of 1 Select MAX Targets Output Display 17 GPS Certification a The KGX requires a valid GPS source so that aircraft position can be transmitted in its ADS B message The GPS source is usually ce...

Страница 150: ...n in the software GPS auto is automatically set from the velocity FOM VFOM data from the GPS unit The NACv value is hard coded to be broadcast better than 3 meters sec even if GPS Auto is selected Fig...

Страница 151: ...distance from the nose can be entered anywhere between 2 meters and 60 meters by rotating the CODE knob either clockwise or counterclockwise to display the correct distance Once selected press the EN...

Страница 152: ...ions from above e Rotate the CODE knob either clockwise or counterclockwise to display the options above and select either enable or disable Once selected press the ENT key to confirm selection and mo...

Страница 153: ...set at Bottom Only b The display screen is as shown in Figure 3074 c Rotate the CODE knob either clockwise or counterclockwise to display the correct antenna diversity option Once selected press the...

Страница 154: ...e altitude seen on the pilot s primary altimeter is the same as what is transmitted by the KGX The maximum allowed difference between the primary altimeter and the altitude encoder is 125 feet 38 1 m...

Страница 155: ...the configuration modes until reaching the calibrate altitude encoder section When you are in the calibrate altitude encoder setup mode the display shows the information shown in Figure 3077 4 Rotate...

Страница 156: ...own in Figure 3081 for pressure altitude reported c Use at least 10 test points and verify that in each case the altitude displayed on the primary altimeter and the altitude displayed on the KGX contr...

Страница 157: ...itude reported by the primary altimeter Refer to Figure 3082 Figure 3082 Sheet 1 of 1 Pressure Altitude Reported Display b Push the ENT button and the display instructs completion of setup and powers...

Страница 158: ...SYSTEM INSTALLATION MANUAL 89000016 Blank Page EFFECTIVITY ALL Page 3060 22 Dec 2016 Honeywell International Inc Do not copy without express permission of Honeywell...

Страница 159: ...Check KGX control panel system messages ST LED is flashing quickly GPS fault has occurred Check GPS connection configuration Check KGX control panel system messages GPS LED is flashing slowly GPS is...

Страница 160: ...bly not be transmitting ADS B messages To view the system messages on the Warning page push the FN button four times and WARNING is displayed top center along with a brief description of the fault The...

Страница 161: ...t or nominal rate failure Cycle power on the KGX Check for valid ICAO address config Tx Power Low Transmitter power too low Check antennas and cabling Return for maintenance if problem persists Tx PSU...

Страница 162: ...antenna disconnected Check antenna connection Make sure antenna is DC grounded Disable DC ground check in config if antennas are not DC grounded PSU Fail Internal DC power supply failure Cycle power o...

Страница 163: ...perature 4 5 3 C4 158 F 70 C Ground survival low temperature 4 5 1 C4 67 F 55 C Ground survival high temperature 4 5 3 C4 185 F 85 C Loss of cooling 4 5 5 NA Altitude 4 6 D 50 000 feet 15 240 m Decomp...

Страница 164: ...anel DO 160 qualification Table 5002 KGX Control Panel DO 160F Qualification Condition Paragraph Category Spec Temperature and altitude 4 C4 C4 A4 Ground survival low temperature 4 5 1 C4 67 F 55 C Sh...

Страница 165: ...netic effect 15 Z Power input 16 NA Voltage spike 17 NA Audio frequency conducted susceptibility Power inputs 18 NA Induced signal susceptibility 19 BC Radio frequency susceptibility 20 TT Emission of...

Страница 166: ...SYSTEM INSTALLATION MANUAL 89000016 Blank Page EFFECTIVITY ALL Page 5004 22 Dec 2016 Honeywell International Inc Do not copy without express permission of Honeywell...

Страница 167: ...econd 2 Compatible devices include Rosetta encoders and serializers ARS 50 and ARS 100 The compatible format for altitude information is the 10 byte ASCII message shown in Table 6001 Table 6001 ASCII...

Страница 168: ...ield ends with a carriage return line feed CR 0D0AH 4 All numeric fields are ASCII decimal right justified and zero filled If the ADC cannot supply data in a particular field the field is filled with...

Страница 169: ...n Air ground discrete input 10 North velocity From GPS data 11 East velocity From GPS data 12 Ground speed From GPS data 13 Track angle From GPS data 14 Heading From configured heading input 15 Barome...

Страница 170: ...ng Not supported in current software 38 Barometric pressure setting Not supported in current software 39 Selected heading Not supported in current software 40 Status of MCP FCU mode Not supported in c...

Страница 171: ...llation Overview 1 Connectors a Connectors present on the WiFi module are as follows Signal Power DB 15 Signal WiFi Antenna SMA NOTE The WiFi module SMA antenna is preinstalled with the system 2 Statu...

Страница 172: ...0 C Storage 67 to 185 F 55 to 85 C Altitude 50 000 feet 15 24 km Power requirements 10 to 37 VDC typical 40 mA at 28 VDC Frequency 2 402 to 2 480 MHz Receiver sensitivity 83 dBm typical 2 Refer to Tab...

Страница 173: ...interface details pertaining to installation Adherence to these installation procedures and information will assure satisfactory system performance B Unpacking and Inspecting Equipment 1 Exercise car...

Страница 174: ...ting requirements illustrated in Figure 8002 Figure 8002 Sheet 1 of 1 WiFi Module Mounting Dimensions D Electrical Interface 1 Electrical interconnection to the WiFi module is made through a 15 pin D...

Страница 175: ...te is 115 200 E Connecting to the WiFi Module 1 The WiFi module can be connected from any device that supports AM 802 11 wireless solution or chipset For example the WiFi module can be connected using...

Страница 176: ...UAL 89000016 Figure 8003 Sheet 1 of 1 Example Screen Shots for Connecting to Wireless Network in Windows EFFECTIVITY ALL Page 8006 22 Dec 2016 Honeywell International Inc Do not copy without express p...

Страница 177: ...ple Screen Shots for Connecting to Wireless Network on an Apple iPad Figure 8005 Sheet 1 of 1 Example Screen Shots for Wireless Windows Connection EFFECTIVITY ALL Page 8007 22 Dec 2016 Honeywell Inter...

Страница 178: ...al Qualifications Environmental Test Section Category Compliance Method Temperature and altitude 4 C4 D A 1 T Loss of cooling 4 5 5 NA X 2 Temperature variation 5 B T Humidity 6 A T Shock crash safety...

Страница 179: ...ostatic discharge 25 NA X Fire flammability 26 NA X Compliance method key T Test X No testing required no credit requested NA Not applicable NOTES 1 D Altitude at 50 000 feet 15 24 km A Overpressure a...

Страница 180: ...SYSTEM INSTALLATION MANUAL 89000016 Blank Page EFFECTIVITY ALL Page 8010 22 Dec 2016 Honeywell International Inc Do not copy without express permission of Honeywell...

Страница 181: ...ON MANUAL 89000016 Figure 8007 Sheet 1 of 1 Typical KGX and WiFi Module Interconnect Diagram EFFECTIVITY ALL Pages 8011 8012 22 Dec 2016 Honeywell International Inc Do not copy without express permiss...

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