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89000109-002

xVue Touch Installation Manual

Rev 2

Page 1-7

For Use in Non-Certified Aircraft

PBIT

Power-up Built-in Test

Personal Computer

PMA

Parts Manufacturer Approval

Part Number

POH

Pilot’s Operating Handbook

PWR

Power

RAM

Random Access Memory

REF

Reference

Radio Frequency

Rngs

RIngs

RTCA

Radio Technical Commission for Aeronautics

RTD

Resistance Temperature Detectors

RTN

Return

Receive

Second

SDI

Serial Digital Interface

SEL

Select

International System of Units

Serial Number

SPI

Serial Peripheral Interface

Stainless Steel

STD

Standard

SVS

Synthetic Vision System

Software

SXM

XM Satellite Data

TAWS

Terrain Awareness and Warning System

Type Certificate

TCDS

Type Certificate Data Sheet

TIS-B

Traffic Information Service-Broadcast

TSO

Technical Standard Order

Transmit

Table 1-3 Acronyms and Abbreviations

Acronyms and
Abbreviations

Definition

Summary of Contents for KG 71EXP

Page 1: ...7 International Direct XVUE TOUCH PRIMARY FLIGHT DISPLAY SYSTEM INSTALLATION MANUAL FOR USE IN NON CERTIFIED AIRCRAFT Document P N 89000109 002 Rev 2 November 2019 Export Control Thisdocumentcontainst...

Page 2: ...ever this License Agreement will govern in the event of a conflict between its terms and conditions and those of a purchase order or acknowledgment 1 License Grant If you are a party to an applicable...

Page 3: ...se Agreement you will return these Materials to Honeywell without retaining any copies and will have one of your authorized officers certify that all Materials have been returned with no copies retain...

Page 4: ...A Form 174 or equivalent from the manufacturers or suppliers of the materials to be used The user must know the manufacturer supplier data and obey the procedures recommendations warnings and cautions...

Page 5: ...e in the preparation of this document to assure its accuracy Honeywell assumes no liability resulting from any errors or omissions in this document or from the use of the information contained herein...

Page 6: ...ircraft RECORD OF REVISIONS NOTE The revision level for every page of this document will be updated during the revision process A list of effective pages is therefore not required Revision Revision Da...

Page 7: ...m ADAHRS 2 4 2 3 4 KMG 7010 MD32 Magnetometer 2 4 2 3 5 KDC 100EXP Data Converter 2 4 2 3 6 KTP 73 OAT Probe 2 5 2 4 Technical Specifications 2 5 2 5 Environmental Qualification Form EQF 2 9 2 6 Regul...

Page 8: ...3 22 3 6 6 KCP 100EXP Installation Considerations 3 22 3 6 6 1 KCP 100EXP Location 3 22 3 6 7 KG 71EXP Installation Considerations 3 23 3 6 7 1 KG 71EXP Location 3 23 3 6 7 2 KG 71EXP Orientation 3 24...

Page 9: ...t Verification 4 11 4 5 KG 71EXP Installation 4 12 4 5 1 KG 71EXP Installation Procedures 4 12 4 5 2 KG 71EXP Post Installation Unit Verification 4 13 4 6 KMG 7010 Installation 4 14 4 6 1 KMG 7010 Ins...

Page 10: ...23 6 2 3 GPS NAV Configuration Setup 6 23 6 2 3 1 GPS Navigation Source 6 25 6 2 3 2 VLOC Navigation Source 6 26 6 2 4 Autopilot Configuration Setup 6 29 6 2 4 1 AP Computer 6 31 6 2 4 2 Sync FD Offs...

Page 11: ...heckout 7 13 7 3 EMI Interaction Checkout 7 14 7 4 Post Installation Flight Checks 7 14 7 5 Post Installation Activities 7 14 7 5 1 Database Updates 7 14 7 5 1 1 USB Database Loading 7 15 7 5 1 2 Wi F...

Page 12: ...4 8 Adjustments 9 8 9 2 4 9 Testing 9 8 9 2 4 10 Lubrication 9 8 9 2 5 Servicing Information 9 8 9 2 6 Troubleshooting 9 8 9 2 7 Storage Limitation 9 8 9 2 8 Removal and Reinstallation Information 9 8...

Page 13: ...odule Circuit Card Assembly 4 6 Figure 4 8 Bottom Side of J2 Backshell 4 6 Figure 4 9 KSD 100EXP Grip Installation Sheet 1 of 2 4 7 Figure 4 10 KSD 100EXP Grip Installation Sheet 2 of 2 4 8 Figure 4 1...

Page 14: ...d Keypad Example 6 21 Figure 6 29 Master VOL Sub Menu 6 22 Figure 6 30 TAWS Toggle 6 22 Figure 6 31 GPS NAV Sub Menu 6 23 Figure 6 32 GPS 1 Sub Menu 6 25 Figure 6 33 GPS2 Sub Menu 6 26 Figure 6 34 VLO...

Page 15: ...bled 7 19 Figure 7 22 Connected to KSD Wi Fi 7 20 Figure 7 23 DataManager Lite Main Page 7 20 Figure 7 24 Wi Fi Webpage with Selected Database 7 21 Figure 7 25 Uploading Databases to KSD 100EXP 7 21 F...

Page 16: ...ure A 8 KMG 7010 Outline and Mounting Drawing Sheet 1 of 2 A 8 Figure A 9 KMG 7010 Outline and Mounting Drawing Sheet 2 of 2 A 9 Figure A 10 MD32 Outline Drawing A 10 Figure A 11 KDC 100EXP Outline an...

Page 17: ...egulatory Compliance 2 19 Table 3 1 Pre Installation Checklist 3 3 Table 3 2 xVue Touch System Components and Kits 3 5 Table 3 3 Installation Kit Backshell Assembly KSD 100EXP PN 89000120 002 3 5 Tabl...

Page 18: ...Viewed from LRU 5 11 Table 5 10 KTP 73 Wire Descriptions 5 12 Table 5 11 Configuration Module J2 Backshell Pin Descriptions 5 12 Table 6 1 Supported Navigation Sources 6 24 Table 6 2 Supported Autopi...

Page 19: ...ragraph or step Notes follow the applicable paragraph or step 1 1 2 Observance of Manual Instructions 1 Make sure that you carefully obey all safety quality operation and shop procedures for the unit...

Page 20: ...iption United States GPO Style Manual available at http www gpo gov fdsys pkg GPOSTYLEMANUAL 2008 content detail html 14 CFR Part 43 Title 14 of Code of Federal Regulations 14 CFR Part 43 MAINTENANCE...

Page 21: ...3 Electrostatic Discharge Control Handbook for Protection of Electrical and Electronic Parts Assemblies and Equipment Excluding Electrically Initiated Explosive Devices Metric available from any milit...

Page 22: ...aircraft and the CG of the unit installed on the aircraft AS Aerospace Standard ASME American Society of Mechanical Engineers AWG American Wire Gauge A429 ARINC 429 Data Transfer Standard BL Backligh...

Page 23: ...on System ESD Electrostatic Discharge ESDS Electrostatic Discharge Sensitive EGPWS Enhanced Ground Proximity Warning System EQF Environmental Qualification Form ETH Ethernet F Fahrenheit FAA Federal A...

Page 24: ...r second kg Kilogram kPa Kilopascal KT Knots lb Pound LED Light Emitting Diode Lgnd Legend LOC Localizer LRU Line Replaceable Unit m Meter Mbit Megabit MEMS Micro Electromechanical Sensors MIL Militar...

Page 25: ...Radio Technical Commission for Aeronautics RTD Resistance Temperature Detectors RTN Return RX Receive s Second SDI Serial Digital Interface SEL Select SI International System of Units SN Serial Numbe...

Page 26: ...metallic aircraft refers to all other aircraft fiberglass or composite skin and aircraft with tube and fabric construction UAT Universal Access Transceiver USB Universal Serial Bus USMS United States...

Page 27: ...fication of non type certificated aircraft to install the xVue Touch This installation manual is not a substitute for an approved airframe specific flight and or maintenance manuals installation drawi...

Page 28: ...P Data Converter included with MD32 Magnetometer 6 KTP 73 Outside Air Temperature OAT Probe 7 Configuration Module The xVue Touch System is depicted in Figure 2 1 and Figure 2 2 Figure 2 1 xVue Touch...

Page 29: ...r glove The display has a light sensor that detects cockpit lighting conditions for automatic dimming of the display Dimming can also be controlled manually The KSD 100EXP includes a USB port for data...

Page 30: ...speed ARINC The KG 71EXP communication with the KMG 7010 Magnetometer is via a dedicated Controller Area Network CAN bus The KG 71EXP communication with the MD32 Magnetometer is via the KDC 100EXP da...

Page 31: ...p and 32 2VDC max Circuit Breaker 2 AMP for 28 VDC 3 AMP for 14 VDC systems Cooling Convection cooled does not required forced air cooling within the unit operational temperature range refer to Sectio...

Page 32: ...thin the unit operational temperature range refer to Section 3 6 7 3 for cooling considerations Connectors Male 50 pin D sub Female 9 pin D sub Maintenance port Table 2 5 KG 71EXP ADAHRS Performance C...

Page 33: ...25 C after 2 minute warmup 200 mA Nominal 55 C after 2 minute warmup 700 mA Maximum 55 C Typical 28VDC 0 08 AMP Typical 14VDC 0 16 AMP Circuit Breaker 1 AMP for 28 VDC 2 AMP for 14 VDC systems Signal...

Page 34: ...mA Maximum 55 C Circuit Breaker 1 AMP for 28 VDC 2 AMP for 14 VDC systems Signal Inputs Outputs Serial CAN Bus Cooling Convection cooled No external cooling required Connector Male 15 pin Certificati...

Page 35: ...pplicable 5 0 Temperature Variation C 2 C minute 6 0 Humidity A 7 0 Operational Shocks and Crash Safety B A C Type 3 Test R 8 0 Vibration S curve M Zone 2 9 0 Explosive Atmosphere X 10 0 Waterproofnes...

Page 36: ...oprene with horizontal burn Test Bezel Seal Neoprene Cord with horizontal burn 4 Conducted Susceptibility CS testing was performed using DO 160E Cat A per FAA Policy PS ACE 23 10 5 Radiated Susceptibi...

Page 37: ...perational Shocks and Crash Safety B A C Type 3 Test R 8 0 Vibration S curve M Zone 2 9 0 Explosive Atmosphere X 10 0 Waterproofness X 11 0 Fluids Susceptibility X 12 0 Sand and Dust X 13 0 Fungus Res...

Page 38: ...rizontal burn 4 Conducted Susceptibility CS testing was performed using DO 160E Cat A per FAA Policy PS ACE 23 10 5 Radiated Susceptibility RS testing was performed using the following levels per FAA...

Page 39: ...nal Shocks and Crash Safety B See Note 4 Aircraft Type 3 Test F 8 0 Vibration S curve M 9 0 Explosive Atmosphere X 10 0 Waterproofness Y Condensing water 11 0 Fluids Susceptibility X 12 0 Sand and Dus...

Page 40: ...erformed using DO 160E Cat A per FAA Policy PS ACE 23 10 6 Radiated Susceptibility RS testing was performed using the following levels per FAA Policy PS ACE 23 10 7 The Outside Air Temperature OAT par...

Page 41: ...Vibration S curves E L M T R curve G See Note 1 Fixed Wing Zone 5 Helicopter Zone 1b 9 0 Explosive Atmosphere E Environment II Supplemental Analysis Performed beyond DO 160D DO 160G Section 9 analysi...

Page 42: ...0 Lightning Direct Effects X Not Tested 24 0 Icing A 25 0 Electrostatic Discharge ESD A N A Fire Flammability Not Applicable Supplemental Testing beyond DO 160D DO 160G Section 26 Cat C Labels only HP...

Page 43: ...EE1 9 0 Explosion X 10 0 Waterproofness W 11 0 Fluids X 12 0 Sand and Dust X 13 0 Fungus Resistance X 14 0 Salt Fog S 15 0 Magnetic Effect Z 16 0 Power Input Z 17 0 Voltage Spike A 18 0 Audio Frequenc...

Page 44: ...able 5 0 Temperature Variation A 10 C per minute 6 0 Humidity C 7 0 Operational Shocks and Crash Safety A 6 g 11 ms Pulse Crash Safety Impulse Sustained no test performed 8 0 Vibration S Curve M T Zon...

Page 45: ...6 Regulatory Compliance Table 2 17 xVue Touch System Component Regulatory Compliance Component Function Approval Type KSD 100EXP Display PMA KCP 100EXP Display Control PMA KG 71EXP Air Data Attitude a...

Page 46: ...lateral map display at the location corresponding to the obstacle latitude and longitude 2 7 4 Terrain Database The Terrain Database is used to render the terrain to create a realistic view of the te...

Page 47: ...standby instruments provide a secondary reference altitude altimeter and airspeed indication 2 10 Required GPS Navigator Installation of the xVue Touch System requires at least one GPS SBAS navigator...

Page 48: ...2 xVue Touch Installation Manual Rev 2 Page 2 22 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure 2 3 Standby Instrument Power R...

Page 49: ...rn Refer to the troubleshooting instructions in Section 8 Troubleshooting If repair is necessary the unit must be sent to a BendixKing certificated repair facility The xVue Touch System components are...

Page 50: ...the installation considerations in Section 3 6 along with the installation procedures in Section 4 as they are presented to accomplish a successful installation Read the entire sections before beginn...

Page 51: ...SCHARGE SENSITIVE ESDS DEVICES ESDS DEVICES ARE SUBJECT TO DAMAGE BY EXCESSIVE LEVELS OF VOLTAGE AND OR CURRENT THE LOW ENERGY SOURCE THAT MOST COMMONLY DESTROYS ESDS DEVICES IS THE HUMAN BODY WHICH I...

Page 52: ...h the xVue Touch System Section 3 6 1 xVue Touch System Interfaces Acceptable KSD 100EXP instrument panel location within the primary field of view Section 3 6 5 KSD 100EXP Installation Considerations...

Page 53: ...Audio Panel and Section 6 2 2 3 Master Audio Volume Installation operational limitations reviewed to ensure no adverse impact to the installation Section 2 11 Installation Limitations Section 9 2 2 A...

Page 54: ...Connectors Install Kit 89000120 003 KSD 100EXP Mounting Hardware and Grip Install Kit 89000120 007 KCP 100EXP Control Panel Install Kit for Portrait Mounting 89000126 004 KCP 100EXP Control Panel Inst...

Page 55: ...ctor Contact Crimp Socket Size 22 78 EA Table 3 5 Installation Kit Mounting Hardware and Grip KSD 100EXP PN 89000120 007 Part Number Description Qty UM 89500020 024 KSD 100EXP Grip 1 EA MS51957 1B 2 5...

Page 56: ...ruction For Harness Assembly Parts REF REF 010 00068 0002 Crimp Terminal 4S 1 EA 030 01157 0011 Socket Crimp 20G 9 EA 030 01499 0011 Connector D Sub Hood EMI RFI Metal Jackscrews 9 Pos 1 EA 057 05944...

Page 57: ...d MD32 and performing the post installation compass verification Table 3 13 Installation Materials Required but Not Supplied Description PN or Specification Quantity Note Wire 22 20 18 16 AWG M22759 1...

Page 58: ...is maintained Nutplates 4 40 MS21069L04 or MS21071L04 4 Orientation is optional as long as minimum edge distance is maintained Rivets MS20426AD3 X 16 X size 10 32 Rivet nuts NAS1329A3KXX 4 XX size St...

Page 59: ...ter Equivalent inclinometer with accuracy of 0 1 degrees Commercially Available Pitot static tester Commercially Available NAV ILS Signal Generator Commercially Available Aircraft Power Unit Commercia...

Page 60: ...XP ADAHRS Installation Kit 89000123 007 M81969 1 04 RED and White Metal Insert Removal Tools AMF8 Crimp Tool M22520 2 01 K13 1 Crimper Turret Head Positioner M22520 2 08 D sub 9 Socket Connector Tools...

Page 61: ...1 Discrete Inputs Refer to the tables below for the discrete input states Table 3 15 KSD 100EXP Discrete Input Ground Open DIGO States State Voltage Level Active 0 VDC Inactive Open Circuit Table 3 16...

Page 62: ...ta rate on this bus is 1 Mbit s 3 6 Installation Considerations In general equipment must be installed in a location convenient for operation inspection and maintenance and in an area free from excess...

Page 63: ...9 002 xVue Touch Installation Manual Rev 2 Page 3 14 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure 3 2 xVue Touch System Inte...

Page 64: ...e may be other devices that can be configured the same as the ones listed below but have not been tested by BendixKing Table 3 22 xVue Touch Compatible Equipment Category Vendor Model Audio Panel Bend...

Page 65: ...GTN 725 Avidyne IFD 410 IFD 510 IFD 545 Radio Navigators BendixKing KX 155 KX 155A KX 165 KX 165A Garmin GNC 255 GPS Radio Navigators BendixKing KSN 770 Garmin GNS 430W GNS 530W GTN 650 GTN 750 Avidy...

Page 66: ...inches For airplane with original panel thickness of 0 063 inches or greater the new panel thickness must match the original panel Magnetometer BendixKing KMG 7010 Magnetometer MidContinent Instrument...

Page 67: ...Either two inch or three inch standby instruments may be used 3 6 3 1 Standby Instrument Location Standby instrument locations are recommended per AC 23 1311 1C Section 15 to be within 35 degrees fro...

Page 68: ...ASI needs a battery pack or an emergency power system that meets the 30 minute operational requirement 3 6 3 4 Standby Altimeter The existing airplane altimeter must be retained for use as a standby...

Page 69: ...guidance and are recommended for the xVue Touch System installation The primary field of view is measured in both the horizontal and vertical fields as illustrated in Figure 3 3 reference AC 23 1311 1...

Page 70: ...struments is 0 5 inch 12 7 mm from the top or bottom of the KSD 100EXP cutout to the instrument 2 The installed location is away from heat sources including electronic instruments Heat generating sour...

Page 71: ...y the KG 71EXP is not the lowest point in the pitot static system to reduce the chance of allowing moisture to enter the unit The locations chosen for the KG 71EXP and the method of installation will...

Page 72: ...must be leveled with the airplane s pitch and roll within 15 degrees Many airplane models have an airplane level reference shelf that is in alignment with the actual airplane s pitch and roll level A...

Page 73: ...es of the level airplane The KMG 7010 MD32 should be located as far as possible from all sources of magnetic disturbance or ferrous materials such as nickel iron steel cobalt or magnetic field inducin...

Page 74: ...ter is located alongside it Isolate the specific electrical device causing the current and ground the device using a wire rather than the airframe The wire should be routed alongside the devices power...

Page 75: ...llation orientations 3 6 10 KTP 73 Installation Considerations 3 6 10 1 KTP 73 Location To ensure accurate temperature readings the KTP 73 OAT probe must be mounted to the wing or fuselage and away fr...

Page 76: ...f the airplane structure sufficient to extend the tip into the free stream Ensure adequate space for sensor lead cable routing is available Refer to the airplane maintenance manual for additional info...

Page 77: ...d be connected to the essential bus If the airplane has more than one essential bus the xVue Touch System components should be connected to one essential bus and the electronic standby instruments con...

Page 78: ...d the nearest airframe grounding point Electrical bonding begins with the equipment attach point s such as the mounting rack or the instrument panel Ensure good metal to metal bonding as brackets and...

Page 79: ...lateral and vertical deviation from GPS sources and navigation receivers in the airplane It is not recommended to use external CDI in conjunction with the xVue Touch System External serial data source...

Page 80: ...th the existing autopilot on the airplane must be retained and may require relocation refer to AC 23 1311 1C Due to space constraints it may be necessary to blind mount the unit The installer must ens...

Page 81: ...Ensure the instrument panel is prepared per Section 3 6 2 and the locations for the KSD 100EXP PFD and KCP 100EXP Control Panel are determined based on considerations in Section 3 6 5 and Section 3 6...

Page 82: ...ttach to the P1 upper and P2 lower wiring harness connectors refer to Figure 4 1 Each 78 pin D sub connector housing provided in the KSD 100EXP Installation Kit Configuration Module And Connectors is...

Page 83: ...ms and part descriptions See Table 5 1 KSD 100EXP J1 Pin Descriptions Viewed from LRU for pin designations Figure 4 3 KSD 100EXP J1 Connector Assembly Using the KSD 100EXP Installation Kit Backshell A...

Page 84: ...ottom Side of J2 Backshell Torque screws to 4 0 4 in lbs 0 45 0 05 Nm 4 3 1 2 J2 Connector Configuration Module Assembly The KSD 100 J2 Connector Configuration Module Assembly mounts to the lower D Su...

Page 85: ...per J STD 001 to the Configuration Module CCA provided in the KSD 100EXP Installation Kit Configuration Module using Table 4 1 Configuration Module J2 Backshell Pin Descriptions Table 4 1 Configurati...

Page 86: ...ewed from LRU 6 Insert the seven socket connector contacts from the Configuration Module into J2 housing per Table 4 1 Configuration Module J2 Backshell Pin Descriptions 7 Inside the backshell base in...

Page 87: ...ocedures 1 Prepare the KSD 100EXP for installation a Using the KSD 100EXP Mounting Hardware and Grip Installation Kit install the Santoprene Grip by sliding the grip from the back of the KSD 100EXP an...

Page 88: ...been prepared per Section 4 2 3 Ensure all power is removed from the airplane 4 Verify grounding for the KSD 100EXP see note below If utilizing the center ground stud located on the back of the KSD 10...

Page 89: ...10 Electrical Bonding Considerations 7 Install the KSD 100EXP into the instrument panel while ensuring that the USB port is located on the left side of the unit from the pilot s perspective and secur...

Page 90: ...ions refer to Figure A 5 4 4 1 KCP 100EXP Instrument Panel Installation Procedures 1 Ensure all wiring and power checks have been completed per Section 6 1 2 Ensure airplane instrument panel has been...

Page 91: ...nting hole locations b Install Center Stack Adapter using the four 6 32 pan head screws and clip nuts refer to Figure 4 13 KCP 100EXP Landscape Center Stack Installation 6 Install the KCP 100EXP to th...

Page 92: ...educe airplane vibration effects 4 Prepare mounting rivet nut locations as bonding points such that the bonding resistance conforms to the guidelines listed in Section 3 10 Electrical Bonding Consider...

Page 93: ...12 Attach the pitot and static lines to their corresponding fitting on the KG 71EXP 60 in lbs 6 8 Nm maximum DO NOT OVERTIGHTEN The KG 71EXP is labeled PITOT and STATIC at the fitting sites to provid...

Page 94: ...nector The only restriction is that once the KMG 7010 is installed the KMG 7010 pitch and roll offsets should be within 5 degrees from the airplane pitch and roll The total count of acceptable install...

Page 95: ...the three KMG 7010 primary axes are parallel within 5 degrees of the longitudinal lateral and vertical axes of the level airplane The KMG 7010 may be mounted parallel to the lateral pitch longitudina...

Page 96: ...ll the MD32 Magnetometer per its installation manual see Appendix D MD32 Installation Manual 4 7 1 MD32 Post Installation Unit Verification Accomplish the following steps in this manual before return...

Page 97: ...d 7 Apply conversion coating material conforming to MIL C 81706 per AC 43 13 1B to exposed metal surfaces 8 Install mounting adapter plate as applicable 9 Using the KDC 100EXP Installation Kit mount t...

Page 98: ...Certified Aircraft 13 Verify the electrical bond between the KDC 100EXP and the airframe conforms to the guidelines listed in Section 3 10 Electrical Bonding Considerations Verify the electrical bond...

Page 99: ...t skins from 0 016 to 0 032 inch thickness The number rivets can be increased and shape of the doubler modified to suit the particular installation For thicker skins a separate approval is required Do...

Page 100: ...ugh to enable maintenance personnel to troubleshoot repair and service the electrical system The diagrams should also include a method of determining the connector type if other than the connectors su...

Page 101: ...n the Type Certificate Data Sheet TCDS and airplane specification s The various xVue Touch System components and associated nominal weights are listed in Table 4 3 below Note The connector and backshe...

Page 102: ...tified Aircraft KMG 7010 Magnetometer 065 00189 0101 0 9 0 41 See Figure A 8 MD32 Magnetometer 6420032 0 19 0 085 N A KDC 100EXP Data Converter 89000138 001 0 9 0 41 See Figure A 8 KTP 73 OAT Probe 89...

Page 103: ...if published in the Airplane Flight Manual In addition in the event of a complete loss of the primary electrical system the battery s must be capable of providing at least 30 minutes of electrical po...

Page 104: ...ed in Table and should be used for the ELA values Verify the aircraft electrical load does not exceed 80 of the alternator generator data plate rated capacity or the maximum load value if published in...

Page 105: ...3_RX_H In Reserved 7 WX_RADAR_A429_TX_A Out Reserved 8 UAT_WX_RS232_RX In Included 9 UAT_WX_RS232_TX Out Included 10 NAV1_2_ROLL_STR_VAL_DO28VO Out Reserved 11 NAV1_ROLL_STR_VALID_DI28VO In Reserved 1...

Page 106: ...SPARE_A429_RX_B In Reserved 41 SPARE_A429_RX_A In Reserved 42 KA_52 57_P15V_PWR PWR Reserved 43 AFCS_DATUM_VAL_DO5VO Out Reserved 44 AFCS_CRS_DATUM_OUT Out Included 45 AFCS_CMD_BAR_RTRCT_DI15VO In Inc...

Page 107: ...72 NAV_FLAG_ Out Included 73 NAV_DEV_ _RT Out Included 74 AFCS_HDG_DATUM_OUT Out Included 75 TRANSPONDER_A429_RX_B In Reserved 76 TRANSPONDER_A429_RX_A In Reserved 77 ADAHRS2_A429_TX_B Out Reserved 78...

Page 108: ...KINGBUS_CLK_DI5VO In Reserved 27 AFCS_KINGBUS_DATA_DI5VO In Reserved 28 AFCS_KINGBUS_STROBE_DI5VO In Reserved 29 SXM_WX_RS422_RX_A In Reserved 30 SXM_WX_RS422_RX_B In Reserved 31 SXM_WX_RS422_TX_A Out...

Page 109: ...TN GND Included 60 NAV_DEV_ _RT_IN In Reserved 61 NAV_DEV_ _LT_IN In Reserved 62 NAV_FLAG_ _IN In Reserved 63 NAV_FLAG_ _IN In Reserved 64 APM_DATA_MISO In Included 65 APM_DATA_MOSI Out Included 66 AP...

Page 110: ...3 KCP 100EXP J1 Pin Descriptions Viewed from LRU 5 3 KG 71EXP 5 3 1 KG 71EXP Connector J71 The electrical interface for the KG 71EXP is provided via the 50 pin D Sub connector referenced as J71 Table...

Page 111: ...5 Temp Probe 2 In 16 Temp Probe 3 In 17 Not Used N A 18 Power GND In 19 Power GND In 20 Power GND Spare In 21 RS 232 Ch0 TXD Out 22 RS 232 Ch0 RTS Out 23 RS 232 Ch0 RXD In 24 RS 232 Ch0 CTS In 25 DGND...

Page 112: ...Pressure Port Fitting s Figure 5 1 Pressure Port Fitting s 43 A429 TX1 A Out 44 A429 TX1 B Out 45 Chassis GND GND 46 CAN H In 47 CAN L In 48 A429 TX2 B Out 49 Interlock 1 In 50 Interlock 2 In Table 5...

Page 113: ...for the KMG 7010 is provided via the 9 pin DB 9 connector referenced as J7010 Details about the J7010 connector interface are shown in Table 5 7 Table 5 7 KMG 7010 DB 9 Pin Descriptions Viewed from L...

Page 114: ...5 2 KMG 7010 Backshell 5 5 MD32 The electrical interface for the MD32 is provided via the 9 pin DB 9 connector Table 5 8 Table 5 8 MD32 DB 9 Pin Descriptions Viewed from LRU Pin Description I O 1 Grou...

Page 115: ...ble 5 9 Table 5 9 KDC 100EXP Pin Descriptions Viewed from LRU Figure 5 3 KDC 100EXP Backshell Pin Description I O 1 Magnetometer 429 RX HI In 2 Magnetometer 429 RX LO In 3 Ground NC 4 Magnetometer CAN...

Page 116: ...rtified Aircraft 5 7 KTP 73 5 8 Configuration Module Table 5 10 KTP 73 Wire Descriptions Wire Color Description I O Red TEMP3 Out Black TEMP1 Out White TEMP2 Out Table 5 11 Configuration Module J2 Bac...

Page 117: ...le the KSD 100EXP will display the Database Acknowledge Screen see Figure 6 3 The maintenance technician may enter the Installation Maintenance Menu from this page The KSD 100EXP PFD has one dedicated...

Page 118: ...ouch Installation Manual Rev 2 Page 6 2 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure 6 1 KSD 100EXP Installation Maintenance...

Page 119: ...ess must be checked for proper connections to the airplane power bus Point to point continuity must be checked to identify any faults such as shorting to ground Any faults or discrepancies must be cor...

Page 120: ...only accessible on ground from the Database Acknowledge Screen Figure 6 3 or the APM Mismatch Error Screen Figure 6 4 To access Config Mode apply the following touch sequence 1 Touch the B on the Ben...

Page 121: ...Installation Manual Rev 2 Page 6 5 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure 6 4 APM Configuration Mismatch Screen Figure...

Page 122: ...onfiguration settings in the Installer Main Menu Fields which have been changed are displayed in a green font Figure 6 6 Configuration Preview Window The Installer Main Menu on the left side of the Co...

Page 123: ...Non Certified Aircraft button is available on the top left side of each of the sub menus Selecting the Back Arrow button will return to the previous active menu Only upon pressing the Save Exit butto...

Page 124: ...Use in Non Certified Aircraft 6 2 1 System Configuration Setup The System Config button allows the technician to configure the following parameters as shown in Figure 6 8 1 Lighting 2 External Dimmin...

Page 125: ...ay the System Config sub menu Figure 6 8 2 To change lighting configuration press the Lighting button to display the Lighting sub menu and select between 28 VDC and 14 VDC shown in Figure 6 9 Figure 6...

Page 126: ...htness level is appropriately balanced with the other cockpit instruments Note Default value is 1 e With the external lighting control at its minimum value set the KCP Lgnd Legend min value by touchin...

Page 127: ...buttons to adjust the Display backlight so the maximum brightness level is appropriately balanced with the other cockpit instruments Note Default value in 80 e With the external lighting control at it...

Page 128: ...1 3 Aircraft Tail Number 1 From the System Config sub menu Figure 6 8 press the A C Tail button 2 Using the alpha numeric keyboard shown in Figure 6 13 input the aircraft tail number and press the En...

Page 129: ...Keypad 3 Verify that the Serial Number is reflected correctly on the Aircraft Serial button as illustrated in Figure 6 16 Figure 6 16 A C Serial 6 2 1 5 Aircraft Pitch Bias Pitch bias function provide...

Page 130: ...tem Config sub menu Figure 6 8 when the Pilot V Spd indicator shows Locked the Configurable Pilot V Speed settings on the PFD menu cannot be modified The avionics installer should use the following pr...

Page 131: ...e Back Arrow button to exit the System Config sub menu and return to the Installer Main Menu Figure 6 7 6 2 1 8 Units Configuration The Units configuration is accessed from the System Config sub menu...

Page 132: ...Config sub menu Figure 6 8 3 Press the Back Arrow button to exit the System Config sub menu and return to the Installer Main Menu Figure 6 7 6 2 2 PFD Configuration Setup The PFD button allows the tec...

Page 133: ...figuration options include 2000 fpm 3000 fpm 4000 fpm The VSI Range configuration is accessed from the PFD sub menu Figure 6 23 and the current VSI Range is shown on the VSI button Pressing the VSI bu...

Page 134: ...st be less than or equal to VNE 3 VFE Maximum Flaps Extended speed top of white band 4 VS1 No Flaps Stall speed A green band is displayed on the airspeed tape between VS1 and VNO VS1 must be less than...

Page 135: ...MANUAL AFM PILOT S OPERATING HANDBOOK POH OR OTHER LEGAL DOCUMENTATION E G PLACARDS NOTE THE V SPEED UNITS ARE DEFINED IN SECTION 6 2 1 8 UNITS CONFIGURATION AND THE V SPEED VALUES ARE CLEARED IF THE...

Page 136: ...press the Airspeed button to display the Airspeed sub menu Figure 6 27 Figure 6 27 Airspeed Sub Menu 2 From the Airspeed sub menu press the desired V Speed button to display the V Speed Keypad NOTE AN...

Page 137: ...the modified V Speed button on the Airspeed sub menu Figure 6 27 5 After the V Speeds are entered press the Back Arrow button to return to the PFD sub menu 6 2 2 3 Master Audio Volume 1 From the PFD s...

Page 138: ...ther system s and adjust as needed 6 Press the Back Arrow button to return to the PFD sub menu 6 2 2 4 Terrain Awareness and Warning System TAWS Toggle The TAWS configuration is used to indicate if an...

Page 139: ...altitude preselect configuration is used to indicate whether the KSD 100EXP PFD pilot selected altitude function is enabled or disabled If the airplane is already equipped for a pilot selectable altit...

Page 140: ...avigators two digital VHF Navigator radios and one analog legacy VHF Navigator radio A GPS Navigator and VHF Navigator may be integrated in a single unit In addition to the ARINC 429 data the KSD 100E...

Page 141: ...avigator and will process and monitor all analog signals provided by the Analog VHF Navigator The default configuration for the VHF Navigator analog interface is Not Connected In this configuration th...

Page 142: ...ted LRU is reflected correctly on the GPS2 button shown in Figure 6 31 6 2 3 2 VLOC Navigation Source NOTE THE XVUE TOUCH WILL AUTOMATICALLY SET THE NAVIGATION RADIO SOURCE VLOC 1 OR 2 WHEN THE SELECT...

Page 143: ...6 34 3 Press the Back Arrow button to return to the GPS NAV sub menu 4 Verify that the selected LRU is reflected correctly on the VLOC1 button shown in Figure 6 31 5 If there is a second NAV radio ins...

Page 144: ...tified Aircraft Figure 6 35 VLOC2 Sub Menu 6 Press the button for the installed LRU option from the VLOC2 sub menu Figure 6 35 7 Press the Back Arrow button to return to the GPS NAV sub menu 8 Verify...

Page 145: ...ation Setup The Autopilot button allows the technician to configure the following parameters as shown in Figure 6 36 1 Autopilot LRU 2 Sync FD Offset 3 Sync FD Gain 4 GPSS K Factor Figure 6 36 Autopil...

Page 146: ...nected The KSD 100EXP in this configuration does not drive outputs for a legacy autopilot and related monitoring is deactivated Only the analog autopilot interface is supported The technician must con...

Page 147: ...gure 6 36 press the AP Computer button to display the AP Computer sub menu Figure 6 37 l Figure 6 37 AP Computer Sub Menu 2 Press the button for the installed LRU option from the AP Computer sub menu...

Page 148: ...tor adjusts the Heading Datum Roll Steering relationship from 50 GPSS K Factor of 0 5 to 200 GPSS K Factor of 2 0 with 10 resolution Use the following procedure for setting the GPSS K Factor 1 Create...

Page 149: ...mission of Honeywell For Use in Non Certified Aircraft Figure 6 39 GPSS K Factor Keypad 5 Using the keypad input the new value for the GPSS K Factor and press the Enter button 6 Verify that the new GP...

Page 150: ...6 41 Broadcast WX Sub Menu 2 From the Broadcast WX sub menu Figure 6 41 press the Broadcast WX button Table 6 3 Supported Broadcast WX Sources Manufacturer Model BendixKing KGX 130x KGX 150x FreeFligh...

Page 151: ...t LRU sub menu Figure 6 42 4 Press the Back Arrow button to return to the Broadcast WX sub menu 5 Verify that the selected Broadcast LRU is reflected correctly on the Broadcast WX button shown in Figu...

Page 152: ...on to display the Traffic sub menu Figure 6 43 Figure 6 43 Traffic Sub Menu 2 From the Traffic sub menu Figure 6 44 press the ADS B Traffic button Figure 6 44 ADS B Sub Menu 3 Press the button for the...

Page 153: ...the KG 71EXP is physically installed into the airplane and the wiring complete and verified complete the following configuration steps 1 Maintenance Interface Configuration 2 KG 71EXP Installation Ori...

Page 154: ...operated by the technician The KG 71EXP should be powered off when the USB to RS 232 cable is connected to the maintenance port The CMT application should be started after the PC is connected to the...

Page 155: ...ilt angles offsets must be configured and stored as a first step during the unit configuration The KG 71 tab provides two sub tabs 1 Installation in Airframe 2 Digital I O The tab Installation in Airf...

Page 156: ...ned the pitch angle and roll angle are measured and displayed If the KG 71EXP pitch and roll offsets are installed within 15 degrees and the detected pitch and roll angle are within 1 degree typically...

Page 157: ...The Digital I O tab illustrated in displays the KG 71EXP I O configuration and provides means to modify the I O setup The KG 71EXP has a dedicated receive channel Rx0 for the PFD and the SDI must be s...

Page 158: ...10 11 The value must be the same as the SDI of labels which are provided by the GPS Navigator 2 GPS Standard a GAMA if GPS meets the GAMA standard common for General Aviation GPS navigators b ARINC 74...

Page 159: ...r as the Tx channel which is dedicated for communication with the KSD 100EXP 6 3 1 3 2 Attitude Heading The transmit channel can be configured to support existing AHRS systems with a basic set of atti...

Page 160: ...80 Hz 2 325 Roll Angle transmit rate 80 Hz 6 3 1 3 6 Altitude Interface The transmit channel can be configured to support existing systems with an altitude data set This configuration sets transmit ch...

Page 161: ...dy Longitudinal Acceleration BNR 80 332 Body Lateral Acceleration BNR 80 333 Body Normal Acceleration BNR 80 336 Inertial Pitch Rate BNR 80 337 Inertial Roll Rate BNR 80 340 Inertial Yaw Rate BNR 80 3...

Page 162: ...ct any combination of AHRS and ADC labels to send out If the rate for the label is selected the label will be transmitted at that rate Once ARINC Bus Speed and all required labels and rates are select...

Page 163: ...erface can be configured to use one of the following protocols 1 Icarus 10 2 Icarus 100 3 SHADIN S 4 SHADIN M 5 BendixKing Format C 6 4 KMG 7010 MD32 Calibration Magnetometer The KG 71EXP system suppo...

Page 164: ...Location MD32Mounting Location MD32Connector Location KMG CMT Image Up Back Down Right 7 Up Left Down Back 16 Up Front Down Left 3 Up Right Down Front 15 Down Back Up Left 5 Down Left Up Front 14 Down...

Page 165: ...6 4 1 Magnetometer Installation Orientation Figure 6 53 KMG 7010 Calibration Page As shown in Figure 6 53 once the mounting orientation is selected the technician must enter the measured pitch offset...

Page 166: ...ometer offsets have been entered and while aircraft is leveled the maintenance connection can be disconnected and the KG 71EXP circuit breaker can be cycled and pitch and roll should be displayed as z...

Page 167: ...uired heading value it should begin with 360 degrees 4 Once the airplane is physically oriented to the specified heading wait 30 60 seconds for the reading to stabilize NOTE BEFORE THE MAGNETOMETER CA...

Page 168: ...ng button on the CMT screen 6 Verify that the Measured Heading value is within 9 degrees a If the value is within range press the Confirm Reading button refer to Figure 6 55 b If the value is out of t...

Page 169: ...heading values displayed on the PFD orienta tion in 4 directions North 90 180 and 270 degrees Verify accuracy of 2 degrees of the air plane s orientation and verify drift from each of the target head...

Page 170: ...hed before proceeding to the ground and flight tests 7 1 Recommended Test Equipment The following test equipment is recommended to complete the post installation checkout procedures in this section 1...

Page 171: ...ith the pitot static tester connect the tester to the airplane pitot static system and perform a leak check of the system This may be conducted concurrently with the Altitude Display Vertical Display...

Page 172: ...ter is achieved and stabilized verify that the KSD 100EXP altitude tape and standby altimeter display the same altitude as the pitot static tester the tolerance listed in 14 CFR Part 43 Appendix E Tab...

Page 173: ...irspeed Labels button Figure 7 4 and ensure that Airspeed Labels are toggled on Figure 7 3 PFD Setup Sub Menu Figure 7 4 Airspeed Labels Button 2 Verify the airspeed units KTS OR MPH set during the co...

Page 174: ...S display or through the GPS status page available on most GPS systems 3 On the Navigator clear any existing Flight Plan and enter a Direct To waypoint with a known location relative to the airplanes...

Page 175: ...2 Page 7 6 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft 9 From the Menu Figure 7 6 press the PFD button to launch the PFD Menu Figu...

Page 176: ...t the Bearing 1 source to GPS1 Figure 7 9 Figure 7 9 Pointer 1 Sub Menu 12 From the Pointer 1 sub menu press the Up Arrow button to return to the Bearing Pointers sub menu 13 From the Bearing Pointers...

Page 177: ...ointer matches the Bearing Pointer 1 and Bearing Pointer 2 21 On the KCP 100EXP rotate the CRS knob counterclockwise such that the CDI course pointer is to the left of the GPS1 bearing 22 From the KSD...

Page 178: ...nu Figure 7 8 press the Pointer 2 button and set the source to VLOC1 Figure 7 9 12 Close the Main Menu by pressing the X button to return to the KSD 100EXP screen 13 On the VHF Radio Tester set the mo...

Page 179: ...EXP PFD screen verify the following a Verify the CDI source is set to VOR1 displayed in green b Verify the CDI course deviation is deflected right at the first deviation scale dot 5 degree dot 25 On t...

Page 180: ...scale dot and the Vertical Deviation bar is deflected down near the first deviation scale dot 37 On the VHF Radio Tester set the LOC DDM to simulate a two dot right deviation and set the G S DDM to si...

Page 181: ...ge is no longer listed b Press the Up Arrow button to return to the Main menu a Close the Main Menu by pressing the X button to return to the KSD 100EXP screen 7 2 10 Autopilot System Setup The manufa...

Page 182: ...lue increases 5 Enter a Flight Plan to an OBS WPT on the Navigator a Verify the course on the HSI is synchronized with the GPS Bearing to WPT value by pushing the CRS knob on the KCP 100EXP 6 Turn the...

Page 183: ...equipment for 30 seconds each 5 Individually turn on for 30 seconds then turn off each fuel pump deice boots windshield heat prop heat and flaps 6 Individually operate autopilot servos yaw damper and...

Page 184: ...isplay 3 Press Enter on the Database Acknowledge Screen refer to Figure 6 3 4 On the KSD 100EXP screen Figure 7 1 press the Menu button Figure 7 2 located at the top right of the screen 5 From the Mai...

Page 185: ...se Loading Menu 8 The Database Loading Page is displayed while the files are unpacked During this time the External Database column shows status as Scanning Figure 7 16 Figure 7 16 Database Loading Pa...

Page 186: ...than the installed database Expired Cycle the USB database is older than the installed database If no database is available on the USB drive an error message Error No database detected on external de...

Page 187: ...is displayed for each remaining database to be loaded shown in Figure 7 19 Figure 7 19 Database Loading in Progress Screen 12 When the database loading is complete a pop up window is displayed as show...

Page 188: ...e KSD 100EXP 3 Press Enter on the Database Acknowledge Screen refer to Figure 6 3 4 On the KSD 100EXP screen Figure 7 1 press the Menu button Figure 7 2 located at the top right of the screen 5 From t...

Page 189: ...net browser and enter the web address https ksd100 bendixking com to access the DataManager Lite application Figure 7 23 12 From the webpage select Choose File Figure 7 23 DataManager Lite Main Page 1...

Page 190: ...t Loading to KSD to begin the database loading process Figure 7 24 Wi Fi Webpage with Selected Database Uploading and verifying the database s takes about 6 to 10 minutes This process uploads the data...

Page 191: ...restart window appears on the external device signaling the completion of the Wi Fi database loading procedure Figure 7 28 Figure 7 28 Restart KSD 100EXP Window 17 Cycle power on the KSD 100EXP 18 Rev...

Page 192: ...ission of Honeywell For Use in Non Certified Aircraft 4 On the FlyQ App main screen press the Download symbol Figure 7 29 Figure 7 29 FlyQ App Main Screen The ChartData Manager screen appears and disp...

Page 193: ...screen Figure 7 30 6 Select the chart data type to download for each selected region available charts depend on subscription Figure 7 30 Charts IFR Lo NOTE SELECT ALL STATES THAT YOU MAY FLY TO IN THE...

Page 194: ...the connection has been set up FlyQ application detected window appears on the KSD 100EXP Figure 7 31 9 On the iPad iPhone check that the desired states have been updated 10 Press OK on the KSD 100 Fi...

Page 195: ...e appears Figure 7 32 Figure 7 32 FlyQ Database Update Available Window 11 Press OK to update or Cancel Figure 7 32 Performing FlyQ database update window appears Figure 7 33 Figure 7 33 Performing Fl...

Page 196: ...escription Corrective Action ERROR NODATABASES DETECTED ON EXTERNAL DEVICE Database not present on the USB drive Download the database again and reload Future Cycle Database on USB drive is newer than...

Page 197: ...Figure 7 36 Database Loading Completed with Errors Window The Wi Fi database loading has unique error messages that will appear in the status window refer to the example in Figure 7 37 and the list o...

Page 198: ...mismatch between what is set in the database and the serial number of the unit on the airplane Verify KSD 100EXP serial number unit on airplane download a new database ZIP file with the correct KSD 1...

Page 199: ...have part numbers and serial numbers stored in the various system component s NVM Installation of new software in a xVue Touch component will change the part number of the unit and must follow the pr...

Page 200: ...ning on the avionics 4 Access Config Mode refer to steps in Section 6 2 5 Insert the USB drive with USB C adapter into the front USB port on the KSD 100EXP refer to Figure 2 1 for USB port location 6...

Page 201: ...e 7 41 10 A prompt window Figure 7 42 will appear and states the projected duration of the software load and a reminder to not interrupt power Press the Ok button to proceed and the system will begin...

Page 202: ...7 45 Software Loading Pop Up Window Power Cycle 14 During boot up Access Config Mode refer to steps in Section 6 2 if there is an APM configuration mismatch error message is displayed on the screen o...

Page 203: ...ing the loading process 7 5 2 3 KG 71EXP Software Update The KG 71EXP software cannot be updated in the field The unit must be returned to BendixKing if an update is required Table 7 5 Software Loadin...

Page 204: ...4 4 Check wiring to KSD 100EXP Circuit Breaker Not Set or Defective Check and or replace circuit breaker KSD 100EXP Defective Replace KSD 100EXP Smart Touch Not Working Touch Sensor Failure Reset KSD...

Page 205: ...ed X AHRS Has Not Completed Initialization Wait for Attitude Aligning message to complete If on ground do not move aircraft while alignment is annunciated If in flight maintain straight and level flig...

Page 206: ...peed failed See Altimeter Airspeed Failures troubleshooting procedure Any status parameters related to Ground Speed Track Angle Magnetic Variation True Airspeed and Magnetic Heading are invalid See No...

Page 207: ...e performed RAM Memory Check Heartbeat Check APM Backup Check APM Module Check APM Module Data Check APM Backup Module and APM Module Mismatch Pilot Configuration NVM Memory Check Loopback Check FPGA...

Page 208: ...LE DETECTION FAULT Displayed PBIT APM Module Detection Fault Loss of Communication with Configuration Module Check that Configura tion Module is installed and wired properly Configuration Module Defec...

Page 209: ...iring from Autopilot to KSD 100EXP Reset KSD 100EXP If fault persists replace KSD 100EXP CBIT AFCS_CRS_ DEV _FLAG_OUT Loopback Fault Data Corrupted Reset KSD 100EXP If fault persists replace KSD 100EX...

Page 210: ...owledge Screen refer to Figure 6 3 3 On the KSD 100EXP screen Figure 7 1 select the Menu button Figure 7 2 located at the top right of the screen 4 From the Main Menu Figure 7 6 select the System Tool...

Page 211: ...h point presented as a plus sign Figure 8 3 Example of Touch Calibration Utility Screen 9 When the user s touch is detected a bloom is displayed around the requested touch point 10 The touch point plu...

Page 212: ...at random locations one after the other on the screen where the user should touch to test the precision of the Touch operation 15 Following the test button operation the Accept button is displayed at...

Page 213: ...is restored to normal display with no menus open 8 2 2 Default Touch Calibration The user has the option to revert to the default calibration settings 1 Press the Restore Def Touch Cal button from the...

Page 214: ...Restore Def Touch Cal menu the following screen Figure 8 7 is displayed indicating the successful restoration of the default values Figure 8 7 Restoration of Default Values Successful Screen 3 Press...

Page 215: ...replace the KG 71EXP unit Note that because the CMT Application SW cannot communicate with the KG 71EXP there is no event logged After power up the KG 71EXP system does not provide any valid data all...

Page 216: ...perature probe wiring including the KG 71EXP connector If there is no problem with wiring replace temperature probe If problem persists replace the KG 71EXP unit Note If temperature is out of the rang...

Page 217: ...ck fails NA Restart the KG 71EXP If problem per sists replace the KG 71EXP unit Note that because of this failure Applica tion SW cannot start thus no event is logged Next the communication with the C...

Page 218: ...e data and heading data during flight is reported HG 1120 CBIT detects a failure 7 Restart the KG 71EXP If problem per sists replace the KG 71EXP unit HG 1120 SPI Communication CBIT detects a failure...

Page 219: ...more reliable Magnetometer availability CBIT detects a failure 14 Check the KMG 7010 MD32 wiring and circuit breaker including KMG 7010 MD32 and KG 71EXP connec tors If there is no issue with wiring r...

Page 220: ...the magnetometer data readouts are significantly off from the required heading values there are the following probable sources 1 Ferrous bolts nuts were used to secure magnetometer or ferrous connecto...

Page 221: ...or ALTITUDE FAIL Barometric altitude failure Use the standby altitude indicator VERTICAL SPEED FAIL Altitude rate failure or rate is out of range 5500 Use the standby vertical speed indicator GPS SOUR...

Page 222: ...troubleshooting procedure in Table 8 1 xVue Touch System Troubleshooting Chart SVS POS Fault If any of the following inputs become invalid o Pressure Altitude o True Airspeed o Calibrated Airspeed See...

Page 223: ...FAIL See No Navigation Data or Failure troubleshooting procedure in Table 8 1 xVue Touch System Troubleshooting Chart UAT FAIL Loss of Communication with UAT Check Wiring from UAT to KSD 100EXP Impro...

Page 224: ...d database Re download failed database source content to USB drive and reload failed database If fault persists replace KSD 100EXP Database Tiles Corrupted During Run Time Reload failed database Re do...

Page 225: ...ired prop erly Replace Configuration Module PILOT CONFIGURATION FAULT Pilot Stored Configuration Data Has Been Lost Replace KSD 100EXP APM MODULE CONFIGURATION DATA FAULT Configuration Module Defectiv...

Page 226: ...off to allow it to cool down Check for adequate ventilation Check airflow around the KSD 100EXP for any blockages WARNING TERRAIN TERRAIN Warning during flight Comply with Warning WARING OBSTACLE OBS...

Page 227: ...100EXP provides an alternative to the KSD 100EXP touch control capability for entering parameters such as altitude and barometric pressure course and heading The configuration module stores the confi...

Page 228: ...tergent solution Dawn dish washing soap or similar and distilled water 1 Apply the water based detergent solution onto a clean lint free cotton cloth or cotton swab to clean the glass face 2 Carefully...

Page 229: ...er to confirm that there is a maximum resistance of 2 5 milliohms or less between the unit and airframe ground If a resistance is found to be too high disassembly of the brackets will be required Chec...

Page 230: ...ding straps or ground wires are in good condition and are not loose or chafing Connection points to the units and to the airframe must be inspected for evidence of corrosion If any of these indication...

Page 231: ...osion If any of these indications are present an electrical bonding test must be performed 12 months KMG 7010 MD32 Magnetometer A general visual inspection of the KMG 7010 MD32 Magnetometer and the as...

Page 232: ...chanical installation for condition including checking the unit and all mounting brackets for security Loose and chafing brackets will increase the resistance between parts Check for signs that the un...

Page 233: ...es are in good condition and are not loose or chafing Connection points to the units and to the airframe must be inspected for evidence of corrosion If any of these indications are present an electric...

Page 234: ...uch System components 9 2 6 Troubleshooting Refer to Section 8 of this document for troubleshooting steps The xVue Touch System components are not field repairable Repairs must be made by a properly c...

Page 235: ...nector and remove the KTP 73 from the airplane 9 2 8 1 4 KG 71EXP Removal Execute the following steps for removal of the KG 71EXP 1 Ensure all power is removed from airplane 2 Disconnect the KG 71EXP...

Page 236: ...2 3 Leak Test and Section 9 2 8 2 5 KMG 7010 Reinstallation For reinstallation of the KMG 7010 execute the steps in Section 4 6 KMG 7010 Installation as well as the steps in Section 6 3 KG 71EXP Confi...

Page 237: ...e 9 11 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft 9 2 8 3 Return to Service Verify proper operation of the xVue Touch System by f...

Page 238: ...llation Manual Rev 2 Page A 1 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft APPENDIX A OUTLINE AND INSTALLATION DRAWINGS Figure A 1...

Page 239: ...002 xVue Touch Installation Manual Rev 2 Page A 2 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure A 2 KSD 100EXP Panel Cutout D...

Page 240: ...Installation Manual Rev 2 Page A 3 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure A 3 KCP 100EXP Dimensions and Center of Grav...

Page 241: ...nstallation Manual Rev 2 Page A 4 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure A 4 KCP 100EXP Dimensions and Center of Gravi...

Page 242: ...l International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure A 5 KCP 100EXP Panel Cutout Dimensions NOTE UTILIZE SAME KCP 100EXP PANEL CUTOUT DIMENS...

Page 243: ...xVue Touch Installation Manual Rev 2 Page A 6 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure A 6 KG 71EXP Dimensions and Cente...

Page 244: ...2 xVue Touch Installation Manual Rev 2 Page A 7 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure A 7 KG 71EXP Mounting Hole Patt...

Page 245: ...Touch Installation Manual Rev 2 Page A 8 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure A 8 KMG 7010 Outline and Mounting Dra...

Page 246: ...Touch Installation Manual Rev 2 Page A 9 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure A 9 KMG 7010 Outline and Mounting Dra...

Page 247: ...00109 002 xVue Touch Installation Manual Rev 2 Page A 10 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure A 10 MD32 Outline Draw...

Page 248: ...ouch Installation Manual Rev 2 Page A 11 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure A 11 KDC 100EXP Outline and Mounting D...

Page 249: ...ouch Installation Manual Rev 2 Page A 12 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure A 12 KDC 100EXP Outline and Mounting D...

Page 250: ...xVue Touch Installation Manual Rev 2 Page A 13 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure A 13 KTP 73 Dimensions and Cente...

Page 251: ...Rev 2 Page A 14 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure A 14 KTP 73 Mounting Hole Pattern Figure A 15 KTP 73 Generic D...

Page 252: ...tallation Manual Rev 2 Page B 1 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft APPENDIX B INTERCONNECT DIAGRAMS Figure B 1 xVue Touch...

Page 253: ...3 D Z W d E E D Z ZK E E E s s Zd E s s d h E s E s hW E s D z E s K K K E Z W K K Z dhD Khd dhD Khd dhD Khd Z t y t D hdKW Kd KDWhd Z D Z Z E s s Zd E s s d E s E s hW E KDW s E K E Z E W E Z dhD dh...

Page 254: ...Y Where XX is gauge and Y is color 2 Twisted Shielded Pair Triplet and Shielded Single Wire x All wires shall conform to ANSI NEMA WC 27500 x Do not remove any wiring between other active aircraft sys...

Page 255: ...Zy W d Zy W D Zy W D Zy W D dy W D dy W D Zy W D Zy W D dy W D dy W Z E W Z dy E W Z dy E W Z E sKZ dy sKZ dy sKZ Zy sKZ Zy sKZ Zy sKZ Zy sKZ dy sKZ dy KtE E hW E KtE E hW E d d d d E E E E Z h Z h Z...

Page 256: ...31 29 T 17 14 15 16 T 17 32 43 31 32 33 1 1 NOTES 1 Twisted Shielded Pair Triplet and Shielded Single Wire x All wires shall conform to ANSI NEMA WC 27500 x Do not remove any wiring between other acti...

Page 257: ..._15VDC KSD100_CTRL_PANEL_PWR_RTN 9 8 15VDC_PWR_IN 15VDC_PWR_RTN 5 NOTES 1 Single Conductor Wire x All wires shall be 22 AWG unless otherwise noted power wires x Wiring shall meet AS22759 16 XX Y Where...

Page 258: ...nc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure B 7 KG 71 LRU Interconnect Diagram 1 yW d DW WZK d DW WZK d DW WZK Z t dW d DW d DW d DW yW E E D E h E...

Page 259: ...002 xVue Touch Installation Manual Rev 2 Page B 8 Honeywell International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure B 8 KG 71 LRU Interconnect D...

Page 260: ...express permission of Honeywell For Use in Non Certified Aircraft Figure B 9 KG 71 LRU Interconnect Diagram 3 E t yW dy dy Zy Zy E t E t W t W t dE dE dE dE dE E E EKd t x t x t yy z t yy z d W d t x...

Page 261: ...not copy without express permission of Honeywell For Use in Non Certified Aircraft Figure B 10 KG 71 LRU Interconnect Diagram 4 yW Z dy d Z d E EKd t x t x t yy z t yy z d W d t x E E D t x d D yW dy...

Page 262: ..._______________________________ Table C 1 xVue Touch System Component Locations Description PN Airplane Location Access Panels KSD 100EXP PFD 89000120 001 KCP 100EXP Control Panel Portrait KCP 100EXP...

Page 263: ...l International Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft On Figure C 1 draw in the location of the xVue Touch System components and the wiring routing...

Page 264: ...Non Certified Aircraft On Figure C 2 draw in the location of the xVue Touch System components and the wiring routing Figure C 2 xVue Touch System Components and Cable Routing Side View On Figure C 3 d...

Page 265: ...Power Source Capacity Analysis and confirm the aircraft electrical system is capable of supporting the xVue Touch System Refer to Section 4 12 for additional information Table C 2 Electrical Load Anal...

Page 266: ...nal Inc Do not copy without express permission of Honeywell For Use in Non Certified Aircraft APPENDIX D MD32 INSTALLATION MANUAL For instructions on how to install the MD32 Magnetometer see the Insta...

Page 267: ...structions Model MD32 Series Remote Magnetometer Mid Continent Instrument Co Inc dba Mid Continent Instruments and Avionics 9400 E 34th Street N Wichita KS 67226 Manual Number 9019050 PH 800 821 1212...

Page 268: ...mcico com We welcome your comments concerning this manual Although every effort has been made to keep it free of errors some may occur When reporting a specific problem please describe it briefly and...

Page 269: ...ided additional details in 2 4 regarding limitations and deviations 2 Added description for wire shield terminations 3 Updated Environmental Qualification Statement in 3 2 4 Removed reference to EASA...

Page 270: ...Performance Limits 6 Qualifications 6 SECTION 2 INSTALLATION 7 2 1 GENERAL INFORMATION 7 2 2 PARTS LIST 7 2 3 EQUIPMENT LOCATION 7 2 4 LIMITATIONS 7 2 5 MODIFICATIONS 8 2 6 CABLE HARNESS 9 Wire Gauge...

Page 271: ...e 4 wire shielded cable connecting data and power to the MD302 As an added benefit the backup battery integral to the MD302 is also capable of supporting the MD32 Remote Magnetometer in the case of ai...

Page 272: ...inches x 0 81 inches LxWxH Mating Connector MCI P N 8017287 Mounting Base mount any orientation Table 1 2 Performance Limits Heading Accuracy vs Latitude Within 2 up to 55 N or 45 S increasing error t...

Page 273: ...incomplete system It must be installed in conjunction with an MD302 Standby Attitude Module MCIA part number 6420302 to provide complete heading functionality The MD302 must have software version 1 1...

Page 274: ...r 6420032 has a nameplate that identifies the manufacturer part number description certifications and technical specifications of the unit It also includes the MOD or modification number representing...

Page 275: ...make a tee connection to Pin 1 of the MD302 Another option is to connect to Pin 11 of a MOD 2 MD302 for backup power from the internal battery Pin 6 ARINC Out B connects to MD302 Pin 13 Optionally it...

Page 276: ...Rev C March 30 2018 10 Manual Number 9019050 Figure 2 1 MD32 Outline Drawing...

Page 277: ...nued airworthiness of the MD32 Remote Magnetometer If the unit fails to perform to specifications or if the magnetic environment of the aircraft installation changes over time recalibration may be per...

Page 278: ...ash Safety 7 Category B Vibration 8 Category R Curves E E1 REE1 Explosion 9 Category X Waterproofness 10 Category W Fluids 11 Category X Sand and Dust 12 Category X Fungus 13 Category X Salt Fog 14 Ca...

Page 279: ...Honeywell International Inc Do not copy without express permission of Honeywell...

Page 280: ...umber of Reviewers 1 Finished 1 Not Finished 0 Approver Progress Approver Name Title Percent Complete Approval Date Signature Signature Comments Dustin J Sinko Engineer Pr Systems 100 November 1 2019...

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