Fault Designation GPS BUS Bus Type Basic, Utc | Honeywell MKXXII

Honeywell

MK XXII EGPWS Installation Manual

MSL type. The Universal GPS1000 based GPS sources are of WGS-84 type. If the internal GPS source (ID=2) is defined, the GPS altitude reference in Category 7 must be MSL.

Note 2: Universal GPS 1000 does not calculate VFOM and HFOM correctly which makes it an unacceptble position source for helicopters.

TABLE E 3.1.3-0: POSITION INPUT TYPE 0 (LOW SPEED ARINC 743A GPS)

CHANNEL

429RX_4

CONNECT TO: GPS (Low Speed) per ARINC 743A-2

Fault Designation: GPS BUS

Bus Type: Basic

A= J2-25 B = J2-8

Data

Latitude - Normal

Longitude - Normal

GPS Hor. Int. Limit

Altitude

VFOM

HFOM

Ground Speed

True Track Angle

Sensor Status

**UTC

**Date

**This label is not required.

Data used if present

Label

110

111

130

076

136

247

112

103

273

125

260

Sig. Bits

20

20

17

20

18

18

15

15

19

19

19

Range

±180 Degrees ±180 Degrees

16nm

±131,072 FT 32768 ft

16nm

±4096 Knots ±180 Degrees Discrete Wd Discrete Wd Discrete Wd

Signal Type

Basic

Basic

Basic

Basic

Basic

Basic

Basic

Basic

Basic

Basic

Basic

Resolution

0.00017166137695

0.00017166137695

0.00012207

0.125

0.125

0.000061035

0.125

0.0054931640625

n/a

0.1min

1 day

*Rate (ms)

1000

1000

1000

1000

1000

1000

1000

1000

1000

1000

1000

*Slowest acceptable update rate in milliseconds.

TABLE E 3.1.3-1: POSITION INPUT TYPE 1 (LOW SPEED ARINC 743 GPS)

CHANNEL

429RX_4

CONNECT TO: GPS (Low Speed) per ARINC 743

Fault Designation: GPS BUS

Bus Type: Basic

A= J2-25 B = J2-8

Data

Latitude - Normal

Longitude - Normal

GPS Hor. Int. Limit

Altitude

VFOM

HFOM

Ground Speed

True Track Angle

Sensor Status

**UTC

**Date

**This label is not required.

Data used if present

Label

110

111

130

076

136

247

112

103

273

125

260

Sig. Bits

20

20

17

20

15

15

15

15

19

19

19

Range

±180 Degrees ±180 Degrees

16nm

±131,072 FT 1024 meters 1024 meters ±4096 Knots ±180 Degrees Discrete Wd Discrete Wd Discrete Wd

Signal Type

Basic

Basic

Basic

Basic

Basic

Basic

Basic

Basic

Basic

Basic

Basic

Resolution

0.00017166137695

0.00017166137695

0.00012207

0.125

0.03125

0.03125

0.125

0.0054931640625

n/a

0.1min

1 day

*Rate (ms)

1000

1000

1000

1000

1000

1000

1000

1000

1000

1000

1000

*Slowest acceptable update rate in milliseconds.

CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225

REV: C SHEET 196

Image 196

Honeywell MKXXII installation manual Fault Designation GPS BUS Bus Type Basic, Utc

Contents

Release Date 12/14/00 REV C Sheet ALL Revisions REV Description Honeywell MK Xxii Egpws Installation Manual Table of Contents Honeywell MK VI MK Viii Egpws Installation Design Guide Honeywell MK VI MK Viii Egpws Installation Design Guide 104 Section V Certification 143 149158 160 Aircraft Application Data Section General Information Honeywell MK Xxii Egpws Installation Manual Section I General Information License Requirements Introduction How To Use This Docu mentApplicability Reference Documents Description of Equipm ent MK Xxii Egpws Comp uter MK Xxii Egpws Conf iguration ModuleGPS Antenna OAT Sensor Smart Cable Pcmcia Interface MK Xxii Egpws Smart Cable Technical Characteris tics Units Supplied Configuration ModuleMK Xxii Egpws Honeywell MK Xxii Egpws Installation Manual Installation and Acces sories Kits New Egpws installation with Internal GPS2 RS-232 Cable Smart Cable Terrain Database Card s Flight History Card Circuit Breaker GPS Antenna & cableAnnunciators & Switc h/Annunciators Cockpit Speaker Opti onal Tools Required Crimping Tool P1, P 2, P3 Contact Positioner P 1, P2, P3Insertion/Removal Too l P1, P2, P3 Spare Contacts P1, P 2, P3 Honeywell MK Xxii Egpws Installation Manual Section Installation Honeywell MK Xxii Egpws Installation Manual Section II Installation Equipment Installation 2.3.1 General Unpacking and Inspec ting the Equipment MK Xxii Computer Loc ation MK Xxii Computer Ins tallation Configuration Module Location Configuration Module Installation Configuration Module Assembly Required Installation Assembly Sequence 1 MK Xxii Egpws Configuration Module 2 MK Xxii Egpws Configuration Module 3 MK Xxii Egpws Configuration Module 4 MK Xxii Egpws Configuration Module 5 MK Xxii Egpws Configuration Module 6 MK Xxii Egpws Configuration Module 7 MK Xxii Egpws Configuration Module GPS Antenna Installat ion OAT Sensor Installatio nCockpit Annunciators / Switches GPS Antenna location Description Egpws cautionGPWS G/S Cancld Location Gpws warning red & Gpws alert amber 8 MK Xxii Egpws Annunciators/Switches Location Inhibit Switch Functio ns and Selection Low Altitude ModeTerrain Inhibit Audio Inhibit Timed MK Xxii Egpws Outline MK Xxii Egpws Mounting Tray Honeywell P/N 405-0383-001 Honeywell MK Xxii Egpws Installation Manual Section System Planning Honeywell MK Xxii Egpws Installation Manual Section III System Planning Category 8 Radio Altitude Input Select Category 14 Audio Output Level Primary Power Input System Wiring/ Electr ical InterfacesChassis Ground Discrete Inputs Analog and Digital Inp utsSerial Outputs Audio Output Discrete Outputs Configurable Interface s Category 1 Aircraft / Mode Type SelectAircraft / Mode Type Instructions Category 2 Air Data Input Select Examples Analog altitude and 500 ohm OAT Egpws MK Digital Arinc 429 Cat ID 5, 1 Digital -ARINC 575 Cat ID Arinc Shadin 2000 Cat ID Digital Arinc 429 Dual IOC Buses Cat . ID Category 3 Position Input Select Arinc 743 Format Examples Arinc 429 BUS Cat ID 0,1,4,5 3.2 RS-232 Transmit-Receive, 9600 baud Cat ID Dual Arinc 429 BUS Cat ID Category 4 Altitude Callouts Category 5 Audio Menu Select Category 6 Terrain Display Select TAD Selection Terrain Display Configuration Group Type of sweep used for terrain data fan, standard, etc 6-1 Single Tube Wx/Terrain Display Output 429 Bus Group Display Input Control GroupExample Egpws TRA-45A J101 Egpws Avidyne FSD Honeywell Radar Indicator Honeywell WRX R/T Avtech DSU Arinc 429 Range #1 Arinc 429 Range #2 Kcpb Video #1 Out Steep Approach Not Available in the Mk Category 7 Options Select Group #17.3 TA&D Alternate Pop-up Obstacle Awareness Peaks ModeBank Angle Callout Enabling WOW Reversal GPS Altitude Reference Category 8 Radio Altitude Input Select Example Digital Radio Altitude Interface DH Discrete Gnd Valid Radio Altimeter Indicator Analog Radio Altitude Interface Category 9 Navigation Inputs Select Example Analog Glideslope Interface cat ID 0,1,5 RNA-34A Digital Glideslope/Localizer Interface Dual Glideslope Receiver Attitude Signals Category 10 Attitude Input Select Example Analog Roll Angle Synchro Vertical Gyro Digital Arinc 429 High Speed Ahrs Category 11 Heading Input Select Magnetic Heading Example Analog Heading Synchro CAT ID Directional Gyro Heading High Speed Category 12 Windshear Input Select Instruction Category 13 Input / Output Discrete Type Select Input/Output Discretes Audio Inhibit Discrete Weight on Wheels WOW DiscreteLanding Gear Discrete Mode 6 Low Volume Discrete Glideslope Cancel DiscreteAutopilot Engaged Discrete Self Test Discrete Terrain Awareness InhibitGlideslope Inhibit Discrete Low Altitude Mode Select Discrete Timed Audio Inhibit DiscreteOutput Discretes Lamp Format Gpws Inop Discrete TAD Inop DiscreteGpws Warning Discrete Gpws Alert Discrete Low Altitude Mode Discrete Terrain Display Select #1 & #2 Discrete REV C Sheet Category 14 Audio Output Level Ohm Category 15, Autorotation Threshold Autorotation Threshold 107 108 Harness Checkout and Power Check Unit InstallationEgpwc Initialization a nd Configuration 1 RS-232 Communicatio n with the MK Xxii Egpws Egpwc Front Panel T est Connector WinVIEWS Configuration Module Programming WinVIEWS Operation 112 CUW and CMR Comm ands CFG CUW 0/15 128 3 2 134 128 3 29 1 0 2 0 0 129 0 Configuration Module Reprogramming CATspacecategory #spaceID#spaceT or FEnter Regional Terrain Data base Loading 4.6.1 Effectivity Approval Material Cost and Av ailability Accomplishment Instr uctions Verification of the Ter rain Database Version END of Test 120 Section Certification Honeywell MK Xxii Egpws Installation Manual Section V Certification Certification Procedur e Equipment Compatibi lity Equipment LocationFAA Requirements Ground Test Failure Modes, Effects , and Safety Analysis Flight TestPilots Guide Existing STC’s Honeywell MK Xxii Egpws Installation Manual Appendix a Customer Worksheet Honeywell MK Xxii Egpws Installation Manual MK Xxii Egpws Cockpit Displays GPS Discrete Inputs Parameter Generic Model Information System REV C Sheet REV C Sheet REV C Sheet REV C Sheet REV C Sheet Appendix B Sample Wiring Diagrams DWG no 060-4314-225 Revc Sheet Honeywell MK Xxii Egpws Installation Manual Honeywell MK Xxii Egpws Installation Manual Appendix C Honeywell MK Xxii Egpws Installation Manual RS-232 Communication with the Egpws Baud, No Parity, 8 bits, and 1 stop bit REV C Sheet REV C Sheet Honeywell MK Xxii Installation Manual Appendix D Vendor Drawings Honeywell MK Xxii Egpws Installation Manual Vendor Contact Information AMP For orders and AOG requirements, contact D1-1 Edmo GPS RF Cable Sets D1-2 Emteq Per 100 ft Inches Bend Radius Minimum 1 Connectors for Tflx cable series GPS 1 Connectors for Pflx cable series GPS Tool Frame and Die Part Numbers Installation Considerations Aerospace Optics Inc D1-3 Aerospace Optics Mail switches@vivisun.com StacoSwitch Honeywell MK Xxii Egpws Installation Manual Appendix E Interface Description Document Honeywell MK Xxii Egpws Installation Manual Connector Interface Purpose Introduction Part NumberSystem Overview Signal Interfaces Primary Power InputElectrical Interface Introduction Chassis Ground DC Analog Inputs Radio AltitudeLOW Level Glideslope Localizer Deviation or LOW Level Glideslope Validity Outside AIR Temperature Configuration Defined DC Inputs2.4 Barometric Altitude AC Analog Inputs 2.7.1Synchro Roll Attitude 2.7.2 Configuration Defined Synchro Inputs Signal Timing Reference Inputs 2.9 Arinc 429/575 Digital Serial BUS Inputs GPS RS-232 Digital Serial BUS Serial Port 2.9.1 RS-232 / RS-422 Digital Serial BUS InputsGPS RS-422 Digital Serial BUS Serial Port +28 VDC Discrete Characteristics AIR Data RS-232 Digital Serial BUS Serial PortAIR Data RS-422 Digital Serial BUS Serial Port SCI Range RS-422 Digital Serial BUS Serial Port Ground Discrete Characteristics Configuration Module InterfaceGPS Antenna Input Monitor Output Characteristics Discrete Output CharacteristicsOAT Voltage Reference Output Lamp Driver Outputs High Level Speaker Audio Output LOW Level Interphone Audio OutputArinc Digital Serial Output Busses Arinc 429 Output BUS Arinc 453 Output BUS 2.18.1 RS-232 Maintenance Port Serial PortFront Panel Test Interface Pcmcia / Smartcable Port Front Panel Status IndicatorsGSE Present Discrete Input Configuration Selection Configuration TypesAircraft Application Data Table E 3 Category ID Selection Procedure Signal SelectionInstruction Configuration Selection Tables Category 1, Aircraft / Mode Type Select Torque Type Table E Effectivity App Cfg Fault Designation Engine 2 BUS Bus Type Basic Fault Designation Engine 1 BUS Bus Type BasicEngine Torque Data Selection Fault Designation Engine 1 BUS Bus Type RS-422 9600 baud Fault Designation Engine 2 BUS Bus Type RS-422 9600 baud Torque Data Select 8 AS365 Dauphin N3 Torque Data Select 9 BellTorque Data Select 10 Bell Summary Data Torque Data Select 11 Bell 212/412 Summary Data Fault Designation Engine 1 BUS Torque Data Select 14 Coast Guard HH-65 Summary DataTorque Data Select 16 Common DC Torque Connection Summary Data Table E Description Category 2, AIR Data Input SelectTable E 3.1.2 AIR Data Input Select for Egpws Mkxxii Fault Designation AIR Data BUS Bus Type Basic Configuration DataType Summary Data Table E 3.1.2-3 AIR Data Input Select #3 Summary Data Table E 3.1.2-5 AIR Data Input Select #5 Table E 3.1.2-4 AIR Data Input Select #4 Summary DataConnect to Channel Channel 429RX2 Table E 3.1.2-6 AIR Data Input Select #6Channel Connect to Table E 3.1.2-10 AIR Data Input Select #10 Table E 3.1.2-11 AIR Data Input Select #11 Summary Data Category 3, Position Input Select 3.3Position Input Type TableE Description Fault Designation GPS BUS Bus Type Basic UTC Fault Designation Internal GPS Bus Type Basic Internal Fault Designation GPS BUS Bus Type Basic App Cfg Category 4, Altitude CalloutsTable E 3.1.4 Altitude Callouts for Egpws Mkxxii Honeywell MK Xxii Egpws Installation Manual Category 5, Audio Menu Select Effectivity App Cfg 006Table E 3.1.5 Audio Menu Type Table E 3.1.5-128 Audio Menu Type 128 Basic Helicopter IDand TCF Disable Application Notes Category 6, Terrain Display SelectSection Overview Defined By Honeywell MK Xxii Egpws Installation Manual Table E KC Picture Bus Table Table E 3.1.6-2 TA&D / TCF Disabled Table Table E 3.1.6-1 No Display TAD and TCF EnabledChannel Fault Designation Display BUS Bus Type Basic Display Configuration Group 6 Collins PRO-LINE IITable Table E 3.1.6-3 Collins ProLine II Integration note Display Configuration Group 1 Bendix RDR 4A/B PPI with MOD Table Table E 3.1.6-4 Bendix PPI-4A/4B Display Configuration Group 2 Collins Proline II Table E Collins ProLine II Display Configuration Group 3 Collins Proline II, 5X4 Table E Collins ProLine II 5x4,5x5 Display Configuration Group 7 NON-INTEGRATED Efis 40/50 Table E Non-Integrated Efis 40/50 Honeywell/Bendix Display Configuration Group 8 Integrated Efis 40/50 Peaks Always EnabledTable E 3.1.6-10 Integrated Efis 40/50 Honeywell/Bendix Honeywell MK Xxii Egpws Installation Manual Table E 3.1.6-12 Collins WXI-701/711, without Auto Range Integration note Pins Terrain Display BUS #1 453TX1Terrain Display BUS #2 Reference Name Table E 3.1.6-14 Bendix PPI-4A/4B without Auto Range Terrain Display BUS #2 453TX2 Reference Name PIN Function 6.2-3 Display Input Control Group6.3-0OUTPUT 429 BUS Group Traceability Table E 3.1.6-16 Bendix IN182A/IN812A Radar display RDR Reference section Pins Comments Output 429 Bus Group Table E Bendix IN842A/IN862A Radar display RDR Function ValueCategory 7, Options Select Group #1 TA&D Alternate Pop Up False TA&D Alternate Pop Up True Display Input Control Group Display Input Control Group Honeywell Fault Designation IOC BUS Table E3.1.6-236 Display Configuration Collins ProLine IV Honeywell Channel 429RX8 Table E 3.1.6-246 Non-Integrated Efis 10 Bendix/Honeywell Channel 422RX2 Connect to DC811 #1 Display Input Control GroupConnect to DC811 #2 Honeywell MK Xxii Egpws Installation Manual SCI Bus RS-422 12K baud Altitude Reference6 Effectivity App Cfg Category 7, Options 1 SelectTable E 317 Options Select Group #1 True False WGS-84 Radio Altitude Type Table E Description Category 8, Radio Altitude Input SelectDescription Value PIN Function Connection PIN Type Channel Designation Reference Table E 3.1.8-5 Radio Altitude Input Select Type 5 ALT Reference Summary Data Category 9, Navigation Input Select Table E 3.1.9 Navigation Input Select for Egpws MkxxiiTable E 3.1.9-0 Navigation Inputs Select Summary Data Connection PIN Type Fault Designation ILS BUS Bus T ype Basic Fault Designation ILS BUS Category 10, Attitude Input Select Attitude Input SelectTable E 3.1.10 Attitude Input Select for Egpws MK Table E 3.1.10-0 Attitude Input Select Type Table E 3.1.10-4 Attitude Input Select Type Fault Designation Ahrs BUSTable E 3.1.10-128 Attitude Input Select Type Connect to Fault Designation Ahrs BUS Bus Type Basic Category 11, Heading Input SelectHeading Input Select Table E Description Table E 3.1.11 Heading Input Select for Egpws MK Category 12, Windshear Input Select No WindshearEffectivity App Cfg 003 Table E 3.1.12 Windshear Input Select Category 13, Input / Output Discrete Type Select Input/Output Discrete Type Table E State Configuration Data Possible StatesTable E 3.1.13-128 INPUT/OUTPUT Discrete Type Table E 3.1.13-129 INPUT/OUTPUT Discrete Type Category 14, Audio Output Level Volume SelectTable E 3.1.14 Audio Output Level Autorotation Threshold Torque Category 15, Autorotation ThresholdTable E 3.1.15 Autorotation Threshold for Egpws MK SYN1X SYN1Z SYN2Z Connector Pin Refer to Category 13 where multiple uses are possible Honeywell MK Xxii Egpws Installation Manual Figure E 4.1, Connector Pin References J1, J2, J3 AcronymInterpretation Definitions Acronym Interpretation Pcmcia