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
160
143
149
158
Aircraft Application Data
Section General Information
Honeywell MK Xxii Egpws Installation Manual
Section I General Information
License Requirements
Introduction
How To Use This Docu ment
Applicability
Reference Documents
Description of Equipm ent
OAT Sensor
MK Xxii Egpws Comp uter
MK Xxii Egpws Conf iguration Module
GPS Antenna
Smart Cable Pcmcia Interface
Technical Characteris tics
MK Xxii Egpws Smart Cable
Units Supplied
Configuration Module
MK Xxii Egpws
Honeywell MK Xxii Egpws Installation Manual
Smart Cable
Installation and Acces sories Kits
New Egpws installation with Internal GPS
2 RS-232 Cable
Flight History Card
Terrain Database Card s
Circuit Breaker
GPS Antenna & cable
Annunciators & Switc h/Annunciators
Cockpit Speaker Opti onal
Spare Contacts P1, P 2, P3
Tools Required Crimping Tool P1, P 2, P3
Contact Positioner P 1, P2, P3
Insertion/Removal Too l P1, P2, P3
Honeywell MK Xxii Egpws Installation Manual
Section Installation
Honeywell MK Xxii Egpws Installation Manual
Section II Installation
Unpacking and Inspec ting the Equipment
Equipment Installation 2.3.1 General
MK Xxii Computer Ins tallation
MK Xxii Computer Loc ation
Configuration Module Installation
Configuration Module Location
Required
Configuration Module Assembly
1 MK Xxii Egpws Configuration Module
Installation Assembly Sequence
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 location
GPS Antenna Installat ion
OAT Sensor Installatio n
Cockpit Annunciators / Switches
Egpws cautionGPWS G/S Cancld
Description
Gpws warning red & Gpws alert amber
Location
8 MK Xxii Egpws Annunciators/Switches Location
Audio Inhibit Timed
Inhibit Switch Functio ns and Selection
Low Altitude Mode
Terrain Inhibit
MK Xxii Egpws Outline
Honeywell P/N 405-0383-001
MK Xxii Egpws Mounting Tray
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 Interfaces
Chassis Ground
Discrete Inputs
Analog and Digital Inp uts
Serial Outputs
Discrete Outputs
Audio Output
Instructions
Configurable Interface s
Category 1 Aircraft / Mode Type Select
Aircraft / Mode Type
Category 2 Air Data Input Select
Egpws MK
Examples Analog altitude and 500 ohm OAT
Digital Arinc 429 Cat ID 5, 1
Arinc
Digital -ARINC 575 Cat ID
Shadin 2000 Cat ID
Digital Arinc 429 Dual IOC Buses Cat . ID
Arinc 743 Format
Category 3 Position Input Select
3.2 RS-232 Transmit-Receive, 9600 baud Cat ID
Examples Arinc 429 BUS Cat ID 0,1,4,5
Dual Arinc 429 BUS Cat ID
Category 4 Altitude Callouts
Category 5 Audio Menu Select
TAD Selection
Category 6 Terrain Display Select
Type of sweep used for terrain data fan, standard, etc
Terrain Display Configuration Group
6-1 Single Tube Wx/Terrain Display
Output 429 Bus Group
Display Input Control Group
Example
TRA-45A
Egpws
J101
Egpws Avidyne FSD
Honeywell WRX R/T
Honeywell Radar Indicator
Arinc 429 Range #1 Arinc 429 Range #2 Kcpb Video #1 Out
Avtech DSU
Steep Approach Not Available in the Mk
Category 7 Options Select Group #1
7.3 TA&D Alternate Pop-up
Obstacle Awareness
Peaks Mode
Bank Angle Callout Enabling
GPS Altitude Reference
WOW Reversal
Example Digital Radio Altitude Interface
Category 8 Radio Altitude Input Select
Analog Radio Altitude Interface
DH Discrete Gnd Valid Radio Altimeter Indicator
Category 9 Navigation Inputs Select
RNA-34A
Example Analog Glideslope Interface cat ID 0,1,5
Dual Glideslope Receiver
Digital Glideslope/Localizer Interface
Category 10 Attitude Input Select
Attitude Signals
Vertical Gyro
Example Analog Roll Angle Synchro
Ahrs
Digital Arinc 429 High Speed
Magnetic Heading
Category 11 Heading Input Select
Directional Gyro
Example Analog Heading Synchro CAT ID
Heading High Speed
Instruction
Category 12 Windshear Input Select
Input/Output Discretes
Category 13 Input / Output Discrete Type Select
Audio Inhibit Discrete
Weight on Wheels WOW Discrete
Landing Gear Discrete
Mode 6 Low Volume Discrete
Glideslope Cancel Discrete
Autopilot Engaged Discrete
Self Test Discrete
Terrain Awareness Inhibit
Glideslope Inhibit Discrete
Lamp Format
Low Altitude Mode Select Discrete
Timed Audio Inhibit Discrete
Output Discretes
Gpws Alert Discrete
Gpws Inop Discrete
TAD Inop Discrete
Gpws Warning Discrete
Terrain Display Select #1 & #2 Discrete
Low Altitude Mode Discrete
REV C Sheet
Ohm
Category 14 Audio Output Level
Category 15, Autorotation Threshold
Autorotation Threshold
107
108
1 RS-232 Communicatio n with the MK Xxii Egpws
Harness Checkout and Power Check
Unit Installation
Egpwc Initialization a nd Configuration
WinVIEWS
Egpwc Front Panel T est Connector
WinVIEWS Operation
Configuration Module Programming
112
CFG CUW 0/15 128 3 2 134 128 3 29 1 0 2 0 0 129 0
CUW and CMR Comm ands
CATspacecategory #spaceID#spaceT or FEnter
Configuration Module Reprogramming
Approval
Regional Terrain Data base Loading 4.6.1 Effectivity
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
Ground Test
Certification Procedur e Equipment Compatibi lity
Equipment Location
FAA Requirements
Existing STC’s
Failure Modes, Effects , and Safety Analysis
Flight Test
Pilots Guide
Honeywell MK Xxii Egpws Installation Manual
Appendix a Customer Worksheet
Honeywell MK Xxii Egpws Installation Manual
Cockpit Displays
MK Xxii Egpws
GPS
Parameter
Discrete Inputs
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
Baud, No Parity, 8 bits, and 1 stop bit
RS-232 Communication with the Egpws
REV C Sheet
REV C Sheet
Honeywell MK Xxii Installation Manual
Appendix D Vendor Drawings
Honeywell MK Xxii Egpws Installation Manual
AMP
Vendor Contact Information
For orders and AOG requirements, contact
D1-1 Edmo
D1-2 Emteq
GPS RF Cable Sets
Inches Bend Radius Minimum
Per 100 ft
1 Connectors for Tflx cable series GPS
1 Connectors for Pflx cable series GPS
Tool Frame and Die Part Numbers
Installation Considerations
D1-3 Aerospace Optics
Aerospace Optics Inc
Mail switches@vivisun.com
StacoSwitch
Appendix E Interface Description Document
Honeywell MK Xxii Egpws Installation Manual
Honeywell MK Xxii Egpws Installation Manual
Connector Interface
Purpose
Introduction Part Number
System Overview
Chassis Ground
Signal Interfaces
Primary Power Input
Electrical Interface Introduction
Localizer Deviation or LOW Level Glideslope Validity
DC Analog Inputs
Radio Altitude
LOW Level Glideslope
Barometric Altitude
Outside AIR Temperature
Configuration Defined DC Inputs
2.4
2.7.2
AC Analog Inputs
2.7.1
Synchro Roll Attitude
Signal Timing Reference Inputs
Configuration Defined Synchro Inputs
Arinc 429/575 Digital Serial BUS Inputs
2.9
GPS RS-232 Digital Serial BUS Serial Port
2.9.1 RS-232 / RS-422 Digital Serial BUS Inputs
GPS RS-422 Digital Serial BUS Serial Port
SCI Range RS-422 Digital Serial BUS Serial Port
+28 VDC Discrete Characteristics
AIR Data RS-232 Digital Serial BUS Serial Port
AIR Data RS-422 Digital Serial BUS Serial Port
Ground Discrete Characteristics
Configuration Module Interface
GPS Antenna Input
Lamp Driver Outputs
Monitor Output Characteristics
Discrete Output Characteristics
OAT Voltage Reference Output
Arinc 429 Output BUS
High Level Speaker Audio Output
LOW Level Interphone Audio Output
Arinc Digital Serial Output Busses
Arinc 453 Output BUS
2.18.1 RS-232 Maintenance Port Serial Port
Front Panel Test Interface
Pcmcia / Smartcable Port
Front Panel Status Indicators
GSE Present Discrete Input
Configuration Selection
Configuration Types
Aircraft Application Data
Table E 3 Category ID Selection Procedure
Signal Selection
Instruction
Configuration Selection Tables
Category 1, Aircraft / Mode Type Select
Effectivity App Cfg
Torque Type Table E
Fault Designation Engine 2 BUS Bus Type Basic
Fault Designation Engine 1 BUS Bus Type Basic
Engine Torque Data Selection
Fault Designation Engine 2 BUS Bus Type RS-422 9600 baud
Fault Designation Engine 1 BUS Bus Type RS-422 9600 baud
Torque Data Select 11 Bell 212/412 Summary Data
Torque Data Select 8 AS365 Dauphin N3
Torque Data Select 9 Bell
Torque Data Select 10 Bell Summary Data
Connection Summary Data
Fault Designation Engine 1 BUS
Torque Data Select 14 Coast Guard HH-65 Summary Data
Torque Data Select 16 Common DC Torque
Table E Description
Category 2, AIR Data Input Select
Table E 3.1.2 AIR Data Input Select for Egpws Mkxxii
Fault Designation AIR Data BUS Bus Type Basic
Configuration Data
Type 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 Data
Connect to Channel
Table E 3.1.2-10 AIR Data Input Select #10
Channel 429RX2
Table E 3.1.2-6 AIR Data Input Select #6
Channel Connect to
Table E 3.1.2-11 AIR Data Input Select #11 Summary Data
Category 3, Position Input Select
3.3
Position Input Type TableE Description
UTC
Fault Designation GPS BUS Bus Type Basic
Internal
Fault Designation Internal GPS Bus Type Basic
Bus Type Basic
Fault Designation GPS BUS
App Cfg
Category 4, Altitude Callouts
Table E 3.1.4 Altitude Callouts for Egpws Mkxxii
Honeywell MK Xxii Egpws Installation Manual
Table E 3.1.5-128 Audio Menu Type 128 Basic Helicopter
Category 5, Audio Menu Select
Effectivity App Cfg 006
Table E 3.1.5 Audio Menu Type
Defined By
IDand TCF Disable Application Notes
Category 6, Terrain Display Select
Section Overview
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 Enabled
Channel
Integration note
Fault Designation Display BUS Bus Type Basic
Display Configuration Group 6 Collins PRO-LINE II
Table Table E 3.1.6-3 Collins ProLine II
Table Table E 3.1.6-4 Bendix PPI-4A/4B
Display Configuration Group 1 Bendix RDR 4A/B PPI with MOD
Table E Collins ProLine II
Display Configuration Group 2 Collins Proline II
Table E Collins ProLine II 5x4,5x5
Display Configuration Group 3 Collins Proline II, 5X4
Table E Non-Integrated Efis 40/50 Honeywell/Bendix
Display Configuration Group 7 NON-INTEGRATED Efis 40/50
Display Configuration Group 8 Integrated Efis 40/50
Peaks Always Enabled
Table 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
Reference Name
Integration note Pins
Terrain Display BUS #1 453TX1
Terrain Display BUS #2
Terrain Display BUS #2 453TX2
Table E 3.1.6-14 Bendix PPI-4A/4B without Auto Range
Reference Name PIN Function
6.2-3 Display Input Control Group
6.3-0OUTPUT 429 BUS Group Traceability
Reference section
Table E 3.1.6-16 Bendix IN182A/IN812A Radar display RDR
Output 429 Bus Group
Pins Comments
TA&D Alternate Pop Up False TA&D Alternate Pop Up True
Table E Bendix IN842A/IN862A Radar display RDR
Function Value
Category 7, Options Select Group #1
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 Group
Connect to DC811 #2
Honeywell MK Xxii Egpws Installation Manual
SCI Bus RS-422 12K baud
Altitude Reference6 Effectivity App Cfg
Category 7, Options 1 Select
Table E 317 Options Select Group #1
True False WGS-84
Radio Altitude Type Table E Description
Category 8, Radio Altitude Input Select
Description Value
PIN Type Channel Designation Reference
PIN Function Connection
Reference Summary Data
Table E 3.1.8-5 Radio Altitude Input Select Type 5 ALT
Connection PIN Type
Category 9, Navigation Input Select
Table E 3.1.9 Navigation Input Select for Egpws Mkxxii
Table E 3.1.9-0 Navigation Inputs Select Summary Data
Fault Designation ILS BUS
Fault Designation ILS BUS Bus T ype Basic
Table E 3.1.10-0 Attitude Input Select Type
Category 10, Attitude Input Select
Attitude Input Select
Table E 3.1.10 Attitude Input Select for Egpws MK
Table E 3.1.10-4 Attitude Input Select Type
Fault Designation Ahrs BUS
Table E 3.1.10-128 Attitude Input Select Type Connect to
Table E 3.1.11 Heading Input Select for Egpws MK
Fault Designation Ahrs BUS Bus Type Basic
Category 11, Heading Input Select
Heading Input Select Table E Description
Table E 3.1.12 Windshear Input Select
Category 12, Windshear Input Select
No Windshear
Effectivity App Cfg 003
Input/Output Discrete Type Table E
Category 13, Input / Output Discrete Type Select
State
Configuration Data Possible States
Table 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 Select
Table E 3.1.14 Audio Output Level
Autorotation Threshold Torque
Category 15, Autorotation Threshold
Table 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
Definitions
AcronymInterpretation
Acronym Interpretation
Pcmcia