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REVISION STATUS OF SHEETS INDEX
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TABLE OF CONTENTS
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SECTION I GENERAL INFORMATION
1.1 Introduction
1.2 Applicability
1.3 How To Use This Document
1.4 Reference Doc uments
1.5 Description o f Equipment
1.5.1 MK VI EGPWS Computer
1.5.2 MK VIII EGPWS Computer
1.5.3 MK VI/MK VII I EGPWS Configuration Module
1.5.4 GPS Antenn a and Cabling
1.5.5 OAT Sensor
1.5.6 Smart Cable (PCMCIA Interface)
FIGURE 1-1 MK VI/MK VIII EGPWS SMART CABLE
1.6 Technical Cha racteristics
1.7 Units Suppli ed 1.7.1 MK VI EGPWS
1.7.2 MK VIII EGPWS
1.7.3 Configuration Module
1.7.4 Smart Cable (PCMCIA Interface)
1.8 Installation K its and Accessories
1.8.1 MK VI/MK VII I EGPWS Installation Kits
1.8.2 RS-232 Cabl e
1.8.3 Smart Cable
1.8.4 Terrain Datab ase Cards
1.8.5 Flight History Card
1.9 Accessories not Supplied 1.9.1 ARINC 453 Te rrain Display wiring
1.9.2 GPS Antenna & Cable
1.9.3 Circuit Breake r
1.9.4 Annunciator s & Switch/Annunciators
1.9.5 Cockpit Spe akers
1.9.6 Temperature Probes
1.10 Tools Requi red 1.10.1 Crimping Too l - P1, P2, P3
1.10.2 Contact Posi tioner - P1, P2, P3
1.10.3 Insertion/Rem oval Tool - P1, P2, P3
1.10.4 Spare Conne ctors and Contacts - P1, P2, P3
1.11 License Req uirements
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SECTION II - INSTALLATION
2.1 Introduction
2.2 Unpacking a nd Inspecting the Equipment
2.3 Equipment I nstallation 2.3.1 General
CAUTION
2.3.3 MK VI/ MK VI II Computer Installation
2.3.4 Configuration Module Location
2.3.5 Configuration Module Installation
CONFIGURATION MODULE ASSEMBLY
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FIGURE 2.1-4 MK VI/MK VIII EGPWS CONFIGURATION MODULE
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2.3.6 GPS Antenn a location
2.3.7 GPS Antenn a Installation
2.3.8 OAT Sensor Location
2.3.9 OAT Sensor Installation
2.3.10 Cockpit Light s
2.3.10.1 Description
2.3.10.2 Location
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SECTION III SYSTEM PLANNING
3.1 Introduction
3.2 System Wirin g/ Electrical Interfaces
3.2.1 Primary Powe r Input
3.2.2 Chassis Grou nd
3.2.3 GPS Antenn a
3.2.4 Analog and D igital Inputs
3.2.5 Discrete Input s
3.2.6 Serial Output s
3.2.7 Audio Output
3.2.8 Discrete Outp uts
3.2.9 Configuration Module
3.3 Category 1 - Aircraft / Mode Type Select
3.3.1 Aircraft / Mod e Type
3.3.2 Mode 1 type
3.3.3 Mode 2 type
3.3.4 Mode 3 type
3.3.5 Mode 4 type
3.3.6 Bank Angle Type
3.3.7 Runway Leng th (MK VIII EGPWS only)
3.3.8 Instructions
3.4 Category 2 Air Data Input Select
3.4.1 Analog (Cat. 2 ID 0, 3, 4, 11, 12)
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3.4.2 Digital ARIN C 429 (Cat. 2 ID 5, 1, 6, 13)
3.4.3 Digital ARIN C 575 (Cat. 2 ID 2)
3.4.4 Shadin 2000 (Cat. 2 ID 10)
3.4.5 Digital ARIN C 429 Dual IOC Buses (Cat. 2. ID 255)
3.4.6 Instructions
3.5 Category 3 Position Input Select
3.5.1 ARINC 743 Fo rmat
3.5.2 GPS Altitude (Label 076) Reference
3.5.3 North-South East-West Velocity labels
3.5.4 ARINC 429 BU S (Cat. 3 ID 0,1,4,5,10-13)
25 8
A B
J2 ARINC 429 GPS ARINC 429 Bus - Hi ARINC 429 Bus -Lo
EGPWS MK VI / MK VIII A B
GND
NC
3.5.6 Dual ARINC 4 29 BUS (Cat. 3 ID 253 & 255)
3.5.7 Instructions
3.6 Category 4 Altitude Callouts
3.7 Category 5 Audio Menu Select
3.7.1 Audio Menu S election
3.7.2 Instructions
3.8 Category 6 Terrain Display Select
3.8.1 TAD & TCF Selection
3.8.2 Terrain Displ ay Configuration Group
3.8.3 Display Input Control Group
Display Input Control Group
3.8.4 Output 429 B us Group
Output 429 Bus Group
3.8.5 Instructions
3.8.6 Sample Displ ay Schematics
Honeywell GNS-XLS
J101
No connection
EGPWS GNS-XLS
J1
Honeywell KMD 540/
550/850
EGPWS
J3001
J1
Honeywell Grimes
TRA-45A
EGPWS TRA-45A
TRA-45A
AVTECH DSU Primus WXR UDI
EGPWS
AVTECH DSU
Integrated Primus 440/660/880
EGPWS
Honeywell Radar Indicator
Honeywell WRX R/T
Honeywell Primus
1000
Display Unit DU-870
Integrated Avionics
EGPWS Integrated Avionics
Honeywell / Bendix RDR 2000 / IN182A
J1
EGPWS
J2
Honeywell Radar Indicator
Honeywell / Bendix
PPI-4B
Honeywell WRX R/T
EGPWS
J1
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Rockwell Collins
Collins WXI-701
Collins WRX R/T
WXI-701/711
EGPWS
Collins ProLine II with WXP-840/850
Collins Wx Pnl
J2
EGPWS
WXP-840/850
HONEYWELL MK VI-VIII EGPWS 965-1XXX-0XX
#1 - IOC (ICC-4000)
PROLINE 4 INTERFACE MK VI-VIII EGPWS Category 6, ID 5 or 6
#1 - MFD
#1 - WXR
SG-802/803 CAT. 6: ID 243
DC-811
CAT 6: ID 244
SG-806
Radar R/T MK VIII EGPWS
SG-806
Universal MFD-640
J2
EGPWS MFD-640
P1
3.9 Category 7 Options Select Group #1
3.9.1 Steep Appro ach
3.9.2 TA&D Altern ate Pop-up
3.9.3 Peaks Mode
3.9.4 Obstacle Awa reness
3.9.5 Bank Angle Callout Enabling
3.9.6 Flap Reversal
3.9.7 GPS Altitude Reference
3.9.8 Instructions
3.10 Category 8 Radio Altitude Input Select
3.10.1 Radio Altitude Input
3.10.2 Decision Hei ght Discrete Input
3.10.3 Digital Radio Altitude Interface (Cat. 8 ID 2)
J2
3.10.4 Analog Radi o Altitude Interface (Cat. 8 ID 0,1,3,4)
Radio Altimeter R/T
EGPWS MK VI / MK VIII
Radio Altimeter Indicator
3.10.5 Digital ARIN C 429 Dual IOC Buses (Cat. 8 ID 251- 255)
3.10.6 Instructions
3.11 Category 9 Navigation Inputs Select
3.11.1 Navigation In puts Select (Glideslope & Localizer Inputs)
3.11.2 Glideslope Va lidity
3.11.3 Localizer Val idity
3.11.4 ILS Tuned Dis crete Input #1 (+28V) and #2 (GND)
3.11.5 Analog Glides lope Interface (Cat. 9 ID 0,1,5)
ILS Receiver
GS Inhibit (BC) +28
LOC Val +28V
LOC Valid +28
3.11.6 Digital Glides lope / Localizer / ILS Select Interface (Cat. 9 ID 2,3,4)
ILS 429 Bus
EGPWS MK VI / MK VIII
3.11.7 Digital ARIN C 429 Dual IOC buses (Cat. 9 ID 250 - 255)
3.11.8 Instructions
3.12 Category 10 Attitude Input Select
3.12.1 Roll Angle
3.12.2 Analog Pitch & Roll Angle (Synchro) (Cat. 10 ID 0,2,4)
Vertical Gyro
EGPWS MK VI / MK VIII
3.12.3 Digital Pitch & Roll Angle (ARINC 429 High Speed) (Cat. 10 ID 5 & 6)
AHRS 429 Bus
EGPWS MK VI / MK VIII
3.12.4 Digital ARIN C 429 Dual IOC buses (Cat. 10 ID 253 & 255)
3.12.5 Instructions
3.13 Category 11 Heading Input Select
3.13.1 Magnetic Hea ding
3.13.2 Analog Head ing (Synchro) (Cat. 11 ID 0)
Directional Gyro
EGPWS MK VI / MK VIII
3.13.3 Digital ARIN C 429 AHRS Input (Cat. 11 ID 2 & 3)
3.13.4 Digital ARIN C 429 Dual IOC buses (Cat. 11 ID 254 & 255)
3.13.5 Instructions
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3.15 Category 13 Input / Output Discrete Type Select
3.15.1 Input Discret es
3.15.1.1 Glideslope In hibit Discrete
3.15.1.2 Landing Flaps Discrete
3.15.1.3 Audio Inhibit Discrete
3.15.1.4 Landing Gear Discrete
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3.15.1.5 Glideslope Ca ncel Discrete
3.15.1.6 Momentary F lap Override Discrete
3.15.1.7 Mode 6 Low V olume Discrete
3.15.1.8 Autopilot Eng aged Discrete
3.15.1.9 Terrain Awar eness and TCF Inhibit Discrete
3.15.1.10 Self Test Dis crete
3.15.1.11 Steep Appro ach Discrete #2
3.15.1.12 GPWS INHIBI T Discrete (alternate action)
3.15.2 Output Discre tes
3.15.2.1 Lamp Format
3.15.2.2 Flashing Lamp s
3.15.2.3 GPWS INOP D iscrete
3.15.2.4 TAD INOP Dis crete
3.15.2.5 GPWS Warni ng Discrete
3.15.2.6 GPWS Alert Discrete
3.15.2.7 Glideslope Ca nceld Discrete
3.15.2.8 Flap Override Discrete
3.15.2.9 Steep Approac h Discrete
3.15.2.10 Audio On Dis crete (TCAS/TAS Inhibit)
3.15.2.11 Terrain Displ ay Select #1 & #2 Discrete
3.15.2.12 Terrain Pop u p Discrete
Figure 3.15-3 Example of Terrain Display switch with relay
WXR System R/T
TERR ON
WXR/TERR Display
3.15.3 Instructions
3.16 Category 14 Audio Output Level
3.16.1 Instructions
8 ohm
3.17 Category 15 - 17 Undefined Input Selects
3.17.1 Undefined In put Select
3.17.2 Instructions
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SECTION IV CONFIGURATION MODULE PROGRAMMING AND REGIONAL TERRAIN DATABASE LOADING
SECTION IV Config Module Programming And Regional TDB Loading
4.1 Introduction
4.2 Harness Che ckout and Power Check
4.3 Unit Installati on
4.4 EGPWC Initi alization and Configuration
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4.4.3 WinVIEWS
4.4.4 WinVIEWS Op eration
4.5 Configuration Module Programming
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4.5.1 CUW and CMR Commands
4.5.2 Configuration Module Reprogramming
4.6 Terrain Datab ase Loading 4.6.1 Effectivity
4.6.2 Description
4.6.3 Approval
4.6.4 Material Cos t and Availability
4.6.5 Accomplishme nt Instructions
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4.6.6 Verification o f the Terrain Database Version
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SECTION V CERTIFICATION
5.2.7 Pilots Guide
5.2.8 Failure Modes , Effects, and Safety Analysis
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SECTION VI - MK VI GPWS to MK VI/VIII EGPWS Signal Mapping
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NEW CONNECTOR
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MK VI / MK VIII EGPWS
ENHANCED GROUND PROXIMITY WARNING SYSTEM
CUSTOMER INTERFACE WORK SHEET
CURRENT GPWS INSTALLATION:
COCKPIT DISPLAYS:
AIRCRAFT SYSTEMS INFORMATION: (Use N/A if Not Applicable)
DISCRETE INPUTS:
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APPENDIX C WinVIEWS Operation Instructions
RS-232 COMMUNICATION WITH THE EGPWS
19200 Baud, No Parity, 8 bits, and 1 stop bit.
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APPENDIX D - Vendor Contact Information Vendor Contact Information
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Table of Contents
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APPENDIX E - Interface Description Document 1 INTRODUCTION 1.1 Part Number
1.2 Purpose
1.3 System Overview
1.4 Document Overview
2 REFERENCES
3 MECHANICAL INTERFACE 3.1 Weight
3.2 System Interface Components
3.2.1 EGPWC Mounting
3.2.2 EGPWC Connectors
3.2.3 Configuration Module
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4 ELECTRICAL INTERFACE 4.1 Introduction
4.2 Signal Interfaces
4.2.1 Grounds 4.2.1.1 Chassis Ground
4.2.1.2 DC Ground
4.2.2 Primary Power Input
4.2.3 DC Analog Inputs
4.2.3.1 Radio Altitude
4.2.3.2 Low Level Glideslope
4.2.3.3 Localizer Deviation or Low Level Glideslope Validity
4.2.3.4 Barometric Altitude
4.2.3.5 Outside Air Temperature
4.2.3.6 Configuration Defined DC Inputs
4.2.4 AC Analog Inputs
4.2.4.1 Synchro Roll Attitude
4.2.4.2 Synchro Magnetic Heading
4.2.4.3 Synchro Pitch Attitude
4.2.4.4 Configuration Defined Synchro Inputs
4.2.4.5 Signal Timing Reference Inputs
4.2.5 ARINC 429/575 Digital Serial Bus Inputs
4.2.6 RS-232 / RS-422 Digital Serial Bus Inputs
4.2.6.1 GPS RS-232 Digital Serial Bus (serial port 3)
4.2.6.2 GPS RS-422 Digital Serial Bus (serial port 3)
4.2.6.3 Air Data RS-232 Digital Serial Bus (serial port 2)
4.2.6.4 Air Data RS-422 Digital Serial Bus (serial port 2)
4.2.6.5 SCI Range RS-422 Digital Serial Bus (serial port 1)
4.2.7 Discrete Inputs
4.2.8 Configuration Module Interface
4.2.9 GPS Antenna Input
4.2.10 OAT Voltage Reference Output
4.2.11 Lamp Driver Outputs
4.2.11.1 Monitor Output Characteristics
4.2.11.2 Discrete Output Characteristics
4.2.12 Audio Outputs
4.2.12.2 Low Level (Interphone) Audio Output
4.2.13 ARINC Digital Serial Output Buses 4.2.13.1 ARINC 429 Output Bus
4.2.13.2 ARINC 453 Output Bus
4.3 Front Panel Test Interface
4.3.1 RS-232 Maintenance Port (serial port 4)
4.3.2 PCMCIA / SmartCable Port
4.3.3 GSE Present Discrete Input
4.4 Front Panel Status Indicators
5 AIRCRAFT APPLICATION DATA
5.1 Configuration Types
5.2 Configuration Selection
CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 175
Table 5.2: Category ID Selection Procedure
1
12
11
10
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5.3 Configuration Selection Tables
5.3.1 Category 1, Aircraft / Mode Type Select
Table 5.3.1: Aircraft / Mode Type Select
5.3.2 Category 2, Air Data Input Select
TABLE 5.3.2: AIR DATA INPUT SELECT
TABLE 5.3.2-0: AIR DATA INPUT SELECT #0
Uncorrected Barometric Altitude. Baro Rate is not available with this air data source.
TABLE 5.3.2-1: AIR DATA INPUT SELECT #1
TABLE 5.3.2-2: AIR DATA INPUT SELECT #2
TABLE 5.3.2-3: AIR DATA INPUT SELECT #3
Uncorrected Barometric Altitude. Baro Rate is not available with this air data source.
TABLE 5.3.2-4: AIR DATA INPUT SELECT #4
Uncorrected Barometric Altitude. Baro Rate is not available with this air data source.
TABLE 5.3.2-5: AIR DATA INPUT SELECT #5
TABLE 5.3.2-6: AIR DATA INPUT SELECT #6
TABLE 5.3.2-10: AIR DATA INPUT SELECT #10
TABLE 5.3.2-11: AIR DATA INPUT SELECT #11
TABLE 5.3.2-12: AIR DATA INPUT SELECT #12
TABLE 5.3.2-13: AIR DATA INPUT SELECT #13
TABLE 5.3.2-255: AIR DATA INPUT SELECT #255
5.3.3 Category 3, Position Input Select
Table 5.3.3: Position Input Select
Table 5.3.3-0: Position Input Type 0 (Low Speed ARINC 743A GPS)
Table 5.3.3-1: Position Input Type 1 (Low Speed ARINC 743 GPS)
Table 5.3.3-2: Position Input Type 2 (Internal GPS)
Table 5.3.3-3: Position Input Type 3 (RS232 GPS, PXpress format)
Table 5.3.3-4: Position Input Type 4 (High Speed ARINC 743A GPS)
Table 5.3.3-5: Position Input Type 5 (High Speed ARINC 743 GPS)
Table 5.3.3-10: Position Input Type 10 (Low Speed ARINC 743A GPS, no N/S-E/W Velocities)
Table 5.3.3-11: Position Input Type 11 (Low Speed ARINC 743 GPS, no N/S-E/W Velocities)
Table 5.3.3-12: Position Input Type 12 (High Speed ARINC 743A GPS, no N/S-E/W Velocities)
Table 5.3.3-13: Position Input Type 13 (High Speed ARINC 743 GPS, no N/S-E/W Velocities)
Table 5.3.3-253: Position Input Type 253 (Dual High Speed ARINC 743A GPS)
Table 5.3.3-255: Position Input Type 255 (Dual High Speed ARINC 743A GPS)
Fault Designation: GPS BUS 1
5.3.4 Category 4, Altitude Callouts
Table 5.3.4: Altitude Callouts
5.3.5 Category 5, Audio Menu Select
Table 5.3.5: Audio Menu Type
Table 5.3.5-0: Audio Menu Type 0 (Basic)
Table 5.3.5-1: Audio Menu Type 1 (Alternate)
Table 5.3.5-2: Audio Menu Type 2 (Basic for Fixed Gear Aircraft)
Table 5.3.5-3: Audio Menu Type 3 (Alternate for Fixed Gear Aircraft)
5.3.6 Category 6, Terrain Display Select
Table 5.3.6: Terrain Display Select
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Table 5.3.6.1-0 KC Picture Bus Display Configuration Group 0
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Table 5.3.6.1-3 Collins Pro-Line II, 4x4 Display Configuration Group 6
Table 5.3.6.1-4 Honeywell/Bendix PPI-4A/4B with Auto Range Display Configuration Group 1
2.
Table 5.3.6.1-5 Collins ProLine II, 5x6 Display Configuration Group 2
Table 5.3.6.1-6 Collins ProLine II, 5x4, 5x5 Display Configuration Group 3
Table 5.3.6.1-7 Honeywell/Bendix IN182A/IN812A (RDR 2000, RDS 81/82) Display Configuration Group 4
Table 5.3.6.1-8 Honeywell/Bendix IN842A/IN862A (RDR 2100, RDS 84/86) Display Configuration Group 5
Table 5.3.6.1-9 Honeywell/Bendix EFIS 40/50 (Non-Integrated) Display Configuration Group 7
CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 209
Table 5.3.6.1-10 Honeywell/Bendix EFIS 40/50 (Integrated) Display Configuration Group 8
Auto Pop Up Pop Up on Caution or Warning. Never Pop Up
5.3.7 Category 7, Options Select Group #1
Peaks Mode Peaks Always Enabled (See Note 1)
Channel Pins Comments
Table 5.3.6.1-11 Collins WXI-701/711 PPI, with Auto Range Display Configuration Group 9
1. 2.
Table 5.3.6.1-12 Collins WXI-701/711 PPI, without Auto Range Display Configuration Group 10
Display Input Control Group 3
Table 5.3.6.1-14 Honeywell/Bendix PPI-4A/4B without Auto Range Display Configuration Group 12
2.
Display Input Control Group 3
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Table 5.3.6.1-19 KC Picture Bus with Soft Keys Display Configuration Group 0
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Table 5.3.6.1-235 Collins ProLine 4 (Non-Integrated) Display Configuration Group 2
Display Input Control Group 244
Table 5.3.6.1-236 Collins ProLine 4 (Integrated) Display Configuration Group 241
Display Input Control Group 244
Table 5.3.6.1-237 Honeywell Primus 1000 with binary Peaks Elevations and Cyan ASCII window text
Display Configuration Group 242
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Display Configuration Group 247
Table 5.3.6.1-243 Honeywell EDZ802, EDZ603, EDZ803 (non-Integrated) with dual SCI range
Display Configuration Group 238
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Display Input Control Group 246
2.
3.
Table 5.3.6.1-248 Honeywell Primus 1000 MK VIII Only Display Configuration Group 248
2. 3.
Table 5.3.6.1-249 Honeywell Primus EPIC CDS/R, (Integrated) with overlay Peaks Elevations
Display Configuration Group 249
Display Input Control Group 250
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Display Input Control Group 250
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Table 5.3.6.1-252 Honeywell SPZ8000, EDZ605, EDZ805 and EDZ806, with ARINC 429 Range
Display Configuration Group 250
Display Input Control Group 252
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2.
3.
Table 5.3.6.1-254 Collins ProLine 21 (Integrated) MK VIII Only Display Configuration Group 254
1. 2.
3. 4.
Table 5.3.6.1-255 Honeywell SPZ8000 older style MK VIII Only Display Configuration Group 255
Display Input Control Group 255
5.3.7 Category 7, Options Select Group #1
Table 5.3.7: Options Select Group #1
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5.3.8 Category 8, Radio Altitude Input Select
Table 5.3.8: Radio Altitude Input Select
Table 5.3.8-0: Radio Altitude Input Select Type 0 (ARINC 552)
Table 5.3.8-1: Radio Altitude Input Select Type 1 (ALT 55)
Table 5.3.8-2: Radio Altitude Input Select Type 2 (ARINC 429)
Fault Designation: RADIO ALTIMETER BUS
Table 5.3.8-3: Radio Altitude Input Select Type 3 (RT-200/300)
Table 5.3.8-4: Radio Altitude Input Select Type 4 (KRA 405)
Table 5.3.8-251: Radio Altitude Input Select Type 251 (ARINC 429 via dual IOC buses with DH/MDA)
Table 5.3.8-252: Radio Altitude Input Select Type 252
Table 5.3.8-253: Radio Altitude Input Select Type 253
Table 5.3.8-254: Radio Altitude Input Select Type 254 (ARINC 429 via dual IOC buses)
Table 5.3.8-255: Radio Altitude Input Select Type 255 (ARINC 429 via dual IOC buses)
5.3.9 Category 9, Navigation Input Select
TABLE 5.3.9: NAVIGATION INPUT SELECT
Table 5.3.9-0: Navigation Inputs Select 0
Table 5.3.9-1: Navigation Inputs Select 1
Table 5.3.9-2: Navigation Inputs Select 2
Table 5.3.9-3: Navigation Inputs Select 3
Table 5.3.9-4: Navigation Inputs Select 4
Table 5.3.9-5: Navigation Inputs Select 5
Table 5.3.9-250: Navigation Inputs Select 250
Table 5.3.9-251: Navigation Inputs Select 251
Table 5.3.9-252: Navigation Inputs Select 252
Table 5.3.9-253: Navigation Inputs Select 253
Table 5.3.9-254: Navigation Inputs Select 254
Table 5.3.9-255: Navigation Inputs Select 255
5.3.10 Category 10, Attitude Input Select
Table 5.3.10: Attitude Input Select
Table 5.3.10-0: Attitude Input Select Type 0
Table 5.3.10-2: Attitude Input Select Type 2
Table 5.3.10-4: Attitude Input Select Type 4
Table 5.3.10-5: Attitude Input Select Type 5
Table 5.3.10-6: Attitude Input Select Type 6
Table 5.3.10-253: Attitude Input Select Type 253
Table 5.3.10-255: Attitude Input Select Type 255
5.3.11 Category 11, Heading Input Select
Table 5.3.11: Heading Input Select
Table 5.3.11-0: Heading Input Select 0
Table 5.3.11-2: Heading Input Select Type 2
Table 5.3.11-3: Heading Input Select Type 3
Table 5.3.11-254: Heading Input Select 254
Table 5.3.11-255: Heading Input Select 255
5.3.12 Category 12, Windshear Input Select
Table 5.3.12: Windshear Input Select
5.3.13 Category 13, Input / Output Discrete Type Select
Table 5.3.13: Input/Output Discrete Type Select
Table 5.3.13-0: Input/Output Discrete Type 0
Table 5.3.13-1: Input/Output Discrete Type 1
Table 5.3.13-2: Input/Output Discrete Type 2
Table 5.3.13-3: Input/Output Discrete Type 3
Table 5.3.13-4: Input/Output Discrete Type 4
Flashing Lamps True, False True
Table 5.3.13-5: Input/Output Discrete Type 5
Flashing Lamps True, False True
Table 5.3.13-6: Input/Output Discrete Type 6
Table 5.3.13-7: Input/Output Discrete Type 7
Table 5.3.13-254: Input/Output Discrete Type 254
Table 5.3.13-255: Input/Output Discrete Type 255
5.3.14 Category 14, Audio Output Level
Table 5.3.14: Audio Output Level
5.3.15 Category 15, Undefined for this software release
Table 5.3.15: Undefined Type
5.3.16 Category 16, Undefined for this software release
6 CONFIGURABLE INPUT DATA DEFINITION
6.1 Analog Input Data 6.1.1 ARINC 552 Radio Altimeter
6.1.2 ALT 55 Radio Altimeter
6.1.3 Uncorrected Barometric Altitude
6.1.4 Outside Air Temperature (500 ohm probe)
6.1.5 Outside Air Temperature (Internal Constant)
6.1.6 ARINC 547/578-4 Low Level Glideslope Deviation with Discrete Valid
6.1.7 ARINC 547/578-4 Low Level Glideslope Deviation with Low Level Valid
6.1.8 Roll Attitude, 3 Wire Synchro (11.8 VAC )
6.1.9 Magnetic Heading, 5 Wire Synchro
6.1.10 Uncorrected Barometric Altitude (ADS-65)
6.1.11 RT-221/300 Radio Altimeter
6.1.12 Pitch Synchro Attitude, 3 Wire Synchro (11.8 VAC )
6.1.13 Uncorrected Barometric Altitude (CIC 02702)
6.1.14 ARINC 547/578-4 Low Level Glideslope Deviation Validity
6.1.15 Roll Attitude, 3 Wire Synchro (11.8 VAC ) with Validity
6.1.16 Uncorrected Barometric Altitude (AZ-241, AZ-800)
6.1.17 ARINC 547 Localizer Deviation with Discrete Valid
6.2 Digital Input Data, ARINC 429
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6.2.1 Uncorrected Barometric Altitude (203)
6.2.2 Static Air Temperature (213)
6.2.3 Barometric Altitude Rate (212)
6.2.4 Altitude (076) - GPS (MSL)
6.2.5 Horizontal Integrity Limit (130) - GPS
6.2.7 Latitude (110) - GPS
6.2.8 Longitude (111) - GPS
6.2.9 Track Angle (103) - GPS
6.2.10 Horizontal Figure Of Merit (247) GPS (ARINC 743A)
6.2.11 Horizontal Figure Of Merit (247) GPS (ARINC 743)
6.2.16 Sensor Status (273) - GPS
6.2.17 Universal Time Correlation (125) - GPS
6.2.18 Date (260) - GPS
6.2.19 Control Word (154) - MFD
6.2.20 Control Word 2 (271/273)
6.2.20.1 Control Word 2 (271/273) Type 2
6.2.21 Discrete Word (155 or 176) - MFD
6.2.22 Hazard Range Output (077)
6.2.23 Range (050) - Multifunction Signal Generator (MG) or IC600
6.2.24 Query / Continuous Response (011) - KCPB
6.2.25 Key Press Data (012) KCPB
6.2.26 Control Word 1 (270)
6.2.27 Discrete Word (273) Bendix Weather Radar Vertical Profile Mode
6.2.28 Discrete Word (275) IC600 only
6.2.29 Radio Altitude (164)
6.2.30 Glideslope Deviation (174 or 117)
6.2.31 Roll Angle (325)
6.2.32 Magnetic Heading (320)
6.2.33 Localizer Deviation (173 or 116)
6.2.34 Pitch Angle (324)
6.2.35 Range (271) - KCPB
6.2.37 True Heading (314)
6.2.38 Corrected Barometric Altitude (204)
6.2.39 Computed Airspeed (206)
6.2.40 True Airspeed (210)
6.2.41 Decision Height (370) IOC Scaling
6.2.43 Longitudinal Acceleration (331)
6.2.44 Left Body Angle of Attack (224)
6.2.45 Right Body Angle of Attack (225)
6.2.46 VOR/ILS Frequency (034)
6.2.47 PFD Mode Select Word (163)
6.2.48 FWC & GP Discrete Word (171)
6.2.49 Body Pitch Rate (326)
6.2.50 Body Roll Rate (327)
6.2.51 Minimum Descent Altitude (170) IOC Scaling
6.2.52 Normal Angle of Attack (236)
6.2.53 North/South Velocity (166) - GPS
6.2.54 East/West Velocity (174) - GPS
6.2.55 Discrete Word (017) - KMD 550/850
6.2.56 Inertial Vertical Speed (365)
6.2.57 Inertial Altitude (361)
6.2.59 Latitude Fine (120) - GPS
6.2.60 Longitude Fine (121) - GPS
6.2.61 Selected Course (100) - IOC
6.2.62 DH/MDA Selected (170) DAU Scaling
6.3 Digital Data, ARINC 575
6.3.2 Uncorrected Barometric Altitude (203)
6.3.3 Barometric Altitude Rate (212)
6.3.4 Computed Airspeed (206)
6.4 Digital Data, RS-232
6.4.1 Xpress GPS Packets ID 15: Lat/Lon/Estimated Horizontal Position Error
6.4.4 Xpress GPS Packets ID 18: East/North/Up Velocity
6.4.5 Xpress GPS Packets ID 1C: GPS State
6.5 Digital Data, RS-422
6.5.1 Honeywell RS-422 Serial Control Interface (SCI) Mode/Range Word
6.5.1.1 Serial Control Interface (SCI) Mode/Range Word 1 (80)
6.5.1.2 Serial Control Interface (SCI) Status Word 1 (FF)
6.5.2 Honeywell RS-232 Serial Control Interface for DC811 Up/Down Range
6.6 Discrete Inputs
6.6.1 Analog Radio Altitude Validity Flags
6.6.2 GND Landing Gear Discrete
6.6.3 +28V Landing Gear Discrete
6.6.4 GND Landing Flap Discrete
6.6.5 +28V Landing Flap Discrete
6.6.6 Momentary Flap Override Discrete
6.6.7 Self-Test Discrete
6.6.8 GND ILS Tuned Discrete #1
6.6.9 +28V ILS Tuned Discrete #1
6.6.10 Glideslope Validity Discrete #1
6.6.11 GND Glideslope Inhibit Discrete
6.6.12 +28 V Glideslope Inhibit Discrete
6.6.13 Glideslope Cancel Discrete
6.6.14 Decision Height Discrete
6.6.15 Mode 6 Low Volume Discrete
6.6.16 GND Audio Inhibit Discrete
6.6.17 +28V Audio Inhibit Discrete
6.6.18 Display Select Discrete #1
6.6.19 Display Select Discrete #2
6.6.20 Terrain Awareness & TCF Inhibit Discrete
6.6.21 Autopilot Engaged Discrete #1
6.6.22 Barometric Altitude Validity Discrete
6.6.23 Magnetic Heading Validity Discrete
6.6.25 Steep Approach Discrete #2
6.6.26 Timed Audio Inhibit Discrete
6.6.27 GPWS Inhibit Discrete
6.6.28 Localizer Validity Discrete #1
7 OUTPUT DATA DEFINITION 7.1 ARINC 429 Output Data
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7.1.1 Discrete Output Words
7.1.1.1 EGPWS Alert Discrete #1 (270)
7.1.1.2 EGPWC Logic Discretes (271)
7.1.1.3 Mode 6 Callouts Discrete #1 (272)
7.1.1.4 Mode 6 Callouts Discrete #2 (273)
7.1.1.5 EGPWS Alert Discrete #2 (274)
7.1.1.6 EGPWC Alert Discrete #3 (300)
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7.1.2.8 Body Angle of AttackLeft (224) MKVIII EGPWS w/ Windshear only
7.1.2.9 Corrected Airspeed (242) MKVIII EGPWS w/ Windshear only
7.1.2.10 Windshear Warning Threshold (331) MKVIII EGPWS w/ Windshear only
7.1.2.11 Corrected Longitudinal Acceleration (332) MKVIII EGPWS w/ Windshear only
7.1.2.12 Raw Total Shear (362) MKVIII EGPWS w/ Windshear only
7.1.3 Terrain Display Outputs
The following ARINC 429 outputs support the Terrain Display function.
7.1.3.1 Displayed Range (050)
NOTE: Bits contain left and right side Terrain Display Ranges (0.5 to 2000 NM, format as follows)
7.1.3.2 Terrain Display Status Word (051)
7.1.3.3 Message Word #1 (052)
This label contains the color to be displayed on the 6-character terrain display window.
7.1.3.4 Message Word #2 (053)
7.1.3.5 Message Word #3 (054)
NOTE: Text code for degree sign is non-standard ASCII for 40HEX.
7.1.3.6 Message Word #4 (055)
This label contains the last 2 characters to be displayed on the 6-character terrain display window.
7.1.4 Equipment Identification
Provides equipment identification for maintenance reporting.
7.1.4.1 Equipment Identification Word (377)
7.1.5 Fault Summary Words (for Proline 4/21)
Provides fault diagnosis information.
7.1.5.3 Fault Diagnostic Word #3 (355)
7.1.6 Peak Binary Labels
7.1.6.1 Peaks Upper Elevation (011)
7.1.6.2 Peaks Lower Elevation (012)
7.2 ARINC 708A Output
7.3 Audio Output
7.4 Discrete Outputs
7.4.1 Ground Proximity Alerts Discrete (Lamp) Outputs
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7.4.11 Windshear Caution
7.4.12 Steep Approach Discrete
7.5 System Configuration Status
TABLE 7.5-1: CONFIGURATION OPTIONS AND MESSAGES
7.5.1 System Status Messages
TABLE 7.5.1-1: EGPWC SYSTEM STATUS MESSAGES
8 CONNECTOR INTERFACE 8.1 Pinout for Front Connectors sorted by pin number
Table 8.1-1: Pin Assignment For Front Connectors Sorted by Pin Number
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9 DEFINITIONS
