Honeywell MK VI, MK VIII - page 124

Honeywell

MK VI MK VIII EGPWS Installation Design Guide

Proprietary notice on title page applies

CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 124

NOTE: Precautionary notes on the PCMCIA card, regarding insertion and/or removal while power is

applied, should be ignored since the EGPWC automatically handles the application and removal

of PCMCIA card power.

(4) While the loading is in progress, the IN PROG LED on the Smart Card remains ON and the

COMPUTER OK LED on the EGPWC is OFF.

(5) When loading is complete the XFER COMP LED on the Smart Card turns ON.

(6) Remove the PCMCIA card from the Smart Card slot.

(7) After approximately 15 seconds the COMPUTER OK LED comes ON to indicate that the contents

of the PCMCIA card were successfully transferred.

(8) Remove the Smart Card connector from the EGPWC front panel J3 connector.

(9) To perform the verification of the Terrain Database version, go to paragraph 4.6.6 below.

B. Loading the PCMCIA Card Data with Computer Mounted on the Bench

(1) Locate a 28 VDC Power Supply with a minimum supply current of 2 amps.

(2) With the Power Supply turned OFF, connect the Power Supply to the J1 connector of the EGPWC

as follows (pin J1-53 is connected to chassis ground internally and does not need to be ground in

aircraft wiring):

J1 connector Pin Pin Nomenclature

J1-40, J1-60 28 VDC (+)

J1-41, J1-61 28 VDC (-)

J1-42, J1-53 Chassis GND

Pins J1-42 and J1-53 are both connected to chassis ground internally. It is not necessary to tie them

both to ground in the aircraft wiring. Pin J1-53 was made available to provide a convenient way to

supply a ground to external equipment. If the OAT probe is not present, nothing needs to be tied to J1-

53.

(3) Connect the Smart Cable (Honeywell PN 951-0386-001) to the EGPWC J3 connector.

(4) Turn the Power Supply ON and that the COMPUTER OK LED on the EGPWC front panel is on.

(5) Insert the PCMCIA card into the Smart Cable PCMCIA card slot.

NOTE: Precautionary notes on the PCMCIA card, regarding insertion and/or removal while power is

applied, should be ignored since the EGPWC automatically handles the application and removal

of PCMCIA card power.

(6) While the loading is in progress, the IN PROG LED on the Smart Card remains ON and the

COMPUTER OK LED on the EGPWC is OFF.

Contents

Main Page REVISION STATUS OF SHEETS INDEX Page TABLE OF CONTENTS Page Page Page Page Page Page Page 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 Page Page Page 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 Page Page Page FIGURE 2.1-4 MK VI/MK VIII EGPWS CONFIGURATION MODULE Page Page Page 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 Page Page Page Page Page Page Page Page 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) Page 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 Page Page 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 Page 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 Page 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 Page 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 Page 4.4.3 WinVIEWS 4.4.4 WinVIEWS Op eration 4.5 Configuration Module Programming Page 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 Page 4.6.6 Verification o f the Terrain Database Version Page Page SECTION V CERTIFICATION 5.2.7 Pilots Guide 5.2.8 Failure Modes , Effects, and Safety Analysis Page SECTION VI - MK VI GPWS to MK VI/VIII EGPWS Signal Mapping Page Page Page Page NEW CONNECTOR Page Page 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: Page Page Page Page Page APPENDIX C WinVIEWS Operation Instructions RS-232 COMMUNICATION WITH THE EGPWS 19200 Baud, No Parity, 8 bits, and 1 stop bit. Page Page Page APPENDIX D - Vendor Contact Information Vendor Contact Information Page Page Page Table of Contents Page Page Page Page 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 Page Page 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 Page 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 Page Table 5.3.6.1-0 KC Picture Bus Display Configuration Group 0 Page 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 Page Table 5.3.6.1-19 KC Picture Bus with Soft Keys Display Configuration Group 0 Page 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 Page Page Page Display Configuration Group 247 Table 5.3.6.1-243 Honeywell EDZ802, EDZ603, EDZ803 (non-Integrated) with dual SCI range Display Configuration Group 238 Page Page Page 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 Page Display Input Control Group 250 Page 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 Page 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 Page Page 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 Page 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 Page 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) Page 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 Page 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 Page Page Page Page 9 DEFINITIONS