Honeywell MKXXII - Manual

Honeywell MKXXII

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Table of Contents:

  • Page 2 – This document is an unpublished work. Copyright
  • Page 5 – Proprietary notice on title page applies; TABLE OF CONTENTS
  • Page 9 – SECTION V – CERTIFICATION 124
  • Page 12 – SECTION I
  • Page 14 – SECTION I – GENERAL INFORMATION
  • Page 16 – construed as formal FAA approved work authorization.; How To Use This Docu m ent
  • Page 17 – Reference Documents
  • Page 18 – Description of Equipm e nt; Fig 1.0 MK XXII EGPWC
  • Page 19 – MK XXII EGPWS Conf i guration Module; GPS antenna should meet the following qualifications:
  • Page 20 – pressure altitude with a corresponding reduction in accuracy.
  • Page 21 – FIGURE 1-1 MK XXII EGPWS SMART CABLE; MK XXII EGPWS
  • Page 22 – GPS Antenna Sensor
  • Page 24 – Installation and Acces s ories Kits
  • Page 25 – Accessories Required but not Supplied
  • Page 28 – License Requirements
  • Page 30 – SECTION II
  • Page 32 – SECTION II – INSTALLATION
  • Page 33 – SECTION II - INSTALLATION; NOTE; Unpacking and Inspec t ing the Equipment
  • Page 34 – from excessive vibration, heat, and noise generating sources.
  • Page 35 – Configuration Module Installation
  • Page 36 – CONFIGURATION MODULE ASSEMBLY
  • Page 37 – INSTALLATION ASSEMBLY SEQUENCE
  • Page 38 – MK XXII EGPWS CONFIGURATION MODULE
  • Page 40 – shielded pigtails of wires at this connector.
  • Page 46 – either the instrument panel or the edge of the glareshield.
  • Page 47 – MK XXII EGPWS Annunciators/Switches Location
  • Page 48 – Altitude Mode is also described below for reference.
  • Page 49 – FIGURE 2-2 MK XXII EGPWS OUTLINE
  • Page 50 – FIGURE 2-3 MK XXII EGPWS MOUNTING TRAY
  • Page 52 – SECTION III
  • Page 54 – SECTION III – SYSTEM PLANNING
  • Page 57 – System Wiring/ Electr i cal Interfaces
  • Page 58 – The EGPW C provides for ARINC 453 and ARINC 429 serial outputs.
  • Page 59 – inputs are valid and the audio inhibit discretes are not active.
  • Page 60 – Configurable Interface s; which has detailed interface configuration information.
  • Page 61 – digital air data types.
  • Page 62 – Uncorrected Baro Altitude
  • Page 63 – EGPWS MK XXII; Vendor Model
  • Page 65 – ohm probe using +5 volt excitation from the MK XXII EGPWC.; Vendor PN
  • Page 67 – CAUTION; know to have FOM computational errors:
  • Page 68 – EGPW S MK XXII; GND
  • Page 70 – Autorotation callout enablement.
  • Page 71 – Category 5 defines one Audio Menu options for Helicopters (ID 128).
  • Page 72 – Category 6 – Terrain Display Select; Display Configuration; Table E; Display Configuration Group, Display Input
  • Page 73 – provided in the table below.
  • Page 74 – TERR; Wx; Single Tube W
  • Page 75 – Display Mode, and Display status to the MK XXII EGPWC.
  • Page 76 – Honeywell Gr; RR; EGPW
  • Page 77 – XLS
  • Page 78 – AVIDYNE FSD
  • Page 79 – Integr; Honeywell W
  • Page 80 – AVTECH DSU
  • Page 81 – Table E 3
  • Page 82 – For Helicopters TA&D Alternate Pop Up should always be set to False.; displays terrain based on the absolute terrain elevations.; Note: TAD must be enabled if Obstacle Awareness is enabled.; appropriate for this installation.
  • Page 83 – WOW Reversal
  • Page 84 – Category 8 – Radio Altitude Input Select; Radio Altitude; Radio Altimeter Indicator
  • Page 86 – Category 9 – Navigation Inputs Select; Appendix E Table E 3
  • Page 87 – ILS Receiver; Low Level
  • Page 88 – ILS Bus
  • Page 89 – 0 Category 10 – Attitude Input Select; Appendix E Tables E 3 and Table E 3.1.10
  • Page 90 – Vertical Gyro; Roll Synchro
  • Page 91 – AHRS; HS
  • Page 92 – 1 Category 11 – Heading Input Select
  • Page 93 – Directional Gyro; Heading Synchro; Heading; 6 VAC Reference; Heading Ref
  • Page 95 – 2 Category 12 – Windshear Input Select; Category 12 defines the Windshear interface.; Windshear is not applicable to MK XXII.; Select ID 0 for all helicopter configurations.
  • Page 96 – Appendix E Table; This; ICD; Additional information for the discretes is provided below.
  • Page 100 – Appendix E Section 7.4
  • Page 101 – the remaining alerts and warnings.
  • Page 102 – switch-lamp assemblies mounted near the displays being selected.
  • Page 103 – Table 0-1 MKXXII EGPWS – Example Cockpit Lights
  • Page 104 – as described above, select the Audio Output; Appendix E Table E 3.
  • Page 105 – defines the Autorotation threshold options.; Appendix E
  • Page 106 – AUTOROTATION THRESHOLD; Aircraft Type ID
  • Page 107 – SECTION IV
  • Page 108 – SECTION IV – CONFIGURATION MODULE PROGRAMMING AND
  • Page 109 – that will be operating outside of the North American region.; Harness Checkout and Power Check; potential areas that may cause binding and/or chafing.; Unit Installation; for the unit locations and mounting information.; EGPWC Initialization a n d Configuration; for instructions related to using the WinViews software.
  • Page 110 – configured as follows:; (Windows Virtual Interface to the Enhanced Warning System); Configuration Module.
  • Page 111 – Configuration Module Programming
  • Page 112 – Invalid Parameter. Not enough
  • Page 114 – Configuration Module Reprogramming; Power EGPWC and PC and start WinVIEW S.; prompt use the CAT command with the following structure:
  • Page 115 – display the EGPWC and Configuration Module data.; Regional Terrain Data b ase Loading; in the Terrain Awareness function being unavailable.; On The Bench. An optional verification procedure is provided.
  • Page 117 – COMPUTER OK LED on the EGPWC front panel is on.
  • Page 118 – (5) Insert the PCMCIA card into the Smart Cable PCMCIA card slot.; and the COMPUTER OK LED on the EGPWC remains OFF.; the contents of the PCMCIA card were successfully transferred.; Verification of the Ter r ain Database Version
  • Page 119 – SYSTEM CONFIGURATION; versions will follow the same pattern.; END OF TEST
  • Page 121 – SECTION V
  • Page 124 – SECTION V – CERTIFICATION; Certification Procedur e; 37 with an applicable STC package.
  • Page 127 – APPENDIX A
  • Page 129 – ENH; COCKPIT DISPL
  • Page 131 – RA; PEN
  • Page 139 – APPENDIX B
  • Page 143 – APPENDIX C
  • Page 145 – APPENDIX C – WinViews Operation Instructions; RS-232 COMMUNICATION WITH THE EGPWS; EGPWS Front Connector
  • Page 146 – Windows Virtual Interface to the Enhanced Warning System; quick identification of system anomalies.
  • Page 149 – APPENDIX D
  • Page 151 – D 1-0 Vendor Contact Information
  • Page 153 – EDMO; Switch
  • Page 154 – EMTEQ; GPS - RF Cable Sets
  • Page 155 – TABLE 1
  • Page 156 – TABLE 2
  • Page 158 – Tool Frame and Die Part Numbers
  • Page 159 – Installation Considerations:; help in the configuration and meet your requirements.
  • Page 160 – Aerospace Optics; Aerospace Optics Inc.
  • Page 162 – StacoSwitch; Please check out our full line of products at
  • Page 163 – APPENDIX E
  • Page 166 – INTRODUCTION; XXX = Application Software (including Configuration Software); PURPOSE
  • Page 168 – DC ANALOG INPUTS
  • Page 169 – BAROMETRIC ALTITUDE
  • Page 170 – AC ANALOG INPUTS; SYNCHRO MAGNETIC HEADING
  • Page 171 – CONFIGURATION DEFINED SYNCHRO INPUTS; SIGNAL TIMING REFERENCE INPUTS
  • Page 174 – DISCRETE INPUTS; +28 VDC Discrete Characteristics
  • Page 175 – Ground Discrete Characteristics; CONFIGURATION MODULE INTERFACE; Output to Config Module; INTERFACE OF EGPWS OUTPUTS TO CONFIGURATION MODULE; GPS ANTENNA INPUT
  • Page 176 – OAT VOLTAGE REFERENCE OUTPUT
  • Page 177 – ARINC DIGITAL SERIAL OUTPUT BUSSES
  • Page 178 – FRONT PANEL TEST INTERFACE
  • Page 179 – PCMCIA / SMARTCABLE PORT
  • Page 180 – AIRCRAFT APPLICATION DATA
  • Page 181 – Signal; Ident No
  • Page 182 – E 5.3 CONFIGURATION SELECTION TABLES
  • Page 184 – Torque; DESCRIPTION; Effectivity; Helo, Agusta 109E Power, Retractable Gear
  • Page 185 – ENGINE TORQUE DATA SELECTION
  • Page 189 – CATEGORY 2, AIR DATA INPUT SELECT; Description
  • Page 190 – Temperature Probe only.; Configuration Data; Derive Baro Altitude Rate
  • Page 195 – CATEGORY 3, POSITION INPUT SELECT
  • Page 196 – *Slowest acceptable update rate in milliseconds.; *Slowest acceptable update rate in milliseconds.
  • Page 197 – * Slowest acceptable update rate in milliseconds.
  • Page 198 – Fault Designation: GPS BUS 1
  • Page 199 – CATEGORY 4, ALTITUDE CALLOUTS; t Callout function will not be given if in autorotation
  • Page 201 – CATEGORY 5, AUDIO MENU SELECT
  • Page 202 – CATEGORY 6, TERRAIN DISPLAY SELECT
  • Page 204 – KC Picture Bus
  • Page 217 – Function; Display Input Control Group 2
  • Page 218 – Channel
  • Page 221 – K C P ictu re B u s w /o p resen tation of T errain A w aren ess C orrected; Display Input Control Group 0
  • Page 223 – Display Input Control Group; Fault Designation: IOC BUS 1
  • Page 224 – Display Input Control
  • Page 226 – Display Configuration Group 0 (KC Picture Bus; Display Input Control Group 245
  • Page 229 – The display will change to Map mode.
  • Page 230 – Display Configuration Group 255 (Honeywell SPZ8000 older style); Display Input Control Group 255; Fault Designation: DISPLAY BUS 1
  • Page 231 – CATEGORY 7, OPTIONS 1 SELECT
  • Page 233 – CATEGORY 8, RADIO ALTITUDE INPUT SELECT; In this category, only the following signals are defined:
  • Page 236 – CATEGORY 9, NAVIGATION INPUT SELECT; Glideslope source selection.
  • Page 237 – KN40 Nav Source
  • Page 238 – CATEGORY 10, ATTITUDE INPUT SELECT
  • Page 240 – CATEGORY 11, HEADING INPUT SELECT
  • Page 241 – CATEGORY 12, WINDSHEAR INPUT SELECT; The Windshear warning is not applicable to Helicopters.; No Windshear
  • Page 242 – CATEGORY 13, INPUT / OUTPUT DISCRETE TYPE SELECT; Discrete Type
  • Page 243 – Lamp Format
  • Page 245 – CATEGORY 14, AUDIO OUTPUT LEVEL; Volume Select; Nominal
  • Page 246 – CATEGORY 15, AUTOROTATION THRESHOLD; Autorotation
  • Page 247 – CONNECTOR INTERFACE; Pin
  • Page 249 – *Refer to Category 13 where multiple uses are possible.
  • Page 252 – DEFINITIONS; Acronym
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Airlines & Cvionics Products
Honeywell International, Inc.
15001 N.E. 36 th Street
Redmond, WA 98052

MK XXII

Enhanced Ground Proximity

Warning System

for

Rotorwing

Aircraft

Installation Manual
060-4314-225 Rev C

Part Numbers:

965-1590-006
965-1590-008
965-1590-010
965-1590-011

Release Date: 12/14/00

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Summary

Page 2 - This document is an unpublished work. Copyright

Honeywell MK XXII EGPWS Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 2 This document is an unpublished work. Copyright ” 2000 Honeywell, International, Inc. All rights reserved. This document and all information and expression contained herein are the pr...

Page 5 - Proprietary notice on title page applies; TABLE OF CONTENTS

Honeywell MK VI MK VIII EGPWS Installation Design Guide Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 5 TABLE OF CONTENTS SECTION I – GENERAL INFORMATION....................................................................................

Page 9 - SECTION V – CERTIFICATION 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: 060-4314-225 REV: C SHEET 9 3.3.14.1 Instructions .......................................................................................................... ....

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