Honeywell MKXXII User Manual
Airlines & Cvionics Products
Honeywell International, Inc.
15001 N.E. 36 th Street
Redmond, WA 98052
Enhanced Ground Proximity
Warning System
MK XXII
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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Honeywell
MK XXII EGPWS Installation Manual
This document is an unpublished work. Copyright 2000 Honeywell, International, Inc. All
rights reserved.
This document a nd all informati on and expressio n contained herein are the property of Honeywell International
Inc., and is provided to the recipient i n confidence on a “nee d to know” basis. Your use of this document is strictly
limited to a legit imate business purpose requiring the information c ontained therein. Your use of this document
constitutes acceptance of these terms.
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MK XXII EGPWS Installation Manual
Typed names constitute approval signatures. Actual signatures are on file at Honeywell in
Redmond, WA.
DRAWN
CHECK
ENGR
Dennis Martin 12/8/00
Sara Stark 12/8/00
Dennis Martin 12/8/00
MFG
QA
APVD
Dennis Martin 12/8/00
APVD
REVISIONS
SH REV DESCRIPTION DATE APPROVED
ALL A Added Software –008 Revisions.
8/9/01
8/9/01
S. Wright
D. Martin
Reason: 01 Severity: 10
ALL B Added Software –010 Revisions.
Reason: 01 Severity: 10
ALL C Added Software –011 Revisions.
Reason: 01 Severity: 10
3/22/02
3/22/02
6/07/02
6/7/02
D. Martin
R Gilliland
D Martin
T Curtis
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MK XXII EGPWS Installation Manual
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MK VI MK VIII EGPWS Installation Design Guide
TABLE OF CONTENTS
SECTION I – GENERAL INFORMATION............................................................................................16
1.1 I
NTRODUCTION.................................................................................................................................... 16
1.2 A
PPLICABILITY.................................................................................................................................... 16
1.3 H
OW TO USE THIS DOCUMENT ........................................................................................................... 16
1.4 R
EFERENCE DOCUMENTS .................................................................................................................... 17
1.5 D
ESCRIPTION OF EQUIPMENT...............................................................................................................18
1.5.1 MK XXII EGPWS Computer........................................................................................................ 19
1.5.2 MK XXII EGPWS Configuration Module.................................................................................... 19
1.5.3 GPS Antenna................................................................................................................................ 19
1.5.4 OAT Sensor..................................................................................................................................19
1.5.5 Smart Cable (PCMCIA Interface)................................................................................................20
1.6 T
ECHNICAL CHARACTERISTICS ........................................................................................................... 21
1.7 U
NITS SUPPLIED ..................................................................................................................................22
1.7.1 MK XXII EGPWS......................................................................................................................... 22
note 1: -0XX defines the Application software version......................................................................... 22
1.7.2 Configuration Module..................................................................................................................22
1.7.3 Smart Cable (PCMCIA Interface)................................................................................................22
1.8 I
NSTALLATION AND ACCESSORIES KITS .............................................................................................. 24
1.8.1 MK XXII EGPWS Installation Kits.............................................................................................. 24
1.8.2 RS-232 Cable............................................................................................................................... 24
1.8.3 Smart Cable................................................................................................................................. 24
1.8.4 Terrain Database Cards.............................................................................................................. 25
1.8.5 Flight History Card ..................................................................................................................... 25
1.9 A
CCESSORIES REQUIRED BUT NOT SUPPLIED.......................................................................................25
1.9.1 ARINC 453 Terrain Display wiring.............................................................................................25
1.9.2 GPS Antenna & cable.................................................................................................................. 26
1.9.3 Circuit Breaker............................................................................................................................ 26
1.9.4 Annunciators & Switch/Annunciators.......................................................................................... 26
1.9.4.1 GPWS Warning (red) P/TEST; switch/annunciator assembly............................................................... 26
1.9.4.2 GPWS Caution (amber) G/S CANCLD switch/annunciator assembly.................................................. 27
1.9.4.3 LOW ALT / ON switch/annunciator assembly...................................................................................... 27
1.9.4.4 TERR INHIB / ON switch/annunciator assembly................................................................................. 27
1.9.4.5 AUDIO INHIBIT / ON switch/annunciator assembly........................................................................... 27
1.9.4.6 GPWS INOP / TERR INOP annunciator assemblies............................................................................. 27
1.9.4.7 TERR DISPLAY / ON switch/annunciator assemblies.........................................................................27
1.10 COCKPIT SPEAKER (OPTIONAL)......................................................................................................... 27
1.11 T
OOLS REQUIRED.............................................................................................................................. 28
1.11.1 Crimping Tool - P1, P2, P3...................................................................................................... 28
1.11.2 Contact Positioner - P1, P2, P3................................................................................................28
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1.11.3 Insertion/Removal Tool - P1, P2, P3........................................................................................ 28
1.11.4 Spare Contacts - P1, P2, P3...................................................................................................... 28
1.12 L
ICENSE REQUIREMENTS................................................................................................................... 28
SECTION II - INSTALLATION ..............................................................................................................................33
2.1 I
NTRODUCTION.................................................................................................................................................... 33
2.2 U
NPACKING AND INSPECTING THE EQUIPMENT................................................................................................... 33
2.3 E
QUIPMENT INSTALLATION ................................................................................................................................. 33
2.3.1 General........................................................................................................................................................33
2.3.2 MK XXII Computer Location....................................................................................................................... 34
2.3.3 MK XXII Computer Installation...................................................................................................................34
2.3.4 Configuration Module Location .................................................................................................................. 35
2.3.5 Configuration Module Installation.............................................................................................................. 35
2.3.6 GPS Antenna location.................................................................................................................................. 44
2.3.7 GPS Antenna Installation............................................................................................................................ 44
2.3.8 OAT Sensor Location................................................................................................................................... 44
2.3.9 OAT Sensor Installation...............................................................................................................................44
2.3.10 Cockpit Annunciators / Switches................................................................................................................44
2.3.10.1 Description............................................................................................................................................................45
2.3.10.2 Location................................................................................................................................................................. 46
2.3.10.3 Inhibit Switch Functions and Selection .................................................................................................................48
2.3.10.3.1 Terrain Inhibit ................................................................................................................................................ 48
2.3.10.3.2 Audio Inhibit (Timed)....................................................................................................................................48
2.3.10.3.3 Audio Inhibit (Not Described Above)............................................................................................................ 48
2.3.10.3.4 Low Altitude Mode........................................................................................................................................48
SECTION III – SYSTEM PLANNING.................................................................................................................................57
3.1 I
NTRODUCTION.................................................................................................................................... 57
3.2 S
YSTEM WIRING/ ELECTRICAL INTERFACES........................................................................................57
3.2.1 Primary Power Input................................................................................................................................................57
3.2.2 Chassis Ground ........................................................................................................................................................57
3.2.3 GPS Antenna............................................................................................................................................................. 58
3.2.4 Analog and Digital Inputs.........................................................................................................................................58
3.2.5 Discrete Inputs..........................................................................................................................................................58
3.2.6 Serial Outputs...........................................................................................................................................................58
3.2.7 Audio Output.............................................................................................................................................................59
3.2.8 Discrete Outputs.......................................................................................................................................................59
3.2.9 Configuration Module...............................................................................................................................................59
3.3 C
ONFIGURABLE INTERFACES............................................................................................................... 60
3.3.1 Category 1 - Aircraft / Mode Type Select.................................................................................................................60
3.3.1.1 Aircraft / Mode Type............................................................................................................................. 60
3.3.1.2 Instructions............................................................................................................................................ 60
3.3.1.3 Generic Helicopter with and without Torque......................................................................................... 60
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3.3.2 Category 2 – Air Data Input Select........................................................................................................................... 61
3.3.2.1 Instructions........................................................................................................... ................................. 61
3.3.2.2 Examples............................................................................................................... ................................ 62
3.3.2.3 Analog altitude and 500 ohm OAT........................................................................................ ........... 62
3.3.2.4 Digital – ARINC 429 (Cat. 2 ID 5, 1, 6)........................................................................................... 63
3.3.2.5 Digital –ARINC 575 (Cat. 2 ID 2).................................................................................................... 64
3.3.2.6 Shadin 2000 (Cat. 2 ID 10) ............................................................................................................... 65
3.3.2.7 Digital – ARINC 429 Dual IOC Buses (Cat. 2. ID 255)................................................................... 66
3.3.3 Category 3 – Position Input Select...........................................................................................................................67
3.3.3.1 Instructions............................................................................................................................................ 67
3.3.3.2 ARINC 743 Format ............................................................................................................................... 67
3.3.3.Examples.................................................................................................................................................. 68
3.3.3.1 ARINC 429 BUS (Cat. 3 ID 0,1,4,5)................................................................................................. 68
3.3.3.2 RS-232 Transmit-Receive, 9600 baud (Cat. 3 ID 3) ......................................................................... 68
3.3.3.3 Dual ARINC 429 BUS (Cat. 3 ID 255)............................................................................................. 69
3.3.4 Category 4 – Altitude Callouts .................................................................................................................................70
3.3.4.1 Instructions............................................................................................................................................ 70
3.3.5 Category 5 – Audio Menu Select .............................................................................................................................. 71
3.3.5.1 Instructions............................................................................................................................................ 71
3.3.6 Category 6 – Terrain Display Select ........................................................................................................................72
3.3.6.1 Instructions............................................................................................................................................ 72
3.3.6.2 TAD Selection....................................................................................................................................... 72
3.3.6.3 Terrain Display Configuration Group.................................................................................................... 73
3.3.6.4 Display Input Control Group............................................................................................ ..................... 75
3.3.6.5 Output 429 Bus Group........................................................................................................................... 75
3.3.6.6 Example................................................................................................................................................. 75
3.3.7 Category 7 – Options Select Group #1.....................................................................................................................81
3.3.7.1 Instructions............................................................................................................................................ 81
3.3.7.2 Steep Approach (Not Available in the Mk XXII).................................................................................. 81
3.3.7.3 TA&D Alternate Pop-up........................................................................................................................ 81
3.3.7.4 Peaks Mode ........................................................................................................................................... 82
3.3.7.5 Obstacle Awareness............................................................................................................................... 82
3.3.7.6 Bank Angle Callout Enabling................................................................................................................ 82
3.3.7.8 WOW Reversal...................................................................................................................................... 83
3.3.7.9 GPS Altitude Reference......................................................................................................................... 83
3.3.8 Category 8 – Radio Altitude Input Select..................................................................................................................84
3.3.8.1 Instructions............................................................................................................................................ 84
3.3.8.2 Example................................................................................................................................................. 84
3.3.8.3 Digital Radio Altitude Interface........................................................................................................ 84
3.3.8.4 Analog Radio Altitude Interface........................................................................................................ 85
3.3.9 Category 9 – Navigation Inputs Select..................................................................................................................... 86
3.3.9.1 Instructions............................................................................................................................................ 86
3.3.9.2 Example................................................................................................................................................. 87
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3.3.9.3 Analog Glideslope Interface (cat. 9 ID 0,1,5) ................................................................................... 87
3.3.9.4 Digital Glideslope/Localizer Interface.............................................................................................. 88
3.3.9.5 Dual Glideslope Receiver.................................................................................................................. 88
3.3.10 Category 10 – Attitude Input Select........................................................................................................................89
3.3.10.1 Attitude Signals ................................................................................................................................... 89
3.3.10.2 Instructions.......................................................................................................... ................................ 89
3.3.10.3 Example............................................................................................................... ................................ 90
3.3.10.4 Analog Roll Angle (Synchro).......................................................................................................... 90
3.3.10.5 Digital ARINC 429 High Speed.......................................................................................... ............ 91
3.3.11 Category 11 – Heading Input Select.......................................................................................................................92
3.3.11.1 Instructions.......................................................................................................................................... 92
3.3.11.2 Magnetic Heading................................................................................................................................ 92
3.3.11.3 Example............................................................................................................................................... 93
3.3.11.3.1 Analog Heading (Synchro) (CAT. 11 ID 0)................................................................................. 93
3.3.11.3.2 Digital ARINC 429 High Speed........................................................................................ ........... 94
3.3.12 Category 12 – Windshear Input Select ...................................................................................................................95
3.3.12.1 Instruction............................................................................................................................................ 95
3.3.13 Category 13 – Input / Output Discrete Type Select................................................................................................96
3.3.13.1 Instruction............................................................................................................................................ 96
3.3.13.2 Input/Output Discretes......................................................................................................................... 96
3.3.13.3 Audio Inhibit Discrete..................................................................................................................... 97
3.3.13.4 Landing Gear Discrete..................................................................................................................... 97
3.3.13.5 Weight ON Wheels (WOW) Discrete............................................................................................. 97
3.3.13.6 Glideslope Cancel Discrete............................................................................................................. 98
3.3.13.7 Mode 6 Low Volume Discrete........................................................................................................ 98
3.3.13.8 Autopilot Engaged Discrete ............................................................................................................ 98
3.3.13.9 Terrain Awareness Inhibit............................................................................................................... 99
3.3.13.10 Self Test Discrete .......................................................................................................................... 99
3.3.13.11 Glideslope Inhibit Discrete............................................................................................................ 99
3.3.13.12 Timed Audio Inhibit Discrete...................................................................................................... 100
3.3.13.13 Low Altitude Mode Select Discrete............................................................................................ 100
3.3.13.14 Output Discretes.......................................................................................................................... 100
3.3.13.15 Lamp Format.......................................................................................................... ..................... 100
3.3.13.16 GPWS INOP Discrete................................................................................................................. 101
3.3.13.17 TAD INOP Discrete .................................................................................................................... 101
3.3.13.18 GPWS Warning Discrete............................................................................................................. 101
3.3.13.19 GPWS Alert Discrete .................................................................................................................. 101
3.3.13.20 Glideslope Cancel Discrete......................................................................................................... 101
3.3.13.21 TCAS Inhibit Discrete................................................................................................................. 101
3.3.13.22 Terrain Display Select #1 & #2 Discrete..................................................................................... 102
3.3.13.23 Timed Audio Inhibit Discrete...................................................................................................... 102
3.3.13.24 Low Altitude Mode Discrete....................................................................................................... 102
3.3.14 Category 14 – Audio Output Level.......................................................................................................................104
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3.3.14.1 Instructions.......................................................................................................... .............................. 104
3.3.15 Category 15, Autorotation Threshold...................................................................................................................105
3.3.15.1 Instruction.......................................................................................................................................... 105
SECTION IV – CONFIGURATION MODULE PROGRAMMING AND REGIONAL TERRAIN
DATABASE LOADING........................................................................................................................................................109
4.1 I
NTRODUCTION.................................................................................................................................. 109
4.2 H
ARNESS CHECKOUT AND POWER CHECK ........................................................................................ 109
4.3 U
NIT INSTALLATION.......................................................................................................................... 109
4.4 EGPWC I
NITIALIZATION AND CONFIGURATION ............................................................................... 109
4.4.1 RS-232 Communication with the MK XXII EGPWS..................................................................109
4.4.2 EGPWC Front Panel Test Connector........................................................................................ 110
4.4.3 WinVIEWS................................................................................................................................. 110
4.4.4 WinVIEWS Operation................................................................................................................ 111
4.5 C
ONFIGURATION MODULE PROGRAMMING .......................................................................................111
4.5.1 CUW and CMR Commands..................................................................................................... .. 113
4.5.2 Configuration Module Reprogramming.....................................................................................114
4.6 R
EGIONAL TERRAIN DATABASE LOADING ........................................................................................ 115
4.6.1 Effectivity...................................................................................................................................115
4.6.2 Description ................................................................................................................................ 115
4.6.3 Approval .................................................................................................................................... 115
4.6.4 Material – Cost and Availability................................................................................................116
4.6.5 Accomplishment Instructions..................................................................................................... 117
4.6.6 Verification of the Terrain Database Version............................................................................ 118
SECTION V – CERTIFICATION 124
5.1 I
NTRODUCTION .................................................................................................................................124
5.2 C
ERTIFICATION PROCEDURE .............................................................................................................124
5.2.2 Equipment Location ...............................................................................................................................................124
5.2.3 FAA Requirements .................................................................................................................................................124
5.2.4 Ground Test ...........................................................................................................................................................124
5.2.5 Flight Manual Revision .........................................................................................................................................124
5.2.6 Flight Test ..............................................................................................................................................................125
5.2.7 Pilots Guide ...........................................................................................................................................................125
5.2.8 Failure Modes, Effects, and Safety Analysis ..........................................................................................................125
5.2.9 Existing STC’s .......................................................................................................................................................125
APPENDIX A.........................................................................................................................................................................127
CUSTOMER WORKSHEET...............................................................................................................................................127
APPENDIX B.........................................................................................................................................................................139
SAMPLE WIRING DIAGRAMS.........................................................................................................................................139
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APPENDIX C.........................................................................................................................................................................143
WINVIEWS OPERATION INSTRUCTIONS...................................................................................................................143
APPENDIX D............................................................................................................................................149
VENDOR DRAWINGS............................................................................................................................ 149
D 1-0 V
ENDOR CONTACT INFORMATION.................................................................................................151
D1-1 EDMO................................................................................................................................. 153
D1-2 EMTEQ...............................................................................................................................154
GPS - RF Cable Sets......................................................................................................................... 154
TABLE 2 ............................................................................................................................................. 156
Table 2.A.1 Connectors (for TFLX cable series) - GPS ...................................................................156
TABLE 2 (continued).......................................................................................................................... 157
Table 2.B.1 Connectors (for PFLX cable series) – GPS.................................................................... 157
TOOL FRAME AND DIE PART NUMBERS....................................................................................... 158
I
NSTALLATION CONSIDERATIONS:........................................................................................................... 159
D1-3 Aerospace Optics................................................................................................................160
AEROSPACE OPTICS INC....................................................................................................................160
LED LIGHTING ...................................................................................................................................... 160
INTRODUCTION.................................................................................................................................................................166
E 1 P
E 2 P
E 3 S
ART NUMBER..........................................................................................................................................................166
URPOSE...................................................................................................................................................................166
YSTEM OVERVIEW..................................................................................................................................................166
E 4 ELECTRICAL INTERFACE....................................................................................................... ...........................167
E 4.1 Introduction.....................................................................................................................................................167
E 4.2 Signal Interfaces..............................................................................................................................................167
E 4.2.1 Grounds...........................................................................................................................................................167
E 4.2.2 Primary Power Input.......................................................................................................................................167
E 4.2.3 DC Analog Inputs............................................................................................................................................168
E 4.2.7 AC Analog Inputs.............................................................................................................................................170
E 4.2.9 ARINC 429/575 Digital Serial Bus Inputs................................................................................. ......................172
E 4.2.9.1 RS-232 / RS-422 Digital Serial Bus Inputs ..................................................................................................173
E 4.2.10 Discrete Inputs.............................................................................................................................................174
E 4.2.11 Configuration Module Interface..................................................................................................................175
E 4.2.12 GPS Antenna Input ......................................................................................................................................175
E 4.2.13 OAT Voltage Reference Output....................................................................................................................176
E 4.2.14 Lamp Driver Outputs...................................................................................................................................176
E 4.2.16 Audio Outputs..............................................................................................................................................176
E 4.2.17 ARINC Digital Serial Output Busses...........................................................................................................177
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MK VI MK VIII EGPWS Installation Design Guide
E 4.2.17.1 ARINC 429 Output Bus............................................................................................................................177
E 4.2.17.2 ARINC 453 Output Bus............................................................................................................................178
E 4.2.18 F
E 4.2.18.1 RS-232 M
RONT PANEL TEST INTERFACE........................................................................................................................178
AINTENANCE PORT (SERIAL PORT 4).............................................................................................178
E 4.2.18.2 PCMCIA / SmartCable Port ....................................................................................................................179
E 4.2.18.3 GSE Present Discrete Input.....................................................................................................................179
E 4.2.19 F
RONT PANEL STATUS INDICATORS .................................................................................................................179
E 5 AIRCRAFT APPLICATION DATA.......................................................................................................................180
E 5.1 C
E 5.2 C
ONFIGURATION TYPES........................................................................................................................................180
ONFIGURATION SELECTION................................................................................................................................180
E 5.3 Configuration Selection Tables........................................................................................................................ 182
E 5.3.1 Category 1, Aircraft / Mode Type Select..........................................................................................................183
E 5.3.2 Category 2, Air Data Input Select....................................................................................................................189
E 5.3.3 Category 3, Position Input Select...................................................................................................................195
E 5.3.4 Category 4, Altitude Callouts ..........................................................................................................................199
E 5.3.5 Category 5, Audio Menu Select........................................................................................................................201
E 5.3.6 Category 6, Terrain Display Select..................................................................................................................202
E 5.3.7 Category 7, Options 1 Select...........................................................................................................................231
E 5.3.8 Category 8, Radio Altitude Input Select...........................................................................................................233
E 5.3.9 Category 9, Navigation Input Select................................................................................................................236
E 5.3.10 Category 10, Attitude Input Select...............................................................................................................238
E 5.3.11 Category 11, Heading Input Select..............................................................................................................240
E 5.3.12 Category 12, Windshear Input Select...........................................................................................................241
E 5.3.13 Category 13, Input / Output Discrete Type Select .......................................................................................242
E 5.3.14 Category 14, Audio Output Level ................................................................................................................245
E 5.3.15 Category 15, Autorotation Threshold..........................................................................................................246
E 6 CONNECTOR INTERFACE...................................................................................................................................247
E 6.1 P
INOUT FOR FRONT CONNECTORS SORTED BY PIN NUMBER ................................................................................. 247
E 7 DEFINIT IONS ........................................................................................................................................................252
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MK XXII EGPWS Installation Manual
SECTION I
GENERAL INFORMATION
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MK XXII EGPWS Installation Manual
SECTION I – GENERAL INFORMATION
SECTION I – GENERAL INFORMATION............................................................................................16
1.1 I
NTRODUCTION.................................................................................................................................... 16
1.2 A
PPLICABILITY.................................................................................................................................... 16
1.3 H
OW TO USE THIS DOCUMENT ........................................................................................................... 16
1.4 R
EFERENCE DOCUMENTS .................................................................................................................... 17
1.5 D
ESCRIPTION OF EQUIPMENT...............................................................................................................18
1.5.1 MK XXII EGPWS Computer........................................................................................................ 19
1.5.2 MK XXII EGPWS Configuration Module.................................................................................... 19
1.5.3 GPS Antenna................................................................................................................................ 19
1.5.4 OAT Sensor..................................................................................................................................19
1.5.5 Smart Cable (PCMCIA Interface)................................................................................................20
1.6 T
ECHNICAL CHARACTERISTICS ........................................................................................................... 21
1.7 U
NITS SUPPLIED ..................................................................................................................................22
1.7.1 MK XXII EGPWS......................................................................................................................... 22
note 1: -0XX defines the Application software version......................................................................... 22
1.7.2 Configuration Module..................................................................................................................22
1.7.3 Smart Cable (PCMCIA Interface)................................................................................................22
1.8 I
NSTALLATION AND ACCESSORIES KITS .............................................................................................. 24
1.8.1 MK XXII EGPWS Installation Kits.............................................................................................. 24
1.8.2 RS-232 Cable............................................................................................................................... 24
1.8.3 Smart Cable................................................................................................................................. 24
1.8.4 Terrain Database Cards.............................................................................................................. 25
1.8.5 Flight History Card ..................................................................................................................... 25
1.9 A
CCESSORIES REQUIRED BUT NOT SUPPLIED.......................................................................................25
1.9.1 ARINC 453 Terrain Display wiring.............................................................................................25
1.9.2 GPS Antenna & cable.................................................................................................................. 26
1.9.3 Circuit Breaker............................................................................................................................ 26
1.9.4 Annunciators & Switch/Annunciators.......................................................................................... 26
1.9.4.1 GPWS Warning (red) P/TEST; switch/annunciator assembly............................................................... 26
1.9.4.2 GPWS Caution (amber) G/S CANCLD switch/annunciator assembly.................................................. 27
1.9.4.3 LOW ALT / ON switch/annunciator assembly...................................................................................... 27
1.9.4.4 TERR INHIB / ON switch/annunciator assembly................................................................................. 27
1.9.4.5 AUDIO INHIBIT / ON switch/annunciator assembly........................................................................... 27
1.9.4.6 GPWS INOP / TERR INOP annunciator assemblies............................................................................. 27
1.9.4.7 TERR DISPLAY / ON switch/annunciator assemblies.........................................................................27
1.10 COCKPIT SPEAKER (OPTIONAL)......................................................................................................... 27
1.11 T
OOLS REQUIRED.............................................................................................................................. 28
1.11.1 Crimping Tool - P1, P2, P3...................................................................................................... 28
1.11.2 Contact Positioner - P1, P2, P3................................................................................................28
1.11.3 Insertion/Removal Tool - P1, P2, P3........................................................................................ 28
1.11.4 Spare Contacts - P1, P2, P3...................................................................................................... 28
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1.12 LICENSE REQUIREMENTS................................................................................................................... 28
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MK XXII EGPWS Installation Manual
SECTION I – GENERAL INFORMATION
1.1 Introduction
The Honeywell MK XXII Enhanced Ground Proximity Warning System (MK XXII EGPWS)
provides alerts and warnings to prevent controlled flight into terrain (CFIT).
This Installation Manual must be used in conjunction with the Interface Description
Document (Appendix E) for the MK XXII Enhanced Ground Proximity Warning System (MK
XXII EGPWS) to select features and design the installation for this system.
It is assumed that the user of this document is familiar with avionics installation practices
and helicopter systems associated with the installation and operation of the MK XXII
EGPWS. It also assumes access to pertinent aircraft wiring diagrams, modification
records and manuals.
The information contained herein, together with general procedures outlined in FAA AC.43.13
must be followed carefully to assure a safe, electrically sound, certifiable and operational
installation.
The contents of this document are for information and reference only and must not be
construed as formal FAA approved work authorization.
1.2 Applicability
This manual is applicable only to MK XXII EGPWS computers with the following part number:
MK XXII 965-1590-0XX
Part numbers 965-1590-0XX include an internal GPS card.
1.3 How To Use This Document
Section 1 provides a system overview.
Section 2 provides mechanical installation and location information.
Section 3 provides information and instructions for selecting required features of the EGPWS.
Section 4 provides Configuration Module programming instructions.
Section 5 provides certification requirements.
Appendix A Customer Worksheet.
Appendix B Sample Wiring Diagrams.
Appendix C provides WinViews operation instructions.
Appendix D Vendor drawings.
Appendix E Interface Description Document
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1.4 Reference Documents
Following is a list of Honeywell reference documents:
965-1590-601 Product Specification for the MK XXII Enhanced Ground Proximity
Warning System (EGPWS)
993-1176-401 Interface Control Document (ICD) for the MK VI/VIII/XXII Enhanced
Ground Proximit y Wa rning S ystem
965-1590-206 Outline, MK XXII EGPWC
060-4326-000 EGPWS Terrain Database Airport Coverage List
060-4314-009 Generic RWFM Supplement For EGPWS
060-4314-200 Mk XXII Helicopter-Enhanced GPWS Pilot’s Guide
060-4314-006 General Flight Test Procedure
060-4167-167 Installation Ground Test Procedure for the Mk XXII EGPWS for
Rotary Wing Aircraft
060-4314-002 Failures Modes, Effects, and Safety Analysis
060-4314-011 Line Maintenance Manual
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1.5 Description of Equipment
The MK XXII EGPWS is a rack mount ground proximity warning (GPWS) and terrain display
(TAWS) computer. Some of the system features include:
♦
Basic Helicopter Ground Proximity Warning Modes 1-5
♦
Mode 6 Altitude, Bank Angle, and Tail Strike Callouts
♦
Terrain and Obstacle Awareness alert and display
♦
Terrain map with runways
♦
Internal GPS card
♦
Front loading updateable database
♦
External Configuration Module
♦
Internal heater blanket for operation outside of the heated area of the aircraft
Fig 1.0 MK XXII EGPWC
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1.5.1 MK XXII EGPWS Computer
The MK XXII EGPWS computer is available under P/N 965-1590-0XX with internal GPS. The MK
XXII EGPWS computer is intended for Helicopters and provides a mixture of analog and digital
interfaces. The type of supported displays is limited and includes some EFIS displays. The terrain
database included with the MK XXII EGPWS computer are North America, South America,
Europe, Eastern Europe, Afr ica, As ia, Pac if ic , Sout h Pac if ic , and Mid dle East regi ons and ar e
comprises of terrain data (6 arc second where available), all known airports, many heliports and
man-made obstacles (North America only).
1.5.2 MK XXII EGPWS Configuration Module
The MK XXII EGPWS Configuration Module is available under P/N 700-1710-001 (Included in
Installation Kits, see section 1.8). The MK XXII EGPWS uses a Configuration Module installed in
the aircraft wiring to store aircraft/EGPWS interface configuration.Specifically, the module comes
prewired and replaces part of the backshell of the (P2) connector that plugs into the front of the
MK XXII computer. The Configuration Module is read by the EGPWS only during power up. The
configuration is copied into Non Volatile Memory (NVM) of the EGPWS. The Configuration
Module is programmable via an RS-232 interface with the EGPWS. The contents of the
Configuration Module can also be read back via the same RS-232 interface.
1.5.3 GPS Antenna
EGPWS installations using the internal GPS require an active GPS antenna and cabling. The
GPS antenna should meet the following qualifications:
Frequency: 1575.42 MHz
Impedance: 50 ohms
Gain: 33dB max, 26.5 dB preferred
Power: 5 VDC
Qualification: TSO C129 or C129a or C144
The following GPS antennas are found to be compatible with the EGPWS internal GPS card.
Other GPS antennas may be found compatible, contact EGPWS engineering for assistance. It is
the responsibility of the OEM or owner/operator (and ultimately the regulatory authorities) to
assess the antenna acceptance criteria relative to ARINC, MIL, or other specifications.
King KA 91 P/N 071-01545-0200 TSO-C129
King KA 92 P/N 071-01553-0200 TSO-C129
Sensor Systems P/N S67-1575-52 TSO-C129, ARINC 743A
Sensor Systems P/N S67-1575-133 TSO-C129a, ARINC 743A
1.5.4 OAT Sensor
The OAT sensor is available from Computer Instruments Corp. (CIC) P/N 05257. The EGPWS
uses a separate OAT sensor (Outside Air Temperature) to measure outside air temperature on
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aircraft that do not have another compatible source of outside air temperature. Outside Air
Temperature is used by the EGPWS along with pressure altitude in computing Geometric
Altitude. If Outside Air Temperature is not available, Geometric Altitude is computed using
pressure altitude with a corresponding reduction in accuracy.
Geometric Altitude is computed by the EGPWS to reduce or eliminate errors potentially induced
in corrected barometric altitude by temperature extremes, non-standard altitude conditions, and
altimeter miss-sets. Geometric Altitude also allows continuous EGPWS operation in QFE
environments without crew intervention.
1.5.5 Smart Cable (PCMCIA Interface)
The EGPWS Smart Cable (part number 951-0386-001) is a removable PCMCIA card interface.
The Smart Card is compatible with any Honeywell supplied EGPWS PCMCIA style cards. The
purpose of the Smart Cable in the EGPWS system is for upload of software and databases and
also for download of EGPWS Flight History. The Smart Card loading operation will closely
emulate that of an ARINC 615 Data Loader.
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FIGURE 1-1 MK XXII EGPWS SMART CABLE
1.6 Technical Characteristics
MK XXII EGPWS
TSO Compliance: TSO-C92c, TSO-C151a, class A
Physical size (HxWxD): 6.20” x 3.04” x 10.30”
Weight: 3.9 pounds maximum
Mounting: Standard 3 inch King Radio rack
Temperature (operational): -55°C to +70°C (F2)
Altitude range: 55,000 feet (F2)
Cooling: No cooling necessary
Shock: No shock mounting required
Power Consumption (28 VDC): 3 Amps
9 watts – no warning
+7 watts – with warning over 8 ohm speaker
+3 watts – with GPS card
+49 watts – with heater blanket on
Configuration Module
TSO Compliance: same as MK XXII EGPWS
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Physical size: 2.68” x 1.51” x 0.32” (fits Positronic connector backshell)
Weight: <1 pound with connector and backshell
Mounting: Mounts to Positronic connector backshell
Temperature (operational): same as MK XXII EGPWS
Altitude range: same as MK XXII EGPWS
Cooling: No cooling necessary
Shock: No shock mounting required
Power Consumption (5 VDC): from MK XXII EGPWS
GPS Antenna Sensor
See Manufacturer’s specif ic at ions Ap pen dix D.
OAT Sensor
See Manufacturer’s specifications Appendix D.
1.7 Units Supplied
1.7.1 MK XXII EGPWS
The MK XXII EGPWS The part number for the units is as follows:
965-1590-0XX with Internal GPS card
note 1: -0XX defines the Application software version
1.7.2 Configuration Module
The MK XXII EGPWS Configuration Module is available in one version. When ordering the
Configuration Module, order part number 700-1710-001.
1.7.3 Smart Cable (PCMCIA Interface)
The MK XXII EGPWS Smart Cable is available in one version. The Smart Cable is used for Line
Maintenance, only one Smart Cable is required for an installation house or operator. When
ordering the Smart Cable, order part number 951-0386-001.
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1.8 Installation and Accessories Kits
NOTE: Not all installation kits are immediately available, contact Honeywell Order
Administration (425-885-8719) for availability.
1.8.1 MK XXII EGPWS Installation Kits
(A) New EGPWS installation with OAT and Internal GPS
The MK XXII EGPWS Installation Kit #1, P/N 755-7013-001, contains the following parts:
Vendor Name Vendor P/N Description QTY UM Honeywell P/N
Positronic Ind. DD78F1OJVLC-15 P1 connector 1 EA 440-1158-009
Positronic Ind. RD50F1OJVLC-15 P2 connector 1 EA 440-1233-001
Amphenol 79075 GPS Antenna connector 1 EA 440-1239-0 01
Honeywell 700-1710-001 Configuration Module 1 EA 700-1710-001
Bendix/King 071-04003-0002 Computer Mounting Tray 1 EA 405-0383-001
CIC 05257 OAT Sensor 1 EA 107-1049-001
CIC 05257-TOMK OAT mounting Kit 1 EA 107-1049-002
CIC 05257-TPIK OAT Connector Kit 1 EA 107-1049-003
(B) New EGPWS installation with Internal GPS
The MK XXII EGPWS Installation Kit #5, P/N 755-7013-005, contains the following parts:
Vendor Name Vendor P/N Description QTY UM Honeywell P/N
Positronic Ind. DD78F1OJVLC-15 P1 connector 1 EA 440-1158-009
Positronic Ind. RD50F1OJVLC-15 P2 connector 1 EA 440-1233-001
Amphenol 79075 GPS Antenna connector 1 EA 440-1239-0 01
Honeywell 700-1710-001 Configuration Module 1 EA 700-1710-001
Bendix/King 071-04003-0002 Computer Mounting Tray 1 EA 405-0383-001
1.8.2 RS-232 Cable
The MK XXII EGPWS RS-232 Cable can be ordered using the following part numbers:
NOTE: The RS-232 Cable can be built by the Installer/Operator per the description in Section 4.4.2
Vendor Name Vendor P/N Description QTY UM Honeywell P/N
Honeywell 704-2617-001 RS-232 Cable 1 EA 704-2617-001
1.8.3 Smart Cable
The MK XXII EGPWS Smart Cable can be ordered using the following part numbers:
Vendor Name Vendor P/N Description QTY UM Honeywell P/N
Honeywell 951-0386-001 Smart Cable 1 EA 951-0386-001
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1.8.4 Terrain Database Cards
The MK XII EGPWS Terrain Database Cards can be ordered using the following part numbers:
Vendor Name Vendor P/N Description QTY UM Honeywell P/N
Honeywell 424N AM North America 1 EA 718-1447-xxx
Honeywell 424 SA M South America 1 EA 718-1448-xxx
Honeywell 424EUR Europe 1 EA 718-1449-xxx
Honeywell 424EEU Eas tern Eur o pe 1 EA 718-1450-xxx
Honeywell 424AFR Africa 1 EA 718-1451-xxx
Honeywell 424PAC Pacific 1 EA 718-1452-xxx
Honeywell 424ASI Asia 1 EA 718-1453-xxx
Honeywell 424SP A South Pacific 1 EA 718-1457-xxx
Honeywell 424MES Middle East 1 EA 718-1458-xxx
Honeywell 402-6075-xxx Label, TDB Front Panel 1 EA 402-6075-xxx
1.8.5 Flight History Card
The Flight History Card is a PCMCIA card that has been loaded with a down load instruction file
to allow the down loading of flight history data from an EGPWS. Flight History files contain status
information, fault history and flight data from 20 seconds prior to 10 seconds after a EGPWS
caution or warning event. The card is used to aid in troubleshooting systems faults and or
nuisance warnings.
The MK XXII EGPWS Flight History Card can be ordered using the following part numbers:
Vendor Name Vendor P/N Description QTY UM Honeywell P/N
Honeywell * Flight History Download 1 EA *
* For flight history download cards call Honeywell GPWS Hotline 1 800 813-2099
1.9 Accessories Required but not Supplied
1.9.1 ARINC 453 Terrain Displ ay wiring
The Terrain display wiring (ARINC 453) must meet the display manufacturer’s specifications
including termination method. ARINC 453 buss wiring must meet the following requirements:
• Cable length must be less than 300 feet (91.4 meters).
• Wire to wire capacitance must not exceed 50 pF/foot.
• Shielded twisted pair with not less than one twist per inch.
• Impedance of 78 ohms ±10% at 1 MHz.
Vendor Name Vendor P/N Description QTY UM Honeywell P/N
Pic Wire&Cable D620224 ARINC 453 cable A/R EA
Pic Wire&Cable D5102QX Hi Temp Quadraxial A/R EA
Pic Wire&Cable D771553 MIL-STD 1553 Data Bus A/R EA
ECS 4122021 ARINC 453 cable A/R EA
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Vendor Name Vendor P/N Description QTY UM Honeywell P/N
Emteq D 07002-100 ARINC 453 Cable A/R EA
M17/176-00002 M ilitary Specification A/R EA
1.9.2 GPS Antenna & cable
The GPS Antenna & cable can be ordered from their manufacturers using the following part
numbers:
Vendor Name Vendor P/N Description QTY UM Honeywell P/N
Bendix/King 071-01545-0200 KA 91 GPS Antenn a 1 EA
Bendix/King 071-01553-0200 KA 92 GPS Antenn a 1 EA 300-1147-001
Comant CI 405-2 KA 92 GPS Antenna 1 EA 300-1147-001
Bendix/King 050-03318-0000 Antenna Installation Kit OPT EA 405-0432-001
Sensor Systems
Sensor Systems
Sensor Systems
Thermax M17/128-RG400 Coax Cable, RG400 A/R EA
Amp 225554-6 TNC Angle Plug, Male 1 EA 440-1239-001
Amphenol 79075 TNC Angle Plug, Male 1 EA 440-1239-001
S67-1575-38 S67 GPS Antenna 1 EA
S67-1575-52 S67 GPS Antenna 1 EA
S67-1575-133 S67 GPS Antenna 1 EA
Coax Cable, RG-142 A/R EA
1.9.3 Circuit Breaker
The Circuit Breaker needs to be a 3 Amp delayed action circuit breaker.
Vendor Name Vendor P/N Description QTY UM Honeywell P/N
Klixon (T.I.) 7277-2-3 3 Amp Circuit Breaker,
EGPWS power +28
Klixon (T.I.) 7277-2-1 1 Amp Circuit Breaker,
lamp power +28
1EA
1EA
1.9.4 Annunciators & Switch/Annunciators
The devices shown below are switch/annunciators and are representative of those used in some
installations. The installer/customer is cautioned to verify regulatory approval of the annunciation
devices installed. See Appendix D for Vendors.
1.9.4.1 GPWS Warning (red) P/TES T; s wi tch/a nnuncia tor assem bly
The ‘GPWS’ annunciator provides visual indication of an EGPWS alert. The GPWS warning (red)
annunciator also has a switch that is used to manually initiate EGPWS Self Test.
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1.9.4.2 GPWS Caution (amber) G/S C ANCLD switch/annunciator assembly.
The ‘GPWS caution annunciator provides visual indication of an EGPWS alert. The EGPWS
caution (amber) annunciator also has a switch that is used to manually inhibit EGPWS Mode 5
glideslope alerts. The bottom half of the annunciator provides visual indication that the mode 5
glideslope alerts have been canceled.
1.9.4.3 LOW ALT / ON switch/annunciator assembly
The LOW ALT / ON switch/annunciator provides for manual selection of low altitude mode and
visual indication that the Mk XXII EGPWS is in low altitude mode.
1.9.4.4 TERR INHIB / ON switch/annunciator assembly
The ‘TERR INHIBIT’ switch/annunciator provides for manual selection of terrain inhibit mode and
visual indication that the EGPWS Terrain functions have been inhibited.
1.9.4.5 AUDIO INHIBIT / ON switch/annunciator assembly
The ‘AUDIO INHIBIT’ switch/annunciator provides for manual selection of audio inhibit mode and
visual indication that the EGPWS mode 6 functions have been inhibited.
1.9.4.6 GPWS INOP / TERR INOP annunciator assemblies
The ‘GPWS INOP’ annunciator provides visual indication that the EGPWS GPWS modes have a
disabled function.
The ‘TERR INOP’ annunciator provides visual indication that the EGPWS Terrain modes have a
disabled function.
1.9.4.7 TERR DISPLAY / ON switch/annunciator assemblies
The ‘TERR DISPLAY’ switch/annunciator provides for manual selection of the terrain display and
visual indication that the EGPWS Terrain Display has been selected for the associated display.
1.10 Cockpit Speaker (Optional)
The MK XXII EGPWS can interface to an 8 ohm audio speaker for cockpit annunciation of aural
alerts.
Vendor Name Vendor P/N Description QTY UM Honeywell P/N
Quam 30A05Z8 Audio Sp eaker 1 EA
Utah SP-3A Audio Speaker 1 EA
CTS 4AC3 Audio Speaker 1 EA 300-0218-002
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1.11 Tools Required
1.11.1 Crimping Tool - P1, P2, P3
Description UM QTY Vendor Name & Part Number
Hand Crimping Tool EA 1 Positronic Ind. 9507
Hand Crimping Tool EA 1 Daniels AFM8
Hand Crimping Tool EA 1 Military M22520/2-1
1.11.2 Contact Positioner - P1, P2, P3
Description UM QTY Vendor Name & Part Number
Contact Positioner, Sock et P1 EA 1 Positronic Ind. 9502-3
Contact Positioner, Socket P1 EA 1 Daniels K41 (for 22 to 28 AWG)
Contact Positioner, Socket P1 EA 1 Military M22520/2-06
Contact Positioner, Sock et P2 EA 1 Positronic Ind. 9502-5
Contact Positioner, Socket P2 EA 1 Daniels K13-1 (20-24 AWG)
Contact Positioner, Socket P2 EA 1 Military M22520/2-08
Contact Positioner, Pin P3 EA 1 Positronics 9502-4
Contact Positioner, Pin P3 EA 1 Daniles K42 (22-28 AWG)
Contact Positioner, Pin P3 EA 1 Military M22520/2-09
1.11.3 Insertion/Removal Tool - P1, P2, P3
Description UM QTY Vendor Name & Part Number
Removal Tool P1, P3 EA 1 Daniels DRK 95-22M
Removal Tool P1, P3 EA 1 Military M81969/8-02
Removal Tool P2 EA 1 Daniels DRK145
Insertion Tool P1, P3 EA 1 Daniels DAK 95-22M
Insertion Tool P1, P3 EA 1 Military M81969/8-01
Insertion Tool P2 EA 1 Daniels DAK145
Insertion/Removal T ool P1, P3 EA 1 Military M81969/1-04
Insertion/Removal Tool P2 EA 1 Military M81969/1-02
1.11.4 Spare Contacts - P1, P2, P3
Description Mil Spec Part Number
Contacts (P1) socket M39029/57-354 22-28 GA Wire
Contacts (P2) socket M39029/63-368 20-24 GA Wire
Contacts (P3) Pin M39029/58-360 22-28 GA Wire
1.12 License Requirements
There are no Radio license requirements for the MK XXII EGPWS.
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SECTION II
INSTALLATION
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