Honeywell MKXXII User Manual

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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Honeywell

MK XXII EGPWS Installation Manual

This document is an unpublished work.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 property of Honeywell International Inc., and is provided to the recipient in confidence on a “need to know” basis. Your use of this document is strictly limited to a legitimate business purpose requiring the information contained therein. Your use of this document constitutes acceptance of these terms.

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Honeywell

MK XXII EGPWS Installation Manual

Typed names constitute approval signatures. Actual signatures are on file at Honeywell in Redmond, WA.

DRAWN	Dennis Martin		12/8/00
CHECK	Sara Stark		12/8/00
ENGR	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

S. Wright

8/9/01

D. Martin

Reason: 01 Severity: 10

ALL

B

Added Software –010 Revisions.

3/22/02

D. Martin

Reason: 01

Severity: 10

3/22/02

R Gilliland

ALL

C

Added Software –011 Revisions.

6/07/02

D Martin

Reason: 01

Severity: 10

6/7/02

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 INTRODUCTION ....................................................................................................................................	16
1.2 APPLICABILITY ....................................................................................................................................	16
1.3 HOW TO USE THIS DOCUMENT ...........................................................................................................	16
1.4 REFERENCE DOCUMENTS ....................................................................................................................	17
1.5 DESCRIPTION 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 TECHNICAL CHARACTERISTICS ...........................................................................................................	21
1.7 UNITS 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 INSTALLATION 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 ACCESSORIES 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 TOOLS REQUIRED ..............................................................................................................................	2 8
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 LICENSE REQUIREMENTS ...................................................................................................................	28
SECTION II - INSTALLATION ...................................................................................................... ........................	33
2.1 INTRODUCTION ....................................................................................................................................................	33
2.2 UNPACKING AND INSPECTING THE EQUIPMENT ...................................................................................................	33
2.3 EQUIPMENT 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 INTRODUCTION ....................................................................................................................................	57
3.2 SYSTEM 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 CONFIGURABLE 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 INTRODUCTION ..................................................................................................................................	109
4.2 HARNESS CHECKOUT AND POWER CHECK ........................................................................................	109
4.3 UNIT INSTALLATION ..........................................................................................................................	109
4.4 EGPWC INITIALIZATION 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 CONFIGURATION MODULE PROGRAMMING .......................................................................................	111
4.5.1 CUW and CMR Commands .......................................................................................................	113
4.5.2 Configuration Module Reprogramming.....................................................................................	114
4.6 REGIONAL 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 INTRODUCTION .................................................................................................................................	124
5.2 CERTIFICATION 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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		MK VI MK VIII EGPWS Installation Design Guide
APPENDIX C.....................................................................................................................			....................................................143
WINVIEWS OPERATION INSTRUCTIONS ................................................................................................			...................143
APPENDIX D..................................................................................................................... .......................			149
VENDOR DRAWINGS................................................................................................................ ............			149
D 1-0 VENDOR 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
INSTALLATION ...........................................................................................................CONSIDERATIONS:			159
D1-3 ................................................................................................................		Aerospace Optics	160
AEROSPACE ....................................................................................................................OPTICS INC			160
LED LIGHTING ......................................................................................................................................			160
INTRODUCTION .................................................................................................................................................................			166
E 1	PART ..........................................................................................................................................................NUMBER		166
E 2	PURPOSE...................................................................................................................................................................		166
E 3	SYSTEM ..................................................................................................................................................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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E 4.2.17.1			ARINC 429 Output Bus ................................................................................................. ...........................	177
E 4.2.17.2			ARINC 453 Output Bus ................................................................................................. ...........................	178
E 4.2.18		FRONT PANEL TEST INTERFACE........................................................................................................................		178
E 4.2.18.1			RS-232 MAINTENANCE 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		FRONT PANEL STATUS INDICATORS .................................................................................................................		179
E 5 AIRCRAFT APPLICATION DATA .......................................................................................................................				180
E 5.1		CONFIGURATION TYPES........................................................................................................................................		180
E 5.2		CONFIGURATION 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		PINOUT FOR FRONT CONNECTORS SORTED BY PIN NUMBER .................................................................................		247
E 7	DEFINITIONS ........................................................................................................................................................			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 INTRODUCTION ....................................................................................................................................			16
1.2 APPLICABILITY ....................................................................................................................................			16
1.3 HOW TO USE THIS DOCUMENT ...........................................................................................................			16
1.4 REFERENCE DOCUMENTS ....................................................................................................................			17
1.5 DESCRIPTION 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 TECHNICAL CHARACTERISTICS ...........................................................................................................			21
1.7 UNITS 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 INSTALLATION 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 ACCESSORIES 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 TOOLS REQUIRED ..............................................................................................................................			2 8
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 ...................................................................................................................

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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 Docu ment

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 Proximity Warning System

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 Equipm ent

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 Comp uter

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, Africa, Asia, Pacific, South Pacific, and Middle East regions and are 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 Conf iguration 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 Characteris tics

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 specifications Appendix 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 Acces sories Kits

NOTE: Not all installation kits are immediately available, contact Honeywell Order

Administration (425-885-8719) for availability.

1.8.1 MK XXII EGPWS Insta llation 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	440-1239-001
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	440-1239-001
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 Card s

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	424NAM	North America	1	EA	718-1447-xxx
Honeywell	424SAM	South America	1	EA 718-1448-xxx
Honeywell	424EUR	Europe	1	EA	718-1449-xxx
Honeywell	424EEU	Eastern Europe	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	424SPA	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 [phone]

1.9 Accessories Required but not Supplied

1.9.1 ARINC 453 Terrain Dis play 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	Military 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 Antenna	1	EA
Bendix/King	071-01553-0200	KA 92 GPS Antenna	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	S67-1575-38	S67 GPS Antenna	1	EA
Sensor Systems	S67-1575-52	S67 GPS Antenna	1	EA
Sensor Systems	S67-1575-133	S67 GPS Antenna	1	EA
Thermax	M17/128-RG400	Coax Cable, RG400	A/R	EA
		Coax Cable, RG-142	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

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,	1	EA
		EGPWS power +28
Klixon (T.I.)	7277-2-1	1 Amp Circuit Breaker,	1	EA
		lamp power +28

1.9.4 Annunciators & Switc h/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; switch/annunciator assembly

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 CANCLD 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/annu nciator 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/an nunciator 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 a nnunciator 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 (Opti onal)

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 Speaker	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, P 2, 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 - P 1, P2, P3

	Description	UM	QTY	Vendor Name & Part Number
	Contact Positioner, Socket 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, Socket 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 Too l	- 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 Tool P1, P3	EA	1	Military	M81969/1-04
	Insertion/Removal Tool P2	EA	1	Military	M81969/1-02
	1.11.4 Spare Contacts - P1, P 2, 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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