Honeywell MK VI, MK VIII User Manual

Airlines & Avionics Products Honeywell Inc. 15001 N.E. 36th Street Redmond, WA 98052

MK VI MK VIII

Enhanced Ground Proximity Warning System

(Class A TAWS)

Installation Design Guide

Hardware/Software Part Numbers:

965-1180-020 965-1190-020 965-1210-020 965-1220-020

Release Date: July 14, 2003

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MK VI MK VIII EGPWS Installation Design Guide

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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Redmond, WA.

Honeywell

MK VI MK VIII EGPWS Installation Design Guide

SHEET

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MK VI MK VIII EGPWS Installation Design Guide

SECTION I – GENERAL INFORMATION ..........................................................................................................13

1.1 I

NTRODUCTION.........................................................................................................................................................13

1.2 A

PPLICABILITY.........................................................................................................................................................13

1.3 H

OW TO USE THIS DOCUMENT ................................................................................................................................13

1.4 R

EFERENCE DOCUMENTS .........................................................................................................................................14

1.5 D

ESCRIPTION OF EQUIPMENT ...................................................................................................................................15

1.5.1 MK VI EGPWS Computer .................................................................................................................................... 15

1.5.2 MK VIII EGPWS Computer..................................................................................................................................15

1.5.3 MK VI/MK VIII EGPWS Configuration Module ..................................................................................................15

1.5.4 GPS Antenna and Cabling....................................................................................................................................16

1.5.5 OAT Sensor ..........................................................................................................................................................17

1.5.6 Smart Cable (PCMCIA Interface)........................................................................................................................17

1.6 T

ECHNICAL CHARACTERISTICS ................................................................................................................................18

1.7 U

NITS SUPPLIED.......................................................................................................................................................18

1.7.1 MK VI EGPWS .....................................................................................................................................................18

1.7.2 MK VIII EGPWS.................................................................................................................................................19

1.7.3 Configuration Module ........................................................................................................................................19

1.7.4 Smart Cable (PCMCIA Interface) ...................................................................................................................... 19

1.8 I

NSTALLATION KITS AND ACCESSORIES .................................................................................................................19

1.8.1 MK VI/MK VIII EGPWS Installation Kits ..........................................................................................................19

1.8.2 RS-232 Cable......................................................................................................................................................20

1.8.3 Smart Cable........................................................................................................................................................20

1.8.4 Terrain Database Cards.....................................................................................................................................20

1.8.5 Flight History Card ............................................................................................................................................20

1.9 A

CCESSORIES NOT SUPPLIED ..................................................................................................................................20

1.9.1 ARINC 453 Terrain Display wiring....................................................................................................................20

1.9.2 GPS Antenna & Cable........................................................................................................................................21

1.9.3 Circuit Breaker...................................................................................................................................................21

1.9.4 Annunciators & Switch/Annunciators ................................................................................................................22

1.9.5 Cockpit Speakers ................................................................................................................................................23

1.9.6 Temperature Probes ...........................................................................................................................................23

1.10 T

OOLS REQUIRED .................................................................................................................................................24

1.10.1 Crimping Tool - P1, P2, P3.............................................................................................................................24

1.10.2 Contact Positioner - P1, P2, P3 ......................................................................................................................24

1.10.3 Insertion/Removal Tool - P1, P2, P3............................................................................................................... 24

1.10.4 Spare Connectors and Contacts - P1, P2, P3..................................................................................................25

1.11 L

ICENSE REQUIREMENTS......................................................................................................................................25

SECTION II - INSTALLATION ............................................................................................................................. 29

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2.1 INTRODUCTION....................................................................................................................................................... 29

2.2 U

NPACKING AND INSPECTING THE EQUIPMENT ......................................................................................................29

2.3 E

QUIPMENT INSTALLATION ....................................................................................................................................29

2.3.1 General...............................................................................................................................................................29

2.3.2 MK VI/MK VIII Computer Location...................................................................................................................29

2.3.3 MK VI/ MK VIII Computer Installation..............................................................................................................30

2.3.4 Configuration Module Location .........................................................................................................................31

2.3.5 Configuration Module Installation.....................................................................................................................31

2.3.6 GPS Antenna location.........................................................................................................................................40

2.3.7 GPS Antenna Installation ...................................................................................................................................40

2.3.8 OAT Sensor Location..........................................................................................................................................40

2.3.9 OAT Sensor Installation .....................................................................................................................................40

2.3.10 Cockpit Lights...................................................................................................................................................40

2.3.10.1 Description........................................................................................................................................................................ 41

2.3.10.2 Location............................................................................................................................................................................ 42

SECTION III – SYSTEM PLANNING................................................................................................................... 51

3.1 I

NTRODUCTION.......................................................................................................................................................51

3.2 S

YSTEM WIRING/ ELECTRICAL INTERFACES .......................................................................................................... 51

3.2.1 Primary Power Input..........................................................................................................................................51

3.2.2 Chassis Ground ..................................................................................................................................................52

3.2.3 GPS Antenna ......................................................................................................................................................52

3.2.4 Analog and Digital Inputs ..................................................................................................................................52

3.2.5 Discrete Inputs....................................................................................................................................................52

3.2.6 Serial Outputs.....................................................................................................................................................52

3.2.7 Audio Output.......................................................................................................................................................53

3.2.8 Discrete Outputs.................................................................................................................................................53

3.2.9 Configuration Module ........................................................................................................................................53

3.3 C

ATEGORY 1 - AIRCRAFT / MODE TYPE SELECT ...................................................................................................54

3.3.1 Aircraft / Mode Type...........................................................................................................................................54

3.3.2 Mode 1 type ........................................................................................................................................................54

3.3.3 Mode 2 type ........................................................................................................................................................54

3.3.4 Mode 3 type ........................................................................................................................................................55

3.3.5 Mode 4 type ........................................................................................................................................................55

3.3.6 Bank Angle Type.................................................................................................................................................55

3.3.7 Runway Length (MK VIII EGPWS only) ............................................................................................................56

3.3.8 Instructions.........................................................................................................................................................56

3.4 C

ATEGORY 2 – AIR DATA INPUT SELECT ...............................................................................................................57

3.4.1 Analog (Cat. 2 ID 0, 3, 4, 11, 12) ....................................................................................................................... 57

3.4.2 Digital – ARINC 429 (Cat. 2 ID 5, 1, 6, 13).......................................................................................................59

3.4.3 Digital –ARINC 575 (Cat. 2 ID 2)......................................................................................................................60

3.4.4 Shadin 2000 (Cat. 2 ID 10).................................................................................................................................61

3.4.5 Digital – ARINC 429 Dual IOC Buses (Cat. 2. ID 255).....................................................................................62

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3.4.6 Instructions.........................................................................................................................................................62

3.5 C

ATEGORY 3 – POSITION INPUT SELECT ................................................................................................................63

3.5.1 ARINC 743 Format.............................................................................................................................................63

3.5.2 GPS Altitude (Label 076) Reference...................................................................................................................63

3.5.3 North-South East-West Velocity labels...............................................................................................................63

3.5.4 ARINC 429 BUS (Cat. 3 ID 0,1,4,5,10-13).........................................................................................................64

3.5.5 RS-232 Transmit-Receive, 9600 baud (Cat. 3 ID 3)...........................................................................................65

3.5.6 Dual ARINC 429 BUS (Cat. 3 ID 253 & 255).................................................................................................... 66

3.5.7 Instructions.........................................................................................................................................................66

3.6 C

ATEGORY 4 – ALTITUDE CALLOUTS ....................................................................................................................67

3.7 C

ATEGORY 5 – AUDIO MENU SELECT ....................................................................................................................68

3.7.1 Audio Menu Selection.........................................................................................................................................68

3.7.2 Instructions.........................................................................................................................................................68

3.8 C

ATEGORY 6 – TERRAIN DISPLAY SELECT.............................................................................................................69

3.8.1 TAD & TCF Selection.........................................................................................................................................69

3.8.2 Terrain Display Configuration Group................................................................................................................70

3.8.3 Display Input Control Group..............................................................................................................................70

3.8.4 Output 429 Bus Group........................................................................................................................................71

3.8.5 Instructions.........................................................................................................................................................71

3.8.6 Sample Display Schematics................................................................................................................................71

3.9 C

ATEGORY 7 – OPTIONS SELECT GROUP #1........................................................................................................... 88

3.9.1 Steep Approach...................................................................................................................................................88

3.9.2 TA&D Alternate Pop-up.....................................................................................................................................88

3.9.3 Peaks Mode ........................................................................................................................................................88

3.9.4 Obstacle Awareness............................................................................................................................................88

3.9.5 Bank Angle Callout Enabling.............................................................................................................................89

3.9.6 Flap Reversal......................................................................................................................................................89

3.9.7 GPS Altitude Reference ......................................................................................................................................89

3.9.8 Instructions.........................................................................................................................................................90

3.10 C

ATEGORY 8 – RADIO ALTITUDE INPUT SELECT..................................................................................................91

3.10.1 Radio Altitude Input..........................................................................................................................................91

3.10.2 Decision Height Discrete Input ........................................................................................................................ 91

3.10.3 Digital Radio Altitude Interface (Cat. 8 ID 2).................................................................................................. 91

3.10.4 Analog Radio Altitude Interface (Cat. 8 ID 0,1,3,4).........................................................................................92

3.10.5 Digital – ARINC 429 Dual IOC Buses (Cat. 8 ID 251- 255)............................................................................92

3.10.6 Instructions .......................................................................................................................................................93

3.11 C

ATEGORY 9 – NAVIGATION INPUTS SELECT.......................................................................................................94

3.11.1 Navigation Inputs Select (Glideslope & Localizer Inputs) ...............................................................................94

3.11.2 Glideslope Validity ........................................................................................................................................... 94

3.11.3 Localizer Validity .............................................................................................................................................94

3.11.4 ILS Tuned Discrete Input #1 (+28V) and #2 (GND) ........................................................................................ 94

3.11.5 Analog Glideslope Interface (Cat. 9 ID 0,1,5)..................................................................................................95

3.11.6 Digital Glideslope / Localizer / ILS Select Interface (Cat. 9 ID 2,3,4).............................................................96

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3.11.7 Digital – ARINC 429 Dual IOC buses (Cat. 9 ID 250 - 255)...........................................................................96

3.11.8 Instructions .......................................................................................................................................................97

3.12 C

ATEGORY 10 – ATTITUDE INPUT SELECT ...........................................................................................................98

3.12.1 Roll Angle .........................................................................................................................................................98

3.12.2 Analog Pitch & Roll Angle (Synchro) (Cat. 10 ID 0,2,4) .................................................................................98

3.12.3 Digital Pitch & Roll Angle (ARINC 429 High Speed) (Cat. 10 ID 5 & 6)........................................................99

3.12.4 Digital – ARINC 429 Dual IOC buses (Cat. 10 ID 253 & 255) ....................................................................... 99

3.12.5 Instructions .......................................................................................................................................................99

3.13 C

ATEGORY 11 – HEADING INPUT SELECT ..........................................................................................................100

3.13.1 Magnetic Heading ..........................................................................................................................................100

3.13.2 Analog Heading (Synchro) (Cat. 11 ID 0)...................................................................................................... 100

3.13.3 Digital – ARINC 429 AHRS Input (Cat. 11 ID 2 & 3).................................................................................... 101

3.13.4 Digital – ARINC 429 Dual IOC buses (Cat. 11 ID 254 & 255) ..................................................................... 101

3.13.5 Instructions .....................................................................................................................................................101

3.14 C

ATEGORY 12 – WINDSHEAR INPUT SELECT ..................................................................................................... 102

3.14.1 No Windshear ................................................................................................................................................. 102

3.14.2 Dual ARINC 429 BUS (Cat. 14 ID 253,254,255)...........................................................................................102

3.14.3 Instructions .....................................................................................................................................................102

3.15 C

ATEGORY 13 – INPUT / OUTPUT DISCRETE TYPE SELECT ................................................................................103

3.15.1 Input Discretes................................................................................................................................................103

3.15.1.1 Glideslope Inhibit Discrete ............................................................................................................................................. 103

3.15.1.2 Landing Flaps Discrete ................................................................................................................................................... 103

3.15.1.3 Audio Inhibit Discrete..................................................................................................................................................... 104

3.15.1.4 Landing Gear Discrete.................................................................................................................................................... 104

3.15.1.5 Glideslope Cancel Discrete............................................................................................................................................. 106

3.15.1.6 Momentary Flap Override Discrete................................................................................................................................. 106

3.15.1.7 Mode 6 Low Volume Discrete........................................................................................................................................ 106

3.15.1.8 Autopilot Engaged Discrete............................................................................................................................................ 107

3.15.1.9 Terrain Awareness and TCF Inhibit Discrete.................................................................................................................. 107

3.15.1.10 Self Test Discrete.......................................................................................................................................................... 107

3.15.1.11 Steep Approach Discrete #2.......................................................................................................................................... 108

3.15.1.12 GPWS INHIBIT Discrete (alternate action).................................................................................................................. 108

3.15.2 Output Discretes.............................................................................................................................................108

3.15.2.1 Lamp Format................................................................................................................................................................... 109

3.15.2.2 Flashing Lamps............................................................................................................................................................... 109

3.15.2.3 GPWS INOP Discrete..................................................................................................................................................... 109

3.15.2.4 TAD INOP Discrete........................................................................................................................................................ 109

3.15.2.5 GPWS Warning Discrete ................................................................................................................................................ 109

3.15.2.6 GPWS Alert Discrete...................................................................................................................................................... 110

3.15.2.7 Glideslope Cancel’d Discrete.......................................................................................................................................... 110

3.15.2.8 Flap Override Discrete.................................................................................................................................................... 110

3.15.2.9 Steep Approach Discrete................................................................................................................................................. 110

3.15.2.10 Audio On Discrete (TCAS/TAS Inhibit)....................................................................................................................... 110

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3.15.2.11 Terrain Display Select #1 & #2 Discrete....................................................................................................................... 111

3.15.2.12 Terrain Pop up Discrete ................................................................................................................................................ 112

3.15.3 Instructions .....................................................................................................................................................113

3.16 C

ATEGORY 14 – AUDIO OUTPUT LEVEL ............................................................................................................ 113

3.16.1 Instructions .....................................................................................................................................................113

3.17 C

ATEGORY 15 - 17 – UNDEFINED INPUT SELECTS ............................................................................................. 114

3.17.1 Undefined Input Select....................................................................................................................................114

3.17.2 Instructions .....................................................................................................................................................114

SECTION IV – CONFIG MODULE PROGRAMMING AND REGIONAL TDB LOADING ......................117

4.1 I

NTRODUCTION.....................................................................................................................................................117

4.2 H

ARNESS CHECKOUT AND POWER CHECK ...........................................................................................................117

4.3 U

NIT INSTALLATION.............................................................................................................................................117

4.4 EGPWC I

NITIALIZATION AND CONFIGURATION ..................................................................................................117

4.4.1 RS-232 Communication with the MK VI/VIII EGPWS ..................................................................................... 117

4.4.2 EGPWC Front Panel Test Connector...............................................................................................................118

4.4.3 WinVIEWS ........................................................................................................................................................119

4.4.4 WinVIEWS Operation....................................................................................................................................... 119

4.5 C

ONFIGURATION MODULE PROGRAMMING..........................................................................................................119

4.5.1 CUW and CMR Commands..............................................................................................................................121

4.5.2 Configuration Module Reprogramming ........................................................................................................... 122

4.6 T

ERRAIN DATABASE LOADING.............................................................................................................................122

4.6.1 Effectivity..........................................................................................................................................................122

4.6.2 Description .......................................................................................................................................................123

4.6.3 Approval ...........................................................................................................................................................123

4.6.4 Material – Cost and Availability ......................................................................................................................123

4.6.5 Accomplishment Instructions............................................................................................................................ 123

4.6.6 Verification of the Terrain Database Version ..................................................................................................125

SECTION V – CERTIFICATION......................................................................................................................... 128

5.1 I

NTRODUCTION.....................................................................................................................................................128

5.2 C

ERTIFICATION PROCEDURE ................................................................................................................................128

5.2.1 Equipment Compatibility ..................................................................................................................................128

5.2.2 Equipment Location..........................................................................................................................................128

5.2.3 FAA Requirements............................................................................................................................................ 128

5.2.4 Ground Test ......................................................................................................................................................128

5.2.5 Flight Manual Revision ....................................................................................................................................128

5.2.6 Flight Test.........................................................................................................................................................128

5.2.7 Pilots Guide......................................................................................................................................................129

5.2.8 Failure Modes, Effects, and Safety Analysis.....................................................................................................129

SECTION VI - MK VI GPWS TO MK VI/VIII EGPWS SIGNAL MAPPING ...............................................131

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APPENDIX A - CUSTOMER WORKSHEET .....................................................................................................137

APPENDIX B - SAMPLE WIRING DIAGRAMS ............................................................................................... 141

APPENDIX C – WINVIEWS OPERATION INSTRUCTIONS.........................................................................146

APPENDIX D - VENDOR CONTACT INFORMATION...................................................................................150

APPENDIX E – INTERFACE DESCRIPTION DOCUMENT .......................................................................... 153

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SECTION I

GENERAL INFORMATION

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SECTION I – GENERAL INFORMATION

SECTION I – GENERAL INFORMATION ..................................................................................................................... 13

1.1 I

NTRODUCTION.............................................................................................................................................................. 13

1.2 A

PPLICABILITY.............................................................................................................................................................. 13

1.3 H

OW TO USE THIS DOCUMENT ..................................................................................................................................... 13

1.4 R

EFERENCE DOCUMENTS .............................................................................................................................................. 14

1.5 D

ESCRIPTION OF EQUIPMENT ........................................................................................................................................ 15

1.5.1 MK VI EGPWS Computer ..................................................................................................................................... 15

1.5.2 MK VIII EGPWS Computer................................................................................................................................... 15

1.5.3 MK VI/MK VIII EGPWS Configuration Module ................................................................................................... 15

1.5.4 GPS Antenna and Cabling..................................................................................................................................... 16

1.5.5 OAT Sensor ........................................................................................................................................................... 17

1.5.6 Smart Cable (PCMCIA Interface)......................................................................................................................... 17

1.6 T

ECHNICAL CHARACTERISTICS ..................................................................................................................................... 18

1.7 U

NITS SUPPLIED............................................................................................................................................................ 18

1.7.1 MK VI EGPWS ...................................................................................................................................................... 18

1.7.2 MK VIII EGPWS ................................................................................................................................................... 19

1.7.3 Configuration Module ........................................................................................................................................... 19

1.7.4 Smart Cable (PCMCIA Interface)......................................................................................................................... 19

1.8 I

NSTALLATION KITS AND ACCESSORIES........................................................................................................................ 19

1.8.1 MK VI/MK VIII EGPWS Installation Kits............................................................................................................. 19

1.8.2 RS-232 Cable......................................................................................................................................................... 20

1.8.3 Smart Cable........................................................................................................................................................... 20

1.8.4 Terrain Database Cards........................................................................................................................................ 20

1.8.5 Flight History Card............................................................................................................................................... 20

1.9 A

CCESSORIES NOT SUPPLIED......................................................................................................................................... 20

1.9.1 ARINC 453 Terrain Display wiring....................................................................................................................... 20

1.9.2 GPS Antenna & Cable........................................................................................................................................... 21

1.9.3 Circuit Breaker...................................................................................................................................................... 21

1.9.4 Annunciators & Switch/Annunciators ................................................................................................................... 22

1.9.5 Cockpit Speakers ................................................................................................................................................... 23

1.9.6 Temperature Probes.............................................................................................................................................. 23

1.10 T

OOLS REQUIRED........................................................................................................................................................ 24

1.10.1 Crimping Tool - P1, P2, P3................................................................................................................................ 24

1.10.2 Contact Positioner - P1, P2, P3 ......................................................................................................................... 24

1.10.3 Insertion/Removal Tool - P1, P2, P3.................................................................................................................. 24

1.10.4 Spare Connectors and Contacts - P1, P2, P3..................................................................................................... 25

1.11

LICENSE REQUIREMENTS............................................................................................................................................. 25

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SECTION I – GENERAL INFORMATION

1.1 Introductio n

The Honeywell MK VI/MK VIII Enhanced Ground Proximity Warning System (MK VI/MK VIII EGPWS) provides

alerts and warnings to prevent controlled flight into terrain (CFIT).

This Installation Design Guide must be used in conjunction with the Interface Description Document

(Appendix E) for the MK VI/MK VIII Enhanced Ground Proximity Warning System (MK VI/MK VIII 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 aircraft

systems associated with the installation and operation of the MK VI/MK VIII 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 Applicabilit y

This manual is applicable only to MK VI/MK VIII EGPWS computers with the following part numbers:

MK VI

965-1180-020

965-1190-020

MK VIII

965-1210-020

965-1220-020

Part numbers 965-1190-xxx and 965-1220-xxx include an internal GPS card.

1.3 How To Us e 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.

Section 6 provides a pin to pin comparison of the classic MK VI GPWS to the MK VI/MK VIII EGPWS.

Appendix A Customer Worksheet.

Appendix B Sample Wiring Diagrams.

Appendix C provides WinViews operation instructions.

Appendix D provides Vendor Contact Information

Appendix E Interface Description Document

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MK VI MK VIII EGPWS Installation Design Guide

1.4 Reference D o cuments

Following is a list of Honeywell reference documents:

965-1180-601 Product Specification for the MK VI and MK VIII Enhanced Ground Proximity Warning

System (EGPWS)

965-1180-201

965-1190-201

965-1210-201

965-1220-201

060-4199-180

060-4267-000

Outline, MK VI EGPWC (without GPS)

Outline, MK VI EGPWC (with GPS)

Outline, MK VIII EGPWC (without GPS)

Outline, MK VIII EGPWC (with GPS)

Line Maintenance Manual

MK VIII EGPWS Terrain Database Airport Coverage List (3500’ Runways)

060-4326-000 MK VI / MK VIII EGPWS Terrain Database Airport Coverage List (2000’ Runways)

060-4199-194 MK VI / MK VIII EGPWS Generic AFM Supplement

060-4314-000 MK VI / MK VIII Enhanced GPWS Pilot’s Guide

060-4188-023 MK VIII Bizjet Flight Test Procedure

060-4188-038 Flight Test Procedure for EGPWS with Internal GPS card

060-4188-041 MK VI / MK VIII GA Fast/GA Slow General Flight Test Procedure

060-4167-158 MK VI / MK VIII Installation Ground Test Procedure

060-4199-190 Trouble Shooting Guide

060-4199-182

076-4610-000

MK VI / MK VIII Failures Modes, Effects, and Safety Analysis

MK VI / MK VIII Failure Modes, Effects, and Criticality Analysis

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MK VI MK VIII EGPWS Installation Design Guide

1.5 Description of Equipment

The MK VI/MK VIII EGPWS is a rack mount ground proximity warning (GPWS) and terrain awareness and

warning (Class A TAWS) computer. Some of the system features include:

♦ Basic Ground Proximity Warning Modes 1-5 ♦ Mode 6 Altitude Callouts and Bank Angle alert ♦ Terrain Clearance Floor ♦ Terrain and Obstacle Awareness alert and display ♦ Terrain map with runways >= 2000 feet in length (optionally >= 3500 feet in length on the MK VIII EGPWS) ♦ Internal GPS card (MK VI 965-1190-0XX and MK VIII 965-1220-0XX only) ♦ Front loading updateable database (requires Smart cable) ♦ External Configuration Module (with a Real Time Clock for use with Internal GPS) ♦ Internal heater blanket for operation outside of the heated area of the aircraft ♦ Fixed Gear operation

1.5.1 MK VI EGP WS Computer

The MK VI EGPWS computer is available under P/N 965-1180-0XX without internal GPS and P/N 965-1190-

0XX with internal GPS. The MK VI EGPWS computer is intended for small turboprop aircraft that provide a

mixture of analog and digital interfaces. The type of supported displays is limited and does not typically include

EFIS displays (Collins ProLine II and Bendix EFIS 40/50 are supported). The terrain database included with the

MK VI EGPWS computer is regional having three separately defined databases for the AMERICAS (North &

South America), ATLANTIC (Europe/Asia/Africa), and PACIFIC (Asia/Australia).

1.5.2 MK VIII EGP WS Computer

The MK VIII EGPWS computer is available under P/N 965-1210-0XX without internal GPS and P/N 965-1220-

0XX with internal GPS. The MK VIII EGPWS computer is intended for regional turboprop and small turbofan

aircraft that provide 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 VIII EGPWS computer is global.

1.5.3 MK VI/MK V III EGPWS Configuration Module

The MK VI/MK VIII EGPWS Configuration Module is available under P/N 700-1710-020. The MK VI/MK VIII

EGPWS use a Configuration Module installed in the aircraft wiring to store aircraft/EGPWS interface

configuration and includes a Real Time Clock for EGPWS installations using internal GPS. 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. An optional

Configuration Module is available under P/N 700-1710-001 for non-Internal GPS operation only.

The 700-1710-020 Configuration Module includes a GPS Real Time Clock (RTC) counter and position memory

to aid in GPS initialization. A capacitor will keep the position memory retained and clock current for

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approximately 35 days. GPS initialization time should be less than 3 minutes with active RTC data. If the

capacitor has discharged then GPS initialization time may be as long as 10 minutes.

1.5.4 GPS Anten n a and Cabling

EGPWS installations using the internal GPS require a GPS antenna and cabling. The GPS antenna should

meet the following qualifications:

Frequency: 1575.42 MHz Impedance: 50 ohms Gain: 33 dB max, 26.5 dB preferred Power: 5 VDC Qualification: TSO C129 or C129a or C144

Antenna gain is limited to 33dB gain, maximum. Antennas with 26dB gain are preferred. There are Active GPS

antennas with higher gain. However, as the active antenna amplifiers amplify noise as well as the signal, this

can overdrive the GPS input AGC circuitry and actually reduce performance.

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. Boeing has certified the Sensor Systems antenna S67-1575-133

(an ARINC 743A antenna with a 33dB gain) for use on all A/C. This antenna is certified for HIRF/EMI, Class 1

flight critical operation. As a result, it is very expensive (about 3X other versions).

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

The EGPWS requires an input signal of no less than -106 dB (at the EGPWS-GPS coax connector). Installers

need to calculate signal strength, plus antenna gain, minus cable line loss to ensure that the input signal does

not exceed the -106 dB limit. To calculate signal strength at the EGPWS coax connector, assume a received

signal strength of -118 dB at the antenna (this is average signal strength from a GPS satellite at zenith over the

antenna). Add the gain of the antenna, then subtract the line loss of the coax cable, and insertion loss at each

connector, except at the EGPWS. Assume 0.6dB insertion loss per connector.

EXAMPLE: Active GPS Antenna with 26dB gain. A 40 foot coax cable run with 1 coax connector (at the rack

disconnect). The cable has a specified line loss of 0.25dB/foot.

-118dB (received signal) + 26dB (antenna gain)

-92dB

-10dB (line loss) (0.25dB/foot x 40 foot run)

- 0.6dB (rack coax connector insertion loss) = -102.6dB at EGPWS coax connector, better than required -106dB. This is an acceptable installation.

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1.5.5 OAT Senso r

The EGPWS uses a separate OAT sensor (Outside Air Temperature) to measure outside air temperature on

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 the Geometric Altitude computation. If Outside Air Temperature is

not available, Geometric Altitude is computed using pressure altitude and GPS Altitude with a corresponding

reduction in accuracy. Honeywell engineers have determined that the reduction in accuracy is small because

the GPS Altitude is the strongest element in the computation.

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.

1.5.6 Smart Cabl e (PCMCIA Interface)

The EGPWS Smart Cable (part number 951-0386-001) is a removable PCMCIA card interface. The Smart

Cable is compatible with Honeywell supplied ATA style PCMCIA cards for use with MK VI and MK VIII EGPWS.

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 Cable loading operation will closely emulate that of an ARINC

615 Data Loader. (Reference Figure 1-1 MK VI/MK VIII EGPWS SMART CABLE)

FIGURE 1-1 MK VI/MK VIII EGPWS SMART CABLE

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1.6 Technical C haracteristics

MK VI / VIII EGPWS

TSO Compliance: (MK VI) TSO-C92c, TSO-C151b Class A

(MK VIII) TSO-C92c, TSO-C151b Class A, TSO-C117a

Application for UKCAA Spec 14 is in process 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): 2.5 Amps max

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: TSO-C151b

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 VI/MK VIII EGPWS

Altitude range: same as MK VI/MK VIII EGPWS

Cooling: No cooling necessary

Shock: No shock mounting required

Power Consumption (5 VDC): from MK VI/MK VIII EGPWS

GPS Antenna Sensor

See Section 1.5.4, ARINC 743A,TSO-C129A and Manufacturer’s specifications.

OAT Sensor

Nominal 500 ohm Temperature probe, resistance at 0°C 500-ohm ± 0.6 ohm, Range -70°C to +60°C (reference

ARINC 575 Section 3.8 or ARINC 706 Section 4.8). See Manufacturer’s specifications.

1.7 Units Supp l ied

1.7.1 MK VI EGP WS

The MK VI EGPWS is available in two versions, with internal GPS card or without. The part number for the units

is as follows:

965-1180-XXX without internal GPS card

965-1190-XXX with Internal GPS card

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The MK VI EGPWS is normally shipped with an AMERICAS Terrain database. When ordering a MK VI EGPWS that will be operating in the ATLANTIC or PACIFIC1 region the specific Terrain database must be specified with the order. NOTE 1: Terrain Database cards for the ATLANTIC or PACIFIC region are no longer required to be ordered separately. NOTE 2: -XXX defines Application software version.

1.7.2 MK VIII EGP WS

The MK VIII EGPWS is available in two versions, with internal GPS card or without. The part number for the

units is as follows:

965-1210-XXX without internal GPS card

965-1220-XXX with Internal GPS card

The MK VIII EGPWS is shipped with a world Terrain database.

NOTE 1: -XXX defines Application software version.

1.7.3 Configurati on Module

The MK VI/MK VIII EGPWS Configuration Module is available in two versions. When ordering the Configuration

Module, order part number 700-1710-020 or part number 700-1710-001. The part number 700-1710-020 is

required for installations with internal GPS.

1.7.4 Smart Cabl e (PCMCIA Interface)

The MK VI/MK VIII EGPWS Smart Cable is available in one version. The Smart Cable is used for Line

Maintenance; Application/Configuration code and Terrain Database uploads and Flight History downloads.

Only one Smart Cable is required for an installation house or operator. When ordering the Smart Cable,

order part number 951-0386-001.

1.8 Installation Kits and Accessories

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

Administration (425-885-8719) for availability.

1.8.1 MK VI/MK V III EGPWS Installation Kits

Note: For all parts in the Installation kits the weight of each part is less than 0.25 pounds.

(A) Retrofit classic MK VI GPWS installation

The MK VI/MK VIII EGPWS Installation Kit, P/N 755-7013-011, contains the following parts:

Vendor Name Vendor P/N Description QTY UM Honeywell P/N

Positronic Ind. RD50F1OJVLC-15 P2 connector 1 EA 440-1233-001

Honeywell 700-1710-020 Configuration Module 1 EA 700-1710-020

(B) New EGPWS installation

The MK VI/MK VIII EGPWS Installation Kit, P/N 755-7013-010, contains the following parts:

Vendor Name Vendor P/N Description QTY UM Honeywell P/N

Positronic Ind. DD78F1OJVLC-15 P1 connector, female 1 EA 440-1158-009

Positronic Ind. RD50F1OJVLC-15 P2 connector, female 1 EA 440-1233-001

Honeywell 700-1710-020 Configuration Module 1 EA 700-1710-020

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Bendix/King 071-04003-0002 Computer Mounting Tray 1 EA 405-0383-001

1.8.2 RS-232 Cab l e

The MK VI/MK VIII 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 Cabl e

The MK VI/MK VIII 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

1.8.4 Terrain Dat abase Cards

The MK VI EGPWS Terrain Database Cards can be ordered using the following part numbers:

Vendor Name Vendor P/N Description QTY UM Honeywell P/N

Honeywell 718-1391-xxx North & South America 1 EA 718-1391-xxx

Honeywell 718-1392-xxx Europe, Africa, Asia 1 EA 718-1392-xxx

Honeywell 718-1393-xxx Asia, Australia, Pacific 1 EA 718-1393-xxx

Honeywell 402-6075-xxx Label, TDB Front Panel 1 EA 402-6075-xxx

1.8.5 Flight Histo ry Card

The MK VI/MK VIII EGPWS Flight History Card can be ordered using the following part numbers:

Vendor Name Vendor P/N Description QTY UM Honeywell P/N

Honeywell

300-1151-006

718-1593-001

Flight History Download

EAEA300-1151-006

718-1593-001

Note 1: Unprogrammed (blank) 32 Mb card ATA PCMCIA card.

Note 2: Programmed 32 Mb card ATA PCMCIA card.

1.9 Accessorie s not Supplied

1.9.1 ARINC 453 Terrain Display wiring

The Terrain display wiring (ARINC 453) must meet the display manufacturer’s specifications including

termination method. ARINC 453 bus 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 (ARINC 708 WXR).

• Impedance of 70 ohms ±10% at 1 MHz (ARINC 453 bus).

Vendor Name Vendor P/N Description QTY UM

Pic Wire&Cable D620224 ARINC 453 cable A/R EA

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Pic Wire&Cable D5102QX Hi Temp Quadraxial A/R EA

Pic Wire&Cable D771553 MIL-STD 1553 Data Bus A/R EA

ECS

4122021

312402

ARINC 453 cable (2 shields)

ARINC 453 cable (3 shields)

A/R

A/REAEA

Emteq D70-022402T-01 ARINC 453 cable A/R EA

M17/176-00002

M83536/6-022M

M12883/44-01

Military Specification

Relay, 4PDT

(Note 1)

Relay, Socket (Note 1)

A/R

Note 1: Recommended in EFS 40/50 Installation Manual.

1.9.2 GPS Anten n a & 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 071-01553-0200 KA 92 GPS Antenna (26dB) 1 EA 300-1147-001

Comant CI 405-2 KA 92 GPS Antenna (26dB) 1 EA 300-1147-001

Bendix/King 050-03318-0000 Antenna Installation Kit OPT EA 405-0432-001

Sensor Systems

Thermax M17/128-RG400 Coax Cable, RG400/U A/R EA

PIC S14293 Coax Cable A/R EA

PIC S44191 Coax Cable A/R EA

ECS 311901 Coax Cable A/R EA

ECS 311601 Coax Cable A/R EA

ECS 311201 Coax Cable 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 (29dB) 1 EA

S67-1575-52 S67 GPS Antenna (26dB) 1 EA

S67-1575-133 S67 GPS Antenna (33dB) 1 EA

Coax Cable, RG-142B/U A/R EA

NOTE: If a satellite communication system is installed in the aircraft, or the GPS cable run is in the vicinity of a

VHF transceiver and/or cable, DO NOT USE R/G 142 or R/G 400 cable.

1.9.3 Circuit Brea ker

The Circuit Breaker needs to be a 3 Amp delayed action circuit breaker.

Vendor Name Vendor P/N Description QTY UM

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

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1.9.4 Annunciato r s & Switch/Annunciators

The devices shown below are West Coast Specialties and Staco switch/annunciators and are representative of

those used in some installations. However, there are other comparable devices on the market that may be

substituted at the installer/customers choice. The installer/customer is cautioned to verify regulatory

approval of the annunciation devices installed. See Appendix D for Vendors.

A. GPWS (P/TEST); BELOW G/S (P/CANCEL) switch/annunciator assemblies

The ‘GPWS’ annunciator provides visual indication of an EGPWS warning or alert. The GPWS annunciator

also has a momentary switch that is used to manually initiate EGPWS Self Test. Two GPWS annunciators

are required for each aircraft, one in the direct view of each pilot. If the Lamp Format 2 option is selected

(see 3.15.2.1), this switch/annunciator will be labeled ‘PULL UP’ and annunciated in red.

The ‘BELOW G/S’ annunciator provides visual indication of an EGPWS glideslope caution. The BELOW

G/S annunciator also has a momentary switch that is used to manually inhibit EGPWS Mode 5 glideslope

alerts. Two BELOW G/S annunciators are required for each aircraft, one in the direct view of each pilot. If

the Lamp Format 2 option is selected (see 3.15.2.1), this switch/annunciator will be labeled ‘GPWS’ and

annunciated in amber.

Vendor Name Vendor P/N Description QTY UM

West Coast Spec.

STACO

(1) GPWS – BELOW G/S – GPWS FLAP OVRD – G/S CANCLD

90-81401-001 GPWS BELOW G/S 2 EA

90-81401-003 GPWS BELOW G/S ALT EA

90-81401-008 GPWS BELOW G/S (1) ALT EA

90-81401-009 GPWS BELOW G/S (1) ALT EA

61406-003 GPWS G/S CANCEL ALT EA

61406-004 PULL UP GPWS TEST ALT EA

61406-005 GPWS GPWS TEST ALT EA

61406-006 BELOW G/S G/S CANCEL ALT EA

B. GPWS FLAP OVRD; GPWS INOP; G/S CANCLD switch/annunciator assemblies

The ‘GPWS FLAP OVRD’ annunciator provides visual indication that the EGPWS Flap Override function is

activated. The GPWS FLAP OVRD annunciator also has a momentary switch that is used to manually activate

the Flap Override function.

The ‘GPWS INOP’ annunciator provides visual indication that the EGPWS’ GPWS modes have been disabled

or do not function because of an external or internal fault.

The ‘G/S CANCLD’ annunciator provides visual indication that the EGPWS Mode 5 function is inhibited.

Vendor Name Vendor P/N Description QTY UM

West Coast Spec.

90-81401-008 (1) 1 EA

90-81401-009 (2) 1 EA

90-81401-010 (3) 1 EA

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West Coast Spec.

STACO 61406-007 GPWS FLAP

(1) GPWS – BELOW G/S – GPWS FLAP OVRD – G/S CANCLD

(2) GPWS – BELOW G/S – GPWS FLAP OVRD – GPWS INOP

(3) GPWS FLAP OVRD – G/S CANCLD

(4) GPWS INOP – G/S CANCLD – GPWS FLAP OVRD

(5) GPWS FLAP OVRD – GPWS INOP

90-81401-011 (4) 1 EA

90-81401-012 (5) 1 EA

OVERRIDE 1EA

C. TERR DISPLAY; TERR INHIBIT; GPWS FAIL / TERR FAIL switch/annunciator assemblies

The ‘TERR DISPLAY’ annunciator provides visual indication that the EGPWS Terrain Display has been selected

for the associated display. The TERR DISPLAY annunciator also has a momentary switch that is used to

manually select the Terrain Display.

The ‘TERR INHIBIT’ annunciator provides visual indication that the EGPWS Terrain functions have been

inhibited. The TERR INHIBIT annunciator also has a alternate action switch that is used to manually inhibit the

Terrain functions.

The ‘GPWS FAIL / TERR FAIL’ annunciator provides visual indication that the EGPWS GPWS modes or TA&D

and TCF modes have a disabled function.

Vendor Name Vendor P/N Description QTY UM

STACO 61406-001 TERRAIN DISPLAY ON 1 EA

STACO 61406-002 TERR INHIBIT ON 1 EA

STACO

61406-011

GPWS FAIL TERRAIN FAIL

1EA

1.9.5 Cockpit Sp e akers

The MK VI / MK VIII EGPWS can interface to an 8 ohm audio speaker for cockpit annunciation of aural alerts.

Vendor Name Vendor P/N Description QTY UM

Quam 30A05Z8 Audio Speaker 1 EA

Utah SP-3A Audio Speaker 1 EA

1.9.6 Temperatur e Probes

The MK VI / MK VIII EGPWS may be optionally interfaced to a dedicated 500-ohm temperature probe meeting

the specifications of ARINC 575 Section 3.8. The installer may want to discuss availability of a dual-element

probe compatible with the EGPWS and with other systems on the aircraft with the manufacturers.

Vendor Name Vendor P/N Description QTY UM

CIC

Norwich

Rosemount 102CT2CB 500-ohm 1 EA

Rosemount 102AU1AF Single element, heated 1 EA

Rosemount 102AU1AG Dual element, heated 1 EA

05257

103-00157-3

103-00034

Single element, unheated

Dual element, unheated

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Rosemount 102EH2BH Dual element, heated 1 EA

Rosemount 102EH2EB Dual element, heated 1 EA

Rosemount 102JE2FG Triple element, heated 1 EA

Rosemount 129H-500 Single element, unheated 1 EA

Rosemount 129G-500 Dual element, unheated 1 EA

1.10 Tools Requ i red

1.10.1 Crimping T ool - 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

Hand Crimping Tool EA 1 Astro 61517

1.10.2 Contact Po sitioner - P1, 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

1.10.3 Insertion/R emoval 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 Tool P1, P3 EA 1 Military M81969/1-04

Insertion/Removal Tool P2 EA 1 Military M81969/1-02

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1.10.4 Spare Conn e ctors and Contacts - P1, P2, P3

P/N Description UM QTY Vendor Name & Part Number

440-1223-002 15 pin male with hood EA 1 Positronic Ind. DD15M10YOC-15

440-1223-003

440-1223-004

400-5163-002

15 pin female EA 1 Positronic Ind. DD15F10OOC-15

15 pin male EA 1 Positronic Ind. DD15M10OOC-15

15 pin clamp kit EA 1 AMP 745854-3

male contacts for 15 pin 22-30 AWG EA 1 Positronic Ind. MC8022D

male contacts for 15 pin 22-30 AWG EA 1 M39029/58-360

female contacts for 50 pin 20-24 AWG EA 1 Positronic Ind. FC6020D

female contacts for 50 pin 20-24 AWG EA 1 M39029/63-368

female contacts for 78 pin 22-30 AWG EA 1 Positronic Ind. FC8022D

female contacts for 78 pin 22-30 AWG EA 1 M39029/57-354

These parts are available in EGPWS kit PN 755-7013-090.

1.11 License Re q uirements

There are no Radio license requirements for the MK VI/MK VIII EGPWS

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SECTION II

INSTALLATION

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SECTION II - INSTALLATION

SECTION II - INSTALLATION........................................................................................................................................ 29

2.1 I

NTRODUCTION.............................................................................................................................................................. 29

2.2 U

NPACKING AND INSPECTING THE EQUIPMENT ............................................................................................................. 29

2.3 E

QUIPMENT INSTALLATION........................................................................................................................................... 29

2.3.1 General.................................................................................................................................................................. 29

2.3.2 MK VI/MK VIII Computer Location...................................................................................................................... 29

2.3.3 MK VI/ MK VIII Computer Installation................................................................................................................. 30

2.3.4 Configuration Module Location............................................................................................................................ 31

2.3.5 Configuration Module Installation........................................................................................................................ 31

2.3.6 GPS Antenna location ........................................................................................................................................... 40

2.3.7 GPS Antenna Installation...................................................................................................................................... 40

2.3.8 OAT Sensor Location ............................................................................................................................................ 40

2.3.9 OAT Sensor Installation ........................................................................................................................................ 40

2.3.10 Cockpit Lights...................................................................................................................................................... 40

2.3.10.1 Description........................................................................................................................................................................41

2.3.10.2 Location ............................................................................................................................................................................42

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SECTION II - INSTALLATION

2.1 Introductio n

This section contains suggestions and factors to consider before installing the Enhanced Ground Proximity

Warning System. Close adherence to these suggestions will assure satisfactory performance from the

equipment.

NOTE

The conditions and tests performed on this article are minimum performance standards. It is

the responsibility of those desiring to install this article either on or within a specific type or

class of aircraft to determine that the aircraft installation conditions are within these

performance standards. The article may be installed only if further evaluation by the

applicant documents an acceptable installation and is approved by the airworthiness

authority.

2.2 Unpacking a nd Inspecting the Equipment

Exercise extreme caution when unpacking equipment. Perform a visual inspection of the unit for evidence of

damage incurred during shipment. If a damage claim must be filed, save the shipping container and all packing

materials to substantiate your claim. The claim should be filed as soon as possible. The shipping container and

all packing materials should be retained in the event that storage or reshipment of the equipment is necessary.

2.3 Equipment Installation

2.3.1 General

The following paragraphs contain information pertaining to the installation of the MK VI and MK VIII EGPWS,

including instructions concerning the location and mounting of the equipment. The equipment should be

installed in the aircraft in a manner consistent with acceptable workmanship and engineering practices, and in

accordance with the instructions set forth in this publication. To ensure the system has been properly and safely

installed in the aircraft, the installer should make a thorough visual inspection and conduct an overall operational

check of the system, on the ground, prior to flight.

CAUTION

AFTER INSTALLATION OF THE CABLING AND BEFORE INSTALLATION OF THE

EQUIPMENT, A CHECK SHOULD BE MADE WITH THE AIRCRAFT PRIMARY POWER

SUPPLIED TO THE MOUNTING CONNECTOR, TO ENSURE THAT POWER IS APPLIED

ONLY TO THE PINS SPECIFIED IN THE INTERWIRING DIAGRAMS IN SECTION III.

2.3.2 MK VI/MK V III Computer Location

Care should be exercised to avoid mounting components near equipment operating with high pulse current or

high power outputs such as radar and satellite communications equipment. In general, the equipment should be

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MK VI MK VIII EGPWS Installation Design Guide

installed in a location convenient for operation, inspection, and maintenance, and in an area free from excessive

vibration, heat, and noise generating sources.

The MK VI and MK VIII EGPWS have an internal heater blanket therefore they can be mounted outside the

heated area of the aircraft. The computers have been qualified for operation up to 50,000 feet and -55°C using

the heater blanket.

All mechanical installation drawings, connector assembly diagrams, interwiring diagrams, and connector pin

assignment tables referenced in this section are located at the end of Section II of this manual. Determine the

mounting location for the system components following the guidelines below.

Prior to installing any equipment, make a continuity check of all wires and cables associated with the system.

Then apply power and check for proper voltages at system connectors, and then remove power before

completing the installation.

To allow for inspection or repair of the wiring of the connector assembly itself, sufficient lead length should be

left so that EGPWS may be moved several inches. A bend should be made in the harness to allow water

droplets that might form on the harness due to condensation, to drip off at the bend and not collect in the

connector.

NOTE

For retrofit installations of classic MK VI GPWS and installing a EGPWS with internal GPS,

the connector backshell of the classic MK VI P1 connector will interfere with the GPS

antenna connector on the front of the EGPWS. The connector backshells chosen for the

EGPWS kits now extends straight out and does not interfere with the GPS antenna

connector.

The length of cables from the EGPWS connectors to other system units is not generally critical because unit

interfaces are designed with high impedance inputs, low impedance outputs, and low noise susceptibility

characteristics. The exception is the wires from the EGPWS Configuration Module, which was designed to be a

part of the EGPWS connector backshell because of the requirement for short lead length. Follow aircraft

manufacturer’s, sub-system manufacturer’s or ARINC specifications for shield grounding.

2.3.3 MK VI/ MK VIII Computer Installation

The MK VI and MK VIII EGPWS installation will conform to standards designated by the customer, installing

agency, and existing conditions as to the unit location and type of installation. However, the following

suggestions will assure a more satisfactory performance from the equipment.

A. Plan a location on the aircraft so that the EGPWS is accessible for front panel maintenance controls. Check

to be sure that there is adequate space in the front of the computer for connectors and cabling.

B. Refer to Figure 2-2 and 2-3 for outline dimensions of the computer and mounting tray.

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Honeywell MK VI, MK VIII User Manual

Specifications and Main Features

Frequently Asked Questions

User Manual

TABLE OF CONTENTS

SECTION I

Honeywell 700-1710-020 Configuration Module 1 EA 700-1710-020

Honeywell 704-2617-001 RS-232 Cable 1 EA 704-2617-001

Honeywell 951-0386-001 Smart Cable 1 EA 951-0386-001

SECTION II