Installation Design Guide - MK V EGPWS · PDF file3.16 alert volume control ... 4 electrical installation design..... 45 4.1 electrical interfaces

AlliedSignal, Inc.

MK V

Enhanced Ground Proximity WarningSystem

Installation Design Guide

Part Numbers 965-0976-0xx-xxx-xxx

This document is an unpublished work. Copyright ��1999 AlliedSignal Inc. All rights

reserved.

This document and all information and expression contained herein are the property ofAlliedSignal 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 theinformation contained therein. Your use of this document constitutes acceptance of these

terms.

Release Date: October 1999

CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4199-125 REV: SHEET 1 OF 571

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CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4199-125 REV: SHEET 2

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Typed names constitute approval signatures. Actual signatures are on file at AlliedSignal.

DRAWN Ann Sweebe 29 Oct 1999

CHECK

ENGR Ann Sweebe 29 Oct 1999

MFG

QA

APVD Kevin Allen 29 Oct 1999

APVD

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TABLE OF CONTENTS

1 INTRODUCTION ............................................................................................................................. 10

1.1 APPLICABILITY .............................................................................................................................. 10

1.2 HOW TO USE THIS DOCUMENT ...................................................................................................... 10

1.3 REFERENCE DOCUMENTS............................................................................................................... 12

1.4 GENERAL SPECIFICATIONS............................................................................................................. 13

2 SYSTEM OVERVIEW ..................................................................................................................... 15

3 FEATURE AND OPTION SELECTIONS ....................................................................................... 16

3.1 AIRCRAFT TYPE............................................................................................................................. 28

3.2 DISPLAY SELECTION...................................................................................................................... 29

3.3 ALTITUDE CORRECTION................................................................................................................. 30

3.4 EGPWS SUPPRESSION................................................................................................................... 31

3.5 GLIDESLOPE CANCEL..................................................................................................................... 31

3.6 STEEP APPROACH.......................................................................................................................... 32

3.7 ALTERNATE MODE 4B................................................................................................................... 32

3.8 WINDSHEAR DETECTION AND ANNUNCIATION................................................................................ 33

3.9 LAMP FORMAT .............................................................................................................................. 34

3.10 SIMULATOR INSTALLATION .......................................................................................................... 34

3.11 ENHANCED FEATURE CONTROL.................................................................................................... 35

3.11.1 Terrain Awareness & Display and Terrain Clearance Floor ................................................. 35

3.11.2 Obstacle Awareness.............................................................................................................. 36

3.11.3 Peaks Mode.......................................................................................................................... 36

3.12 BANK ANGLE CALLOUT ACTIVATION ........................................................................................... 37

3.12.1 Bank Angle Callout Activation for Bizjet Aircraft .................................................................. 37

3.12.2 Bank Angle Callout Activation for Commercial Air Transport Aircraft .................................. 37

3.13 ALTITUDE CALLOUT MENU SELECTION........................................................................................ 38

3.14 AUDIO MENU SELECTION............................................................................................................. 39

3.15 AUDIO DECLUTTER DISABLE........................................................................................................ 39

3.16 ALERT VOLUME CONTROL........................................................................................................... 40

3.17 MODE 6 VOLUME ........................................................................................................................ 41

3.18 EGPWS DISPLAY POP-UP SELECTION .......................................................................................... 42

3.19 PREDICTIVE WINDSHEAR............................................................................................................. 42

3.20 OPTIONAL SYSTEM INPUTS........................................................................................................... 43

3.21 GPS ALTITUDE REFERENCE......................................................................................................... 44

4 ELECTRICAL INSTALLATION DESIGN ..................................................................................... 45

4.1 ELECTRICAL INTERFACES............................................................................................................... 45

4.1.1 Primary Power Input.............................................................................................................. 45

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4.1.2 Chassis Ground...................................................................................................................... 47

4.1.3 Voltage Reference Output....................................................................................................... 47

4.2 PROGRAM PIN STRAPPING.............................................................................................................. 48

4.2.1 Aircraft Type (Program Pins 1 - 3) ........................................................................................ 50

4.2.2 Altitude Correction, EGPWS Suppress and Glideslope Cancel (Program Pin 10).................... 51

4.2.3 Windshear Control and Lamp Format (Program Pin 12)......................................................... 53

4.2.4 Enhanced Feature Control and Simulator Reposition (Program Pin 13).................................. 55

4.2.5 Bank Angle Callouts and Alternate LRRA Formats (Program Pin 14) ..................................... 58

4.2.6 Altitude Callout Menu Selection (Program Pins 4 – 6) ............................................................ 60

4.2.7 Audio Menu Selection (Program Pin 8)................................................................................... 61

4.2.8 Alert Volume and Audio Declutter (Program Pin 11) .............................................................. 62

4.2.9 Alternate Pop-up Selection & Predictive Windshear System (PWS) Interface Options (Program

Pin 15)............................................................................................................................................ 65

4.2.10 Optional System Inputs, Internal GPS and Alternate Mode 4B Reversal (Program Pins 7 and 9)

....................................................................................................................................................... 67

4.2.11 ARINC 429 Interface Modifications (Program Pin 16) .......................................................... 71

4.2.12 Alternate Display (Program Pin 18) ..................................................................................... 72

4.2.13 GPS Altitude Reference (Program Pin 19) ............................................................................ 73

4.2.14 Program Pin Parity (Program Pin 17).................................................................................. 73

4.3 ARINC 429 DIGITAL AND ANALOG INPUTS.................................................................................... 74

4.4 RS-232 INTERFACE........................................................................................................................ 75

4.5 DISCRETE INPUTS.......................................................................................................................... 76

4.5.1 Air Ground Discrete............................................................................................................... 76

4.5.2 Altitude Callouts Enable Discrete ........................................................................................... 76

4.5.3 AOA Validity Discretes #1 and #2........................................................................................... 76

4.5.4 Audio Inhibit / All Modes Inhibit Discrete...............................................................................77

4.5.5 Decision Height Discrete........................................................................................................ 78

4.5.6 Display Select Discretes #1 and #2 ......................................................................................... 78

4.5.7 EFIS Range Discretes #1A, B, C, D and #2A, B, C, D ............................................................. 78

4.5.8 Flap Position Discretes #1, #2, #3, #4 .................................................................................... 78

4.5.9 Flaps Switch Inputs................................................................................................................ 78

4.5.10 FMS Glideslope Inhibit Discrete........................................................................................... 78

4.5.11 Glideslope Cancel Discrete .................................................................................................. 79

4.5.12 Glideslope Inhibit Discrete................................................................................................... 79

4.5.13 Glideslope Validity Discretes #1 and #2................................................................................ 79

4.5.14 GPWS Inhibit Discrete ......................................................................................................... 80

4.5.15 ILS Bus Select Discretes #1, #2 and #3 ................................................................................. 80

4.5.16 ILS/MLS Select..................................................................................................................... 80

4.5.17 ILS Tuned Discrete #1 .......................................................................................................... 80

4.5.18 ILS Tuned Discrete #2 .......................................................................................................... 80

4.5.19 Landing Flap/Flap Override Discrete ................................................................................... 81

4.5.20 Landing Flap Override Discrete ........................................................................................... 81

4.5.21 Landing Gear/Gear Override Discrete.................................................................................. 81

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4.5.22 Localizer Validity Discretes #1 and #2..................................................................................81

4.5.23 Mode 6 Volume Control Discrete..........................................................................................82

4.5.24 Momentary Audio Suppress Discrete .................................................................................... 82

4.5.25 PWS Interlock Discretes #1 and #2.......................................................................................82

4.5.26 Radio Altitude Validity Flags #1 and #2 (ARINC 552/ALT 55) .............................................. 83

4.5.27 Self-Test Discrete ................................................................................................................. 83

4.5.28 Simulator Reposition ............................................................................................................ 83

4.5.29 Stall Warning Computer Fail Discretes #1 and #2 ................................................................ 83

4.5.30 Steep Approach Discretes #1 and #2..................................................................................... 84

4.5.31 Terrain Awareness and TCF Inhibit...................................................................................... 84

4.5.32 Terrain Displayed on EFIS Discretes (Left and Right)........................................................... 85

4.5.33 Terrain Relay Monitor Discretes #1 and #2 .......................................................................... 85

4.5.34 Weather Display Select Discretes #1 and #2 ......................................................................... 85

4.5.35 Weather Radar On/Off #1 and #2.......................................................................................... 85

4.6 SERIAL OUTPUT............................................................................................................................. 86

4.7 AUDIO OUTPUT ............................................................................................................................. 87

4.8 DISCRETE OUTPUTS....................................................................................................................... 88

4.8.1 Audio On Discrete.................................................................................................................. 88

4.8.2 Callout INOP Monitor Discrete.............................................................................................. 88

4.8.3 Displayable Discretes #1 and #2............................................................................................. 89

4.8.4 Glideslope Cancel Discrete.................................................................................................... 89

4.8.5 GPWC Alert Discrete ............................................................................................................. 89

4.8.6 GPWC Warning Discrete ....................................................................................................... 89

4.8.7 GPWS Monitor Discrete ......................................................................................................... 90

4.8.8 PWS Inhibit Discrete .............................................................................................................. 90

4.8.9 TCAS Inhibit Discrete............................................................................................................. 90

4.8.10 Terrain Awareness Caution and Obstacle Awareness Caution Discrete................................. 90

4.8.11 Terrain Awareness Warning and Obstacle Awareness Warning Discrete............................... 90

4.8.12 Terrain Display Switching Discretes #1 and #2..................................................................... 90

4.8.13 Terrain Displayable Discretes #1 and #2 .............................................................................. 91

4.8.14 Terrain INOP Monitor Discrete............................................................................................ 91

4.8.15 Terrain Not Available Monitor Discrete................................................................................ 91

4.8.16 Windshear Caution Discrete................................................................................................. 91

4.8.17 Windshear Monitor Discrete................................................................................................. 92

4.8.18 Windshear Warning Discrete................................................................................................ 92

4.8.19 WXR Control Discrete.......................................................................................................... 92

5 MECHANICAL INSTALLATION DESIGN DETAILS .................................................................. 93

5.1 SYSTEM COMPONENTS................................................................................................................... 93

5.1.1 MK V Enhanced Ground Proximity Warning Computer.......................................................... 94

5.1.2 Mounting Tray (ARINC 600, 2 MCU)..................................................................................... 96

5.1.3 MK V EGPWC Rear Connector.............................................................................................. 97

5.1.4 Front Panel Test Connector Mate........................................................................................... 99

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5.1.5 Cockpit Annunciators ............................................................................................................. 99

5.1.6 Switching Relays .................................................................................................................. 104

5.1.7 GPS Antenna........................................................................................................................ 104

5.1.8 GPS Cable Contacts............................................................................................................. 105

5.1.9 GPS Cabling........................................................................................................................ 105

5.2 WIRING....................................................................................................................................... 106

5.3 VENDOR CONTACT INFORMATION................................................................................................ 107

5.4 SAMPLE PARTS LISTS, LIGHTS AND LIGHTPLATES......................................................................... 109

5.4.1 Boeing 737-300 with PPI Display (Aircraft Type 16)............................................................ 109

5.4.2 Boeing 737-300 / -400 / -500 UAL “4-Button Push” Layout.................................................. 112

5.4.3 Boeing 737-400 (Aircraft Type 101)...................................................................................... 115

5.4.4 Boeing 757-200 (Aircraft Type 105) or Boeing 767-200 American Airlines (Aircraft Type 106)

..................................................................................................................................................... 119

5.4.5 Airbus A310 (Aircraft Type 108)........................................................................................... 122

5.4.6 MD 80 EFIS (Aircraft Type 114) American Airlines.............................................................. 124

6 INSTALLATION/GROUND CHECK PROCEDURE ................................................................... 127

7 CERTIFICATION ........................................................................................................................... 128

8 QUESTIONS & ANSWERS............................................................................................................ 129

9 WORKSHEETS .............................................................................................................................. 130

10 ACRONYMS ................................................................................................................................. 154

APPENDIX A: AIRCRAFT TYPE TABLES .................................................................................... 156

A-1 AIRBUS.................................................................................................................................. 162

A.1.1 A300/A310..................................................................................................................... 162

A.1.2 A319/A320/A321........................................................................................................... 169

A.1.3 A330/A340..................................................................................................................... 179

A-2 AVRO .................................................................................................................................... 187

A-2.1 RJ ....................................................................................................................................... 187

A-3 BEECHJET.............................................................................................................................. 194

A-3.1 Beechjet 400A..................................................................................................................... 194

A-4 BOEING ................................................................................................................................. 201

A-4.1 737-300......................................................................................................................... 201

A-4.2 737-400......................................................................................................................... 215

A-4.3 737-500......................................................................................................................... 230

A-4.4 737-600, 737-700 and 737-800...................................................................................... 244

A-4.5 747-400......................................................................................................................... 249

A-4.6 757-200......................................................................................................................... 262

A-4.7 757-300......................................................................................................................... 277

A-4.8 767-200......................................................................................................................... 282

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A-4.9 767-300......................................................................................................................... 293

A-4.10 767-300ER.................................................................................................................... 304

A-4.11 777-200......................................................................................................................... 316

A-4.12 777-300......................................................................................................................... 321

A-5 CANADAIR ............................................................................................................................. 326

A.5.1 Global Express.............................................................................................................. 326

A.5.2 CL601/3A...................................................................................................................... 331

A.5.3 CL604 ........................................................................................................................... 337

A.5.4 Regional Jet (RJ-100/RJ-200)........................................................................................ 344

A-6 CESSNA................................................................................................................................. 349

A.6.1 Citation X...................................................................................................................... 349

A.6.2 Citation Excel................................................................................................................ 354

A-7 DASSAULT............................................................................................................................. 362

A-7.1 Falcon 20F.................................................................................................................... 362

A-7.2 Falcon 2000.................................................................................................................. 372

A-7.3 Falcon 50 ...................................................................................................................... 379

A-7.4 Falcon 50 EX................................................................................................................. 389

A-7.5 Falcon 900/900B ...........................................................................................................396

A-7.6 Falcon 900 EX............................................................................................................... 401

A-8 DEHAVILLAND ...................................................................................................................... 408

A-8.1 Dash 8-400.......................................................................................................................... 408

A-9 DORNIER...............................................................................................................................413

A-9.1 Do-328 Jet........................................................................................................................... 413

A-10 DOUGLAS........................................................................................................................... 418

A-10.1 DC8-72............................................................................................................................. 418

A-10.2 DC-9-82/-83 EFIS............................................................................................................. 423

A-10.3 MD10................................................................................................................................ 428

A-10.4 MD11................................................................................................................................ 433

A-10.5 MD80................................................................................................................................ 438

A-10.6 MD87................................................................................................................................ 447

A-10.7 MD88/90 ........................................................................................................................... 452

A-10.8 MD95................................................................................................................................ 457

A-11 EMBRAER .......................................................................................................................... 462

A-11.1 EMB-135/EMB-145........................................................................................................... 462

A-12 FOKKER............................................................................................................................. 467

A-12.1 Fokker 100 ........................................................................................................................ 467

A-13 GULFSTREAM..................................................................................................................... 472

A-13.1 Gulfstream II ................................................................................................................. 472

A-13.2 Gulfstream IIB/III .......................................................................................................... 479

A-13.3 Gulfstream IV................................................................................................................ 486

A-13.4 Gulfstream V ................................................................................................................. 494

A-14 HAWKER............................................................................................................................ 500

A.14.1 Hawker 800................................................................................................................... 500

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A.14.2 Hawker 1000................................................................................................................. 512

A-15 IAI .................................................................................................................................... 517

A-15.1 Astra SPX.......................................................................................................................... 517

A-15.2 Galaxy............................................................................................................................... 522

A-16 LEARJET............................................................................................................................ 527

A-16.1 Learjet Model 45 ............................................................................................................... 527

A-16.2 Model 60 ........................................................................................................................... 536

A-17 SAAB ................................................................................................................................. 541

A-17.1 Saab 2000......................................................................................................................... 541

A-18 SIMULATORS...................................................................................................................... 546

APPENDIX B: ALTITUDE CALLOUT MENU OPTIONS ............................................................. 547

APPENDIX C: AUDIO MENU OPTIONS ........................................................................................ 554

APPENDIX D: SAMPLE WIRING DIAGRAMS .........................................................................................................559

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1 Introduction

The AlliedSignal MK V Enhanced Ground Proximity Warning System (MK V EGPWS) provides

alerts and warnings to prevent Controlled Flight Into Terrain (CFIT) and for low altitude windshear

conditions. This Installation Design Guide provides information for selecting features and options

and designing the installation for this system.

This document assumes a familiarity with avionics installation practices and aircraftsystems associated with the installation and operation of the MK V EGPWS. It alsoassumes 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 beconstrued as formal FAA approved work authorization. This document is a guide and isas accurate as poss ible at the time of its release. Ref erence documents 1 and 2 are thecontrolling documents for the MK V EGPWS.

1.1 Applicability

This manual is applicable only to MK V EGPWS computers with the following part numbers:

Version –204

965-0976-003-204-204

965-0976-040-204-204

Version –206

965-0976-003-206-206

965-0976-040-206-206

Version –208

965-0976-003-208-208

965-0976-040-208-208

965-0976-020-208-208

1.2 How To Use This Document

Section 2 provides a system overview.

Section 3 provides guidance to the aircraft owner/operator (or installer representative) for

selecting required features and options of the MK V EGPWS. This section includes a worksheet

for recording feature and option preferences.

Section 4 provides instructions to aid the installation designer in creating aircraft wiring diagrams

for the MK V EGPWS based on the worksheet completed in Section 3.

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Section 5 provides mechanical installation details of the MK V EGPWC and associated

components.

Other activities associated with the installation design include preparing a ground checkout

procedure (Section 6), a certification package (Section 7) and troubleshooting any problems

encountered during the installation or checkout (Section 8). This document provides basic

information and references to support these activities.

Section 9 contains a full set of the worksheets contained in Sections 3 and 4 and in Appendix A.

These worksheets are used for feature selection and documenting the wiring for an installation.

This section may be copied and used in place of the worksheets throughout this document.

Acronyms are defined in Section 10.

Appendix A contains the Aircraft Type descriptions that define the operational environment and

basic configuration of the MK V EGPWS.

Appendix B contains the altitude callout menus available.

Appendix C contains the audio callout menus (all callouts except for altitude callouts).

Appendix D contains sample wiring diagrams for selected aircraft configurations.

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1.3 Reference Documents

Following is a list of AlliedSignal reference documents:

1. 965-0976-603 Product Specification for the Enhanced Ground Proximity Warning

System

2. 993-0976-401 Interface Control Document for the MK V Enhanced Ground

Proximity Warning Computer

3. 960-0329 System, Enhanced Ground Proximity Warning, 115 VAC

4. 960-0329-201 Enhanced Ground Proximity Warning System (EGPWS), 115 VAC,

Outline

5. 960-0335 System, Enhanced Ground Proximity Warning, 28 VDC

6. 960-0335-201 EGPW System, 28 VDC, Outline

7. 960-0336 System, EGPW, 115 VAC with Internal GPS

8. 960-0336-201 Enhanced Ground Proximity Warning System (EGPWS), 115 VAC

with Internal GPS, Outline

9. 060-4199-014 Line Maintenance Manual

10. 060-4267-000 EGPWS Terrain Database Airport Coverage List

11. 060-4199-038 Generic AFM Supplement For EGPWS

12. 060-4241-000 Enhanced GPWS Pilot’s Guide

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1.4 General Specifications

Refer to the following table for general specifications for the MK V Enhanced Ground Proximity

Warning Computer.

CHARACTERISTIC SPECIFICATION

Certification FAA: TSO-C92c (GPWS) TSO-C117a (Windshear) N8110.64 (Enhanced functions)

UKCAA: Specification 14

Physical

Size

Dimensions:

Markings/Identification

Weight

Mounting

2 MCU ARINC 600-6 form factor chassis

H W D7.64” x 2.43” x 12.76” (14.26” including handle)

per ARINC 723-1

7.0 pounds (maximum)

Rack mounted per ARINC 600-6Vibration isolation or shock mounting not required

Reliability

MTBF

MTBUR

� 12,500 (operating) hours

� 11,250 (operating) hours

Power

Input Type:

965-0976-003-xxx-xxx

965-0976-020-xxx-xxx (Internal GPS)

965-0976-002-xxx-xxx

965-0976-040-xxx-xxx

Requirement

115 VAC/400 Hz

115 VAC/400 Hz

28 VDC

28 VDC

22 Watts (maximum) – warning over 8� speaker

48 Watts (with Heater Blanket - On)*

[* Heater Blanket only applicable to 965-0976-040-xxx-xxxEGPWC which turns on at � -20o C and off at � -10o C.]

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CHARACTERISTIC SPECIFICATION

Control Device (recommended):

965-0976-003-xxx-xxx/965-0976-020-xxx-xxx

965-0976-002-xxx-xxx

965-0976-040-xxx-xxx

2 Amp Delayed Action Circuit Breaker



Environmental

Temperature range

Operational

965-0976-002-xxx-xxx/965-0976-003-xxx-xxx/ 965-0976-020-xxx-xxx

965-0976-040-xxx-xxx

Storage

Altitude

High Altitude

Decompression

Overpressure

Cooling

Humidity

Shock

Operational

Crash Safety

Impulse

Sustained

Radio Frequency Susceptibility

RTCA/DO-160C

-40 to +70 oC

-55 to +70 oC

-55 to +85 oC

55,000 feet

8,000 to 55,000 feet

-15,000 feet

Convection (no forced air cooling)

48 hours at 95% relative humidity

6g for 11 msec

15g for 11 msec

12g for 3 sec

HIRF (radiated and conducted)

Table 1.4-1 General Specifications

Additional environmental information can be found in the EGPWS Product Specification, drawing

number 965-0976-603.

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2 System Overview

The MK V EGPWS provides aural and visual alerts to help prevent controlled flight into terrain

during all phases of flight and for low-altitude windshear conditions. The system is designed for

current generation aircraft that have primarily serial digital interfaces. A complete system

description can be found in the Product Specification for the Enhanced Ground Proximity Warning

System.

The MK V Enhanced Ground Proximity Warning Computer (EGPWC) is designed to operate in

any one of a set of pre-defined aircraft configurations called Aircraft Types. Each Aircraft Type is

uniquely defined by a combination of the following:

� aircraft model

� cockpit display characteristics (sweep style and display)

� signal interfaces (analog, digital and discrete)

� non-operator-selectable features

� cockpit lamp configuration and mode (flashing or steady)

� windshear detection enabling

Figure 2-1 Enhanced Ground Proximity Warning System shows the interfaces of the MK V

EGPWS.

E G P W C

Audio AlertMessages

Discrete InputsAnalog Inputs

ARINC 429 Inputs

Discrete OutputsARINC 429 Outputs

RS-453 Outputs

GPW SALGORITHMS

TERRAIN AW ARENESS& OBSTACLE ALERTING

AND DISPLAYALGORITHMS

TERRAINCLEARANCE

FLOORALGORITHMS

WINDSHEARDETECTION AND

ALERTING ALGORITHMS

A L E R T LA M P SA N D E F ISD IS P L A Y

F LIG H T D E C KS P E A K E R S A N D

IN T E R P H O N E

E F IS N A V .D IS P L A Y O R W x

R A D A RIN D IC A T O R

A IR C R A FTS E N S O R S

A N DS Y S T E M S

AURALCALLOUTS

Figure 2-1 Enhanced Ground Proximity Warning System

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3 Feature and Option Selections

This sect ion requires inputs from the ai rcraft owner or operator.

The purpose of this section is to document the feature and option selections necessary for

generating wiring diagrams for the MK V EGPWS installation.

The MK V EGPWC provides a set of default features that are defined by Aircraft Type. The

functionality of many of these features may be tailored to suit customer preferences by

appropriately wiring the system. Refer to the Product Specification for the Enhanced Ground

Proximity Warning System for more detailed information on basic MK V EGPWS functionality,

features and options.

Table 3-1 MK V EGPWS Feature Selection Worksheet provides brief descriptions of the features

and cross-references to sections containing detailed descriptions and instructions to assist with

feature selections. The left side of this worksheet selection is used for recording feature

selections. The right side is provided to help select the Aircraft Type most compatible with the

aircraft configuration and the feature selections.

The availability of some features is controlled by the Aircraft Type and explained in Section 3.1.

When completing Table 3-1 MK V EGPWS Feature Selection Worksheet either complete the

feature and option selections on the left side and then compare the selections with the candidate

Aircraft Types OR compare each the availability of each feature/options with the candidate

Aircraft Types(s) as each selection is made. Items grayed out under the Candidate Aircraft Type

in Table 3-1 MK V EGPWS Feature Selection Worksheet are independent of the Aircraft Type.

NOTE: If a feature or option is selected for an aircraft that is not supported by the selected

Aircraft Type, the selection should be revised.

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Table 3-1 MK V EGPWS Feature Selection Worksheet

Feature and Option Selections Comparison of Candidate Aircraft Typesversus Feature Selections

Feature/Option DescriptionFeatureAvail-ability

ReferenceSection

CandidateAircraft Type(s) ->

Aircraft Type

Does the aircraftconfiguration support therequired ARINC 429inputs?

Aircraft Type

_____________________

The Aircraft Type defines the basic operating environment ofthe MK V EGPWC by defining the specific aircraft model,electrical interfaces and non-selectable features. The AircraftType controls the availability of some options. A single aircraftmodel may have several Aircraft Types to allow for different on-board systems and features.

ACTION: Review information in reference sections;identify potential Aircraft Types and record the AircraftType Numbers at right. Complete feature selection portionof this worksheet (the left side) then select the specificAircraft Type from the options at left.

-101 andon (seeApp. A

for avail.of each

A/CType)

3.14.2.1

Does the aircraftconfiguration support therequired analog inputs (ifany)?

Display

Terrain display

_____________________

Terrain is displayed on an existing display (typically the samedisplay used to display weather). Display discussions applyonly to the display(s) for terrain data. Auto-ranging is availablefor some displays.

Terrain display is only used if Terrain Awareness & Display isenabled (see Section 3.11.1.)

Prior to version –208, the PPIN State 1 display interface in theAircraft Type’s “Display Options & Peaks Availability” table isthe only display supported by that Aircraft Type.

ACTION: Record the PPIN States for applicable terraindisplay types for each candidate Aircraft Type at right. Ifinstalling version –208 or newer, complete the left side ofthis worksheet and select the Aircraft Type, then recordthe PPIN state for the display at left (enter N/A if installinga version older than –208).

-101 andon

3.24.2.12

If display(s) will be usedand installing version –208or newer, does the aircraftconfiguration match any ofthe displays defined for the

Aircraft Type?OR

If display(s) will be usedand installing version –206or older, does the aircraftconfiguration match therequired display for the

Aircraft Type?

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ReferenceSection


Basic GPWS Functions/Options

Altitude Correction

QNH

QFE

QNH is barometric altitude corrected to mean sea level and isthe most common correction format.

QFE is barometric altitude corrected to read zero feet at therunway regardless of the mean sea level altitude of the runway.

ACTION: Review reference sections and record the QNHor QFE selection at left.

-101 andon

3.34.2.2

4.2.2.1

EGPWS Suppression

Suppress Audio Only

Suppress Audio andVisual

No Suppression(Do not use discreteinput)

The MK V EGPWS Audio Inhibit discrete input normallysuppresses MKV EGPWS callouts (except reactive windshear)manually via a cockpit-mounted switch or automatically via theDSWC and PWS computers.

Audio Inhibit discrete can be configured to also suppress non-windshear visual alerts (lamps).

If EGPWS suppression is not desired, the Audio Inhibit discretecan be left disconnected.

Recommendation: AlliedSignal recommends the use of theAudio Inhibit feature to maintain appropriate audio and visualprioritization in the cockpit.

ACTION: Review reference sections and record thepreferred suppression behavior at left.

-101 andon

3.44.2.2

4.2.2.2

Allied Signal, Inc.





ReferenceSection


Glideslope Cancel

2000’ Standard G/SCancel


Alternate G/S Cancel

The Standard Glideslope Cancel allows the crew to manuallycancel the “Glideslope” alert when below 2000 feet RadioAltitude. The cancel is automatically reset when above 2000feet RA. (Some Aircraft Types use 1000 feet RA for theStandard G/S Cancel.)

The Alternate Glideslope Cancel allows the crew to manuallycancel and re-activate the “Glideslope” alert any time at anyaltitude. This option is not currently being certified by the FAAin Part 121 aircraft.

ACTION: Review reference sections and record theGlideslope Cancel preference at left.

-101 andon

3.54.2.2

4.2.2.3

If the Standard GlideslopeCancel is selected, doesthe Aircraft Type supportthe G/S Cancel Altitude

preference?

Steep Approach

Enabled

Disabled

Steep Approach desensitizes the Mode 1 (Excessive DescentRate) alert boundaries to permit safe but steeper than normalinstrument precision approaches (e.g. MLS or GPSapproaches) without unwanted alerts.

This feature is not available on all aircraft .

NOTE: This option is controlled by discrete inputs (notProgram Pins).

ACTION: Review reference sections and record thepreferred Steep Approach enabling at left.

-101 andon

3.64.5.30

If Steep Approach isselected, does the Aircraft

Type support it?

Allied Signal, Inc.





ReferenceSection


Alternate Mode 4B 2

Use Alt. Mode 4B

Do not use Alt. Mode4B

Mode 4 provides alerts for insufficient terrain clearance withrespect to phase of flight and speed. Alternate Mode 4Bprevents nuisance MK V EGPWC warnings during approacheswith the gear up.

Prior to version –208, Alternate Mode 4B is activated only bythe Aircraft Type.

Recommendation: AlliedSignal recommends the use ofAlternate Mode 4B and the flap override switch for all GeneralAviation and Bizjet aircraft.

ACTION: Review reference sections and record thepreferred Mode 4B functionality at left.

-208 andon

3.74.2.10

If installing version –206 orolder and Alternate Mode4B is selected, does the

Aircraft Type select itAlternate Mode 4B?

Windshear Detection andAnnunciation

W/S Enabled & W/SCaution uses no voice

W/S Enabled & W/SCaution uses voice

W/S Enabled & No W/SCaution

W/S Disabled

W/S Disabled & W/SINOP discrete disabled

The MK V EGPWS provides a reactive Windshear capabilitythat is enabled only by the Aircraft Type. Windshear can bedisabled during installation.

The basic W/S enabling includes both the W/S Warning andW/S Caution. This W/S Caution does not include an audio(voice) alert.

Recommendation: AlliedSignal recommends disabling theWindshear INOP discrete if Windshear is disabled.

ACTION: Review reference sections and record thepreferred Windshear functionality at left.

-101 andon

3.84.2.3

If Windshear is required,does the Aircraft Type

enable it?

Allied Signal, Inc.





ReferenceSection


Lamp Format 2

Lamp Format 1

Lamp Format 2

The Aircraft Type defines the lamp configuration (Lamp FormatType 1 or 2) for an installation. The lamp formats are definedin the reference section. Beginning with version –208, LampFormat Type 2 can be selected via Program Pin if the AircraftType defines the lamp configuration as Lamp Format Type 1.

Note: AlliedSignal recommends Lamp Format Type 2.

ACTION: Review reference sections and record thepreferred Lamp Format at left.

-208 andon

3.94.2.3

4.2.3.2

If installation version –208or newer and Lamp Format

Type 1 is required, doesthe Aircraft Type select it?

ORIf installing version –206 or

older, does the AircraftType select the required

Lamp Format?

Simulator Installation

Aircraft Installation


The Simulator Reposition Program Pin and discrete inputs areused to enable instantaneous repositioning for non-aircraftinstallations. Refer to Aircraft Type to determine if theSimulation Reposition discrete input is defined for the AircraftType.

ACTION: Review reference sections and record theinstallation location at left.

-208 andon

3.104.2.4

4.2.4.2

If this installation is in asimulator, does the A/CType support the SimulatorReposition discrete input?

Note: A simulatorinstallation is possible evenif the Simulation Repositionoption is not available.

TAD & TCF(Enhanced Feature

Control)

Enabled

Disabled

The Terrain Awareness & Display feature computes terrainclearance envelopes ahead of the aircraft, issues and displaysthe terrain data relative to aircraft altitude.

The Terrain Clearance Floor (TCF) algorithm identifiespremature descent for approaches regardless of aircraftconfiguration.

ACTION: Review reference sections and record thepreferred TAD & TCF enabling at left.

-101 andon

3.113.11.14.2.4

4.2.4.1

Allied Signal, Inc.





ReferenceSection


Obstacle Awareness

Enabled

Disabled

Added in version –204, Obstacle Awareness warns of man-made obstacles at least 100’ taller than surrounding terrain.Obstacle data is currently available for North America and partsof the Caribbean. Not all obstacles will be contained in thedatabase.

Note: TAD & TCF must be enabled for Obstacle Awareness.

ACTION: Review reference sections and record thepreferred Obstacle Alerting enabling at left.

-204 andon

3.113.11.24.2.4

4.2.4.1

Peaks Mode 1

Enabled

If installing version –208 ornewer and the Peaks

display mode is preferred,does the selected display

support it?

Disabled

Peaks mode is an alternate means of displaying terrain datathat provides increased situational awareness by displayingabsolute terrain elevations in addition to the standard modepresentation.

Note: For version –206, TAD, TCF and Obstacles must beenabled if Peaks mode is enabled. Beginning with –208, TADand TCF must be enabled if Peaks mode is enabled.

ACTION: Review reference sections and record thepreferred Peaks Mode enabling at left.

-206 andon (somedisplays)

3.113.11.34.2.4

4.2.4.1 If Obstacle Awareness isdesired, is version –204 or

newer being installed?

Bank Angle Callouts(Bizjet)

Enabled

Disabled

Bank Angle Callouts may be enabled or disabled.

ACTION: Review reference sections and record the BankAngle enabling at left (if Bizjet aircraft).

-101 andon

3.123.12.14.2.5

4.2.5.1

Is the Aircraft Class“Bizjet”?

Allied Signal, Inc.





ReferenceSection


Bank Angle Algorithm(Commercial AT)

AlliedSignal algorithm

Bank Angle Option 1

Bank Angle Option 2

Disabled

For Commercial Air Transport Aircraft any one of the threeBank Angle algorithms described below may be selected orBank Angle callouts may be disabled.

ACTION: Review reference sections and record the BankAngle functionality at left (if Commercial AT aircraft).

BAOptions 1

& 2added in

-202

3.123.12.24.2.5

4.2.5.2

Is the Aircraft Class“Commercial AT”?

Altitude Callout Menu

Altitude Callout Menu ID

___________________

“Minimums” only

Disabled

Each Mode 6 Altitude Callout Menu listed in Appendix Bdefines a set of altitude awareness callouts. The optional“Smart 500” foot callout will issue a “500” foot callout when theaircraft is 500’ AGL. As an alternative to the predefined calloutmenus, a “Minimums” only callout is possible.

Recommendation: AlliedSignal recommends the use of the“Smart 500” callout if the selected menu does NOT contain a500’ callout or if all callouts in the selected menu are below500’. AlliedSignal recommends at least a callout at 500’ and a“Minimums“-type callout.

ACTION: Review reference sections and record theselected Altitude Callout menu or the altitude calloutbehavior at left.

Notes for installer:� Is ARINC 429 DH required? ______� Is DH discrete input required? ______

-101 andon

3.134.2.64.5.24.5.5

If the selected AltitudeCallout Menu includes an“Approaching Minimums”-type callout, is the ARINC429 Decision Height inputavailable for the Aircraft

Type?

Allied Signal, Inc.





ReferenceSection


Audio Menu Selection

Audio Callout Menu ID

___________________

One of seven Basic GPWS (non-altitude) alert menus must beselected to provide Basic GPWS callouts. Refer to Appendix Cfor a complete definition of each menu. DGAC-registeredaircraft are required to use Audio Menu #1.

Recommendation: Except for DGAC-registered aircraft,AlliedSignal recommends the Basic Audio Menu (Menu 0).

ACTION: Review reference sections and record theselected Audio Callout Menu at left.

-101 andon

3.144.2.7

Audio Declutter

Enabled

Disabled

Audio Declutter prevents excessive aural alerts and warningsby preventing an alert or warning from being constantlyrepeated while the condition remains true.

ACTION: Review reference sections and record the AudioDeclutter enabling at left.

-101 andon

3.154.2.8

4.2.8.3

Alert Volume

High Volume

Medium Volume

Low Volume

The Alert volume level applies to the Audio menu (warningsand cautions) and sets the baseline volume for the Mode 6callouts (altitude and bank angle callouts). The Aircraft Typedefines the default “Audio Volume”.

For –206 and on: The default Audio volume must be used ifAudio Declutter is disabled.

ACTION: Review reference sections and record thepreferred Audio volume at left.

“Medium”added in

-206

3.164.2.8

4.2.8.14.7

Allied Signal, Inc.





ReferenceSection


Mode 6 Volume

Default Volume

-6dB (permanent)

-6dB (temporary)

-3dB(version-206 and on)

-3dB & -6dB (perm.)(version-206 and on)

-3dB & -6dB (temp.)(version-206 and on)

The default Mode 6 volume is based on the Audio volume andthe Aircraft Type’s Mode 6 volume.

The Mode 6 volume can be either temporarily or permanentlyreduced 6dB below its default volume. Many installations usethe windshield wiper control to reduce the volume when thewipers are off and restore it to its default level when the wipersare on (and cabin noise increases).

For version –206 and on: An additional control is available topermanently reduce the Mode 6 volume an additional 3dB.This control may be used separately or in conjunction with the–6dB control described above.

Note: The –3dB option is not available if Audio Declutter isdisabled.

ACTION: Review reference sections and record thepreferred Mode 6 (altitude callout) volume at left.

Note: -6dB options controlled by Mode 6 Volume Controldiscrete input. –3dB option controlled by PPIN 11.

-3dBoption

added in-206

3.174.2.8

4.2.8.24.5.23

If the selected Mode 6volume is __________,does the Aircraft Type

select “Low” for the initialMode 6 Volume?

Allied Signal, Inc.





ReferenceSection


EGPWS DisplayPop-up

Yes (Pop Up)

No (Do not Pop Up)

A terrain display “pops up” when an EGPWS alert conditionoccurs and the display switches to terrain data from whateverwas being displayed prior to the alert condition (typicallyweather).

Terrain display pop up behavior is controlled by either theEGPWS or by the display itself as defined in the Aircraft Type’sDisplay Options & Peaks Availability Worksheet.

ACTION: Review reference sections; indicate whetherterrain displays should pop up over non-terrain displays atleft. (Assumes display behavior is controlled by theEGPWS.)

-101 andon

3.184.2.9

4.2.9.1

For the display selectedabove, does either the

default or alternate Pop Upbehavior support the

selected Pop Up behavior?

Predictive WindshearSystem

PWS Option 1

PWS Option 2

An external Predictive Windshear System (PWS) may beavailable on the aircraft and can be used in addition or in placeof the reactive windshear system available as part of the MK VEGPWS.

Only the PWS interface(s) defined in the Aircraft Type’s“Optional System Inputs” table are supported by the AircraftType.

NOTE: The reactive windshear Caution must be disabled if aPWS is used.

ACTION: Review reference sections and indicate at leftwhich, if any, of the optional PWS interfaces should beused.

-101 andon

3.194.2.9

4.2.9.2

Does the Aircraft Typesupport the selected

optional inputs?

Allied Signal, Inc.





ReferenceSection


Optional System Inputs

Internal GPS

Optional Inputs Select

Dual External GPS

Single External GPS

Dual GPIRS

Single GPIRS

Triple LRRA

Dual LRRA

Beginning with version –208, the MK V EGPWC (part number965-0976-020-xxx-xxx) is available with an internal RS-232GPS receiver. Use of the internal GPS receiver is optional.

The Aircraft Type’s “Optional System Inputs” table defines anyoptional interfaces supported by the Aircraft Type. The ARINC429 Input Channel Assignments worksheet, Analog InputsWorksheet and Radio Altimeter Formats worksheet also showthese interfaces.

If the internal GPS receiver is activated, GPS inputs via theARINC 429 cannot be enabled. (See Optional System Inputsabove.)

ACTION: Review reference sections and record theoptional inputs to be used at left.

InternalGPS -

208 andon

3.204.2.10

4.2.10.1


optional inputs?

GPS Altitude Reference 2

Referenced to meansea level

Referenced to WGS-84

Prior to version –208, the GPS Altitude (label 076) must bereferenced to mean sea level. Beginning with version –208,the GPS Altitude may be referenced to either mean sea level orWGS-84.

ACTION: Review reference sections and record the GPSaltitude reference at left.

-208 andon

3.214.2.13

1 Added in –206.2 Added in –208.3 Available only for MK V ECPWC part numbers 965-0976-020-xxx-xxx.


Allied Signal, Inc.


3.1 Aircraft Type

An Aircraft Type must be specified for the installation. The Aircraft Type defines the basic

operating environment of the MK V EGPWC by defining the specific aircraft model, electrical

interfaces and non-selectable features. The Aircraft Type controls the availability of some of the

selectable features. A single aircraft model may have several Aircraft Types to allow for different

on-board systems and features.

Issues to consider when selecting an Aircraft Type:

� Prior to version –208, the actual aircraft configuration must exactly match the first entry

(Program Pin State 1) in the Aircraft Type’s “Display Options & Peaks Availability” worksheet.

� Beginning with version –208, alternate display configurations are defined for some Aircraft

Types. The actual aircraft configuration must exactly match one of the display options

available for the version being installed.

� The aircraft configuration must match the required ARINC 429 and analog inputs for the

Aircraft Type. Refer to the “Required System Inputs” section of the Aircraft Type Description

and the Analog Inputs worksheet. Note: The “Optional System Inputs” may provide

additional input options or provide the capability to replace certain of the required inputs.

� If, after completing the worksheet, no Aircraft Type supports the installation contact

AlliedSignal at www.egpws.com or call the GPWS Hotline (refer to Section 8).

The following process should be used when selecting an Aircraft Type:

1. Review the Aircraft Types defined in Appendix A for the aircraft model. A guide for readingand using the Aircraft Type Tables is provided at the beginning of Appendix A.

2. If only one Aircraft Type is defined for the aircraft model, this Aircraft Type must be selected

for the installation. If multiple Aircraft Types are defined for the aircraft model, use the issues

described above to eliminate candidate Aircraft Types that are incompatible with the aircraft

configuration.

Record the Aircraft Type Number(s) under the “Comparison of Candidate Aircraft Types

versus Feature Selections” in Table 3-1 MK V EGPWS Feature Selection Worksheet.

Hint: When filling out the Feature Selection Worksheet, either complete the Feature and Option

Selections (left side) and then compare choices to the Aircraft Type(s) OR if there is only one

candidate Aircraft Type compare the choices to the Aircraft Type as each feature selection is

made.

Allied Signal, Inc.


3.2 Display Selection

Terrain is displayed on an existing display (typically the same display used to display weather

data). Display discussions apply only to the displays for terrain data.

The Aircraft Type’s “Display Options & Peaks Availability” worksheet in Appendix A identifies the

specific display interfaces supported by each Aircraft Type and MK V EGPWS version.

Issues to consider when identifying the terrain display:

� Terrain displays are only used if TAD and TCF are enabled (refer to Section 3.11.1).

� Prior to version –208, only the PPIN State 1 display is available for any Aircraft Type.

� For version –208 and later, some Aircraft Types have multiple display options available.

� Display behaviors and Peaks Mode availability are defined by the display.

� Some displays support auto-ranging to 10 nautical miles.

Review the Display column in the Display Options & Peaks Availability Worksheet for the display

options each Aircraft Type (Appendix A).

For each candidate Aircraft Type, record the PPIN State numbers for each display that matches

the aircraft configuration in the Aircraft Type comparison section (right side) of Table 3-1 MK V

EGPWS Feature Selection Worksheet.

Allied Signal, Inc.


3.3 Altitude Correction

Corrected Barometric Altitude can be measured relative to mean sea level (QNH) or field

(runway) elevation (QFE). Selection of the altitude correction method should be based on how

and where the aircraft will be operated. If the aircraft operates in a QFE environment full-time,

select QFE.

QNH is barometric altitude corrected to mean sea level and is the most common correction

format.

QFE is barometric altitude corrected to read zero feet at the runway regardless of the mean sea

level altitude of the runway.

Issues to consider when selecting the altitude correction format:

� QNH should be selected if the aircraft will be operating in a QNH environment or if geometric

altitude is available via direct GPS input.

� If geometric altitude is available, the aircraft can be strapped for QNH even if the aircraft is

operating in a QFE environment.

� Only select QFE if the operating environment is QFE 100% of the time.

� Terrain Awareness & Display must be inhibited if the aircraft is operating in the opposite

environment (QFE vs. QNH) unless geometric altitude is available via the GPS inputs.

� The Altitude Correction selection cannot be altered during flight since a Program Pin change

is required to revise the selection.

NOTE: Geometric Altitude is available if direct GPS inputs has GPS altitude and GPS Vertical

Figure of Merit (VFOM).

Indicate the selected Altitude Correction method in Table 3-1 MK V EGPWS Feature Selection

Worksheet.

Allied Signal, Inc.


3.4 EGPWS Suppression

The MK V EGPWS Audio Inhibit discrete input normally suppresses EGPWS audio callouts

(except reactive Windshear) manually via a cockpit-mounted switch or automatically via the

DSWC and PWS computers. This feature can be modified to also suppress visual (lamp) alerts

or it can be disabled by not providing the EGPWS Suppression discrete input. Refer to Section

4.5.4 for more information on Audio Inhibit.

Activation of the Audio Inhibit input for more than 60 seconds will result in the “Audio Inhibit

Monitoring” fault (described in Section 4.5.4) when either of the following conditions is true:

� Audio and visual EGPWS suppression is enabled, or

� The Aircraft Type enables audio Inhibit Monitoring.

Note: If EGPWS Suppression is not desired, do not connect the Audio Inhibit discrete.

Recommendation: AlliedSignal recommends the use of the Audio Inhibit feature to maintain

appropriate audio and visual prioritization in the cockpit.

Indicate the selected EGPWS Suppression in Table 3-1 MK V EGPWS Feature Selection

Worksheet.

3.5 Glideslope Cancel

The standard Glideslope Cancel allows the crew to manually cancel the “Glideslope” alert when

below 2000 feet Radio Altitude. The Glideslope Cancel is automatically reset when ascending

above 2000 feet Radio Altitude or descending below 30 feet. For some Aircraft Types, the crew

can manually cancel the “Glideslope” alert when below 1000 feet. For these Aircraft Types, the

automatic Glideslope Cancel Reset altitude is also 1000 feet. The Aircraft Type’s Glideslope

Cancel Alt. entry defines the Glideslope Cancel altitude.

The Alternate Glideslope Cancel allows the crew to manually cancel and re-activate the

“Glideslope” alert any time at any altitude. It is automatically reset when the aircraft is on the

ground or is configured for a Go-Around (flaps not in landing configuration or gear up). AlternateGlideslope Cancel requires a cockpit annunciation that this cancel is in effect.

The Alternate Glideslope Cancel is manually reset via the G/S Cancel switch. Note that the

cockpit annunciation will extinguish.

Note: Alternate Glideslope Cancel cannot be FAA certified in Part 121 aircraft.

Indicate the preferred Glideslope Cancel in Table 3-1 MK V EGPWS Feature Selection

Worksheet.

Allied Signal, Inc.


3.6 Steep Approach

Steep Approach desensitizes the Mode 1 (Excessive Descent Rate) alert boundaries to permit

safe but steeper than normal instrument precision approaches (e.g. MLS or GPS approaches)

without unwanted alerts.

This feature is not available on all aircraft. The Aircraft Type’s Steep Approach entry indicates

availability of this feature.

Indicate the preferred Steep Approach implementation in Table 3-1 MK V EGPWS Feature

Selection Worksheet.

3.7 Alternate Mode 4B

Mode 4 provides alerts for insufficient terrain clearance with respect to phase of flight and speed.

Mode 4A is active during cruise and approach with gear not in landing configuration and issues

the “Too Low Gear” warning. Mode 4B is active during cruise and approach with the gear down

and flaps not in landing configuration and issues the “Too Low Flaps” annunciation. The EGPWS

normally transitions from Mode 4A to Mode 4B when the Landing Gear is lowered (Landing Gear

Discrete active). When Alternate Mode 4B is enabled the EGPWS will transition from Mode 4A to

Mode 4B when either the Landing Gear is lowered (Landing Gear Discrete active) or the Flaps (or

Flap Override switch) are in landing configuration (Landing Flaps Discrete active). This allows

the pilot to approach with gear up without nuisance MK V EGPWC warnings.

Issues to consider when selecting Mode 4B functionality:

� Prior to version –208, Alternate Mode 4B is activated only by the Aircraft Type (refer to the

Aircraft Type’s Aircraft Description in Appendix A).

� Beginning with version –208, the preferred Mode 4B functionality is selectable.

Recommendation: AlliedSignal recommends the use of Alternate Mode 4B and the flap override

switch for all General Aviation and Bizjet aircraft.

Indicate the preferred Mode 4B functionality in Table 3-1 MK V EGPWS Feature Selection

Worksheet.

Allied Signal, Inc.


3.8 Windshear Detection and Annunciation

The windshear detection and annunciation feature is a reactive windshear system that provides a

Windshear Caution and/or Windshear Warning during a windshear event.

Each Aircraft Type defines Windshear detection and annunciation availability. If the Aircraft Type

provides the Windshear functions, they can be modified via Program Pin. If the Aircraft Type

disallows Windshear, it cannot be enabled.

If windshear detection and annunciation is available, the default functionality provides both aural

and visual Windshear Warnings and only visual Windshear Cautions. Its function can be

modified as follows:

� Windshear detection and annunciation can be completely disabled

� The Windshear Caution can be disabled without affecting the Windshear Warning

� An audio output can be added to the visual Windshear Cautions. The voice alert will be

“Caution, Windshear”.

� The Windshear INOP discrete output can be disabled if Windshear is disabled or is not

available per the Aircraft Type.

Recommendation: If Windshear is disabled, AlliedSignal recommends disabling the Windshear

INOP discrete.

Issues to consider when selecting reactive Windshear functionality:

� If the aircraft has a Predictive Windshear System, the reactive Windshear Caution must be

disabled per FAA requirements.

Indicate the preferred reactive Windshear functionality in Table 3-1 MK V EGPWS Feature


Allied Signal, Inc.


3.9 Lamp Format

The Aircraft Type defines the operation of the read and amber GPWS cockpit lamps (Lamp

Format Type 1 or 2) for an installation. The lamp formats are as follows:

� Lamp Format Type 1: Amber “Below G/S” lamps are driven by the GPWS Alert discrete

output for a Below Glideslope Caution alert. Red “GPWS” lamps are driven by the

remaining non-windshear caution and warning alerts.

� Lamp Format Type 2: Amber “GPWS” lamps are driven by the non-windshear (i.e GPWS)

caution alerts and red “Pull Up” lamps are driven by the non-windshear (i.e. GPWS) warning

alerts. The warnings generate “Pull Up” audio messages.

This option functions as follows:

� The Aircraft Type selects the default Lamp Format.

� Beginning with version –208, if the Aircraft Type selects Lamp Format Type 1 then Lamp

Format Type 2 can be selected via Program Pin.

� Prior to version –208, the Lamp Format cannot be changed.


Indicate the selected lamp format in Table 3-1 MK V EGPWS Feature Selection Worksheet.

3.10 Simulator Installation

Instantaneous repositioning (using the latitude and longitude inputs) typical of a simulator

installation is supported for Aircraft Types whose Discrete Inputs Worksheet defines a “Simulator

Reposition” input. Stationary laboratory installations do not require the simulator repositioning

capability and can use Aircraft Types that do not support repositioning.

Note: This feature must be disabled for all aircraft installations.

Indicate the installation location in Table 3-1 MK V EGPWS Feature Selection Worksheet.

Allied Signal, Inc.


3.11 Enhanced Feature Control

Prior to version –204, the enhanced features are Terrain Awareness Display and Terrain

Clearance Floor. Obstacle Awareness was added in version -204. Peaks Mode was added for

selected Aircraft Types in version –206. These features are described in the following

subsections. Feature availabilty for each software version is shown in the table below.

SoftwareVersion Features Available

-101 to -202 � TAD and TCF

-204 � TAD and TCF� TAD, TCF and Obstacle Awareness

-206� TAD and TCF� TAD, TCF and Obstacle Awareness� TAD, TCF, Obstacle Awareness and Peaks Mode1

-208 and on

� TAD and TCF� TAD, TCF and Obstacle Awareness� TAD, TCF and Peaks Mode1

� TAD, TCF, Obstacle Awareness and Peaks Mode1

1 Depends on selected display.

3.11.1 Terrain Awareness & Display and Terrain C learance Floor

Terrain Awareness & Display feature continuously computes terrain clearance envelopes ahead

of the aircraft, issues alerts if the boundaries of these envelopes conflict with terrain elevation

data in the terrain database and displays the terrain data relative to aircraft altitude.

The Terrain Clearance Floor (TCF) algorithm identifies premature descent for approaches

regardless of aircraft configuration. It creates a terrain clearance envelope around the airport to

provide protection against controlled flight into terrain situations beyond that of the basic GPWS.

Issues to consider when selecting TAD & TCF enabling:

� TAD & TCF must be enabled if Obstacle Awareness is enabled.

� For version –206, TAD, TCF and Obstacles must be enabled if Peaks mode is enabled.

� Beginning with –208, TAD and TCF must be enabled if Peaks mode is enabled.

� If no terrain display will be used in this installation, do not enable TAD and TCF.

Indicate the preferred TAD & TCF enabling in Table 3-1 MK V EGPWS Feature Selection

Worksheet.

Allied Signal, Inc.


3.11.2 Obstacle Awareness

The Obstacle Awareness feature adds a database of (man-made) obstacles that are at least 100

feet taller than the surrounding terrain to the Terrain Awareness Alerting calculations. Obstacle

data is currently available for North America and parts of the Caribbean. Not all obstacles will be

contained in the database.

Issues to consider when selecting Obstacle Awareness enabling:

� Obstacle Awareness is available for version –204 and on.

� TAD & TCF must be enabled if Obstacle Awareness is enabled.

Indicate the preferred Obstacle Awareness enabling in Table 3-1 MK V EGPWS Feature


3.11.3 Peaks Mode

Available for selected Aircraft Types starting with version –206, Peaks mode is an alternate

means of displaying terrain data. The standard terrain display mode displays terrain relative to

the aircraft altitude that is within the aircraft envelope (the terrain is above or not more than 2000

feet below the aircraft). The terrain display is typically blank during the cruise portion of a flight.

Peaks mode provides increased situational awareness by displaying absolute terrain elevations in

addition to the standard mode presentation.

Issues to consider when selecting Peaks mode enabling:

� Peaks mode is available for some displays beginning with version –206. The display

selection determines the availability of Peaks mode for the installation.

� For version –206, TAD, TCF and Obstacles must be enabled if Peaks mode is enabled.

� Beginning with –208, TAD and TCF must be enabled if Peaks mode is enabled.

Indicate the preferred Obstacle Awareness enabling in Table 3-1 MK V EGPWS Feature


Allied Signal, Inc.


3.12 Bank Angle Callout Activation

Bank Angle Callout options depend on whether the aircraft class is Business Jet (Bizjet) or

Commercial Air Transport (AT) as defined by the Aircraft Type’s Aircraft Class. (Bizjet includes

General Aviation (GA) aircraft.)

3.12.1 Bank Angle Callout Activation for Bizjet Air craft

Bank Angle callouts can be enabled or disabled for Aircraft Types whose Aircraft Class is “Bizjet”

This Aircraft Class includes all General Aviation aircraft. All Bizjet aircraft use a Bank Angle

algorithm provided by AlliedSignal.

For Bizjet aircraft, indicate the preferred Bank Angle Callout enabling in Table 3-1 MK V EGPWS

Feature Selection Worksheet.

3.12.2 Bank Angle Callout Activation for Commerc ial Air Transport Aircraft

Bank Angle callouts can be enabled or disabled for Commercial AT aircraft. Any one of the three

Bank Angle algorithms described below may be selected for Commercial AT aircraft.

The AlliedSignal algorithm bases Bank Angle callouts on the aircraft’s roll angle versus Radio

Altitude (RA).

Bank Angle Option 1 uses the basic Boeing algorithm. Callouts are annunciated when the aircraft

roll crosses any one of three thresholds: 35O, 40O or 45O.

Bank Angle Option 2 callouts use the Boeing algorithm described above when the aircraft is

above 130 feet Radio Altitude (RA) and the AlliedSignal algorithm when the aircraft is at or below

130 feet.

The algorithms are described in more detail in the Product Specification for the Enhanced Ground

Proximity Warning System Sections 6.4.4 – 6.4.6.

Recommendation: AlliedSignal recommends the use of a Bank Angle algorithm.

For Commercial AT aircraft, indicate the selected Bank Angle algorithm or indicate that Bank

Angle Callout should be disabled in Table 3-1 MK V EGPWS Feature Selection Worksheet.

Allied Signal, Inc.


3.13 Altitude Callout Menu Selection

The Mode 6 Altitude Callout Menus are listed in Appendix B of this document and define the

available altitude awareness callouts.

Issues to consider when selecting altitude callout functionality:

� The “Approaching Minimums” or “Approaching Decision Height” callout is issued on descent

below Decision Height plus 80 or 100 feet respectively. The “Fifty Above” and “Plus

Hundred” callouts are issued at 50 and 100 feet above Decision Height respectively. These

callouts require an ARINC 429 Decision Height (DH) input not provided by all Aircraft Types

(refer to the Aircraft Type’s ARINC 429 DH entry). If the ARINC 429 DH is not supported,

selecting a menu containing an “Approaching Minimums”-type callout will result in error

messages and no Mode 6 callouts.

� The “Minimums”, “Decision Height” or “Decide” callout is issued when the aircraft descends

below the Decision Height setting.

� As an alternative to the predefined callout menus, a “Minimums” only callout is possible.

� Menus containing an optional “Smart 500” foot callout will issue a “500” foot callout when the

aircraft descends to 500’ RA. This callout is active only during non-precision approaches or

when the Glideslope or Localizer deviation is greater than 2 dots. If the Smart 500’ callout is

selected and the altitude callout menu includes a 500-foot callout, then that callout will

function as the Smart 500’ callout.

Recommendation: AlliedSignal recommends the use of the “Smart 500” callout if the selected

menu does NOT contain a 500’ callout or if all callouts in the selected menu are below 500’.

AlliedSignal recommends at least a callout at 500’ and a “Minimums “-type callout.

Indicate the selected altitude callout functionality in Table 3-1 MK V EGPWS Feature Selection

Worksheet.

Allied Signal, Inc.


3.14 Audio Menu Selection

One of seven Basic GPWS (non-altitude) alert menus must be selected to provide Basic GPWS

callouts. Refer to Appendix C for a complete definition of each menu. DGAC-registered aircraft

are required to use Audio Menu #1.

Recommendation: AlliedSignal strongly recommends Menu 0 (the Basic Audio Menu) except

for DGAC-registered aircraft. Menu 0 is the default menu.

Indicate the selected Audio Callout Menu in Table 3-1 MK V EGPWS Feature Selection

Worksheet.

3.15 Audio Declutter Disable

Audio Declutter prevents excessive aural alerts by preventing a caution or warning alert from

being constantly repeated while the condition remains true. Entry into an EGPWS caution or

warning envelope generates the appropriate EGPWS lamp and aural message. If the situation

worsens by a pre-determined amount, the alert or warning will be repeated. The appropriate

EGPWS lamp remains illuminated while the aircraft is in the alert or warning envelope. Refer to

the Product Specification for the Enhanced Ground Proximity Warning System Section 6.2 for

more information on how Audio Declutter functions in each basic GPWS mode.

Issues to consider:

� Audio Declutter defaults to active and must be turned off if it is not wanted.

� For version –206 and on, if Audio Declutter is disabled the default Basic GPWS volume must

be used and the Alternate Mode 6 volume reduction is not available.

Recommendation: AlliedSignal recommends the Audio Declutter feature be left active. (This

feature defaults to active.)

Indicate the selected Audio Declutter enabling in Table 3-1 MK V EGPWS Feature Selection

Worksheet.

Allied Signal, Inc.


3.16 Alert Volume Control

Each Aircraft Type has a default alert output volume level defined as the “Normal Volume” in the

Aircraft Type table. This volume level applies to the Audio menu callouts and sets the baseline

volume for the Mode 6 (altitude and bank angle) callouts. The volume level for altitude and bank

angle callouts is discussed in Section 3.17.

The high and low volumes for alert callouts to the cockpit speakers and headsets are shown in

the table below. Both the 8 and 600 ohm outputs are always provided. (The difference between

the high and low volumes is approximately 6dB.)

Basic GPWSVolume

600 OhmHardware(headset)

8 Ohm Hardware(cockpitspeaker)

High 25mW 2W

Medium 1 High –3dB High –3dB

Low 4mW 0.5W1 Added in –206.

Issues to consider when selecting the alert volume:

� For version –206 and on, a Medium volume level, approximately equal to High volume – 3dB,

is available for Basic GPWS callouts.

� For –206 and on, the default Alert volume set by the Aircraft Type must be used if Audio

Declutter is disabled.

� If a lower alert volume is selected, the Mode 6 (altitude and bank angle) callout volume is

also lowered.

Indicate the selected Normal Audio (alert) volume in Table 3-1 MK V EGPWS Feature Selection

Worksheet.

Allied Signal, Inc.


3.17 Mode 6 Volume

The selected alert volume (Section 3.16) defines the baseline Mode 6 volume that is modified as

defined by the Aircraft Type Mode 6 volume entry. Mode 6 provides the altitude and bank angle

callouts. If the Aircraft Type’s Mode 6 Volume is:

� “Normal” - the Mode 6 volume defaults to the alert callout volume.

� “Low” - the Mode 6 volume defaults to the selected alert volume less 6dB.

Issues to consider when selecting the Mode 6 volume:

� The Mode 6 volume can be either temporarily or permanently reduced 6dB below its default

volume by using the Mode 6 Volume Control discrete input. Many installations use the

windshield wiper control to reduce the volume when the wipers are off and restore it to its

default level when the wipers are on (and cabin noise increases).

� For version –206 and on, an additional independent Program Pin control is available to

permanently reduce the Mode 6 volume an additional 3dB. This control may be used

separately or in conjunction with the –6dB control described above.

� Audio Declutter must be enabled if the –3dB option is selected.

Default Mode 6 Volume Mode 6 Volume OptionsMode 6 VolumePer A/C Type

Actual DefaultVolume Version –204 Version –206 and On

“Normal”Same as theselected alert

volume

“Low” Selected alertvolume -6dB

A. Default VolumeB. Default Volume -6dB

(Permanent or Connectto Switch)

A. Default VolumeB. Default Volume -6dB

(Permanent or Connectto Switch)

C. Default Volume -3dB(not available if AudioDeclutter is disabled)

D. Default Volume -9dB(Both B and C) (notavailable if AudioDeclutter is disabled)

Indicate the selected Mode 6 volume modifications in Table 3-1 MK V EGPWS Feature Selection

Worksheet.

Allied Signal, Inc.


3.18 EGPWS Display Pop-up Selection

A terrain display “pops up” when an EGPWS alert condition occurs and the display switches to

terrain data from whatever was being displayed prior to the alert condition (typically weather).

Terrain display pop up behavior is controlled by either the EGPWS or by the display itself as

defined in the Aircraft Type’s Display Options & Peaks Availability worksheet. Some Aircraft

Types do not support an Alternate Pop-up definition. Definitions of the pop-up terms are provided

at the beginning of Appendix A.

Indicate whether or not terrain displays should Pop Up over other data (typically weather) when

an EGPWS alert condition occurs in Table 3-1 MK V EGPWS Feature Selection Worksheet.

3.19 Predictive Windshear

An external Predictive Windshear System (PWS) may be available on the aircraft and can be

used in addition to or in place of the reactive windshear system available as part of the MK V

EGPWS.

Issues to consider when determining whether to provide PWS data to the MK V EGPWS:

� The Aircraft Type must have a defined optional interface that supports the PWS interface.

The Aircraft Type’s Optional System Inputs table shows any optional PWS inputs and the

control signals for enabling them. (Any PWS Option not listed in the Optional System Inputs

table is not applicable to the Aircraft Type.)

� The reactive Windshear Caution must be disabled if the aircraft has a PWS. Refer to Section

3.8 for information on disabling the Windshear Caution.

Indicate the PWS control signals, if any, to be enabled for PWS inputs in Table 3-1 MK V EGPWS


Note: The PWS control signals are uniquely defined for each Aircraft Type.

Allied Signal, Inc.


3.20 Optional System Inputs

The EGPWC may be configured to accept alternative, secondary and tertiary signal sources to

provide redundancy if the appropriate aircraft signal sources are available. The Aircraft Type’s

Optional System Inputs table specifies which additional signal sources may be provided and how

to configure the EGPWC to enable them.

Issues to consider when determining the optional inputs to provide:

� Beginning with version –208, the MK V EGPWC (part number 965-0976-020-xxx-xxx) is

available with an internal RS-232 GPS receiver. Use of the internal GPS receiver is optional.

� If the internal GPS receiver is activated, GPS inputs via the ARINC 429 cannot be enabled.

� In cases where multiple inputs are enabled by a single control mechanism, such as Dual

External GPS or Optional Input Select, all of the inputs must be provided.

� When signals enable mutually exclusive optional interfaces they are noted in the table.

� Beginning with version –206, some Aircraft Types support ARINC 743 format GPS data.

(Prior to –206, only ARINC 743A is supported.) If dual GPS inputs are provided, both inputs

must be the same format (either ARINC 743 or ARINC 743A). The default GPS format is

defined in the ARINC 429 Input Channel Assignments Worksheet. If applicable, the alternate

format is defined in the ARINC 429 Interface Modification Options Worksheet.

� Beginning with version –208, any GPS must have eight or more channels with Receiver

Autonomous Integrity Monitoring (RAIM) capability.

� Some optional inputs replace inputs defined as required. These are noted in the Optional

System Inputs table and in the ARINC 429 Input Channel Assignments Worksheet for the

Aircraft Type.

Indicate the optional input control signals, if any, to be enabled in Table 3-1 MK V EGPWS


Allied Signal, Inc.


3.21 GPS Altitude Reference

For version –206 only, the GPS Altitude (label 076) must be referenced to mean sea level.

Beginning with version –208, the GPS Altitude may be referenced to either mean sea level or

WGS-84.

Indicate the selected GPS Altitude Reference in Table 3-1 MK V EGPWS Feature Selection

Worksheet.

Allied Signal, Inc.


4 Electrical Installation Design

Table 3-1 MK V EGPWS Feature Selection Worksheet in the previous sect ion must becompleted prior to proceeding with this sect ion.

This section provides guidance for determining the wiring for the MK V EGPWS based on the

feature selections from Section 3 and additional information provided in this section.

System wiring is broken down into the following main components:

� Electrical Interfaces (Section 4.1)

� Program Pins (Section 4.2)

� Analog and Digital Inputs (Section 4.3)

� RS-232 Interface (Section 4.4)

� Discrete Inputs (Section 4.5)

� Digital Outputs (Section 4.6)

� Audio Outputs (Section 4.7)

� Discrete Outputs (Section 4.8)

Sample wiring diagrams for the most commonly used MK V EGPWS configurations are provided

in Appendix A with the Aircraft Type tables.

4.1 Electrical Interfaces

The MK V EGPWC requires a primary power input (either 115 VAC or 28 VDC input power

depending on the MK V EGPWC part number being installed) and ground. The MK V EGPWC

also provides a voltage reference output that may be used as an excitation voltage for an external

device.

4.1.1 Primary Power Input

Primary power should be connected as follows for both the 115 VAC and 28 VDC versions of the

MK V EGPWC.

Pin Signal

BP2 Power Hi (+)

BP3 Power Low (ground)

Allied Signal, Inc.


4.1.1.1 Specifications for Primary Power for the 115 VAC MK V EGPWC

The following specifications apply to the 115 VAC MK V EGPWC.

Nominal Input 115 VAC, 400 Hz

Normal Voltage Range 104 to 122 VAC RMS

Power Requirements

23 Watts if no warnings+1 Watt with warning voice over 8 ohm speaker+5 Watts with internal GPS (includes antenna power)+3.8 Watts with Phantom Power connections (2.7 dissipatedoutside of the EGPWC)32.8 Watts maximum

Recommended Power ControlDevice 2 Amp delayed action circuit breaker

4.1.1.2 Specifications for Primary Power for the 28 VDC MK V EGPWC

The following specifications apply to the 28 VDC MK V EGPWC.

Nominal Input 28 VDC

Normal Voltage Range 22.0 TO 29.5 VDC

Power Requirements

24 Watts if no warnings+3 Watts with warning voice over 8 ohm speaker+3.8 Watts with Phantom Power connections (2.7 dissipatedoutside of the EGPWC)30.8 Watts maximum70 Watts (typical) when heater blanket on1

Recommended Power ControlDevice 2 Amp delayed action circuit breaker1The heater blanket (965-1076-040-xxx-xxx only) turns on at temperatures � -20o C and turns offat temperatures � -10o C.2PWRL is not a floating input. 28 VDC must be applied to PWRH and ground to PWRL.

Allied Signal, Inc.


4.1.2 Chassis Ground

Chassis ground provides a redundant metal connection and should not be used a s a normal

current carrying conductor. Chassis ground should be connected as follows:

Pin Signal

BP4 GND_C

4.1.3 Voltage Reference Output

The voltage reference output is typically used as an excitation voltage for an external device such

as vane mounted potentiometers used to provide AOA to the EGPWC.

Pin Output Voltage Current Capability

TP2D 10.00 VDC +- 0.1% 10 milliamps

Allied Signal, Inc.


4.2 Program Pin Strapping

This section provides instructions for completing the Program Pin Strapping Worksheet (Figure

4.2-1), along with worksheets for the selected Aircraft Type in Appendix A. These worksheets are

intended to provide the information required for generating wiring diagrams for the MK V EGPWS.

Program Pins define the operational environment of the MK V EGPWC including aircraft make

and model, electrical interfaces and feature selections. This section provides instructions for

defining the Program Pin strapping for the features and options selected in Table 3-1 MK V

EGPWS Feature Selection Worksheet.

19 Program Pins are defined for MK V EGPWC versions –208 and on. 17 Program Pins are

defined for MK V EGPWC versions prior to -208. Program Pins 1 through 6 can be set to one of

eight states by strapping each Program Pin to one of six MK V EGPWC output discretes,

strapping it to ground or leaving the connection open. Beginning with version –208, the

remaining Program Pins can be set to 10 states; for older versions the remaining Program Pins

can be set to only eight states. During power-up initialization, the MK V EGPWC cycles the state

of these output discretes to determine its operating configuration.

Figure 4.2-1 Program Pin Strapping Worksheet shows the possible connections for each Program

Pin and is used to record the Program Pin strapping information required for generating wiring

diagrams. Explanations of the strapping options for each Program Pin are provided in the

sections below.

Allied Signal, Inc.


PPCOM (MP03A)

E G P W S A IR C R A F T C O N FIG U R A TIO N S TR A P P IN G

DOUTL1 (MP15D)

DOUTL4 (TP12C)DOUTL5 (TP12A)DOUTL7 (TP4D)

DOUTL2 (MP03D)

PPCNF2 (TP10B)PPCNF3 (TP10C)

PPCNF4 (MP4D)PPCNF5 (MP4B)PPCNF6 (MP08A)

PPCNF8 (MP05A)PPCNF7 (MP14D)

PPCNF12 (TP05B)

PPCNF9 (MP02C)PPCNF10 (MP04A)PPCNF11 (MP04C)

PPCNF13 (MP05B)PPCNF14 (TP02C)PPCNF15 (MP15C)PPCNF16 (MP08B)

CONFIGURATION SELECTION(NONE OR ONE SELECTION PER ROW)

DOUTL3 (MP07B)

GLIDESLOPE CANCEL

TERRAIN DISPLAYABLE #1

GPWS ALERTGPWS WARNING

WINDSHEAR WARNING

PPCNF1 (TP10A)

WINDSHEAR CAUTION

PROGRAM PIN COMMON

MULTIPLEXEDSELECTPINS

PROGRAM PINSAIRCRAFT TYPE #:

CALLOUT MENU #:

AIRCRAFT STRAP #2AIRCRAFT STRAP #1

AIRCRAFT STRAP #3

CALLOUT MENU STRAP #3CALLOUT MENU STRAP #2CALLOUT MENU STRAP #1

OPTIONAL GPS/GPIRSAUDIO MENU2 ILS/2 LRRA/3 LRRAGS CAN/EGPWS SUP/QFE SELAUDIO DECLUTTER/VOLUMEWINDSHEAR CONTROLTCF DIS/TAD DIS/SIM REPO

GPS SPEEDALT POPUP / PWS OPTIONSBANK ANG/ALT RADALT

2 Count each "Program Pin" row selected (PPCNF1-PPCNF16, PPCNF18 and PPCNF19), if the number iseven, then select this block (PPCNF17). The count of all program pins selected must be odd.

All "Select Pins" used as discrete outputs that are not pulled up to at least 12 VDCmust be isolated by the use of a diode.

1

1

3

3

3 Not available prior to -208.

AUDIO ONTERRAIN DISPLAYABLE #2

DOUTL6 (TP12B)DOUTL10(TP11A)

ALT DISPLAY SELECTION PPCNF18 (MP15A) 3

OPTIONS SELECTION PPCNF19 (MP15B) 3PPCNF17 (TP06D)PROGRAM PIN PARITY (ODD) 2

PROGRAM PIN STATES (State 1 is "open".) 2 3 4 5 6 7 8 9 10

Figure 4.2-1 Program Pin Strapping Worksheet

Note: After the correct Program Pin strapping is determined for this installation, it is possible that

several Program Pins will be connected to the same output discrete. This may be implemented

by daisy-chaining the Program Pins. However, DO NOT daisy-chain the output discretes as the

MK V EGPWC will produce an error message and will not function.

Allied Signal, Inc.


4.2.1 Aircraft Type (Program Pins 1 - 3)

The Aircraft Type Number identifies a specific aircraft model, electrical interfaces and non-

selectable features.

The Aircraft Types are defined in Appendix A and are organized by aircraft make and model. Aguide for reading and using the Aircraft Type tables is included in Appendix A. The

Program Pin strapping to select an Aircraft Type is shown in the “Program Pin Strapping for

Aircraft Type” table for the aircraft model.

Verify the selected Aircraft Type (see Table 3-1 MK V EGPWS Feature Selection Worksheet) is

consistent with the aircraft systems. If not, resolve any discrepancies with the owner or operator

before continuing.

Record the Aircraft Type Number and Program Pin strapping in Figure 4.2-1 Program Pin

Strapping Worksheet.

Allied Signal, Inc.


4.2.2 Altitude Correction, EGPWS Suppress and Glideslope Cancel(Program Pin 10)

Program Pin 10 controls the options for Altitude Correction, EGPWS Suppression and Glideslope

Cancel. These options are discussed in the following sections. Table 4.2.2-1 Program Pin 10

Worksheet shows the alternatives and Program Pin strapping for each of these options.

ProgramPin State

AltitudeCorrection

EGPWSSuppress

GlideslopeCancel

PPCNF10(MP4A)

Strapping1 Standard Open

2Audio Only

Alternate MP3A(PPCOM)

3 Standard MP15D

4

QNH

Audio & VisualAlternate MP3D

5 Standard MP7B

6Audio Only

Alternate TP12C

7 Standard TP12A

8

QFE

Audio & VisualAlternate TP4D

ThisInstallation

Table 4.2.2-1 Program Pin 10 Worksheet

Determine the Program Pin strapping (per Sections 4.2.2.1, 4.2.2.2 and 4.2.2.3) and record in

Figure 4.2-1 Program Pin Strapping Worksheet.

4.2.2.1 Altitude Correction

This Program Pin determines whether Corrected Barometric Altitude is measured relative to field

elevation (QFE) or to mean sea level (QNH).

Refer to Altitude Correction in Table 3-1 MK V EGPWS Feature Selection Worksheet for the

selected correction method.

Enter the selected Altitude Correction method in Table 4.2.2-1 Program Pin 10 Worksheet.

Allied Signal, Inc.


4.2.2.2 EGPWS Suppress

The EGPWS Suppress option determines whether activation of the “Audio Inhibit” discrete input

inhibits audio outputs (except for reactive windshear) or audio and visual outputs (except for

reactive windshear).

The Audio Inhibit discrete input is optional and can be left disconnected if EGPWS Suppression is

not desired.

Refer to the Non-Windshear EGPWS Suppress entry in Table 3-1 MK V EGPWS Feature

Selection Worksheet for the preferred setting of EGPWS Suppress.

Enter the selected EGPWS Suppress in Table 4.2.2-1 Program Pin 10 Worksheet (if the discrete

is not used, select Audio Only).

Section 4.5.4 contains information for wiring the Audio Inhibit input discrete.

4.2.2.3 Glideslope Cancel and Alternate Glideslope Cancel

Program Pin 10 determines whether the Standard or Alternate Glideslope Cancel will be used.

Refer to Glideslope Cancel in Table 3-1 MK V EGPWS Feature Selection Worksheet for the

selected Glideslope Cancel.

Alternate Glideslope Cancel requires a cockpit annunciation that the cancel is in effect.

This can be done using the Glideslope Cancel output discrete to control a cockpit light(refer to Section 4.8.4).

Enter the selected Glideslope Cancel option in Table 4.2.2-1 Program Pin 10 Worksheet.

Allied Signal, Inc.


4.2.3 Windshear Control and Lamp Format (Prog ram Pin 12)

Program Pin 12 controls the Windshear options and, beginning with version –208, provides for

the selection of Lamp Format Type 2. These options are described in the following sections.

ProgramPin State Windshear Windshear

CautionWindsh ear INOP

Output

Change toLamp

Format 2 1

PPCNF12(TP5B)

Strapping

1 Windshear Caution(no Voice) Open

2Normal Function

MP3A(PPCOM)

3Disabled Disabled

(no Caution)Disabled MP15D

4 Caution withVoice MP3D

5Windshear

DisabledNormal Function

No

MP7B

61 Windshear Caution(no Voice) TP12C

71Normal Function

TP12A

81 Disabled Disabled(no Caution) Disabled TP4D

91 Caution withVoice TP12B

101Windshear


Yes

TP11A

ThisInstallation

1Added in version –208.


Determine the Program Pin strapping per Table 4.2.3-1 Program Pin 12 Worksheet and record in


Allied Signal, Inc.


4.2.3.1 Windshear Control

The Aircraft Type may enable reactive windshear detection and annunciation. If the Aircraft Type

does not enable Windshear, it cannot be enabled. If enabled, Program Pin 12 can be used to

tailor the windshear feature to meet customer requirements as shown in Table 4.2.3-1 Program

Pin 12 Worksheet.

The “Windshear INOP Disable” is used when Windshear is disabled and an interface requires the

INOP outputs not be set.

Refer to the Windshear Detection and Annunciation entry in Table 3-1 MK V EGPWS Feature

Selection Worksheet for the selected Windshear options.

Enter the selected Windshear options in Table 4.2.3-1 Program Pin 12 Worksheet.

If Windshear is disabled, determine the required state of “Windshear INOP Disable” and enter it

in Table 4.2.3-1 Program Pin 12 Worksheet.

4.2.3.2 Lamp Format Selection

The Aircraft Type defines the default Lamp Format Type (see Section 3.9 for Lamp Format Type

definitions). Prior to version –208, only the default Lamp Format Type for the Aircraft Type is

supported. Beginning with version –208, Lamp Format Type 2 may be selected if Lamp Format

Type 1 is the default lamp format.

For versions –208 and on, refer to Lamp Format in Table 3-1 MK V EGPWS Feature Selection

Worksheet for the selected Lamp Format.

For version –208 and on, enter the appropriate response in Table 4.2.3-1 Program Pin 12

Worksheet for “Change to Lamp Format 2”. (For older versions, enter “No”.)

Allied Signal, Inc.


4.2.4 Enhanced Feature Control and Simulator Reposition (Program Pin 13)

Program Pin 13 controls the options for Enhanced Feature Control, Obstacle Alerting and

Simulator Reposition for version -204. Added in version –206, the Peaks mode terrain display

option is also controlled by Program Pin 13. These features are discussed in the following

sections. Table 4.2.4-1 Program Pin 13 Worksheet shows the alternatives available for each of

these options and provides a place to record the selections for this installation.

ProgramPin State

SimulatorRepositionAllowed?

TAD & TCF ObstacleAwareness 1 Peaks3

PPCNF13(MP5D)

Strapping1 Default2 Open

2 Opposite of Default2Off MP3A

(PPCOM)

33

Enabled

On On MP15D

4

No

Disabled Off MP3D

5 Default2 MP7B

6 Opposite of Default2Off

TP12C

73

Enabled

On On TP12A

8

Yes

Disabled Off TP4D

94 No TP12B

104 YesEnabled

OffOn

TP11A

ThisInstallation

1 Added in -204.2Default Obstacle Awareness enabling is defined by the Aircraft Type.3Added in –206 (Peaks mode applies only to selected Aircraft Types).4Added in –208.


Determine the Program Pin strapping (per Sections 4.2.4.1 and 4.2.4.2) and record in Figure

4.2-1 Program Pin Strapping Worksheet.

Allied Signal, Inc.


4.2.4.1 Enhanced Feature Control (TAD, TCF, Obstacle Awareness & PeaksMode)

Program Pin 13 provides the capability to disable all enhanced functions: Terrain Awareness

Display (TAD), Terrain Clearance Floor (TCF), Obstacle Awareness (for version –204 and newer)

and (for version –206 and newer) Peaks terrain display mode.

Refer to the TAD & TCF, Obstacle Awareness and Peaks mode entries in Table 3-1 MK V

EGPWS Feature Selection Worksheet for the selected options. Table 4.2.4-1 Program Pin 13

Worksheet shows the options available for enhanced feature control.

Issues to consider when strapping for the enhanced feature enabling:

� Obstacle Awareness is not available prior to version –204.

� If Obstacle Awareness is to be enabled then TAD & TCF must also be enabled.

� Prior to version –206 Obstacle Awareness is enabled/disabled by reversing the default

enabling defined by the Aircraft Type.

� Obstacle Awareness and Peaks mode are not available if TAD & TCF are disabled.

Disabling of TAD may have the effect of disabling Envelope Modulation (refer to the Interface

Control Document for the MK V Enhanced Ground Proximity Warning Computer for more

information.

� Peaks Mode is not available prior to version –206 and is dependent on the display selection.

Refer to the Aircraft Type’s Display Options & Peaks Availability table to determine whether

Peaks is available for the specific Aircraft Type and display.

� For version –206 only: Obstacles must be enabled for Peaks to be enabled.

Record the appropriate enhanced feature enabling in Table 4.2.4-1 Program Pin 13 Worksheet

(refer to Table 3-1 MK V EGPWS Feature Selection Worksheet, the options shown in Table

4.2.4-1 Program Pin 13 Worksheet and the Aircraft Type’s default Obstacle Awareness enabling.)

Allied Signal, Inc.


4.2.4.2 Simulator Reposition

Program Pin 13 provides for instantaneous aircraft repositioning for simulator installations and

must not be used for aircraft installations. This input is not required for stationary laboratory

installations where latitude and longitude are not changing.

Simulation repositioning requires the use of the Simulation Reposition discrete input (refer to the

Aircraft Type’s Discrete Inputs Worksheet). This input is not defined for all Aircraft Types.

Note: Simulator Reposition must be set to “No Reposition” (reference Table 4.2.4-1 Program Pin

13 Worksheet) for non-simulator installations.

Enter the appropriate Simulation Reposition behavior in Table 4.2.4-1 Program Pin 13

Worksheet.

Document the Simulation Reposition strapping in the Aircraft Type’s Discrete Inputs Worksheet

(Appendix A).

Allied Signal, Inc.


4.2.5 Bank Angle Callouts and Alternate LRRA Formats (Program Pin 14)

The Aircraft Type’s Aircraft Class (Business Jet or Commercial Air Transport) determines the

function of this Program Pin. The following paragraphs describe the options controlled by

Program Pin 14.

4.2.5.1 Business Jet (Bizjet) Installations (includes General Aviation-typeaircraft)

Program Pin 14 enables Bank Angle callouts and provides for the selection of an alternate Analog

Radio Altimeter format.

The MK V EGPWC supports three Radio Altimeter formats: ARINC 552, ALT 55 and ARINC 429.

The Aircraft Type defines the default and alternate (if any) RA formats. If the aircraft is not

equipped with the default RA, select an alternate RA format.

BIZJET CONTROLSProgramPin State RA Source/Format Bank Angle Callouts

PPCNF14(TP2C)

Strapping1 Disabled Open

2Default

Enabled MP3A(PPCOM)

3 Disabled MP15D

4Alternate Radio Altitude

#1 Enabled MP3D

5 Disabled MP7B


#2 Enabled TP12C

ThisInstallation

Table 4.2.5-1 Program Pin 14 Worksheet for BIZJET Aircraft

Refer to Bank Angle Callouts in Table 3-1 MK V EGPWS Feature Selection Worksheet for Bank

Angle Callout enabling.

Enter the selected Bank Angle Callout option in Table 4.2.5-1 Program Pin 14 Worksheet for

BIZJET Aircraft.

Refer to the Aircraft Type’s Radio Altimeter Formats worksheet for default and alternate RA

formats. Determine the format of the Radio Altimeter data to be supplied to the MK V EGPWC.

(In order for optional ARINC 429 RA inputs to be provided, they must be defined in the “Optional

System Inputs” table for the Aircraft Type and the controlling signal must be enabled.)

Allied Signal, Inc.


Enter the selected RA format option in Table 4.2.5-1 Program Pin 14 Worksheet for BIZJET

Aircraft.

Document the RA source and format in the Aircraft Type’s Analog Input Channel Assignments

Worksheet (as applicable to the Aircraft Type) and in the Radio Altimeter Formats worksheet.

Determine the Program Pin strapping per the above paragraphs and record in Figure 4.2-1

Program Pin Strapping Worksheet.

4.2.5.2 Commercial Air Transport (AT) Installations

Program Pin 14 provides for the enabling/disabling of Bank Angle callouts and the selection of a

Bank Angle algorithm.

COMMERCIAL AIR TRANSPORT CONTROLSProgramPin State Bank Angle Algorithm Bank Angle Callouts

PPCNF14(TP2C)

Strapping1 Default Disabled Open

2 AlliedSignal MP3A(PPCOM)

3 Bank Angle Option #1 MP15D

4 Bank Angle Option #2

Enabled

MP3D

ThisInstallation

Table 4.2.5-2 Program Pin 14 Worksheet for Non-BIZJET Aircraft

Refer to Bank Angle Callouts in Table 3-1 MK V EGPWS Feature Selection Worksheet for Bank

Angle Callout enabling and algorithm selection.

Enter the selected Bank Angle callout and algorithm options in Table 4.2.5-2 Program Pin 14

Worksheet for Non-BIZJET Aircraft.

Determine the Program Pin strapping per the above paragraphs and record in Figure 4.2-1

Program Pin Strapping Worksheet.

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4.2.6 Altitude Callout Menu Selection (Program Pins 4 – 6)

Program Pins 4, 5 and 6 select the altitude callouts that the MK V EGPWS will issue. The

Altitude Callout Enable discrete must be enabled for the selected callouts to be issued. (Refer to

Section 4.5.2 for information on the Altitude Callout Enable.)

Using the selected Altitude Callout Menu ID in Table 3-1 MK V EGPWS Feature Selection

Worksheet, review the Altitude Callout Menu definition in Appendix B.

Issues to consider when configuring for the selected Altitude Callout Menu:

� If the selected Altitude Callout Menu includes an “Approaching Minimums”-type callout, the

ARINC 429 interface must support a digital Decision Height input to the MK V EGPWC. (The

Aircraft Type’s Aircraft Description table “ARINC 429 DH” entry to indicates whether ARINC

429 DH is supported.) If this interface is not supported, an alternate menu must be selected.

In the event that two ARINC 429 DH inputs are provided to the MK V EGPWC, the higher of

the two Decision Height values will be used for Approaching Minimums and Minimums

calculations and callouts.

� If an Altitude Callout Menu has been selected which includes a “Minimums”-type callout

either the ARINC 429 Selected DH or the Decision Height input discrete is required. Section

4.5.5 describes the Decision Height discrete. Both the ARINC 429 DH and DH discrete

inputs may be provided, if desired.

� The MK V EGPWS will generate an error message if ARINC 429 Selected DH is required and

is not provided. Failure to provide the Less Than DH discrete input can only be detected

during ground check out or flight test.

Appendix B contains the Program Pin strapping for the Altitude Callout Menus.

Note: In order to activate the altitude callout menu, the menu must be selected and the Altitude

Callout Enable discrete (MP8C) must be grounded. Referenced Section 4.5.2 and the Aircraft

Type’s Discrete Inputs Worksheet for more information.

Record the Altitude Callout Menu ID and Program Pin strapping in Figure 4.2-1 Program Pin

Strapping Worksheet.

Note: If no menu is selected and the “Minimums” callout is specified the Altitude CalloutEnable discrete must be DISABLED and the Decision Height discrete must be provided

(reference Sect ions 4.5.2 and 4.5.5, respectively).

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4.2.7 Audio Menu Selection (Program Pin 8)

Program Pin 8 selects the audio menu for non-altitude alerts.

Refer to EGPWS Callout Menu in Appendix C for the Alert Audio Menu selected Table 3-1 MK V

EGPWS Feature Selection Worksheet. Table 4.2.7-1 Program Pin 8 Worksheet defines the

Program Pin strapping for each menu.

Note: DGAC-registered aircraft are required to use Audio Menu #1.

Program PinState Basic GPWS Menu ID PPCNF8 (MP5A)

Strapping

1 Basic Menu Open

2 Alternate #1 MP3A (PPCOM)

3 Alternate #2 MP15D

4 Alternate #3 MP3D

5 Alternate #4 MP7B

6 Alternate #5 TP12C

7 Alternate #6 TP12A

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4.2.8 Alert Volume and Audio Declutter (Program Pin 11)

Program Pin 11 controls the options for Volume Level and Audio Declutter. These options are

discussed in the following sections. The Program Pin 11 Worksheets (Table 4.2.8-1 and Table

4.2.8-2) show the options and Program Pin strapping for the various EGPWS part numbers.

ProgramPin State Volume Level Audio Declutter

PPCNF11(MP4C)

Strapping1 Enabled Open

2Default

Disabled MP3A(PPCOM)

3 Enabled MP15D

4Alternate #1

Disabled MP3D

ThisInstallationNote: “Default” volume is “High” or “Low” as defined by Aircraft Type.

“Alternate #1” is the opposite (“Low” or “High”) of the Default volume.

Table 4.2.8-1 Program Pin 11 Worksheet for Version –204 and Older

ProgramPin State Volume Level Adjust Mode 6

Volume by –3dB? Audio DeclutterPPCNF11(MP4C)


2Default



4 Alternate #2

No

MP3D

5 Default MP7B


7 Alternate #2

Yes

Enabled

TP12A


“Alternate #1” is the opposite (“Low” or “High”) of the Default volume.“Alternate #2” is approximately “High” volume - 3dB and is approximately halfwaybetween the “High” and “Low” volumes.

Table 4.2.8-2 Program Pin 11 Worksheet for Version –206 And On

Determine the Program Pin strapping (per Sections 4.2.8.1 and 4.2.8.3) and record in Figure

4.2-1 Program Pin Strapping Worksheet.

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4.2.8.1 Volume Level Controls

Program Pin 11 can be used to change the alert volume from its default volume (per the Aircraft

Type) to an alternate volume. This controls the output volumes to both cockpit speakers and

headsets. (Refer to Section 3.16 for the actual output wattage.) (The difference between the

high and low volumes is approximately 6dB.)

Issues to consider when configuring the selected audio volume level:

� Prior to version –206, Program Pin 11 is used to select a pre-defined alternate volume level

for audio callouts (instead of the default for the Aircraft Type).

� Beginning with version –206, Program Pin 11 provides a Medium volume for the audio

outputs.

� Beginning with version –206, if an alternate volume is selected, Audio Declutter must be

enabled.

� Beginning with version –206, Program Pin 11 provides the capability to adjust the Mode 6

volume by –3dB independently of the state of the Mode 6 Volume Control discrete.

Reference Section 4.7 for information on wiring the audio output.

Using the table below, determine the appropriate volume level option for the selection in Table 3-

1 MK V EGPWS Feature Selection Worksheet.

If Default Volume is… High Low

Then Alternate #1 is… Low High

And Alternate #2 (applies only to

version –206 and on) is…

Medium Medium

Enter the selected volume level option in either Table 4.2.8-1 Program Pin 11 Worksheet for

Version –204 and Older or Table 4.2.8-2 Program Pin 11 Worksheet for Version –206 And On.

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4.2.8.2 Mode 6 Volume Control (-3dB Adjustment)

For version –206 and on: Program Pin 11 provides the capability to adjust the Mode 6 volume

by –3dB independently of the state of the Mode 6 Volume Control discrete.

Note: Audio Declutter must be enabled if the –3dB adjustment is made.

Refer to Table 3-1 MK V EGPWS Feature Selection Worksheet for the Mode 6 volume

adjustments.

Enter the –3dB Mode 6 volume adjustment in Table 4.2.8-2 Program Pin 11 Worksheet for

Version –206 And On.

4.2.8.3 Audio Declutter Disable

The Audio Declutter feature can be disabled using Program Pin 11.

Refer to Audio Declutter in Table 3-1 MK V EGPWS Feature Selection Worksheet for Audio

Declutter setting.

Note: For version –206 and on, Audio Declutter cannot be disabled if an alternate volume is

selected for Basic GPWS callouts or if the Mode 6 –3dB volume adjustment is used.

Enter the Audio Declutter option in Table 4.2.8-1 Program Pin 11 Worksheet for Version –204 or

Table 4.2.8-2 Program Pin 11 Worksheet for Version –206 And On.

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4.2.9 Alternate Pop-up Selection & Predictive Windshear System (PWS)Interface Options (Program Pin 15)

Program Pin 15 controls the options for Alternate Pop-up and Predictive Windshear (PWS)

interface enabling. These options are discussed in the following sections. Table 4.2.9-1 Program

Pin 15 Worksheet shows the alternatives and Program Pin strapping for each of these options.

ProgramPin State PWS Options Alternate Pop-Up

PPCNF15(MP15C)


2None

Enabled MP3A(PPCOM)

3 Disabled MP15D4

PWS Option 2Enabled MP3D

5 Disabled MP7B6

PWS Option 1Enabled TP12C

ThisInstallation




4.2.9.1 Alternate Pop-up Selection

The Aircraft Type defines whether a display not currently display terrain will switch to displaying

terrain when a terrain warning or caution occurs. This is referred to as a Pop-up. Program Pin 15

provides for the selection of an alternate Pop-up functionality as defined by the Aircraft Type.

Compare the EGPWS Pop-up selected in Table 3-1 MK V EGPWS Feature Selection Worksheet

with the “Auto Pop-up” and “Alternate Pop-up” defined in the Aircraft Type’s Aircraft Description

table. Alternate Pop-ups are not defined for all Aircraft Types.

Enter the Alternate Pop-up state (Enabled or Disabled) in Table 4.2.9-1 Program Pin 15

Worksheet.

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4.2.9.2 PWS Interface Options

The Aircraft Type Optional System Inputs table identifies any optional PWS Interfaces defined for

the Aircraft Type by including PWS Option 1 and/or PWS Option 2 in the table and identifying the

effect of enabling the option.

Refer to Optional System Inputs in Table 3-1 MK V EGPWS Feature Selection Worksheet for the

selected PWS optional system inputs.

Verify the selected PWS Optional Inputs (Table 3-1 MK V EGPWS Feature Selection Worksheet)

are consistent with the aircraft configuration.

Enter the selected PWS Option enabling in Table 4.2.9-1 Program Pin 15 Worksheet.

Note: Any PWS Option not listed in Appendix A is not applicable to the Aircraft Type and must

not be enabled.

Record the interfaces for any PWS Optional Inputs in the Aircraft Type’s ARINC 429 Input

Channel Assignments worksheet. (Refer to Section 4.3.)

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4.2.10 Optional System Inputs, Internal GPS and A lternate Mode 4BReversal (Program Pins 7 and 9)

For most Aircraft Types, Program Pins 7 and 9 enable pre-defined optional interfaces excluding

PWS interfaces enabled via Program Pin 15 (refer to 4.2.9). For a few Aircraft Types, Program

Pin 7 also modifies interface(s) as defined in the Aircraft Type’s ARINC 429 Interface Modification

Options worksheet. Beginning with version –208, Program Pin 9 also reverses the default

Alternate Mode 4B enabling (see the Aircraft Type’s Aircraft Description).

ProgramPin State

Optional Interfaces /Interf ace ModificationsEnabled

PPCNF7(MP14D)

Strapping1 None Open

2 Optional Inputs Select MP3A(PPCOM)

3 Dual GPS Overlay MP15D

4 Dual GPS Overlay & Optional Inputs Select MP3D

5 Single GPS Overlay MP7B

6 Single GPS Overlay & Optional Inputs Select TP12C

7 Single GPIRS Overlay TP12A

8 Dual GPIRS Overlay TP4D

9 Internal GPS TP12B

10 Optional Inputs Select & Internal GPS TP11A

ThisInstallation


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ProgramPin State Optional Interfaces Enabled Alternate

Mode 4B 1

PPCNF9(MP2C)


2 Triple LRRA MP3A(PPCOM)

3 Dual LRRA

Default2

MP15D

41 None Opposite ofDefault2 MP3D

5 Dual ILS MP7B

6 Dual ILS & Triple LRRA TP12C

7 Dual ILS & Dual LRRA

Default2

TP12A

81 Dual LRRA TP4D

91 Dual ILS TP12B


Opposite ofDefault2

TP11A

ThisInstallation

1Added in version –208.2The Aircraft Typed defines the default activation of Alternate Mode 4B.


Determine the Program Pin strapping per Table 4.2.10-1 Program Pin 7 Worksheet and Table

4.2.10-2 Program Pin 9 Worksheet and record in Figure 4.2-1 Program Pin Strapping Worksheet.

4.2.10.1 Optional System Inputs

The Aircraft Type’s Aircraft Description table identifies any optional interfaces enabled by

Program Pins 7 and 9. The Aircraft Type’s ARINC 429 Interface Modification Options worksheet

identifies any interface modifications controlled by Program Pin 7.

The following rules apply to the enabling of optional interfaces:

� The internal GPS receiver is available for MK V EGPWC part numbers 965-0976-020-xxx-

xxx. If enabled, other GPS inputs (ARINC 429) are not allowed.

� If more than one input is enabled by a signal (such as Optional Input Select), all of the inputs

must be provided if the signal is enabled or the MK V EGPWS will report an error.

� Mutually exclusive optional inputs are noted in the Aircraft Type’s Aircraft Description table

and shown in the ARINC 429 Input Channel Assignments Worksheet.

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� Single, Dual and Triple option enables for the same system or systems are mutually

exclusive in that the Dual option enable activates the single input (if optional) and the Triple

option enable activates the dual input (if optional).

� The Dual ILS option is valid for installations in which Single ILS is basic and ILS #2 is

optional.

� The Dual and Triple LRRA options are mutually exclusive and are valid when Single LRRA is

basic and either one or two additional LRRAs are optional.

Verify the selected Optional System Inputs and GPS Receiver (Table 3-1 MK V EGPWS Feature

Selection Worksheet) are consistent with the aircraft configuration.

If any interface modifications are controlled by Program Pin 7 or 9 (refer to the ARINC 429

Interface Modifications worksheet), determine the desired state. (ARINC 429 interface

modifications are discussed in Section 4.2.11.)

Enter the optional input signals to be enabled in Table 4.2.10-1 Program Pin 7 Worksheet and

Table 4.2.10-2 Program Pin 9 Worksheet.

Note: Only the optional inputs shown in the Aircraft Type’s Aircraft Description table can be

enabled; other optional inputs are not applicable to the Aircraft Type and must remain disabled.

Record the interface selections in the Aircraft Type’s ARINC 429 Input Channel Assignments

worksheet (refer to Section 4.3.) and ARINC 429 Interface Modification worksheet (refer to

Section 4.2.11).

4.2.10.1.1 GPS Antenna Input

A single GPS input connector is available on the rear of the 965-0976-020-208-208 or later MK V

EGPWS if Internal GPS is used.

Pin Signal

BP1 GPS COAX Connector

The following technical information is provided:

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Quantity 1

Connector AMP 225791-2 or equivalent

Cable Length/Allowed Signal Loss Not more than 8 dB at 1575 MHz for cable andconnector loss from antenna to unit.

Connector Type Low Level DC on RF Output +5 VDC +-5%, 50 ma maximum, ShieldGround

4.2.10.2 Alternate Mode 4B

The Alternate Mode 4B option applies only to version –208 and on.

If the MK V EGPWC version is –208 or newer, compare the Alternate Mode 4B enabling in Table

3-1 MK V EGPWS Feature Selection Worksheet with that defined by the Aircraft Type’s Aircraft

Description table. If they agree, enter “Default” in Table 4.2.10-2 Program Pin 9 Worksheet;

otherwise, enter “Opposite of Default”.

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4.2.11 ARINC 429 Interface Modifications (Program Pin 16)

Program Pin 16 modifies ARINC 429 interfaces as defined in the Aircraft Type’s ARINC 429

Interface Modification Options worksheet. For some Aircraft Types, Program Pin 7 also modifies

ARINC 429 interfaces. Modifications controlled by Program Pin 7 should have been processed in

Section 4.2.10

Configuration Option 1 is typically used to change the GPS input data format from ARINC 743A to

ARINC 743. Configuration Option 2 is typically used to enable Nav mode label 266 from the FMS

input(s). The Aircraft Type ARINC 429 Interface Modification Options worksheet defines the

specific use of these controls for the Aircraft Type.

The availab ility of Configuration Options 1 and 2 is defined in the Ai rcraft Type’s ARINC

429 Interface Modifications Worksheet in Appendix A.

ProgramPin State Configuration Options Enabled GPS Bus Speed

PPCNF16(MP8B)

Strapping1 Default Open

2None


3 Default MP15D

4Configuration Option 1

Alternate MP3D

5 Default MP7B


Alternate TP12C

7 Default TP12A

8Configuration Options 1 and 2

Alternate TP4D

ThisInstallation


Determine which, if any, of the ARINC 429 Interface Modifications are required by the aircraft

configuration.

Enter the interface options to be enabled in Table 4.2.11-1 Program Pin 16 Worksheet.

Note: Only the interface modifications shown in the Aircraft Type’s ARINC 429 Interface

Modifications worksheet can be enabled; other options are not applicable to the Aircraft Type and

must remain disabled.

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4.2.12 Alternate Display (Program Pin 18)

Display strapping applies only to version –208 and on. Prior to version –208 Program Pin 18 is

undefined and the PPIN State 1 display is the required display. Beginning with –208, alternate

display interfaces have been defined for some Aircraft Types and are selected via Program Pin

18.

ProgramPin State Display

PPCNF18(MP15A)


2 Alternate Display 1 MP3A(PPCOM)

3 Alternate Display 2 MP15D


5 Alternate Display 4 MP7B

6 Alternate Display 5 TP12C

7 Alternate Display 6 TP12A

8 Alternate Display 7 TP4D

9 Alternate Display 8 TP12B


ThisInstallation


Refer to Table 3-1 MK V EGPWS Feature Selection Worksheet for the selected terrain display

PPIN State.

Determine the Program Pin strapping per Table 4.2.12-1 Program Pin 18 Worksheet and record

in Figure 4.2-1 Program Pin Strapping Worksheet.

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4.2.13 GPS Altitude Reference (Program Pin 19)

The GPS Altitude (label 076) must be referenced to mean sea level. Beginning with version –

208, the GPS Altitude may be referenced to either mean sea level or WGS-84 using Program Pin

19.

Note: Beginning with version –208, any GPS must have eight or more channels with Receiver

Autonomous Integrity Monitoring (RAIM) capability.

ProgramPin State GPS Reference Altitude

PPCNF19(MP15B)

Strapping1 Mean Sea Level Open

2 WGS-84 MP3A(PPCOM)

ThisInstallation


Determine the Program Pin strapping per Table 4.2.13-1 Program Pin 19 Worksheet and record


4.2.14 Program Pin Parity (Program Pin 17)

Figure 4.2-1 Program Pin Strapping Worksheet should now show the required strapping for

Program Pins 1 through 16 (versions –204 and on) and Program Pins 18-19 (version –208 and

on) to configure the MK V EGPWC to meet customer requirements. The MK V EGPWS requires

odd parity for the Program Pins. If the number of connections is even (do NOT count “open”),

Program Pin 17 must be strapped to PPCOM. If odd, Program Pin 17 must be left open.

Determine the Program Pin 17 strapping necessary to achieve odd Program Pin parity and record


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4.3 ARINC 429 Digital and Analog Inputs

The ARINC 429 Input Channel Assignments worksheet and Analog Input Channel Assignments

worksheet (if present) show the required and optional inputs for the selected Aircraft Type.

Optional inputs should have been selected in the preceding sections and documented in the

ARINC 429 and Analog Input Channel Assignments worksheets in Appendix A for the Aircraft

Type. If not, return to the appropriate sections and record the interface selections in these

worksheets.

Record the required ARINC 429 interfaces for this installation in the ARINC 429 Input Channel

Assignments worksheet.

Record the required analog interfaces for this installation in the Analog Input Channel

Assignments worksheet.

Note: The MK V EGPWC will accept either a digital or analog input with validity for each of

several inputs as defined in the Aircraft Type’s ARINC 429 and Analog input Channel

Assignments worksheets (typically Radio Altitude and Glideslope). Allow only one source for

these inputs. Providing both the digital and analog signals to the MK V EGPWC will result in the

GWPS using the default signal(s).

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4.4 RS-232 Interface

The MK V EGPWS provides RS-232 ports via the front and rear connectors to support monitoring

of internal parameters via a PC for testing purposes (refer to Section 6 for information on ground

checkout). The monitoring of these parameter values enables the operator to quickly determine if

the correct signal and scaling is being used by the EGPWS computer.

� An RS-232 cable must be fabricated to interface between a PC and the EGPWC front panel

connector or between a PC and a breakout of RS-232 from the EGPWC rear connector. See

Section 5.1.4 for details on interfacing to the EGPWC front panel connector.

� The RS-232 port defaults to 19,200 Baud, 8 bits, no parity and one stop bit. (A 38,400 baud

rate is used for file/database loading only.)

� The RS-232 cable should be no more than 15 meters long.

� The PC connector is a 9-pin “D” male that attaches to the serial port interface.

The table below shows the wiring of the 3-wire RS-232 cable.

RS-232 Receive RS-232 Transmit RS-232 Ground

EGPWS Rear Connector Pin TP6C Pin TP6B Pin MP3A

EGPWS Front Connector Pin 3 Pin 4 Pin 1

Standard DB9 Connector(for a PC)* Pin 3 Pin 2 Pin 5

*NOTE: Some PC Comm Ports have Pins 2 & 3 reversed in a DB-25 alternate termination

configuration.

The EGPWS will activate the first RS-232 port upon which it receives the link initialization

character (control z) after power on.

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4.5 Discrete Inputs

The Program Pin selection portion of this procedure should be completed prior to thesetting of the discretes.

This section contains brief descriptions of the MK V EGPWS discrete inputs. No single Aircraft

Type will use all of these discretes. The Aircraft Type’s Discrete I nputs worksheet identifiesthe specific set of discretes that are defined for that particular Aircraft Type. Use this

worksheet and the information provided below to determine the discrete inputs for a particular

installation. Typical connections may be indicated.

Record connections for each discrete listed in the Aircraft Type’s Discrete Inputs worksheet.

4.5.1 Air Ground Discrete

The Air Ground Discrete is used on Boeing aircraft and indicates whether the aircraft is in the air

or on the ground. Refer to Aircraft Type’s Discrete Inputs table to determine if the Air Ground

Discrete applies to this installation.

The Air Ground Discrete is connected to the Air/Ground relay.

Fault monitoring: Indication of on-ground for more than 60 seconds at airspeeds above 290 knots

will result in an Air Ground Invalid fault which will cause a GPWS INOP indication.

4.5.2 Altitude Callouts Enable Discrete

The Altitude Callouts Enable discrete is used to enable the altitude callouts. This discrete must

be enabled if an Altitude Callout Menu has been selected (refer to Sections 3.13 or 4.2.6).

This discrete must be connected to ground (PPCOM) to enable the altitude callouts. (The

“Minimums” callout will be provided if this discrete is disabled and the Decision Height discrete or

ARINC 429 DH input is provided.)

4.5.3 AOA Validity Discretes #1 and #2

These discretes are used for Windshear processing when the MK V EGPWS is receiving

computer-based non-potentiometer analog AOA inputs. Depending on aircraft wiring the AOA

Validity discretes may be received directly from the AOA Indication System or via the Stall

Warning Computer(s). (The actual AOA inputs may not be received via the same path as the

AOA Validity discretes.)

Either the AOA Indication System or the Stall Warning Computer(s) supply these discretes.

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4.5.4 Audio Inhibit / All Modes Inhibit Discrete

The Audio Inhibit discrete is an optional input but is strongly recommended to maintain audio and

visual prioritization. Refer to Non-Windshear EGPWS Suppress in Table 3-1 MK V EGPWSFeature Selection Worksheet for Audio Inhibit enabling. If Non-Windshear EGPWS

Suppression is disabled, the Audio Inhibit discrete is not required; otherwise it is required.

The Audio Inhibit discrete should be connected to outputs from the Stall Warning System and

Predictive Windshear System for automatic operation.

The function of this discrete is controlled by Program Pin 10. When activated, this discrete always

inhibits all audio except for the windshear warning. If configured via Program Pin 10 to suppress

the visual outputs in addition to the audio outputs, activation of this discrete will suppress all

visual and audio outputs except for the windshear warning.

Activation of the Audio Inhibit input for more than 60 seconds will result in the “All Modes Inhibit”

fault (described in Section 4.5.4) when either of the following conditions is true:

� audio and visual EGPWS suppression is enabled, or

� the Aircraft Type enables audio Inhibit Monitoring (see the “All Modes Inhibit” entry).

The Audio Inhibit discrete input can be connected to any or all of the following (as applicable to

the Aircraft Type):

� the Stall Warning computers (this is required for CAA-registered aircraft)

� the PWS Audio Inhibit output discrete if Hazard bus label 077 is used (To determine which

Hazard bus label is used, refer to the Interface Control Document for the Hazard bus

definitions for the selected Aircraft Type.)

� a separately labeled guarded cockpit switch

� a reactive Windshear system (if separate from the EGPWS).

For some existing GPWS installations, this discrete may have been tied to the analog Radio

Altimeter Receiver/Transmitter Self-Test output. This connection is no longer required but may

be left intact for this installation.

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4.5.5 Decision Height Discrete

The Decision Height discrete indicates to the MK V EGPWC whether the aircraft is above or

below the selected Decision Height. The Decision Height input (via this discrete or ARINC 429

Decision Height) must be provided if the selected Altitude Callout menu includes a “Decision

Height”, “Minimums” or “Decide” callout.

This discrete is typically connected to the Decision Height output on the Radio Altimeter indicator.

Note: The Decision Height discrete does not support altitude callout menus containing an

“Approaching Decision Height”, “Approaching Minimums”, “50 Above” or “Plus Hundred” callout.

4.5.6 Display Select Discretes #1 and #2

These discretes are used to change the state of the Terrain Awareness Display function. When

activated, the displays will either be activated or cancelled.

A momentary cockpit manual switch typically supplies these discretes.

4.5.7 EFIS Range Discretes #1A, B, C, D and #2A, B, C, D

The EFIS Range discretes are used to scale the EGPWS output data to match the displays.

The EFIS Range discretes are supplied by the EFIS Control Panel(s). The number of range

discretes varies among EFIS Control Panels with some supplying the maximum of four range

discretes.

4.5.8 Flap Position Discretes #1, #2, #3, #4

The Flap Position discretes are typically used on Bizjet and General Aviation aircraft. They

provide flap angle data for windshear processing. Up to four Flap Position discretes are supplied

from the flap handle, flap selector switch or flap transmitter.

4.5.9 Flaps Switch Inputs

These inputs apply to the DeHavilland Dash 8-400. They are used with the digital flap angle to

determine landing flap angle.

4.5.10 FMS Glideslope Inhibit Discrete

The FMS Glideslope Inhibit discrete inhibits use of the pseudo Glideslope signal generated by

certain types of FMS. Enabling this discrete will disable Below Glideslope alerting based on the

FMS Glideslope.

This discrete is NOT presently used.

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4.5.11 Glideslope Cancel Discrete

The Glideslope Cancel discrete provides the crew with the capability to manually cancel Mode 5

during an approach. This is automatically reset when the aircraft descends below 30 feet or

ascends above 2000 feet or 1000 feet as defined in the Appendix A Aircraft Type Aircraft

Description.

This discrete is typically supplied by a momentary action cockpit Glideslope mode manual inhibit

switch.

Fault monitoring: Activation of this input for more than 15 seconds will result in the ‘Glideslope

Cancel Invalid’ fault which will cause a GPWS INOP indication. Typically the Glideslope cancel is

only selectable below 2000 feet AGL. However some configurations only allow cancellation below

1000 feet AGL. The Aircraft Type tables in Appendix A indicate the Glideslope Cancel Reset

altitude.

4.5.12 Glideslope Inhibit Discrete

The Glideslope Inhibit Discrete is used to indicate that the aircraft is on a backcourse approach.

During a backcourse approach, the MK V EGPWS will ignore Glideslope inputs. Mode 5 will be

disabled and “Glideslope” will not be annunciated during the Level 1 Self Test or the Level 1

Go/NoGo test.

This discrete is supplied on some aircraft by a backcourse discrete.

4.5.13 Glideslope Validity Discretes #1 and #2

A Validity flag is required for each ARINC 547 Glideslope input to the MK V EGPWS. Refer to

the Aircraft Type’s Analog Inputs table to determine if any analog Glideslope inputs are used for

this installation.

The Glideslope Validity Discretes should indicate validity from each ARINC 547 Glideslope

receiver.

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4.5.14 GPWS Inhibit Discrete

The GPWS Inhibit discrete is used to inhibit all GPWS audio and visual outputs except for

Windshear, Terrain Awareness and TCF. It is frequently not used.

This discrete is supplied by a flight deck mounted switch sometimes referred to as the “ditch

switch”. The GPWS Inhibit discrete is typically used during emergency approaches to “quiet” the

cockpit.

Fault monitoring: Activation of this input for more than 5 seconds will result in the ‘GPWS Inhibit’

fault which will cause a GPWS INOP indication. The functionality of this input is not affected by

the ‘EGPWS Suppress’ Program Pin 10 option (PPCNF10).

4.5.15 ILS Bus Select Discretes #1, #2 and #3

There are often multiple sources for the Glideslope Deviation, Localizer Deviation and Runway

Heading input signals. There is always a preferred source for these signals but the preferred

source varies depending on the source selection method used for a particular Aircraft Type.

These discretes are used on only a few Aircraft Types with multiple ILS inputs. The discretes

indicate which ILS bus the tuned data is on. The three ILS select discretes are typically supplied

from the ILS tuning panel.

4.5.16 ILS/MLS Select

The ILS/MLS Select discrete is used to set the preferred source for Glideslope and Localizer

inputs to either ILS or MLS.

4.5.17 ILS Tuned Discrete #1

The ILS Tuned Discrete #1 indicates that an Instrument Landing System frequency has been

selected on ILS #1. This discrete is typically used with analog Glideslope and Localizer inputs.

When ILS #1 is tuned, the MK V EGPWS checks the Glideslope and Localizer Valid discretes

and monitors the Glideslope and Localizer inputs. The ILS #1 provides this discrete input as

defined in the Aircraft Type’s Analog Input Channel Assignments worksheet.

4.5.18 ILS Tuned Discrete #2

The ILS Tuned Discrete #2 indicates that an Instrument Landing System frequency has been

selected on ILS #2. This discrete is typically used with analog Glideslope and Localizer inputs.

When ILS #2 is tuned, the MK V EGPWS checks the Glideslope and Localizer Valid discretes

and monitors the Glideslope and Localizer inputs. This discrete is provided by the ILS #2 input as

defined in the Aircraft Type’s Analog Input Channel Assignments worksheet.

Allied Signal, Inc.


4.5.19 Landing Flap/Flap Override Discrete

The Landing Flap discrete indicates a landing flap position.

The Landing Flap discrete is typically connected to the flap handle or flap selector switch. It can

be paralleled with or used exclusively by a Flap Override Switch if an alternate source of Flap

Position is used.

4.5.20 Landing Flap Override Discrete

The Landing Flap override discrete indicates the flaps are in landing position. This discrete is

used on Aircraft Types where landing flap position is determined via the ARINC 429 discrete

input.

This discrete can be used to activate Alternate Mode 4B if Alternate Mode 4B is selected by

Program Pin strapping or by the Aircraft Type (refer to Section 3.7.)

4.5.21 Landing Gear/Gear Override Discrete

The Landing Gear discrete indicates the landing gear position.

The Landing Gear discrete is typically connected to the landing gear relay or landing gear

selector handle position-sensitive switch. It can be paralleled with or used exclusively by a Gear

Override Switch if an alternate source of Gear Position is used.

4.5.22 Localizer Validity Discretes #1 and #2

A Validity flag is required for each analog Localizer input. The Localizer Validity discretes

indicate Validity status from each ARINC 547 Localizer Receiver.

Allied Signal, Inc.


4.5.23 Mode 6 Volume Control Discrete

Refer to Table 3-1 MK V EGPWS Feature Selection Worksheet to determine the preferredMode 6 Volume level.

The Mode 6 Volume Control discrete is used to modify the volume of the Mode 6 altitude and

bank angle callouts. The Aircraft Type’s Aircraft Description table includes an entry defining the

Mode 6 Volume as either “Normal” or “Low”.

If the default Mode 6 volume is “Normal”, the Mode 6 callouts will be issued at the same volume

level as the GPWS callouts. If the default volume is “Low”, the Mode 6 callouts will be 6dB lower

than the GPWS callouts.

The Mode 6 Volume Control discrete is used to decrease the default Mode 6 volume by an

additional 6dB. The resulting Mode 6 volume will either be 6 or 12dB lower than the alert callouts

(for default volumes of “Normal” and “Low” respectively).

This discrete is typically connected to ground/PPCOM (MP3A) to lower the volume an additional

6dB. In some installations, it is connected to the windshield wiper control to decrease the Mode 6

Volume level under normal conditions and increase it 6dB when the cabin noise increases due to

the windshield wipers being on.

For version –206 and on: Program Pin 11 can be used independently of this discrete to adjust

the Mode 6 volume by –3dB.

4.5.24 Momentary Audio Suppress Discrete

This discrete suppresses audio outputs while the momentary action switch is depressed to

ensure that alerts are not repeated continuously during an event.

This discrete is typically not used since the Audio Declutter option (Sections 3.15 and 4.2.8.3)

performs the same function.

A cockpit switch typically supplies the input for Momentary Audio Suppress.

Fault monitoring: Activation of this input for more than 30 seconds will result in the ‘Audio Cancel

Invalid’ fault which will cause a GPWS INOP indication.

4.5.25 PWS Interlock Discretes #1 and #2

The PWS Interlock discretes are used to determine the priority between the PWS and GPWS

alerts. They indicate which PWS Hazard Bus the EGPWS should monitor for PWS data. Most

Aircraft Types do not support the use of these discretes.

The PWS Control Panel supplies the PWS Interlock discretes.

Allied Signal, Inc.


4.5.26 Radio Altitude Validity Flags #1 and #2 (ARINC 552/ALT 55)

A Validity flag is required for each Analog Radio Altimeter providing data to the MK V EGPWS.

Refer to the Appendix A Aircraft Type information to determine if any analog RA inputs are used

for this installation.

4.5.27 Self-Test Discrete

The Self-Test discrete is used to initiate MK V EGPWS Self Test.

The Self-Test discrete is typically connected to a momentary action cockpit self test switch. The

Self-Test switch may be part of the Pull Up or GPWS lamp assembly or a separately labeled

switch.

Note: The Self-Test discrete is ignored when indicated Radio Altitude is greater than 5 feet.

4.5.28 Simulator Reposition

For all MK V EGPWS installations in an aircraft, this discrete must be left open.

4.5.29 Stall Warning Computer Fail Discretes #1 and #2

These discretes are used for Windshear processing when the Angle of Attack inputs are received

via the Stall Warning Computers.

The Stall Warning Computers supply these discretes.

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4.5.30 Steep Approach Discretes #1 and #2

This feature desensitizes the Mode 1 (Excessive Descent Rate) alert boundaries to permit safe

but steeper than normal instrument precision approaches (e.g. MLS or GPS approaches) without

unwanted alerts. Refer to Steep Approach in Table 3-1 MK V EGPWS Feature SelectionWorksheet for Steep Approach enabling.

The Aircraft Type’s Steep Approach entry indicates whether Steep Approach is an option for the

Aircraft Type. Steep Approach is typically enabled and selected using discrete inputs as

indicated in the Aircraft Type’s Discrete Inputs worksheet. Several Aircraft Types support the use

of digital Steep Approach using ARINC 429 label 171, bit 24. Digital Steep Approach requires a

Primus 1000 or 2000 supporting this interface.

To use the discrete Steep Approach, discrete #1 must be enabled (it can be hardwired); discrete

#2 is selected in flight when starting a steep approach typically via an alternate action switch or

latching discrete. Steep Approach discrete #2 should not be hardwired. On ground self-test isinhibited if Steep Approach is active.

Digital Steep Approach will function if the Aircraft Type supports it and the appropriate input

(ARINC 429 label 171, bit 24) is provided to the MK V EGPWS.

4.5.31 Terrain Awareness and TCF Inhibit

The Terrain Awareness and TCF Inhibit discrete indicates to the MK V EGPWS whether these

functions are enabled or inhibited. This di screte is required for all installations.

This discrete is typically connected to an alternate action switch in the cockpit. The

recommended label for this switch is “Terrain Override” although labeling for this switch should be

consistent with existing cockpit nomenclature.

“Terrain Inhibited” will be annunciated during cockpit Self-Test if these functions are inhibited.

Fault monitoring: For some installations, activation of this input for more than 5 seconds will

activate the Terrain Monitor (refer to the Interface Control Document (ICD) Appendix F Terrain

Display Configuration Data table for each aircraft type). The functionality of this input is not

affected by the ‘EGPWS Suppress’ Program Pin 10 option (PPCNF10).

Note: Terrain INOP is NOT illuminated by this switch except for Airbus aircraft.

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4.5.32 Terrain Displayed on EFIS Discretes (Left and Right)

These discretes indicate to the MK V EGPWS if terrain is displayed on the Left and/or Right side

EFIS. The Left Terrain Displayed discrete will be grounded when Terrain is displayed on the

Pilot’s side and the Right Terrain Displayed discrete will be grounded when Terrain is displayed

on the Co-pilot’s side.

These inputs are supplied by Terrain Select relays.

4.5.33 Terrain Relay Monitor Discretes #1 and #2

The Terrain Relay Monitor discretes allow the MK V EGPWS to determine if the terrain select

relays are functioning properly. When EGPWS terrain displays are active (relays energized),

these discretes are monitored for feedback from the relays via the Terrain INOP annunciator. If

there is no feedback an error is indicated to the crew.

These discretes are supplied by the Terrain Select Relays.

4.5.34 Weather Display Select Discretes #1 and #2

The Weather Display Select discretes are used on Aircraft Types 217-224. These discretes are

necessary because the EFIS requires data on the Weather bus at all times if the weather radar is

on. These discretes ensure a constant data stream from the EGPWS.

4.5.35 Weather Radar On/Off #1 and #2

This discrete is typically supplied by the Weather Radar and indicates whether the Weather

Radar is turned on or off.

Allied Signal, Inc.


4.6 Serial Output

The EGPWC provides for ARINC 453 and ARINC 429 serial outputs. The Aircraft Type’s Serial

Outputs worksheet is provided to document these interfaces.

Terrain display data is output on two ARINC 453 channels when the Terrain Awareness display

function is enabled.

Specific low speed ARINC 429 output labels provided by the EGPWC are listed in ICD Appendix

E. The ARINC 429 output data includes:

1. Internal data (data output for test purposes only such as Radio Altitude used, Computed True

Airspeed and Corrected AOA information).

2. Alert/Warning status (Voice and Lamp activity can be provided to EFIS, EICAS, and flight

recorders).

3. Program Pin option selections and input discrete status.

4. Fault diagnostic words.

5. Maintenance system interactive protocol data (for some installations).

Note: During EGPWS Self Test, the Sign/Status Matrix (SSM) of each output label is set to the

Functional Test status code.

Allied Signal, Inc.


4.7 Audio Output

Alert output messages are provided as specified in the selected Audio Callout Menu when inputs

are valid and the audio suppression discretes are disabled. Refer to Table 3-1 MK V EGPWS

Feature Selection Worksheet for the selected Audio Callout Menu. The output volume level is

initially defined in the Aircraft Type and may be modified using either Program Pin 11 or the Mode

6 Volume Control discrete.

Audio output messages are provided as specified in the Altitude Callout menu when inputs are

valid, the Altitude Callout Enable discrete input is enabled and the audio suppression discretes

are disabled. When audio suppress ion is enabled, the output dis crete(s) associated with asuppressed message are activated unless both audio and visual suppress ion is enabled.

The audio outputs consist of both an 8-ohm amplifier output and a transformer isolated 600-ohm

output. The 600-ohm output is intended for headphones and interphone system and is also

provided to an EGPWC front panel jack. The 8-ohm output is capable of driving a speaker or can

be used to drive other devices with equal or higher impedance.

The electrical connections and specifications are shown below:

Electrical RangePins Signals

“High Volume” is strapped “Low Volume” is strapped

MP13C Hi

MP13D Low600-ohminterphoneoutput Front panel

connector N/A

� output power is 25 mW� 14.4+-2 volts peak-to-

peak� 50 mW RMS @ 800 Hz

� output power is 4 mW� 8.2+-1 volts peak-to-peak� 16 mW RMS @ 800 Hz

MP3B Hi8-ohmspeakeroutput MP3C Low

� output power is 2 W� 13.8+-2 volts peak-to-

peak� 4.4 W RMS @ 800 Hz

� output power is 0.5 W� 7.2+-1 volts peak-to-peak� 1.1 W RMS @ 800 Hz

Allied Signal, Inc.


4.8 Discrete Outputs

The MK V EGPWS provides for up to ten 0.5 amp (1 amp maximum) general purpose and three

monitor discrete outputs. The general purpose discretes indicate the states of EGPWS Warnings

and Cautions and control the terrain displays. The Aircraft Type’s Discrete Outputs worksheet

lists the discrete outputs and pins used for the Aircraft Type. This worksheet is used to document

the discrete output connections for the installation.

The discrete monitor outputs indicate the overall health and status of the EGPWS. These three

discretes are programmed, via aircraft configuration, to reflect any one or any combination of the

following functions: GPWS INOP, Windshear INOP, Callout INOP and Terrain INOP or Terrain

Not Available. All three of these discretes activate with loss of EGPWC power. The status of

these three discretes is also contained on an ARINC 429 output word.

The discrete outputs are optional if the ARINC 429 output data is used for driving the

alert/warning lamps via a symbol generator. Most Aircraft Types do not use the ARINC 429

output data for lamp control. (This data is typically sent to the Flight Data Recorder.)

All outputs to lamps are driven by solid state switches to ground. These outputs can also be used

as discrete drivers for other devices (e.g. the EFIS symbol generator).

4.8.1 Audio On Discrete

The Audio On discrete output goes true whenever any EGPWS alert or warning is being

annunciated. It will stay true until the voice is completed. This output can be used to inhibit other

audio systems (e.g., TCAS) during EGPWS warnings. In addition it can be used to drive the

audio key line input provided on some aircraft audio systems.

4.8.2 Callout INOP Monitor Discrete

The Callout INOP monitor discrete output is used only on Boeing integrated aircraft. It is

activated when a condition exists which would cause a failure to issue any of the altitude callouts.

This discrete output is provided to the EFIS symbol generator to produce an EICAS message. It

does not affect the lamps.

On aircraft with the Callout INOP Monitor discrete the Terrain INOP and Terrain Not Available

monitor discretes are transmitted via ARINC 429 output label 274. (See ICD Appendix E.)

Allied Signal, Inc.


4.8.3 Displayable Discretes #1 and #2

If required by the Aircraft Type, the MK V EGPWC produces two Displayable discrete outputs.

These discretes are used to light the mode annunciation lamps (Terrain mode or WXR mode)

when the MK V EGPWC is controlling the display of weather and terrain data.

Displayable discrete #1 is activated when the EFIS is in a mode that supports terrain display on

the Captain’s display. Terrain Displayable discrete #2 is activated when the EFIS is in a mode

that supports terrain display on the First Officer’s display.

Each output is routed through the picture bus switching relay to drive either the TERR mode

annunciation if terrain is displayed or the WXR mode annunciation if the WXR R/T is on (weather

data need not be displayed).

4.8.4 Glideslope Cancel Discrete

The Glideslope Cancel discrete output is optional unless the Alternate Glideslope Cancel has

been selected. It is activated when the Glideslope Cancel discrete input (Section 4.5.11) is

activated (either manually or automatically). It is deactivated when the Glideslope Cancel

discrete input is deactivated.

This discrete is typically output to the Glideslope Cancel lamp.

4.8.5 GPWC Alert Discrete

The GPWC Alert is activated when a non-windshear Basic GPWS alert condition exists. Other

conditions, such as the Terrain Awareness and Obstacle Alerting Cautions, may activate this

discrete. The Aircraft Type’s Discrete Outputs worksheet identifies the conditions that activate

the GPWC Alert discrete.

This discrete is typically output to the Below Glideslope lamp (Lamp Format Type 1) or the amber

Ground Proximity lamp (Lamp Format Type 2).

4.8.6 GPWC Warning Discrete

The GPWC Alert is activated when a non-windshear Basic GPWS warning condition exists. Other

conditions, such as the Terrain Awareness and Obstacle Awareness Warnings, may activate this

discrete. The Aircraft Type’s Discrete Outputs worksheet identifies the conditions that activate

the GPWC Warning discrete.

This discrete is typically output to the red GPWS Lamp (Lamp Format Type 1) or Pull Up lamp

(Lamp Format Type 2).

Allied Signal, Inc.


4.8.7 GPWS Monitor Discrete

The GPWS monitor discrete output indicates the health of the Basic Ground Proximity functions

of the MK V EGPWS. The default state of this discrete indicates the Windshear function is failed.

This discrete is typically output to the GPWS INOP/Fail lamp or the EICAS/ECAM discrete input.

4.8.8 PWS Inhibit Discrete

This discrete is activated whenever the EGPWS audio output out-prioritizes the PWS audio

output.

This discrete is typically output to the PWS.

4.8.9 TCAS Inhibit Discrete

This output is activated to inhibit TCAS resolution advisories whenever an EGPWS Warning or

Alert condition exists. (This does not include Altitude Awareness callouts.) For some

installations, the GPWS Alert and Warning, the Terrain Awareness/Obstacle Awareness Alert and

Warning and the Windshear Warning discrete outputs are used to inhibit TCAS.

4.8.10 Terrain Awareness Caution and Obstacle Awareness CautionDiscrete

Terrain and Obstacle Awareness Caution discretes are provided as one discrete output. This

discrete is active when a Terrain Awareness or Obstacle Awareness Caution event occurs.

This output will typically activate the GPWS Warn Lamp, the GPWS Alert Lamp or its own lamp.

This output can also be used as a discrete input to an EFIS.

4.8.11 Terrain Awareness Warning and Obstacle Awareness WarningDiscrete

Terrain and Obstacle Awareness Warning discretes are provided as one discrete output. This

discrete is active when a Terrain Awareness or Obstacle Awareness Warning event occurs.

This output will typically activate either the GPWS Warn Lamp or its own lamp. This output can

also be used as a discrete input to an EFIS.

4.8.12 Terrain Display Switching Discretes #1 and #2

The EGPWC produces two discrete outputs for controlling the terrain display. They can either be

used to control picture bus switching relay(s) or be connected directly to the symbol generators.

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4.8.13 Terrain Displayable Discretes #1 and #2

If required by the Aircraft Type, the MK V EGPWC produces two Terrain Displayable discrete

outputs. These discretes are used to light the terrain mode annunciation lamps when terrain data

is being displayed.

When the EFIS is in a mode that supports terrain display, the terrain display function is valid and

terrain display has been selected (manually or via auto pop-up) on the Captain’s display, the

Terrain Displayable discrete #1 is activated to light the Captain’s terrain mode annunciation lamp.

When the EFIS is in a mode that supports terrain display, the terrain display function is valid and

terrain display has been selected (manually or via auto pop-up) on the First Officer’s display, the

Terrain Displayable discrete #2 is activated to light the First Officer’s terrain mode annunciation

lamp.

If more than two displays are used, they should be multiplexed together to define two sets

(Captain’s and First Officer’s) of displays.

4.8.14 Terrain INOP Monitor Discrete

The Terrain INOP discrete output indicates the health of the Terrain Awareness and Alerting

function of the MK V EGPWS. The default state of this discrete indicates the Terrain Awareness

and Alerting function is failed.

This discrete is typically output to the Terrain INOP/Fail lamp or the EICAS/ECAM discrete input.

4.8.15 Terrain Not Available Monitor Discrete

The Terrain Not Available monitor discrete output is activated when a position error occurs that

prevents the Terrain Awareness and Alerting function from executing. This discrete is also setwhenever the Terrain INOP discrete output is set.

This discrete is typically output to the EICAS/ECAM discrete input or the Terrain Not Available

lamp.

4.8.16 Windshear Caution Discrete

The Windshear Caution discrete output is an optional discrete not typically used on Boeing

aircraft. It is activated when a Windshear Caution event occurs and is deactivated when the

event is no longer true. Priority logic prevents a Windshear Caution lamp output during a

Windshear Warning condition.

This output is typically used to drive a cockpit lamp.

Allied Signal, Inc.


4.8.17 Windshear Monitor Discrete

The Windshear monitor discrete output indicates the health of the Windshear Detection and

Alerting function of the MK V EGPWS. The default state of this discrete indicates the windshear

function is failed.

This discrete is typically output to the Windshear INOP/Fail lamp or the EICAS discrete input.

4.8.18 Windshear Warning Discrete

The Windshear Warning discrete output is required if Windshear is enabled. It is activated when

a Windshear Warning event occurs and is deactivated when the event is no longer true. Priority

logic prevents a Windshear Caution lamp output during a Windshear Warning condition and turns

off the EGPWS alert and warning aural outputs.

This discrete is required if Windshear is enabled.

4.8.19 WXR Control Discrete

This discrete was added in version –206. The WXR Control discrete output is provided, for some

installations, to control the On/Off signal to the WXR R/T (the R/T can be turned off when the PPI

is turned on to display terrain).

Allied Signal, Inc.


5 Mechanical Installation Design Details

This section provides information for completing the installation design including a typical parts

list with vendors, part numbers, and component specifications.

Environmental data is provided in the Product.

5.1 System Components

A typical MK V Enhanced Ground Proximity Warning System consists of the components listed

below. Supporting installation hardware my also be required.

Description Qty Specification Section

Ground Proximity Warning Computer 1 5.1.1

Computer Mounting Tray 1 5.1.2

Rear Connector (with pins) 1 5.1.2

Front Panel Test Connector Mate Optional 5.1.4

Cockpit Lights (light plates) 5.1.5

Switching RelaysInstallationDependant 5.1.5.1

GPS Antenna Optional 5.1.7

GPS Cable Contacts Optional 5.1.8

GPS Cabling Optional 5.1.9

Terrain Override Switch 1 Table 5.1.5-1

Terrain Display Select Switch 1 or 2 Table 5.1.5-1

Allied Signal, Inc.


5.1.1 MK V Enhanced Ground Proximity Warning Computer

The MK V EGPWC is available in either a 115 VAC input power model or a 28 VDC input power

model. The part numbers, front view and outline drawing are shown below. Beginning with –208,

the MK V EGPWS is available with an internal GPS (part number 965-0976-020-xxx-xxx). The

MK V EGPWS will use its internal GPS position rather than external GPS data.

Description & Part NumbersItem Qty

28 Volt Computer 115 Volt Computer 115 Volt Computer withInternal GPS

965-0976-040-204-204 965-0976-003-204-204 N/A

965-0976-040-206-206 965-0976-003-206-206 N/AMK V EGPWCComputer 1

965-0976-040-208-208 965-0976-003-208-208 965-0976-020-208-208

NOTE: The 115-volt version of the MK V EGPWC has the same connector as the MK V GPWC (Classic MK V).Replacing a Classic MK V with a MK V EGPWC without updating the Program Pin strapping will result in error messages(and no functionality) but will not cause physical damage to the MK V EGPWC.

Figure 5.1.1-1 MK V EGPWC - Front View

IDENTIFICATIONLABEL

MODIFICATIONSTATUS

HANDLE

HOOK

SELF-TEST SWITCH

HEADPHONE JACK

DOOR

STATUSINDICATORS

PCMCIAINTERFACE

UPLOAD/DOWNLOADSTATUS INDICATORS

FRONT PANELTESTCONNECTOR (RS232)

Allied Signal, Inc.


EGPWC Electrical & Physical Specifications

Part No.Packaging:Weight:Mounting:Cooling:

965-0976-003-xxx-xxx/965-0976-040-xxx-xxx/965-0976-020-xxx-xxx2 MCU ARINC 600-67.0 LB MAXPer ARINC 600-6Per ARINC 600-6 & ARINC 404A convection cooling

PowerConsumption:

� 15 Watts, Non- Warning� 22 Watts, With Warning (over 8 �� speaker)� 48 Watts (typical) , With heater blanket On,

(applicable only to 965-0976-040-xxx-xxx)

Figure 5.1.1-2 MK V Enhanced Ground Proximity Warning Computer Outline

Allied Signal, Inc.


5.1.2 Mounting Tray (ARINC 600, 2 MCU)

Vendor Qty Short Mounting Tray

AlliedSignal 600-4697-001

Barry Controls1 T600-2-S-R-A-XXXX

(xxxx indicates the surface finish)

Figure 5.1.2-1 Mounting Tray Outline Drawing

Allied Signal, Inc.


5.1.3 MK V EGPWC Rear Connector

5.1.3.1 115V MK V EGPWC Rear Connector

Vendor & Part No.Item Qty

AlliedSignal AMP Cannon Souriau

EGPWC Rear Connector(ARINC 600 Size 1):

1 440-0497-002 NIC66F11A08AA1 BK AD1-125-30008-F0

S611-MG-05W2-P0008-L

Lower Plug Power Pins 2 404-4127-002 208270-2 031-1303-000 8660-249

- Insertion/Extraction Tool - 91066-3 - -

- Crimp Tool M22520/1-01 with Positioner M22520/1-02 (AMP Coaxicon)

Lower Plug Ground Pin 1 404-4127-003 208273-2 031-1308-000 8660-250



Top and Middle Plug I/O Pins 120 404-4127-004 208262-3 030-2259-000 8660-202

- Insertion/Extraction Tool 91066-1 - -


GPS Coax Connector – RFSocket Size 5

1 440-1238-001 225791-2 for RG142 Type

- Crimp Tool 1 M22520/2-01 setting #5 with Positioner Tool 1-601966 AMP

Figure 5.1.3.1-1 Rear Connect Keying for 115V MK V EGPWC (Internal or External GPS)

F A CE VI E W OF E N GA GIN G E N D S

CE N T E RP OS T

D A R K E N E D P OR T I ON I N D I CA T E S E X T E N D E D P A R T OF P OS T I N P L U G

K E Y H OL E S H OW N I N R E CE P T A CL E

P OL A R I Z A T I ON L E GE N D

1

2

3

4

5

6

R I GH TP OS T

L E F TP OS T

CE N T E R K E Y

R I GH T K E YL E F T K E Y

P OL A R I Z A T I ON P OS I T I ON S - P L U G (R A CK )

P OS I T I ON

0 8

L E F T P OS T

2

CE N T E RP OS T

R I GH TP OS T

1 6

P OL A R I Z A T I ON P OS I T I ON S - R E CE P T A CL E (B OX )

P OS I T I ON

0 8

L E F T K E Y

5

CE N T E RK E Y

R I GH TK E Y

4 3

EG PW S RearConnector

Lower Plug

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5.1.3.2 28V MK V EGPWC Rear Connector

Vendor & Part No.Item Qty

AlliedSignal AMP Cannon Souriau

EGPWC Rear Connector(ARINC 600 Size 1):

1 440-0497-005 NIC66F11A10AA1 BK AD1-125-30010-F0

S611-MG-05W2-P0010-L

Lower Plug Power Pins 2 404-4127-002 208270-2 031-1303-000 8660-249



Lower Plug Ground Pin 1 404-4127-003 208273-2 031-1308-000 8660-250



Top and Middle Plug I/O Pins 120 404-4127-004 208262-3 030-2259-000 8660-202

- Insertion/Extraction Tool 91066-1 - -


GPS Coax Connector – RFSocket Size 5

1 440-1238-001 225791-2 for RG142 Type

- Crimp Tool 1 M22520/2-01 setting #5 with Positioner Tool 1-601966 AMP

Figure 5.1.3.2-1 Rear Connect Keying for 28V MK V EGPWC

F A CE VI E W OF E N GA GI N G E N D S

CE N T E RP OS T

D AR K E N E D P OR T ION IN D ICA T E S E X T E N DE D P A R T OF P OS T IN P L U G

K E Y H OL E S H OW N I N R E CE P T ACL E

P OL A R IZ A T ION L E GE N D

1

2

3

4

5

6

R I GH TP OS T

L E F TP OS T

CE N T E R K E Y

R I GH T K E YL E F T K E Y

P OL A R IZ A T ION P OS IT ION S - P L U G (R ACK )

P OS IT ION

1 0

L E F T P OS T

4

CE N T E RP OS T

R I GH TP OS T

1 6

P OL A R IZ A T ION P OS IT ION S - R E CE P T ACL E (B OX )

P OS IT ION

1 0

L E F T K E Y

5

CE N T E RK E Y

R I GH TK E Y

4 1

EGPW S RearConnector

Lower Plug

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5.1.4 Front Panel Test Connector Mate

A test connector is provided on the EGPWC front panel. This provides access for a PC test

monitor via RS-232. Reference ICD Appendix C for pinout and functional details. The mating

connector for the EGPWC test plug is a male (pins) 15 pin double density D-subminiature type,

Positronics Industries (kit) part number ODD15M1OYOZ or the following individual parts:

Vendor & Part No.Description (AMP)

Amp

Connector Shell (HDP-22 Crimp Snap In Contact) 748364-1

Size 22 DM Crimp Snap In Contacts Pin ø.030 204370-2

Backshell (Shielded Cable Clamp Assembly) 745854-5

Jackscrews (4-40 Male Jackscrew Kit)747784-8

(specify quantity of 2 perconnector)

Grommet Sets 747746-1

The following tools will work with Positronics, Amp, and Mil Spec Connectors:

Insertion / Extraction Tool 91067-1 M81969/1-04

Hand Crimp Tool M22520/2-01

Positioner M22520/2-09

5.1.5 Cockpit Annunciators

Two Lamp formats are defined as a function of aircraft type and are not modifiable (prior to –208).

Appendix A provides a definition of the lamp formats and identifies the lamp format for each

Aircraft Type.

All alert/warning lamp outputs are normally a steady state switch to ground. The lamps can be

individually programmed to flash as a function of Aircraft Type only (refer to Appendix A). The

flashing outputs operate at a nominal 70 cycles per minute at a 50% duty cycle. For Windshearor Basic GPWS lights, contact A lliedSignal, Inc.

The following table shows the indicators and controls associated with the Enhanced GPWS:

Allied Signal, Inc.


Indicator/Control Color Recommended Location Function

Required Indicators and Controls

Lamp Format

1 2Lamp Format is defined by the Aircraft Type

GPWS PULL UP RED In front of each pilot GPWS or PULL UP warning alerts

BELOW G/S GPWS AMBER In front of each pilot GPWS or BELOW G/S caution alerts

GPWS FAIL orGPWS INOP AMBER -

Indicates basic GPWS functions areinoperative

TERR INOP AMBER - Indicates that TAD and TCFfunctions are inoperative

TERR OFF or TERR OVRD /TERR INHIBIT switch

WHITEOr Blue Within reach of both pilots

Indicates that TAD and TCFfunctions have been manually turnedoff /Illuminated with features inhibited

GPWS P/TEST (Note-1) N/A In front of each pilot EGPWS Press to Self-Test

G/S P/CANCEL (Note-2) N/A In front of each pilot Press to cancel G/S function

Optional Indicators and Controls

WINDSEAR WARNING RED In front of each pilot WINDSHEAR warning

WINDSHEAR CAUTION AMBER In front of each pilot WINDSHEAR caution

WINDSHEAR FAIL orWINDSHEAR INOP

AMBER - Indicates that Windshear detection isinoperative

G/S CANCELEDWHITE,

visible BLUEor AMBER

In front of each pilotTypically only used withAlternate G/S Cancel

On when G/S alerts are manuallycanceled

GPWS FLAP OVERRIDEWhite

LabelingWHITE

On center panel, near flaphandle

Inhibits GPWS Mode 4B “Too LowFlaps” alert (pilot may manuallyreset)

GPWS VOICE OVERRIDE WHITE On center panelTypically not used

Silences GPWS & TERR voiceannouncements

RAD ALT VOICE OVERRIDE WHITE On center panelTypically not used

Silences radio altitude voice calloutson approach

WX RADAR RANGE SelectorKnob

- - - On WX radar controllerPart of the WXR installation

Controls range of display

TERR Display select switch

WHITE,visible BLUEor GREEN ifnot on DCP

Near each Terrain Display oron each Display Control

Panel

Momentary contact switch used toselect terrain display. Use one foreach terrain display or a maximum oftwo terrain display select switches.

Note-1 Typically, GPWS Press to Test is located on the red Pull UP or GPWS annunciator. Note-

2 Typically, G/S Press to Cancel is a located on the amber GPWS or Below G/S annunciator.

Table 5.1.5-1 Cockpit Annunciators

Allied Signal, Inc.


5.1.5.1 Enhanced GPWS Lights and Lightplates

The following are example lightplates that have been used in the past. IDD Aerospace

Corporation is a manufacturer and vendor of lightplates commonly used in MK V EGPWS

installations. The most commonly used lightplate configurations are shown below although IDD

can manufacture to meet other customer requirements.

Description IDD Part Number

EGPWS Lightplate – Aircraft Types 217-220 -

- Captain’s Side (see Figure 5.1.5.1-2) 800-008082-1

- F.O.’s Side (see Figure 5.1.5.1-1, gray) 800-008081-1

EGPWS Lightplate – Aircraft Types 221-224 -

- Captain’s Side (see Figure 5.1.5.1-3) 800-008083-1

- F.O.’s Side (see Figure 5.1.5.1-1, brown) 800-008080-1

Korry Electronics is manufacturing LRUs with the same dimensions and nomenclature and

lightplates as shown in Figure 5.1.5.1-1, Figure 5.1.5.1-2 and Figure 5.1.5.1-3. The LRUs contain

lightplates matching these figures with LED switches installed in a contained connectorized

assembly. Contact Korry for additional information.

The following are example lights that have been used in the past. Other lights may be used.

2.25

3.25

0.94 SQUARESWITCH CUTOUTS

SWITCH CUTOUTS TOBE RING-LIGHTED PERBOEING SPEC. S233T100

Figure 5.1.5.1-1 F.O.'s EGPWS Panel IDD 800-008083-1

Figure 5.1.5.1-1 F.O.'s EGPWS Panel IDD 800-008083-1 applies to Aircraft Types 217-224:

B737-300/500, B757-200/200ER, and B767-200/300/300ER (when gray) and Aircraft Types 221-

224: Boeing 757-200/200ER and Boeing 767-200/300/300ER (when brown).

Allied Signal, Inc.


2.25

5.50


1.15 SQUARESWITCH CUTOUT

SWITCH CUTOUTS TOBE RING-LIGHTED PERBOEING SPEC S233T100

Figure 5.1.5.1-2 Captain’s EGPWS Panel IDD 800-008082-1 Gray

Figure 5.1.5.1-2 Captain’s EGPWS Panel IDD 800-008082-1 Gray applies to Aircraft Types 217-

224: B737-300/500, B757-200/200ER, and B767-200/300/300ER.

2.25

5.50


1.15 SQUARESWITCH CUTOUT

SWITCH CUTOUT TOBE RING-LIGHTED PERBOEING SPEC S233T100

Figure 5.1.5.1-3 Captain’s EGPWS Panel IDD 800-008083-1 Brown

Figure 5.1.5.1-3 Captain’s EGPWS Panel IDD 800-008083-1 Brown applies to Aircraft Types

221-224: Boeing 757-200/200ER and Boeing 767-200/300/300ER

Allied Signal, Inc.


Korry P/N Qty per A/C Switch Type IlluminationSource Legend Color Legend

Nomenclature Voltage Switch Action

43300-001 2 433 (1”) LED WhiteGreen

TERRPEAKS

28 VDC28 VDC Indicator

433-673-1006-6044 433 (1”) LED White ON 28 VDC Momentary

433-673-1006-6120 1 433 (1”) LED WhiteAmber

OVRDFAIL

5 VAC28 VDC Alt.

433-673-1006-6121 1 433 (1”) LED WhiteAmber

OVRDINOP

28 VDC28 VDC Alt.

311-1537-015 2 311 Base N/A N/A N/A N/A Mom.

21657-002 2 427 (5/8”) Incand. WhiteGreen

TERRPEAKS

28 VDC28VDC Indicator

17479-575 2 427 (5/8”) Incand. RedAmber

GPWSGPWS

28 VDC28 VDC Mon.

43300-002 2 433 (1”) LED GreenAmber

TERRINOP

28 VDC28 VDC Mom.

433-673-1006-6035 1 433 (1”) LED WhiteWhite

OVRD------

5 VACN/A Alt.

433-673-1006-6107 1 433 (1”) LED WhiteAmber

G/S INHBGND PROX

28 VDC28 VDC Mom.

23246-303 1 318 Cap LED White G/S INHB 28 VDC N/A

23246-002 1 318 (1/2”x1”) LED Amber GPWS 28 VDC Ind. (PTT)

23328-001 2 427 (5/8”) LED Red PULL UP 28 VDC Mom.

23328-002 2 427 (5/8”) LED RedAmber

WIND SHRWIND SHR

28 VDC28 VDC Indicator

23328-003 1 427 (5/8”) LED WhiteAmber

TERRINOP

28 VDC28 VDC Mom.

Table 5.1.5.1-1 Sample Lights

Allied Signal, Inc.


5.1.6 Switching Relays

Switching relays are only used when required by the aircraft configuration to switch the displays

between weather radar and terrain. AlliedSignal has no specific vendor recommendations for

relays.

The minimum relay requirements are:

� 4 PDT� Continuous duty cycle� Pickup voltage: 13.5 VDC (maximum)� Dropout voltage: 7.5 VDC to 20 VDC� Coil resistance: ~500 ohms� Coil rating: 26.0 VDC (nominal) to 34.0 VDC (maximum)� Contact V-drop: No more than 125 mV at rated load� Contact current rating: 2A resistive at 28 VDC

Coaxial relays are not required. The standard relay recommendations are:

� Airbus: Specification number OE246-28AO.

� Boeing: Specification number BACR13CE2, vendors vary.

� McDonnell Douglas: Specification number 5D0004-1, vendors vary.

� Alternate sources: Leach International K4D series

Struthers-Dunn, Inc. FCA410-xxx

5.1.7 GPS Antenna

A GPS antenna is required when installing a MK V EGPWC that includes an internal GPS (part

number 965-0976-020-xxx-xxx). Note: The MK V EGPWC with internal GPS is not available prior

to 965-0976-020-208-208.

Recommended GPS Antennas are:

Sensor System L1 GPSAntenna Part Number Description

S67-1575-52 An active ARINC 743A antenna with a 26dB pre-amp.

S67-1575-133An active ARINC 743 antenna with a 33dB pre-amp.

Note: Boeing has selected this antenna for all aircraft withMMR installations.

Allied Signal, Inc.


5.1.8 GPS Cable Contacts

GPS cabling and contacts are required when installing a MK V EGPWC that includes an internal

GPS (part number 965-0976-020-xxx-xxx). Note: The MK V EGPWC with internal GPS is not

available prior to –208.

Vendor & Part No.Item

AMP AlliedSignalPIC Wire & Cable

Supply

RG/U Cable 142

AMP Connector P/N 225791-2 440-1238-001

Center Contact Tool 220066-2

Crimp Tool Positioner

Ferrule Crimping Tool 220066-1 or -2

Insertion & Extraction Tool 91074-1

5.1.9 GPS Cabling

GPS cabling is required when installing a MK V EGPWC that includes an internal GPS (part

number 965-0976-020-xxx-xxx). Note: The MK V EGPWC with internal GPS is not available prior

to –208.

The maximum cable loss allowable between the GPS antenna and the EGPWC is:

GPS Antenna Part Number Maximum Allowable Cable Loss

S67-1575-52 8dB

S67-1575-133 15dB

The following table shows the PIC Wire & Cable part numbers and the attenuation of the various

cables:

GPS Cable Part Number (PIC) Attenuation (dB/ft)

S44191 0.158

S44193 0.150

S67163 0.098

S33141 0.094

S55122 0.068

Allied Signal, Inc.


5.2 Wiring

ARINC 429 wiring must be a twisted shielded pair.

Terrain Display wiring (ARINC 453) must meet the weather radar display manufacturer’s

requirements including termination.

ARINC 453 bus wiring must meet the following requirements:

� Cable length must be 300 feet (91.4 meters) or less� Wire to wire capacitance must not exceed 5 pF/foot� Shielded twisted pair with not less than one twist/inch� Impedance of 70 ohms +- 10% at 1 MHz� PIC wire and cable part number: D771553

Allied Signal, Inc.


5.3 Vendor Contact Information

The vendor contact information provided below is current at the time of publication of this

document.

AMP 2800 Fulling Mill RoadMS 038-035Middletown, PA 17507800 806-0480

Barry Controls Burbank, CA818 843-1000

Brighton, MA616 787-1555

United Kingdom:Surrey, England44 (0932) 22-4122

Germany:Raunheim, Germany49 (6142) 43077/8/9

Barry ControlsAvionics Racking Systems

4510 Vanowen StreetBurbank, CA 91505818-955-4234

The Boeing Company Seattle, WA425-865-7950Fax: 425-865-7841email: [email protected]

Chelton, Inc.(previously EMHTechnologies)

P.O. Box 976Lewisville, TX 75067972-221-1783

Electronic Cable Specialistsand Electrical ConservationSystems, Inc.

5300 W Franklin DriveFranklin, WI 53132-8642414 421-5300

Framatome (Souriau)Connectors International

Namchester, NH1-800-237-2374

Hollingsead International Santa Fe Springs, CA213 921-3436

IDD Aerospace Redmond, WA425 885-4353

ITT Cannon Santa Ana, CA714 557-4700

Allied Signal, Inc.


Korry Electronics 901 Dexter Avenue NorthSeattle, WAAttention: Airline Sales206 281-1300800 257- 8921

For orders and AOG requirements, contact:Sonya Cordova206 281-3567email: [email protected]: 206 281-3576SITA: SEAKEXD

For engineering inquiries, contact:Bob JacquesAirline Business Manager206 281-3584email: [email protected]: 206 273-4128

Tom HowardAirline Business Manager206 281-1458email: [email protected]: 206 273-4128

Leach International 6900 Orangethorpe AvenueP.O. Box 5032Buena Park, CA 90622-5032

Master Specialties Co. Costa Mesa, CA714 642-2427

PIC Wire & Cable Supply N63 W22619 Main StreetP.O. Box 330Sussex, WI 53089-0330414 246-0500Fax: 414 246-0450

Sensor Systems, Inc. 8929 Fullbright AvenueChatsworth, CA 91311818 341-5366Fax: 818 341-9059

TRI-Star 800 645-2202

West Coast Specialties Issaquah, WA425 392-3118

Allied Signal, Inc.


5.4 Sample Parts Lists, Lights and Lightplates

5.4.1 Boeing 737-300 with PPI Display (Aircraft Type 16)

This is a sample “Installation Parts List” based on installation of the EGPWS MK V P/N 965-0976-

003-202-202 in Aircraft Type 16 (B737-300 Southwest Airlines). Terrain Awareness and PPI

display are located on P9 panel between the two pilots.

Item Quantity Vendor Part Number Drawing Number

EGPWS Master Kit(includes:annunciators,harness, circuitbreaker)

120-80111

Annunciators InstallKit

600-80339-101 600-80339

� GPWSAnnunciator

200-80242-101

� Relay Socket 14contact

BACS16AF1

� Relay 4 PDT, 2Amp

BACR13CE2 or equivalent

� ON/-AnnunciationSwitchlight

1 Korry Electronics 433-673-1006-6122

� INHIBIT/FAILSwitchlight

1 Korry Electronics 433-673-1006-6123

EGPWS Harness KitElectronic Cable

Spec. 600-80273-101 600-80273

� EGPWS PlacardElectronic Cable

Spec. 200-80270-002

� D9102J PlacardElectronic Cable

Spec.200-80270-004

� ConnectorElectronic Cable

Spec. MS24264R20B41SN

Circuit Breaker InstallKit

Electronic CableSpec. 600-80274-101 600-80274

� TERR SELECTPlacard

1 Electronic CableSpec. 200-80270-001

� Circuit Breaker2.5A

1 Electronic CableSpec. BACC18Z2R

� Circuit BreakerPlacard

Electronic CableSpec. C9901 200-80270-003

Allied Signal, Inc.


The following indicators and switches are associated with the EGPWS:

Indicator/Control Color Location Function

PULL UP light (2) RED Pilot’s P1-1 and copilot’sP3-1 panel EGPWS Pull Up warning alerts

GLIDESLOPE light (2) AMBER Pilot’s P1-1 and copilot’sP3-1 panel BELOW GLIDESLOPE caution alerts

WINDSHEAR light &annunciation (2) RED Pilot’s P1-1 and copilot’s

P3-1 panel WINDSHEAR warning

GPWS INOP annunciation AMBER Copilot’s P3-7 panel Indicates GPWS and/or Windshearwarning is inoperative

GEAR INHIBIT switch none Copilot’s P3-7 panel Inhibits GPWS Mode 4A “Too LowGear” alert.

FLAP INHIBIT switch none Copilot’s P3-7 panel Inhibits GPWS Mode 4B “Too LowFlap” alert.

Terrain DISPLAY switch GREEN P9 panel forward ofweather radar indicator

Provides manual selection/deselectionof EGPWS terrain display

Terrain INHIBIT switch WHITE P9 panel forward ofweather radar indicator

Inhibits TAAD and TCF functions.White INHIBIT illuminated whenselected.

Terrain FAIL AMBER P9 panel forward ofweather radar indicator

Indicates TAAD and TCF areinoperative.

WXR switch none On weather radar indicator Enables display of TAAD

Allied Signal, Inc.


Allied Signal, Inc.


5.4.2 Boeing 737-300 / -400 / -500 UAL “4-Button Push” Layout

The list is a sample “Installation Parts List” based on installation of the EGPWS MKV P/N 965-

0976-003-206-207.


EGPWS LightplateP1-3 CAPT.

1 9F22978-504 6F16811-105

EGPWS LightplateP3 –3 F/O 1 9F22978-502 6F16811-102

Lightplate Placard 836-7035-005U1 3F18879

Insulator (Lightplate)P1

634-3042-001

Lightswitch, (S1, S2) 2 Korry Electronics 17479-463 6F16811-101

Switching Relay E2-3 4 3SAH1326A2

� Relay Bracket 2 3F18880-501

� Relay SocketHardware KitCNS110902

9F23056-101

� Contact 34 BACC47ER1

� EGPWS RelayPlacards Kit(R9024, R9025,R9026, R9027)

9F18876-1, -2, -3 ,-4

Allied Signal, Inc.




PULL UP light (2) RED Pilot’s P1-1 andcopilot’s P3-1 panel

EGPWS warnings andcautions

BELOW G/S switch/light (2) AMBER Pilot’s P1-1 andcopilot’s P3-1 panel

BELOW GLIDESLOPECaution and push-to-inhibit

WINDSHEAR Annunciation (2) RED Captain’s and FirstOfficer’s EADI WINDSHEAR warning

Ground Proximity INOP light AMBER First Officer’s P3-7 panel Indicates GPWS and/or Windshearwarning is inoperative

GEAR INHIBIT switch(See note 1)

none First Officer’s P3-7 panel Inhibits GPWS Mode 4A “Too LowGear” alerts

FLAP INHIBIT switch(See note 1) none First Officer’s P3-7 panel Inhibits GPWS Mode 4B “Too Low

Flap” alerts

TERR ON switch/light (2) WHITE P1-3 & P3-3 Instrumentpanel

Provides manual selection/deselectionofWeather radar on the EHSI display

WXR/TERR ON switch/light (2) WHITE P1-3 & P3-3 Instrumentpanel

Provides manual selection/deselectionof EGPWS terrain/obstacle display

WXR/TERR ON switch/light (2)CAUTION: see note 2) WHITE Captain’s and First Officer’s

EHSI control Panel

Enables weather radar andterrain/obstacles to be displayed on theEHSI on that side.CAUTION; see note 2

TERR OVRD OVRD switch/light WHITE P1-3 Instrument panelInhibits TAAD and TCF functions.White OVRD illuminated whenselected.

TERR OVRD INOP light AMBER P1-3 Instrument panel Indicates TAAD and TCF areinoperative.

Ground Proximity Sys TestSwitch none First Officer’s P3-7 panel Activates the EGPWS self test (ref

section V.7)

Captain’s Lightplate GRAY P1-3 Instrument panel Lightplate (ref. Section 5.1.5.1)

First Officer’s Lightplate GRAY P3-3 Instrument panel Lightplate (ref. Section 5.1.5.1)

Allied Signal, Inc.


The following is an example cockpit layout for a Boeing 737-300/400/500 EGPWS installation.

W X R T E R R

O N O NOVRD

TERROVRDTERRWXR

ONON

WXR/TER

Modified light plate & switch

Currentlylabeled“WXR”

Allied Signal, Inc.


5.4.3 Boeing 737-400 (Aircraft Type 101)


001-100-100 in Aircraft Type 101 (B737-400 Alaska Airlines). Terrain Awareness and PPI display

are located on P9 panel between the two pilots.


EGPWS Lightplate B-3444010141

� Terrain System 1 B-3444010141-1

� Terrain Display 1 B-3444010141-2

� Terrain System 1 B-3444010141-3

Terrain ModuleAssembly Kit P8-60

B3444010142

� LightplateConnector

1 (L1) West CoastSpecialties

90-42301-1

� Lightswitch(S1, S2)

2 Korry Electronics 17479-463

� ConnectorReceptacle

1 (J1) MS24264R14B15P

Switching Relay E2-3

2 R671 & R672 B3444010143

Annunciator &Control Panels (P3-1, P1-3, P3-3)

B3444010144

� Captain’sTerrainAnnunciators(L1330, P1-3)

B3444010145

� First Officer’sTerrainAnnunciators(L1331, P3-3)

B3444010145

� Terrain SystemINOP Light(L1332, InhibitSwitch,LightplateAnnunciators)

B3444010145

Terrain & RelayPlacards

2 R671 & R672 B3444010147

� “TERRAINDISPLAY”(Capt, “R671”,F/O, “R672”)

B3444010147-1

Allied Signal, Inc.




PULL UP lights (2) REDUpper left of EADI onCaptain's and FO'sInstrument Panel

EGPWS warning alerts

BELOW G/S lights (2) AMBERUpper left of EADI onCaptain's and FO'sInstrument Panel

G/S caution and push to inhibit

WINDSHEAR RED On each EADI WINDSHEAR warning

Ground Proximity INOP light AMBERGround Proximity Panel onlower Portion of FO'sInstrument Panel

Indicates GPWS and/or Windshearwarning inoperative

GEAR INHIBIT switch noneGround Proximity Panel onlower Portion of FO'sInstrument Panel

Inhibits GPWS Mode 4A “Too LowGear” caution. (May be manually resetby pilot)

FLAP INHIBIT switch noneGround Proximity Panel onlower Portion of FO'sInstrument Panel

Inhibits GPWS Mode 4B “Too LowFlap” caution. (May be manually resetby pilot)

CAPT/FO Terrain DisplaySelector Switches (2) none Aft Electronics Panel


CAPT/FO Terrain Display ONlights (2)

WHITE Aft Electronics Panel Indicates the terrain/obstacle display isactive

Terrain System INHIBIT switch noneTerrain System Panel onlower Portion of FO'sInstrument Panel

Inhibits TAAD and TCF functions.

TERR lights (2) GREENUpper right of EHSI onCaptain's and FO'sInstrument Panel

Indicates the terrain/obstacle display isactive

Terrain System INOP light AMBERTerrain System Panel onlower Portion of FO'sInstrument Panel

Indicates the terrain/obstacle display isnot available.

Allied Signal, Inc.


Allied Signal, Inc.


Allied Signal, Inc.


5.4.4 Boeing 757-200 (Aircraft Type 105) or Boeing 767-200 AmericanAirlines (Aircraft Type 106)


001-100-100 in Aircraft Type 105 (B757-200) or Aircraft Type 106 (B767-200 American Airlines).


EGPWSSwitchlights

Boeing BOEING KIT F0455-16 & -2 CBE1229

� TERR(L9002, P1-1)

1 433-673-1004-4119

� TERR(L9003, P3-1)

1 433-673-1004-4119

� TERR OVRD(L9004, P1-3)

1 433-673-1004-4120

� Switchguard 433-100-002

EGPWSSwitchlightsPlacard

Boeing BOEING KIT F0455-3 CBE1227-1

� Terrain DisplayP1 & P3

� Terrain SystemOverride &Display

Connectors Boeing

� Connector E2-3D9020P

1 BACC45FT22A55P8

� Connector E2-3D9020J

1 BACC45FN22-55S8

� Connector P-36D9021P

1 BACC45FT18A31P8

� Connector P-36D9021J

1 BACC45FN18-31S8

Switching RelayP-36

1 Boeing Boeing Kit F0455-1

� Relay 2 BACR13CE2 or equivalent

� Sockets 2 BACS16AF1

� Placards K9002& K9003

-5 &-7 CBE1228

Note: * Kits F0455-2, -3, -4, -5 & -6 wiring cards. All wires and connectors included for Interfacing.

Allied Signal, Inc.


EGPWS INDICATORS AND CONTROLS



PULL UP light RED Next to standby ADI EGPWS Pull Up warning alerts

GND PROX light AMBER Next to EICAS EGPWS caution alerts

WINDSHEAR light & annunciation RED Next to standby ADIAnd on each PFD

WINDSHEAR warning

WINDSHEAR annunciation AMBER On each PFD WINDSHEAR prealert

GPWS FAULT annunciation AMBER On EICASIndicates GPWS and/or Windshearwarning isinoperative

GEAR OVRD switch none In front of co-pilotInhibits GPWS Mode 4A “Too LowGear” alert. (May bemanually reset by pilot).

FLAP OVRD switch none In front of co-pilot

Inhibits GPWS Mode 4B “ TooLow Flap” alert. (May beManually reset by pilot)

Terrain SELECT switches (2) WHITE In front of pilot near EHSIProvides manual selection/deselectionofEGPWS terrain display

Terrain OVRD switch none On main panel near EHSIInhibits TAAD and TCF functions.White OVRD illuminated whenselected.

Terrain FAIL AMBER On main panel near EHSI Indicates TAAD and TCF areinoperative.

WXR switch none On EHSI control panel Enables display of TAAD

Allied Signal, Inc.


Allied Signal, Inc.


5.4.5 Airbus A310 (Aircraft Type 108)


003-105-105 in Aircraft Type 108 (A310 FedEx). The aircraft configuration is dual WXR, EFIS

Display with popup feature, and no Windshear.


Relay 4 Boeing BACR13CE2, 4PDT

� Socket Kit 2 BACS16AF1

� EGPWS Bracket 1 Z-34-009

� Kit E0634-4

� Module Contact 9 NSA937910EA2200*

� Pin Contacts 8 BACC47EF1*

EGPWS RackConnector (Mateswith TRI-StarEGPWS EnclosureConnector)

1ITT Cannon,Amp, Inc., or

Souriau

BKAD1-125-30008-FONIC66F11A08AA1

S611-MG-05W2-P0008-LM960-0329-201

EGPWSAnnunciator/SWPanel,Capt 9001 WZ

1 EMH Technologies 907-1102-022* Z-34-006

EGPWSAnnunciator/SWPanel,FO 9002 W


EGPWS Placards EMH Technologies Z-11-083

Cover PlateAssembly EGPWS

EMH Technologies Z-34-014

Allied Signal, Inc.





GPWS light/switch (2) RED Right of Baro Altimeter

EGPWS alert.Pressing this switch will initiate anEGPWS Level 1 self test when theAircraft is on the ground.

G/S light/switch (2) AMBER Right of Baro AltimeterEGPWS Glideslope alerts.Pressing this switch between 30-1000 FT AGL will inhibit G/S alerts.

GPWS FAULT/OVRD light AMBER/WHITE

Side Panel on Left ofCaptain.

Indicates FAULT if GPWSFunction is inoperative.Indicated OVRD if Flap OverrideIs selected.

GPWS OFF and FLAP OVRDSwitch None Side Panel on Left of

Captain.Inhibits EGPWS audio or setsFlap Override to EGPWS.

Warning System EmergencyCancel switch none Pedestal-below flaps

Control.

Inhibits GPWS Mode 4A “Too LowGear” caution. (May be manually resetby pilot)

GPWS Landing Slats/Flapsswitch none

Pedestal – near right FMCCDU.

Inhibits GPWS Mode 4B “Too LowFlap” caution. (May be manually resetby pilot)

Terrain SELECT switches (2) BLUEIn front of each Pilot nearND on EGPWS Panel.


Terrain OVRD switches (2) WHITE In front of each Pilot nearND on EGPWS Panel.

Inhibits TAAD and TCFFunctions. White OVRDIlluminated when selected.

Terrain FAULT light AMBER In front of each Pilot nearND on EGPWS Panel.

Indicates FAULT if TAAD andTCF are inoperative.

Allied Signal, Inc.


5.4.6 MD 80 EFIS (Aircraft Type 114) American Ai rlines


003-105-105 in Aircraft Type 114 (MK 80 EFIS American Airlines).


EGPWS Switchlights Boeing Wiring Kit K2037-6 CBE1229

� TERR CaptAL20-2

1 433-673-1004-4119

� TERR FOAL20-1

1 433-673-1004-4119

� Terr OVRD CaptAL20-3

1 433-673-1004-4120

� Switchguard 433-100-002

EGPWS SwitchlightsPlacard

Boeing Wiring Kit K2037-7 CBE1227-1

� TERR CaptAL20-2

CD2956-11

� Terr OVRD CaptAL20-3

CD2956-7

� TERR FOAL20-1

CD2956-5

� Capt TERR SYSOVRD & Display

CTY2039-5

� FO TERR SYSOVRD & Display

CTY2039-7

Connectors Boeing

� Connector E2-3D9020P

1 BACC45FT22A55P8

� Connector E2-3D9020J

1 BACC45FN22-5588

� Connector P-36D9021P

1 BACC45FT18A31P8

� Connector P-36D9021J

1 BACC45FN18-3188

EGPWS TrayAssembly AU10-34GPWS

FDK2957-501

EGPWS Placard TrayAU10-34 GPWS

CDK2957-3

Switching Relay P-36 1 Boeing Kit F0455-1

� Relay 2 BACR13CE2

� Sockets 2 BACS16AF1

� Placards K9000 &K9001

-5 & -7 CBE1228

EGPWSAnnunciator/SW Panel,FO 9002 W


EGPWS Placards EMH Technologies Z-11-083

Cover Plate AssemblyEGPWS EMH Technologies Z-34-014

Note: Kits F0455-2, -3, -4, -5 & -6 wiring cards. All wires and connectors included for interfacing.

Allied Signal, Inc.





GPWS lights (2) RED

One on the Captain’sInstrument Panel, One onthe First Officer’sInstrument Panel

EGPWS “PULL UP” warnings andcautionary alerts except for“GLIDESLOPE”

Below G/S lights (2) AMBER


EGPWS cautionary “GLIDESLOPE”

Push light to inhibit glideslope alert.

GPWS FAIL light AMBER Forward Overhead SwitchPanel

Indicates parts or all of the GPWSare inoperative. Does not includeTAAD and TCF.

FLAP OVRD Switch(combined with TEST switch) None Forward Overhead Switch

Panel

Inhibits GPWS Mode 4B “TOO LOWFLAP” alert. (Must be manually reset bthe pilot.)

Terrain SELECT switches (2) WHITE



Terrain OVRD switches (2) None Captain’s Instrument Panel

Inhibits TAAD and TCFFunctions. A white OVRD isilluminated when selected. (Must bemanually reset by the pilot.)

Terrain FAIL AMBER Captain’s Instrument Panel Indicates the TAAD and/or TCFfunctions are not available.

Allied Signal, Inc.


Allied Signal, Inc.


6 Installation/Ground Check Procedure

AlliedSignal ground test procedures are available for some Aircraft Types and will be provided

upon request. If a ground test procedure is not available for a particular Aircraft Type,

AlliedSignal will provide assistance generating a procedure.

The MK V EGPWS provides RS-232 ports via the front and rear connectors to support monitoring

of internal parameters for testing purposes. The monitoring of these parameter values enables

the operator to quickly determine if the correct signal and scaling is being used by the EGPWS

computer.

For testing purposes, AlliedSignal provides, free of charge, a terminal emulation program called

WinVIEWS designed to run on a Windows (3.1 or later) based PC. To use WinVIEWS, an RS-

232 cable must be fabricated to interface between a PC and the EGPWC front panel connector or

between a PC and a breakout of RS-232 from the EGPWC rear connector. See Section 5.1.4 for

details on interfacing to the EGPWC front panel connector.

The PC connector is a 9-pin “D” male that attaches to the serial port interface. The table below

shows the wiring of the 3-wire RS-232 cable.

RS-232 Receive RS-232 Transmit RS-232 Ground

EGPWS Rear Connector Pin TP6C Pin TP6B Pin MP3A

EGPWS Front Connector Pin 3 Pin 4 Pin 1

Standard DB9 Connector(for a PC)* Pin 3 Pin 2 Pin 5

*NOTE: Some PC Comm Ports have Pins 2 & 3 reversed from the above DB9 description.

The communication link utilizes the RS-232 Communication Protocol configured as follows:

19200 Baud, No Parity, 8 bits, and 1 stop bit.

The EGPWS will activate the first RS-232 port upon which it receives the link initialization

character (control z) after power on.

Allied Signal, Inc.


7 Certification

AlliedSignal Air Transport STCs are available at no cost for some Aircraft Types to use as

templates. STCs may also be privately owned. For General Aviation aircraft, AlliedSignal holds

no STCs but does have a database of STCs available from other sources. More information onSTCs is available at the AlliedSignal website: www.egpws.com.

For Installation Service Bulletins (SBs), contact the Original Equipment Manufacturer for price

and availability.

Allied Signal, Inc.


8 Questions & Answers

Refer to the Line Maintenance Manual, 060-4199-014, for information on troubleshooting an

installation or call AlliedSignal for assistance.

GPWS Hotline 1-800-813-2099

When troubleshooting Program Pin strapping, refer to the Program Pin state.

Allied Signal, Inc.


9 Worksheets

This section contains a full set of the worksheets contained in this document.

Allied Signal, Inc.





ReferenceSection


Aircraft Type

Does the aircraftconfiguration support therequired ARINC 429inputs?

Aircraft Type

_____________________

The Aircraft Type defines the basic operating environment ofthe MK V EGPWC by defining the specific aircraft model,electrical interfaces and non-selectable features. The AircraftType controls the availability of some options. A single aircraftmodel may have several Aircraft Types to allow for different on-board systems and features.

ACTION: Review information in reference sections;identify potential Aircraft Types and record the AircraftType Numbers at right. Complete feature selection portionof this worksheet (the left side) then select the specificAircraft Type from the options at left.

-101 andon (seeApp. A

for avail.of each

A/CType)

3.14.2.1

Does the aircraftconfiguration support therequired analog inputs (ifany)?

Display

Terrain display

_____________________

Terrain is displayed on an existing display (typically the samedisplay used to display weather). Display discussions applyonly to the display(s) for terrain data. Auto-ranging is availablefor some displays.

Terrain display is only used if Terrain Awareness & Display isenabled (see Section 3.11.1.)

Prior to version –208, the PPIN State 1 display interface in theAircraft Type’s “Display Options & Peaks Availability” table isthe only display supported by that Aircraft Type.

ACTION: Record the PPIN States for applicable terraindisplay types for each candidate Aircraft Type at right. Ifinstalling version –208 or newer, complete the left side ofthis worksheet and select the Aircraft Type, then recordthe PPIN state for the display at left (enter N/A if installinga version older than –208).

-101 andon

3.24.2.12

If display(s) will be usedand installing version –208or newer, does the aircraftconfiguration match any ofthe displays defined for the

Aircraft Type?OR

If display(s) will be usedand installing version –206or older, does the aircraftconfiguration match therequired display for the

Aircraft Type?

Allied Signal, Inc.





ReferenceSection


Basic GPWS Functions/Options

Altitude Correction

QNH

QFE

QNH is barometric altitude corrected to mean sea level and isthe most common correction format.

QFE is barometric altitude corrected to read zero feet at therunway regardless of the mean sea level altitude of the runway.

ACTION: Review reference sections and record the QNHor QFE selection at left.

-101 andon

3.34.2.2

4.2.2.1

EGPWS Suppression

Suppress Audio Only

Suppress Audio andVisual

No Suppression(Do not use discreteinput)

The MK V EGPWS Audio Inhibit discrete input normallysuppresses MKV EGPWS callouts (except reactive windshear)manually via a cockpit-mounted switch or automatically via theDSWC and PWS computers.

Audio Inhibit discrete can be configured to also suppress non-windshear visual alerts (lamps).

If EGPWS suppression is not desired, the Audio Inhibit discretecan be left disconnected.

Recommendation: AlliedSignal recommends the use of theAudio Inhibit feature to maintain appropriate audio and visualprioritization in the cockpit.

ACTION: Review reference sections and record thepreferred suppression behavior at left.

-101 andon

3.44.2.2

4.2.2.2

Allied Signal, Inc.





ReferenceSection


Glideslope Cancel



Alternate G/S Cancel

The Standard Glideslope Cancel allows the crew to manuallycancel the “Glideslope” alert when below 2000 feet RadioAltitude. The cancel is automatically reset when above 2000feet RA. (Some Aircraft Types use 1000 feet RA for theStandard G/S Cancel.)

The Alternate Glideslope Cancel allows the crew to manuallycancel and re-activate the “Glideslope” alert any time at anyaltitude. This option is not currently being certified by the FAAin Part 121 aircraft.

ACTION: Review reference sections and record theGlideslope Cancel preference at left.

-101 andon

3.54.2.2

4.2.2.3

If the Standard GlideslopeCancel is selected, doesthe Aircraft Type supportthe G/S Cancel Altitude

preference?

Steep Approach

Enabled

Disabled

Steep Approach desensitizes the Mode 1 (Excessive DescentRate) alert boundaries to permit safe but steeper than normalinstrument precision approaches (e.g. MLS or GPSapproaches) without unwanted alerts.

This feature is not available on all aircraft .

NOTE: This option is controlled by discrete inputs (notProgram Pins).

ACTION: Review reference sections and record thepreferred Steep Approach enabling at left.

-101 andon

3.64.5.30

If Steep Approach isselected, does the Aircraft

Type support it?

Allied Signal, Inc.





ReferenceSection


Alternate Mode 4B 2

Use Alt. Mode 4B

Do not use Alt. Mode4B

Mode 4 provides alerts for insufficient terrain clearance withrespect to phase of flight and speed. Alternate Mode 4Bprevents nuisance MK V EGPWC warnings during approacheswith the gear up.

Prior to version –208, Alternate Mode 4B is activated only bythe Aircraft Type.

Recommendation: AlliedSignal recommends the use ofAlternate Mode 4B and the flap override switch for all GeneralAviation and Bizjet aircraft.

ACTION: Review the reference sections and record thepreferred Mode 4B functionality at left.

-208 andon

3.74.2.10

If installing version –206 orolder and Alternate Mode4B is selected, does the

Aircraft Type select itAlternate Mode 4B?

Windshear Detection andAnnunciation

W/S Enabled & W/SCaution uses no voice

W/S Enabled & W/SCaution uses voice

W/S Enabled & No W/SCaution

W/S Disabled

W/S Disabled & W/SINOP discrete disabled

The MK V EGPWS provides a reactive Windshear capabilitythat is enabled only by the Aircraft Type. Windshear can bedisabled during installation.

The basic W/S enabling includes both the W/S Warning andW/S Caution. This W/S Caution does not include an audio(voice) alert.

Recommendation: AlliedSignal recommends disabling theWindshear INOP discrete if Windshear is disabled.

ACTION: Review the reference sections and record thepreferred Windshear functionality at left.

-101 andon

3.84.2.3

If Windshear is required,does the Aircraft Type

enable it?

Allied Signal, Inc.





ReferenceSection


Lamp Format 2

Lamp Format 1

Lamp Format 2

The Aircraft Type defines the lamp configuration (Lamp FormatType 1 or 2) for an installation. The lamp formats are definedin the reference section. Beginning with version –208, LampFormat Type 2 can be selected via Program Pin if the AircraftType defines the lamp configuration as Lamp Format Type 1.


ACTION: Review reference sections and record thepreferred Lamp Format at left.

-208 andon

3.94.2.3

4.2.3.2

If installation version –208or newer and Lamp Format

Type 1 is required, doesthe Aircraft Type select it?

ORIf installing version –206 or

older, does the AircraftType select the required

Lamp Format?


Aircraft Installation


The Simulator Reposition Program Pin and discrete inputs areused to enable instantaneous repositioning for non-aircraftinstallations. Refer to Aircraft Type to determine if theSimulation Reposition discrete input is defined for the AircraftType.

ACTION: Review reference sections and record theinstallation location at left.

-208 andon

3.104.2.4

4.2.4.2

If this installation is in asimulator, does the A/CType support the SimulatorReposition discrete input?

Note: A simulatorinstallation is possible evenif the Simulation Repositionoption is not available.

TAD & TCF(Enhanced Feature

Control)

Enabled

Disabled

The Terrain Awareness & Display feature computes terrainclearance envelopes ahead of the aircraft, issues and displaysthe terrain data relative to aircraft altitude.

The Terrain Clearance Floor (TCF) algorithm identifiespremature descent for approaches regardless of aircraftconfiguration.

ACTION: Review reference sections and record thepreferred TAD & TCF enabling at left.

-101 andon

3.113.11.14.2.4

4.2.4.1

Allied Signal, Inc.





ReferenceSection


Obstacle Awareness

Enabled

Disabled

Added in version –204, Obstacle Awareness warns of man-made obstacles at least 100’ taller than surrounding terrain.Obstacle data is currently available for North America and partsof the Caribbean. Not all obstacles will be contained in thedatabase.

Note: TAD & TCF must be enabled for Obstacle Awareness.

ACTION: Review reference sections and record thepreferred Obstacle Alerting enabling at left.

-204 andon

3.113.11.24.2.4

4.2.4.1

Peaks Mode 1

Enabled

If installing version –208 ornewer and the Peaks

display mode is preferred,does the selected display

support it?

Disabled

Peaks mode is an alternate means of displaying terrain datathat provides increased situational awareness by displayingabsolute terrain elevations in addition to the standard modepresentation.

Note: For version –206, TAD, TCF and Obstacles must beenabled if Peaks mode is enabled. Beginning with –208, TADand TCF must be enabled if Peaks mode is enabled.

ACTION: Review reference sections and record thepreferred Peaks Mode enabling at left.

-206 andon (somedisplays)

3.113.11.34.2.4

4.2.4.1 If Obstacle Awareness isdesired, is version –204 or

newer being installed?

Bank Angle Callouts(Bizjet)

Enabled

Disabled

Bank Angle Callouts may be enabled or disabled.

ACTION: Review reference sections and record the BankAngle enabling at left (if Bizjet aircraft).

-101 andon

3.123.12.14.2.5

4.2.5.1

Is the Aircraft Class“Bizjet”?

Allied Signal, Inc.





ReferenceSection


Bank Angle Algorithm(Commercial AT)

AlliedSignal algorithm

Bank Angle Option 1

Bank Angle Option 2

Disabled

For Commercial Air Transport Aircraft any one of the threeBank Angle algorithms described below may be selected orBank Angle callouts may be disabled.

ACTION: Review reference sections and record the BankAngle functionality at left (if Commercial AT aircraft).

BAOptions 1

& 2added in

-202

3.123.12.24.2.5

4.2.5.2

Is the Aircraft Class“Commercial AT”?

Altitude Callout Menu

Altitude Callout Menu ID

___________________

“Minimums” only

Disabled

Each Mode 6 Altitude Callout Menu listed in Appendix Bdefines a set of altitude awareness callouts. The optional“Smart 500” foot callout will issue a “500” foot callout when theaircraft is 500’ AGL. As an alternative to the predefined calloutmenus, a “Minimums” only callout is possible.

Recommendation: AlliedSignal recommends the use of the“Smart 500” callout if the selected menu does NOT contain a500’ callout or if all callouts in the selected menu are below500’. AlliedSignal recommends at least a callout at 500’ and a“Minimums“-type callout.

ACTION: Review reference sections and record theselected Altitude Callout menu or the altitude calloutbehavior at left.

Notes for installer:� Is ARINC 429 DH required? ______� Is DH discrete input required? ______

-101 andon

3.134.2.64.5.24.5.5

If the selected AltitudeCallout Menu includes an“Approaching Minimums”-type callout, is the ARINC429 Decision Height inputavailable for the Aircraft

Type?

Allied Signal, Inc.





ReferenceSection


Audio Menu Selection

Audio Callout Menu ID

___________________

One of seven Basic GPWS (non-altitude) alert menus must beselected to provide Basic GPWS callouts. Refer to Appendix Cfor a complete definition of each menu. DGAC-registeredaircraft are required to use Audio Menu #1.

Recommendation: Except for DGAC-registered aircraft,AlliedSignal recommends the Basic Audio Menu (Menu 0).

ACTION: Review reference sections and record theselected Audio Callout Menu at left.

-101 andon

3.144.2.7

Audio Declutter

Enabled

Disabled

Audio Declutter prevents excessive aural alerts and warningsby preventing an alert or warning from being constantlyrepeated while the condition remains true.

ACTION: Review reference sections and record the AudioDeclutter enabling at left.

-101 andon

3.154.2.8

4.2.8.3

Alert Volume

High Volume

Medium Volume

Low Volume

The Alert volume level applies to the Audio menu (warningsand cautions) and sets the baseline volume for the Mode 6callouts (altitude and bank angle callouts). The Aircraft Typedefines the default “Audio Volume”.

For –206 and on: The default Audio volume must be used ifAudio Declutter is disabled.

ACTION: Review reference sections and record thepreferred Audio volume at left.

“Medium”added in

-206

3.164.2.8

4.2.8.14.7

Allied Signal, Inc.





ReferenceSection


Mode 6 Volume

Default Volume

-6dB (permanent)

-6dB (temporary)

-3dB(version-206 and on)

-3dB & -6dB (perm.)(version-206 and on)

-3dB & -6dB (temp.)(version-206 and on)

The default Mode 6 volume is based on the Audio volume andthe Aircraft Type’s Mode 6 volume.

The Mode 6 volume can be either temporarily or permanentlyreduced 6dB below its default volume. Many installations usethe windshield wiper control to reduce the volume when thewipers are off and restore it to its default level when the wipersare on (and cabin noise increases).

For version –206 and on: An additional control is available topermanently reduce the Mode 6 volume an additional 3dB.This control may be used separately or in conjunction with the–6dB control described above.

Note: The –3dB option is not available if Audio Declutter isdisabled.

ACTION: Review reference sections and record thepreferred Mode 6 (altitude callout) volume at left.

Note: -6dB options controlled by Mode 6 Volume Controldiscrete input. –3dB option controlled by PPIN 11.

-3dBoption

added in-206

3.174.2.8

4.2.8.24.5.23

If the selected Mode 6volume is __________,does the Aircraft Type

select “Low” for the initialMode 6 Volume?

Allied Signal, Inc.





ReferenceSection


EGPWS DisplayPop-up

Yes (Pop Up)

No (Do not Pop Up)

A terrain display “pops up” when an EGPWS alert conditionoccurs and the display switches to terrain data from whateverwas being displayed prior to the alert condition (typicallyweather).

Terrain display pop up behavior is controlled by either theEGPWS or by the display itself as defined in the Aircraft Type’sDisplay Options & Peaks Availability Worksheet.

ACTION: Review reference sections; indicate whetherterrain displays should pop up over non-terrain displays atleft. (Assumes display behavior is controlled by theEGPWS.)

-101 andon

3.184.2.9

4.2.9.1

For the display selectedabove, does either the

default or alternate Pop Upbehavior support the

selected Pop Up behavior?

Predictive WindshearSystem

PWS Option 1

PWS Option 2

An external Predictive Windshear System (PWS) may beavailable on the aircraft and can be used in addition or in placeof the reactive windshear system available as part of the MK VEGPWS.

Only the PWS interface(s) defined in the Aircraft Type’s“Optional System Inputs” table are supported by the AircraftType.

NOTE: The reactive windshear Caution must be disabled if aPWS is used.

ACTION: Review reference sections and indicate at leftwhich, if any, of the optional PWS interfaces should beused.

-101 andon

3.194.2.9

4.2.9.2


optional inputs?

Allied Signal, Inc.





ReferenceSection


Optional System Inputs

Internal GPS

Optional Inputs Select

Dual External GPS

Single External GPS

Dual GPIRS

Single GPIRS

Triple LRRA

Dual LRRA

Beginning with version –208, the MK V EGPWC (part number965-0976-020-xxx-xxx) is available with an internal RS-232GPS receiver. Use of the internal GPS receiver is optional.

The Aircraft Type’s “Optional System Inputs” table defines anyoptional interfaces supported by the Aircraft Type. The ARINC429 Input Channel Assignments worksheet, Analog InputsWorksheet and Radio Altimeter Formats worksheet also showthese interfaces.

If the internal GPS receiver is activated, GPS inputs via theARINC 429 cannot be enabled. (See Optional System Inputsabove.)

ACTION: Review reference sections and record theoptional inputs to be used at left.

InternalGPS -

208 andon

3.204.2.10

4.2.10.1


optional inputs?

GPS Altitude Reference 2

Referenced to meansea level

Referenced to WGS-84

Prior to version –208, the GPS Altitude (label 076) must bereferenced to mean sea level. Beginning with version –208,the GPS Altitude may be referenced to either mean sea level orWGS-84.

ACTION: Review reference sections and record the GPSaltitude reference at left.

-208 andon

3.124.2.13

1 Added in –206.2 Added in –208.3 Available only for MK V ECPWC part numbers 965-0976-020-xxx-xxx.


Allied Signal, Inc.


PPCOM (MP03A)

E G P W S A IR C R A F T C O N FIG U R A TIO N S TR A P P IN G

DOUTL1 (MP15D)

DOUTL4 (TP12C)DOUTL5 (TP12A)DOUTL7 (TP4D)

DOUTL2 (MP03D)

PPCNF2 (TP10B)PPCNF3 (TP10C)

PPCNF4 (MP4D)PPCNF5 (MP4B)PPCNF6 (MP08A)

PPCNF8 (MP05A)PPCNF7 (MP14D)

PPCNF12 (TP05B)

PPCNF9 (MP02C)PPCNF10 (MP04A)PPCNF11 (MP04C)

PPCNF13 (MP05B)PPCNF14 (TP02C)PPCNF15 (MP15C)PPCNF16 (MP08B)

CONFIGURATION SELECTION(NONE OR ONE SELECTION PER ROW)

DOUTL3 (MP07B)

GLIDESLOPE CANCEL

TERRAIN DISPLAYABLE #1

GPWS ALERTGPWS WARNING

WINDSHEAR WARNING

PPCNF1 (TP10A)

WINDSHEAR CAUTION

PROGRAM PIN COMMON

MULTIPLEXEDSELECTPINS

PROGRAM PINSAIRCRAFT TYPE #:

CALLOUT MENU #:

AIRCRAFT STRAP #2AIRCRAFT STRAP #1

AIRCRAFT STRAP #3

CALLOUT MENU STRAP #3CALLOUT MENU STRAP #2CALLOUT MENU STRAP #1

OPTIONAL GPS/GPIRSAUDIO MENU2 ILS/2 LRRA/3 LRRAGS CAN/EGPWS SUP/QFE SELAUDIO DECLUTTER/VOLUMEWINDSHEAR CONTROLTCF DIS/TAD DIS/SIM REPO

GPS SPEEDALT POPUP / PWS OPTIONSBANK ANG/ALT RADALT

2 Count each "Program Pin" row selected (PPCNF1-PPCNF16, PPCNF18 and PPCNF19), if the number iseven, then select this block (PPCNF17). The count of all program pins selected must be odd.

All "Select Pins" used as discrete outputs that are not pulled up to at least 12 VDCmust be isolated by the use of a diode.

1

1

3

3

3 Not available prior to -208.

AUDIO ONTERRAIN DISPLAYABLE #2

DOUTL6 (TP12B)DOUTL10(TP11A)

ALT DISPLAY SELECTION PPCNF18 (MP15A) 3

OPTIONS SELECTION PPCNF19 (MP15B) 3PPCNF17 (TP06D)PROGRAM PIN PARITY (ODD) 2

PROGRAM PIN STATES (State 1 is "open".) 2 3 4 5 6 7 8 9 10

Figure 4.2-1 Program Pin Strapping Worksheet

Note: After the correct Program Pin strapping is determined for this installation, it is possible that

several Program Pins will be connected to the same output discrete. This may be implemented

by daisy-chaining the Program Pins. However, DO NOT daisy-chain the output discretes as the

MK V EGPWC will produce an error message and will not function.

Allied Signal, Inc.


ProgramPin State

AltitudeCorrection

EGPWSSuppress

GlideslopeCancel

PPCNF10(MP4A)

Strapping1 Standard Open

2Audio Only


3 Standard MP15D

4

QNH

Audio & VisualAlternate MP3D

5 Standard MP7B

6Audio Only

Alternate TP12C

7 Standard TP12A

8

QFE

Audio & VisualAlternate TP4D

ThisInstallation


ProgramPin State Windshear Windshear

CautionWindsh ear INOP

Output

Change toLamp

Format 2 1

PPCNF12(TP5B)

Strapping

1 Windshear Caution(no Voice) Open

2Normal Function

MP3A(PPCOM)

3Disabled Disabled

(no Caution)Disabled MP15D

4 Caution withVoice MP3D

5Windshear


No

MP7B

61 Windshear Caution(no Voice) TP12C

71Normal Function

TP12A

81 Disabled Disabled(no Caution) Disabled TP4D

91 Caution withVoice TP12B

101Windshear


Yes

TP11A

ThisInstallation

1Added in version –208.


Allied Signal, Inc.


ProgramPin State

SimulatorRepositionAllowed?

TAD & TCF Obstacle Awareness Peaks2PPCNF13(MP5D)

Strapping1 Default1 Open

2 Opposite of Default1Off MP3A

(PPCOM)32

Enabled

On On MP15D

4

No

Disabled Off MP3D

5 Default1 MP7B

6 Opposite of Default1Off

TP12C

72

Enabled

On On TP12A

8

Yes

Disabled Off TP4D

93 No TP12B

103 YesEnabled

OffOn

TP11A

ThisInstallation

1Default Obstacle Awareness enabling is defined by the Aircraft Type.2Added in –206 (Peaks mode applies only to selected Aircraft Types).3Added in –208.


BIZJET CONTROLSProgramPin State RA Source/Format Bank Angle Callouts

PPCNF14(TP2C)


2Default

Enabled MP3A(PPCOM)

3 Disabled MP15D


#1 Enabled MP3D

5 Disabled MP7B


#2 Enabled TP12C

ThisInstallation

Table 4.2.5-1 Program Pin 14 Worksheet for BIZJET Aircraft

Allied Signal, Inc.


COMMERCIAL AIR TRANSPORT CONTROLSProgramPin State Bank Angle Algorithm Bank Angle Callouts

PPCNF14(TP2C)

Strapping1 Default Disabled Open

2 AlliedSignal MP3A(PPCOM)

3 Bank Angle Option #1 MP15D

4 Bank Angle Option #2

Enabled

MP3DThis

Installation

Table 4.2.5-2 Program Pin 14 Worksheet for Non-BIZJET Aircraft

Program PinState Basic GPWS Menu ID PPCNF8 (MP5A)

Strapping

1 Basic Menu Open

2 Alternate #1 MP3A (PPCOM)


4 Alternate #3 MP3D

5 Alternate #4 MP7B


7 Alternate #6 TP12A

This Installation


Allied Signal, Inc.


ProgramPin State Volume Level Audio Declutter

PPCNF11(MP4C)


2Default


3 Enabled MP15D

4Alternate #1

Disabled MP3D


“Alternate #1” is the opposite (“Low” or “High”) of the Default volume.

Table 4.2.8-1 Program Pin 11 Worksheet for Version –204 and Older

ProgramPin State Volume Level Adjust Mode 6

Volume by –3dB? Audio DeclutterPPCNF11(MP4C)


2Default



4 Alternate #2

No

MP3D

5 Default MP7B


7 Alternate #2

Yes

Enabled

TP12A


“Alternate #1” is the opposite (“Low” or “High”) of the Default volume.“Alternate #2” is approximately “High” volume - 3dB and is approximately halfwaybetween the “High” and “Low” volumes.

Table 4.2.8-2 Program Pin 11 Worksheet for Version –206 And On

Allied Signal, Inc.


ProgramPin State PWS Options Alternate Pop-Up

PPCNF15(MP15C)


2None

Enabled MP3A(PPCOM)

3 Disabled MP15D4

PWS Option 2Enabled MP3D

5 Disabled MP7B6

PWS Option 1Enabled TP12C

ThisInstallation


ProgramPin State

Optional Interfaces /Interf ace ModificationsEnabled

PPCNF7(MP14D)


2 Optional Inputs Select MP3A(PPCOM)

3 Dual GPS Overlay MP15D

4 Dual GPS Overlay & Optional Inputs Select MP3D

5 Single GPS Overlay MP7B

6 Single GPS Overlay & Optional Inputs Select TP12C

7 Single GPIRS Overlay TP12A

8 Dual GPIRS Overlay TP4D

9 Internal GPS TP12B

10 Optional Inputs Select & Internal GPS TP11A

ThisInstallation


Allied Signal, Inc.


ProgramPin State Optional Interfaces Enabled Alternate

Mode 4B 1

PPCNF9(MP2C)


2 Triple LRRA MP3A(PPCOM)

3 Dual LRRA

Default2

MP15D

41 None Opposite ofDefault2 MP3D

5 Dual ILS MP7B

6 Dual ILS & Triple LRRA TP12C


Default2

TP12A

81 Dual LRRA TP4D

91 Dual ILS TP12B


Opposite ofDefault2

TP11A

ThisInstallation

1Added in version –208.2The Aircraft Typed defines the default activation of Alternate Mode 4B.


ProgramPin State Configuration Options Enabled GPS Bus Speed

PPCNF16(MP8B)


2None


3 Default MP15D


Alternate MP3D

5 Default MP7B


Alternate TP12C

7 Default TP12A

8Configuration Options 1 and 2

Alternate TP4DThis

Installation


Allied Signal, Inc.


ProgramPin State Display

PPCNF18(MP15A)


2 Alternate Display 1 MP3A(PPCOM)



5 Alternate Display 4 MP7B

6 Alternate Display 5 TP12C


8 Alternate Display 7 TP4D

9 Alternate Display 8 TP12B


ThisInstallation


ProgramPin State GPS Reference Altitude

PPCNF19(MP15B)

Strapping1 Mean Sea Level Open

2 WGS-84 MP3A(PPCOM)

ThisInstallation


Allied Signal, Inc.


Blank copies of the Appendix A Aircraft Type worksheets are included below.

Analog Input Channel Assignment

ANALOG INPUT CHANNEL ASSIGNMENTS FOR AIRCRAFTTYPES

AnalogInputChannel

Pins Connections

1+ = TP13A- = TP13B

2+ = TP14A- = TP14B

3+ = TP13C- = TP13D

4+ = TP14C- = TP14D

Radio Altimeter Formats

FormatRadio Altimeter Alternatives Selected?

Default

Alternate RA Configuration #1

Alternate RA Configuration #2

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet

AIRCRAFT TYPESARINC429

InputChannel

Pins Connections

1A=MP6AB=MP6B

2A=MP10CB=MP10D

3A=MP11AB=MP11B

4A=MP12AB=MP12B

5A=MP10AB-MP10B

6A=MP11CB=MP11D

7A=MP12CB=MP12D

8A=MP13AB=MP13B

9A=TP9CB=TP9D

10A=MP9AB=MP9B

11A=TP8AB=TP8B

12A=TP8CB=TP8D

13A=TP5AB=TP6A

14A=TP1CB=TP1D

15A=TP4AB=TP4B

16A=TP5CB=TP5D

17A=TP11CB=TP11D

18A=MP6CB=MP6D

ARINC 429 Interface Modification Options Worksheet

Program Pin / Signal FirstAvailable Changes to Interfaces Applies to

Aircraft Types Connections

Alternate GPSSpeed

ConfigurationOption 116


Allied Signal, Inc.


Discrete Inputs Worksheet

DISCRETES DISCRETE STATES FOR AIRCRAFT TYPES

Name PinConnections

MP1A

MP1B

MP2A

MP5C

MP7D

MP8C

MP8D

MP9A

MP9B

MP9C

MP9D

MP14A

MP14B

MP2D

TP1A

TP1B

MP2B

TP4C

MP5D

MP7A

TP15A

TP15B

TP15C

TP15D

TP7A

TP7B

TP7C

TP7D

Allied Signal, Inc.


Serial Outputs Worksheet

SERIAL INTERFACES FOR AIRCRAFT TYPESSerialOutput

ChannelPins Connections

TX453-1A=TP3AB=TP3B

TX453-2A=TP3CB=TP3D

TX429-1Low Speed

A=MP1CB=MP1D

TX429-2Low Speed

A=TP2AB=TP2B

Discrete Outputs Worksheet

Connections For Aircraft TypesPin Discrete Outputs

FlashingLamp

MP15D N/A

MP3D

MP7B

TP12C

TP12A

TP12B N/A

TP4D

TP10D N/A

MP14C N/A

TP11A N/A

MP7C N/A

TP12D N/A

TP11B N/A

Allied Signal, Inc.


10 AcronymsA AmpsA/C AircraftAC Alternating CurrentADC Air Data ComputerADIRU Air Data Inertial Reference UnitAFM Airplane Flight ManualAFMS Airplane Flight Manual SupplementAGL Above Ground LevelAHRS Attitude Heading Reference SystemAIMS Airplane Information Management SystemALT AltitudeALT AlternateAOA Angle of AttackARINC Aeronautical Radio, IncorporatedAT Air TransportBA Bank AngleBizjet Business Jet and General Aviation aircraftCAS Computed Air SpeedCFDS Centralized Fault Display systemCFIT Controlled Flight Into TerrainCFM Cubic Feet per MinuteCMC Central Maintenance ComputerCNX CancelDAA Digital/Analog AdapterDAU Data Acquisition UnitdB decibelsDC Direct CurrentDCP Display Control PanelDEU Display Electronics UnitDGAC Director Generale de l‘Aviation Civile (French certifying authority equivalent of

FAA)DH Decision HeightDSWC Digital Stall Warning ComputerECAM Electronic Centralized Aircraft MonitoringEFIS Electronic Flight Instrument SystemEGPWC Enhanced Ground Proximity Warning ComputerEGPWS Enhanced Ground Proximity Warning SystemEICAS Engine Indication and Crew Alerting SystemFAA Federal Aviation AdministrationFCC Flight Control ComputerFDAU Flight Data Acquisition UnitFDR Flight Data RecorderFMC Flight Management ComputerFMS Flight Management SystemFWC Fault Warning ComputerGA General AviationGPGPIRS Global Positioning/Inertial Reference SystemGPS Global Positioning SystemGPWS Ground Proximity Warning SystemG/S GlideslopeHDOP Horizontal Dilution of PositionHFOM Horizontal Figure of Merit

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Hz HertzIC Integrated CircuitICD Interface Control DocumentILS Instrument Landing SystemINOP InoperableIOC Input/Output ConcentratorIRS Inertial Reference SystemLRRA Low Range Radio AltimeterMCP Mode Control PanelMCU Modular Component UnitMFD Multi-Function DisplayMK V Mark VMLS Microwave Landing SystemmW milliwattsPC Personal ComputerpF picoFaradRAIM Receiver Autonomous Integrity MonitoringRFD Primary Flight DisplayPPIN Program PinP/TEST Push to TestPWS Predictive Windshear SystemQFE Corrected Barometric Altitude Relative to Field ElevationQNH Corrected Barometric Altitude Relative to Mean Sea LevelRA Radio AltitudeR ALT Radio AltitudeR/T Receiver/TransmitterTAD Terrain Awareness DisplayTC Type CertificationTCAS Terrain Collision Avoidance SystemTCF Terrain Clearance FloorSB Service BulletinSMYD Stall Margin Yaw DamperSPS Stall Protection SystemSSM Sign/Status MatrixSTC Supplemental Type CertificateSWC Stall Warning ComputerTCAS Terrain Collision Avoidance SystemUDI Universal Display InterfaceV VoltsVDOP Vertical Dilution of PositionVIA Versatile Integrated AvionicsVFOM Vertical Figure of MeritW WattW/S WindshearWx WeatherWXR Weather Radar

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Appendix A: Aircraft Type Tables

Appendix A contains tables and worksheets describing the aircraft configurations (Aircraft Types)

supported by the MKV EGPWS. These tables are organized by aircraft model and are described

below.

The first table for any aircraft model is the Aircraft Description Table. This table provides an

overview of each Aircraft Type defined for the aircraft model and is used to select the Aircraft

Type for an installation. An example Aircraft Description table with explanations of the entries is

provided below. A few Aircraft Description entries require additional information. They are:

Lamp Format Defines the operation of the red and amber GPWS cockpit lamps.

Beginning with version –208 Lamp Format Type 2 may be selected for

Aircraft Types using Lamp Format Type 1.

Lamp Format Type 1: Amber “Below G/S” lamps are driven by the GPWS

Alert discrete for a Below Glideslope Caution alert. Red “GPWS” lamps

are driven by the remaining non-windshear caution and warning alerts.

Lamp Format Type 2: Amber “GPWS” lamps are driven by the non-

windshear (i.e. GPWS) caution alerts and red “Pull-Up” lamps are driven

by the non-windshear (i.e. GPWS) warning alerts. The warnings generate

“Pull-up” audio messages.

AlliedSignal recommends Lamp Format Type 2.

Pop-Up andAlternate Pop-Up

Defines whether EGPWC visual alerts will “pop-up” on displays not

currently displaying terrain data. The entries are:

Yes Selected terrain-compatible displays will switch to display

surrounding terrain data.

Contained Selected terrain-compatible displays will switch to display

terrain data only when no terrain display is active.

No EGPWS alerts will not pop-up in terrain-compatible

displays.

N/A Not applicable to the Aircraft Type.

Controlled

by displayPop-up behavior is defined by the display strapping. Refer

to the display manufacturer for more information.

Allied Signal, Inc.


Aircraft Description

Aircraft Type The Aircraft Type Number(s) are listed here.

Description A phrase describing the installation environment.

P/N Availability “xxx or later” indicates the MK V EGPWC versions which include the Aircraft Type

REQUIRED SYSTEM INPUTSThese systems MUST be present on the aircraft and providing data to the MKV EGPWS as described in the ARINC 429

Input Channel Assignments Worksheet table. Only those systems required by the Aircraft Type are listed.

ADC

FMC

IOC

IRS or AHRS

LRRA

� “Single” indicates that inputs are required from one of each system listed (typically from thePrimary (#1) systems).

� “Dual” indicates that inputs are required from two of each system listed (typically from thePrimary (#1) and Secondary (#2) systems).

� “Triple” indicates that inputs are required from three of each system listed (typically fromthe Primary (#1), Secondary (#2) and Tertiary (#3) systems).

� “Four” indicates that inputs are required from four of each system listed.OPTIONAL SYSTEM INPUTS

These inputs are optional and must be enabled using the specified signals. Only those signals defined for the AircraftType are listed. If a signal is enabled, all inputs it controls MUST be provided.

OptionalInput Select

� Enables the listed inputs; may exclude inputs from other systems.� “See ARINC 429 Interface Modification Options Worksheet” indicates Optional Input Select

modifies an interface rather than enabling one.SingleExternalGPS

� Enables the optional Single GPS input; may exclude inputs from other systems.

PP

IN 7

DualExternalGPS

� Enables the optional Dual (and Single) GPS input; may exclude inputs from other systems.

Dual ILS � Enables the listed inputs; may exclude inputs from other systems.

PP

IN 9 Dual orTriple RA � Enables the listed inputs; may exclude inputs from other systems.

Alt. XXX Format � Listed inputs are optional; if controlling mechanism is not indicated, EGPWS will use ifprovided.

FEATURESThese include aircraft configuration items and options controlled by the Aircraft Type definition.

Aircraft ClassDefines the Radio Altimeter and Bank Angle options for the Aircraft Type. Is either “Bizjet” or“Commercial Air Transport”.

Audio InhibitMonitoring

Defines whether or not activating the Audio Inhibit discrete input for 60 seconds causes an“Audio Inhibit Monitoring” fault.

Alternate Mode 4B Defines whether or not Alternate Mode 4B is enabled by the Aircraft Type.

ARINC 429 DHDefines whether or not ARINC 429 Decision Height (and therefore “Approaching Minimums”callout) is available for the Aircraft Type.

G/S Cancel Alt.The altitude below which the G/S Cancel may be manually activated and above which it isautomatically reset.

Lamp FormatDefines the cockpit lamp format supported by the Aircraft Type. See definitions provided in thissection.

Mode 6 Volume The default volume for the Altitude and Bank Angle callouts.

Alert Volume The default volume for the Basic GPWS callouts.

Steep ApproachDefines whether the Aircraft Type supports the optional “Discrete” Steep Approach and/or“Digital” Steep Approach feature. (“Digital Supported” indicates label 171 bit 24 is not providedat the time of the release of this document but would be used if provided.)

Terrain RelayMonitoring

Defines whether or not the terrain select relays are monitored. If so, the inputs must beprovided. (See the Discrete Inputs Worksheet table.)

Windshear Defines whether or not Windshear Detection and Alerting is enabled.

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Display Options & Peaks Availability Falcon 2000

PPINState

DisplayAvail-ability

Display SweepStyle

AutoPop Up

AlternatePop Up

ObstacleAlertingEnabled

PeaksAvail.

PPIN 18(MP15A)

Strapping

Aircraft Type: 91 (Ref. ICD App G-16.1, 16.2)

1-202

and on

Collins ProLine IVIntegrated

(Bus type: ARINC 708Standard Data Format)

10 NM auto rangingcontrolled by display

Fan modewith +-60o

limit

Based ondisplay

controllerstrapping

N/A No No Open

2-208

and on




Fan modewith +-90o

limit

Based ondisplay

controllerstrapping

N/A No No MP3A

Aircraft Type: 125 (Ref. ICD App G-3.1)

1-101

and on

Collins ProLine IV(non-integrated), 5x6(Bus type: ARINC 708Standard Data Format)

No auto ranging

Defaultwith +-60o

limitNo Yes No No Open

Note: Prior to version –208, the display option for Program Pin State 1 is the required display. Program Pin 18 wasadded in version –208.

In the example table above, the Program Pin State 1 display (Collins ProLine IV Integrated; Fan

mode with +-60o limit) is required for Aircraft Type 91 prior to MK V EGPWC version –208. No

action is required to select this display prior to version –208 (Program Pin 18 was not defined until

version –208). Beginning with version –208 the Program Pin State 2 display (Collins ProLine IV

Integrated; Fan mode with +-90o limit) is also available. In versions –208 and on, Program Pin 18

must be strapped to MP3A (Program Pin Common) to select this display.

Definitions for the entries in the Display Options & Peaks Availability table are provided below:

PPIN State The Program Pin State associated with the display options, etc., and thespecified strapping.

Display Avail-ability

The first version of the MK V EGPWC for which the display is defined.

Display Identifies the make (and model), if applicable, of the display supported bythe aircraft type. Identifies display bus and auto ranging capability.

Sweep style Defines the sweep style the display uses: Standard, Fan, Standard with +/-60o limit, etc.

Auto Pop-up Defines the default behavior of EGPWS visual alerts on selected displayswhen Terrain is not being displayed. See definitions provided in this section.

AlternatePop-up

Defines the alternate behavior of EGPWS visual alerts on selected displayswhen Terrain is not being displayed. See definitions provided in this section.

ObstacleAlerting

Defines whether or not Obstacle Alerting is enabled as part of the AircraftType definition.

Peaks Avail. Defines whether or not Peaks Mode is available for the Aircraft Type.

Allied Signal, Inc.


The Aircraft Type Program Pin Strapping table identifies the Program Pin strapping required to

select the Aircraft Types defined for the aircraft model. The strapping for the selected Aircraft

Type must be recorded in Figure 4-1 Program Pin Strapping.

Some MKV EGPWS Aircraft Types have required or optional analog inputs. The Analog Input

Channel Assignments Worksheet is provided only for those Aircraft Types with defined analog

inputs. In the example table below, the input on Channel 1 is optional and defaults to enabled;

the inputs on Channel 2 and 4 are required; and the input on Channel 3 is optional and enabled

unless digital ILS is provided. Optional inputs must be enabled as defined in the Aircraft

Description table. The last column is provided to document the connections for the installation

and is used to prepare the installation drawings.

Example Analog Input Channel Assignment Worksheet


AnalogInputChannel

Pins69

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ARINC 552 with Validity Discrete)(use Alt. RA Config. #1 to select ALT 55)

OrNot used (use Alternate RA Config. #2 to select)

2+ = TP14A- = TP14B

AOA, Right DPTPotentiometer

Format: DC voltage excitedvia EGPWC 10 Volt reference

Offset: 48.0o

Gain = -6.0o

Electrical Range = 60o

Mechanical Range = 60 o

T P2D(10 VDC)

T P14A (+)

T P14B (-)

3+ = TP13C- = TP13D

Glideslope (ARINC 547 with Validity Flag & ILS Select)Or

Not Used (will use digital ILS if provided)

4+ = TP14C- = TP14D

AOA, Left DPT PotentiometerFormat: DC voltage excited

via EGPWC 10 Volt referenceOffset: 48.0o

Gain = -6.0o



T P2D(10 VDC)

T P14C (+)

T P14D (-)


Alternate Radio Altimeter formats are valid only when the Aircraft Class is Bizjet. The Radio

Altimeter Formats worksheet defines the alternate RA formats defined for the Aircraft Types (use

Program Pin 14 to select an alternate RA format). The actual aircraft configuration will determine

the correct RA format for the installation. The last column in the worksheet is provided to

document the RA configuration. Any restrictions on other RA options created by selecting an

alternate RA format will be noted with the worksheet.

Allied Signal, Inc.


Example Radio Altimeter Formats Worksheet

FormatRadio Altimeter Alternatives

69Selected?

Default ARINC 552

Alternate RA Configuration #1 ALT 55

Alternate RA Configuration #2 ARINC 429

The ARINC 429 Input Channel Assignments Worksheet is provided to define the ARINC 429

inputs. In the abbreviated example table below one of the two inputs identified on Channel 1 as

well as the input on Channel 4 must be provided. The input identified on Channel 5 is optional

and Channel 18 is not used. Optional inputs must be enabled as defined in the Aircraft

Description table. The last column is provided to document the connections for the installation


Example ARINC 429 Input Channel Ass ignments Wo rksheet

ARINC 429 INPUT CHANNEL ASSIGNMENTS FORAIRCRAFT TYPES

ARINC429

InputChannel

Pins187

Connections

1A=MP6AB=MP6B

IRS #1 (High Speed) - PreferredOr

AHRS #1 (High Speed)..

.

...

4A=MP12AB=MP12B ADC #1 (Low Speed) ��

5A=MP10AB-MP10B

Not usedor

GPS #1 (High Speed)..

.

...

18A=MP6CB=MP6D Not used ��

If modifications to the ARINC 429 interfaces are defined, they are listed in the ARINC 429

Interface Modification Options Worksheet. The ARINC 429 interface modifications for the Aircraft

Type are enabled via Program Pin strapping as defined in this worksheet. The “P/N Availability”

column indicates the first MK V EGPWC version that supports the interface modification. The last

column is provided to document the ARINC 429 interface modifications for the installation.

Example ARINC 429 Interface Modification Options Worksheet

Program Pin / Signal P/NAvailability Changes to Interfaces Aircraft Types Connections

Alternate GPSSpeed - GPS #1, #2 Low Speed bus(es)

4, 16, 144, 174,192, 217, 218


-206 and on GPS #1, #2 Use if input is ARINC 743(instead of ARINC 743A)

4, 16, 144, 174,217, 21816


- FMC #1,#2Use if Nav Mode label 266

available4, 16, 144, 174,

217, 218

Allied Signal, Inc.


Discrete Inputs Worksheet are required for normal operation of the MKV EGPWC. The Discrete

Inputs Worksheet identifies the required and optional discretes, their states and their input pins

for the Aircraft Type. The last column is provided to document the connections for the installation


The Serial Outputs Worksheet identifies the Serial Outputs Worksheet for the Aircraft Type. The

Serial Outputs Worksheet include the display data and data sent to the flight data recorder. The

ICD Appendix E label sets for the ARINC 429 serial output data are included for reference.

The final worksheet for the Aircraft Type is the Discrete Outputs Worksheet. This worksheet

identifies the Aircraft Type’s Discrete Outputs Worksheet, their output pins and the lamp behavior

for lamp outputs. The last column is provided to document the connections for the installation


Allied Signal, Inc.


A-1 Airbus

A.1.1 A300/A310


Aircraft Type 108 172

DescriptionA300-600 AA

(Also supports A310-200) A300-600R/ A310

P/N Availability -100 or later -202 or later

REQUIRED SYSTEM INPUTS

ADC Dual Single

EFIS Dual

FMC Dual Single

ILS Single

IRS Dual Single (see GPIRS Overlay)

LRRA Dual Single

OPTIONAL SYSTEM INPUTS


N/A Dual FMC

SingleExternalGPS

Single GPS Single GPSNo GPIRS

DualExternalGPS

Dual GPS Dual GPSNo GPIRSP

PIN

7

SingleGPIRSOverlay

N/A Single GPIRSReplaces Single IRS; No GPS

Dual ILS Dual ILS N/A

PP

IN 9

Dual RA N/A

PP

IN15

PWS Option2

N/ASingle or Dual PWS Hazard Bus inputs

PWS Option 2 must be used for either single ordual PWS inputs.

FEATURES

Aircraft Class Commercial AT


No Yes

Alternate Mode 4B Yes

ARINC 429 DH No

G/S Cancel Altitude 2000’

Lamp Format Type 1

Mode 6 Volume Normal

Alert Volume High

Steep Approach N/A

Terrain RelayMonitor Discretes

No

Windshear No

Allied Signal, Inc.


Display Options & Peaks Availability A300/A310

Aircraft Type 108 (Ref. ICD App G-18.1)

PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping

1-101

and on

Sextant EFIS(Bus type: ARINC 708standard data format)

No auto ranging

Fanmode No Yes No Yes Open

Aircraft Type 172 (Ref. ICD App G-18.2)

1-202

and on

Sextant EFIS(Bus type: Airbus

specific header (label055))

No auto ranging



Program Pin Strapping for Aircraft Type

Program PinsAircraft Type

1 (TP10A) 2 (TP10B) 3 (TP10C)

108 MP7B TP12C MP3A

172 MP7B TP12C MP15D

Analog Input Channel Assignments

There are no Analog Input Channel assignments for these Aircraft Types.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet A300/A310


ARINC429

InputChannel

Pins108

Connections

3A=MP11AB=MP11B

ADC #1 (Low Speed) ��

14A=TP1CB=TP1D


4A=MP12AB=MP12B

EFIS #1 (Low Speed) ��

9A=TP9CB=TP9D EFIS #2 (Low Speed) ��

2A=MP10CB=MP10D FMC #1 (High Speed) ��

15A=TP4AB=TP4B FMC #2 (High Speed) ��

6A=MP11CB=MP11D ILS #1 (Low Speed) � ��

16A=TP5CB=TP5D

Not usedOr

ILS #2 (Low Speed)

1A=MP6AB=MP6B IRS #1 (High Speed) ��

13A=TP5AB=TP6A IRS #2 (High Speed) ��

8A=MP13AB=MP13B LRRA #1 (Low Speed) ��

12A=TP8CB=TP8D LRRA #2 (Low Speed) ��

18A=MP6CB=MP6D

Not usedOr

GPS #1 (ARINC 743A; Low Speed)

17A=TP11CB=TP11D

Not usedOr


5A=MP10AB-MP10B Not used ��


10A=TP9AB=TP9B Not used ��



Program Pin / Signal P/NAvailability Changes to Interfaces Aircraft

Types Connections

16 Alternate GPSSpeed

- GPS #1, #2 High Speed bus(es) 108

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet A300/A310


ARINC429

InputChannel

Pins172

Connections

3A=MP11AB=MP11B


4A=MP12AB=MP12B


9A=TP9CB=TP9D



7A=MP12CB=MP12D

Not usedOr

FMC #2 (Low Speed)

6A=MP11CB=MP11D

ILS #1 (Low Speed) � ��

1A=MP6AB=MP6B

IRS #1 (High Speed)Or

GPIRS #1 (High Speed)

8A=MP13AB=MP13B

LRRA #1 (Low Speed) ��

13A=TP5AB=TP6A

Not usedOr


17A=TP11CB=TP11D

Not usedOr


11A=TP8AB=TP8B

Not usedOr

Wx Radar Hazard Bus #1 (High Speed)

18A=MP6CB=MP6D

Not usedOr


5A=MP10AB-MP10B

Not used ��

10A=TP9AB=TP9B

Not used ��

12A=TP8CB=TP8D Not used ��






Types Connections



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Discrete Inputs Worksheet A300/A310

DISCRETE INPUTS DISCRETE STATES FOR AIRCRAFT TYPES

Name Pin 108Connections

REQUIRED

Self-Test MP9A Momentary Ground = Self Test; Open = Normal

Landing Gear MP9B Ground = Gear Down; Open = Gear Up

Landing Flap MP9C Ground = Landing Flap; Open = Not Landing Flap

Glideslope Cancel MP9D Momentary Ground = Cancel; Open = Normal

Terrain Awareness &TCF Inhibit

MP14B Ground = Inhibit; Open = Normal

WX-Radar On/Off #1 MP14A Ground = On; Open = Off

OPTIONAL

Glideslope Inhibit MP1B Ground = Inhibit; Open = Not Inhibit

Mode 6 Volume Control MP2A Ground = Low Volume; Open = Normal

Decision Height MP5C Ground = <DH; Open = >DH

Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal

Altitude Callouts Enable MP8C Ground = Voice Enabled; Open = Disabled

Momentary AudioSuppress

MP8D Ground = GPWS Audio Suppress; Open = Normal

Display Select #1 TP1A Momentary Ground Switch

Display Select #2 TP1B Momentary Ground Switch

NOT USED

Simulator Reposition MP7A Ground = Reposition; Open = Normal ��

MP1A N/A ��

MP2B N/A ��

MP2D N/A ��

MP5D N/A ��

TP4C N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.


Discrete Inputs Worksheet A300/A310



REQUIRED








OPTIONAL




GPWS Inhibit MP7D Ground = GPWS Inhibit; Open = Normal

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled


MP8D Momentary Ground = Audio Suppress; Open =Normal

WX-Radar On/Off #2 MP2D Ground = On; Open = OffRequired for ‘PWS Opt 2’ and dual RT




NOT USED


MP1A N/A ��

MP2B N/A ��

TP4C N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.


Serial Outputs Worksheet A300/A310


ChannelPins

108 172Connections

TX453-1A=TP3AB=TP3B

Terrain Display data to Symbol Generator Relay #1��

��

TX453-2A=TP3CB=TP3D Terrain Display data to Symbol Generator Relay #2

��

��

TX429-1Low Speed

A=MP1CB=MP1D

TX429-2Low Speed

A=TP2AB=TP2B

ICD Appendix E label sets: E-1/2/5/6/8/11

ICD Appendix E label sets: E-1/2/6/8/11


Connections For Aircraft TypePin Discrete Outputs

FlashingLamp 108 172

MP15D Glideslope Cancel N/A �� !� �� "�� #

MP3D Below G/S Caution No �� !� ��$�� %$��& ��' ��#

MP7BAll

GPWS Cautions and Warnings(except Below G/S Caution)

No �� !� �� %�()�' ��#

TP12C Spare ��

TP12A Spare ��

TP12BAudio On

(required if TCAS equipped) N/A �� *+�� *��## ,�!��- ��

TP4D Terrain Displayable #1 N/A �� +� ��*�"��

TP10D Terrain Display Discrete #1 N/A �� "� ��

MP14C Terrain Display Discrete #2 N/A �� !� �� "� ��

TP11A Terrain Displayable #2 N/A �� !� �� +� ��*�"��

MP7C GPWS Monitor N/A ��$�� ()� .�( ��

TP12D Terrain Not Available N/A �� .�( �� .��

TP11B Terrain Monitor N/A �� $�� .�( ��

Note: The above table applies to default Lamp Format Type 1. Beginning with version –208, Lamp Format Type 2 may

be selected via Program Pin 12. For Lamp Format Type 2, the changes are as follows:

MP3D All GPWS Cautions No �� !� �� ()� ��#

MP7B All GPWS Warnings (“Pull Up”) No �� !� ��+ (*�� /� ��#

Allied Signal, Inc.


A.1.2 A319/A320/A321


Aircraft Type 1 113 132 148

Description A319/A320/A321UA

A319/A320/A321OEM

A319/A320/A321Alternate Lamp

FormatOEM

A319/A320/A321Contained Pop-Up;

Lamp Format 2OEM

P/N Availability -100 or later -100 or later -102 or later -204 or later


ADC

CFDSSingle

Display Bus Dual

EFIS Single

FMC Dual

ILS

IRS

LRRA

Single


SingleExternalGPS

Single GPS

DualExternalGPS

N/A Dual GPS

SingleGPIRS

N/ASingle GPIRS

Replaces Single IRS;No GPS allowed

N/A N/APP

IN 7

OptionalInputSelect

Dual ADC, IRS

Dual ILS Dual ILS

PP

IN 9

Dual RA

N/A

Dual LRRA

PP

IN15

PWSOption 2

Single or Dual PWS Hazard Bus inputsPWS Option 2 must be used for either single or dual PWS inputs.

FEATURES

Aircraft Class Commercial Air Transport


Yes


ARINC 429 DH Yes

G/S Cancel Alt. 2000’

Lamp Format 1 2


Alert Volume High

Steep Approach N/A


No

Windshear No

Allied Signal, Inc.


Display Options A319/A320/A321


PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping

1-100

and on

Sextant EFIS(Bus type: ARINC 708data format with PWS(label 055); Revisedpicture header bits

(CTR mode))No auto ranging

Fanmode

No Yes No Yes Open

Aircraft Type: 113, 132 (Ref. ICD App G-25.1)

1-100

and on

Sextant EFIS(Bus type: Airbus DataFormat for PWS (label

066))No auto ranging



1-204

and on



Fanmode

Yes -Contained No No Yes Open


Program Pin Strapping for Aircraft Type A319/A320/A321


1 (TP10A) 2 (TP10B) 3 (TP10C)

1 MP3A Open Open

113 MP3A TP12A MP3A

132 MP7B Open MP15D

148 MP7B MP15D MP15D


Not applicable to these Aircraft Types.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet A319/A320/A321


ARINC429

InputChannel

Pins1

Connections

3A=MP11AB=MP11B


10A=TP9AB=TP9B

CFDS (Low Speed) ��

5A=MP10AB-MP10B


2A=MP10CB=MP10D FMC EIS (High Speed) ��

7A=MP12CB=MP12D FMC OWN C (Low Speed) �� ). �

17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D




4A=MP12AB=MP12B Nav Display Bus #1 (Low Speed) .�0 ��#�� $*# ��

9A=TP9CB=TP9D Nav Display Bus #2 (Low Speed) .�0 ��#�� $*# ��

11A=TP8AB=TP8B

Not UsedOr


18A=MP6CB=MP6D

Not UsedOr


12A=TP8CB=TP8D

Not Used ��

13A=TP5AB=TP6A Not Used ��

14A=TP1CB=TP1D Not Used ��

15A=TP4AB=TP4B Not Used ��




Types Connections

16Alternate GPSSpeed

- GPS #1, #2 High Speed bus(es)1, 113, 132,

148

Allied Signal, Inc.




ARINC429

InputChannel

Pins113, 132

Connections

3A=MP11AB=MP11B


10A=TP9AB=TP9B


5A=MP10AB-MP10B


2A=MP10CB=MP10D FMC EIS (High Speed) ��

7A=MP12CB=MP12D FMC OWN C (Low Speed) �� ). �

17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D


1A=MP6AB=MP6B

IRS #1 (High Spd)Or

GPIRS #1 (High Speed)��

8A=MP13AB=MP13B


4A=MP12AB=MP12B

Nav Display Bus #1 (Low Speed) .�0 ��#�� $*# ��


11A=TP8AB=TP8B

Not UsedOr


18A=MP6CB=MP6D

Not UsedOr



13A=TP5AB=TP6A

Not Used ��

14A=TP1CB=TP1D

Not Used ��

15A=TP4AB=TP4B

Not Used ��

16A=TP5CB=TP5D

Not Used ��



Types Connections

Alternate GPSSpeed - GPS #1, #2 High Speed bus(es) 113, 132

16ConfigurationOption 2

- FMC OWN C Use if Nav Mode label 270 isnot available

113, 132

Allied Signal, Inc.




ARINC429

InputChannel

Pins148

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D

Not UsedOr

ADC #2 (Low Speed)

10A=TP9AB=TP9B CFDS (Low Speed) ��

5A=MP10AB-MP10B


2A=MP10CB=MP10D

FMC EIS (High Speed) ��

7A=MP12CB=MP12D

FMC OWN C (Low Speed) �� ). �

17A=TP11CB=TP11D

Not UsedOr


16A=TP5CB=TP5D

Not UsedOr



12A=TP8CB=TP8D

Not UsedOr

ILS #2 (Low Speed)


13A=TP5AB=TP6A

Not UsedOr

IRS #2 (High Speed)


15A=TP4AB=TP4B

Not UsedOr

LRRA #2 (Low Speed)



11A=TP8AB=TP8B

Not UsedOr


18A=MP6CB=MP6D

Not UsedOr




Types Connections

Alternate GPSSpeed - GPS #1, #2 High Speed bus(es) 148


- FMC OWN C Use to activate Discrete wordon label 270

148

Allied Signal, Inc.


Discrete Inputs Worksheet A319/A320/A321



REQUIRED

Self-Test MP9A Momentary Ground = Self-Test; Open = Normal




WXR Radar On/Off #1 MP14A Ground = On; Open = Off



OPTIONAL




Audio Inhibit MP7D Ground = Inhibit; Open = Normal



MP8D Momentary Ground = Audio Suppress;Open = Normal

WXR Radar On/Off #2 MP2D Ground = On; Open = OffRequired for dual PWS only



NOT USED


MP1A N/A ��

MP2B N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.




Name Pin 113, 132Connections

REQUIRED





WXR Radar On/Off #1 MP14A Ground = On; Open = Off



OPTIONAL












NOT USED


MP1A N/A ��

MP2B N/A ��

TP4C N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED







OPTIONAL









Audio Inhibit MP5D Ground = Inhibit; Open = Normal



NOT USED


MP1A N/A ��

MP14A N/A ��

MP2B N/A ��

TP4C N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.


Serial Outputs Worksheet A319/A320/A321


ChannelPins

1, 113, 132, 148Connections

TX453-1A=TP3AB=TP3B

Terrain Display data to Symbol Generator Relay #1

TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D

ICD Appendix E label sets: E-1/2/5/6/8/11/14

TX429-2Low Speed

A=TP2AB=TP2B


Discrete Outputs Worksheet A319/A320/A321

Connections For Aircraft TypePin Discrete Outputs

FlashingLamp 1

MP15D Glideslope Cancel N/A �� +� ��

MP3D Below G/S Caution No �� $��& �� #

MP7BAll


No �� + �()� ��#

TP12C Spare No ��

TP12A Spare No ��

TP12B Audio On N/A �� *+�� *��## ,�!��- ��





MP7CGPWS MonitorTerrain Monitor N/A �� ()� .�( ��

TP12D Terrain Not Available N/A �� .��

TP11B Spare N/A ��





Allied Signal, Inc.


Discrete Outputs Worksheet A319/A320/A321

Connections for Aircraft TypePin Discrete Outputs

FlashingLamp 113



MP7BAll


No �� + �()� ��#



TP12B Audio On N/A �� *+�� *��## ,�!��- ��





MP7C GPWS Monitor N/A �� ()� .�( ��


TP11B Terrain Monitor N/A �� .�( ��






FlashingLamp 132, 148


MP3D All GPWS Cautions No �� ()� ��#

MP7B All GPWS Warnings (“Pull Up”) No �� + (*��1/� ��#



TP12B Audio On N/A �� *+�� *��## ,�!��- ��








Allied Signal, Inc.


A.1.3 A330/A340


Aircraft Type 57 136 133

Description A330/A340 OEM A330/A340 Lamp Format 2 A330/A340 DLH/Cathay

P/N Availability -204 or later -206 or later -102 or later


ADC Single

CMC Single N/A

CFDS N/A Single

EFIS Single

FMC Dual

ILS Single

IRS Single (see GPIRS Overlay)

LRRA Single


SingleExternalGPS

Single Low Speed GPSNo GPIRS

PP

IN 7

SingleGPIRSOverlay

Single GPIRSReplaces Single IRS inputs; No GPS N/A

PP

IN16

PWS Option2

Single or Dual PWS Hazard Bus inputsPWS Option 2 must be used for either single or dual PWS inputs.

FEATURES



Yes


ARINC 429 DH Yes


Lamp Format Type 1 Type 2 Type 1


Alert Volume High

Steep Approach N/A


No

Windshear No

Allied Signal, Inc.


Display Options A330/340


PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping

1-204

and on





1-102

and on

Sextant EFIS(Bus type: ARINC 708data format with PWS(label 055); Revisedpicture header bits



Note: Prior to version –208, the display option for Program Pin State 1 is the required display.



1 (TP10A) 2 (TP10B) 3 (TP10C)

57 MP3A TP4D Open

133 TP12C Open MP15D

136 Open MP3A MP15D


There are no Analog Input Channel assignments for these Aircraft Types.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet A330/340


ARINC429

InputChannel

Pins57, 136

Connections

3A=MP11AB=MP11B


10A=TP9AB=TP9B

CMC (Low Speed) ��

5A=MP10AB-MP10B


2A=MP10CB=MP10D FMC #1 (FMC EIS) (High Speed) ��

7A=MP12CB=MP12D FMC #2 (FMC OWN C) (Low Speed) ��

17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D


1A=MP6AB=MP6B



8A=MP13AB=MP13B

LRRA #1 (Low Speed) ��+��

4A=MP12AB=MP12B

Nav Display Bus #1 (Low Speed) .�0 ��#�� $*# ��


11A=TP8AB=TP8B

Not UsedOr


18A=MP6CB=MP6D

Not UsedOr



13A=TP5AB=TP6A

Not Used ��

14A=TP1CB=TP1D

Not Used ��

15A=TP4AB=TP4B

Not Used ��

16A=TP5CB=TP5D

Not Used ��

ARINC 429 Interface Modification Options Worksheet A330/340

Program Pin / Signal P/NAvailability

Changes to Interfaces AircraftTypes

Connections

Alternate GPSSpeed

- GPS #1, #2 High Speed bus(es) 57, 136


- FMC #2 Use if Nav Mode label 270 isNOT available 57, 136

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet A330/340


ARINC429

InputChannel

Pins133

Connections

3A=MP11AB=MP11B


10A=TP9AB=TP9B


5A=MP10AB-MP10B


2A=MP10CB=MP10D FMC #1 (FMC EIS) (High Speed) ��

7A=MP12CB=MP12D FMC #2 (FMC OWN C) (Low Speed) ��

17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D



8A=MP13AB=MP13B LRRA #1 (Low Speed) ��+��



11A=TP8AB=TP8B

Not UsedOr


18A=MP6CB=MP6D

Not UsedOr


12A=TP8CB=TP8D

Not Used ��





ARINC 429 Interface Modification Options Worksheet A330/340


Types Connections

16Alternate GPSSpeed - GPS #1, #2 High Speed bus(es) 133

Allied Signal, Inc.


Discrete Inputs Worksheet A330/340



REQUIRED








OPTIONAL










WX-Radar On/Off #2 MP2D Ground = On; Open = OffRequired for dual PWS only


NOT USED


MP1A N/A ��

MP2B N/A ��

TP4C N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED








OPTIONAL




Audio Inhibit MP7D Ground = GPWS Inhibit; Open = Normal






WX-Radar On/Off #2 MP2D Ground = On; Open = OffRequired for dual PWS only

NOT USED


MP1A N/A ��

MP2B N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.


Serial Outputs Worksheet A330/340


ChannelPins

57, 133, 136Connections

TX453-1A=TP3AB=TP3B


TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B


Discrete Outputs Worksheet A330/340

Connections for Aircraft TypesPin Discrete Outputs

FlashingLamp 57



MP7BAll


No �� + �()� ��#

TP12C Spare ��

TP12A Spare ��

TP12B Audio On N/A �� *+�� *��## ,�!��- ��












Allied Signal, Inc.




FlashingLamp 133



MP7BAll


No �� + �()� ��#

TP12C Spare ��

TP12A Spare ��

TP12B Audio On N/A �� *+�� *��## ,�!��- ��





MP7CGPWS Monitor (A/C 133)

Terrain MonitorN/A �� ()� .�( ��








FlashingLamp 136


MP3D All GPWS Cautions No �� $��& �� #

MP7B All GPWS Warnings (“Pull Up”) No �� + �()� ��#

TP12C Spare ��

TP12A Spare ��

TP12B Audio On N/A �� *+�� *��## ,�!��- ��








Allied Signal, Inc.


A-2 Avro

A-2.1 RJ


Aircraft Type 54 55

Description AVRO Regional Jet with EFIS AVRO Regional Jet



ADCDisplay Bus

Single

EFIS Dual N/AFMCILSIRS

LRRAMCP

Single


SingleExternal GPS

Single GPS

Dual ExternalGPS

Dual GPS

PP

IN 7


Dual ADC, FMC, IRS

Dual ILS Dual ILS

PP

IN 9

Dual LRRA Dual LRRA

FEATURES



No

Alternate Mode 4B No

ARINC 429 DH No


Lamp Format Type 2


Alert Volume High

Steep Approach Yes - Discrete


No

Windshear No

Allied Signal, Inc.


Display Options AVRO RJ

PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping

Aircraft Type: 54 (Ref. ICD App G-23.1, G-5.2, G-2.3)

1-206

and on

RDR 4A/B Bendix(PPI) 2

(Bus type: ARINC 708Data Format)

10 NM auto ranging

Standard Yes No No Yes Open

2-208

and on

Honeywell Primus 708Radar with auto range(Bus type: ARINC 708

Data Format)No auto ranging

Fanmode Yes No No Yes MP3A

3-208

and on

Collins WXI-701/711PPI


10 NM auto ranging

Fanmode Yes No No Yes MP15D


1-204

and on




Note: Prior to version –208, the display option for Program Pin State 1 is the required display. Program Pin 18 wasadded in version –208.1 PPI part number 2041222-0434 (Mod 24) is required for –208 and on for correct blue color display.



1 (TP10A) 2 (TP10B) 3 (TP10C)

54 TP12A TP12A Open

55 TP4D TP12A Open


There are no analog inputs for this Aircraft Type.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet AVRO RJ


InputChannel

Pins54

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D

Not UsedOr

ADC #2 (Low Speed)

5A=MP10AB-MP10B

Display Bus (Low Speed)(WX-IND 429 out (range) Bus #1) ��

7A=MP12CB=MP12D


9A=TP9CB=TP9D


2A=MP10CB=MP10D

FMC #1 (High Speed) ��

15A=TP4AB=TP4B

Not UsedOr

FMC #2 (High Speed)

6A=MP11CB=MP11D

ILS #1 (Low Speed) ��

12A=TP8CB=TP8D

Not UsedOr

ILS #2 (Low Speed)


13A=TP5AB=TP6A

Not UsedOr

IRS #2 (High Speed)


11A=TP8AB=TP8B

Not UsedOr

LRRA #2 (Low Speed)

4A=MP12AB=MP12B MCP (Low Speed) ��

17A=TP11CB=TP11D

Not UsedOr

GPS 2 (High Speed – ARINC 743A)

18A=MP6CB=MP6D

Not UsedOr


10A=TP9AB=TP9B

Not Used ��

16A=TP5CB=TP5D

Not Used ��



Types Connections

Alternate GPSSpeed - GPS #1, #2 Low Speed bus(es) 54


- FMS/GPSEnables direct FMS position

inputs if GPS options selectedbut GPS data is not usable

5416

ConfigurationOption 2 - FMC #1, #2

Use if Nav Mode label 266 isavailable 54

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet AVRO RJ


InputChannel

Pins55

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D

Not UsedOr

ADC #2 (Low Speed)

5A=MP10AB-MP10B

Display Bus (Low Speed)(WX-IND 429 out (range) Bus #1) ��

2A=MP10CB=MP10D


15A=TP4AB=TP4B

Not UsedOr

FMC #2 (High Speed)

17A=TP11CB=TP11D

Not UsedOr


18A=MP6CB=MP6D

Not UsedOr


6A=MP11CB=MP11D ILS #1 (Low Speed) ��

12A=TP8CB=TP8D

Not UsedOr

ILS #2 (Low Speed)

1A=MP6AB=MP6B

IRS #1 (High Speed) ��

13A=TP5AB=TP6A

Not UsedOr

IRS #2 (High Speed)

8A=MP13AB=MP13B


11A=TP8AB=TP8B

Not UsedOr

LRRA #2 (Low Speed)

4A=MP12AB=MP12B MCP (Low Speed) ��

7A=MP12CB=MP12D

Not Used ��

9A=TP9CB=TP9D

Not Used ��

10A=TP9AB=TP9B

Not Used ��

16A=TP5CB=TP5D

Not Used ��



Types Connections



- FMS/GPSEnables direct FMS position

inputs if GPS options selectedbut GPS data is not usable

5516



Allied Signal, Inc.


Discrete Inputs Worksheet AVRO RJ



REQUIRED


Landing Gear MP9B Ground = Gear Down; Open = Not Landing Gear

Landing Flap MP9C Ground = Landing Flap;Open = Not Landing Flap

Glideslope Cancel MP9D Momentary Ground = Cancel; Open = Normal From glareshield “Push GSInhibit”


MP2D Ground = Inhibit; Open = Normal

OPTIONAL

Glideslope Inhibit MP1B Ground = Glideslope Inhibit; Open = Not Inhibit �� !� "��#� ��







Display Select 1 TP1A Momentary Ground Switch

Steep Approach #1 MP1A Ground = Enabled; Open = Disabled

Steep Approach #2 MP14B Ground = Selected; Open = Not Selected

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Normal

NOT USED

Simulator Reposition MP7A Ground = Reposition; Open = Normal Open

MP14A N/A Open

TP1B N/A Open

TP4C N/A Open

MP5D N/A Open

TP15A N/A Open

TP15B N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet AVRO RJ


ChannelPins

54, 55Connections

TX453-1A=TP3AB=TP3B

Picture Bus Output port (to relay driving single PPI)

TX453-2A=TP3CB=TP3D

Not Used ��

TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B


Allied Signal, Inc.


Discrete Outputs Worksheet AVRO RJ

Connections For Aircraft TypesPin Discrete Outputs Flashing

Lamp 54

MP15D Glideslope Cancel N/A ��$�%�� !� "�� &�

MP3D All GPWS Cautions No ��$�%�� !� �&'�( "�)� ��&�

MP7B All GPWS Warnings (“Pull Up”) No ��$�%�� !� �� &�



TP12B Audio On N/A *�� !�'��

TP4D Spare N/A ��

TP10D Terrain Display Discrete #1 N/A *� #��(� �+��#!�� (�� , -).�%*�((��/

MP14C Spare N/A ��

TP11A WXR Control Discrete N/A *� #��(� (�� '�� ).�

MP7C GPWS Monitor N/A "�)� ��* ��&

TP12D Terrain Monitor N/A *�((�� &

TP11B Terrain Not Available N/A *�((�� %� ��&


Lamp 55

MP15D Glideslope Cancel N/A ��$�%�� !� "�� &�

MP3D All GPWS Cautions No ��$�%�� !� �&'�( "�)� ��&�

MP7B All GPWS Warnings (“Pull Up”) No ��$�%�� !� �� &�



TP12B Audio On N/A *�� !�'��


TP10D Terrain Display Discrete #1 N/A *� #��(� �+��#!�� (�� , -).�%*�((��/


TP11A Spare N/A ��

MP7C GPWS Monitor N/A "�)� ��* ��&

TP12D Terrain Monitor N/A *�((�� &

TP11B Terrain Not Available N/A *�((�� %� ��&

Allied Signal, Inc.


A-3 Beechjet

A-3.1 Beechjet 400A


Aircraft Type 162

Description Beechjet Model 400A

P/N Availability -208 or later


ADC

AHRSDual

CDU Single

IOC

ILSDual

External GPS Single

Analog RA Single

VanePotentiometers

Single (left)


Dual ExternalGPS

Dual GPS

PP

IN 7

OptionalInputs Select

Left Vane Potentiometer Teledyne SLZ-7275-1Replaces Left Vane Potentiometer Rosemont 861EB

Alternate RAFormat

Single digital RA (use Alternate RA Configuration to select)Replaces Single analog LRRA

Digital DH Single Digital Decision Height from CDU-3 bus

FEATURES

Aircraft Class Bizjet


No


ARINC 429 DH Yes - optional


Lamp Format Type 2


Alert Volume High



No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Beechjet 400A

Aircraft Type: 162 (Ref. ICD App G-3.6, G-16.1)

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping

1-206

and on

Collins ProLine IVNon-integrated, 7x6


No auto ranging

Default with+/- 60o limit No Yes No No Open

2-208

and on


(Bus type: ARINCCompatible Format –

Collins ProLine IV(label 077))

Auto rangingcontrolled by display

Fan modewith +/- 60o

limitControlled by display No No MP3A




1 (TP10A) 2 (TP10B) 3 (TP10C)

162 MP15D MP7B MP15D

Allied Signal, Inc.




AnalogInputChannel

Pins162

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ALT 55 with Validity Discrete)Or

Not Used (use Alternate RA Configuration to select digital RA)

2+ = TP14A- = TP14B

Left Vane Potentiometer

CCWC

CW

=IN

CR

EA

SIN

G A

OAT P2D

(10 VDC)

T P14A (+)

T P14B (-)

Vane: Rosemont 861EBFormat: DC voltage excited by 10

VDC reference from EGPWCRange: 0 – 10 VDC

Offset: 50o

Gain = -10.0o


Mechanical Range = 100o

OrVane: Teledyne SLZ-7275-1

Format: DC voltage excited by 10VDC reference from EGPWC

Range: 0 – 10 VDCOffset: 53.889o

Gain = -7.7778o

Electrical Range = 77.77778o


(use Optional Inputs Select forTeledyne vane)

3+ = TP13C- = TP13D Not Used ��

4+ = TP14C- = TP14D

Not Used ��


Radio Altimeter Alternatives Format Selected?

Default ALT 55



Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Beechjet 400A


InputChannel

Pins162

Connections

4A=MP12AB=MP12B

ADC #1 ARINC 429 (Low Speed) ��

12A=TP8CB=TP8D


1A=MP6AB=MP6B

AHRS #1 (High Speed) (AHC-1-2) ��

13A=TP5AB=TP6A AHRS #2 (High Speed) ��

14A=TP1CB=TP1D

Not UsedOr

CDU Bus (Low Speed) (CDU-3)

17A=TP11CB=TP11D

Not UsedOr

GPS 2 (Low Speed – ARINC 743A)

18A=MP6CB=MP6D GPS 1 (Low Speed – ARINC 743A) ��

5A=MP10AB-MP10B


6A=MP11CB=MP11D

ILS #1 (Low Speed) ILS #1

2A=MP10CB=MP10D

IOC Bus #1 (High Speed) (LA-IOC-1) ��

3A=MP11AB=MP11B

IOC Bus #2 (High Speed) (RA-IOC-1) ��

10A=TP9AB=TP9B

Not UsedOr

LRRA #1 (Low Speed)(use Alt. RA Conf. to select analog RA)

7A=MP12CB=MP12D Not Used ��

8A=MP13AB=MP13B Not Used ��

9A=TP9CB=TP9D

Not Used ��

11A=TP8AB=TP8B

Not Used ��

15A=TP4AB=TP4B

Not Used ��

16A=TP5CB=TP5D

Not Used ��

Allied Signal, Inc.


ARINC 429 Interface Modification Options Worksheet Beechjet 400A


Types Connections

Alternate GPSSpeed -206 and on GPS #1, #2 High Speed bus(es) 162


-206 and on GPS #1, #2Use if input is ARINC 743 and not

ARINC 743A 162

PP

IN 1

6

ConfigurationOption 2 -206 and on IOC 1, 2

Use to activate labels 147, 302,310-313 on IOC buses. 162

Allied Signal, Inc.


Discrete Inputs Worksheet Beechjet 400A



REQUIRED

Self-Test MP9A Momentary Ground = Self Test; Open = Normal�� !� �"

��#� #�$� ��!$%

Landing Gear TP15D +28V = Gear Down; 0V = Gear Up ��$ �!��

Landing Flap MP9CGround = Landing Flap;

Open = Not Landing Flap

&�� &�� !�� " ��

��!� �!�'�� #� &�� ( �

��

Glideslope Cancel MP9D Momentary Ground = Cancel; Open = Normal�)� �� !�

�*+�$ ��#� ��$� ��!$%


MP14B Ground = Inhibit; Open = Normal �� !� ��$$�� +��

(Alternate) RadioAltitude Valid

TP15A +28V = Valid; 0V = Not Valid �"�! �� (��"��

Flap Position #2 (10 o) TP7B +28V = Selected; 0V = Not Selected &�� , o ��

Flap Position #3 (20 o) TP7C +28V = Selected; 0V = Not Selected &�� , o ��

Flap Position #4 (30 o) TP7D +28V = Selected; 0V = Not Selected &�� -, o ��

OPTIONAL

Glideslope Inhibit MP1B Ground = Inhibit; Open = Not Inhibit&��.�� "��

/��'�!�$�� "��!�%

Mode 6 Volume Control MP2A Ground = Low Volume; Open = Normal ��$�$�� $!��"

Decision Height MP5C Ground = <DH; Open = >DH �" �� "��$�� !��

Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal�� $��. !$ �$�"��0� #)�

��"�! ��+�� !��

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled ��$�$�� $!��"



�!�'�� #� ��"�! ��$��

��


Display Select #1 TP1A Momentary Ground Switch �!�'�� $$��

Display Select #2 TP1B Momentary Ground Switch �!�'�� $$��

Steep Approach #1 TP4C Ground = Enabled; Open = Disabled ��$�$�� $!��"

Steep Approach #2 MP5D Ground = Selected; Open = Not Selected�!�'�� !� ��

��$!��

NOT USED


MP1A N/A Open

MP9B N/A Open

MP14A N/A Open

MP2D N/A Open

TP15B N/A Open

TP15C N/A Open

TP7A N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet Beechjet 400A


ChannelPins

162Connections

TX453-1A=TP3AB=TP3B

Left picture bus to Left MFD relay(Display #1 (PPIN 18 State 1))

OrLeft picture bus to Left MFD (Display #1 (PPIN 18 State 2))

�� $ �!��*�

TX453-2A=TP3CB=TP3D

Right picture bus to Right MFD relay (Display #1 (PPIN 18State 1))

OrRight picture bus to Right MFD (Display #1 (PPIN 18 State

2))

�� $ �!��*�

TX429-1Low Speed

A=MP1CB=MP1D ICD Appendix E label sets: E-1/2/3/5/6/12/17

TX429-2Low Speed

A=TP2AB=TP2B ICD Appendix E label sets: E-1/2/3/5/6/12/17



Lamp 162

MP15D Glideslope Cancel N/A �*+�$ �)� ��" ��*�

MP3D All GPWS Cautions No ��) �.�� *+�$ ��#� ��*��

MP7B All GPWS Warnings (“Pull Up”) No ��) �.�� " �� *��

TP12C Windshear Caution No ��) �.�� *+�$ #)� ��!� ��*��

TP12A Windshear Warning No ��) �.�� " #)� #�$��. ��*��

TP12B Audio On N/A �� +��

TP4D Spare No ��

TP10D Terrain Display Discrete #1 N/A �� $$��

MP14C Terrain Display Discrete #2 N/A �.�� $$��


MP7C GPWS Monitor N/A �*+�$ ��#� �1�� *�

TP12D Windshear Monitor N/A �*+�$ #��"��$ �1�� *�

TP11B Terrain Not Available N/A �*+�$ ��$$�� 1�� *�

Allied Signal, Inc.


A-4 Boeing

A-4.1 737-300


Aircraft Type 4 144 192 217 218 174 16

Description Basic

ContainedPop-up &

LampFormat 2

OEM UALUAL

(LampFormat 2)

No WxROn Label

BendixPPI-4BDisplay

P/N Availability -102 orlater

-204 orlater

-202 orlater

-104 orlater

-104 orlater

-204 orlater

-202 orlater


ADC

DAASingle

Display Bus N/A Single

DSWC Dual

EFCP Dual Single

FCC-MCP

FMC

IRS

Analog RA

Analog G/S

Single


SingleExternal

GPS

Single GPSNo Optional Input Select, No Dual External GPS

DualExternal

GPS

Dual GPSNo Dual ILS, No Optional Input Select, No Single External GPS

PP

IN 7

OptionalInputSelect

Dual IRS, ADC and FMSNo Single or Dual External GPS

Dual ILSDual DAA and Dual G/S (Analog) with Validity

No Dual External GPS

PP

IN 9

Dual RA Dual Analog RA with Validity

PP

IN15

PWSOption 1 Single PWS Hazard Bus

FEATURES



No


ARINC 429 DH Yes

G/S Cancel Alt. 2000’ 1000’ 2000’

Lamp Format Type 1 Type 2 Type 1 Type 2 Type 1


Alert Volume Low

Steep Approach N/A

Terrain Relay M No Yes No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability 737-300

PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-102

and on

Collins EFIS(Non-Integrated)


No auto ranging

Default No Yes No Yes Open


1-202

and on

RDR 4A/B Bendix(PPI)1


10 NM auto ranging


204 and on Aircraft Type: 144 (Ref. ICD App G-15.5)

1-204

and on



No auto ranging

DefaultYes -

Contained No No Yes Open


1-204

and on



No auto ranging

Default

Yes(No WxROn label

req’d)

No No Yes Open


1-202

and on



No auto ranging

DefaultYes -



1-104

and on



No auto ranging

DefaultYes -

Contained No Yes Yes Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

4 MP7B Open Open

16 Open MP15D Open

144 Open MP15D MP15D

174 TP12A TP12C MP15D

192 Open Open MP3D

217 MP3A MP3D MP3D

218 MP15D MP3D MP3D

Allied Signal, Inc.




AnalogInputChannel

Pins4, 144, 174, 192, 217, 218, 16

Connections

1+ = TP13A- = TP13B Radio Altimeter #1 (ARINC 552 with Validity Discrete)

2+ = TP14A- = TP14B

Not UsedOr

Radio Altimeter #2 (ARINC 552 with Validity Discrete)

3+ = TP13C- = TP13D Glideslope #1 (ARINC 547 with Validity Discrete)

4+ = TP14C- = TP14D

Not UsedOr

Glideslope #1 (ARINC 547 with Validity Discrete)


Alternate RA formats do not apply to these Aircraft Types.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Worksheet 737-300


ARINC429

InputChannel

Pins4, 144, 174, 217, 218

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D

Not usedor

ADC #2 (Low Speed)

6A=MP11CB=MP11D DAA #1 (Low Speed) ��

7A=MP12CB=MP12D

DSWC #1 (Low Speed) ��

9A=TP9CB=TP9D


5A=MP10AB-MP10B


16A=TP5CB=TP5D

EFIS #2 ��

4A=MP12AB=MP12B FCC-MCP #1 (Low Speed) ��


18A=MP6CB=MP6D

Not usedor

GPS #1 (High Speed; ARINC 743A)or

FMC #2 (High Speed)

17A=TP11CB=TP11D

Not usedor


DAA #2 (Low Speed)


13A=TP5AB=TP6A

Not usedor

IRS #2 (High Speed)

12A=TP8CB=TP8D

Not usedor

Wx Radar Hazard Bus (High Speed)

8A=MP13AB=MP13B Not used ��






Alternate GPSSpeed

- GPS #1, #2 Low Speed bus(es)4, 144, 174,

217, 218



4, 144, 174,217, 21816

ConfigurationOption 2 - FMC #1,#2

Use if Nav Mode label 266available

4, 144, 174,217, 218

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet 737-300


ARINC429

InputChannel

Pins16

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D

Not usedor

ADC #2 (Low Speed)


8A=MP13AB=MP13B

Display Bus (Low Speed) ��

7A=MP12CB=MP12D


9A=TP9CB=TP9D


5A=MP10AB-MP10B




17A=TP11CB=TP11D

Not usedor


DAA #2 (Low Speed)

18A=MP6CB=MP6D

Not usedor


FMC #2 (High Speed)


13A=TP5AB=TP6A

Not usedor

IRS #2 (High Speed)

12A=TP8CB=TP8D

Not usedor








Alternate GPSSpeed

- GPS #1, #2 Low Speed bus(es) 16


-206 and on GPS #1, #2 Use if input is ARINC 743(instead of ARINC 743A) 1616


Use if Nav Mode label 266available 16

Allied Signal, Inc.




ARINC429

InputChannel

Pins192

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D

Not usedor

ADC #2 (Low Speed)


7A=MP12CB=MP12D


9A=TP9CB=TP9D


5A=MP10AB-MP10B


10A=TP9AB=TP9B




18A=MP6CB=MP6D

Not usedor


FMC #2 (High Speed)

17A=TP11CB=TP11D

Not usedor


DAA #2 (Low Speed)


13A=TP5AB=TP6A

Not usedor

IRS #2 (High Speed)

12A=TP8CB=TP8D

Not usedor








16Alternate GPSSpeed


Allied Signal, Inc.


Discrete Inputs Worksheet 737-300


Name Pin 4, 144, 174Connections

REQUIRED

Air Ground Discrete MP1A Ground = In Air; Open = On Ground



Landing Flap MP9C Ground = Not Landing Flap; Open = Landing Flap




Radio Altimeter #1 Valid TP15A +28 V = Valid; 0 V = Fail

Glideslope #1 Valid TP15B +28 V = Valid; 0 V = Fail

OPTIONAL








GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Not Inhibit



Radio Altimeter #2 Valid TP15C +28 V = Valid; 0 V = Fail

Glideslope #2 Valid TP15D +28 V = Valid; 0 V = Fail

NOT USED


MP14A N/A ��

MP2D N/A ��

TP4C N/A ��

MP5D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED










OPTIONAL












NOT USED


MP14A N/A ��

MP2D N/A ��

TP1B N/A ��

TP4C N/A ��

MP5D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED








WXR Display Select #1 MP14A Ground = Pressed; Open = Released

WXR Display Select #2 MP2D Ground = Pressed; Open = Released



Terrain Relay Monitor #1 TP7C +28 V = Relay On; 0 V = Relay Off

Terrain Relay Monitor #2 TP7D +28 V = Relay On; 0 V = Relay Off

OPTIONAL













NOT USED


TP4C N/A ��

MP5D N/A ��

TP7A N/A ��

TP7B N/A ��

Allied Signal, Inc.





REQUIRED












OPTIONAL













NOT USED


TP4C N/A ��

MP5D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.


Serial Outputs Worksheet 737-300


ChannelPins

4, 144, 174, 192, 217, 218, 16Connections

TX453-1A=TP3AB=TP3B

Terrain Display data to left display switching relay

TX453-2A=TP3CB=TP3D

Terrain Display data to right display switching relay

TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B



Pin Discrete Outputs FlashingLamp

Connections For Aircraft Types

4, 174

MP15D Glideslope Cancel N/A �� !� "�� #�� $��

MP3D Below G/S Caution No �� $%�& ��'( "�� $��

MP7BAll


No �� !� ��) "�� $��

TP12C Windshear Caution No

TP12A Windshear Warning No

TP12B Audio On N/A *�� )�' ��&�� +��!�%��, ��

TP4D Terrain Displayable #1 N/A

TP10D Terrain Display Discrete #1 N/A

MP14C Terrain Display Discrete #2 N/A

TP11A Terrain Displayable #2 N/A

MP7CGPWS Monitor

Windshear Monitor N/A �$%�& "�� -�� $�

TP12D Terrain Not Available N/A *�&&�� -�� $�

TP11B Reserved N/A ��



MP3D All GPWS Cautions No �� !� �$%�& "�� $��

MP7B All GPWS Warnings (“Pull Up”) No �� !� ��) �� .� ��$��

Allied Signal, Inc.


Discrete Outputs Worksheet 737-300


FlashingLamp 16


MP3D Below G/S Caution No �� !� �$%�& ��'( "�� $��

MP7BAll


No �� !� ��) "�� $��



TP12B PWS Inhibit N/A

TP4D TCAS Inhibit N/A




MP7CGPWS Monitor

Windshear MonitorN/A

TP12D Terrain Not Available N/A

TP11B Callout Monitor N/A ��






FlashingLamp 144


MP3D All GPWS Cautions No �� $%�& "�� $��









MP7CGPWS Monitor

Windshear MonitorN/A �$%�& "�� -�� $�



Allied Signal, Inc.




FlashingLamp 192


MP3D Below G/S Caution No �� !� �$%�& ��'( "�� $��

MP7BAll


No �� !� ��) "�� $��




TP4D Displayable #1 N/A



TP11A Displayable #2 N/A

MP7CGPWS Monitor



TP11B Callout Monitor N/A





Allied Signal, Inc.




FlashingLamp 217



MP7BAll


No �� !� ��) "�� $��



TP12B Audio On N/A *�� )�' ��&�� +��!�%��, ��





MP7CGPWS Monitor









FlashingLamp 218






TP12B Audio On N/A *�� )�' ��&�� +��!�%��, ��





MP7CGPWS Monitor




Allied Signal, Inc.


A-4.2 737-400


Aircraft Type 8 145 193 225 226 101

737-400 Basic

ContainedPop-up &

LampFormat 2

OEM UALUAL

LampFormat 2

AK

P/N Availability -102 or later -204 or later -202 or later -204 or later -204 or later -100 or later

REQUIRED SYSTEMS AND/OR INPUTS

ADC Single Dual

DAA Single

DSWC

EFCPDual

FCC Single

FMC Single None

GPS None Dual

IRS Single Dual

Analog RA

Analog G/SSingle

OPTIONAL SYSTEMS AND/OR INPUTS

SingleExternalGPS

Single GPSNo Optional Input Select N/A

DualExternalGPS

Dual GPSNo Dual ILS, No Optional Input Select N/A

PP

IN 7


Dual IRS, ADC and FMCNo GPS Dual FMC


No Dual GPS

PP

IN 9


PP

IN15

PWS Option1

Single PWS Hazard Bus

FEATURES BASIC TO AIRCRAFT TYPE



No


ARINC 429 DH Yes

G/S Cancel Alt. 2000’ 1000’ 2000’

Lamp Format Type 1 Type 2 Type 1 Type 2 Type 1


Alert Volume Low

Steep Approach N/A


No Yes No

Windshear Yes - Boeing Algorithm

Allied Signal, Inc.



PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-102

and on



No auto ranging



1-100

and on



No auto ranging

Default No YesYes

(Alwaysenabled)

Yes(Alwaysenabled)

Open


1-204

and on



No auto ranging

DefaultYes -


Aircraft Type: 193 (Ref. ICD App G-15.6

1-202

and on



No auto ranging

DefaultYes -



1-204

and on



No auto ranging

DefaultYes -





1 (TP10A) 2 (TP10B) 3 (TP10C)

8 Open MP3A Open

101 TP12C D03 MP3A

145 MP3A MP15D MP15D

193 MP3A Open MP3D

225 MP3A MP7B MP3D

226 MP15D MP7B MP3D

Allied Signal, Inc.


Analog Input Channel Assignments 737-400


AnalogInputChannel

Pins8, 101, 145, 193, 225, 226

Connections


2+ = TP14A- = TP14B

Not UsedOr


3+ = TP13C- = TP13D Glideslope #1 (ARINC 547 with Validity Discrete & ILS Select)

4+ = TP14C- = TP14D

Not UsedOr

Glideslope #1 (ARINC 547 with Validity Discrete & ILS Select)


The Radio Altimeter data format is ARINC 552. Alternate RA formats do not apply to these

Aircraft Types. (Alternate RA formats are available only for Aircraft Types where Aircraft Class is

“Bizjet”).

Allied Signal, Inc.




ARINC429

InputChannel

Pins8, 145, 225, 226

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D

Not usedor

ADC #2 (Low Speed)


7A=MP12CB=MP12D


9A=TP9CB=TP9D


5A=MP10AB-MP10B


16A=TP5CB=TP5D




17A=TP11CB=TP11D

Not usedor


DAA #2 (Low Speed)

18A=MP6CB=MP6D

Not usedor


FMC #2 (High Speed)


13A=TP5AB=TP6A

Not usedOr

IRS #2 (High Speed)

12A=TP8CB=TP8D

Not UsedOr






Allied Signal, Inc.


ARINC 429 Interface Modification Options Worksheet 737-400


Types Connections

Alternate GPSSpeed - GPS #1, #2 Low Speed bus(es)

8, 145, 225,226

ConfigurationOption 1 -206 and on GPS #1, #2

Use if input is ARINC 743(instead of ARINC 743A)

8, 145, 225,22616

ConfigurationOption 2 - FMC #1,#2 Use Nav Mode label 266

8, 145, 225,226

Allied Signal, Inc.




ARINC429

InputChannel

Pins101

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D ADC #2 (Low Speed)


12A=TP8CB=TP8D

Not UsedOr

DAA #2 (Low Speed)

7A=MP12CB=MP12D DSWC #1 (Low Speed) ��

9A=TP9CB=TP9D DSWC #2 (Low Speed) ��

5A=MP10AB-MP10B EFIS #1 (Low Speed) ��



2A=MP10CB=MP10D

Not UsedOr

FMC #1 (High Speed)

15A=TP4AB=TP4B

Not UsedOr

FMC #2 (High Speed)

8A=MP13AB=MP13B

GPS #1(High Speed; ARINC 743A)

17A=TP11CB=TP11D

GPS #2(High Speed; ARINC 743A)



11A=TP8AB=TP8B

Not UsedOr






Types Connections


16ConfigurationOption 1 -206 and on GPS #1, #2

Use if input is ARINC 743(instead of ARINC 743A) 101

Allied Signal, Inc.




ARINC429

InputChannel

Pins193

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D

Not usedor

ADC #2 (Low Speed)


7A=MP12CB=MP12D


9A=TP9CB=TP9D


5A=MP10AB-MP10B


10A=TP9AB=TP9B




17A=TP11CB=TP11D

Not usedor


DAA #2 (Low Speed)

18A=MP6CB=MP6D

Not usedor


FMC #2 (High Speed)


13A=TP5AB=TP6A

Not usedOr

IRS #2 (High Speed)

12A=TP8CB=TP8D

Not UsedOr








Types Connections

Alternate GPSSpeed



-206 and on GPS #1, #2Use if input is ARINC 743(instead of ARINC 743A) 193

Allied Signal, Inc.





REQUIRED









OPTIONAL














NOT USED


MP14A N/A ��

MP2D N/A ��

TP4C N/A ��

MP5D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED









OPTIONAL












NOT USED


MP1B N/A ��

MP14A N/A ��

MP2D N/A ��

MP2B N/A ��

TP4C N/A ��

MP5D N/A ��

TP7A N/A ��

TP7A N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED













OPTIONAL














NOT USED


TP4C N/A ��

MP5D N/A ��

TP7A N/A ��

TP7B N/A ��

Allied Signal, Inc.





REQUIRED











OPTIONAL














NOT USED


TP4C N/A ��

MP5D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.




ChannelPins

8, 101, 145, 193, 225, 226Connections

TX453-1A=TP3AB=TP3B


TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B




FlashingLamp 8



MP7BAll


No �� !� ��) "�� $��

TP12C Windshear Caution N/A

TP12A Windshear Warning No ��$%'� "��&��'&�

TP12B Audio On N/A





MP7CGPWS Monitor








Allied Signal, Inc.




FlashingLamp 101



MP7BAll


No �� !� ��) "�� $��








MP7CGPWS Monitor









FlashingLamp 145



MP7B All GPWS Warnings (“Pull Up”) No �� ) �� .� ��$��








MP7CGPWS Monitor




Allied Signal, Inc.




FlashingLamp 193



MP7BAll


No �� !� ��) "�� $��








MP7CGPWS Monitor








Allied Signal, Inc.




FlashingLamp 225



MP7BAll


No �� !� ��) "�� $��



TP12B Audio On N/A





MP7CGPWS Monitor









FlashingLamp 226






TP12B Audio On N/A





MP7CGPWS Monitor




Allied Signal, Inc.


A-4.3 737-500


Aircraft Type 9 194 219 220 17

737-500 Basic OEM UAL UAL – LampFormat 2

Bendix PPI-4BDisplay

P/N Availability -102 or later -202 or later -104 or later -104 or later -202 or later


ADC

DAASingle

Display Bus N/A Single

DSWC Dual

EFCP Dual Single

FMC

IRS

Analog RA(ARINC 552)

Analog G/S

Single


SingleExternalGPS

Single GPSNo Optional Input Select, No Dual GPS

DualExternalGPS

Dual GPSNo Dual ILS, No Optional Input Select, No Single GPS

PP

IN 7

OptionalInputSelect

Dual IRS, ADC and FMSNo GPS


No Dual GPS

PP

IN 9


PP

IN15

PWSOption 1





No


ARINC 429 DH Yes

G/S Cancel Alt. 2000’ 1000’ 2000’

Lamp Format Type 1 Type 2 Type 1


Alert Volume Low

Steep Approach N/A


No Yes No


Allied Signal, Inc.



PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-102

and on



No auto ranging



1-202

and on



10 NM auto ranging



1-202

and on



No auto ranging

DefaultYes -



1-104

and on



No auto ranging

DefaultYes -





1 (TP10A) 2 (TP10B) 3 (TP10C)

9 MP3A MP3A Open

17 MP3A MP15D Open

194 MP15D Open MP3D

219 MP3D MP3D MP3D

220 MP7B MP3D MP3D

Allied Signal, Inc.


Analog Input Channel Assignments 737-500


AnalogInputChannel

Pins9, 194, 219, 220, 17

Connections


2+ = TP14A- = TP14B

Not UsedOr


3+ = TP13C- = TP13D Glideslope #1 (ARINC 547 with Validity Discrete & ILS Select)

4+ = TP14C- = TP14D

Not UsedOr

Glideslope #1 (ARINC 547 with Validity Discrete & ILS Select)


The Radio Altimeter data format is ARINC 552. Alternate RA formats do not apply to Commercial

Air Transport Aircraft Types.

Allied Signal, Inc.




ARINC429

InputChannel

Pins9, 219, 220

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D

Not usedOr

ADC #2 (Low Speed)


7A=MP12CB=MP12D


9A=TP9CB=TP9D


5A=MP10AB-MP10B

EFIS #1 (Low Speed)Provides Decision Height ��

16A=TP5CB=TP5D




17A=TP11CB=TP11D

Not usedOr

GPS #2 (High Speed; ARINC 743A)Or

DAA #2 (Low Speed)

18A=MP6CB=MP6D

Not usedOr


FMC #2 (High Speed)


13A=TP5AB=TP6A

Not usedOr

IRS #2 (High Speed)

12A=TP8CB=TP8D

Not usedOr








Types Connections

Alternate GPSSpeed

- GPS #1, #2 Low Speed bus(es) 9, 219, 220


-206 and on GPS #1, #2 Use if input is ARINC 743(instead of ARINC 743A) 9, 219, 22016


- FMC #1,#2Use Nav Mode label 266

(deactivates FMC MagneticTrack)

9, 219, 220

Allied Signal, Inc.




ARINC429

InputChannel

Pins17

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D

Not usedOr

ADC #2 (Low Speed)


8A=MP13AB=MP13B

Display Bus (Low Speed) ��

7A=MP12CB=MP12D


9A=TP9CB=TP9D


5A=MP10AB-MP10B




17A=TP11CB=TP11D

Not usedOr


DAA #2 (Low Speed)

18A=MP6CB=MP6D

Not usedOr


FMC #2 (High Speed)


13A=TP5AB=TP6A

Not usedOr

IRS #2 (High Speed)

12A=TP8CB=TP8D

Not usedOr








Types Connections

Alternate GPSSpeed





- FMC #1,#2Use Nav Mode label 266

(deactivates FMC MagneticTrack)

17

Allied Signal, Inc.




ARINC429

InputChannel

Pins194

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D

Not usedOr

ADC #2 (Low Speed)


7A=MP12CB=MP12D


9A=TP9CB=TP9D


5A=MP10AB-MP10B


10A=TP9AB=TP9B




17A=TP11CB=TP11D

Not usedOr


DAA #2 (Low Speed)

18A=MP6CB=MP6D

Not usedOr


FMC #2 (High Speed)


13A=TP5AB=TP6A

Not usedOr

IRS #2 (High Speed)

12A=TP8CB=TP8D

Not usedOr








Types Connections

Alternate GPSSpeed




Allied Signal, Inc.





REQUIRED









OPTIONAL














NOT USED


MP14A N/A ��

MP2D N/A ��

TP4C N/A ��

MP5D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED








OPTIONAL














NOT USED


MP14A N/A ��

MP2D N/A ��

TP1B N/A ��

TP4C N/A ��

MP5D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED













OPTIONAL














NOT USED


TP4C N/A ��

MP5D N/A ��

TP7A N/A ��

TP7B N/A ��

Allied Signal, Inc.





REQUIRED











OPTIONAL














NOT USED


TP4C N/A ��

MP5D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.




ChannelPins

9, 194, 219, 220, 17Connections

TX453-1A=TP3AB=TP3B


TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B




FlashingLamp 9

MP15D Glideslope Cancel N/A


MP7BAll


No �� ) "�� $��



TP12B Audio On N/A *�� !�%��





MP7CGPWS Monitor








Allied Signal, Inc.




FlashingLamp 17



MP7BAll


No �� ) "�� $��








MP7CGPWS Monitor

Windshear Monitor N/A







Allied Signal, Inc.




FlashingLamp 194



MP7BAll


No �� ) "�� $��








MP7CGPWS Monitor








Allied Signal, Inc.




FlashingLamp 219



MP7BAll


No �� ) "�� $��








MP7CGPWS Monitor









FlashingLamp 220











MP7CGPWS Monitor




Allied Signal, Inc.


A-4.4 737-600, 737-700 and 737-800



Integrated 737 737-600 737-700 737-800



ADC Single

DSWC

EFCPDual

FCC-MCP

FMC

ILS

IRS

Single


OptionalInputSelect

Dual IRS, ADC and FMSNo GPS

SingleExternalGPS

Single GPSNo Optional Input Select

PP

IN 7

DualExternalGPS

Dual GPSNo Dual ILS, No Optional Input Select

Dual ILSDual ILS

No Dual GPS

PP

IN 9

Dual RA Dual LRRA

PWSOption 1


PP

IN15 PWS

Option 2Dual PWS Hazard Bus




No


ARINC 429 DH Yes


Lamp Format Type 1


Alert Volume Low

Obstacle Alerting No

Steep Approach N/A


Yes


Allied Signal, Inc.


Display Options & Peaks Availability 737-600, 737-700 and 737-800

Aircraft Type: 195, 196, 197 (Ref. ICD App G-14.2)

PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping

1-202

and on

Honeywell LCD(Bus type: ARINC 708Standard Data Format)

No auto ranging

DefaultNo – Controlled within

displays No No Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

195 MP3D Open MP3D

196 MP7B Open MP3D

197 TP12C Open MP3D


There are no Analog Inputs for these Aircraft Types.


The Radio Altimeter data format is ARINC 429. Alternate RA formats do not apply to Commercial

Air Transport Aircraft Types.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Worksheet 737-600, 737-700 and 737-800


ARINC429

InputChannel

Pins195, 196, 197

Connections

3A=MP11AB=MP11B


7A=MP12CB=MP12D

DSWC #1 (Low Speed)(SMYD bus 1) ��

9A=TP9CB=TP9D

DSWC #2 (Low Speed)(SMYD bus 2) ��

5A=MP10AB-MP10B

EFIS #1 (Low Speed)(DEU #1 – Left EFIS CP pass through bus) ��

10A=TP9AB=TP9B

EFIS #2 (Low Speed)(SMYD bus 2) ��



17A=TP11CB=TP11D

Not usedor

GPS #2 (High Speed)or

ILS #2 (Low Speed)

18A=MP6CB=MP6D

Not usedor

GPS #1 (High Speed)or

FMC #2 (High Speed)


1A=MP6AB=MP6B


13A=TP5AB=TP6A

Not usedor

IRS #2 (High Speed)

8A=MP13AB=MP13B

LRRA #1 (Low Speed)(Left) ��

11A=TP8AB=TP8B

Not usedOr

LRRA #2 (Low Speed – Right)

12A=TP8CB=TP8D

Not usedor


14A=TP1CB=TP1D

Not usedor

ADC #2 (Low Speed)

15A=TP4AB=TP4B

Not usedOr





Types Connections

16Alternate GPSSpeed - GPS #1, #2 Low Speed bus(es) 195, 196, 197

Allied Signal, Inc.


Discrete Inputs Worksheet 737-600, 737-700 and 737-800


Name Pin 195, 196, 197Connections

REQUIRED










OPTIONAL








NOT USED


MP5C N/A ��

MP14A N/A ��

MP2D N/A ��

TP1A N/A ��

TP1B N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

Allied Signal, Inc.


Serial Outputs Worksheet 737-600, 737-700 and 737-800


ChannelPins


TX453-1A=TP3AB=TP3B


TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D

ICD Appendix E label sets: E-1C/2/4/5/6/7/10

TX429-2Low Speed

A=TP2AB=TP2B




FlashingLamp 195, 196, 197


MP3D Below G/S Caution No �� $%�& ��'( "�� $�

MP7BAll


No �� ) "�� $�







TP11A Spare N/A

MP7C GPWS Monitor N/A

TP12D Windshear Monitor N/A






Allied Signal, Inc.


A-4.5 747-400


Aircraft Type 2 30 198 100 111

747-400 BA Basic Integrated Simulator JAL Simulator

P/N Availability -100 or later -102 or later -202 or later -100 or later -101 or later

REQUIRED SYSTEMS AND/OR INPUTS

ADC Single DualCMC SingleDisplay Bus N/A Dual N/ADSWC DualEFCP Single Dual Single DualFMCILS

Single

IRS Single DualLRRA SingleWXR Hazard Bus Dual None

OPTIONAL SYSTEMS AND/OR INPUTS


N/A Dual IRS, ADC and FMCNo GPS N/A N/A

SingleExternalGPS

Single GPS Single GPSNo Optional Input Select Single GPS Single GPS

PP

IN 7

DualExternalGPS

N/ADual GPS

No Dual ILS, No Optional InputSelect

N/A Dual GPS

Dual ILS Dual ILS Dual ILSNo GPS inputs

N/A

Dual RA Dual LRRA N/A Dual LRRA

PP

IN 9

Triple RA Triple LRRA N/A Triple LRRAPWS Option1

N/A Single PWS Hazard Bus N/A

PP

IN15 PWS Option

2N/A Dual PWS Hazard Bus N/A




No


ARINC 429 DH Yes

G/S Cancel Alt. 2000’ 1000’ 2000’

Lamp Format Type 2

Mode 6 Volume Low

Alert Volume High

Steep Approach N/A


No Yes No

Windshear Yes

Allied Signal, Inc.



PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-100

and on



No auto ranging

Standard No No No Yes Open


1-100

and on



No auto ranging



1-101

and on



No auto ranging

DefaultYes if WX

is on No No Yes Open


1-202

and on



No auto ranging

DefaultNo – controlled within

displays No No Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

2 MP15D Open Open

30 TP12A MP3D Open

100 MP7B MP7B MP15D

111 TP4D TP12C MP3A(MP3A)

198 TP12A Open MP3D


The are no analog inputs for these Aircraft Types.



Aircraft Types.

Allied Signal, Inc.



ARINC 429 INPUT CHANNEL ASSIGNMENTS FOR AIRCRAFTTYPES

ARINC429

InputChannel

Pins2

Connections

3A=MP11AB=MP11B


10A=TP9AB=TP9B


7A=MP12CB=MP12D





18A=MP6CB=MP6D

Not usedor

GPS #1 (Low Speed; ARINC 743A)


12A=TP8CB=TP8D

Not UsedOr

ILS #2 (Low Spd)

1A=MP6AB=MP6B


8A=MP13AB=MP13B LRRA #1 (Left) (Low Speed) ��

11A=TP8AB=TP8B

Not UsedOr

LRRA #2 (Right) (Low Speed)

4A=MP12AB=MP12B

Not UsedOr

LRRA #3 (Center) (Low Speed)

13A=TP5AB=TP6A

Wx Radar Hazard Bus 1 (Low Spd)(WxR Ctlr CB1)

14A=TP1CB=TP1D

Wx Radar Hazard Bus 2 (Low Spd)(WxR Ctlr CB2)

15A=TP4AB=TP4B

Not used ��

16A=TP5CB=TP5D

Not used ��

17A=TP11CB=TP11D

Not Used ��



Types Connections



Allied Signal, Inc.




ARINC429

InputChannel

Pins30, 198

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D

Not UsedOr

ADC #2 (Low Speed)

10A=TP9AB=TP9B CMC (Low Speed) ��

7A=MP12CB=MP12D


9A=TP9CB=TP9D


5A=MP10AB-MP10B


16A=TP5CB=TP5D



18A=MP6CB=MP6D

Not usedOr GPS #1 (High Speed; ARINC 743A)

Or FMC #2 (High Speed)

17A=TP11CB=TP11D

Not usedOr GPS#2 (Hi Speed)Or ILS#2 (Low Speed)

6A=MP11CB=MP11D


1A=MP6AB=MP6B


13A=TP5AB=TP6A

Not UsedOr

IRS #2 (High Speed)

8A=MP13AB=MP13B

LRRA #1 (Left) (Low Speed) ��

11A=TP8AB=TP8B

Not UsedOr


4A=MP12AB=MP12B

Not UsedOr


12A=TP8CB=TP8D

Not UsedOr

Wx Radar Hazard Bus 1 (High Spd)

15A=TP4AB=TP4B

Not UsedOr

Wx Radar Hazard Bus 2 (High Speed)



Types Connections

Alternate GPSSpeed

- GPS #1, #2 Low Speed bus(es) 30, 198




Use if Nav Mode label 266available 30

Allied Signal, Inc.




ARINC429

InputChannel

Pins100

Connections

3A=MP11AB=MP11B


10A=TP9AB=TP9B


11A=TP8AB=TP8B

Display Bus 1 (Low Spd)(EFCP-L-1 or WXR Controller) ��

12A=TP8CB=TP8D

Display Bus 2 (Low Spd)(EFCP-R-1) ��





18A=MP6CB=MP6D

Not usedor

GPS (High Speed; ARINC 743A)






14A=TP1CB=TP1D

Not Used ��

15A=TP4AB=TP4B

Not Used ��

16A=TP5CB=TP5D

Not Used ��

17A=TP11CB=TP11D

Not Used ��



Types Connections



Allied Signal, Inc.




ARINC429

InputChannel

Pins111

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D


10A=TP9AB=TP9B







18A=MP6CB=MP6D

Not usedor

GPS #1 (High Speed; ARINC 743A)

17A=TP11CB=TP11D

Not usedOr

GPS #2 (High Speed)





11A=TP8AB=TP8B

Not UsedOr


4A=MP12AB=MP12B

Not UsedOr


12A=TP8CB=TP8D

Not Used ��

15A=TP4AB=TP4B

Not Used ��



Types Connections



Allied Signal, Inc.





REQUIRED



Landing Gear/GearOverride

MP9B Ground = Landing Gear Down;Open = Not Landing Gear

Landing Flap/FlapOverride

MP9C Ground = Landing Flap; Open = Not Landing Flap




OPTIONAL









NOT USED

Simulator Reposition MP7A N/A ��

MP5C N/A ��

MP14A N/A ��

MP2D N/A ��

MP2B N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED








OPTIONAL











WxR #2 On/Off 1 MP5D Ground = On; Open = OffReq’d for dual PWS only; indicates R/T #2 selected

NOT USED


MP14A N/A ��

MP2D N/A ��

TP4C N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

1Only required for Dual PWS installations

Allied Signal, Inc.





REQUIRED










OPTIONAL










WxR #1 On/Off 1 TP4C Ground = On; Open = OffReq’d for single/dual PWS

WxR #2 On/Off 1 MP5D Ground = On; Open = OffReq’d for dual PWS only

NOT USED


MP5C N/A ��

MP14A N/A ��

MP2D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

1Only required for Dual PWS installations

Allied Signal, Inc.





REQUIRED










OPTIONAL








NOT USED


MP5C N/A ��

MP14A N/A ��

MP2D N/A ��

TP1A N/A ��

TP1B N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

Allied Signal, Inc.




ChannelPins

2, 30, 100, 111Connections

TX453-1A=TP3AB=TP3B


TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B



ChannelPins

198Connections

TX453-1A=TP3AB=TP3B Terrain Display data to left display switching relay

TX453-2A=TP3CB=TP3D Terrain Display data to right display switching relay

TX429-1Low Speed

A=MP1CB=MP1D ICD Appendix E label sets: E-1C/2/4/5/6/7/10/16

TX429-2Low Speed

A=TP2AB=TP2B ICD Appendix E label sets: E-1C/2/4/5/6/7/10



Lamp 2

MP15D Spare N/A ��

MP3D Spare No ��

MP7B Spare No ��

TP12C Spare N/A ��



TP4D

Terrain Awareness CautionObstacle Awareness CautionTerrain Awareness Warning

Obstacle Awareness Warning

N/A







Allied Signal, Inc.




Lamp 30

MP15D Terrain Displayable #2 N/A




TP12A Windshear Warning N/A





TP11A Glideslope Cancel N/A

MP7CGPWS Monitor





Lamp 100






TP12B Audio On N/A





MP7CGPWS Monitor




Allied Signal, Inc.




Lamp 111




TP12C Spare N/A

TP12A Spare N/A






MP7CGPWS Monitor





Lamp 198














Allied Signal, Inc.


A-4.6 757-200


Aircraft Type 6 146 199 224 116 105 169

Description BasicContained

Pop-up Integrated UALSaudiRoyal AA

= AC 105Except NoWxR OnLabel On

EFIS

P/N Availability -102 orlater

-204 orlater

-202 orlater

-104 orlater

-101 orlater

-100 orlater

-204 orlater


ADC Single Dual

DSWC

EFCPDual

FMC Single Single (#2) Dual

GPS FMC N/A Single N/A

ILS Single

IRS Single Dual

LRRA Single


SingleExternal

GPS

Single GPSNo Optional Input Select or Dual External GPS

N/A Single GPS

DualExternal

GPS

Dual GPSNo Dual ILS, Optional Input Select, Single External

GPSN/A Dual GPS

PP

IN 7


Dual IRS, ADC and FMSNo Single or Dual External GPS N/A

Dual ILSDual ILS

No Dual External GPS Dual ILS

Dual RA Dual LRRA

PP

IN 9

Triple RA Triple LRRA

PWS Option1


PP

IN15 PWS Option

2Dual PWS Hazard Buses N/A

FEATURES



No


ARINC 429 DH Yes

G/S Cancel Alt. 2000’ 1000’ 2000’

Lamp Format Type 2


Alert Volume High

Steep Approach N/A


No Yes No

Windshear Yes

Allied Signal, Inc.



PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-101

and on

Collins EFIS (Non-Integrated)


No auto ranging



1-101

and on



No auto ranging

Default Yes No No Yes Open


1-204

and on



No auto ranging

DefaultYes -



1-202

and on

Collins EFIS(Integrated)


No auto ranging


displays No No Open


1-104

and on



No auto ranging

DefaultYes -





1 (TP10A) 2 (TP10B) 3 (TP10C)

6 TP12A Open Open

105 MP3A TP12C MP3A

116 MP7B TP12A MP3A

146 MP15D MP15D MP15D

169 MP3A TP12C MP15D

199 TP4D Open MP3D

224 Open MP7B MP3D


There are no analog inputs for these Aircraft Types.



Allied Signal, Inc.




ARINC429

InputChannel

Pins6, 146, 199, 224

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D

Not usedor

ADC #2 (Low Spd)


9A=TP9CB=TP9D


5A=MP10AB-MP10B


16A=TP5CB=TP5D


2A=MP10CB=MP10D


18A=MP6CB=MP6D


Or FMC #2 (High Speed)

17A=TP11CB=TP11D


Or ILS #2 (Low Speed)


1A=MP6AB=MP6B


13A=TP5AB=TP6A

Not usedor

IRS #2 (High Spd)


11A=TP8AB=TP8B

Not UsedOr


4A=MP12AB=MP12B

Not UsedOr

LRRA #3 (Center) ( Low Speed)

12A=TP8CB=TP8D

Not usedor

WxR Hazard Bus #1 (High Speed)

15A=TP4AB=TP4B

Not UsedOr





Changes to Interfaces Applies toA/C Types

Connections

Alternate GPSSpeed

- GPS #1, #2 Low Speed bus(es) 6, 146, 199,224


206 and on GPS #1, #2 Use if input is ARINC 743(instead of ARINC 743A) 6, 146, 22416


- FMC #1,#2 Use if Nav Mode label 266 isavailable 6, 146, 224

Allied Signal, Inc.




ARINC429

InputChannel

Pins105, 169

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D


7A=MP12CB=MP12D







18A=MP6CB=MP6D

Not usedor


17A=TP11CB=TP11D

Not usedor



12A=TP8CB=TP8D

Not usedor

ILS #2 (Low Speed)

1A=MP6AB=MP6B


13A=TP5AB=TP6A

IRS #2 (High Speed)


11A=TP8AB=TP8B

Not UsedOr


4A=MP12AB=MP12B

Not UsedOr


10A=TP9AB=TP9B

Not usedOr



Program Pin / Signal P/NAvailability Changes to Interfaces Applies to

A/C TypesConnections

Alternate GPSSpeed



206 and on GPS #1, #2 Use if input is ARINC 743(instead of ARINC 743A)

105, 16916


- FMC #1,#2 Use if Nav Mode label 266 isavailable

105, 169

Allied Signal, Inc.




ARINC429

InputChannel

Pins116

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D


7A=MP12CB=MP12D





2A=MP10CB=MP10D FMC (High Speed) ��

18A=MP6CB=MP6D GPS FMC (High Speed; ARINC 743A) GPS FMC


12A=TP8CB=TP8D

Not usedor

ILS #2 (Low Speed)




11A=TP8AB=TP8B

Not UsedOr


4A=MP12AB=MP12B

Not UsedOr


10A=TP9AB=TP9B

Not usedOr


15A=TP4AB=TP4B

Not UsedOr





Changes to Interfaces Applies toA/C Types

Connections

Alternate GPSSpeed

- GPS FMC Low Speed bus(es) 11616


- GPS FMC& FMC #2


Allied Signal, Inc.





REQUIRED








OPTIONAL











WxR #2 On/Off MP5D Ground = On; Open = OffRequired for dual PWS only

NOT USED


MP14A N/A ��

MP2D N/A ��

TP4C N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED





Landing Flap/FlapsOverride

MP9C Ground = Landing Flap;Open = Not Landing Flap




OPTIONAL











NOT USED

Simulator Reposition MP7A Ground = Reposition; Open = Normal

MP14A N/A ��

MP2D N/A ��

MP5D N/A ��

TP4C N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED










OPTIONAL












NOT USED

Simulator Reposition MP7A Ground = Reposition; Open = Normal

MP14A N/A ��

MP2D N/A ��

TP4C N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED








OPTIONAL











NOT USED


MP14A N/A ��

MP2D N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED










OPTIONAL









NOT USED


MP14A N/A ��

MP2D N/A ��

TP1A N/A ��

TP1B N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

Allied Signal, Inc.





REQUIRED







WXR Display Select #1 MP14AGround = switch pressed; Open = switch released

Momentary ground switch to select/deselect weatheron left side.

WXR Display Select #2 MP2DGround = switch pressed; Open = switch released

Momentary ground switch to select/deselect weatheron right side.


OPTIONAL











WxR #2 On/Off MP7A Ground = On; Open = OffRequired for dual PWS only

NOT USED

Simulator Reposition TP15D +28V = Reposition; Open = Normal ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.




ChannelPins

6, 105, 146, 169, 224Connections

TX453-1A=TP3AB=TP3B


TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B



ChannelPins

116Connections

TX453-1A=TP3AB=TP3B Left side picture to symbol generator port

TX453-2A=TP3CB=TP3D

Right side picture to symbol generator port

TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B



ChannelPins

199Connections



TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B


Allied Signal, Inc.




Lamp 6, 224











MP7CGPWS Monitor





Lamp 105, 169











MP7CGPWS Monitor




Allied Signal, Inc.




Lamp 116











MP7CGPWS Monitor





Lamp 146











MP7CGPWS Monitor




Allied Signal, Inc.




Lamp 199














Allied Signal, Inc.


A-4.7 757-300

Aircraft Type

Aircraft Type 200

Description Integrated



ADC Single

DSWC

EFCPDual

FMC

ILS

IRS

LRRA

Single


SingleExternal

GPS


DualExternal

GPS

Dual GPSNo Dual ILS, Optional Input Select, Single External GPSP

PIN

7



Dual ILSDual ILS

No Dual External GPS

Dual RA Dual LRRA

PP

IN 9


PWS Option1


PP

IN15 PWS Option

2Dual PWS Hazard Buses

FEATURES



No


ARINC 429 DH Yes


Lamp Format Type 2


Alert Volume High

Steep Approach N/A


Yes

Windshear Yes

Allied Signal, Inc.



PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-202

and on



No auto ranging


displays No No Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

200 Open MP3A MP3D




The Radio Altimeter data format is ARINC 429. Alternate RA formats do not apply to this Aircraft

Type.

Allied Signal, Inc.




ARINC429

InputChannel

Pins200

Connections

3A=MP11AB=MP11B


7A=MP12CB=MP12D


9A=TP9CB=TP9D




17A=TP11CB=TP11D

Not usedor

GPS #2 (High Spd)or

ILS #2 (Low Spd)


1A=MP6AB=MP6B IRS #1 (High Speed) IRS #1

13A=TP5AB=TP6A

Not usedor

IRS #2 (High Speed)

8A=MP13AB=MP13B LRRA #1 (Left – Low Speed) ��

11A=TP8AB=TP8B

Not UsedOr

LRRA #2 (Right – Low Speed)

4A=MP12AB=MP12B

Not UsedOr

LRRA #3 (Center – Low Speed)

12A=TP8CB=TP8D

Not usedor


14A=TP1CB=TP1D

Not usedor

ADC #2 (Low Speed)

15A=TP4AB=TP4B

Not UsedOr



18A=MP6CB=MP6D

Not usedor

GPS #1 (High Spd)or

FMC #2 (High Spd)




Changes to Interfaces Applies toAircraft Types

Connections



Allied Signal, Inc.





REQUIRED










OPTIONAL









NOT USED


MP14A N/A ��

MP2D N/A ��

TP1A N/A ��

TP1B N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

Allied Signal, Inc.




ChannelPins

200Connections



TX429-1Low Speed

A=MP1CB=MP1D ICD Appendix E label sets: E-1C/2/4/5/6/7/10

TX429-2Low Speed

A=TP2AB=TP2B ICD Appendix E label sets: E-1C/2/4/5/6/7/10


Connections For Aircraft TypesPin Discrete Outputs Worksheet Flashing

Lamp 200














Allied Signal, Inc.


A-4.8 767-200


Aircraft Type 31 201 221 106 170

Description Basic Integrated UAL AA

= AC 106Except No WxR

On Label OnEFIS

P/N Availability -102 or later -202 or later 104 or later 100 or later 204 or later


ADC Single Dual

DSWC

EFCPDual

FMC Single Dual

ILS Single

IRS Single Dual

LRRA Single


SingleExternal

GPS

Single GPSNo Optional Input Select or Dual External GPS Single GPS

DualExternal

GPS

Dual GPSNo Dual ILS, Optional Input Select, Single External GPS Dual GPS

PP

IN 7



N/A

Dual ILSDual ILS

No Dual External GPSDual ILS

Dual RA Dual LRRA

PP

IN 9


PWS Option1


PP

IN15 PWS Option


FEATURES



No


ARINC 429 DH Yes

G/S Cancel Alt. 2000’ 1000’ 2000’

Lamp Format Type 2


Alert Volume High

Steep Approach N/A


No Yes No

Windshear Yes

Allied Signal, Inc.



PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-102

and on



No auto ranging



1-100

and on



No auto ranging



1-202

and on



No auto ranging


displays No No Open


1-104

and on



No auto ranging

DefaultYes -





1 (TP10A) 2 (TP10B) 3 (TP10C)

31 TP4D MP3D Open

106 MP15D TP12C MP3A

170 MP15D TP12C MP15D

201 MP3A MP3A MP3D

221 TP12C MP3D MP3D





Aircraft Types.

Allied Signal, Inc.




ARINC429

InputChannel

Pins31, 201, 221

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D

Not usedor

ADC #2 (Low Speed)


9A=TP9CB=TP9D


5A=MP10AB-MP10B


16A=TP5CB=TP5D


2A=MP10CB=MP10D


18A=MP6CB=MP6D

Not usedor


FMC #2 (High Speed)

17A=TP11CB=TP11D

Not usedor


ILS #2 (Low Spd)



13A=TP5AB=TP6A

Not usedor

IRS #2 (High Speed)


11A=TP8AB=TP8B

Not UsedOr


4A=MP12AB=MP12B

Not UsedOr


12A=TP8CB=TP8D

Not usedor

WxR Haz. Bus #1 (High Spd)

15A=TP4AB=TP4B

Not UsedOr






Connections

Alternate GPSSpeed

- GPS #1, #2 Low Speed bus(es) 31, 201, 221


-206 and on GPS #1, #2 Use if input is ARINC 743(instead of ARINC 743A) 31, 22116

ConfigurationOption 2 - FMC #1,#2 Use Nav Mode label 266 31, 221

Allied Signal, Inc.




ARINC429

InputChannel

Pins106, 170

Connections



7A=MP12CB=MP12D


9A=TP9CB=TP9D





15A=TP4AB=TP4B FMC #2 (High Speed)


12A=TP8CB=TP8D

Not usedor

ILS #2 (Low Speed)


13A=TP5AB=TP6A IRS #2 (High Speed)

8A=MP13AB=MP13B

LRRA #1 (Left – Low Speed) ��

11A=TP8AB=TP8B

Not UsedOr


4A=MP12AB=MP12B

Not UsedOr


17A=TP11CB=TP11D

Not usedor

GPS #2 (High Speed; ARING 743A)

18A=MP6CB=MP6D

Not usedor


10A=TP9AB=TP9B

Not usedOr

WxR Haz. Bus #1 (High Speed)



Types Connections

Alternate GPSSpeed - GPS #1, #2 Low Speed bus(es) 106, 170



106, 17016

ConfigurationOption 2 - FMC #1,#2 Use Nav Mode label 266 106, 170

Allied Signal, Inc.





REQUIRED








OPTIONAL












NOT USED


MP14A N/A ��

MP2D N/A ��

TP4C N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED










OPTIONAL











NOT USED


MP14A N/A ��

MP2D N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED










OPTIONAL









NOT USED


MP14A N/A ��

MP2D N/A ��

TP1A N/A ��

TP1B N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

Allied Signal, Inc.





REQUIRED








WXR Display Select #1 MP14AGround = Pushed; Open = Released

Momentary ground switch to select/deselect weatheron left side

WXR Display Select #2 MP2DGround = Pushed; Open = Released

Momentary ground switch to select/deselect weatheron right side

OPTIONAL









Display Select #1 TP1AMomentary Ground Switch

Momentary ground switch to select/deselect terrainon left side

Display Select #2 TP1BMomentary Ground Switch

Momentary ground switch to select/deselect terrainon right side


NOT USED

Simulator Reposition TP15D Ground = Reposition; Open = Normal ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.




ChannelPins

31, 106, 170, 221Connections

TX453-1A=TP3AB=TP3B


TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B



ChannelPins

201Connections


TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B


Allied Signal, Inc.




Lamp 31











MP7CGPWS Monitor





Lamp 106, 170











MP7CGPWS Monitor




Allied Signal, Inc.




Lamp 201















Lamp 221











MP7CGPWS Monitor




Allied Signal, Inc.


A-4.9 767-300



Description Basic Integrated UALNo WxR On Label On

EFIS



ADC Single Dual

DSWC

EFCPDual

FMC Single Dual

ILS Single

IRS Single Dual

LRRA Single


SingleExternal

GPS


Single GPS

DualExternal

GPS


PP

IN 7



Dual ILSDual ILS


Dual RA Dual LRRA

PP

IN 9


PWS Option1


PP

IN15 PWS Option


FEATURES



No


ARINC 429 DH Yes

G/S Cancel Alt. 2000’ 1000’ 2000’

Lamp Format Type 2


Alert Volume High

Steep Approach N/A


No Yes No

Windshear Yes

Allied Signal, Inc.



PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-102

and on



No auto ranging



1-204

and on



No auto ranging



1-202

and on



No auto ranging


displays No No Open


1-104

and on



No auto ranging

DefaultYes -





1 (TP10A) 2 (TP10B) 3 (TP10C)

5 TP12C Open Open

171 MP3D TP12C MP15D

202 MP15D MP3A MP3D

223 TP4D MP3D MP3D





Aircraft Types.

Allied Signal, Inc.




ARINC429

InputChannel

Pins5, 202, 223

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D

Not usedor

ADC #2 (Low Speed)


9A=TP9CB=TP9D


5A=MP10AB-MP10B


16A=TP5CB=TP5D


2A=MP10CB=MP10D




13A=TP5AB=TP6A

Not usedor

IRS #2 (High Speed)


11A=TP8AB=TP8B

Not UsedOr


4A=MP12AB=MP12B

Not UsedOr


12A=TP8CB=TP8D

Not usedor

WxR Haz. Bus #1 (High Speed)

15A=TP4AB=TP4B

Not UsedOr


17A=TP11CB=TP11D

Not usedor


ILS #2 (Low Speed)

18A=MP6CB=MP6D

Not usedor


FMC #2 (High Speed)





Connections

Alternate GPSSpeed

- GPS #1, #2 Low Speed bus(es)5, 202,

223


-206 and on GPS #1, #2 Use if input is ARINC 743(instead of ARINC 743A) 5, 22316


Use if Nav Mode label 266 isavailable 5, 223

Allied Signal, Inc.




ARINC429

InputChannel

Pins171

Connections

3A=MP11AB=MP11B







2A=MP10CB=MP10D


15A=TP4AB=TP4B

FMC #2 (High Speed)

18A=MP6CB=MP6D

Not usedor


17A=TP11CB=TP11D

Not usedor



12A=TP8CB=TP8D

Not usedor

ILS #2 (Low Speed)


13A=TP5AB=TP6A IRS #2 (High Speed)


11A=TP8AB=TP8B

Not UsedOr


4A=MP12AB=MP12B

Not UsedOr


10A=TP9AB=TP9B

Not usedOr




Types Connections




17116



Allied Signal, Inc.





REQUIRED








OPTIONAL












NOT USED


MP14A N/A ��

MP2D N/A ��

TP4C N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED










OPTIONAL











NOT USED

Simulator Reposition MP7A Gnd = Reposition; Open = Normal ��

MP14A N/A ��

MP2D N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED










OPTIONAL









NOT USED


MP14A N/A ��

MP2D N/A ��

TP1A N/A ��

TP1B N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

Allied Signal, Inc.





REQUIRED








WXR Display Select #1 MP14AGround = Pressed; Open = Released


WXR Display Select #2 MP2DGround = Pressed; Open = Released

Momentary ground switch to select/deselect weatheron right side

OPTIONAL












NOT USED


TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.




ChannelPins


TX453-1A=TP3AB=TP3B


TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B



ChannelPins

202Connections


TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B


Allied Signal, Inc.




Lamp 5






TP12B Audio On N/A





MP7CGPWS Monitor





Lamp 171






TP12B Audio On N/A





MP7CGPWS Monitor




Allied Signal, Inc.




Lamp 202















Lamp 223






TP12B Audio On N/A





MP7CGPWS Monitor




Allied Signal, Inc.


A-4.10 767-300ER


Aircraft Type 3 147 203 222 109 173

Description BasicContained

Pop-up Integrated UAL AA

AC 109Except NoWxR OnLabel On

EFIS

P/N Availability -102 or later -204 or later -202 or later -104 or later -100 or later -204 or later


ADC Single Dual

DSWC

EFCPDual

FMC Single Dual

GPS FMC N/A N/A

ILS Single

IRS Single Dual

LRRA Single


SingleExternal GPS


Single GPS

Dual ExternalGPS


PP

IN 7



Dual ILSDual ILS


Dual RA Dual LRRA

PP

IN 9


PWS Option1


PP

IN 1

5

PWS Option2 Dual PWS Hazard Buses N/A

FEATURES



No


ARINC 429 DH Yes

G/S Cancel Alt. 2000’ 1000’ 2000’

Lamp Format Type 2


Alert Volume High

Steep Approach N/A


No Yes No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability 767-300ER

PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-102

and on



No auto ranging



1-100

and on



No auto ranging



1-204

and on



DefaultYes -



1-202

and on



No auto ranging


displays No No Open


1-104

and on



No auto ranging

DefaultYes -





1 (TP10A) 2 (TP10B) 3 (TP10C)

3 MP3D Open Open

109 TP12C TP12C MP3A

147 MP3D MP15D MP15D

173 TP12C TP12C MP15D

203 MP3D MP3A MP3D

222 TP12A MP3D MP3D





Aircraft Types.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Worksheet 767-300ER


ARINC429

InputChannel

Pins3, 147, 203, 222

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D

Not usedor

ADC #2 (Low Speed)


9A=TP9CB=TP9D


2A=MP10CB=MP10D


5A=MP10AB-MP10B


16A=TP5CB=TP5D


18A=MP6CB=MP6D

Not usedor


FMC #2 (High Speed)

17A=TP11CB=TP11D

Not usedor


ILS #2 (Low Speed)



13A=TP5AB=TP6A

Not usedor

IRS #2 (High Speed)


11A=TP8AB=TP8B

Not UsedOr


4A=MP12AB=MP12B

Not UsedOr


12A=TP8CB=TP8D

Not usedor


15A=TP4AB=TP4B

Not UsedOr



ARINC 429 Interface Modification Options Worksheet 767-300ER



Connections

Alternate GPSSpeed

- GPS #1, #2 Low Speed bus(es)3, 147, 203,

2223, 147, 203,


-206 and on GPS #1, #2 Use if input is ARINC 743(instead of ARINC 743A) 3, 147, 22216


Use if Nav Mode label 266is available 3, 147, 222

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet 767-300ER


ARINC429

InputChannel

Pins109, 173

Connections

3A=MP11AB=MP11B


14A=TP1CB=TP1D


7A=MP12CB=MP12D







18A=MP6CB=MP6D

Not usedor


17A=TP11CB=TP11D

Not usedor



12A=TP8CB=TP8D

Not usedor

ILS #2 (Low Speed)

1A=MP6AB=MP6B


13A=TP5AB=TP6A



11A=TP8AB=TP8B

Not UsedOr


4A=MP12AB=MP12B

Not UsedOr


10A=TP9AB=TP9B

Not usedOr


ARINC 429 Interface Modification Options Worksheet 767-300ER



Alternate GPSSpeed - GPS #1, #2 Low Speed bus(es) 109, 173



109, 17316


- FMC #1,#2Use if Nav Mode label 266

is available 109, 173

Allied Signal, Inc.


Discrete Inputs Worksheet 767-300ER



REQUIRED








OPTIONAL












NOT USED


MP14A N/A ��

MP2D N/A ��

TP4C N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED










OPTIONAL











NOT USED

Simulator Reposition MP7A Gnd = Reposition; Open = Normal ��

MP14A N/A ��

MP2D N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED








OPTIONAL











NOT USED


MP14A N/A ��

MP2D N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED










OPTIONAL









NOT USED


MP14A N/A ��

MP2D N/A ��

TP1A N/A ��

TP1B N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

Allied Signal, Inc.





REQUIRED








WXR Display Select #1 MP14AGround = Pressed; Open = Released


WXR Display Select #2 MP2DGround = Pressed; Open = Released

Momentary ground switch to select/deselectweather on right side

OPTIONAL







MP8D Momentary Ground = Audio Suppress; Open =Normal Momentary Ground Switch





NOT USED


TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.


Serial Outputs Worksheet 767-300ER


ChannelPins

3, 109, 147, 173, 222Connections

TX453-1A=TP3AB=TP3B


TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B



ChannelPins

203Connections


TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B


Discrete Outputs Worksheet 767-300ER


Lamp 3






TP12B Audio On N/A





MP7CGPWS Monitor




Allied Signal, Inc.




Lamp 109, 173






TP12B Audio On N/A





MP7CGPWS Monitor





Lamp 147











MP7CGPWS Monitor




Allied Signal, Inc.




Lamp 203















Lamp 222






TP12B Audio On N/A





MP7CGPWS Monitor




Allied Signal, Inc.


A-4.11 777-200


Aircraft Type 205




AIMS GP Bus 1

AIMS GP Bus 3

AIMS IRS

Dual (Left and Right)

CMC

ILS

LRRA

Single


SingleExternal

GPSSingle GPS

PP

IN 7

DualExternal

GPSDual GPS

Dual ILS Dual ILS

Dual RA Dual LRRA

PP

IN 9


PWS Option1


PP

IN15 PWS Option

2Dual PWS Hazard Buses

FEATURES



No


ARINC 429 DH Yes


Lamp Format Type 2

Mode 6 Volume Low

Alert Volume High

Steep Approach N/A


Yes

Windshear Yes

Allied Signal, Inc.



PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-202

and on


No auto ranging


displays No No Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

205 TP12C MP3A MP3D





Type.

Allied Signal, Inc.




ARINC429

InputChannel

Pins205

Connections

7A=MP12CB=MP12D

Left AIMS GP Bus 1 (Low Speed) �� "� ��

9A=TP9CB=TP9D

Right AIMS GP Bus 1 (Low Speed) �� !� �� "� ��

3A=MP11AB=MP11B

Left AIMS GP Bus 3 (Low Speed) �� "� �� /

5A=MP10AB-MP10B Right AIMS GP Bus 3 (Low Speed) �� !� �� "� �� /

2A=MP10CB=MP10D Right AIMS IRS (High Speed) �� !� ��

1A=MP6AB=MP6B Left AIMS IRS (High Speed) ��


18A=MP6CB=MP6D

Not usedor


17A=TP11CB=TP11D

Not usedor


6A=MP11CB=MP11D


12A=TP8CB=TP8D

Not usedor

ILS #2 (Low Speed)

8A=MP13AB=MP13B


11A=TP8AB=TP8B

Not UsedOr


4A=MP12AB=MP12B

Not UsedOr


13A=TP5AB=TP6A

Not usedor


15A=TP4AB=TP4B

Not UsedOr


14A=TP1CB=TP1D

Not used ��

16A=TP5CB=TP5D

Not Used ��




Connections



Allied Signal, Inc.





REQUIRED


Gear Override MP9B Ground = Landing Gear Override (down);Open = Not Landing Gear Override

Flap Override MP9C Ground = Landing Flap Override (down);Open = Not Landing Gear Override






OPTIONAL








NOT USED


MP1A N/A ��

MP5C N/A ��

MP14A N/A ��

MP2D N/A ��

TP1A N/A ��

TP1B N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

Allied Signal, Inc.




ChannelPins

205Connections



TX429-1Low Speed

A=MP1CB=MP1D ICDAppendix E label sets: E-1B; E-1C/2/4/5/6/7/10/16

TX429-2Low Speed

A=TP2AB=TP2B ICD Appendix E label sets: E-1B; E-1C/2/4/5/6/7/10



Lamp 205














Allied Signal, Inc.


A-4.12 777-300


Aircraft Type 206




AIMS GP Bus 1

AIMS GP Bus 3

AIMS IRS

Dual (Left and Right)

CMC

ILS

LRRA

Single


SingleExternal

GPSSingle GPS

PP

IN 7

DualExternal

GPSDual GPS

Dual ILS Dual ILS

Dual RA Dual LRRA

PP

IN 9


PWS Option1 Single PWS Hazard Bus

PP

IN 1

5

PWS Option2

Dual PWS Hazard Buses

FEATURES



No


ARINC 429 DH Yes


Lamp Format Type 2

Mode 6 Volume Low

Alert Volume High

Steep Approach N/A


Yes

Windshear Yes

Allied Signal, Inc.



PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-202

and on


No auto ranging


displays No No Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

206 TP12A MP3A MP3D





Type.

Allied Signal, Inc.




ARINC429

InputChannel

Pins206

Connections

7A=MP12CB=MP12D

Left AIMS GP Bus 1 (Low Speed) �� "� ��

9A=TP9CB=TP9D

Right AIMS GP Bus 1 (Low Speed) �� !� �� "� ��

3A=MP11AB=MP11B

Left AIMS GP Bus 3 (Low Speed) �� "� �� /

5A=MP10AB-MP10B Right AIMS GP Bus 3 (Low Speed) �� !� �� "� �� /

1A=MP6AB=MP6B Left AIMS IRS (High Speed) ��

2A=MP10CB=MP10D Right AIMS IRS (High Speed) �� !� ��


18A=MP6CB=MP6D

Not usedor


17A=TP11CB=TP11D

Not usedor


6A=MP11CB=MP11D


12A=TP8CB=TP8D

Not usedor

ILS #2 (Low Speed)

8A=MP13AB=MP13B


11A=TP8AB=TP8B

Not UsedOr


4A=MP12AB=MP12B

Not UsedOr


13A=TP5AB=TP6A

Not usedor


15A=TP4AB=TP4B

Not UsedOr


14A=TP1CB=TP1D

Not used ��

16A=TP5CB=TP5D

Not Used ��




Connections



Allied Signal, Inc.





REQUIRED


Gear Override MP9B Ground = Landing Gear Override (down);Open = Not Landing Gear Override

Flap Override MP9C Ground = Landing Flap Override (down);Open = Not Landing Gear Override






OPTIONAL








NOT USED


MP1A N/A ��

MP5C N/A ��

MP14A N/A ��

MP2D N/A ��

TP1A N/A ��

TP1B N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

Allied Signal, Inc.




ChannelPins

206Connections



TX429-1Low Speed

A=MP1CB=MP1D ICDAppendix E label sets: E-1B; E-1C/2/4/5/6/7/10/16

TX429-2Low Speed

A=TP2AB=TP2B ICD Appendix E label sets: E-1B; E-1C/2/4/5/6/7/10


Connections For Aircraft TypesPin Discretes Flashing

Lamp 206














Allied Signal, Inc.


A-5 Canadair

A.5.1 Global Express


Aircraft Type 97

Description Canadair Global Express



ADC Dual

DAU-3A Single

FMC Dual

FWC Triple

GPS Single

IRS

LRRA

SPS

Dual


PP

IN 7 Dual External

GPSDual GPS

FEATURES



No


ARINC 429 DH Yes


Lamp Format Type 2


Alert Volume Low

Steep Approach Yes - Discrete (Digital Supported)


No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Canadair GEX

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-202

and on

Honeywell Primus2000, 7x8 MFD

(Bus type: HoneywellProprietary Data

Format)10 NM auto ranging

Honeywell

Controlled viaHoneywell display

controller IC strapping(label 171, bit 18)

No No Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

97 MP3A MP7B MP3A





Type.

RS-232 Channel Ass ignment


InputChannel

Pins97

Connections

1Tx=TP6BRx=TP6CCm=MP3A

Used for database uploading and data download ��

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Worksheet Canadair GEX


ARINC429

InputChannel

Pins97

Connections

3A=MP11AB=MP11B


12A=TP8CB=TP8D ADC #2 (Low Speed) ��

8A=MP13AB=MP13B DAU-3A (Low Speed) ��

7A=MP12CB=MP12D FMC #1 (Low Speed) ��

9A=TP9CB=TP9D FMC #2 (Low Speed) ��

4A=MP12AB=MP12B FWC #1 (Low Speed) ��

15A=TP4AB=TP4B

FWC #2 (Low Speed) ��

18A=MP6CB=MP6D

FWC #3 (Low Speed) ��

2A=MP10CB=MP10D

GPS 1 (Low Speed – ARINC 743A) ��

11A=TP8AB=TP8B

Not UsedOr

GPS #2 (Low Speed – ARINC 743A)

1A=MP6AB=MP6B

IRS Bus #1 (High Speed) ��

10A=TP9AB=TP9B


5A=MP10AB-MP10B


14A=TP1CB=TP1D LRRA #2 (Low Speed) ��

6A=MP11CB=MP11D SPS #1 (Low Speed) ��

13A=TP5AB=TP6A SPS #2 (Low Speed) ��

16A=TP5CB=TP5D Not Used !��

17A=TP11CB=TP11D Not used !��





-202 or later GPS #1, #2 High Speed bus(es) 97

Allied Signal, Inc.


Discrete Inputs Worksheet Canadair GEX



REQUIRED

Landing Gear MP9B Ground = Gear Down; Open = Gear Up ��" ��#� #��$

Flap Override MP9C Ground = Flap Override;Open = Not Landing Flap �� !%�� #��$

Glideslope Cancel MP9D Momentary Ground = Cancel; Open = Normal GPWS G/S Muted switch


MP14B Ground = Inhibit; Open = Normal &�""�� !'' #��$

OPTIONAL

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled �"�"�'� �"� �(

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Not Inhibit Cockpit Alt act switch

Steep Approach #1 TP4C Ground = Enabled; Open = Disabled �"�"�'� �"� �(

Steep Approach #2 MP5D Ground = Selected; Open = Not Selected��

��"��$ #��$

NOT USED

Simulator Reposition MP7A Ground = Reposition; Open = Normal !��

MP1A N/A !��

MP1B N/A !��

MP2A N/A !��

MP5C N/A !��

MP7D N/A !��

MP8D N/A !��

MP9A N/A !��

MP14A N/A !��

MP2D N/A !��

TP1A N/A !��

TP1B N/A !��

TP15A N/A !��

TP15B N/A !��

TP15C N/A !��

TP15D N/A !��

TP7A N/A !��

TP7B N/A !��

TP7C N/A !��

TP7D N/A !��

Allied Signal, Inc.


Serial Outputs Worksheet Canadair GEX


ChannelPins

97Connections

TX453-1A=TP3AB=TP3B Left/Right multiplexed picture bus to DU-870 #1 & #2 (port 2)

��) �� *��+

��) �� , *��+

TX453-2A=TP3CB=TP3D Not Used -�� (

TX429-1Low Speed

A=MP1CB=MP1D ICD Appendix E label sets: E-1/2/3/5/6/12/15 �� . �$��

TX429-2Low Speed

A=TP2AB=TP2B ICD Appendix E label sets: E-1/2/3/5/6/12/15 �� . �$�� /

Discrete Outputs Worksheet Canadair GEX


Lamp 97

MP15D Spare N/A !��

MP3D Spare No !��

MP7B Spare No !��

TP12C Spare No !��

TP12A Spare No !��

TP12B Audio On N/A &�� $�0��

TP4D Spare N/A !��


MP14C Spare N/A !��

TP11A Spare N/A !��



TP11B Spare N/A !��

Allied Signal, Inc.


A.5.2 CL601/3A


Aircraft Type 81 85

Description SafeFlight AOA Rosemont AOA



ADC

FMC

IRS

RA

ILS

Single


SingleExternal GPS

Single GPS

Dual ExternalGPS

Dual GPS

PP

IN 7


Dual EFIS Range BusesRequired for EFIS displays

PP

IN 1

4

Alt RAFormat

Single digital LRRAReplaces Analog RA

Alt ILS FormatSingle digital ILS

Automatically replaces Analog G/S if present

FEATURES



No


ARINC 429 DH No


Lamp Format Type 1


Alert Volume Low

Steep Approach Discrete


No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Canadair CL601/3A

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-100

and on

Honeywell SPZ8000,5x6



Honeywell Yes No No No Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

81 MP3A MP15D MP3A

85 TP12C MP15D MP3A

Allied Signal, Inc.



AIRCRAFT TYPESAnalogInputChannel

Pins81 85

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ARINC 552 with Validity Discrete)Use Program Pin14 to enable alternate configurations

OrNot Used

2+ = TP14A- = TP14B Not Used -�� (

3+ = TP13C- = TP13D

Glideslope (ARINC 547 with Validity Flag and ILS Select)Or

Not UsedAOA Indication

� 0-10 VDC Rosemont DCAnalog

� Gain: -5.50� Offset: +55o

� Electrical Range: 55o

� Mechanical Range: 50o

4+ = TP14C- = TP14D

AOA Indication� +-10 VDC SafeFlight

AOA Analog� Gain: -3.333333� Offset: 16o

� Range: -15 to +45o

T P2D(10 VDC)

T P14C (+)

T P14D (-)



81, 85Selected?

Default ARINC 552



Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Canadair CL601/3A


InputChannel

Pins81, 85

Connections

3A=MP11AB=MP11B

ADC #1 (Low Speed- ARINC 429)1

OrNot Used

12A=TP8CB=TP8D

ADC #1 (High Speed – ARINC 575) 1

OrNot Used

2A=MP10CB=MP10D

Not UsedOr

EFIS #1 – Left Range Bus (Low Speed)

9A=TP9CB=TP9D

Not UsedOr

EFIS #2 – Right Range Bus (Low Speed)

4A=MP12AB=MP12B

FMC #1 (Low Speed) 1

OrNot Used

11A=TP8AB=TP8B

FMC #1 (High Speed) 1

OrNot Used

5A=MP10AB-MP10B

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D

Not UsedOr

ILS #1 (Low Speed)

1A=MP6AB=MP6B IRS Bus #1 (High Speed) ��

8A=MP13AB=MP13B

Not UsedOr

LRRA #1 (Low Speed)

7A=MP12CB=MP12D Not Used !��

10A=TP9AB=TP9B Not Used !��

13A=TP5AB=TP6A Not Used !��

14A=TP1CB=TP1D

Not Used !��

15A=TP4AB=TP4B

Not Used !��

16A=TP5CB=TP5D

Not Used !��

18A=MP6CB=MP6D

Not Used !��

1Provide only one ADC input as indicated by bus format; provide only one FMC input as indicated by bus speed.

ARINC 429 Interface Modification Options Worksheet Canadair CL601/3A



Alternate GPSSpeed



-206 and on GPS #1, #2 Use if input is ARINC 743and not ARINC 743A 81, 8516


- FMC #1 Use if Nav Mode label 266is available 81, 85

Allied Signal, Inc.


Discrete Inputs Worksheet Canadair CL601/3A

DISCRETE INPUTS CONNECTIONS

Name PinDISCRETE STATES

81 85

REQUIRED

Self-Test MP9A Momentary Ground = Self-Test;Open = Normal

��' &�� #��$ * ��) �� ( ��

��"� �� "+

Landing Gear MP9B Ground = Gear Down; Open = Gear Up ��" ��#� #��$

Landing Flap MP9CGround = Landing Flap;

Open = Not Landing Flap

�� #� #��$

��( ��

!%�� #��$

Glideslope Cancel MP9D Momentary Ground = Cancel;Open = Normal

�1� �� #��$ * ��) �� 20�"

�� "� �� "+


MP2B Ground = Inhibit; Open = Normal �� &�""�� $�0�� #��$

ILS Select 1 MP14A Ground = ILS Selected;Open = Not Selected � � & ��( ��

Flaps Position #2 (20 o) MP1A Ground = Selected; Open = Not Selected �� 3� #��$

Flaps Position #3 (30 o) MP14B Ground = Selected; Open = Not Selected �� 3� #��$

Flaps Position #4 (45 o) MP2D Ground = Selected; Open = Not Selected �� 43� #��$

Radio Altitude Valid TP15A +28 = Valid; 0V = Not Valid ��(�� %��(��)

Glideslope Valid 1 TP15B +28 = Valid; 0V = Not Valid � � ��(�� %��(��)

AOA Valid TP15D +28 = Valid; 0V = Not Valid! ��2� ��"

%��(��)!��

OPTIONAL

Glideslope Inhibit MP1B Ground = Inhibit; Open = Not Inhibit � � /�� "� ��(��

Mode 6 Volume Control MP2A Ground = Low Volume; Open = Normal �"�"�'� �"� �(

Decision Height MP5C Ground = <DH; Open = >DH ��( �� 5 0 � � ��

Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal�� #�"�� " �"�(��6� �1� (��

� ��"� *��$�0��+ � ��



MP8D Momentary Ground = Audio Suppress;Open = Normal �� (�� "� #��$

Steep Approach #1 TP4C Ground = Enabled; Open = Disabled �"�"�'� �"� �(

Steep Approach #2 MP5D Ground = Selected; Open = Not Selected�� "��$

#��$

NOT USED


Display Select 1 TP1A Do not use !��

Display Select 2 TP1B Do not use !��

TP15C N/A !��

TP7C N/A !��

TP7D N/A !��

TP7A N/A !��

TP7B N/A !��1 ILS Select and Glideslope Valid not required if digital ILS provided. (EGPWS will automatically use digital ILS ifprovided.)

Allied Signal, Inc.


Serial Outputs Worksheet Canadair CL601/3A


ChannelPins

81, 85Connections

TX453-1A=TP3AB=TP3B

Left side picture bus 5��)#�� . ��

TX453-2A=TP3CB=TP3D

Right side picture bus 5��)#�� . ��

TX429-1Low Speed

A=MP1CB=MP1D

ICD Appendix E label sets: E-1/2/3/5/6/9/12 5��)#�� 7�. ��

TX429-2Low Speed

A=TP2AB=TP2B

ICD Appendix E label sets: E-1/2/3/5/6/9/12 !��

Discrete Outputs Worksheet Canadair CL601/3A


Lamp 81, 85

MP15D Glideslope Cancel N/A 20�" �1� ��( ��2�

MP3D Below G/S Caution Yes �'�1��$� 20�" /��# �1� ��2�

MP7BAll


Yes �'�1��$� ��( �� 2�

TP12C Windshear Caution Yes �'�1��$� 20�" �1� �� 2�

TP12A Windshear Warning Yes �'�1��$� ��( �1� ��"�� 2�


TP4D Spare N/A -�� (


MP14C Spare N/A -�� (

TP11A Spare N/A -�� (

MP7C GPWS Monitor N/A 20�" �� -!� ��2�

TP12D Windshear Monitor N/A 20�" ��($��" �-!� ��2�

TP11B Terrain Not Available N/A 20�" &�""�� -!� ��2�



MP3D All GPWS Cautions Yes �'�1��$� 20�" �� 2�

MP7B All GPWS Warnings (“Pull Up”) Yes �'�1��$� ��( � �� 2�

Allied Signal, Inc.


A.5.3 CL604


Aircraft Type 39 40

Description Non-Integrated Display Integrated Display



ADC Dual

ILS N/A

IOC

IRS

Dual

Dual


SingleExternal

GPSSingle GPS

PP

IN 7

DualExternal

GPSDual GPS

FEATURES



No


ARINC 429 DH Yes


Lamp Format Type 1 Type 2


Alert Volume Low

Steep Approach Yes – Discrete


No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Canadair CL604

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-202

and on

Collins ProLine IV(non-integrated)


No auto ranging

Defaultwith +- 60o



1-206

and on

Collins ProLine IVIntergrated




Defaultwith +- 60o

limit

Based on Collinsdisplay controller

strappingNo No Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

39 TP4D MP7B Open

40 Open TP12C Open




There are no alternate Radio Altimeter formats for this Aircraft Type.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Worksheet Canadair CL604


InputChannel

Pins39 40

Connections

12A=TP8CB=TP8D


4A=MP12AB=MP12B


18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


2A=MP10CB=MP10D

IOC Bus #1 (LA-GP-5) (High Speed) �!� ��

3A=MP11AB=MP11B

IOC #2 (RA-GP-5) (High Speed) �!� ��

5A=MP10AB-MP10B ILS #2 (Low Speed) Not Used

6A=MP11CB=MP11D

ILS #1 (Low Speed) Not Used


13A=TP5AB=TP6A IRS Bus #2 (High Speed) ��

7A=MP12CB=MP12D

Not Used !��

8A=MP13AB=MP13B

Not Used !��





15A=TP4AB=TP4B

Not Used !��

16A=TP5CB=TP5D

Not Used !��




Connections

Alternate GPSSpeed

-102 and on GPS #1, #2 Low Speed bus(es) 39, 40


-206 and on GPS #1, #2 Use if input is ARINC 743and not ARINC 743A

39, 4016


-204 and on IOC #1, #2 Use if Nav Mode label 302is available

39

Allied Signal, Inc.


Discrete Inputs Worksheet Canadair CL604

DISCRETE INPUTS DISCRETE STATES FOR AIRCRAFTTYPES


REQUIRED


��'�&�� #��$ * ��) �� (

�� "� �� "+


MP9B Ground = Landing Gear Down;Open = Not Landing Gear ��" ��#� #��$



�� #� #��$ ��( ��

�� !%�� #��$


�1� �� #��$ * ��) �� 20�"

�� "� �� "+


MP2D Ground = Inhibit; Open = Normal �� &�""�� $�0�� #��$

OPTIONAL



Decision Height MP5C Ground = <DH; Open = >DH ��( �� 5 0 � � ��

Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal�� #�"�� " �"�(��6� �1� � (��

��$�0��




Steep Approach #1 MP1A Ground = Enabled; Open = Disabled �"�"�'� �"� �(

Steep Approach #2 MP14B Ground = Selected; Open = Not Selected�� "��$

#��$

Display Select 1 TP1A Momentary Ground Switch �'� ��""�� (��) �� #��$

Display Select 2 TP1B Momentary Ground Switch ��$� ��""�� (��) �� #��$

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Normal 8��$9 #��$

NOT USED


MP14A N/A !��

TP4C N/A !��

MP5D N/A !��

TP15A N/A !��

TP15B N/A !��

TP15C N/A !��

TP15D N/A !��

TP7C N/A !��

TP7D N/A !��

TP7A N/A !��

TP7B N/A !��

Allied Signal, Inc.


Discrete Inputs Worksheet Canadair CL604



REQUIRED


��'�&�� #��$ * ��) �� (

�� "� �� "+

Landing Gear MP9B Ground = Landing Gear Down;Open = Not Landing Gear ��" ��#� #��$


MP9C Ground = Landing Flap; Open = NotLanding Flap

�� #� #��$ ��( ��

�� !%�� #��$


�1� �� #��$ * ��) �� 20�"

�� "� �� "+



OPTIONAL



Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal�� #�"�� " �"�(��6� �1� � (��

��$�0��






#��$


NOT USED


Decision Height MP5C N/A !��

MP14A N/A !��

TP1A N/A !��

TP1B N/A !��

TP4C N/A !��

MP5D N/A !��

TP15A N/A !��

TP15B N/A !��

TP15C N/A !��

TP15D N/A !��

TP7C N/A !��

TP7D N/A !��

TP7A N/A !��

TP7B N/A !��

Allied Signal, Inc.


Serial Outputs Worksheet Canadair CL604


ChannelPins

39Connections

TX453-1A=TP3AB=TP3B

Left picture bus �'� �� :1&�""��

"��)

TX453-2A=TP3CB=TP3D Right picture bus

��$� �� :1&�""��

�� "��)

TX429-1Low Speed


��) ��"�� *��+

��. � ��( �

TX429-2Low Speed

A=TP2AB=TP2B ICD Appendix E label sets: E-1/2/3/5/6/9/12 -�� (


ChannelPins

40Connections

TX453-1A=TP3AB=TP3B Left picture bus �'� ��

TX453-2A=TP3CB=TP3D Right picture bus ��$� ��

TX429-1Low Speed

A=MP1CB=MP1D ICD Appendix E label sets: E-1/2/3/5/6/17

��) ��"�� *��+

��. � ��( �

TX429-2Low Speed

A=TP2AB=TP2B ICD Appendix E label sets: E-1/2/3/5/6/17 -�� (

Discrete Outputs Worksheet Canadair CL604


Lamp 39

MP15D Glideslope Cancel N/A 20�" �1� ��( ��2�

MP3D Below G/S Caution Yes �'�1��$� 20�" /��# �1� ��2�

MP7BAll


Yes �'�1��$� ��( �� 2�

TP12C Spare No -�� (

TP12A Spare No -�� (



TP10D Terrain Display Discrete #1 N/A �'� &�""�� )

MP14C Terrain Display Discrete #2 N/A ��$� &�""�� )


MP7C GPWS Monitor N/A 20�" �� -!� ��2�

TP12D Windshear Monitor N/A 20�" ��($��" �-!� ��2�

TP11B Terrain Not Available N/A 20�" &�""�� -!� ��2�



MP3D All GPWS Cautions Yes �'�1��$� 20�" �� 2�

MP7B All GPWS Warnings (“Pull Up”) Yes �'�1��$� ��( � �� 2�

Allied Signal, Inc.


Discrete Outputs Worksheet Canadair CL604


Lamp 40

MP15D Spare N/A -�� (

MP3D Spare Yes -�� (

MP7B Spare Yes -�� (

TP12C Spare No -�� (

TP12A Spare No -�� (








TP11B Spare N/A -�� (

Allied Signal, Inc.


A.5.4 Regional Jet (RJ-100/RJ-200)


Aircraft Type 43

Description Canadair Regional Jet (RJ-100/RJ-200)



ADC

DSWC

ILS

IOC

Dual

IRS Dual (Optional Dual AHRS replaces these interfaces)

LRRA Dual

MFD Dual (Not Used if “No Display” option selected)


SingleExternalGPS

Single GPS

DualExternalGPS

Dual GPS

PP

IN 7

OptionalInputSelect

See ARINC 429 Interface Modification Options Worksheet

FEATURES



No


ARINC 429Decision Height

Yes


Lamp Format Type 1


Alert Volume Low



No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Canadair RJ-100/RJ-200

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-208

and on



No auto ranging

Defaultwith +- 60o


2-208

and onNo Display N/A N/A N/A N/A N/A MP3A




1 (TP10A) 2 (TP10B) 3 (TP10C)

43 MP3D TP12C Open




There are no alternate radio altimeter formats for this Aircraft Type.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Canadair RJ-100/RJ-200


ARINC429

InputChannel

Pins43

Connections

12A=TP8CB=TP8D


4A=MP12AB=MP12B


8A=MP13AB=MP13B



18A=MP6CB=MP6D

Not usedor


17A=TP11CB=TP11D

Not usedor


2A=MP10CB=MP10D

IOC #1 (LA-GP-5) (Low Speed) �!� ��

3A=MP11AB=MP11B

IOC #2 (RA-GP-5) (Low Speed) �!� ��

5A=MP10AB-MP10B

ILS #2 (Low Speed) � � ��

6A=MP11CB=MP11D

ILS #1 (Low Speed) � � ��

1A=MP6AB=MP6B


AHRS #1 (High Speed)

13A=TP5AB=TP6A



10A=TP9AB=TP9B

LRRA #2 (R-RAC-1) (Low Speed) ��

11A=TP8AB=TP8B

LRRA #1 (L-RAC-1) (Low Speed) ��

7A=MP12CB=MP12D

MFD 1 (Left MFD 1) (Low Speed)Or

Not Used (Disable if “No Display” option selected)

14A=TP1CB=TP1D

MFD 2 (Right MFD 1) (Low Speed)Or

Not Used (Disable if “No Display” option selected)

15A=TP4AB=TP4B Not used !��

16A=TP5CB=TP5D Not used !��




Alternate GPSSpeed

-208 and on GPS #1, #2 High Speed bus(es) 43




-208 and on IOC #1, #2 Use if Nav Mode label 277is NOT available 43

7OptionalInputs Select -208 and on FMC #1,#2

Use if FMS #2 inputs areNOT available.

NOTE: FMS inputs are fedto the IOC buses.

43

Allied Signal, Inc.


Discrete Inputs Worksheet Canadair RJ-100/RJ-200



REQUIRED


��'�&�� #��$ * ��) �� (

�� "� �� "+

Landing Gear MP9B Ground = Landing Gear Down;Open = Not Landing Gear ��" ��#� #��$


MP9C Ground = Landing Flap; Open = NotLanding Flap

�� #� #��$ ��( ��

�� !%�� #��$


�1� �� #��$ * ��) �� 20�"

�� "� �� "+



OPTIONAL



Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal�� #�"�� " �"�(��6� �1�

(�� "� *��$�0��+ � ��






#��$

Display Select #1 TP1A Momentary Ground Switch �'� ��""�� (��) �� #��$

Display Select #2 TP1B Momentary Ground Switch ��$� ��""�� (��) �� #��$


NOT USED


Decision Height MP5C N/A !��

MP14A N/A !��

TP4C N/A !��

MP5D N/A !��

TP15A N/A !��

TP15B N/A !��

TP15C N/A !��

TP15D N/A !��

TP7A N/A !��

TP7B N/A !��

TP7C N/A !��

TP7D N/A !��

Allied Signal, Inc.


Serial Outputs Worksheet Canadair RJ-100/RJ-200


ChannelPins

43Connections

TX453-1A=TP3AB=TP3B

Left side picture bus to symbol generator portOr

Not Used (if “No Display” option is selected)

�� )

!"

-�� (

TX453-2A=TP3CB=TP3D

Right side picture bus to symbol generator portOr

Not Used (if “No Display” option is selected)

�� )

!"

-�� (

TX429-1Low Speed

A=MP1CB=MP1D Transmits ICD Appendix E label sets: 1/2/3/5/6/9/12 ��. �� 7 ��

TX429-2Low Speed

A=TP2AB=TP2B Transmits ICD Appendix E label sets: 1/2/3/5/6/9/12 -�� (



FlashingLamp 43

MP15D Glideslope Cancel N/A �'�1��$� �1� �� 2� *�� "� �/+

MP3D Below G/S Caution No �'�1��$� 20�" ��(�� / �" �-� ��!: �/

MP7BAll


No �'�1��$� ��( �� / �" �� /

TP12C Windshear Caution No �'�1��$� �"�2�") ��$� ��)

TP12A Windshear Warning No �'�1��$� �"�2�") ��$� ��)



TP10D Terrain Display Discrete #1 N/A �'� &�""�� )

MP14C Terrain Display Discrete #2 N/A ��$� &�""�� )

TP11A Spare N/A !��


TP12D Windshear Monitor N/A �'�1��$� �"�2�") ��$� ��)

TP11B Terrain Not Available N/A &�""�� -!� �2�



MP3D All GPWS Cautions No �'�1��$� 20�" �-� ��!: �/

MP7B All GPWS Warnings (“Pull Up”) No �'�1��$� ��( � �� /

Allied Signal, Inc.


A-6 Cessna

A.6.1 Citation X


Aircraft Type 62

Description Citation X



ADCAHRSFMCGP

Dual

GPS Single


Dual ExternalGPS

Dual GPS

PP

IN 7


Dual IRSReplaces Dual AHRS

Alternate RA #2Single digital LRRA

Replaces Analog RA

Triple GP GP #3 (will use if provided)

FEATURES



No


ARINC 429 DH No


Lamp Format Type 2


Alert Volume High



No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Cessna Citation X

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-104

and on




Honeywell

Based ondisplay

controllerIC bezelselection

N/A No No Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

62 TP12A TP4D Open



AnalogInputChannel

Pins62

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ARINC 552 with Validity Discrete)Or

Not Used (use Alt. RA Format to select LRRA input)

2+ = TP14A- = TP14B

Right SWC – Vane AOARange: 0-10 VDC

Offset = -80.506234o

Gain = 11.308706Range = 0 to 70o

��


4+ = TP14C- = TP14D

Left SWC – Vane AOARange: 0-10 VDC

Offset = -80.506234o

Gain = 11.308706Range = 0 to 70o

��



62Selected?

Default ARINC 552



Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Cessna Citation X


InputChannel

Pins62

Connections

3A=MP11AB=MP11B



1A=MP6AB=MP6B

AHRS #1 (High Speed) (Default)Or

IRS Bus #1 (High Speed)

13A=TP5AB=TP6A

AHRS #2 (High Speed) (Default)Or


5A=MP10AB-MP10B

FMC #1 (Low Speed) ��

9A=TP9CB=TP9D


4A=MP12AB=MP12B GP #1 (Low Speed) ��

10A=TP9AB=TP9B GP #2 (Low Speed) ��

15A=TP4AB=TP4B

Not UsedOr

GP #3 (Low Speed) (EGPWS will use if provided)

18A=MP6CB=MP6D

GPS #1 (High Speed – ARINC 743A) ��

17A=TP11CB=TP11D

Not UsedOr

GPS #2 (High Speed – ARINC 743A)

8A=MP13AB=MP13B

Not UsedOr

LRRA #1 (Left) (Low Speed)

2A=MP10CB=MP10D Not Used � �

6A=MP11CB=MP11D

Not Used � �

7A=MP12CB=MP12D

Not Used � �

11A=TP8AB=TP8B

Not Used � �

14A=TP1CB=TP1D Not Used � �


ARINC 429 Interface Modification Options Worksheet Cessna Citation X



Connections

Alternate GPSSpeed

-104 and on GPS #1, #2 Low Speed bus(es) 62


Use if input is ARINC 743and not ARINC 743A 6216


-206 and on FMC #1, #2Use if Nav mode label 266

is available 62

Allied Signal, Inc.


Discrete Inputs Worksheet Cessna Citation X



REQUIRED

Landing Gear MP9B Ground = Gear Down; Open = Gear Up ��! ��" �"��#�


�$� � �%$$ ��" �"��#� � � �$� �#��

#�#& �� $� � �� "��#�

Flaps Position #1 (0 o) MP2D Ground = Selected; Open = Not Selected �$� � '� �"��#�

Flaps Position #2 (5 o) TP4C Ground = Selected; Open = Not Selected �$� � (� �"��#�

Flaps Position #3 (15 o) MP5D Ground = Selected; Open = Not Selected �$� � �(� �"��#�

Flaps Position #4 (35 o) MP7A Ground = Selected; Open = Not Selected �$� � )(� �"��#�

Radio Altimeter Valid TP15A +28V = Valid; 0V = Not Valid �� $� ��$��*

Stall Warning ComputerFail Flag - Right

TP15C +28V = Valid; 0V = Not Valid �� $��*

Stall Warning ComputerFail Flag - Left

TP15D +28V = Valid; 0V = Not Valid �� $��*

OPTIONAL

Glideslope Inhibit MP1B Ground = Inhibit; Open = Not Inhibit +�� ,�#&#�%!�� #��

Mode 6 Volume Control MP2A Ground = Low Volume; Open = Normal ��!#!�� !�% �

Decision Height MP5C Ground = <DH; Open = >DH �� $� �- .%� �%� %�

Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal��$$ "�! � � �! !��#��/� �0�

�%�� % !�� %� %�

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled ��!#!�� !�% �


MP8D Momentary Ground = Audio Suppress;Open = Normal �#& �� %�� % !�� "��#�


��$�12�� "��#� 3%�%�$$* � ��

�� ! � % #��!4

Steep Approach #1 MP1A Ground = Enabled; Open = Disabled ��!#!�� !�% �

Steep Approach #2 MP14B Ground = Selected; Open = Not Selected�#& �� $� �#�� !��#�

�"��#�

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Normal 5��#�6 �"��#�

NOT USED

MP9D N/A � �

MP14A N/A � �

TP1A N/A � �

TP1B N/A � �

TP15B N/A � �

TP7A N/A � �

TP7B N/A � �

TP7C N/A � �

TP7D N/A � �

Allied Signal, Inc.


Serial Outputs Worksheet Cessna Citation X


ChannelPins

62Connections

TX453-1A=TP3AB=TP3B

Left/Right multiplexed picture bus to DU-870 #1 & #2�� 3�� 4

��7 3�� 4

TX453-2A=TP3CB=TP3D Not Used � �

TX429-1Low Speed

A=MP1CB=MP1D ICD Appendix E label sets: E-1/2/3/5/6/9/12 ��

TX429-2Low Speed

A=TP2AB=TP2B

ICD Appendix E label sets: E-1/2/3/5/6/9/12 � �



Lamp 62



MP7B Spare No ��



TP12B Audio On N/A 2�� + ��.��








Allied Signal, Inc.


A.6.2 Citation Excel



Description Citation ExcelCitation ExcelLow Speed ILS



ADC

AHRS

FDR

Dual

FMC Single

ILS Single (analog) Dual (digital)

AOA

RASingle


SingleExternal GPS

Single GPS

Dual ExternalGPS

Dual GPS

PP

IN 7


Dual FMC

PP

IN 9

Dual RADual digital LRRA

Applies only if Alternate RA Format #2 (ARINC 429) selected

Alternate RA #2Single digital LRRAReplaces analog RA

Alternate ILSFormat

Single or Dual digital ILS N/A

FEATURES



No


ARINC 429 DH No


Lamp Format Type 2


Alert Volume Low



No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Cessna Citation Excel

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-104

and on








1 (TP10A) 2 (TP10B) 3 (TP10C)

103 TP4D MP7B MP3A

167 TP4D MP7B MP15D

Allied Signal, Inc.


Analog Input Channel Assignments Cessna Citation Excel


AnalogInputChannel

Pins103

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ALT 55B with Validity Flag)(use Alt. RA Format #1 for ARINC 552 with Validity Flag)

OrNot Used (use Alt. RA Format #2 to select LRRA input)

2+ = TP14A- = TP14B

AOA SystemFormat: DC voltage + Validity Flag

Range: +-10 VDCOffset: 0o

Gain = -4.0

�� *��8

3+ = TP13C- = TP13D

Glideslope #1 (ARINC 547 with Validity Flag & ILS Select)Or

Not Used (will use ARINC 429 ILS if provided)

4+ = TP14C- = TP14D

Localizer #1 (ARINC 547 with Validity Flag & ILS Select)Or



AnalogInputChannel

Pins167

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ALT 55B with Validity Flag)(use Alt. RA Format #1 for ARINC 552 with Validity Flag)


2+ = TP14A- = TP14B

AOA SystemFormat: DC voltage + Validity Flag

Range: +-10 VDCOffset: 0o

Gain = -4.0

�� *��8





103, 167Selected?

Default ALT 55



Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Cessna Citation Excel


InputChannel

Pins103 167

Connections



1A=MP6AB=MP6B AHRS Bus #1 (High Speed) +��

10A=TP9AB=TP9B AHRS #2 (High Speed) ��

4A=MP12AB=MP12B

FDR #1 (IC-600 #1) (Low Speed) ��

11A=TP8AB=TP8B

FDR #2 (IC-600 #2) (High Speed) ��


9A=TP9CB=TP9D

Not UsedOr

FMC #2 (High Speed)

18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


5A=MP10AB-MP10B

Not UsedOr

ILS #2 (IC-600 #2) (High Spd)(will use if provided)

ILS #2 (Low Speed)

6A=MP11CB=MP11D

Not UsedOr

ILS #1(IC-600 #1) (High Spd)(will use if provided)

ILS #1 (Low Speed)

8A=MP13AB=MP13B

Not UsedOr

LRRA #1 (Left) (Low Speed)(will use if Alt RA format #2 selected)

2A=MP10CB=MP10D

Not UsedOr


13A=TP5AB=TP6A Not Used � �


15A=TP4AB=TP4B

Not Used � �

16A=TP5CB=TP5D

Not Used � �




Alternate GPSSpeed -204 and on GPS #1, #2 Low Speed bus(es) 103, 167


-206 and on GPS #1, #2Use if input is ARINC 743

and not ARINC 743A 103, 167

Allied Signal, Inc.


Discrete Inputs Worksheet Cessna Citation Excel

DISCRETES DISCRETE STATES FOR AIRCRAFTTYPES


REQUIRED

Self-Test MP9A Momentary Ground = Self Test;Open = Normal

��$�12�� "��#� 3%�%�$$* � ��

�� ! � % #��!4


Flap Override MP9CGround = Flaps Override;

Open = Not Override

�$� � �%$$ ��" �"��#� � � �$�

�#�� #�#& �� $� � ��

�"��#�

Glideslope Cancel MP9D Momentary Ground = Cancel; Open = Normal�0� � #�$ �"��#� 3%�%�$$* �

�8.�! �� $�!� � % #��!4


MP14B Ground = Inhibit; Open = Normal �$� �#�� 2�!!�� + ��.�� "��#�

ILS Select 2 MP14A Ground = ILS Selected; Open = Not Selected +�� 2% �� # �%� %�

Flaps Position #2 (35 o) TP4C Ground = Selected; Open = Not Selected �$� � )(� �"��#�

Radio Altimeter #1Valid 1 TP15A +28 V = Valid; 0 V = Not Valid �� $� ��$��*

Glideslope #1 Valid 2 TP15B +28 V = Valid; 0 V = Not Valid +�� $��$� � ��$��*

AOA Valid TP15C +28 V = Valid; 0 V = Not Valid �� 8 %��! ��$��*

Localizer Valid 2 TP15D +28 V = Valid; 0 V = Fail +�� #�$�9�! ��$��*

OPTIONAL




Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal��$$ "�! � � �! !��#��/� �0�

�%�� % !�� %� %�



MP8D Momentary Ground = Audio Suppress; Open= Normal

�#& �� %�� % !��

�"��#�

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Normal ��!#!�� !�% �

Steep Approach #1 MP1A Ground = Enabled; Open = Disabled�#& �� $� �#�� !��#�

�"��#�

Steep Approach #2 MP5D Ground = Selected; Open = Not Selected 5��#�6 �"��#�

NOT USED


MP2D N/A Open

TP1A N/A Open

TP1B N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open1 RA Valid not required if Alternate RA #2 (digital RA) used.2 ILS Select and Glideslope Valid not required if digital ILS provided. (EGPWS will automatically use digital ILS ifprovided.)

Allied Signal, Inc.


Discrete Inputs Worksheet Cessna Citation Excel



REQUIRED


��$�12�� "��#� 3%�%�$$* � ��

�� ! � % #��!4


Flap Override MP9C Ground = Flap Override;Open = Not Override

�$� � �%$$ ��" �"��#� � � �$� �#��

#�#& �� $� � �� "��#�


�0� � #�$ �"��#� 3%�%�$$* � �8.�!

�� $�!� � % #��!4


MP14B Ground = Inhibit; Open = Normal �$� �#�� 2�!!�� + ��.�� "��#�

Radio Altimeter #1Valid 1 TP15A +28 V = Valid; 0 V = Not Valid �� $� ��$��*

AOA Valid TP15C +28 V = Valid; 0 V = Not Valid �� 8 %��! ��$��*

Flaps Position #2 (35 o) TP4C Ground = Selected; Open = Not Selected �$� � )(� �"��#�

OPTIONAL




Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal��$$ "�! � � �! !��#��/� �0� �%��

�% !�� %� %�



MP8D Momentary Ground = Audio Suppress;Open = Normal �#& �� %�� % !�� "��#�

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Normal 5��#�6 �"��#�

Steep Approach #1 MP1A Ground = Enabled; Open = Disabled ��!#!�� !�% �

Steep Approach #2 MP5D Ground = Selected; Open = Not Selected�#& �� $� �#�� !��#�

�"��#�

NOT USED


MP14A N/A Open

MP2D N/A Open

TP1A N/A Open

TP1B N/A Open

TP15B N/A Open

TP15D N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open1 RA Valid not required if Alternate RA #2 (digital RA) used.

Allied Signal, Inc.


Serial Outputs Worksheet Cessna Citation Excel


ChannelPins

103, 167Connections

TX453-1A=TP3AB=TP3B Honeywell Left/Right multiplexed picture bus to MFD +1:''

TX453-2A=TP3CB=TP3D Not Used � �

TX429-1Low Speed

A=MP1CB=MP1D ICD Appendix E label sets: E-1/2/3/5/6/9/12 +1:''

TX429-2Low Speed

A=TP2AB=TP2B ICD Appendix E label sets: E-1/2/3/5/6/9/12 +1:''

Allied Signal, Inc.


Discrete Outputs Worksheet Cessna Citation Excel


Lamp 103

MP15D Glideslope Cancel N/A �8.�! �� 0� � #�$�� $�8

MP3D Not Used No � �

MP7B Not Used No � �

TP12C Not Used No � �

TP12A Not Used No � �


TP4D Spare N/A � �

TP10D Not Used N/A � �

MP14C Not Used N/A � �

TP11A Spare N/A � �



TP11B Not Used N/A � �


Lamp 167

MP15D Glideslope Cancel N/A �8.�! �� 0� � #�$�� $�8

MP3D Not Used No � �

MP7B Not Used No � �

TP12C Not Used No � �

TP12A Not Used No � �


TP4D Spare N/A � �



TP11A Spare N/A � �



TP11B Not Used N/A � �

Allied Signal, Inc.


A-7 Dassault

A-7.1 Falcon 20F



Description With AHRS and Pro Line 2With IRS Option and

Pro Line 2 Integrated Pro Line 4



ADC Single (ARINC 429 or ARINC 575) Dual

AHRSSingle AHC-85 type AHRS

with A/D converter Optional

FMC Single (High Speed or Low Speed) N/A

IOC N/A Dual

ILS Single (analog) N/A

IRS N/A Single Dual

AOA

RASingle


SingleExternal GPS

Single GPS

Dual ExternalGPS

Dual GPS

PP

IN 7


Dual Wx Control Panel Buses (Range) N/A

PP

IN 9

Dual RA N/A Dual LRRA

Alternate RAFormat

Single digital LRRAReplaces Analog RA Digital RA only

Alternate ILSFormat

Single digital ILSReplaces Analog ILS N/A

Alternate AHRSInputs

N/A Single AHRSReplaces Single IRS

Dual AHRSReplaces Dual IRS

FEATURES



No


ARINC 429 DH No Yes




Alert Volume High



No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Falcon 20F

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-202

and on

Collins ProLine 2 (non-integrated), 5x6


No auto ranging

Defaultwith +-60o



1-204

and on



No auto ranging

Defaultwith +-60o



1-204

and on



(label 077))10 NM auto rangingcontrolled by display

Fan modewith +-60o

limit

Based ondisplay

controllerstrapping

N/A No No Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

70 TP12A Open MP3A

71 TP4D Open MP3A

77 TP12C MP3A MP3A

Allied Signal, Inc.




AnalogInputChannel

Pins70, 71

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ALT 55 with Validity Flag)(use Alt. RA Format #1 for ARINC 552)

OrNot Used (use Alt. RA Format to select LRRA input)

2+ = TP14A- = TP14B Not Used ��

3+ = TP13C- = TP13D



4+ = TP14C- = TP14D

Vane AOA, PotentiometerFormat: 0 - 10 VDC

Offset: 39.27o

Gain = -4.444o



T P2D(10 VDC)

T P14C (+)

T P14D (-)

There are no analog inputs for Aircraft Type 77.



70, 71Selected?

Default ALT 55



Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Falcon 20F


InputChannel

Pins70

Connections

3A=MP11AB=MP11B

ADC #1 - ARINC 575 (Low Speed) 1

orNot Used

12A=TP8CB=TP8D

Not UsedOr

ADC #1 ARINC 429 (Low Speed) 1

1A=MP6AB=MP6B AHRS #1 (High Speed) 2

��

9A=TP9CB=TP9D

FMC (Low Speed) 1

OrNot Used

11A=TP8AB=TP8B

Not UsedOr

FMC (High Speed) 1

18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D

Not UsedOr

ILS #1 (Low Speed) (will use if provided)

8A=MP13AB=MP13B

Not UsedOr

LRRA #1 (Left) (Low Speed) (will use if Alt RA format selected)

5A=MP10AB-MP10B

Not UsedOr

Wx Control Panel Bus 1 (Low Speed)

7A=MP12CB=MP12D

Not UsedOr





13A=TP5AB=TP6A

Not Used ��

14A=TP1CB=TP1D

Not Used ��

15A=TP4AB=TP4B

Not Used ��

16A=TP5CB=TP5D

Not Used ��

1Provide only one ADC input as indicated by bus format; provide only one FMC input as indicated by bus speed.2For A/C Type 70: AHC-85 type AHRS with A/D converter is required (Normal Acceleration = 1g on ground).ARINC 429 Interface Modification Options Worksheet Falcon 20F






and not ARINC 743A 7016

ConfigurationOption 2 - FMC

Use if Nav mode label 266is available 70

Allied Signal, Inc.




InputChannel

Pins71

Connections

3A=MP11AB=MP11B


orNot Used

12A=TP8CB=TP8D

Not UsedOr


1A=MP6AB=MP6B

IRS #1 (High Speed)or

AHRS Bus #1 (High Speed)

9A=TP9CB=TP9D

FMC (Low Speed) 1

OrNot Used

11A=TP8AB=TP8B

Not UsedOr

FMC (High Speed) 1

18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D

Not UsedOr


8A=MP13AB=MP13B

Not UsedOr


5A=MP10AB-MP10B

Not UsedOr


7A=MP12CB=MP12D

Not UsedOr










ARINC 429 Interface Modification Options Worksheet Falcon 20F



Connections

Alternate GPSSpeed





Use if Nav mode label 266is NOT available 71

Allied Signal, Inc.




InputChannel

Pins77

Connections

4A=MP12AB=MP12B

ADC #1 – ARINC 429 (Low Speed) ��

12A=TP8CB=TP8D


5A=MP10AB-MP10B

Not UsedOr

GPS #1 (High Speed)

11A=TP8AB=TP8B

Not UsedOr


2A=MP10CB=MP10D Left IOC #1 (High Speed) Left IOC #1

3A=MP11AB=MP11B Right IOC #2 (High Speed) ��

1A=MP6AB=MP6B



13A=TP5AB=TP6A



8A=MP13AB=MP13B LRRA Bus #1 (Low Speed) ��

10A=TP9AB=TP9B

Not UsedOr

LRRA Bus #2 (Low Speed)









ARINC 429 Interface Modification Options Worksheet Falcon 20F



Alternate GPSSpeed




ConfigurationOption 2 - IOC #1, #2

Use if Nav mode label 302is NOT available 77

Allied Signal, Inc.


Discrete Inputs Worksheet Falcon 20F



REQUIRED

Self-Test MP9A Momentary Ground = Self Test; Open =Normal

�� !

"#$� $�%� �� %&

Landing Gear MP9B Ground = Gear Down; Open = Gear Up "��% � ��

Landing Flap MP9C Ground = Landing Flap; Open = Not LandingFlap

'�� '�� ! ��

� �(�� "#$� '�� )��

Glideslope Cancel MP9D Momentary Ground = Cancel; Open =Normal

"*� �� +,�%

"#$� ��%� �� %&


MP14B Ground = Inhibit; Open = Normal �� %%�� ,��

ILS Select 2 MP14A Ground = ILS Selected; Open = Not Selected �� ! � � � ��

Radio Altimeter #1Valid 1 TP15A +28 V = Valid; 0 V = Not Valid ��!� �� )��!��

Glideslope #1 Valid 2 TP15B +28 V = Valid; 0 V = Not Valid �� "��!�� )��!��

Flaps Position #1 (0 o) TP7A +28 V = Selected; 0 V = Not Selected '�� -� ��

Flaps Position #2 (10 o) TP7B +28 V = Selected; 0 V = Not Selected '�� -� ��

Flaps Position #3 (25 o) TP7C +28 V = Selected; 0 V = Not Selected '�� .� ��

Flaps Position #4 (40 o) TP7D +28 V = Selected; 0 V = Not Selected '�� /-� ��

OPTIONAL

Glideslope Inhibit MP1B Ground = Inhibit; Open = Not Inhibit �� 0��(� �%�� !��

Mode 6 Volume Control MP2A Ground = Low Volume; Open = Normal ��%�%�� "% ��!

Decision Height MP5C Ground = <DH; Open = >DH ��! �� ,��

Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal�� %�� % �%�!��1� $*�

��!� ��,��

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled ��%�%�� "% ��!


MP8D Momentary Ground = Audio Suppress; Open= Normal

�(�� "#$� ��!� ��%��

��

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Normal 2��3 ��

Steep Approach #1 TP4C Ground = Enabled; Open = Disabled ��%�%�� "% ��!

Steep Approach #2 MP5D Ground = Selected; Open = Not Selected �(�� % ��

��

Display Select 1 TP1A Momentary Ground Switch �� %%�� !��

Display Select 2 TP1B Momentary Ground Switch �� %%�� !��

NOT USED


MP1A N/A Open

MP2D N/A Open

TP15C N/A Open


Allied Signal, Inc.


Discrete Inputs Worksheet Falcon 20F



REQUIRED

Self-Test MP9A Momentary Ground = Self Test; Open =Normal

�� !

"#$� $�%� �� %&


Flaps Override MP9C Ground = Flap Override;Open = Not Flap Override

'�� '�� ! ��

� �(�� "#$� '�� )��


"*� �� +,�%

"#$� ��%� �� %&



OPTIONAL




Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal�� %�� % �%�!��1� $*� ��!�

��,��



MP8D Momentary Ground = Audio Suppress;Open = Normal �(�� "#$� ��!� ��%��

Steep Approach #1 MP1A Ground = Enabled; Open = Disabled ��%�%�� "% ��!

Steep Approach #2 MP14A Ground = Selected; Open = Not Selected �(�� % ��

��


NOT USED


MP2D N/A Open

TP1A N/A Open

TP1B N/A Open

TP4C N/A Open

MP5D N/A Open

TP15A N/A Open

TP15B N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet Falcon 20F


ChannelPins

70, 71Connections

TX453-1A=TP3AB=TP3B Left side picture bus �� 4'� $5*��%%�� %��

TX453-2A=TP3CB=TP3D Right side picture bus �� 4'� $5*��%%�� %��

TX429-1Low Speed


TX429-2Low Speed

A=TP2AB=TP2B ICD Appendix E label sets: E-1/2/3/5/6/9/12 ��


ChannelPins

77Connections

TX453-1A=TP3AB=TP3B Left side picture bus Left MFD

TX453-2A=TP3CB=TP3D Right side picture bus Right MFD

TX429-1Low Speed

A=MP1CB=MP1D ICD Appendix E label sets: E-1/2/3/5/6/17 � 6 �7 � 8 9

TX429-2Low Speed

A=TP2AB=TP2B ICD Appendix E label sets: E-1/2/3/5/6/17 ��

Allied Signal, Inc.


Discrete Outputs Worksheet Falcon 20F


Lamp 70, 71

MP15D Glideslope Cancel N/A �+,�% "*� ��! ��+�

MP3D Below G/S Caution Yes ��*�� +,�% "*� ��+��

MP7BAll


Yes ��*�� ! "#$� ��+��

TP12C Windshear Caution Yes ��*�� +,�% $*� �� +��

TP12A Windshear Warning Yes ��*�� ! $*� $�%�� +��

TP12B Audio On N/A � �� ,��


TP10D Terrain Display Discrete #1 N/A �� %%��

MP14C Terrain Display Discrete #2 N/A �� %%��


MP7C GPWS Monitor N/A �+,�% "#$� �:�# ��+�

TP12D Windshear Monitor N/A �+,�% $��!��% �:�# ��+�

TP11B Terrain Not Available N/A �+,�% ��%%�� :�# ��+�



MP3D All GPWS Cautions No ��*�� +,�% "#$� ��+��

MP7B All GPWS Warnings (“Pull Up”) No ��*�� ! #�� 6� ��+��


Lamp 77

MP15D Glideslope Cancel N/A �+,�% "*� ��+��

MP3D All GPWS Cautions Yes ��*�� +,�% "*� ��+��

MP7B All GPWS Warnings (“Pull Up”) Yes ��*�� ! "#$� ��+��

TP12C Windshear Caution Yes #%�+�%� '��

TP12A Windshear Warning Yes #%�+�%� '��



TP10D Terrain Display Discrete #1 N/A ��

MP14C Terrain Display Discrete #2 N/A ��





Allied Signal, Inc.


A-7.2 Falcon 2000



Description Integrated Pro Line 4 Bolt-on Pro Line 4



ADC Dual

FMC N/A (via IOC) Dual

IOC Dual

IRS Dual (or single or dual GPIRS)

LRRA Single


SingleExternal GPS

Single GPSNo GPIRS

Dual ExternalGPS

Dual GPSNo GPIRS

Single GPIRSOverlay

Single GPIRSReplaces dual IRS inputs, no GPS

Dual GPIRSOverlay

Dual GPIRSReplaces IRS inputs, no GPS

PP

IN 7


N/A See ARINC 429 Interface Modifications Options

PP

IN 9

Dual RA Dual LRRA

FEATURES



No


ARINC 429 DH Yes


Lamp Format Type 2


Alert Volume High



No

Windshear Yes

Allied Signal, Inc.



PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-202

and on





Fan modewith +-60o

limit

Based ondisplay

controllerstrapping

N/A No No Open

2-208

and on





Fan modewith +-90o

limit

Based ondisplay

controllerstrapping

N/A No No MP3A


1-105

and on



No auto ranging

Defaultwith +-60o





1 (TP10A) 2 (TP10B) 3 (TP10C)

91 MP3D MP3D MP3A

125 TP12C TP4D MP3A



Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Falcon 2000


InputChannel

Pins91 125

Connections

4A=MP12AB=MP12B


12A=TP8CB=TP8D


6A=MP11CB=MP11D

Not Used FMC #1 (High Speed)

15A=TP4AB=TP4B Not Used FMC #2 (High Speed)

5A=MP10AB-MP10B

Not UsedOr


11A=TP8AB=TP8B

Not UsedOr


2A=MP10CB=MP10D Left IOC #1 (High Speed) ��

3A=MP11AB=MP11B

Right IOC #2 (High Speed) ��

1A=MP6AB=MP6B


GPIRS Bus #1 (High Speed)

13A=TP5AB=TP6A

IRS #2 (High Speed)(IRS #2 not used if Single GPIRS Overlay is selected)

orGPIRS #2 (High Speed)


10A=TP9AB=TP9B

Not UsedOr


7A=MP12CB=MP12D

Not Used : � 6��!

9A=TP9CB=TP9D

Not Used ��








Alternate GPSSpeed



Use if input is ARINC 743and not ARINC 743A 91, 125


Use if Nav Mode label 266is available 125

Allied Signal, Inc.


Discrete Inputs Worksheet Falcon 2000



REQUIRED

Self-Test MP9A Momentary Ground = Self Test;Open = Normal ;"#$� ��

Landing Gear MP9B Ground = Gear Down; Open = Gear Up ��!�� "��% � �� 8 � �(�!

Flap Override MP9C Ground = Flap Override;Open = Not Flap Override �� '�� )��

Glideslope Cancel MP9D Momentary Ground = Cancel;Open = Normal "*� ��,��


MP14B Ground = Inhibit; Open = Normal ��%%�� ,��

OPTIONAL





��,��






��


NOT USED


MP2D N/A Open

TP1A N/A Open

TP1B N/A Open

TP4C N/A Open

MP5D N/A Open

TP15A N/A Open

TP15B N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open

Allied Signal, Inc.





REQUIRED


�� #6��

6#*":� #��5 �� %&

Landing Gear MP9B Ground = Gear Down; Open = Gear Up ��!�� "��% � �� 8 � �(�!

Flap Override MP9C Ground = Flap Override;Open = Not Flap Override �� (�� '�� )��

Glideslope Cancel MP9D Momentary Ground = Cancel;Open = Normal "*� ��,��



OPTIONAL





��,��






��




NOT USED


MP2D N/A Open

TP4C N/A Open

MP5D N/A Open

TP15A N/A Open

TP15B N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet Falcon 2000

SERIAL INTERFACES FOR AIRCRAFTTYPES

SerialOutput

ChannelPins

91Connections

TX453-1A=TP3AB=TP3B Left side picture bus �� 4'�

TX453-2A=TP3CB=TP3D Right side picture bus �� 4'�

TX429-1Low Speed

A=MP1CB=MP1D ICD Appendix E label sets: E-1/2/3/5/6/17 ��#� % � 6

TX429-2Low Speed

A=TP2AB=TP2B ICD Appendix E label sets: E-1/2/3/5/6/17 ��#� % � 6

SERIAL INTERFACES FOR AIRCRAFTTYPES

SerialOutput

ChannelPins

125Connections


TX453-2A=TP3CB=TP3D Right side picture bus �� 4'� $5*��%%�� %��

TX429-1Low Speed

A=MP1CB=MP1D ICD Appendix E label sets: E-1/2/3/5/6/9/12 � 6

TX429-2Low Speed

A=TP2AB=TP2B ICD Appendix E label sets: E-1/2/3/5/6/9/12 : � 6��!

Allied Signal, Inc.


Discrete Outputs Worksheet Falcon 2000


Lamp 91

MP15D Glideslope Cancel N/A �+,�% "*� ��,�� +�

MP3D All GPWS Cautions Yes �� #'� 1�� : /�<&

MP7B All GPWS Warnings (“Pull Up”) Yes �� #'� 1�� : /�<&

TP12C Spare Yes �� #'� 1�� : /�<&

TP12A Spare Yes �� #'� 1�� : /�<&



TP10D Spare N/A : � 6��!

MP14C Spare N/A : � 6��!


MP7C GPWS Monitor N/A �� #'� 1�� : /�<&

TP12D Windshear Monitor N/A �� #'� 1�� : /�<&

TP11B Terrain Not Available N/A �� #'� 1�� : /�<&


Lamp 125


MP3DWhen OR’ed with TP11A is all

GPWS Cautions Yes ��*�� +,�% ":� #��5 ��+�

MP7BWhen diode OR’ed with TP4D

is all GPWS WarningsYes ��*�� ! #�� 6� ��+��

TP12C Windshear Caution Yes #%�+�%� '��

TP12A Windshear Warning Yes #%�+�%� '��


TP4D Terrain Awareness Warning Yes ��*�� ! #�� 6� ��+��



TP11A Terrain Awareness Caution Yes ��*�� +,�% ":� #��5 ��+��

MP7C GPWS Monitor N/A �+,�% "#$� '�� +�

TP12D Windshear Monitor N/A �+,�% $��!��% '�� +�


Allied Signal, Inc.


A-7.3 Falcon 50


Aircraft Type 82 94

Description With Pro Line 2 Integrated Pro Line 4



ADC Single (ARINC 429 or ARINC 575)

AHRS N/A (optional)Dual

FMC Single (High Speed or Low Speed) N/A

IOC N/A (optional) Dual

IRS Dual (dual AHRS optional) N/A

LRRA N/A Single

Analog AOA

Analog RA

Analog G/S

Single N/A


SingleExternal GPS

Single GPS

Dual ExternalGPS

Dual GPS

PP

IN 7


Dual Wx Control Panel Buses(use for Display 1)

No Dual EFIS or IOC inputsN/A

PP

IN 9

Dual RA N/A Dual LRRA

Alternate DisplayBuses

Dual EFIS (use for Display 2)No IOC inputs; No Optional Input Select

OrDual IOC (use for Display 3)

No EFIS inputs; No Optional Input SelectOr

Dual WX Cntrl Panel Buses(see Optional Input Select)

Alternate ILS BusSingle digital ILS

Replaces analog Glideslope

N/A

FEATURES



No


ARINC 429 DH No Yes




Alert Volume High



No

Windshear Yes

Allied Signal, Inc.



PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-202

and on



No auto ranging

Defaultwith +-60o


2-208

and on

Honeywell EDZ805,5x6



Honeywell Yes No No No MP3A

3-208

and on



No auto ranging

Defaultwith +-60o

limitNo Yes No No MP15D


1-204

and on





Fan modewith +-60o

limit

Based ondisplay

controllerstrapping

N/A No No Open

2-208

and on





Fan modewith +-90o

limit

Based ondisplay

controllerstrapping

N/A No No MP3A




1 (TP10A) 2 (TP10B) 3 (TP10C)

82 MP15D MP15D MP3A

94 TP12A MP3D MP3A

Allied Signal, Inc.




AnalogInputChannel

Pins82

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ALT 55 with Validity Flag)(will use ARINC 552 if Alt RA #1 selected)



3+ = TP13C- = TP13D



4+ = TP14C- = TP14D

Vane AOA, PotentiometerFormat: 0 - 10 VDC

Offset: 49.0o

Gain = -5.5o



T P2D(10 VDC)

T P14C (+)

T P14D (-)

There are no analog inputs for Aircraft Type 94.



82Selected?

Default ALT 55



Allied Signal, Inc.




InputChannel

Pins82

Connections

3A=MP11AB=MP11B


orNot Used

12A=TP8CB=TP8D

Not UsedOr


11A=TP8AB=TP8B

FMC (Low Speed) 1

orNot Used

2A=MP10CB=MP10D

Not UsedOr


18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D

Not UsedOr


1A=MP6AB=MP6B

IRS #1 (High Speed) (Preferred)Or

AHRS #1 (High Speed) (Available –208 and on)

13A=TP5AB=TP6A

IRS #2 (High Speed) (Preferred)Or

AHRS #1 (High Speed) (Available –208 and on)

8A=MP13AB=MP13B

Not UsedOr


5A=MP10AB-MP10B

Not Used (If no display)Or

Wx Control Panel Bus #1 (Low Speed) (Available –202 and on)Select Display 1

OrEFIS Bus #1 (Low Speed) (Available –208 and on)

(Multifunction SG Left Bus) – Select Display 2Or

IOC Bus #1 (High Speed) (Available –208 and on)Select Display 3

7A=MP12CB=MP12D

Not Used (If no display)Or

Wx Control Panel Bus 2 (Low Speed) (Available –202 and on)Select Display 1

OrEFIS Bus #2 (Low Speed) (Available –208 and on)(Multifunction SG Right Bus) – Select Display 2

OrIOC Bus #2 (High Speed) (Available –208 and on)

Select Display 3





Allied Signal, Inc.



InputChannel

Pins82

Connections




ARINC 429 Interface Modification Options Worksheet Falcon 50



Alternate GPSSpeed



-206 and on GPS #1, #2 Use if input is ARINC 743and not ARINC 743A 82

16ConfigurationOption 2 -2-4 and on FMC Use if Nav mode label 266

is available 82

Allied Signal, Inc.




InputChannel

Pins94

Connections

4A=MP12AB=MP12B


12A=TP8CB=TP8D


1A=MP6AB=MP6B

AHRS Bus #1 (High Speed) ��


5A=MP10AB-MP10B

Not UsedOr

GPS #1 (High Speed)

11A=TP8AB=TP8B

Not UsedOr



3A=MP11AB=MP11B


8A=MP13AB=MP13B

LRRA Bus #1 (Low Speed) ��

10A=TP9AB=TP9B

Not UsedOr


6A=MP11CB=MP11D

Not Used ��

7A=MP12CB=MP12D

Not Used ��

9A=TP9CB=TP9D

Not Used ��

14A=TP1CB=TP1D

Not Used ��






ARINC 429 Interface Modification Options Worksheet Falcon 50






ConfigurationOption 2 - IOC #1, #2 Use if Nav mode label 302

is NOT available 94

Allied Signal, Inc.





REQUIRED


�� !

"#$� $�%� �� %&



'�� '�� ! ��

� �(�� "#$� '�� )��


"*� �� +,�%

"#$� ��%� �� %&



ILS Select 2 MP14A Ground = ILS Selected; Open = Not Selected �� ! � � � ��




Flaps Position #2 (20 o) TP7B +28 V = Selected; 0 V = Not Selected '�� -� ��

Flaps Position #3 (48 o) TP7C +28 V = Selected; 0 V = Not Selected '�� /=� ��

OPTIONAL





��,��









��

NOT USED


MP1A N/A Open

MP2D N/A Open

TP15C N/A Open

TP15D N/A Open

TP7D N/A Open1 RA Valid not required if Alternate RA #2 (digital RA) used.2 ILS Select and Glideslope Valid not required if digital ILS provided. (EGPWS will automatically use digital ILS ifprovided.)3 Not used with Display 2 (Honeywell EDZ 605/805 EFIS).

Allied Signal, Inc.





REQUIRED


�� !

"#$� $�%� �� %&


Flap Override MP9C Ground = Flap Override;Open = Not Flap Override

'�� '�� ! ��

� �(�� "#$� '�� )��


"*� �� +,�%

"#$� ��%� �� %&


MP14B

Ground = Inhibit; Open = Normal �� %%�� ,��

OPTIONAL





��,��




Steep Approach #1 MP1A Ground = Enabled; Open = Disabled 2��3 ��

Steep Approach #2MP14

A Ground = Selected; Open = Not Selected ��%�%�� "% ��!

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Normal �(�� % ��

��

NOT USED


MP2D N/A Open

TP1A N/A Open

TP1B N/A Open

TP4C N/A Open

MP5D N/A Open

TP15A N/A Open

TP15B N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet Falcon 50


ChannelPins

82Connections


TX453-2A=TP3CB=TP3D Right side picture bus

�� 4'� $5*��%%��

%��

TX429-1Low Speed


� 6 �7 � 8 9

�%

�" �7 � 8 9

TX429-2Low Speed

A=TP2AB=TP2B ICD Appendix E label sets: E-1/2/3/5/6/9/12 : � 6��!


ChannelPins

94Connections



TX429-1Low Speed

A=MP1CB=MP1D ICD Appendix E label sets: E-1/2/3/5/6/17

TX429-2Low Speed

A=TP2AB=TP2B ICD Appendix E label sets: E-1/2/3/5/6/17

Allied Signal, Inc.


Discrete Outputs Worksheet Falcon 50


Lamp 82



MP7BAll


Yes ��*�� ! "#$� ��+��

TP12C Windshear Caution Yes $��!��% �� +�

TP12A Windshear Warning Yes $��!��% $�%�� +�



TP10D Terrain Display Discrete #1 N/A �� $5*��%%��

MP14C Terrain Display Discrete #2 N/A �� $5*��%%��





1 Connection is “Open” for Display 2 (Honeywell EDZ 605/805 EFIS).






Lamp 94


MP3D All GPWS Cautions Yes ��*�� +,�% "*� ��+��

MP7B All GPWS Warnings (“Pull Up”) Yes ��*�� ! "#$� ��+��






MP14C Terrain Display Discrete #2 N/A ��





Allied Signal, Inc.


A-7.4 Falcon 50 EX



Description Integrated Pro Line 4 Bolt-on Pro Line 4



ADC DualFMC N/A (via IOC) DualIOC DualIRS Dual (or single or dual GPIRS)

LRRA Single


SingleExternal GPS

Single GPSNo GPIRS

Dual ExternalGPS

Dual GPSNo GPIRS

Single GPIRSOverlay

Single GPIRSReplaces dual IRS inputs, no GPS

Dual GPIRSOverlay

Dual GPIRSReplaces dual IRS inputs, no GPS

PP

IN 7


N/A See ARINC 429 Interface Modifications Options

PP

IN 9

Dual RA Dual LRRA

FEATURES



No


ARINC 429 DH Yes


Lamp Format Type 2


Alert Volume High



No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Falcon 50 EX

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-202

and on





Fan modewith +-60o

limit

Based ondisplay

controllerstrapping

N/A No No Open

2-208

and on





Fan modewith +-90o

limit

Based ondisplay

controllerstrapping

N/A No No MP3A


1-105

and on



No auto ranging

Defaultwith +-60o





1 (TP10A) 2 (TP10B) 3 (TP10C)

92 MP7B MP3D MP3A

126 TP12A TP4D MP3A



Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Falcon 50 EX


InputChannel

Pins92 126

Connections

4A=MP12AB=MP12B


12A=TP8CB=TP8D


6A=MP11CB=MP11D

Not Used FMC #1 (High Speed)

15A=TP4AB=TP4B Not Used FMC #2 (High Speed)

5A=MP10AB-MP10B

Not UsedOr


11A=TP8AB=TP8B

Not UsedOr



3A=MP11AB=MP11B


1A=MP6AB=MP6B



13A=TP5AB=TP6A

IRS #2 (High Speed)(IRS #2 not used if Single GPIRS Overlay is selected)

orGPIRS #2 (High Speed)


10A=TP9AB=TP9B

Not UsedOr


7A=MP12CB=MP12D

Not Used ��

9A=TP9CB=TP9D

Not Used ��





ARINC 429 Interface Modification Options Worksheet Falcon 50 EX



Alternate GPSSpeed -105 and on GPS #1, #2 Low Speed bus(es) 92, 126





Allied Signal, Inc.


Discrete Inputs Worksheet Falcon 50 EX



REQUIRED

Self-Test MP9A Momentary Ground = Self Test;Open = Normal ;"#$� ��

Landing Gear MP9B Ground = Gear Down; Open = Gear Up ��!�� "��% � �� ! � �(�! ��

Flap Override MP9C Ground = Flap Override;Open = Not Flap Override �� '�� )��

Glideslope Cancel MP9D Momentary Ground = Cancel; Open =Normal "��!�� ,��



OPTIONAL





��,��




Steep Approach #1 MP1A Ground = Enabled; Open = Disabled 2��3 ��

Steep Approach #2 MP14A Ground = Selected; Open = Not Selected ��%�%�� "% ��!

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Normal �(�� % ��

��

NOT USED


MP2D N/A Open

TP1A N/A Open

TP1B N/A Open

TP4C N/A Open

MP5D N/A Open

TP15A N/A Open

TP15B N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open

Allied Signal, Inc.





REQUIRED


;"#$� �� #6��

6#*":� #��5 �� %&


Flap Override MP9C Ground = Flap Override; Open = Not FlapOverride �� '�� )��




OPTIONAL





��,��






��


Display Select 1 TP1A Momentary Ground Switch �� %%��

Display Select 2 TP1B Momentary Ground Switch �� %%��

NOT USED


MP2D N/A Open

TP4C N/A Open

MP5D N/A Open

TP15A N/A Open

TP15B N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet Falcon 50 EX


ChannelPins

92Connections



TX429-1Low Speed

A=MP1CB=MP1D ICD Appendix E label sets: E-1/2/3/5/6/9/17 ��#� % � 6

TX429-2Low Speed

A=TP2AB=TP2B ICD Appendix E label sets: E-1/2/3/5/6/9/17 ��#� % � 6


ChannelPins

126Connections

TX453-1A=TP3AB=TP3B Left side picture bus �� 4'� ��

TX453-2A=TP3CB=TP3D Right side picture bus �� 4'� ��

TX429-1Low Speed


TX429-2Low Speed


Allied Signal, Inc.


Discrete Outputs Worksheet Falcon 50 EX


Lamp 92


MP3D Spare Yes �� #'� 1�� : /�<&

MP7B Spare Yes �� #'� 1�� : /�<&

TP12C Spare Yes �� #'� 1�� : /�<&

TP12A Spare Yes �� #'� 1�� : /�<&






MP7C Spare N/A �� #'� 1�� : /�<&

TP12D Spare N/A �� #'� 1�� : /�<&

TP11B Spare N/A �� #'� 1�� : /�<&


Lamp 126


MP3DWhen diode OR’ed with

TP11A is all GPWS Cautions Yes ��*�� +,�% ":� #��5 ��+�


is all GPWS WarningsYes ��*�� ! #�� 6� ��+��

TP12C Windshear Caution Yes � #%�+�%� '�� +��%

TP12A Windshear Warning Yes � #%�+�%� '�� +��%






MP7C GPWS Monitor N/A �+,�% "#$� '�� +�

TP12D Windshear Monitor N/A �+,�% $��!��% '�� +�


Allied Signal, Inc.


A-7.5 Falcon 900/900B


Aircraft Type 75

Description Falcon 900/900B




FMC Single (High Speed or Low Speed)

ILS Single

IRS Dual

AOA Left and Right

RA Single


SingleExternal GPS

Single GPS

Dual ExternalGPS

Dual GPS

PP

IN 7


Dual EFISRequired for displays

Alternate RAFormat

Single LRRAReplaces analog RA

Alternate ILSFormat

Single digital ILSReplaces analog ILS

FEATURES



No


ARINC 429 DH No


Lamp Format Type 1


Alert Volume High



No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Falcon 900/900B

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


Peaks1

Avail.

PPIN 18(MP15A)

Strapping


1-101

and on

Honeywell SPZ8000,Integrated, 5x6







1 (TP10A) 2 (TP10B) 3 (TP10C)

75 MP3D MP3A MP3A



AnalogInputChannel

Pins75

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ARINC 552 with Validity Discrete)(use Alt. RA Format #1 for ALT 55)


2+ = TP14A- = TP14B

Right Vane AOA,Potentiometer

Format: 0-10 VDCOffset = 46.5o

Gain = -5.50Electrical Range = 55o


T P2D(10 VDC)

T P14A (+)

T P14B (-)

3+ = TP13C- = TP13D



4+ = TP14C- = TP14D

Left Vane AOA, PotentiometerFormat: 0-10 VDC

Offset = 46.5o

Gain = -5.50Electrical Range = 55o


T P2D(10 VDC)

T P14C (+)

T P14D (-)



75Selected?

Default ARINC 552



Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Falcon 900/900B


InputChannel

Pins75

Connections

3A=MP11AB=MP11B


OrNot Used

12A=TP8CB=TP8D

Not UsedOr


2A=MP10CB=MP10D

Not UsedOr

EFIS #1 (MG Multifunction SG Left Bus) (Low Speed

9A=TP9CB=TP9D

Not UsedOr

EFIS #2 (MG Multifunction SG Right Bus) (Low Speed

4A=MP12AB=MP12B

FMC #1 (Low Speed) 1

OrNot Used

11A=TP8AB=TP8B

Not UsedOr


18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D

Not UsedOr

ILS #1 (Low Speed)


13A=TP5AB=TP6A IRS Bus #2 (High Speed) ��

8A=MP13AB=MP13B

Not UsedOr


5A=MP10AB-MP10B

Not Used ��




15A=TP4AB=TP4B

Not Used ��

16A=TP5CB=TP5D

Not Used ��





Connections

Alternate GPSSpeed





- FMC #1Use if Nav Mode label 266

is available 75

Allied Signal, Inc.


Discrete Inputs Worksheet Falcon 900/900B



REQUIRED


�� !

"#$� $�%� �� %&



'�� '�� ! ��

� �(�� "#$� '�� )��


"*� �� +,�%

"#$� ��%� �� %&

ILS Select 2 MP14A Ground = ILS Selected; Open = NotSelected �� %%�� ,��


MP14B Ground = Inhibit; Open = Normal �� ! � � � ��




Flaps Position #2 (7 o) TP7B +28 V = Selected; 0 V = Not Selected '�� >� ��

Flaps Position #3 (20 o) TP7C +28 V = Selected; 0 V = Not Selected '�� -� ��

Flaps Position #4 (40 o) TP7D +28 V = Selected; 0 V = Not Selected '�� /-� ��

OPTIONAL





��,��







��

NOT USED


Display Select 1 TP1A DO NOT USE Open

Display Select 2 TP1B DO NOT USE Open

MP1A N/A Open

MP2D N/A Open

TP15C N/A Open


Allied Signal, Inc.


Serial Outputs Worksheet Falcon 900/900B


ChannelPins

75Connections

TX453-1A=TP3AB=TP3B

Left side picture bus to symbol generator port � �� " �7 4"

TX453-2A=TP3CB=TP3D

Right side picture bus to symbol generator port � �� " �7 4"

TX429-1Low Speed

A=MP1CB=MP1D

ICD Appendix E label sets: E-1/2/3/5/6/9/12 � �� " �8�7 4"

TX429-2Low Speed

A=TP2AB=TP2B

ICD Appendix E label sets: E-1/2/3/5/6/9/12 ��

Discrete Outputs Worksheet Falcon 900/900B


Lamp 75



MP7BAll


Yes ��*�� ! "#$� ��+��







TP11A Spare N/A : � 6��!








Allied Signal, Inc.


A-7.6 Falcon 900 EX



Description Falcon 900 EX Falcon 900 EX - No Display



ADC

DAU

FMC

Dual

FWC Triple Dual (#2 and #3)

IRS Dual (or single or dual GPIRS)

Analog RA Single


SingleExternal

GPS

Single GPSNo GPIRS

PP

IN 7

DualExternal

GPS

Dual GPSNo GPIRS

PP

IN 9

Dual RA Dual Analog RA

FEATURES



No


ARINC 429 DH Yes


Lamp Format Type 2


Alert Volume High

Steep Approach Discrete and/or Digital Discrete


No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Falcon 900 EX

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-105

and on




Honeywell

Based ondisplay

controllerstrapping

(label171, bit

18)

N/A No No Open

Aircraft Type: 157

1-105

and onNo Display N/A N/A N/A N/A N/A Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

93 TP12C MP3D MP3A

157 TP12C MP3D MP15D



AnalogInputChannel

Pins93, 157

Connections


2+ = TP14A- = TP14B

Not UsedOr





Alternate Radio Altimeter formats are not supported by these aircraft.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Falcon 900 EX


InputChannel

Pins93 157

Connections

4A=MP12AB=MP12B


12A=TP8CB=TP8D


2A=MP10CB=MP10D

DAU #1 (Low Speed) ��6 �

3A=MP11AB=MP11B DAU #2 (Low Speed) ��6 �

8A=MP13AB=MP13B FMC #1 (Low Speed) '4 �

11A=TP8AB=TP8B FMC #2 (Low Speed) '4 �

6A=MP11CB=MP11D FWC #1 (Low Speed) Not Used

7A=MP12CB=MP12D FWC #2 (Low Speed) '$ �

9A=TP9CB=TP9D FWC #3 (Low Speed) '$ 9

5A=MP10AB-MP10B

Not UsedOr

GPS #1 (High Speed)

14A=TP1CB=TP1D

Not UsedOr


1A=MP6AB=MP6B



13A=TP5AB=TP6A




15A=TP4AB=TP4B

Not Used ��

16A=TP5CB=TP5D

Not Used ��

17A=TP11CB=TP11D

Not Used ��

18A=MP6CB=MP6D

Not Used ��




Connections

Alternate GPSSpeed





-204 and on FMC #1,#2Use if Nav Mode label 266

is available 157

Allied Signal, Inc.





REQUIRED

Landing Gear MP9B Ground = Gear Down; Open = Gear Up Landing Gear Down and Locked switch

Radio Altimeter Valid #1 TP15A +28V = Valid; 0V = Not Vaild ��!� �� )��!��

Flaps Position #2 (40 o) TP7D +28V = Selected; 0V = Not Selected '�� /-� ��

OPTIONAL





��,��






��

Radio Altimeter Valid #2 TP15B +28V = Valid; 0V = Not Vaild ��!� �� )��!��


NOT USED


Self-Test MP9A Momentary Ground = Self Test;Open = Normal �� : /�< ��! ��!&

Flap Override MP9C Ground = Flap Override; Open = NotFlap Override �� : /�< ��! ��!&

Glideslope Cancel MP9D Momentary Ground = Cancel; Open =Normal �� : /�< ��! ��!&


MP14B Ground = Inhibit; Open = Normal �� : /�< ��! ��!&

MP2D N/A ��

TP1A N/A Open

TP1B N/A Open

TP4C N/A Open

MP5D N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

Allied Signal, Inc.





REQUIRED


�� #6��

6#*":� #��5 �� %&


Flap Override MP9C Ground = Flap Override; Open = Not FlapOverride '�� 1�%%�!� ��




Radio Altimeter Valid #1 TP15A +28V = Valid; 0V = Not Vaild ��!� �� )��!��

Flaps Position #2 (40 o) TP7D +28V = Selected; 0V = Not Selected '�� /-� ��

OPTIONAL





��,��






��

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Normal ��!� �� )��!��

Radio Altimeter Valid #2 TP15B +28V = Valid; 0V = Not Vaild 2��3 ��

NOT USED


MP2D N/A Open

TP1A N/A Open

TP1B N/A Open

TP4C N/A Open

MP5D N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet Falcon 900 EX


ChannelPins

93Connections

TX453-1A=TP3AB=TP3B Left/Right multiplexed picture bus to DU-870 #1 & #2 (port 2)

�6 �4'� �&

�6 �4'� �&

TX453-2A=TP3CB=TP3D Not Used ��

TX429-1Low Speed

A=MP1CB=MP1D ICD Appendix E label sets: E-1/2/3/5/6/9/12 ��6 �

TX429-2Low Speed



ChannelPins

157Connections

TX453-1A=TP3AB=TP3B

Not Used ��


TX429-1Low Speed

A=MP1CB=MP1D ICD Appendix E label sets: E-1/2/3/5/6/9/12 ��6 �

TX429-2Low Speed


Allied Signal, Inc.


Discrete Outputs Worksheet Falcon 900 EX


Lamp 93

MP15D Glideslope Cancel N/A �� 4'� 1�� : /�<&

MP3D All GPWS Cautions Yes �� #'� 1�� : /�<&

MP7B All GPWS Warnings (“Pull Up”) Yes �� #'� 1�� : /�<&

TP12C Windshear Caution Yes �� #'� 1�� : /�<&

TP12A Windshear Warning Yes �� #'� 1�� : /�<&






MP7C GPWS Monitor N/A �� ;� �� 1�� : /�<&

TP12D Windshear Monitor N/A �� ;� �� 1�� : /�<&

TP11B Terrain Not Available N/A �� ;� �� 1�� : /�<&


Lamp 157



TP11A is all GPWS Cautions Yes ��*�� +,�% ":� #��5 ��+��


is all GPWS Warnings Yes ��*�� ! #�� 6� ��+��

TP12C Spare Yes ��

TP12A Spare Yes ��






MP7C GPWS Monitor N/A �� ;� �� 1�� : /�<&

TP12D Windshear Monitor N/A �� ;� �� 1�� : /�<&

TP11B Terrain Not Available N/A �� 4'� 1�� : /�<&

Allied Signal, Inc.


A-8 DeHavilland

A-8.1 Dash 8-400


Aircraft Type 88

Description DeHavilland Dash 8-400



IOP Dual


None None

FEATURES



No



Yes


Lamp Format Type 1


Alert Volume High



No

Windshear No

Note: The –208 certification of MK V EGPWC installed in the DeHavilland Dash 8-400 is forbasic features only without displays. T errain Awareness and Display should be disabledvia Program Pin.

Allied Signal, Inc.


Display Options & Peaks Availability Dash 8-400

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping

Aircraft Type: 88

1-208

and onNo Display1 N/A N/A N/A N/A N/A Open

Note: Prior to version –208, the display option for Program Pin State 1 is the required display. Program Pin 18 wasadded in version –208.1 Display will not be available until version –210.



1 (TP10A) 2 (TP10B) 3 (TP10C)

88 Open MP3D MP3A




There are no alternate radio altimeter formats for this Aircraft Type.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Dash 8-400


ARINC429

InputChanne

l

Pins88

Connections

1A=MP6AB=MP6B IOP #1 (High Speed) ��

10A=TP9AB=TP9B IOP #2 (High Speed) ��


3A=MP11AB=MP11B

Not used ��

4A=MP12AB=MP12B

Not used ��

5A=MP10AB-MP10B

Not used ��

6A=MP11CB=MP11D

Not used ��






13A=TP5AB=TP6A Not used ��







There are no ARINC 429 interface modifications for this Aircraft Type.

Allied Signal, Inc.


Discrete Inputs Worksheet Dash 8-400



REQUIRED

Landing Flap Switch 10 MP8D Ground = Selected; Open = Not Selected � ��


� ��

�� ! ��!"

Landing Flap Switch 15 MP9B Ground = Selected; Open = Not Selected � �� #� ��

Flap Override MP9C Ground = Landing Flap Override;Open = Not Landing Flap Override

� ��

��$�� %�& ��


�'� (�� )*+!

�� ) !� ��!"

Landing Flap Switch 35 MP14A Ground = Selected; Open = Not Selected � �� ,#� ��


MP14B Ground = Inhibit; Open = Normal ) � �� !!�� +��

OPTIONAL

Glideslope Inhibit MP1B Ground = Inhibit; Open = Not Inhibit �-� .��$��!� ��

Mode 6 Volume Control MP2A Ground = Low Volume; Open = Normal )�!�!�� !��

Decision Height MP5C Ground = <DH; Open = >DH �� ) � &/ +�0 ��

Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal�� !�0 �! �!��1 '� ��

��+��

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled )�!�!�� !��

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Normal 2&��3 ��

Steep Approach #1 TP4C Ground = Enabled; Open = Disabled )�!�!�� !��

Steep Approach #2 MP5D Ground = Selected; Open = Not Selected(��$�� )��!��

��


MP15A 28V = Audio Suppress; 0V = Normal (��$�� )�� !��

NOT USED


MP1A N/A ��

MP2D N/A ��

TP1A N/A ��

TP1B N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.


Serial Outputs Worksheet Dash 8-400


ChannelPins

88Connections

TX453-1A=TP3AB=TP3B

Terrain display data to left display switching relay 4��

TX453-2A=TP3CB=TP3D

Terrain display data to right display switching relay 4��

TX429-1Low Speed

A=MP1CB=MP1D

Transmits ICD Appendix E label sets: 1/2/5/6/9/12

TX429-2Low Speed

A=TP2AB=TP2B

Transmits ICD Appendix E label sets: 1/2/5/6/9/12



FlashingLamp 88

MP15D Glideslope Cancel N/A -��'��0�� '� (�� -�*��


MP7BAll


No -��'��0�� -�*��



TP12B Audio On N/A �()� ��+��


TP10D Terrain Display Discrete #1 N/A -�� !!��

MP14C Terrain Display Discrete #2 N/A ��0�� !!��

TP11A Below G/S Caution No -��'��0�� )*+! � �� -�*��

MP7C GPWS Monitor N/A )*+! �� 4�� -�*�

TP12D Terrain Not Available N/A �!!�� 4�� )1�� + -�*�

TP11B Terrain INOP N/A �!!�� 4�� -�*�



MP3D All GPWS Cautions No -��'��0�� )*+! �� -�*��

MP7B All GPWS Warnings (“Pull Up”) No -��'��0�� 5� -�*��

Allied Signal, Inc.


A-9 Dornier

A-9.1 Do-328 Jet


Aircraft Type 35

Description Do-328 Jet



ADC Dual

FMC Single

FWC Dual

IRS Dual (Dual AHRS optional)

Analog RA Single


SingleExternalGPS

Single GPS

DualExternalGPS

Dual GPS

PP

IN 7


Dual FMC

PP

IN 9


Alternate AHRSInput

Dual AHRSReplaces Dual IRS

FEATURES

Aircraft Class Commercial


No



Yes


Lamp Format Type 2


Alert Volume High



No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Do-328

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-206

and on




Honeywell

Based ondisplay

controllerstrapping

(label171, bit

18)

N/A No No Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

35 MP3D MP7B Open



AnalogInputChannel

Pins35

Connections

1+ = TP13A- = TP13B Radio Altimeter #1 (ARINC 552 with Validity Discrete) ��

2+ = TP14A- = TP14B

Not UsedOr



4+ = TP14C- = TP14D

Not Used ��


Alternate RA formats are not supported by this Aircraft Type.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Do-328


ARINC429

InputChannel

Pins35

Connections

3A=MP11AB=MP11B

ADC #1 (Low Speed) � � ��

13A=TP5AB=TP6A ADC #2 (Low Speed) � � ��

9A=TP9CB=TP9D

FMC #1 (LH-IAC) (Low Speed) ��

15A=TP4AB=TP4B

Not UsedOr

FMC #2 (RH-IAC) (Low Speed)

6A=MP11CB=MP11D

FWC #1 (LH-IAC) (Low Speed) ��

5A=MP10AB-MP10B

FWC #2 (RH-IAC) (Low Speed) ��

17A=TP11CB=TP11D

Not usedor


18A=MP6CB=MP6D

Not usedor


1A=MP6AB=MP6B



14A=TP1CB=TP1D






8A=MP13AB=MP13B

Not Used ��

10A=TP9AB=TP9B

Not Used ��

11A=TP8AB=TP8B

Not Used ��






Alternate GPSSpeed

-206 and on GPS #1, #2 Low Speed bus(es) 35



3516


-206 and on FMC #1,#2Use if Nav Mode label 266

is available 35

Allied Signal, Inc.


Discrete Inputs Worksheet Do-328



REQUIRED

Self-Test MP9A Momentary Ground = Self-Test;Open = Normal ��

Landing Gear MP9B Ground = Landing Gear Down;Open = Not Landing Gear Landing Gear Down and Locked switch

Landing Flap MP9C Ground = Landing Flap; Open = NotLanding Flap

�� !��

�� "�##��


$%� �� &''��( �� )*�#

$+�� #� ��'��#,


MP2D Ground = Inhibit; Open = Normal �� ##�� -��*��

Radio Altimeter #1 Valid TP15A +28 V = Valid; 0 V = Fail �� .��(

OPTIONAL

Glideslope Inhibit MP1B Ground = Inhibit; Open = Not Inhibit -/� 0��1��'#� ��

Mode 6 Volume Control MP2A Ground = Low Volume; Open = Normal ��#�#�� $#�'��

Decision Height MP5C Ground = <DH; Open = >DH �� 2 *'3 �'��'�

Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal�� #��3 �# �#��"� �%� �'��

��*�� '��'�

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled ��#�#�� $#�'��


MP8D Momentary Ground = Audio Suppress;Open = Normal ��1�� $+�� '�� '��#� ��

Steep Approach #1 MP1A Ground = Enabled; Open = Disabled ��#�#�� $#�'��

Steep Approach #2 MP14B Ground = Selected; Open = Not Selected��1�� #��

��

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Normal 4 ��5 ��

Radio Altimeter #2 Valid TP15B +28 V = Valid; 0 V = FailRequired if Dual RA selected �� .��(

NOT USED


MP14A N/A ��

TP1A N/A ��

TP1B N/A ��

TP4C N/A ��

MP5D N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.


Serial Outputs Worksheet Do-328


ChannelPins

35Connections

TX453-1A=TP3AB=TP3B

Left/right side picture bus to DU-870 #1 & #2 (port 2) &�� ,

&�� ,


TX429-1Low Speed

A=MP1CB=MP1D ICD Appendix E label sets: E-1/2/3/5/6/8/11 -��

TX429-2Low Speed

A=TP2AB=TP2B

ICD Appendix E label sets: E-1/2/3/5/6/8/11 -��



FlashingLamp 35

MP15D Glideslope Cancel N/A ��

MP3D All GPWS Cautions No �� &+� "�� -�� 6�7,

MP7B All GPWS Warnings (“Pull Up”) No �� &+� "�� -�� 6�7,

TP12C Windshear Caution No �� &+� "�� -�� 6�7,

TP12A Windshear Warning No �� &+� "�� -�� 6�7,

TP12B Audio On N/A �� -��*��





MP7C GPWS Monitor N/A �� &8-�� "�� -�� 6�7,

TP12D Windshear Monitor N/A �� &8-�� "�� -�� 6�7,

TP11B Terrain Not Available N/A �� &)� "�� -�� 6�7,

Allied Signal, Inc.


A-10 Douglas

A-10.1 DC8-72


Aircraft Type 130

Description DC-8-72 with Collins Display




Display Bus

FMC

ILS

IRS

Localizer

RA

Single


SingleExternal

GPSSingle GPS

DualExternal

GPSDual GPS

PP

IN 7


Dual FMC, IRS

PWS Option1

Single Wx Radar Hazard Bus

PP

IN 1

5

PWS Option2

Dual Wx Radar Hazard Buses

PP

IN 9

Dual RADual Analog RA

(Dual digital LRRA if Alternate RA Format #2 is selected)

Alternate ILSFormat

Single digital ILS (will use if provided)Replaces analog ILS and Localizer inputs

Alternate RAFormat

Single digital LRRAReplaces analog RA inputs

FEATURES



No


ARINC 429 DH No


Lamp Format Type 1


Alert Volume Low



No

Windshear No

Allied Signal, Inc.


Display Options & Peaks Availability DC8-72

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-208

and on

Collins ProLine 2(non-integrated), 5x6(Bus type: ARINC 708Standard Data Format)

No auto ranging

Defaultwith +-60o





1 (TP10A) 2 (TP10B) 3 (TP10C)

130 MP15D Open MP15D



AnalogInputChannel

Pins130

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ALT 55 with Validity Discrete)(use Alt. RA Format #1 for ARINC 552)


2+ = TP14A- = TP14B

Not UsedOr

Radio Altimeter #2 (ALT 55 with Validity Discrete)

3+ = TP13C- = TP13D



4+ = TP14C- = TP14D

Localizer (ARINC 547 with Validity Flag & ILS Select)Or




130Selected?

Default ALT 55



Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet DC8-72


InputChannel

Pins130

Connections

3A=MP11AB=MP11B


Or Not Used

12A=TP8CB=TP8D

Not UsedOr ADC #1 ARINC 575 (Low Speed) 1

2A=MP10CB=MP10D

Display Bus (Radar Indicator Bus) (Low Speed) ��

4A=MP12AB=MP12B FMC #1 (Low Speed) ��

11A=TP8AB=TP8B

Not UsedOr FMC #2 (Low Speed)

5A=MP10AB-MP10B

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D

Not UsedOr



13A=TP5AB=TP6A

Not UsedOr


8A=MP13AB=MP13B

Not UsedOr


10A=TP9AB=TP9B

Not UsedOr


7A=MP12CB=MP12D

Not UsedOr


9A=TP9CB=TP9D

Not UsedOr






1Provide only one ADC input as indicated by bus format.




Alternate GPSSpeed






Allied Signal, Inc.


Discrete Inputs Worksheet DC8-72



REQUIRED


��

!"� "�#� ��#$

Landing Gear MP9B Ground = Gear Down; Open = Gear Up ��# ��


MP9C Ground = Landing Flap/Override;Open = Not Landing Flap/Normal

��

��%�� !"� �� &��


'� �� ()*�#

!"� (��#� ��#$


MP2B Ground = Inhibit; Open = Normal (�� ##�� *��

ILS Select 2 MP14A Ground = ILS Selected;Open = Not Selected �+� �� +��

Display Select #1 TP1A Momentary Ground Switch +�� ##��

Radio Altimeter #1Valid 1 TP15A +28 V = Valid; 0 V = Not Valid �� (�� &��

Glideslope #1 Valid 2 TP15B +28 V = Valid; 0 V = Not Valid �+� �� &��

Localizer Valid 2 TP15D +28 V = Valid; 0 V = Not Valid

OPTIONAL

Back Course Select MP1B Ground = Glideslope Inhibit; Open = NotInhibit �+� ��%��#��

Mode 6 Volume Control MP2A Ground = Low Volume; Open = Normal (�#�#�� #��

Decision Height MP5C Ground = <DH; Open = >DH �� (�� , *- ��

Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal�� #��- �# �#��.� "'� ��

��*��

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled (�#�#�� #��


MP8D Momentary Ground = Audio Suppress;Open = Normal ��%�� !"� (�� #��

Steep Approach #1 TP4C Ground = Enabled; Open = Disabled (�#�#�� #��

Steep Approach #2 MP5D Ground = Selected; Open = Not Selected ��%�� (��#��

��

Radio Altimeter #2Valid 1 TP15C +28 V = Valid; 0 V = Not Valid �� (�� / &��

NOT USED


MP1A N/A Open

MP14B N/A Open

MP2D N/A Open

TP1B N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open1 RA Valid not required if Alternate RA #2 (digital RA) used.2 ILS Select, Localizer Valid and Glideslope Valid not required if digital ILS provided. (EGPWS will automatically usedigital ILS if provided.)

Allied Signal, Inc.


Serial Outputs Worksheet DC8-72


ChannelPins

130Connections

TX453-1A=TP3AB=TP3B

Left side picture bus WX indicator (Display)

TX453-2A=TP3CB=TP3D

Not used on this installation ��

TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B




Lamp 130

MP15D Glideslope Cancel N/A ()*�# '� +�)��

MP3D Below G/S Caution Yes +��'��-�� ()*�# '� +�)��

MP7BAll


Yes +��'��-�� !"� ��)��

TP12C Spare N/A 0�� 1��

TP12A Spare N/A 0�� 1��

TP12B TCAS Inhibit N/A � (� ��*��

TP4D PWS Inhibit N/A

TP10D Terrain Display Discrete #1 N/A +�� ##��

MP14C Spare N/A 0�� 1��


MP7C GPWS Monitor N/A ()*�# !"� �0�! ��)�

TP12D Spare N/A 0�� 1��

TP11B Terrain Not Available N/A ()*�# ��##�� 0�! ��)�



MP3D All GPWS Cautions No +��'��-�� ()*�# !"� +�)��

MP7B All GPWS Warnings (“Pull Up”) No +��'��-�� !�� 1� +�)��

Allied Signal, Inc.


A-10.2 DC-9-82/-83 EFIS


Aircraft Type 139

Descriptions DC-9-82/-38 with EFIS



ADC Dual (ARINC 575)

DFGC Dual (Dual AHRS optional)

EFIS Four (Dual EFIS optional)

Analog RA

Analog GS

Localizer

Single


SingleExternal GPS

Single GPS

Dual ExternalGPS

Dual GPS

PP

IN 7


Dual AHRSReplaces Dual DFGC; No EFIS #1 and #3

PP

IN 9

Dual RA Dual analog RA

PP

IN 1

5

PWS Option1


FEATURES



No


ARINC 429 DH No


Lamp Format Type 1


Alert Volume High

Steep Approach N/A


No

Windshear No

Allied Signal, Inc.


Display Options & Peaks Availability DC-9-82/-83

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-208

and on

Honeywell EFIS(Bus type: ARINC 708Standard Data Format)

No auto ranging

Default Yes N/A No Yes Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

139 MP3D MP3A MP15D



AnalogInputChannel

Pins139

Connections

1+ = TP13A- = TP13B Radio Altimeter #1 (ARINC 552 with Validity Discrete) �( ��

2+ = TP14A- = TP14B

Not UsedOr


3+ = TP13C- = TP13D Glideslope #1 (ARINC 547 with Validity Flag & ILS Select)

4+ = TP14C- = TP14D

Localizer #1 (ARINC 547 with Validity Flag) +��2�# ��


Alternate RA formats do not apply.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet DC-9-82/-83


ARINC429

InputChannel

Pins139

Connections

3A=MP11AB=MP11B

ADC #1 (ARINC 575) (Low Speed) 1

OrNot Used

14A=TP1CB=TP1D

Not UsedOr

ADC #1 (ARINC 429) (Low Speed) 1

1A=MP6AB=MP6B

DFGC #1 (High Speed)Or

AHRS #1 (High Speed) (use Optional Inputs Select to enable)

13A=TP5AB=TP6A

DFGC Bus #2 (High Speed)Or

AHRS #2 (High Speed) (use Optional Inputs Select to enable)

11A=TP8AB=TP8B

EFIS Bus #1 (High Speed) (EFIS SG #1 ISDAS Bus)Or

Not Used (use Optional Inputs Select to disable)

4A=MP12AB=MP12B

EFIS Bus #2 (Low Speed)(EFIS SG #1 WXR Control Bus #1) 3�� /

8A=MP13AB=MP13B

EFIS Bus #3 (High Speed) (EFIS SG #2 ISDAS Bus)Or

Not Used (use Optional Inputs Select to disable)

9A=TP9CB=TP9D

EFIS Bus #4 (Low Speed)(WXR Control Bus #2) 3�� 4

18A=MP6CB=MP6D

Not usedor

GPS #1 (High Speed ; ARINC 743A)

17A=TP11CB=TP11D

Not usedor


7A=MP12CB=MP12D

Not UsedOr

Wx Radar Bus (High Speed)

2A=MP10CB=MP10D

Not Used ��

5A=MP10AB-MP10B

Not Used ��

6A=MP11CB=MP11D

Not Used ��





1Provide only one ADC input as indicated by bus format.



Types Connections



-206 and on GPS #1, #2Use if GPS is ARINC 743 (not

ARINC 743A) 139

Allied Signal, Inc.


Discrete Inputs Worksheet DC-9-82/-83



REQUIRED






Radio Altimeter #1 Valid TP15A +28V = Valid; 0V = Not Valid

Glideslope #1 Valid TP15B +28V = Valid; 0V = Not Valid

Landing Gear TP15C +28V = Gear Down; 0V = Gear Up

ILS Select TP7A +28V = ILS Selected; 0V = ILS Not Selected

Localizer Valid TP7C +28V = Valid; 0V = Not Valid

OPTIONAL







GPWS Inhibit MP5D Ground = GPWS Inhibit; Open = Not Inhibit



Glideslope Inhibit TP15D +28V = Inhibit; 0V = Not Inhibit

Radio Altimeter #2 Valid TP7B +28V = Valid; 0V = Not Valid

NOT USED


MP1A N/A ��

MP1B N/A ��

MP9B N/A ��

MP14A N/A ��

MP2D N/A ��

MP2B N/A ��

TP4C N/A ��

TP7D N/A ��

Allied Signal, Inc.


Serial Outputs Worksheet DC-9-82/-83


ChannelPins

139Connections

TX453-1A=TP3AB=TP3B

Terrain Display data to symbol generator relay #1

TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B




Lamp 139

MP15D Glideslope Cancel N/A '� �� +�)�

MP3D Below G/S Caution No +��'��-�� ()*�# '� +�)��

MP7BAll


No +��'��-�� !"� +�)��


TP12A PWS Inhibit No








TP11B Terrain Monitor Discrete N/A





Allied Signal, Inc.


A-10.3 MD10


Aircraft Type 44

Description MD 10



ADIRU ADC

ADIRU IRS

CFDS

LRRA

MMR ILS

Single

VIA EIS

VIA FMCDual


SingleExternal

GPSSingle MMR GPS

DualExternal

GPSDual MMR GPS

PP

IN 7


Dual ADIRU ADC, ADIRU IRS

PWS Option1


PP

IN 1

5

PWS Option2


Dual RA Dual LRRA


PP

IN 9

Dual ILS Dual MMR ILS Buses

FEATURES



No


ARINC 429 DH No


Lamp Format Type 1


Alert Volume High

Steep Approach N/A


No

Windshear No

Allied Signal, Inc.


Display Options & Peaks Availability MD 10

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-202

and on

Honeywell Boeing DPDIntegrated LCD EFIS(Bus type: ARINC 708Standard Data Format)

No auto ranging

DefaultControlledby display(see ICD)

Controlledby display– No Pop

Up (see ICD)

No Yes Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

44 MP7B TP12C Open


There are no analog inputs for this Aircraft Type. Alternate RA formats do not apply to this

Aircraft Type.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet MD 10


InputChannel

Pins44

Connections

3A=MP11AB=MP11B

ADIRU #1 ADC (Low Speed) (��1 �� (� �

14A=TP1CB=TP1D

Not UsedOr

ADIRU #2 ADC Bus (Low Speed)

1A=MP6AB=MP6B ADIRU #1 IRS Bus (High Speed) (��1 ��

13A=TP5AB=TP6A

Not UsedOr

ADIRU #2 IRS Bus (High Speed)

10A=TP9AB=TP9B CFDS Bus (Low Speed) ��

8A=MP13AB=MP13B LRRA #1 (Low Speed) +��( ��

15A=TP4AB=TP4B

Not UsedOr

LRRA #2 (Low Speed)

4A=MP12AB=MP12B

Not UsedOr

LRRA #3 (Low Speed)

18A=MP6CB=MP6D

Not UsedOr

MMR #1 GPS (Low Speed – ARINC 743A)

17A=TP11CB=TP11D

Not UsedOr


12A=TP8CB=TP8D

Not UsedOr

MMR #2 ILS Bus (Low Speed)

5A=MP10AB-MP10B VIA #1 EIS Bus (High Speed) &�( �� 3��

16A=TP5CB=TP5D VIA #2 EIS Bus (High Speed) &�( �/ 3��

9A=TP9CB=TP9D VIA #1 FMC Bus (Low Speed) &�( ��

2A=MP10CB=MP10D

VIA #2 FMC Bus (Low Speed) &�( �/ ��

6A=MP11CB=MP11D

MMR #1ILS (Low Speed) �� +� �

7A=MP12CB=MP12D

Not UsedOr


11A=TP8AB=TP8B

Not UsedOr



Program Pin / Signal P/NAvailability Changes to Interfaces

Applies toAircraftTypes

Connections


- GPS #1, #2 High Speedbus(es) 44

Allied Signal, Inc.


Discrete Inputs Worksheet MD 10



REQUIRED

Landing Gear MP5C Ground = Landing Gear Down;\Open = Not Landing Gear







Wxr On/Off #1 MP14A Ground = On; Open = Off(for EFIS annunciation only)

Wxr On/Off #2 MP2D Ground = On; Open = Off(for EFIS annunciation only)

OPTIONAL







Decision Height TP1A Ground = <DH; Open = >DH

NOT USED


MP1A N/A Open

MP14B N/A Open

TP1B N/A Open

MP2B N/A Open

TP4C N/A Open

MP5D N/A Open

TP15A N/A Open

TP15B N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet MD 10


ChannelPins

44Connections

TX453-1A=TP3AB=TP3B

Terrain display data to left display switching relay

TX453-2A=TP3CB=TP3D

Terrain display data to right display switching relay

TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B




Lamp 44

MP15D Glideslope Cancel N/A � �0,� +�)�


MP7BAll


No 0�� 1�� (�#�#��

TP12C Spare No 0�� 1��

TP12A PWS Inhibit No "5�








TP11B Spare N/A 0�� 1��





Allied Signal, Inc.


A-10.4 MD11


Aircraft Type 45

Description MD 11



ADC Single (ADC #2)

CFDS Single

DEU

FMCDual

IRS

ILS

LRRA

Single


SingleExternal

GPSSingle GPS

DualExternal

GPSDual GPS

PP

IN 7


Dual ADC (#1), IRS

PWS Option1


PP

IN 1

5

PWS Option2


Dual RA Dual LRRA

PP

IN 9

Dual ILS Dual ILS

FEATURES



No


ARINC 429 DH No


Lamp Format Type 1


Alert Volume High

Steep Approach N/A


No

Windshear No

Allied Signal, Inc.



PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-202

and on

Honeywell Boeing DPDIntegrated CRT EFIS(Bus type: ARINC 708Standard Data Format)

No auto ranging

DefaultControlledby display(see ICD)


Up (see ICD)

No Yes Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

45 TP12C TP12C Open



Aircraft Type.

Allied Signal, Inc.




InputChannel

Pins45

Connections

14A=TP1CB=TP1D

Not UsedOr

ADC #1 (Low Speed)

3A=MP11AB=MP11B

ADC #2 (Low Speed)If only one ADC is supplied, it must be ADC #2. (� �/


5A=MP10AB-MP10B

DEU #1 (High Speed) �31 ��

12A=TP8CB=TP8D DEU #2 (High Speed) �31 �/

9A=TP9CB=TP9D FMC #1 (Low Speed) ��

2A=MP10CB=MP10D FMC #2 (Low Speed) �� /

4A=MP12AB=MP12B

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D

ILS #1 (Low Speed) �+� ��


16A=TP5CB=TP5D

Not UsedOr

ILS #2 (Low Speed)

13A=TP5AB=TP6A

Not UsedOr

IRS #2 Bus (High Speed)

8A=MP13AB=MP13B

LRRA #1 (Low Speed) +��( ��

15A=TP4AB=TP4B

Not UsedOr

LRRA #2 (Low Speed)

11A=TP8AB=TP8B

Not UsedOr


7A=MP12CB=MP12D

Not UsedOr






Connections



Allied Signal, Inc.





REQUIRED








Wxr On/Off #2 MP2D Ground = On; Open = Off(for EFIS annunciation only)

Landing Gear TP15D 28V = Landing Gear Down;Open = Not Landing Gear

OPTIONAL








NOT USED


MP1A N/A Open

MP14B N/A Open

TP1A N/A Open

TP1B N/A Open

MP2B N/A Open

TP4C N/A Open

MP5D N/A Open

TP15A N/A Open

TP15B N/A Open

TP15C N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open

Allied Signal, Inc.




ChannelPins

45Connections

TX453-1A=TP3AB=TP3B

Terrain display data to left display

TX453-2A=TP3CB=TP3D

Terrain display data to right display

TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B




Lamp 45



MP7B Spare No 0�� 1��














Allied Signal, Inc.


A-10.5 MD80



Description MD80 AA/EFIS MD80 Alaska/EFIS MD80 AA/non-EFIS MD80 AA/non-EFIS



ADC Dual (ARINC 575)

DFGC Dual

EFIS Four N/A

WXRControl/Display

N/A Single

Analog RA

Analog GSSingle


SingleExternal

GPSSingle GPS

PP

IN 7

DualExternal

GPSDual GPS

PP

IN 1

0

QFE/QNHSelect Standby Altimeter Baro Set Reference & Signal Voltages

FEATURES



No


ARINC 429 DH No


Lamp Format Type 1


Alert Volume High

Steep Approach N/A


No

Windshear No

Allied Signal, Inc.



PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-102

and on


No auto ranging



1-104

and on


(Bus type: Revisedpicture header bits




1-206

and on

Honeywell Primus 708Radar


No auto ranging

Fan mode Yes No No Yes Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

114 MP15D TP12A MP3A

115 MP3D TP12A MP3A

179 MP3D TP12A MP15D

180 MP7B TP12A MP15D

Allied Signal, Inc.




AnalogInputChannel

Pins114, 115, 179, 180

Connections


2+ = TP14A- = TP14B

Not UsedOr

Standby Altimeter Baro Set Reference Voltage (ARINC 575)Range: 0 – 10 VDC

(Select QFE Program Pin option to activate)

3+ = TP13C- = TP13D Glideslope #1 (ARINC 547 with Validity Flag & ILS Select)

4+ = TP14C- = TP14D

Not UsedOr

Standby Altimeter Baro Set Signal Voltage (ARINC 575)Range: 0 – 10 VDC

(Select QFE Program Pin option to activate QNH CorrectedAltitude)



Allied Signal, Inc.




ARINC429

InputChannel

Pins114, 180

Connections

3A=MP11AB=MP11B

ADC #1 (ARINC 575) (Low Speed) (� ��

14A=TP1CB=TP1D ADC #2 (ARINC 575) (Low Speed) (� �/

1A=MP6AB=MP6B DFGC #1 (High Speed) ��

13A=TP5AB=TP6A DFGC Bus #2 (High Speed) �� /

11A=TP8AB=TP8B

EFIS Bus #1 (High Speed)(EFIS SG #1 ISDAS Bus)

EFIS SG #1 ISDAS Bus

4A=MP12AB=MP12B

EFIS Bus #2 (Low Speed)(EFIS SG #1 WXR Control Bus #1)

EFIS SG #1 WXR ControlBus #1

8A=MP13AB=MP13B

EFIS Bus #3 (High Speed)(EFIS SG #2 ISDAS Bus) EFIS SG #2 ISDAS Bus

9A=TP9CB=TP9D

EFIS Bus #4 (Low Speed)(EFIS SG #2 WXR Control Bus #2)

EFIS SG #2 WXR ControlBus #2

17A=TP11CB=TP11D

Not usedor


18A=MP6CB=MP6D

Not usedor


2A=MP10CB=MP10D

Not Used ��

5A=MP10AB-MP10B Not Used ��





15A=TP4AB=TP4B

Not Used ��


For A/C Types 114, 115 and 180 GPS #1 and #2: True heading per ARINC 429-14 for equipment code 004 (IRU).






Allied Signal, Inc.




ARINC429

InputChannel

Pins115, 179

Connections

3A=MP11AB=MP11B

ADC #1 (ARINC 575) (Low Speed) (� ��

14A=TP1CB=TP1D

ADC #2 (ARINC 575) (Low Speed) (� �/

1A=MP6AB=MP6B

DFGC #1 (High Speed) ��

13A=TP5AB=TP6A DFGC Bus #2 (High Speed) �� /

17A=TP11CB=TP11D

Not usedor


18A=MP6CB=MP6D

Not usedor


4A=MP12AB=MP12B WXR Control/Display (Low Speed) "5� ��#��'��

2A=MP10CB=MP10D

Not Used ��

5A=MP10AB-MP10B

Not Used ��

6A=MP11CB=MP11D

Not Used ��









For A/C Types 114, 115 and 180 GPS #1 and #2: True heading per ARINC 429-14 for equipment code 004 (IRU).






Allied Signal, Inc.





REQUIRED






LRRA #1 Valid TP15A +28V = Valid; 0V = Not Valid




OPTIONAL











NOT USED


MP1A N/A ��

MP1B N/A ��

MP9B N/A ��

MP14A N/A ��

MP2D N/A ��

MP2B N/A ��

TP4C N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.





REQUIRED






WX Radar On/Off MP14A Ground = On; Open = Off

LRRA #1 Valid TP15A +28V = Valid; 0V = Not Valid




OPTIONAL











NOT USED


MP1A N/A ��

MP1B N/A ��

MP9B N/A ��

MP2D N/A ��

MP2B N/A ��

TP4C N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.




ChannelPins


TX453-1A=TP3AB=TP3B


TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B



ChannelPins

180Connections

TX453-1A=TP3AB=TP3B Terrain Display data to symbol generator relay #1

TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B


Allied Signal, Inc.


Discrete Outputs Worksheet MD 80


Lamp 114, 180



MP7BAll


No +��'��-�� !"� +�)��



TP12B Audio On N/A � (� ��*��







TP11B Terrain Monitor Discrete N/A






Lamp 115, 179



MP7BAll


No +��'��-�� !"� +�)��




TP4D Terrain Displayable #1 N/A ��


MP14C Spare N/A

TP11A Spare N/A

MP7C GPWS Monitor N/A !"� �� +�)�

TP12D Terrain Not Available N/A ��##�� 0'( +�)�

TP11B Terrain Monitor Discrete N/A ��##�� 0�! +�)�





Allied Signal, Inc.


A-10.6 MD87


Aircraft Type 120

Description MD 87 with PPI Display



ADC

FMC

IRS

RA

ILS

Analog Localizer

Single


SingleExternal

GPSSingle GPS

DualExternal

GPSDual GPS

PP

IN 7


Dual ADC, FMC, IRS

PP

IN 1

5

PWS Option1


PP

IN 9


Digital LRRA not allowed

Alternate ILSFormat

Single digital ILS #1 (will use if provided)Replaces Analog G/S & Localizer inputs

Alternate RAformat

Single digital LRRA #1 ( will use if provided)Replaces Analog RA input; Dual RA not allowed

FEATURES



No


ARINC 429 DH No


Lamp Format Type 1


Alert Volume Low



No

Windshear No

Allied Signal, Inc.



PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-202

and on

RDR 4A/B Bendix(PPI)1


10 NM auto ranging





1 (TP10A) 2 (TP10B) 3 (TP10C)

120 Open TP4D MP3A



AnalogInputChannel

Pins120

Connections

1+ = TP13A- = TP13B



2+ = TP14A- = TP14B

Not UsedOr


3+ = TP13C- = TP13D



4+ = TP14C- = TP14D




Alternate RA formats do not apply to this Aircraft Type.

Allied Signal, Inc.




InputChannel

Pins120

Connections

3A=MP11AB=MP11B

ADC #1 ARINC 575 (Low Speed) (� ��

12A=TP8CB=TP8D

Not UsedOr

ADC #2 ARINC 575 (Low Speed)

2A=MP10CB=MP10D Display Bus (Radar Indicator Bus) (Low Speed) ��

4A=MP12AB=MP12B


11A=TP8AB=TP8B

Not UsedOr

FMC #2 (Low Speed)

5A=MP10AB-MP10B

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D

Not UsedOr


1A=MP6AB=MP6B

IRS Bus #1 (High Speed) ��

13A=TP5AB=TP6A

Not UsedOr


8A=MP13AB=MP13B

Not UsedOr


7A=MP12CB=MP12D

Not UsedOr





15A=TP4AB=TP4B

Not Used ��

16A=TP5CB=TP5D

Not Used ��








Allied Signal, Inc.





REQUIRED


��

!"� "�#� ��#$

Landing Gear MP9B Ground = Gear Down; Open = Gear Up ��# ��


MP9C Ground = Landing Flap/Normal;Open = Not Landing Flap/Override

��

��%�� !"� �� &��


'� �� ()*�#

!"� (��#� ��#$


MP2B Ground = Inhibit; Open = Normal (�� ##�� *��

ILS Select 1 MP14A Ground = ILS Selected; Open = Not Selected �+� �� +��

Radio Altitude Valid #1 TP15A +28V = Valid; 0V = Not Valid �� (�� &��

Glideslope Valid 1 TP15B +28V = Valid; 0V = Not Valid �+� �� &��

Localizer Valid 1 TP15D +28V = Valid; 0V = Not Valid

OPTIONAL

Back Course Select MP1B Ground = Glideslope Inhibit; Open = NotInhibit �+� ��%��#��

Mode 6 Volume Control MP2A Ground = Low Volume; Open = Normal (�#�#�� #��

Decision Height MP5C Ground = <DH; Open = >DH �� (�� , *- ��

Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal�� #��- �# �#��.� "'�

�� *��

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled (�#�#�� #��


MP8D Momentary Ground = Audio Suppress;Open = Normal ��%�� !"� (�� *��

Steep Approach #1 TP4C Ground = Enabled; Open = Disabled (�#�#�� #��

Steep Approach #2 MP5D Ground = Selected; Open = Not Selected ��%�� (��#��

��

Radio Altitude Valid #2 TP15C +28V = Valid; 0V = Not Valid �� (�� / &��

Display Select #1 TP1A Momentary Ground Switch +�� ##��

NOT USED


MP1A N/A Open

MP14B N/A Open

MP2D N/A Open

TP1B N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open1 ILS Select, Localizer Valid and Glideslope Valid not required if digital ILS provided. (EGPWS will automatically usedigital ILS if provided.)

Allied Signal, Inc.




ChannelPins

120Connections

TX453-1A=TP3AB=TP3B

Left side picture bus WX indicator (Display)

TX453-2A=TP3CB=TP3D

Not Used

TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B




Lamp 120


MP3D Below G/S Caution Yes +��'��-�� ()*�# '� +�)��

MP7BAll


Yes +��'��-�� !"� ��)��








MP7C GPWS Monitor N/A ()*�# !"� �0�! ��)�


TP11B Terrain Not Available N/A ()*�# ��##�� 0�! ��)�





Allied Signal, Inc.


A-10.7 MD88/90


Aircraft Type 118

Description MD 88/90 EFIS




EFIS Four

FMC

IRS

Analog RA

Analog G/S

Single


SingleExternal

GPSSingle GPS

DualExternal

GPSDual GPS

PP

IN 7


Dual FMC, IRS

PP

IN 9


FEATURES



No


ARINC 429 DH No


Lamp Format Type 1


Alert Volume High

Steep Approach N/A


No

Windshear No

Allied Signal, Inc.


Display Options & Peaks Availability MD 88/90

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-204

and on


No auto ranging

Default

Yes (ifEFIS indisplay-

able modeand WX

on)

N/A No Yes Open

2-208

and on


No auto ranging

DefaultYes (if WX

on) N/A No Yes MP3A




1 (TP10A) 2 (TP10B) 3 (TP10C)

118 TP12A TP12A MP3A



AnalogInputChannel

Pins118

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ARINC 552 with Validity Discrete) �( ��

2+ = TP14A- = TP14B

Not UsedOr


3+ = TP13C- = TP13D

Glideslope #1 (ARINC 547 with Validity Flag & ILS Select) '� ��

4+ = TP14C- = TP14D Not Used 0��


Alternate RA formats do not apply to this Aircraft Type.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet MD 88/90


InputChannel

Pins118

Connections

3A=MP11AB=MP11B

ADC #1 ARINC 575 (Low Speed)1

OrNot Used

14A=TP1CB=TP1D

Not UsedOr


11A=TP8AB=TP8B

EFIS Bus #1 (High Speed)(EFIS SG #1 ISDAS Bus) 3��

4A=MP12AB=MP12B

EFIS Bus #2 (Low Speed)(EFIS SG #1 WXR Control Bus #1) 3�� /

8A=MP13AB=MP13B

EFIS Bus #3 (High Speed)(EFIS SG #2 ISDAS Bus) 3�� 6

9A=TP9CB=TP9D

EFIS Bus #4 (Low Speed)(EFIS SG #2 WXR Control Bus #2) 3�� 4


12A=TP8CB=TP8D

Not UsedOr

FMC #2 (Low Speed)

18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr



13A=TP5AB=TP6A

Not UsedOr


2A=MP10CB=MP10D

Not Used ��

5A=MP10AB-MP10B

Not Used ��





1Provide only one ADC input as indicated by format.







Allied Signal, Inc.


Discrete Inputs Worksheet MD 88/90



REQUIRED






Radio Altitude Valid #1 TP15A +28V = Valid; 0V = Not Valid

Glideslope Valid TP15B +28V = Valid; 0V = Not Valid



ILS Select TP7A +28V = ILS Selected; 0V = Not Selected

OPTIONAL











Radio Altitude Valid #2 TP7B +28V = Valid; 0V = Not Valid

NOT USED


MP1A N/A Open

MP1B N/A Open

MP9B N/A Open

MP14A N/A Open

MP2D N/A Open

MP2B N/A Open

TP4C N/A Open

TP7C N/A Open

TP7D N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet MD 88/90


ChannelPins

118Connections

TX453-1A=TP3AB=TP3B

Terrain display data to symbol generator relay #1

TX453-2A=TP3CB=TP3D

Terrain display data to symbol generator relay #2

TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B




Lamp 118



MP7BAll


No +��'��-�� !"� ��)��










TP11B Terrain Monitor N/A





Allied Signal, Inc.


A-10.8 MD95


Aircraft Type 129

Description MD 95



ADIRU ADC

ADIRU IRS

CFDS

LRRA

MMR ILS

Single

VIA EIS

VIA FMCDual


SingleExternal

GPSSingle MMR GPS

DualExternal

GPSDual MMR GPS

PP

IN 7


Dual ADIRU ADC, ADIRU IRS

PP

IN 1

5

PWS Option1


Dual RA Dual LRRA


PP

IN 9

Dual ILS Dual MMR ILS Buses

FEATURES



No


ARINC 429 DH No


Lamp Format Type 1


Alert Volume High

Steep Approach N/A


No

Windshear No

Allied Signal, Inc.



PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-202

and on

Honeywell Boeing DPDIntegrated LCD EFIS(Bus type: ARINC 708Standard Data Format)

No auto ranging

DefaultControlledby display(See ICD)


Up(See ICD)

No Yes Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

129 MP3A Open MP15D



Aircraft Type.

Allied Signal, Inc.




InputChannel

Pins129

Connections

3A=MP11AB=MP11B

ADIRU #1 ADC (Low Speed) (��1 �� (� �

14A=TP1CB=TP1D

Not UsedOr

ADIRU #2 ADC Bus (Low Speed)

1A=MP6AB=MP6B ADIRU #1 IRS Bus (High Speed) (��1 ��

13A=TP5AB=TP6A

Not UsedOr

ADIRU #2 IRS Bus (High Speed)


8A=MP13AB=MP13B LRRA #1 (Low Speed) +��( ��

15A=TP4AB=TP4B

Not UsedOr

LRRA #2 (Low Speed)

4A=MP12AB=MP12B

Not UsedOr

LRRA #3 (Low Speed)

18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D

MMR #1ILS (Low Speed) �� +� �

12A=TP8CB=TP8D

Not UsedOr

MMR #2 ILS Bus (Low Speed)

5A=MP10AB-MP10B VIA #1 EIS Bus (High Speed) &�( �� 3��

16A=TP5CB=TP5D VIA #2 EIS Bus (High Speed) &�( �/ 3��

9A=TP9CB=TP9D

VIA #1 FMC Bus (Low Speed) &�( ��

2A=MP10CB=MP10D

VIA #2 FMC Bus (Low Speed) &�( �/ ��

11A=TP8AB=TP8B

Not UsedOr






16Alternate GPSSpeed - GPS #1, #2 High Speed bus(es) 129

Allied Signal, Inc.





REQUIRED


Landing Flap/FlapsOverride






Landing Gear TP7C +28V = Landing Gear Down; 0V = Not Landing Gear

OPTIONAL








NOT USED


MP1A N/A Open

MP9B N/A Open

MP2D N/A Open

TP1A N/A Open

TP1B N/A Open

MP2B N/A Open

TP4C N/A Open

MP5D N/A Open

TP15A N/A Open

TP15B N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

TP7B N/A Open

TP7D N/A Open

Allied Signal, Inc.




ChannelPins

129Connections

TX453-1A=TP3AB=TP3B


TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B




Lamp 129



MP7B Spare No 0�� 1��














Allied Signal, Inc.


A-11 Embraer

A-11.1 EMB-135/EMB-145


Aircraft Type 33

Description EMB-135/EMB-145



ADC

AHRS

DSWC

Dual

FMCDual Low Speed or Single High Speed

See ARINC 429 Input Channel Assignments Worksheets for options

IC Single

Analog RA Single


SingleExternal

GPSSingle GPS

DualExternal

GPSDual GPS

PP

IN 7


Single FMC (High Speed)Disables Dual Low Speed FMC inputs

PP

IN 9


OrDual Digital RA if Alternate RA Configuration #2 is selected

Alternate RAFormat

Digital RAReplaces Analog RA inputs

FEATURES



No


ARINC 429 DH No


Lamp Format Type 2


Alert Volume High



No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability EMB-135/EMB-145

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-202

and on




Honeywell

Based ondisplay

controllerstrapping(see ICD)

N/A No No Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

33 MP3A MP7B Open



AnalogInputChannel

Pins33

Connections

1+ = TP13A- = TP13B



2+ = TP14A- = TP14B

Not UsedOr


3+ = TP13C- = TP13D

Not Used ��

4+ = TP14C- = TP14D

Not Used ��



33Selected?

Default ARINC 552



Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet EMB-135/EMB-145


InputChannel

Pins33

Connections

3A=MP11AB=MP11B

ADC #1 ARINC 429 (Low Speed) � �

14A=TP1CB=TP1D ADC #2 (Low Speed) � ��

1A=MP6AB=MP6B AHRS Bus #1 (High Speed) ��


8A=MP13AB=MP13B



4A=MP12AB=MP12B

FMC #1 (Low Speed)Or

Not Used (if Optional Input Select enabled)

15A=TP4AB=TP4B


Not Used (if Optional Input Select enabled)

2A=MP10CB=MP10D

Not UsedOr

FMC Bus (High Speed)Use if single FMC – Optional Input Select enables

18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


5A=MP10AB-MP10B IC Data Bus (IC-600 #1) (Low Speed) ��

10A=TP9AB=TP9B

Not UsedOr

LRRA #1 (Low Speed)

7A=MP12CB=MP12D

Not UsedOr

LRRA #2 (Low Speed)




16A=TP5CB=TP5D

Not Used ��




Connections

Alternate GPSSpeed




Allied Signal, Inc.


Discrete Inputs Worksheet EMB-135/EMB-145



REQUIRED


�� !"�"#��$ ��

%&�� #'� #��"��#��'(

Landing Gear MP9B Ground = Gear Down; Open = Gear Up )#��* %�#' )��+�� #��


,�#�� ,"�� #�� #�� #��

��+�� %&�� ,�#�� -� ��


%.� �#�� !"�"#��$ �� /0�'

%&�� '� #��"��#��'(


MP14B Ground = Inhibit; Open = Normal �� #�� ''#�� 0��

Radio Altitude Valid #1 TP15A +28V = Valid; 0V = Not Valid �#�� -#��$

OPTIONAL

Glideslope Inhibit MP1B Ground = Inhibit; Open = Not Inhibit �)� 1#�+��"'�� #��

Mode 6 Volume Control MP2A Ground = Low Volume; Open = Normal �'�'#�� %'�"��

Decision Height MP5C Ground = <DH; Open = >DH �#� �� 0"* �"��"�

Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal��#�� #'��* �' �'��2� �.� #"��

�� 0�� "��"�

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled �'�'#�� %'�"��


MP8D Momentary Ground = Audio Suppress;Open = Normal ��+�� %&�� "�� "��'��

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Normal 3�� 4 ��

Steep Approach #1 MP1A Ground = Enabled; Open = Disabled �'�'#�� %'�"��

Steep Approach #2 MP5D Ground = Selected; Open = Not Selected��+�� #�� #�� '�#�

��

Radio Altitude Valid #2 TP15B +28V = Valid; 0V = Not Valid �#�� -#��$

NOT USED


MP14A N/A Open

MP2D N/A Open

TP1A N/A Open

TP1B N/A Open

TP4C N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet EMB-135/EMB-145


ChannelPins

33Connections

TX453-1A=TP3AB=TP3B

Honeywell left/right interleaved picture bus to MFD 5, 6�

TX453-2A=TP3CB=TP3D

Not Used ��

TX429-1Low Speed

A=MP1CB=MP1D

ICD Appendix E label sets: E-1/2/3/5/6/8/11 �� 6�

TX429-2Low Speed

A=TP2AB=TP2B




Lamp 33


MP3D All GPWS Cautions No ��

MP7B All GPWS Warnings (“Pull Up”) No ��

TP12C Windshear Caution No ��

TP12A Windshear Warning No ��

TP12B Audio On N/A �� 0��





MP7C GPWS Monitor N/A ��

TP12D Windshear Monitor N/A ��

TP11B Terrain Not Available N/A ��

Allied Signal, Inc.


A-12 Fokker

A-12.1 Fokker 100


Aircraft Type 131

Description Fokker 100 EFIS



ADC

EFIS

FMC

Dual

ILS Single

IRS Dual

LRRA Single


SingleExternal

GPSSingle GPS

PP

IN 7

DualExternal

GPSDual GPS

Dual ILS Dual ILS

Dual RA Dual LRRA

PP

IN 9


FEATURES



No


ARINC 429 DH Yes


Lamp Format Type 1


Alert Volume High



No

Windshear External to EGPWS

Allied Signal, Inc.


Display Options & Peaks Availability Fokker 100

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-102

and on

Collins EFIS(Bus type: ARINC 708

Data Format)No auto ranging





1 (TP10A) 2 (TP10B) 3 (TP10C)

131 MP3D Open MP15D



Aircraft Type.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Fokker 100


InputChannel

Pins131

Connections

3A=MP11AB=MP11B



5A=MP10AB-MP10B

EFIS Bus #1 (Low Speed)(EFIS CP LH) ��

16A=TP5CB=TP5D

EFIS Bus #2 (Low Speed)(EFIS CP RH) ��



18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr



12A=TP8CB=TP8D

Not UsedOr

ILS #2 (Low Speed)




11A=TP8AB=TP8B

Not UsedOr

LRRA #2 (Low Speed)

4A=MP12AB=MP12B

Not UsedOr

LRRA #3 (Low Speed)

7A=MP12CB=MP12D

Not Used ��

9A=TP9CB=TP9D

Not Used ��

10A=TP9AB=TP9B

Not Used ��




Connections

Alternate GPSSpeed




Allied Signal, Inc.


Discrete Inputs Worksheet Fokker 100



REQUIRED








MP14A Ground = Inhibit; Open = Normal

OPTIONAL












Display Select 2 TP1B Momentary Ground Switch

NOT USED


MP2D N/A Open

TP4C N/A Open

MP5D N/A Open

TP15A N/A Open

TP15B N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet Fokker 100


ChannelPins

131Connections

TX453-1A=TP3AB=TP3B


TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B




Lamp 131


MP3D Below G/S Caution No �� ! �"�#�$"%�� $

MP7BAll


No �� # ��&� "��$

TP12C Spare No �%� '$�#


TP12B Audio On N/A (��

TP4D Terrain Displayable #1 N/A �� (�!!��

TP10D Terrain Display Discrete #1 N/A �� (�!!�� "�)

MP14C Terrain Display Discrete #2 N/A �� (�!!�� "�)

TP11A Terrain Displayable #2 N/A �� (�!!��

MP7C GPWS Monitor N/A ��&� �* ( ��


TP11B Terrain Not Available N/A (�!!��



MP3D All GPWS Cautions No �� ! ��&� ��$

MP7B All GPWS Warnings (“Pull Up”) No �� # �'"" *� ��$

Allied Signal, Inc.


A-13 Gulfstream

A-13.1 Gulfstream II


Aircraft Type 68

Description Gulfstream II




AHRS/IRS Dual (will use either IRS or AHRS inputs as provided)


ILS

RASingle

AOA Dual


SingleExternal

GPSSingle GPS

PP

IN 7

DualExternal

GPSDual GPS

Alternate RAFormat

Single LRRA (use Alt. RA Configuration #2 to select)Replaces Analog RA

Alternate ILSFormat

Single digital ILSReplaces Analog ILS


Dual MFD (Select PPIN 18 State 2 to enable)Or

Dual EFIS (Select PPIN 18 State 3 to enable)

FEATURES



No


ARINC 429 DH No


Lamp Format Type 1


Alert Volume High



No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Gulfstream II

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-101

and onNo Display N/A N/A N/A No No Open

2-208

and on

Collins FDS-255(Bus type: ARINC 708Standard Data Format)

No auto ranging

Fan modewith +-91o

limitYes No No No MP3A

3-208

and on

Honeywell EDZ805,5x6



Honeywell Yes No No NO MP15D




1 (TP10A) 2 (TP10B) 3 (TP10C)

68 MP7B Open MP3A

Allied Signal, Inc.




AnalogInputChannel

Pins68

Connections

1+ = TP13A- = TP13B


Not used (use Alternate RA Format #2 to select)

2+ = TP14A- = TP14B



Offset: 48.0o

Gain = -6.0o



T P2D(10 VDC)

T P14A (+)

T P14B (-)

3+ = TP13C- = TP13D



4+ = TP14C- = TP14D



Gain = -6.0o



T P2D(10 VDC)

T P14C (+)

T P14D (-)



68Selected?

Default ARINC 552



Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Gulfstream II


InputChannel

Pins68

Connections

3A=MP11AB=MP11B


Or Not Used

12A=TP8CB=TP8D


4A=MP12AB=MP12B

FMC (Low Speed) 1

OrNot Used

11A=TP8AB=TP8B

Not UsedOr

FMC (High Speed) 1

18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D

Not UsedOr

ILS #1 (Low Speed) will use if provided

1A=MP6AB=MP6B

IRS #1 (High Speed) Preferredor


13A=TP5AB=TP6A



8A=MP13AB=MP13B

Not UsedOr

LRRA #1 (Left) (Low Speed)(will use if Alt RA format selected)

5A=MP10AB-MP10B

Not UsedOr

MFD #1 range(Select Alt Display PPIN 18 State 2)Or

Left EFIS range (Select Alt Display PPIN 18 State 3)

7A=MP12CB=MP12D

Not UsedOr

MFD #2 range (Select Alt Display PPIN 18 State 2Or

Right EFIS range(Select Alt Display PPIN 18 State 3)

2A=MP10CB=MP10D

Not Used ��

9A=TP9CB=TP9D

Not Used ��






Allied Signal, Inc.









ConfigurationOption 2 - FMC #1


Allied Signal, Inc.


Discrete Inputs Worksheet Gulfstream II



REQUIRED

Self-Test MP9A Momentary Ground = Self Test; Open = Normal��

��

Landing Gear MP9B Ground = Gear Down; Open = Gear Up ��

Landing Flap/FlapOverride MP9C

Ground = Landing Flap Selected;Open = Not Landing Flap

��

��

��

Glideslope Cancel MP9D Momentary Ground = Cancel; Open = Normal�!� "��

#$%�� #��

ILS Select 1 MP14A Ground = ILS Selected; Open = Not Selected &'� �� '��

Terrain Awareness & TCFInhibit

MP14B Ground = Inhibit; Open = Normal #�� &��%��

Alternate Radio AltimeterValidity

TP15A +28V = Valid; 0V = Not Valid �� #��

Glideslope Valid 1 TP15B +28V = Valid; 0V = Fail &'� ��

Flap Position #1 (0 o) TP7A +28V = Selected; 0V = Not Selected �� (� ��

Flap Position #2 (10 o) TP7B +28V = Selected; 0V = Not Selected �� )(� ��

Flap Position #3 (20 o) TP7C +28V = Selected; 0V = Not Selected �� *(� ��

Flap Position #4 (39 o) TP7D +28V = Selected; 0V = Not Selected �� +,� ��

OPTIONAL

Back Course Select MP1B Ground = Glideslope Inhibit; Open = Not Inhibit ��-��

Mode 6 Volume Control MP2A Ground = Low Volume; Open = Normal #��

Decision Height MP5C Ground = <DH; Open = >DH �� #�� . %�- ��

Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal�� - �� /� �!�

�� %��

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled #��



"�� #��

��


Terrain Display Select #1 TP1A Momentary Ground SwitchUsed for Alt Display PPIN 18 State 2 only

OpenOr

Left Terrain Select Switch

Terrain Display Select #2 TP1B Momentary Ground SwitchUsed for Alt Display PPIN 18 State 2 only

OpenOr

Right Terrain Select Switch

Steep Approach #1 TP4C Ground = Enabled; Open = Disabled

Steep Approach #2 MP5D Ground = Selected; Open = Not Selected

NOT USED


MP1A N/A Open

MP2D N/A Open

TP15C N/A Open

TP15D N/A Open1 ILS Select and Glideslope Valid not required if digital ILS provided. (EGPWS will automatically use digital ILS ifprovided.)

Allied Signal, Inc.


Serial Outputs Worksheet Gulfstream II


ChannelPins

68Connections

TX453-1A=TP3AB=TP3B

Not UsedOr

Terrain Display data LH(Used for Alt Display PPIN 18 State 2 only)

OrLeft side picture bus to symbol generator port(Used for Alt Display PPIN 18 State 3 only)

TX453-2A=TP3CB=TP3D

Not UsedOr

Terrain Display data RH(Used for Alt Display PPIN 18 State 2 only)


TX429-1Low Speed


TX429-2Low Speed


Discrete Outputs WorksheetConnections For Aircraft Types

Pin Discrete Outputs FlashingLamp 68

MP15D Glideslope Cancel N/A '��!��-�� !� "�� '�$�

MP3D Below G/S Caution Yes '��!��-�� #$%�� '�$�

MP7BAll


Yes '��!��-�� '�$�

TP12C Windshear Caution Yes �� "�� '�$�

TP12A Windshear Warning Yes �� - '�$�

TP12B Audio On N/A "#� &��%��


TP10D

SpareOr

Terrain Display discrete #1(Used for Alt Display PPIN 18

State 2 only)

N/A

MP14C

SpareOr


State 2 only)

N/A


MP7C GPWS Monitor N/A �� #&' '�$�

TP12D Windshear Monitor N/A �� '�$�

TP11B Terrain Not Available N/A �� &2�� '�$�



MP3D All GPWS Cautions No '��!��-�� #$%�� '�$�

MP7B All GPWS Warnings (“Pull Up”) No '��!��-�� 3� '�$�

Allied Signal, Inc.


A-13.2 Gulfstream IIB/III


Aircraft Type 69

Description Gulfstream IIB/III



ADC Single (ARINC 429 or RS-575)

AHRS/IRS Dual (will use either IRS or AHRS inputs as provided)


ILS

RASingle

AOA Dual


SingleExternal

GPSSingle GPS

PP

IN 7

DualExternal

GPSDual GPS

LRRASingle (use Alternate RA Configuration to select)

Replaces Analog RAAlternate ILS

FormatSingle digital ILS

Replaces Analog ILS


Dual MFD (Select PPIN 18 State 2 to enable)Or

Dual EFIS (Select PPIN 18 State 3 to enable)

FEATURES



No


ARINC 429 DH No


Lamp Format Type 1


Alert Volume High



No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Gulfstream II

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-101

and onNo Display N/A N/A N/A No No Open

2-208

and on

Collins FDS-255(Bus type: ARINC 708Standard Data Format)

No auto ranging

Fan modewith +-91o

limitYes No No No MP3A

3-208

and on

Honeywell EDZ805(Bus type: Honeywell

Proprietary DataFormat)

10NM auto ranging

Honeywell Yes No No No MP15D


Program Pin Strapping for Aircraft Type Gulfstream IIB/III


1 (TP10A) 2 (TP10B) 3 (TP10C)

69 TP12C Open MP3A

Allied Signal, Inc.




AnalogInputChannel

Pins69

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ARINC 552 with Validity Flag)(use Alt. RA Format #1 for ALT 55 with Validity Flag)


2+ = TP14A- = TP14B



Offset: 48.0o

Gain = -6.0o



T P2D(10 VDC)

T P14A (+)

T P14B (-)

3+ = TP13C- = TP13D



4+ = TP14C- = TP14D



Gain = -6.0o



T P2D(10 VDC)

T P14C (+)

T P14D (-)



69Selected?

Default ARINC 552



Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Gulfstream IIB/III


InputChannel

Pins69

Connections

3A=MP11AB=MP11B

ADC #1 – ARINC 429 (Low Speed) 1

Or Not Used

12A=TP8CB=TP8D


4A=MP12AB=MP12B

FMC (Low Speed) 1

OrNot Used

11A=TP8AB=TP8B

Not UsedOr

FMC (High Speed) 1

18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D

Not UsedOr


1A=MP6AB=MP6B



13A=TP5AB=TP6A



8A=MP13AB=MP13B

Not UsedOr

LRRA #1 (Left) (Low Speed) (use Alt RA format #2 to enable)

5A=MP10AB-MP10B

Not UsedOr

MFD #1 range (Select Alt Display PPIN 18 State 2)Or

Left EFIS range (Select Alt Display PPIN 18 State 3)

7A=MP12CB=MP12D

Not UsedOr

MFD #2 range (Select Alt Display PPIN 18 State 2)Or

Right EFIS range(Select Alt Display PPIN 18 State 3)






16A=TP5CB=TP5D

Not Used ��


Allied Signal, Inc.









ConfigurationOption 2 - FMC #1


Allied Signal, Inc.


Discrete Inputs Worksheet Gulfstream IIB/III



REQUIRED


��


Landing Flap/FlapOverride MP9C

Ground = Landing Flap Selected;Open = Not Landing Flap

��

��

��


#$%�� #��

ILS Select MP14A Ground = ILS Selected; Open = Not Selected &'� �� '��

Terrain Awareness & TCFInhibit

MP14B Ground = Inhibit; Open = Normal #�� &��%��

Alternate Radio AltimeterValidity

TP15A +28V = Valid; 0V = Not Valid �� #��

Glideslope Valid TP15B +28V = Valid; 0V = Not Valid &'� ��





OPTIONAL

Back Course Select MP1B Ground = Glideslope Inhibit; Open = Not Inhibit &'� 4��



Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal�� - �� /� �!�

�� %��

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled #��



"�� #��

��


Terrain Display Select #1 TP1A Momentary Ground SwitchUsed for Alt Display PPIN 18 State 2 only

Openor

Left Terrain Select Switch

Terrain Display Select #2 TP1B Momentary Ground SwitchUsed for Alt Display PPIN 18 State 2 only

OpenOr

Right Terrain Select Switch

Steep Approach #1 TP4C Ground = Enabled; Open = Disabled #��

Steep Approach #2 MP5D Ground = Selected; Open = Not Selected"�� #��

��

NOT USED


MP1A N/A Open

MP2D N/A Open

TP15C N/A Open


Allied Signal, Inc.


Serial Outputs Worksheet Gulfstream IIB/III


ChannelPins

69Connections

TX453-1A=TP3AB=TP3B

Not UsedOr

Terrain Display data LH(Used for Alt Display PPIN 18 State 2 only)


TX453-2A=TP3CB=TP3D

Not UsedOr

Terrain Display data RH(Used for Alt Display PPIN 18 State 2 only)


TX429-1Low Speed


TX429-2Low Speed




Lamp 69

MP15D Glideslope Cancel N/A '��!��-�� !� "�� '�$�

MP3D Below G/S Caution Yes '��!��-�� #$%�� '�$�

MP7BAll


Yes '��!��-�� '�$�

TP12C Windshear Caution Yes '��!��-�� #$%�� "�� '�$�

TP12A Windshear Warning Yes '��!��-�� - '�$�



TP10D

SpareOr


State 2 only)

N/A

MP14C

SpareOr


State 2 only)

N/A


MP7C GPWS Monitor N/A #$%�� &2�� '�$�

TP12D Windshear Monitor N/A #$%�� &2�� '�$�

TP11B Terrain Not Available N/A #$%�� &2�� '�$�



MP3D All GPWS Cautions No '��!��-�� #$%�� '�$�

MP7B All GPWS Warnings (“Pull Up”) No '��!��-�� 3� '�$�

Allied Signal, Inc.


A-13.3 Gulfstream IV


Aircraft Type 79 87

Description Gulfstream IVGulfstream IV

With Dual ADC/IRS/RA



ADC Single (ARINC 429 or 575) Dual (ARINC 429)

FMC

ILSDual

IRS

Analog RASingle Dual

AOA Dual


SingleExternal

GPSSingle GPS

DualExternal

GPSDual GPS

PP

IN 7


Triple ILS N/A

LRRASingle

Use Alternate RA Configuration to select;Replaces Analog RA

N/A

FEATURES



No


ARINC 429 DH No


Lamp Format Type 1

Mode 6 Volume Low

Alert Volume Low

Steep Approach N/A


No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Gulfstream IV

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-104

and on

Honeywell SPZ8x00Integrated, 8x8



Honeywell Yes N/A No Yes1 Open

1 –208 and on.Note: Prior to version –208, the display option for Program Pin State 1 is the required display. Program Pin 18 wasadded in version –208.



1 (TP10A) 2 (TP10B) 3 (TP10C)

79 TP4D MP3A MP3A

87 TP4D MP15D MP3A

Allied Signal, Inc.




AnalogInputChannel

Pins79

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ARINC 552 with Validity Flag)(use Alt. RA Format #1 for ALT 55 with Validity Flag)


2+ = TP14A- = TP14B

Right SWC – Vane AOAFormat: DC voltage + Validity Flag, Range: 0 – 10 VDC

Offset: -18o

Gain = 5.555555o

Range = -18 to +42o

3+ = TP13C- = TP13D

Not Used 2�� 3��

4+ = TP14C- = TP14D

Left SWC – Vane AOAFormat: DC voltage + Validity Flag, Range: 0 – 10 VDC

Offset: -18o

Gain = 5.555555o

Range = -18 to +42o


AnalogInputChannel

Pins87

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ARINC 552 with Validity Flag)

2+ = TP14A- = TP14B

Radio Altimeter #2 (ARINC 552 with Validity Flag)

3+ = TP13C- = TP13D

Right SWC – Vane AOAFormat: DC voltage + Validity Flag, Range: 0 – 10 VDC

Offset: -18o

Gain = 5.555555o

Range = -18 to +42o

4+ = TP14C- = TP14D

Left SWC – Vane AOAFormat: DC voltage + Validity Flag, Range: 0 – 10 VDC

Offset: -18o

Gain = 5.555555o

Range = -18 to +42o



79 87Selected?

Default ARINC 552

Alternate RA Configuration #1 ALT 55 N/A

Alternate RA Configuration #2 ARINC 429 N/A

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Gulfstream IV


InputChannel

Pins79

Connections

3A=MP11AB=MP11B

ADC #1 -ARINC 429 (Low Speed) 1

OrNot Used

12A=TP8CB=TP8D

Not UsedOr


9A=TP9CB=TP9D FMC #1 (Low Speed) �5" 6)

4A=MP12AB=MP12B FMC #2 (Low Speed) �5" 6*

13A=TP5AB=TP6A

Not UsedOr


6A=MP11CB=MP11D

Not UsedOr


5A=MP10AB-MP10B

ILS #1 (Low Speed) &'� 6)

7A=MP12CB=MP12D ILS #2 (Low Speed) &'� 6*

10A=TP9AB=TP9B

Not UsedOr

ILS #3 (Low Speed)

1A=MP6AB=MP6B

IRS #1 (High Speed) &�� 6)

8A=MP13AB=MP13B

Not UsedOr

LRRA #1 (Left) (Low Speed)(will use if Alt RA format selected)




15A=TP4AB=TP4B

Not Used ��

16A=TP5CB=TP5D

Not Used ��

17A=TP11CB=TP11D

Not Used ��

18A=MP6CB=MP6D

Not Used ��





Connections

Alternate GPSSpeed





-204 and on FMC #1Use if Nav Mode label 266 is

available 79

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Gulfstream IV


InputChannel

Pins87

Connections

3A=MP11AB=MP11B

ADC #1 - ARINC 429 (Low Speed) #�" 6)

15A=TP4AB=TP4B

ADC #2 – ARINC 429 (Low Speed) #�" 6*

9A=TP9CB=TP9D

FMC #1 (Low Speed) �5" 6)


13A=TP5AB=TP6A

Not UsedOr


6A=MP11CB=MP11D

Not UsedOr


5A=MP10AB-MP10B ILS #1 (Low Speed) &'� 6)

7A=MP12CB=MP12D

ILS #2 (Low Speed) &'� 6*

1A=MP6AB=MP6B

IRS #1 (High Speed) &�� 6)

12A=TP8CB=TP8D

IRS #2 (High Speed) &�� 6*

















ConfigurationOption 2 -206 and on FMC #1


Allied Signal, Inc.


Discrete Inputs Worksheet Gulfstream IV



REQUIRED


��



#��

�/��

Glideslope Cancel MP9D Momentary Ground = Cancel; Open = Normal "�� !� "��


MP2D Ground = Inhibit; Open = Normal #�� &��%��

Radio Altimeter #1 Valid TP15A +28V = Valid; 0V = Not Valid �� #�� 6) ��


TP15C +28V = Fail; 0V = Valid ��-�� " ��


TP15D +28V = Fail; 0V = Valid '�� " ��





OPTIONAL



Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal "�� /��

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled "�� #� #' ��

REQUIRED ONLY IF TERRAIN DISPLAY USED

Range 2-A MP1A Ground = Not Selected; Open = SelectedRight WXR Control Panel Pin J2-A ��-�� 7� "��

Range 2-B MP8D Ground = Not Selected; Open = SelectedRight WXR Control Panel Pin J2-B ��-�� 7� "��

Range 2-C MP14B Ground = Not Selected; Open = SelectedRight WXR Control Panel Pin J2-C ��-�� 7� "��

Range 2-D TP1A Ground = Not Selected; Open = SelectedRight WXR Control Panel Pin J2-D ��-�� 7� "��

Range 1-A TP1B Ground = Not Selected; Open = SelectedLeft WXR Control Panel Pin J2-A '�� 7� "��

Range 1-B MP2B Ground = Not Selected; Open = SelectedLeft WXR Control Panel Pin J2-B '�� 7� "��

Range 1-C TP4C Ground = Not Selected; Open = SelectedLeft WXR Control Panel Pin J2-C '�� 7� "��

Range 1-D MP5D Ground = Not Selected; Open = SelectedLeft WXR Control Panel Pin J2-D '�� 7� "��

NOT REQUIRED

NAV 2 Discrete(ILS Bus Select #1)

MP14A N/A Open

AUX 1 Discrete(ILS Bus Select #2)

TP15B N/A Open

Left Terrain Displayed MP2A N/A Open

Right Terrain Displayed MP7A N/A Open

Allied Signal, Inc.


Discrete Inputs Worksheet Gulfstream IV



REQUIRED


��



#��

�/��

Glideslope Cancel MP9D Momentary Ground = Cancel; Open = Normal "�� !� "��



Radio Altimeter #1 Valid TP15A +28V = Valid; 0V = Not Valid �� #�� 6) ��

Radio Altimeter #2 Valid TP15B +28V = Valid; 0V = Not Valid �� #�� 6* ��


TP15C +28V = Fail; 0V = Valid ��-�� " ��


TP15D +28V = Fail; 0V = Valid '�� " ��





OPTIONAL



Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal "�� /��

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled "�� #� #' ��

REQUIRED ONLY IF TERRAIN DISPLAY USED

Range 2-A MP1A Ground = Not Selected; Open = SelectedRight WXR Control Panel Pin J2-A ��-�� 7� "��

Range 2-B MP8D Ground = Not Selected; Open = SelectedRight WXR Control Panel Pin J2-B ��-�� 7� "��

Range 2-C MP14B Ground = Not Selected; Open = SelectedRight WXR Control Panel Pin J2-C ��-�� 7� "��

Range 2-D TP1A Ground = Not Selected; Open = SelectedRight WXR Control Panel Pin J2-D ��-�� 7� "��

Range 1-A TP1B Ground = Not Selected; Open = SelectedLeft WXR Control Panel Pin J2-A '�� 7� "��

Range 1-B MP2B Ground = Not Selected; Open = SelectedLeft WXR Control Panel Pin J2-B '�� 7� "��

Range 1-C TP4C Ground = Not Selected; Open = SelectedLeft WXR Control Panel Pin J2-C '�� 7� "��

Range 1-D MP5D Ground = Not Selected; Open = SelectedLeft WXR Control Panel Pin J2-D '�� 7� "��

NOT REQUIRED

NAV 2 Discrete(ILS Bus Select #1)

MP14A N/A Open

Left Terrain Displayed MP2A N/A Open

Right Terrain Displayed MP7A N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet Gulfstream IV


ChannelPins

79, 87Connections

TX453-1A=TP3AB=TP3B

Terrain display data to symbol generator relays �� 6)8 6*8 6+

TX453-2A=TP3CB=TP3D

Not used 2�� 3��

TX429-1Low Speed

A=MP1CB=MP1D

ICD Appendix E label sets: E-1/2/3/5/6/9/12 �� 6)8 6*8 6+

TX429-2Low Speed

A=TP2AB=TP2B

ICD Appendix E label sets: E-1/2/3/5/6/9/12 2�� 3��



Lamp 79, 87

MP15D Glideslope Cancel N/A '��!��-�� 4�� 0�� &��1 '�$�

MP3D Below G/S Caution Yes '��!��-�� #$%�� 4�� '�$�

MP7BAll


Yes '��!��-�� 3� '�$�

TP12C Windshear Caution Yes '��!��-�� #$%�� !� "�� '�$�

TP12A Windshear Warning Yes '��!��-�� !� ��- '�$�



TP10D Terrain Display Discrete #1 N/A �� '�� "��

MP14C Terrain Display Discrete #2 N/A �"�� -�� "��


MP7C GPWS Monitor N/A #$%�� #&' �� /�� #3

TP12D Windshear Monitor N/A #$%�� #&' �� /�� #3

TP11B Terrain Not Available N/A �� /�� 5��



MP3D All GPWS Cautions No'��!��-�� #$%�� '�$� �� 8 ��$� 04��

�!�1 ��$� �� 0��1 ��$�


Allied Signal, Inc.


A-13.4 Gulfstream V



Description Gulfstream V with 2 ILS Buses Gulfstream V with 4 ILS Buses



ADC

AOA

DAU

FMC

GPS

Dual

ILS Dual Four

IRS Dual

Analog RA Dual


There are no optional system inputs for these aircraft.

FEATURES



No


ARINC 429 DH Yes


Lamp Format Type 1


Alert Volume 3 (low)



No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-104

and on

Honeywell SPZ8x00Integrated, 8x8


Format)10 NM auto rangingcontrolled by display

Honeywell Yes N/A No Yes Open


Program Pin Strapping for Aircraft Type Gulfstream V


1 (TP10A) 2 (TP10B) 3 (TP10C)

96 Open MP7B MP3A

104 Open TP12C MP3A



AnalogInputChannel

Pins96, 104

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ARINC 552 with Validity Discrete) �# 6)

2+ = TP14A- = TP14B

Radio Altimeter #2 (ARINC 552 with Validity Discrete) �# 6*

3+ = TP13C- = TP13D Not Used 2�� 3��

4+ = TP14C- = TP14D Not Used 2�� 3��


The Radio Altimeter data format is analog ARINC 552. Alternate RA formats do not apply to

Aricraft Types 96 and 104.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Gulfstream V


InputChannel

Pins96 104

Connections

3A=MP11AB=MP11B

ADC #1 - ARINC 429 (Low Speed) #�" 6)

15A=TP4AB=TP4B

ADC #2 - ARINC 429 (Low Speed) #�" 6*

7A=MP12CB=MP12D

AOA #1 (Low Speed) #�# 6)

14A=TP1CB=TP1D AOA #2 (Low Speed) #�# 6*

10A=TP9AB=TP9B DAU #1 (Low Speed) �#3 6)

2A=MP10CB=MP10D DAU #2 (Low Speed) �#3 6*

9A=TP9CB=TP9D FMC #1 (Low Speed) �5" 6)


13A=TP5AB=TP6A GPS #1 (Low Speed – ARINC 743A) �� 6)

8A=MP13AB=MP13B GPS #2 (Low Speed – ARINC 743A) �� 6*

5A=MP10AB-MP10B ILS #1 (Nav #1) (Low Speed) &'� 6)

11A=TP8AB=TP8B

ILS #2 (Nav #2) (Low Speed) &'� 6*

6A=MP11CB=MP11D

Not Used ILS #3 (Aux Nav #1)(Low Speed)

16A=TP5CB=TP5D

Not Used ILS #4 (Aux Nav #2)(Low Speed)

1A=MP6AB=MP6B IRS #1 (High Speed) &�� 6)

12A=TP8CB=TP8D IRS #2 (High Speed) &�� 6*



Provide only one ADC input as indicated by bus format; provide only one FMC input as indicated by bus speed.




16Alternate GPSSpeed -10 and on GPS #1, #2 High Speed bus(es) 96, 104

Allied Signal, Inc.


Discrete Inputs Worksheet Gulfstream V



REQUIRED


��

Flap Override MP9C Ground = Flap Override; Open = Not FlapOverride

#��

� ��


#$%�� #��



NAV 2 Discrete(NAV Bus Select #1)

MP14A Ground = Selected; Open = Not Selected &'� �� '��

Radio Altitude #1 Valid TP15A +28V = Valid; 0V = Not Valid �� #�� 6) ��

Radio Altitude #2 Valid TP15B +28V = Valid; 0V = Not Valid �� #�� 6* ��

OPTIONAL



Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal �� /��

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled �#� #' ��



"�� #��

��




��

NOT USED


MP1A N/A Open

MP5C N/A Open

MP14B N/A Open

TP1A N/A Open

TP1B N/A Open

MP2B N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open

Allied Signal, Inc.


Discrete Inputs Worksheet Gulfstream V



REQUIRED


��

Flap Override MP9CGround = Flap Override;

Open = Not Flap Override

��

��

��


#$%�� #��



AUX 2 Discrete(NAV Bus Select #3)

MP1A Ground = Selected; Open = Not Selected &'� �� '��

NAV 2 Discrete(NAV Bus Select #1)

MP14A Ground = Selected; Open = Not Selected

AUX 1 Discrete(NAV Bus Select #2)

MP14B Ground = Selected; Open = Not Selected

Radio Altitude #1 Valid TP15A +28V = Valid; 0V = Not Valid �� #�� 6) ��

Radio Altitude #2 Valid TP15B +28V = Valid; 0V = Not Valid �� #�� 6* ��

OPTIONAL



Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal �� /��

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled �#� #' ��



"�� #��

��




��

NOT USED


MP5C N/A Open

TP1A N/A Open

TP1B N/A Open

MP2B N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet Gulfstream V


ChannelPins

96, 104Connections

TX453-1A=TP3AB=TP3B

Terrain display data to symbol generator relays �� 6)8 6*8 6*

TX453-2A=TP3CB=TP3D


TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B

To SGs, CAS and FDAU.Transmits ICD Appendix E label sets: E-1C/2/3/5/6/9/12 �� 6)8 6*8 6+



Lamp 96, 104

MP15D Glideslope Cancel N/A '��!��-�� 4�� &��%�� $�

MP3D Below G/S Caution Yes '��!��-�� #$%�� 4�� !� '�$�

MP7BAll


Yes ��

TP12C Spare Yes ��

TP12A Spare Yes ��



TP10D Terrain Display Discrete #1 N/A �� '�� "��

MP14C Terrain Display Discrete #2 N/A �"�� -�� "��


MP7C GPWS Monitor N/A �� "#��

TP12D Windshear Monitor N/A �� "#��




MP3D All GPWS Cautions No'��!��-�� #$%�� '�$� �� 8 ��$� 04��

�!�1 ��$� �� 0��1 ��$�


Allied Signal, Inc.


A-14 Hawker

A.14.1 Hawker 800



DescriptionHawker 800 with

Pro Line 2 displayand Pot AOA

Hawker 800 with ProLine 2 display and

SafeFlight AOA

Hawker 800 withHoneywell EFIS and

Pot AOA

Hawker 800 withHoneywell EFIS and

SafeFlight AOA

P/N Availability -101 or later -101 or later 101 or later -102 or later


ADC Single (ARINC 429 or 575)

FMC Single (High or Low Speed)

IRS Single (single AHRS optional) Single

ILS Single

RA Single

AOASingle

(Potentiometer)Single SafeFlight Single (Potentiometer) Single SafeFlight


SingleExternal

GPSSingle GPS

DualExternal

GPSDual GPS

PP

IN 7


Dual WX Control Panel inputs(Range Control Buses)

Dual EFIS inputsRequired for displays

Alternate RAFormat

Single LRRAUse Alternate RA Configuration #2 - replaces Analog RA

Alternate ILSFormat

Single digital ILSWill use if provided – replaces Analog ILS

FEATURES



No


ARINC 429 DH No


Lamp Format Type 1


Alert Volume High



No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Hawker 800

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-204

and on

Collins ProLine 2Non-Integrated, 5x6


No auto ranging

Defaultwith +-60o



1-101

and on

Honeywell SPZ8000Integrated, 5x6





1-101

and on

Collins ProLine 2Non-Integrated, 5x6


No auto ranging

Defaultwith +-60o





1 (TP10A) 2 (TP10B) 3 (TP10C)

65 MP3A Open MP3A

66 MP15D Open MP3A

73 MP3A MP3A MP3A

138 MP15D MP3A MP15D

Allied Signal, Inc.




AnalogInputChannel

Pins65

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ALT 55 with Validity Discrete)Or

Not Used (use Alt. RA Configuration #2 to select digital RA)

2+ = TP14A- = TP14B

Not Used ��

3+ = TP13C- = TP13D



4+ = TP14C- = TP14D

Left Vane, PotentiometerFormat: 0 –10 VDC

Offset: 38.22o

Gain = -4.44o



T P2D(10 VDC)

T P14C (+)

T P14D (-)


AnalogInputChannel

Pins66

Connections

1+ = TP13A- = TP13B




3+ = TP13C- = TP13D



4+ = TP14C- = TP14D

Left Vane, PotentiometerFormat: 0 –10 VDC

Offset: 38.22o

Gain = -4.44o



T P2D(10 VDC)

T P14C (+)

T P14D (-)


AnalogInputChannel

Pins73

Connections

1+ = TP13A- = TP13B

Radio Altimeter #1 (ALT 50/55 with Validity Discrete)Or



3+ = TP13C- = TP13D



4+ = TP14C- = TP14D

AOA Indication SystemFormat: +-10 VDC

Offset: 15o

Gain = -3.333333o

Range = -15 to +45o

Allied Signal, Inc.


Analog Input Channel Assignment Haw ker 800


AnalogInputChannel

Pins138

Connections

1+ = TP13A- = TP13B



2+ = TP14A- = TP14B

Not Used ��

3+ = TP13C- = TP13D



4+ = TP14C- = TP14D

AOA Indication SystemFormat: +-10 VDC

Offset: 15o

Gain = -3.333333o

Range = -15 to +45o



65, 66, 73, 138Selected?

Default ALT 55



Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Hawker 800


InputChannel

Pins65, 73

Connections

3A=MP11AB=MP11B


Or Not Used

12A=TP8CB=TP8D

Not UsedOr ADC #1 - ARINC 429 (Low Speed) 1

2A=MP10CB=MP10D

FMC (High Speed) 1

OrNot Used

11A=TP8AB=TP8B

Not usedOr

FMC (Low Speed) 1

18A=MP6CB=MP6D

Not UsedOr

GPS #1 ARINC 743A (Low Speed)

17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D

Not UsedOr

ILS #1 (Low Speed)

1A=MP6AB=MP6B

IRS #1 (High Speed) PreferredOr


8A=MP13AB=MP13B

Not UsedOr


5A=MP10AB-MP10B

Not UsedOr

WX Control Panel Bus #1 (Low Speed)

7A=MP12CB=MP12D

Not UsedOr

WX Control Panel Bus #2 (Low Speed)

4A=MP12AB=MP12B

Not Used ��

9A=TP9CB=TP9D

Not Used ��

10A=TP9AB=TP9B

Not Used ��






ARINC 429 Interface Modification Options Worksheet Hawker 800





-206 and on GPS #1, #2Use if ARINC 743 and not

ARINC 743A 65, 7316


Use if Nav Mode label 266is available 65, 66, 73, 138

Allied Signal, Inc.




InputChannel

Pins66, 138

Connections

3A=MP11AB=MP11B


Or Not Used

12A=TP8CB=TP8D

Not UsedOr ADC #1 - ARINC 575 (Low Speed) 1

7A=MP12CB=MP12D

Not UsedOr

EFIS Bus (Low Speed)(MG Multifunction SG Left Bus)

9A=TP9CB=TP9D

Not UsedOr

EFIS Bus (Low Speed)(MG Multifunction SG Right Bus)

2A=MP10CB=MP10D

FMC (High Speed) 1

OrNot Used

11A=TP8AB=TP8B

FMC (Low Speed) 1

OrNot Used

18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D

Not UsedOr

ILS #1 (Low Speed)

1A=MP6AB=MP6B IRS #1 (High Speed)

8A=MP13AB=MP13B

Not UsedOr





13A=TP5AB=TP6A

Not Used ��

14A=TP1CB=TP1D

Not Used ��

15A=TP4AB=TP4B

Not Used ��

16A=TP5CB=TP5D

Not Used ��







Use if ARINC 743 and notARINC 743A 66, 13816


- FMCUse if Nav Mode label 266

is available 65, 66, 73, 138

Allied Signal, Inc.


Discrete Inputs Worksheet Hawker 800



REQUIRED


��

��



��

��!�� "��


�#� $�� %&'��

�� % ��

ILS Select 1 MP14A Ground = ILS Selected;Open = Not Selected ()� �� )��


MP14B Ground = Inhibit; Open = Normal % � �� (��'��

Radio Altitude Valid TP15A +28V = Valid; 0V = Not Valid �� % � "� ��

Glideslope Valid 1 TP15B +28V = Valid; 0V = Not Valid ()� � �� "� ��

Flap Position #1 (0 o) TP7A +28V = Selected; 0V = Not Selected �� *� ��

Flap Position #2 (15 o) TP7B +28V = Selected; 0V = Not Selected �� +,� ��

Flap Position #3 (25 o) TP7C +28V = Selected; 0V = Not Selected �� -,� ��

Flap Position #4 (45 o) TP7D +28V = Selected; 0V = Not Selected �� .,� ��

OPTIONAL

Glideslope Inhibit MP1B Ground = Inhibit; Open = Not Inhibit ()� /��!��

Mode 6 Volume Control MP2A Ground = Low Volume; Open = Normal %��

Decision Height MP5C Ground = <DH; Open = >DH �� % � �0 '�1 ��

Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal�� 1 �� 2� �#�

�� '��

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled %��



$��!�� %��

��

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Not Inhibit 3��4 ��

Display Select #1 TP1A Momentary Ground Switch Left Terrain Select Switch

Display Select #2 TP1B Momentary Ground Switch Right Terrain Select Switch

Steep Approach #1 TP4C Ground = Enabled; Open = Disabled %��

Steep Approach #2 MP5D Ground = Selected; Open = Not Selected$��!�� %��

��

NOT USED


MP1A N/A Open

MP2D N/A Open

TP15C N/A Open


Allied Signal, Inc.





REQUIRED


��

��



��

��!�� "��


�#� $�� %&'��

�� % ��

ILS Select 1 MP14A Ground = ILS Selected; Open = Not Selected ()� �� )��









OPTIONAL





�� '��




$��!�� %��

��




��

NOT USED


MP1A N/A Open

MP2D N/A Open

Display Select #1 TP1A N/A Open

Display Select #2 TP1B N/A Open

TP15C N/A Open


Allied Signal, Inc.





REQUIRED


��

��



��

��!�� "��


�#� $�� %&'��

�� % ��






AOA Valid TP15D +28V = Valid; 0V = Not Valid





OPTIONAL





�� '��




$��!�� %��

��


Display Select #1 TP1A Momentary Ground Switch )��

Display Select #2 TP1B Momentary Ground Switch ��1��



��

NOT USED


MP1A N/A Open

MP2D N/A Open

TP15C N/A Open1 ILS Select and Glideslope Valid not required if digital ILS provided. (EGPWS will automatically use digital ILS ifprovided.)

Allied Signal, Inc.





REQUIRED


��

��



��

��!�� "��


�#� $�� %&'��

�� % ��

ILS Select MP14A Ground = ILS Selected; Open = Not Selected ()� �� )��




Glideslope Valid TP15B +28V = Valid; 0V = Not Valid ()� � �� "� ��






OPTIONAL





�� '��




$��!�� %��

��




��

NOT USED


Display Select #1 TP1A DO NOT USE Open

Display Select #2 TP1B DO NOT USE Open

MP1A N/A Open

MP2D N/A Open

TP1A N/A Open

TP1B N/A Open

TP15C N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet Hawker 800


ChannelPins

65, 73Connections

TX453-1A=TP3AB=TP3B

Left side picture bus to symbol generator port )�� #�5� ��

TX453-2A=TP3CB=TP3D

Right side picture bus to symbol generator port��1�� #�5�

��

TX429-1Low Speed

A=MP1CB=MP1D Transmits ICD Appendix E label sets: E-1/2/3/5/6/9/12 ��

TX429-2Low Speed

A=TP2AB=TP2B

Transmits ICD Appendix E label sets: E-1/2/3/5/6/9/12 ��


ChannelPins

66, 138Connections

TX453-1A=TP3AB=TP3B Left side picture bus to symbol generator port 0�� 6+7 8�

TX453-2A=TP3CB=TP3D Right side picture bus to symbol generator port 0�� 6-7 8�

TX429-1Low Speed

A=MP1CB=MP1D Transmits ICD Appendix E label sets: E-1/2/3/5/6/9/12 0�� 6+9-7 8�

TX429-2Low Speed

A=TP2AB=TP2B Transmits ICD Appendix E label sets: E-1/2/3/5/6/9/12 ��

Allied Signal, Inc.


Discrete Outputs Worksheet Hawker 800


Lamp 65, 73

MP15D Glideslope Cancel N/A )��#��1�� %&'�� )�&� ��

MP3D Below G/S Caution Yes )��#��1�� %&'�� #� )�&�

MP7BAll


Yes )��#��1�� )�&�

TP12C Windshear Caution Yes )��#��1�� %&'�� $�� )�&

TP12A Windshear Warning Yes )��#��1�� 1 )�&

TP12B Audio On N/A �$%� (��'��


TP10D Terrain Display Discrete #1 N/A )��

MP14C Terrain Display Discrete #2 N/A ��1��


MP7C GPWS Monitor N/A %&'�� (�� )�&

TP12D Windshear Monitor N/A %&'�� (�� )�&

TP11B Terrain Not Available N/A %&'�� (�� )�&



MP3D All GPWS Cautions No )��#��1�� %&'�� )�&�

MP7B All GPWS Warnings (“Pull Up”) No )��#��1�� )�&�


Lamp 66, 138

MP15D Glideslope Cancel N/A )��#��1�� %&'�� )�&� ��

MP3D Below G/S Caution Yes )��#��1�� %&'�� #� )�&�

MP7BAll


Yes )��#��1�� )�&�

TP12C Windshear Caution Yes )��#��1�� %&'�� $�� )�&

TP12A Windshear Warning Yes )��#��1�� 1 )�&






MP7C GPWS Monitor N/A %&'�� (�� )�&

TP12D Windshear Monitor N/A %&'�� (�� )�&

TP11B Terrain Not Available N/A %&'�� (�� )�&





Allied Signal, Inc.


A.14.2 Hawker 1000


Aircraft Type 67

Description Hawker 1000



ADC Single (ARINC 429 or 575)

IRS Single


ILS

RASingle

AOA Dual


SingleExternal

GPSSingle GPS

DualExternal

GPSDual GPS

PP

IN 7


Dual EFISRequired for displays

LRRASingle (use Alternate RA Configuration #2 to select)

Replaces Analog RAAlternate ILS

FormatSingle digital ILS

Replaces Analog ILS

FEATURES



No


ARINC 429 DH No


Lamp Format Type 1


Alert Volume High



No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Hawker 1000

PPINState


Display SweepStyle

AutoPop Up

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-102

and on

Honeywell SPZ8000Integrated, 5x6







1 (TP10A) 2 (TP10B) 3 (TP10C)

67 MP3D Open MP3A



AnalogInputChannel

Pins67

Connections

1+ = TP13A- = TP13B


Not used


3+ = TP13C- = TP13D



4+ = TP14C- = TP14D

AOA Indication SystemFormat: +-10 VDC (Safe Flight DC Analog)

Offset: 15o

Gain = -3.333333o

Range = -14 to +45o (+ = nose up)



67Selected?

Default ARINC 552



Allied Signal, Inc.




InputChannel

Pins67

Connections

3A=MP11AB=MP11B


orNot Used

12A=TP8CB=TP8D


OrNot Used

7A=MP12CB=MP12D

Not UsedOr

EFIS Bus (Low Speed) (MG Multifunction SG Left Bus)

9A=TP9CB=TP9D

Not UsedOr

EFIS Bus (Low Speed) (MG Multifunction SG Right Bus)

2A=MP10CB=MP10D

FMC (Low Speed) 1

OrNot Used

11A=TP8AB=TP8B

Not UsedOr

FMC (High Speed) 1

18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D

Not UsedOr


1A=MP6AB=MP6B IRS #1 (High Speed)

8A=MP13AB=MP13B

Not UsedOr





13A=TP5AB=TP6A

Not Used ��

14A=TP1CB=TP1D

Not Used ��

15A=TP4AB=TP4B

Not Used ��

16A=TP5CB=TP5D

Not Used ��









- FMCUse if Nav Mode label 266

is available 67

Allied Signal, Inc.


Discrete Inputs Worksheet



REQUIRED


��

��



��

��!�� "��


�#� $�� %&'��

�� % ��











OPTIONAL





�� '��




$��!�� %��

��




��

NOT USED


Display Select 1 TP1A DO NOT USE Open

Display Select 2 TP1B DO NOT USE Open

MP1A N/A Open

MP2D N/A Open

TP15C N/A Open1 ILS Select and Glideslope Valid not required if digital ILS provided. (EGPWS will automatically use digital ILS ifprovided.)

Allied Signal, Inc.


Serial Outputs Worksheet Hawker 1000


ChannelPins

67Connections

TX453-1 A=TP3AB=TP3B

Left side picture bus 0�� 6+7 8�

TX453-2A=TP3CB=TP3D

Right side picture bus 0�� 6-7 8�

TX429-1Low Speed

A=MP1CB=MP1D

ICD Appendix E label sets: E-1/2/3/5/6/9/12 0�� 6+9-7 8�

TX429-2Low Speed

A=TP2AB=TP2B




Lamp 67

MP15D Glideslope Cancel N/A %&'�� #� $�� &

MP3D Below G/S Caution Yes )��#��1�� %&'�� /� �� #� �&�

MP7BAll


Yes )��#��1�� &�

TP12C Windshear Caution Yes )��#��1�� %&'�� #� $�� &�

TP12A Windshear Warning Yes )��#��1�� #� ��1 �&�






MP7C GPWS Monitor N/A %&'�� (�� &

TP12D Windshear Monitor N/A %&'�� (�� &

TP11B Terrain Not Available N/A %&'�� (�� &





Allied Signal, Inc.


A-15 IAI

A-15.1 Astra SPX


Aircraft Type 90

DescriptionAstra SPX

(Non-Integrated)



ADC

FMC

IOC

Dual


LRRA Single


SingleExternalGPS

Single GPS

DualExternalGPS

Dual GPS

PP

IN 7

OptionalInputSelect


PP

IN 9 Dual RADual LRRA

Applies only to ARINC 429 LRRA inputs

Analog RASingle (use Alt. RA format to enable)Replaces Single ARINC 429 LRRA

FEATURES



No



Yes


Lamp Format Type 1


Alert Volume High



No

WindshearDetection

Yes

Allied Signal, Inc.


Display Options & Peaks Availability Astra SPX

PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-105

and on

Collins ProLine IV Non-Integrated


No auto ranging

Defaultwith +/-60o limit

No Yes No No Open

Note: Prior to version –208, the display option for Program Pin State 1 is the required display. Program Pin 18 wasadded in –208.



1 (TP10A) 2 (TP10B) 3 (TP10C)

90 MP15D MP3D MP3A



AnalogInputChannel

Pins90

Connections

1+ = TP13A- = TP13B

Not UsedOr

Radio Altimeter #1 (ARINC 552 with Validity Discrete)Use Program Pin14 to enable

2+ = TP14A- = TP14B

Not Used ��

3+ = TP13C- = TP13D

Not Used ��

4+ = TP14C- = TP14D

Right Vane PotentiometerRange: 0-10 VDCOffset = -23.8889o

Gain = 7.77778Electrical Range = 77.77o


C W

CW

=IN

CR

EA

SII

NG

AO

ATP2D(10 VDC)

TP14C (+)

TP14D (-)

� ��


Radio Altimeter Alternatives Format Selected?

Default ARINC 429



Note: The alternate RA formats are only applicable for a single RA input. (Do not enable

the Dual LRRA overlay if analog RA is used.)

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Astra SPX


ARINC429

InputChannel

Pins90

Connections

4A=MP12AB=MP12B





5A=MP10AB-MP10B

Not usedor

GPS #1 (Low Speed)

11A=TP8AB=TP8B

Not usedor

GPS #2 (Low Speed)

2A=MP10CB=MP10D IOC #1 (High Speed) ��

3A=MP11AB=MP11B IOC #2 (High Speed) ��

1A=MP6AB=MP6B



13A=TP5AB=TP6A



8A=MP13AB=MP13B

LRRA #1 (Left; Low Speed)Or

Not Used (Select Alt RA format and provide Analog RA if not used)

10A=TP9AB=TP9B

Not UsedOr

LRRA #2 (Right; Low Speed)










Connections

Alternate GPSSpeed




7OptionalInputs Select - FMC #1,#2


Allied Signal, Inc.


Discrete Inputs Worksheet Astra SPX



REQUIRED


�� !�� "��#$ %&�&��' � ��

(�)� )�� & #��*

Landing Gear MP9B Ground = Gear Down; Open = Gear Up (�� " �"��#$

Flap Override MP9C Ground = Flaps Override;Open = Not Flaps Override

�� &�� " �"��#$ � � �� #��

#�#+�� (�)� �� "��#$


(,� �� #�� "��#$ %&�&��' � ��-��

(�)� �� & #��*


MP14B Ground = Inhibit; Open = Normal �� #�� !�� $�-�� "��#$

OPTIONAL

Glideslope Inhibit MP1B Ground = Inhibit; Open = Not Inhibit �.� /�#+#�&�� #��

Mode 6 Volume Control MP2A Ground = Low Volume; Open = Normal ��#�� (��& �

Decision Height MP5C Ground = <DH; Open = >DH �� 0 -&1 �&��&�

Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal�� "�� 1 �� #��2� ),�

�&�� $�-�� &��&�

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled ��#�� (��& �



��#+�� (�)� �&�� &��

�"��#$

Steep Approach #1 MP1A Ground = Enabled; Open = Disabled ��#�� (��& �

Steep Approach #2 MP14A Ground = Selected; Open = Not Selected��#+�� #�� #$

�"��#$

Display Select #1 TP1A Momentary Ground Switch .�� !�� #� �"��#$

Display Select #2 TP1B Momentary Ground Switch �1$� !�� #� �"��#$

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Normal “Ditch” switch

Radio Altimeter #1 Valid TP15A +28 V = Valid; 0 V = Fail Radio Alt Validity

NOT USED


MP2D N/A ��

TP4C N/A ��

MP5D N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.


Serial Outputs Worksheet Astra SPX


ChannelPins

90Connections

TX453-1A=TP3AB=TP3B

Left side picture bus.�� )3,!��

��#� ��'

TX453-2A=TP3CB=TP3D Right side picture bus

�1$� �� )3,!��

��#� ��'

TX429-1Low Speed

A=MP1CB=MP1D Not Used ��

TX429-2Low Speed

A=TP2AB=TP2B Not Used ��



FlashingLamp 90

MP15D Glideslope Cancel N/A .��,�1$� (,� �� #�� .��

MP3D Below G/S Caution No .��,�1$� ��-�� (�� .��

MP7B

When diode ORed withTP4D and TP11A is

all GPWS warnings andcautions

(except Below G/S Caution)

No .��,�1$� �� (�)� .��

TP12C Windshear Caution No .��,�1$� ��' ��1$� ��'

TP12A Windshear Warning No .��,�1$� ��' ��1$� ��'

TP12B Audio On N/A !�� $�-��

TP4D Terrain Awareness Warning N/A .��,�1$� �� (�)� .��

TP10D Terrain Display Discrete #1 N/A .�� !�� #� ��'

MP14C Terrain Display Discrete #2 N/A �1$� !�� #� ��'

TP11A Terrain Awareness Caution N/A .��,�1$� �� (�)� .��

MP7C GPWS Monitor N/A ��-�� (�)� �� .��

TP12D Windshear Monitor N/A ��-�� ),� �� .��

TP11B Terrain Not Available N/A !�� .��



MP3DWhen diode ORed with TP11A

is all GPWS Cautions No .��,�1$� ��-�� (�)� .��

MP7BWhen diode Ored with TP4D is

all GPWS WarningsNo .��,�1$� �� &�� .��

TP4D Terrain Awareness Warning N/A .��,�1$� �� &�� .��

TP11A Terrain Awareness Caution N/A .��,�1$� ��-�� (�)� .��

Allied Signal, Inc.


A-15.2 Galaxy


Aircraft Type 89

Description IAI Galaxy



ADC

DSWC

FMC

IOC

Dual


LRRA Single


SingleExternalGPS

Single GPS

DualExternalGPS

Dual GPS

PP

IN 7

OptionalInputSelect


PP

IN 9 Dual RA Dual LRRA

FEATURES



No


ARINC 429 DH Yes


Lamp Format Type 1


Alert Volume High



No

Windshear Yes1 Added in –208.

Allied Signal, Inc.


Display Options & Peaks Availability IAI Galaxy

PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping

Aircraft Type: 89 (Ref. ICD App G-3.1, 0.1, 3.5)

1-208

and on

Collins ProLine IV Non-Integrated


No auto ranging


No Yes No No Open

2-208

and onNo Display N/A N/A N/A N/A N/A MP3A

3-208

and on

Collins ProLine IV Non-Integrated (with auto

range)(Bus type: ARINC 708Standard Data Format)

10 NM auto ranging


No Yes No No MP15D

Note: Prior to version –208, the display option for Program Pin State 1 is the required display. Program Pin 18 wasadded in version –208.Note: Displays 1 and 3 are identical except Display #3 enables auto range.



1 (TP10A) 2 (TP10B) 3 (TP10C)

89 MP3A MP3D MP3A


There are no analog inputs.


There are no alternate radio altimeter formats.

Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet IAI Galaxy


ARINC429

InputChannel

Pins89

Connections

4A=MP12AB=MP12B

ADC #1 (Low Speed) (L-ADC-2) ��

12A=TP8CB=TP8D

ADC #2 (Low Speed) (R-ADC-2) ��

7A=MP12CB=MP12D

DSWC #1 (Low Speed) (SPQC #1 left channel) ��)� ��

9A=TP9CB=TP9D

DSWC #2 (Low Speed) (SPQC #1 right channel) ��)� ��



5A=MP10AB-MP10B

Not usedor


11A=TP8AB=TP8B

Not usedor


2A=MP10CB=MP10D IOC #1 (High Speed) ��

3A=MP11AB=MP11B

IOC #2 (High Speed) ��

1A=MP6AB=MP6B



13A=TP5AB=TP6A



8A=MP13AB=MP13B

LRRA #1 (Low Speed) (L-RAC-1) .� ��

10A=TP9AB=TP9B

Not UsedOr

LRRA #2 (Low Speed) (R-RAC-1)(select Dual RA to enable)







Types Connections

Alternate GPSSpeed




7OptionalInputs Select

-208 and on FMC #1,#2Use if Nav Mode label 266 is

available 89

Allied Signal, Inc.


Discrete Inputs Worksheet IAI Galaxy



REQUIRED

Self-Test MP9A Momentary Ground = Self-Test; Open = Normal�� !�� "��#$ %&�&��' � ��

(�)� )�� & #��*

Landing Gear MP9B Ground = Gear Down; Open = Gear Up (�� " �"��#$

Glideslope Cancel MP9D Momentary Ground = Cancel; Open = Normal(,� �� #�� "��#$ %�� ..

��,(�� 3 ��*


MP14B Ground = Inhibit; Open = Normal �� #�� !�� $�-�� "��#$

OPTIONAL

Glideslope Inhibit MP1B Ground = Inhibit; Open = Not Inhibit �.� /�#+#�&�� #��

Mode 6 Volume Control MP2A Ground = Low Volume; Open = Normal ��#�� (��& �

Decision Height MP5C Ground = <DH; Open = >DH �� 0 -&1 �&��&�

Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal�� "�� 1 �� #��2� ),�

�&�� $�-�� &��&�

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled ��#�� (��& �



��#+�� (�)� �&�� &��

�"��#$

Flap Override MP9CGround = Flap Override; Open = Not Flap

Override

�� &�� " �"��#$ � � ��

�#�� #�#+�� (�)� ��

�"��#$

Steep Approach #1 MP1A Ground = Enabled; Open = Disabled ��#�� (��& �

Steep Approach #2 MP14A Ground = Selected; Open = Not Selected��#+�� #�� #$

�"��#$

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Normal 4��#$5 �"��#$

Display Select #1 TP1A Momentary Ground SwitchRequired for display .�� !�� ' �"��#$

Display Select #2 TP1B Momentary Ground SwitchRequired for display �1$� !�� ' �"��#$

NOT USED


MP2D N/A ��

TP4C N/A ��

MP5D N/A ��

TP15A N/A ��

TP15B N/A ��

TP15C N/A ��

TP15D N/A ��

TP7A N/A ��

TP7B N/A ��

TP7C N/A ��

TP7D N/A ��

Allied Signal, Inc.


Serial Outputs Worksheet IAI Galaxy


ChannelPins

89Connections

TX453-1A=TP3AB=TP3B

Left side picture bus to Left MFD WX/Terrain select relayOr

Not Used (PPIN 18 State 2 display)

TX453-2A=TP3CB=TP3D

Right side picture bus to Right MFD WX/Terrain selectrelayOr

Not Used (PPIN 18 State 2 display)TX429-1

Low SpeedA=MP1CB=MP1D

Transmits ICD Appendix E label sets: 1/2/3/5/6/9/12 ��

TX429-2Low Speed

A=TP2AB=TP2B

Transmits ICD Appendix E label sets: 1/2/3/5/6/9/12 ��



FlashingLamp 89


MP3D Below G/S Caution No .��,�1$� ��-�� (�� 3 .��

MP7B

When diode OR’ed with TP4Dand TP11A is all GPWSwarnings and cautions


No .��,�1$� �� .. �� .��

TP12C Windshear Caution No .��,�1$� ��' ��1$� ��'

TP12A Windshear Warning No .��,�1$� ��' ��1$� ��'

TP12B Audio On N/A !�� $�-��

TP4D Terrain Awareness Warning N/A .��,�1$� �� .. �� .��

TP10D Terrain Display Discrete #1 N/A .�� !�� #� ��'

MP14C Terrain Display Discrete #2 N/A �1$� !�� #� ��'

TP11A Terrain Awareness Caution N/A .��,�1$� �� (�� 3 .��

MP7C GPWS Monitor N/A ��-�� (�)� �� .��

TP12D Windshear Monitor N/A ��-�� ),� �� .��

TP11B Terrain Not Available N/A ��-�� !�� .��




TP11A is all GPWS cautions No .��,�1$� ��-�� (�� 3 .��


is all GPWS warnings No .��,�1$� �� &�� .��

TP4D Terrain Awareness Warning N/A .��,�1$� �� &�� .��

TP11A Terrain Awareness Caution N/A .��,�1$� ��-�� (�� 3 .��

Allied Signal, Inc.


A-16 Learjet

A-16.1 Learjet Model 45



Description Learjet Model 45 (see Note 1) Learjet Model 45 with Integrated Display



ADC

AOA

AHRS

Dual

FMC Dual (High Speed) Single (Low Speed)

IC N/A Single

RA Single

ILS

Analog Localizer

SingleN/A


SingleExternal

GPSSingle GPS

DualExternal

GPSDual GPS

PP

IN 7


N/A Dual FMC

Alternate RAFormat

Single (use Alternate RA Configuration #2 to select)Replaces Analog RA

Alternate ILSFormat

Single digital ILSReplaces Analog ILS & Localizer

N/A

FEATURES



No


ARINC 429 DH No




Alert Volume High

Steep Approach Yes


No

Windshear Yes

Note 1 – Aircraft Type 102 is to be used for GPWS and Windshear only. It is NOT used for

Terrain Awareness Alerting and Display.

Allied Signal, Inc.


Display Options & Peaks Availability Learjet Model 45

PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping

Aircraft Type: 102

1-102



1-208

and on




Honeywell

Based ondisplay

controllerstrapping(see ICD)

N/A No No Open




1 (TP10A) 2 (TP10B) 3 (TP10C)

102 TP12A MP7B MP3A

166 TP12A MP7B MP15D

Allied Signal, Inc.




AnalogInputChannel

Pins102

Connections

1+ = TP13A- = TP13B


Not Used (use Alt. RA Configuration #2 for digital LRRA)

2+ = TP14A- = TP14B

Not Used ��

3+ = TP13C- = TP13D



4+ = TP14C- = TP14D




AnalogInputChannel

Pins166

Connections

1+ = TP13A- = TP13B


Not Used (use Alt. RA Configuration #2 for digital LRRA)


3+ = TP13C- = TP13D

Not Used ��




102, 166Selected?

Default ARINC 552



Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Learjet Model 45


InputChannel

Pins102

Connections

12A=TP8CB=TP8D


14A=TP1CB=TP1D

ADC #2 ARINC 429 (Low Speed) � ��

1A=MP6AB=MP6B

AHRS #1 (High Speed) ��


7A=MP12CB=MP12D AOA Bus #1 (Low Speed) � �

9A=TP9CB=TP9D AOA Bus #2 (Low Speed) � ��



18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


5A=MP10AB-MP10B Not Used

6A=MP11CB=MP11D

Not UsedOr


8A=MP13AB=MP13B

Not UsedOr

LRRA #1 (Left) (Low Speed)(use Alt RA format #2 to select)












ARINC 743A 10216

ConfigurationOption 2 -204 and on FMC


Allied Signal, Inc.




InputChannel

Pins166

Connections

12A=TP8CB=TP8D


14A=TP1CB=TP1D


1A=MP6AB=MP6B

AHRS #1 (High Speed) ��


7A=MP12CB=MP12D AOA Bus #1 (Low Speed) � �

9A=TP9CB=TP9D AOA Bus #2 (Low Speed) � ��

2A=MP10CB=MP10D FMC #1 (Low Speed) ��

15A=TP4AB=TP4B

Not UsedOr

FMC #2 (Low Speed)

18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


5A=MP10AB-MP10B

IC Data Bus (Low Speed) (IC-600 #1) ��

8A=MP13AB=MP13B

Not UsedOr

LRRA #1 (Left) (Low Speed)(use Alt RA format #2 to select)


4A=MP12AB=MP12B Not Used











ARINC 743A 166

Allied Signal, Inc.


Discrete Inputs Worksheet Learjet Model 45



REQUIRED


�� ! "#�#$��% ��

&'(� ($)� $��#� �$��)*

Landing Gear MP9B Ground = Gear Down; Open = Gear Up &�$) �� !


��$�� #�� ! $�� $�� $ ��

� +�� &'(� ��$�� ,� �� !


&-� �$� �� ! "�$)� �� '�..

�'-&� '��/ �$0�*

ILS Select 1 MP14A Ground = ILS Selected;Open = Not Selected �.� �#�� .� �#��#�


MP2B Ground = Inhibit; Open = Normal �� $ �� ))$�� !�1�� !

Radio Altitude Valid TP15A +28V = Valid; 0V = Not Validonly required for analog RA �$�� ,$��%

Glideslope Valid 1 TP15B +28V = Valid; 0V = Not Validonly required for analog Glideslope �.� &�� ,$��%

Localizer Valid 1 TP15D +28V = Valid; 0V = Not Validonly required for analog Localizer �.� .� $��2�) ,$��%

OPTIONAL

Glideslope Inhibit MP1B Ground = Inhibit; Open = Not Inhibit ��3!� &#��$� � '$��

Mode 6 Volume Control MP2A Ground = Low Volume; Open = Normal �) )$�� &)�#��

Decision Height MP5C Ground = <DH; Open = >DH �$� �� 1#3 �#��#�

Audio Inhibit MP7D Ground = Audio Inhibit; Open = Normal��$�� $)��3 �) �)�� 4� (-� $#��

��!�1�� #��#�

Altitude Callouts Enable MP8C Ground = Enabled; Open = Disabled �) )$�� &)�#��


MP8D Momentary Ground = Audio Suppress;Open = Normal �� +�� &'(� #�� #��)�� !

GPWS Inhibit MP2D Ground = GPWS Inhibit; Open = Normal 5�� !6 �� !

Steep Approach #1 TP4C Ground = Enabled; Open = Disabled �) )$�� &)�#��

Steep Approach #2 MP5D Ground = Selected; Open = Not Selected�� +�� $�� $ �� )�$ !

�� !

NOT USED


MP1A N/A Open

MP14B N/A Open

TP1A N/A Open

TP1B N/A Open

TP15C N/A Open

TP7A N/A Open

Flap Position #2 (8 o) TP7B +28V = Selected; 0V = Not SelectedSelected when >3o Open

Flap Position #3 (20 o) TP7C +28V = Selected; 0V = Not SelectedSelected when >13o Open

Flap Position #4 (40 o) TP7D +28V = Selected; 0V = Not SelectedSelected when >25o Open

1 ILS Select, Localizer Valid and Glideslope Valid not required if digital ILS provided. (EGPWS will automatically usedigital ILS if provided.)

Allied Signal, Inc.





REQUIRED


�� ! "#�#$��% ��

&'(� ($)� $��#� �$��)*



��$�� #�� ! $�� $�� $ ��

� +�� &'(� ��$�� ,� �� !


&-� �$� �� ! "�$)� �� '�..

�'-&� '��/ �$0�*



Radio Altitude Valid TP15A +28V = Valid; 0V = Not Valid �$�� ,$��%

Flap Position #2 (8 o) TP7B +28V = Not Selected; 0V = SelectedSelected when >3o ��$�� 7� �� ! "��*

Flap Position #3 (20 o) TP7C +28V = Not Selected; 0V = SelectedSelected when >13o ��$�� ! "�8*

Flap Position #4 (40 o) TP7D+28V = Not Selected; 0V = Selected

Selected when >25o

Used for GPWS Landing Flap Selected��$�� 9�� ! "�9*

OPTIONAL





��!�1�� #��#�




FMS Glideslope Inhibit MP14A Ground = Inhibit; Open = Not Inhibit �) )$�� &)�#��

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Normal 5�� !6 �� !

Steep Approach #1 MP1A Ground = Enabled; Open = Disabled �) )$�� &)�#��


�� !

NOT USED


MP2D N/A Open

TP1A N/A Open

TP1B N/A Open

TP4C N/A Open

TP15B N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet Learjet Model 45


ChannelPins

102, 166Connections

TX453-1A=TP3AB=TP3B

Honeywell left/right interleaved picture bus to MFD(/ :#� � �) � ��

� � �8

TX453-2A=TP3CB=TP3D Not Used �� #��

TX429-1Low Speed


TX429-2Low Speed

A=TP2AB=TP2B


Allied Signal, Inc.


Discrete Outputs Worksheet Learjet Model 45


Lamp 102

MP15D Glideslope Cancel N/A .��-��3!� &�� !�1�� $0��

MP3D Below G/S Caution No .��-��3!� 01�) :�� &-� .$0��

MP7B

When diode OR’ed with TP4Dand TP11A is all GPWSwarnings and cautions


No .��-��3!� �� '�.. �' .$0��

TP12C Windshear Caution No (��!�$) �$#�� $0�

TP12A Windshear Warning No (��!�$) ($)��3 �$0�

TP12B Audio On N/A �� !�1��

TP4D Terrain Awarenss Warning No .��-��3!� 01�) '#�� .$0��



TP11A Terrain Awareness Caution N/A .��-��3!� 01�) '#�� .$0��

MP7C GPWS Monitor N/A &'(� ��. �$0�

TP12D Windshear Monitor N/A (��!�$) ��. �$0�

TP11B Terrain Not Available N/A ��))$�� ' .$0� "��*




TP11A is all GPWS Cautions No .��-��3!� 01�) &� '��/ .$0��


is all GPWS Warnings No .��-��3!� �� '#�� .$0��

TP4D Terrain Awareness Warning N/A .��-��3!� �� &� '��/ .$0��

TP11A Terrain Awareness Caution N/A .��-��3!� �� '#�� .$0��


Lamp 166

MP15D Glideslope Cancel N/A .��-��3!� &�� !�1�� $0��

MP3D All GPWS Cautions No �� "'�*

MP7B All GPWS Warnings (“Pull Up”) No �� "'�*

TP12C Windshear Caution No �� "'�*

TP12A Windshear Warning No �� "'�*


TP4D Spare No ��




MP7C GPWS Monitor N/A �� ";��*

TP12D Windshear Monitor N/A �� ";��*

TP11B Terrain Not Available N/A �� "��*

Allied Signal, Inc.


A-16.2 Model 60


Aircraft Type 78

Description Learjet Model 60



ADC

AHRSDual

FMC Dual (Low Speed or High Speed)

IOC

ILSDual

RA Single

VanePotentiometers

Dual


SingleExternal

GPSSingle GPS

DualExternal

GPSDual GPS

PP

IN 7


Dual High Speed FMCReplaces Dual Low Speed FMC

Alternate RAFormat

Single analog RA (use Alternate RA Configuration to select)Replaces Single digital LRRA

FEATURES



No


ARINC 429 DH Yes


Lamp Format Type 1


Alert Volume High



No

Windshear Yes

Allied Signal, Inc.


Display Options & Peaks Availability Learjet Model 60

PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping


1-202

and on

Collins ProLine IV(non-integrated), 7x6(Bus type: ARINC 708Standard Data Format)

No auto ranging

Defaultwith +-60o





1 (TP10A) 2 (TP10B) 3 (TP10C)

78 TP12A MP3A MP3A



AnalogInputChannel

Pins78

Connections

1+ = TP13A- = TP13B

Not UsedOr

Radio Altimeter #1 (ARINC 552 with Validity Discrete)use Alternate RA Configuration to select

2+ = TP14A- = TP14B

Right Vane PotentiometerFormat: DC voltage excitedby 10 VDC reference from

EGPWCRange: 0 – 10 VDC

Offset: 52o

Gain = -6.0o



T P2D(10 VDC)

T P14A (+)

T P14B (-)

��3!� ,$�� '��0��)

3+ = TP13C- = TP13D

Not Used ��

4+ = TP14C- = TP14D

Left Vane PotentiometerFormat: DC voltage excitedby 10 VDC reference from

EGPWCRange: 0 – 10 VDC

Offset: 52o

Gain = -6.0o



T P2D(10 VDC)

T P14C (+)

T P14D (-)

.�� ,$�� '��0��)



78Selected?

Default ARINC 429



Allied Signal, Inc.




InputChannel

Pins78

Connections

4A=MP12AB=MP12B


12A=TP8CB=TP8D


1A=MP6AB=MP6B

AHRS #1 (High Speed) (L-AHC-3) ��


7A=MP12CB=MP12D


Not Used

8A=MP13AB=MP13B


Not Used

9A=TP9CB=TP9D

Not UsedOr

FMC #1 (High Speed)

11A=TP8AB=TP8B

Not UsedOr

FMC #2 (High Speed)

18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


6A=MP11CB=MP11D

ILS #1 (Low Speed) ILS #1

5A=MP10AB-MP10B

ILS #2 (Low Speed) �.� �

2A=MP10CB=MP10D

IOC Bus #1 (High Speed) (LA-IOC-1) ��

3A=MP11AB=MP11B

IOC Bus #2 (High Speed) (RA-IOC-1) ��

10A=TP9AB=TP9B

LRRA #1 (Low Speed)Or

Not Used (use Alt. RA Conf. To select analog RA)

14A=TP1CB=TP1D

Not Used ��

15A=TP4AB=TP4B

Not Used ��

16A=TP5CB=TP5D

Not Used ��




Connections

Alternate GPSSpeed





-204 and onHigh SpeedFMC #1, #2

Only

Use if Nav Mode label 266is available

78

Allied Signal, Inc.





REQUIRED

Self-Test MP9A Momentary Ground = Self Test;Open = Normal ;&'(� �� !


Landing Flap MP9C

Ground = Landing Flap;Open = Not Landing Flap

Can be connected to TP7D if TP7D isgrounded when selected.

��$�� #�� ! $�� $�� $ ��

� +�� &'(� ��$�� ,� �� !


&-� �$� �� ! "�$)� �� '�..

�'-&� '��/ �$0�*



(Alternate) RadioAltitude Valid

TP15A +28V = Valid; 0V = Not ValidNot required if digital LRRA used �$�� ,$��%

Flap Position #2 (8 o) TP7B +28V = Selected; 0V = Not SelectedSelected when >3o ��$�� 7� �� ! "��*

Flap Position #3 (20 o) TP7C +28V = Selected; 0V = Not SelectedSelected when >13o ��$�� ! "�8*

Flap Position #4 (40 o) TP7D +28V = Selected; 0V = Not SelectedSelected when >25o ��$�� 9�� ! "�9*

OPTIONAL





��!�1�� #��#�




Display Select #1 TP1A Momentary Ground Switch .�� ))$�� $% �� !

Display Select #2 TP1B Momentary Ground Switch ��3!� ��))$�� $% �� !

GPWS Inhibit MP2B Ground = GPWS Inhibit; Open = Normal 5�� !6 �� !

Steep Approach #1 TP4C Ground = Enabled; Open = Disabled �) )$�� &)�#��


�� !

NOT USED


MP1A N/A Open

MP14A N/A Open

MP2D N/A Open

TP15B N/A Open

TP15C N/A Open

TP15D N/A Open

TP7A N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet Learjet Model 60


ChannelPins

78Connections

TX453-1A=TP3AB=TP3B

Terrain display data .�� $%

TX453-2A=TP3CB=TP3D

Terrain display data ��3!� �� $%

TX429-1Low Speed

A=MP1CB=MP1D

ICD Appendix E label sets: E-1/2/3/5/6/9/12 � �� $% ��

TX429-2Low Speed

A=TP2AB=TP2B

ICD Appendix E label sets: E-1/2/3/5/6/9/12 �� $% ��



Lamp 78

MP15D Glideslope Cancel N/A .��-��3!� 01�) &�� !�1�� $0��

MP3D Below G/S Caution No .��-��3!� 01�) :�� &-� .$0��

MP7B

When diode OR’ed with TP4Dand TP11A is all GPWScautions and warnings


No .��-��3!� �� '#�� .$0��

TP12C Windshear Caution No .��-��3!� ')�0$)% ��3!� ��$%

TP12A Windshear Warning No .��-��3!� ')�0$)% ��3!� ��$%


TP4D Terrain Awareness Warning No .��-��3!� �� &'(� .$0��

TP10D Terrain Display Discrete #1 N/A .�� ))$�� $% ��$%

MP14C Terrain Display Discrete #2 N/A ��3!� ��))$�� $% ��$%


MP7C GPWS Monitor N/A .��-��3!� 01�) &'(� ��. .$0��

TP12D Windshear Monitor N/A .��-��3!� 01�) (��!�$) ��. �$0��

TP11B Terrain Not Available N/A .��-��3!� 01�) ��))$�� 4$��$1�� .$0��




TP11A is all GPWS Cautions No .��-��3!� 01�) &'(� .$0��


is all GPWS Warnings No .��-��3!� �� '#�� .$0��

TP4D Terrain Awareness Warning N/A .��-��3!� �� &'(� .$0��


Allied Signal, Inc.


A-17 Saab

A-17.1 Saab 2000


Aircraft Type 36

Description Saab 2000



ADC Single

ILS Dual

IRS Single (will use AHRS if provided)

IOC

LRRADual


SingleExternal GPS

Single GPS

PP

IN 7

Dual ExternalGPS

Dual GPS

FEATURES



No


ARINC 429 DH Yes


Lamp Format Type 1


Alert Volume Low



No

Windshear No

Allied Signal, Inc.


Display Options & Peaks Availability

PPINState


Display SweepStyle

Auto PopUp

AlternatePop Up


PeaksAvail.

PPIN 18(MP15A)

Strapping

Aircraft Type: 36

1-101



Program Pin Strapping for Aircraft Type Saab 2000


1 (TP10A) 2 (TP10B) 3 (TP10C)

36 MP7B MP7B Open



Allied Signal, Inc.


ARINC 429 Input Channel Ass ignments Wo rksheet Saab 2000


InputChannel

Pins36

Connections

12A=TP8CB=TP8D


18A=MP6CB=MP6D

Not UsedOr


17A=TP11CB=TP11D

Not UsedOr


2A=MP10CB=MP10D

IOC #1 (High Speed)(LA-GP-5) ��

3A=MP11AB=MP11B

IOC #2 (High Speed)(RA-GP-5) ��

5A=MP10AB-MP10B ILS #2 (Low Speed) ��


1A=MP6AB=MP6B



10A=TP9AB=TP9B

LRRA #2 (Low Speed)(R-RAC-1) ��

11A=TP8AB=TP8B

LRRA #1 (Low Speed)(L-RAC-1) ��

4A=MP12AB=MP12B

Not Used � ��

7A=MP12CB=MP12D

Not Used � ��

8A=MP13AB=MP13B

Not Used � ��

9A=TP9CB=TP9D

Not Used � ��

13A=TP5AB=TP6A Not Used � ��

14A=TP1CB=TP1D Not Used � ��

15A=TP4AB=TP4B Not Used � ��

16A=TP5CB=TP5D Not Used � ��







Allied Signal, Inc.


Discrete Inputs Worksheet Saab 2000



REQUIRED




Landing Flap TP7A Ground = Landing Flap; Open = Not Landing Flap

OPTIONAL

Glideslope Inhibit MP1B Ground = Glideslope Inhibit; Open = Not Inhibit ��









Display Select 2 TP1B Momentary Ground Switch




MP2D Ground = Inhibit; Open = Normal

NOT USED


MP9C N/A Open

MP14A N/A Open

TP4C N/A Open

MP5D N/A Open

TP15A N/A Open

TP15B N/A Open

TP15C N/A Open

TP15D N/A Open

TP7B N/A Open

TP7C N/A Open

TP7D N/A Open

Allied Signal, Inc.


Serial Outputs Worksheet Saab 2000


ChannelPins

36Connections

TX453-1A=TP3AB=TP3B

Terrain display data to symbol generator

TX453-2A=TP3CB=TP3D

Terrain display data to symbol generator

TX429-1Low Speed

A=MP1CB=MP1D


TX429-2Low Speed

A=TP2AB=TP2B




Lamp 36


MP3D Below G/S Caution Yes �� !�" ��

MP7BAll


Yes �� # � �

TP12C Spare Yes � ��

TP12A Spare Yes � ��

TP12B Audio On N/A $�� !��

TP4D Spare N/A � ��

TP10D Terrain Display Discrete #1 N/A �� $�""�� %

MP14C Terrain Display Discrete #2 N/A �� $�""�� %

TP11A Spare N/A � ��

MP7C GPWS Monitor N/A ��&� ��#$ �

TP12D Spare N/A � ��

TP11B Terrain Not Available N/A $�""�� '��



MP3D All GPWS Cautions No �� !�" ��&� � �

MP7B All GPWS Warnings (“Pull Up”) No �� # � �

Allied Signal, Inc.


A-18 Simulators

For MK V EGPWS, the simulator configuration must match an Aircraft Type with a Simulator

Reposition discrete input defined (refer to the Aircraft Type’s Discrete Inputs Worksheet). Most

Aircraft Types support simulator installations.

During simulator testing, it is often necessary to instantaneously move the aircraft. The MK V

EGPWS will support this only when the Simulator Reposition Program Pin is strapped to enablesimulator repositions and the Simulator Reposition discrete input indicates reposition.

Allied Signal, Inc.


Appendix B: Altitude Callout Menu Options

Basic Altitude Callouts With Smart 500’ Callout

ID Altitude Callouts

PP

CN

F4

PP

CN

F5

PP

CN

F6

ID

PP

CN

F4

PP

CN

F5

PP

CN

F6

0 100, 50, 30 Low Volume Open Open Open 256 Open Open MP7B1 MINIMUMS, 100, 50, 30 MP3A Open Open 257 MP3A Open MP7B2 No Mode 6 Callouts MP15D Open Open 258 MP15D Open MP7B3 100, 30, 20 MP3D Open Open 259 MP3D Open MP7B

4APPROACHINGMINIMUMS, MINIMUMS,50

MP7B Open Open 260 MP7B Open MP7B

5

APPROACHINGMINIMUMS, MINIMUMS,2500, 50, 40, 30, 20, 10Not available prior to -206

TP12C Open Open 261 TP12C Open MP7B

6 100, 30, 10 TP12A Open Open 262 TP12A Open MP7B7 MINIMUMS, 200, 100 TP4D Open Open 263 TP4D Open MP7B

8 MINIMUMS, 100, 50, 20,10 Open MP3A Open 264 Open MP3A MP7B

9 100 Tone, 35 Tone, 20Tone MP3A MP3A Open 265 MP3A MP3A MP7B

10 MINIMUMS, 500, 50 MP15D MP3A Open 266 MP15D MP3A MP7B

11 MINIMUMS-MINIMUMS,1000 MP3D MP3A Open 267 MP3D MP3A MP7B

12 500 Tone MP7B MP3A Open 268 MP7B MP3A MP7B

13MINIMUMS, 500, 400,300, 200, 100, 50, 40, 30,20, 10

D0 #4 MP3A Open 269 TP12C MP3A MP7B

14 MINIMUMS, 1000, 500 TP12A MP3A Open 270 TP12A MP3A MP7B

15MINIMUMS, 1000, 500,400, 300, 200, 100, 50,40, 30, 20, 10

TP4D MP3A Open 271 TP4D MP3A MP7B

16MINIMUMS-MINIMUMS,200, 100, 50, 40, 30, 20,10 Low Volume

Open MP15D Open 272 Open MP15D MP7B

17MINIMUMS-MINIMUMS,200, 100, 50, 40, 30, 20,10

MP3A MP15D Open 273 MP3A MP15D MP7B

18 MINIMUMS, 500, 100, 50,40, 30, 20, 10 MP15D MP15D Open 274 MP15D MP15D MP7B

19 MINIMUMS, 500, 300, 50,40, 30, 20, 10 MP3D MP15D Open 275 MP3D MP15D MP7B

20 MINIMUMS, 50, 30 MP7B MP15D Open 276 MP7B MP15D MP7B21 50, 30, 10 D0 #4 MP15D Open 277 TP12C MP15D MP7B

Allied Signal, Inc.




PP

CN

F4

PP

CN

F5

PP

CN

F6

ID

PP

CN

F4

PP

CN

F5

PP

CN

F6

22 100, 50, 30 TP12A MP15D Open 278 TP12A MP15D MP7B23 100, 50, 30, 10 TP4D MP15D Open 279 TP4D MP15D MP7B

24MINIMUMS-MINIMUMS,50, 40, 30, 20, 10 LowVolume

Open MP3D Open 280 Open MP3D MP7B

25 MINIMUMS-MINIMUMS,50, 40, 30, 20, 10 MP3A MP3D Open 281 MP3A MP3D MP7B

26 60, 30, 10 MP15D MP3D Open 282 MP15D MP3D MP7B

27MINIMUMS-MINIMUMS,300, 100, 50, 40, 30, 20,10

MP3D MP3D Open 283 MP3D MP3D MP7B

28 MINIMUMS-MINIMUMS MP7B MP3D Open 284 MP7B MP3D MP7B

29APPROACHINGMINIMUMS, MINIMUMS,500, 50, 40, 30, 20, 10

D0 #4 MP3D Open 285 TP12C MP3D MP7B

30 MINIMUMS, 500, 200,100, 50, 40, 30, 20, 10 TP12A MP3D Open 286 TP12A MP3D MP7B

31 N/A N/A N/A N/A 287 N/A N/A N/A

322500, 1000, 500, 100, 50,40, 30, 20, 10Not available prior to –208

Open MP7B Open 288 Open MP7B MP7B

33 N/A N/A N/A N/A 289 N/A N/A N/A34 N/A N/A N/A N/A 290 N/A N/A N/A

35

2500, 1000(B), 500(B),100, 50, 40, 30, 20, 10Not available prior to –208;Available only on 777-200/300and 737-600/700/800.

MP3D MP7B Open 291 MP3D MP7B MP7B


37MINIMUMS, 400, 300,200, 100, 50, 40, 30, 20,10

D0 #4 MP7B Open 293 TP12C MP7B MP7B

38

APPROACHINGMINIMUMS, MINIMUMS,2500, 1000, 500, 100, 50,40, 30, 20, 10

TP12A MP7B Open 294 TP12A MP7B MP7B

39

APPROACHINGMINIMUMS, MINIMUMS,500, 100, 50, 40, 30, 20,10

TP4D MP7B Open 295 TP4D MP7B MP7B

40 1000, 500, 30, 10 Open TP12C Open 296 Open TP12C MP7B

41 PLUS HUNDRED,MINIMUM MP3A TP12C Open 297 MP3A TP12C MP7B

42PLUS HUNDRED,MINIMUM, 50, 40, 30, 20,10

MP15D TP12C Open 298 MP15D TP12C MP7B

Allied Signal, Inc.




PP

CN

F4

PP

CN

F5

PP

CN

F6

ID

PP

CN

F4

PP

CN

F5

PP

CN

F6

43 MINIMUMS MP3D TP12C Open 299 MP3D TP12C MP7B44 2500, 100, 50, 30 MP7B TP12C Open 300 MP7B TP12C MP7B

45

APPROACHINGDECISION HEIGHT,MINIMUMS, 2500, 1000,50, 40, 30, 20, 10

D0 #4 TP12C Open 301 TP12C TP12C MP7B

46 100, 50, 30, 20, 10 TP12A TP12C Open 302 TP12A TP12C MP7B47 2500 TP4D TP12C Open 303 TP4D TP12C MP7B

48

APPROACHINGMINIMUMS, MINIMUMS,1000(B), 500(B), 100, 50,30, 20, 10This menu only availableon 777-200/300 and737-600/700/800.

Open TP12A Open 304 Open TP12A MP7B

49 MINIMUMS, 100, 50, 40,30, 20, 10 MP3A TP12A Open 305 MP3A TP12A MP7B

50 100, 50, 30, 20, 10 MP15D TP12A Open 306 MP15D TP12A MP7B

51

APPROACHINGMINIMUMS, MINIMUMS,2500, 1000, 500, 400,300, 200, 100, 50, 40, 30,20, 10

MP3D TP12A Open 307 MP3D TP12A MP7B

52 50, 30, 20, 10 MP7B TP12A Open 308 MP7B TP12A MP7B

53

RADIO ALTIMETER(@2500), 1000, 100, 50,30, 20, 10Refer to menu 93 forfemale voices.

D0 #4 TP12A Open 309 TP12C TP12A MP7B

54

50 ABOVE, DECIDE,RADIO ALTIMETER(@2500), 1000, 100, 50,30, 20, 10Refer to menu 94 forfemale voices.

TP12A TP12A Open 310 TP12A TP12A MP7B

55MINIMUMS, RADIOALTIMETER (@2500),1000, 100, 50, 30, 20, 10

TP4D TP12A Open 311 TP4D TP12A MP7B


57

APPROACHINGMINIMUMS, MINIMUMS,1000, 500, 400, 300, 200,100, 50, 40, 30, 20, 10

MP3A TP4D Open 313 MP3A TP4D MP7B

58 N/A N/A N/A N/A 314 N/A N/A N/A59 N/A N/A N/A N/A 315 N/A N/A N/A

Allied Signal, Inc.




PP

CN

F4

PP

CN

F5

PP

CN

F6

ID

PP

CN

F4

PP

CN

F5

PP

CN

F6


61APPROACHINGMINIMUMS, MINIMUMS,1000

D0 #4 TP4D Open 317 TP12C TP4D MP7B

62 N/A TP12A TP4D Open 318 TP12A TP4D MP7B63 Not for Aircraft Use N/A N/A N/A 319 N/A N/A N/A

64

APPROACHINGMINIMUMS,MINIMUMS-MINIMUMS,200, 100

Open Open MP3A 320 Open Open TP12C


66

RADIO ALTIMETER (malevoice @2500), 1000Refer to menu 95 forfemale voices.

MP15D Open MP3A 322 MP15D Open TP12C

67 MINIMUMS, 2500, 1000 MP3D Open MP3A 323 MP3D Open TP12C

68 2500, 500, 50, 40, 30, 20,10 MP7B Open MP3A 324 MP7B Open TP12C

69 2500, 50, 30, 10 D0 #4 Open MP3A 325 TP12C Open TP12C

70 MINIMUMS-MINIMUMS,50, 30, 10 TP12A Open MP3A 326 TP12A Open TP12C

71 1000, 500, 50, 40, 30, 20,10 TP4D Open MP3A 327 TP4D Open TP12C

72 1000, 100, 50, 30, 20, 10 Open MP3A MP3A 328 Open MP3A TP12C

73MINIMUMS-MINIMUMS,1000, 500, 100, 50, 40,30, 20, 10

MP3A MP3A MP3A 329 MP3A MP3A TP12C

74 500, 30 MP15D MP3A MP3A 330 MP15D MP3A TP12C75 50, 40, 30, 20, 10 MP3D MP3A MP3A 331 MP3D MP3A TP12C

76MINIMUMS, 2500, 1000,500, 400, 300, 200, 100,50, 40, 30, 20, 10

MP7B MP3A MP3A 332 MP7B MP3A TP12C

77 MINIMUMS, 2500, 1000,50, 40, 30, 20, 10 D0 #4 MP3A MP3A 333 TP12C MP3A TP12C

78 1000 TP12A MP3A MP3A 334 TP12A MP3A TP12C

79 MINIMUMS-MINIMUMS,2500, 1000, 500 TP4D MP3A MP3A 335 TP4D MP3A TP12C

80 MINIMUMS-MINIMUMS,500, 300, 200, 100, 50 Open MP15D MP3A 336 Open MP15D TP12C

81 MINIMUMS-MINIMUMS,500, 300, 200, 100 MP3A MP15D MP3A 337 MP3A MP15D TP12C

82 MINIMUMS-MINIMUMS,1000, 500, 300, 200, 100 MP15D MP15D MP3A 338 MP15D MP15D TP12C

Allied Signal, Inc.




PP

CN

F4

PP

CN

F5

PP

CN

F6

ID

PP

CN

F4

PP

CN

F5

PP

CN

F6

83MINIMUMS-MINIMUMS,1000, 500, 300, 200, 100,50

MP3D MP15D MP3A 339 MP3D MP15D TP12C

84

MINIMUMS, RADIOALTIMETER (@2500),1000, 500, 400, 300, 200,100, 50, 40, 30, 20, 10

MP7B MP15D MP3A 340 MP7B MP15D TP12C

85PLUS HUNDRED,MINIMUMS, 2500, 1000,50, 40, 30, 20, 10

D0 #4 MP15D MP3A 341 TP12C MP15D TP12C

86MINIMUM, 2500, 1000,400, 300, 200, 100, 50,40, 30, 20, 10

TP12A MP15D MP3A 342 TP12A MP15D TP12C

87

APPROACHINGMINIMUMS, MINIMUMS,500, 300, 200, 50, 40, 30,20, 10

TP4D MP15D MP3A 343 TP4D MP15D TP12C

88

APPROACHINGMINIMUMS, MINIMUMS,1000, 500, 300, 200, 50,40, 30, 20, 10, 5

Open MP3D MP3A 344 Open MP3D TP12C

89

APPROACHINGMINIMUMS, MINIMUMS,500, 300, 200, 50, 40, 30,20, 10, 5

MP3A MP3D MP3A 345 MP3A MP3D TP12C

90

APPROACHINGMINIMUMS, MINIMUMS,1000, 500, 300, 200, 50,40, 30, 20, 10, 5

MP15D MP3D MP3A 346 MP15D MP3D TP12C

91 MINIMUMS, 1000, 500,100, 50, 40, 30, 20, 10 MP3D MP3D MP3A 347 MP3D MP3D TP12C

92 PLUS HUNDRED,MINIMUMS, 60, 30, 10 MP7B MP3D MP3A 348 MP7B MP3D TP12C

93

RADIO ALTIMETER(female voice @2500),1000, 100, 50, 30, 20, 10Refer to menu 53 for malevoices.

D0 #4 MP3D MP3A 349 TP12C MP3D TP12C

94

50 ABOVE (female voice),DECIDE (female voice),RADIO ALTIMETER(female voice @2500),1000, 100, 50, 30, 20, 10Refer to menu 54 for malevoices.

TP12A MP3D MP3A 350 TP12A MP3D TP12C

Allied Signal, Inc.




PP

CN

F4

PP

CN

F5

PP

CN

F6

ID

PP

CN

F4

PP

CN

F5

PP

CN

F6

95

RADIO ALTIMETER(female voice @2500),1000Refer to menu 66 for malevoices.

TP4D MP3D MP3A 351 TP4D MP3D TP12C

96

PLUS HUNDRED,MINIMUMS, 2500,1000(B), 500(B), 100, 50,40, 30, 20, 10Only available on 777-200/300 and737-600/700/800/IGW.

Open MP7B MP3A 352 Open MP7B TP12C

97

PLUS HUNDRED,MINIMUMS, 2500, 1000,500, 100, 50, 40, 30, 20,10

MP3A MP7B MP3A 353 MP3A MP7B TP12C

98

50 ABOVE (female voice),DECIDE (female voice),RADIO ALTIMETER(female voice @2500),1000

MP15D MP7B MP3A 354 MP15D MP7B TP12C

99

DECIDE (female voice),RADIO ALTIMETER(female voice @2500),1000, 100, 50, 30, 20, 10

MP3D MP7B MP3A 355 MP3D MP7B TP12C

100

PLUS HUNDRED,MINIMUMS, 2500,1000(B), 60, 30, 10Not available prior to –206;Only available on 777-200/300and 737-600/700/800/IGW.

MP7B MP7B MP3A 356 MP7B MP7B TP12C

101 500 Tone, 100, 50, 30, 20Not available prior to –208.

TP12C MP7B MP3A 357 N/A N/A N/A

102

MINIMUMS (MOA), 2500,1000, 500, 50, 40, 30, 20,10Added in –208; Reserved forNIMROD MRA4.

TP12A MP7B MP3A 358 TP12A MP7B TP12C

103-

254N/A N/A N/A N/A

359-

510N/A N/A N/A

Allied Signal, Inc.




PP

CN

F4

PP

CN

F5

PP

CN

F6

ID

PP

CN

F4

PP

CN

F5

PP

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F6

255

Not Recommended forAircraft Use (Baro TestMenu):APPROACHINGMINIMUMS, MINIMUMS,2500(B), 1000(B), 500(B),400(B), 300(B), 200(B),100(B), 80(B), 60(B),50(B), 40(B), 35(B), 30(B),20(B), 10(B)

MP3D TP4D TP4D 511 TP4D TP4D TP4D

Allied Signal, Inc.


Appendix C: Audio Menu OptionsNote: The order of the messages (top to bottom) in the following tables indicates their auralpriority (e.g. Mode 4 Too Low Terrain has a higher priority than the Mode 6 altitude callouts).Alert or WarningCondition Basic Menu Callouts Alternate Menu #1

Mode 7 WindshearWarning

(SIREN) Windshear WindshearWindshear

Windshear WindshearWindshear

Mode 6 Bank Angle 1 Bank AngleMode 1 Pull Up Pull UpMode 2 Pull Up Preface Terrain TerrainMode 2 Pull Up Pull UpV1 Alert V1Engine Fail Alert Engine FailTerrain AwarenessPreface Terrain Terrain Terrain Ahead Pull Up

Terrain AwarenessWarning Pull Up Terrain Ahead Pull Up

Obstacle AwarenessPreface Obstacle Obstacle Obstacle Ahead Pull Up

Obstacle AwarenessWarning Pull Up Obstacle Ahead Pull Up

PWS Windshear Warning N/A - PWS VoiceMode 2 Terrain TerrainMode 6 Minimums Selected CalloutMode 6 Altitude 1 Altitude AltitudeTerrain AwarenessCaution

Caution Terrain (PAUSE)Caution Terrain (7 sec pause)

Terrain Ahead (PAUSE)Terrain Ahead (7 sec pause)

Obstacle AwarenessCaution

Caution Obstacle (PAUSE)Caution Obstacle (7 sec pause)

Obstacle Ahead (PAUSE)Obstacle Ahead (7 sec pause)

Mode 4 Too Low Terrain Too Low TerrainTCF Too Low Terrain Too Low TerrainAltitude Alert 1 960 Hz ToneMode 6 Altitude Callouts Selected CalloutsSpeed Brake Alert Speed Brake (PAUSE) Speed BrakeMode 4 Too Low Gear Too Low GearMode 4 Too Low Flaps Too Low FlapsMode 1 Sinkrate Sinkrate (PAUSE) SinkrateMode 3 Don’t Sink Don’t Sink (PAUSE) Don’t SinkMode 5 Glideslope GlideslopePWS Windshear Caution N/A – PWS VoiceMode 6 Approaching DH Selected CalloutMode 6 Bank Angle Bank Angle (PAUSE) Bank Angle

Mode 7 Windshear Alert (QUIET)(or CAUTION WINDSHEAR if Caution voice Enabled)

Autopilot Alert 1 AutopilotTakeoff Flap Alert 1 Flaps (PAUSE) FlapsTCAS RATCAS TA

N/A - TCAS Voice (may coincide with Mode 6 voices)1Added in version –208.

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Alert or WarningCondition Alternate Menu #2 Alternate Menu #3

Mode 7 WindshearWarning

(SIREN) Windshear WindshearWindshear

Windshear WindshearWindshear

Mode 6 Bank Angle 1 Bank AngleMode 1 Pull Up Pull UpMode 2 Pull Up Preface Terrain TerrainMode 2 Pull Up Pull UpV1 Alert V1Engine Fail Alert Engine FailTerrain AwarenessPreface Terrain Terrain Terrain Ahead Pull Up

Terrain AwarenessWarning Pull Up Terrain Ahead Pull Up


Obstacle AwarenessWarning Pull Up Obstacle Ahead Pull Up







Mode 4 Too Low Terrain Too Low TerrainTCF Too Low Terrain Too Low TerrainAltitude Alert 1 960 Hz ToneMode 6 Altitude Callouts Selected CalloutsSpeed Brake Alert Speed Brake (PAUSE) Speed BrakeMode 4 Too Low Gear Too Low GearMode 4 Too Low Flaps Too Low FlapsMode 1 Sinkrate Sinkrate (PAUSE) SinkrateMode 3 Don’t Sink Don’t Sink (PAUSE) Don’t SinkMode 5 Glideslope GlideslopePWS Windshear Caution N/A - PWS VoiceMode 6 Approaching DH Selected CalloutMode 6 Bank Angle Bank Angle (PAUSE) Bank Angle




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Alert or WarningCondition Alternate Menu #4 Alternate Menu #5

Mode 7 WindshearWarning (SIREN) Windshear Windshear Windshear

Mode 6 Bank Angle 1 Bank AngleMode 1 Pull Up (WHOOP) (WHOOP) Pull UpMode 2 Pull Up Preface Terrain TerrainMode 2 Pull Up (WHOOP) (WHOOP) Pull UpV1 Alert V1Engine Fail Alert Engine FailTerrain AwarenessPreface Terrain Terrain Terrain Ahead Pull Up

Terrain AwarenessWarning (WHOOP) (WHOOP) Pull Up Terrain Ahead Pull Up


Obstacle AwarenessWarning (WHOOP) (WHOOP) Pull Up Obstacle Ahead Pull Up







Mode 4 Too Low Terrain Too Low TerrainTCF Too Low Terrain Too Low TerrainAltitude Alert 1 960 Hz ToneMode 6 Altitude Callouts Selected CalloutsSpeed Brake Alert Speed Brake (PAUSE) Speed BrakeMode 4 Too Low Gear Too Low GearMode 4 Too Low Flaps Too Low FlapsMode 1 Sinkrate Sinkrate (PAUSE) SinkrateMode 3 Don’t Sink Don’t Sink (PAUSE) Don’t SinkMode 5 Glideslope GlideslopePWS Windshear Caution N/A - PWS VoiceMode 6 Approaching DH Selected CalloutMode 6 Bank Angle Bank Angle (PAUSE) Bank Angle




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Alert or WarningCondition Alternate Menu #6

Mode 7 WindshearWarning (SIREN) Windshear Windshear Windshear

Mode 6 Bank Angle 1 Bank AngleMode 1 Pull Up Pull UpMode 2 Pull Up Preface Terrain TerrainMode 2 Pull Up Pull UpV1 Alert V1Engine Fail Alert Engine FailTerrain AwarenessPreface Terrain Terrain

Terrain AwarenessWarning Pull Up

Obstacle AwarenessPreface Obstacle Obstacle

Obstacle AwarenessWarning Pull Up

PWS Windshear Warning N/A - PWS VoiceMode 2 Terrain TerrainMode 6 Minimums Selected CalloutMode 6 Altitude 1 Altitude AltitudeTerrain AwarenessCaution Caution Terrain (PAUSE) Caution Terrain (7 sec pause)

Obstacle AwarenessCaution Caution Obstacle (PAUSE) Caution Obstacle (7 sec pause)

Mode 4 Too Low Terrain Terrain (PAUSE) TerrainTCF Too Low Terrain Terrain (PAUSE) TerrainAltitude Alert 1 960 Hz ToneMode 6 Altitude Callouts Selected CalloutsSpeed Brake Alert Speed Brake (PAUSE) Speed BrakeMode 4 Too Low Gear Terrain (PAUSE) TerrainMode 4 Too Low Flaps Terrain (PAUSE) TerrainMode 1 Sinkrate Sinkrate (PAUSE) SinkrateMode 3 Don’t Sink Sinkrate (PAUSE) SinkrateMode 5 Glideslope GlideslopePWS Windshear Caution N/A - PWS VoiceMode 6 Approaching DH Selected CalloutMode 6 Bank Angle Bank Angle (PAUSE) Bank Angle




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CAGE CODE: 97896 SCALE: NONE SIZE: B DWG NO: 060-4199-125 REV: SHEET 559

Appendix D: Sample Wiring DiagramsSample wiring diagrams are provided for reference only. The table below shows the Aircraft Types and aircraft models represented.

Aircraft Type Aircraft Model

217 Boeing 737-300 Basic UAL

4, 8, 9 Boeing 737-300/-400/-500 Basic

16, 17 Boeing 737-300/-500 with PPI Display

111 Boeing 747-400 with dual WXr R/T(JAL Simulator installation)

105, 106, 109 Boeing 757-200/767-200/767-300ER with Windshear115 VAC EGPWC

224 Boeing 757-200/-200ER with single WXR

3, 5, 31 Boeing 767-200/-300/-300ER Basic

222 Boeing 767-300ER SAS

222 Boeing 767-300ER with Dual WXR R/T

139 DC-9-82/-83 TWA

65, 73 Hawker 800 with Collins ProLine II(terrain on three displays)

66, 138 Hawker 800 with Honeywell 5x6 EFIS (SPZ-8000)(terrain on three displays)

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��

��

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Allied Signal, Inc.


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SASB767eC(222)Dual.DWG

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Allied Signal, Inc.
