L 3 Communications Avionics Systems TRC899 User Manual

Traffic Alert/Advisory System

Preliminary

SKY899 Installation Manual

This manual contains installation instructions and recommended flightline maintenance information for the SKY899 Traffic Alert/Advisory System. This information is supplemented and kept current by Change Notices, Service Bulletins, and Service Memos published by BFGoodrich Avionics Systems.

009-11900-001 (Rev. A)

BFGoodrich Avionics Systems, Inc. 30 April 2001 5353 52 Grand Rapids, MI USA 49512

Street, S.E.

Preliminary

ABOUT THIS MANUAL

Chapter 1 – General Information

This chapter includes equipment specifications and a functional description. It describes the various hardware configurations and includes a list of items furnished and items required but not supplied with the equipment.

Chapter 2 - Installation

This chapter contains instructions for unpacking the equipment and inspection for in-shipment damage. It also includes information required to locate, assemble and install the equipment.

Chapter 3 – Installation Checkout

This chapter contains instructions for doing post-installation and return to service checkout of the SKY899 using the BFGoodrich Avionics Systems TT391 Flightline Tester.

Chapter 4 – Maintenance

This chapter contains general flightline maintenance procedures. It includes periodic maintenance and troubleshooting; instructions for calibrating the directional antenna and instructions for the return of defective components.

Appendix A – Signal and Cable Characteristics

This appendix defines the electrical characteristics of all input and output signals.

Appendix B – Environmental Qualification Form

This appendix has the environmental qualification forms for the TRC899, NY156 & NY164 antennas, and WX-1000/SKY497 display.

Appendix C – Installation Checkout Using The TCAS-201 Ramp Test Set

This appendix contains instructions for doing post-installation and return to service checkout of the SKY899 using the IFR Systems TCAS-201 Ramp Test Set (with TCAS I firmware).

Appendix D – Installation Checkout Using The TIC T-49C Flightline Tester

This appendix contains instructions for doing post-installation and return to service checkout of the SKY899 using the TIC T-49C Flightline Tester.

Appendix E – Using The Terminal Device

This appendix contains instructions for using the Terminal Device for installation, testing or troubleshooting of the SKY899.

Appendix F – Installation Checkout Using an Alternate Display

This appendix contains instructions for doing post-installation and return to service checkout of the SKY899 using an Alternate Display.

BFGoodrich Avionics Systems, Inc.

____________________________

Trademarks

Alodine® is a registered trademark of Amchem Products, Inc.

Flamemaster® is a registered trademark of Flamemaster.

HyperTerminal® is a registered trademark of Hilgraeve, Inc.

Mylar® and Teflon® are registered trademarks of DuPont.

Procomm® is a registered trademark of Datastorm Technologies, Inc.

SKYWATCH

and Stormscope® are registered trademarks of BFGoodrich Avionics Systems, Inc.

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LIST OF EFFECTIVE PAGES

Dates of original and changed pages are: Original (Rev. A) ..........................30 April 2001

NOTE

The portion of the text affected by the change is indicated by a vertical line in the outer margins of the page. Changes to illustrations (other than diagrams and schematics) are identified with a miniature pointing hand. Shading is used to highlight the area of diagrams and schematics containing a change.

Total number of pages in this publication consists of the following:

Page Change No. No.

Title Page ................................................................. 0

A Page ..................................................................... 0

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INSERT LATEST CHANGED PAGES, DESTROY SUPERSEDED PAGES.

Those responsible for maintaining this publication should ensure that all previous changes have been received and incorporated.

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FOREWORD

This manual provides information intended for use by persons who, pursuant to current regulatory requirements, are qualified to install this equipment. Because installations vary depending on a particular aircraft, this manual is intended as a guideline. Standard installation practices prescribed in FAA Advisory Circular No. 43.13 must be followed. If further information is required, contact:

BFGoodrich Avionics Systems

Attn: Field Service Engineering

5353 52nd Street, S.E.

Grand Rapids, MI USA 49512

Tel. (800) 453-0288 or (616) 949-6600

We welcome your comments concerning this manual. Although every effort has been made to keep it free of errors, some may occur. When reporting a specific problem, please describe it briefly and include the manual part number, the paragraph/figure/table number, and the page number. Send your comments to:

BFGoodrich Avionics Systems

Attn: Technical Publications

5353 52nd Street, S.E.

Grand Rapids, MI USA 49512

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Paragraph Page

Chapter 1

GENERAL INFORMATION

1.1 INTRODUCTION .................................................................................................................................. 1-1

1.2 FUNCTIONAL DESCRIPTION ........................................................................................................... 1-2

1.3 PHYSICAL DESCRIPTION.................................................................................................................. 1-2

1.3.1 TRC899 Transmitter Receiver Computer P/N 805-11900-xxx............................................................ 1-6

1.3.2 Configuration Module P/N 814-18005-001......................................................................................... 1-10

1.3.3 Display (Alternate or WX-1000/SKY497 Display P/N 78-8060-5900-x)........................................... 1-11

1.3.4 Directional Antenna (NY156 P/N 805-10003-001 or NY164 P/N 805-10890-001) ........................... 1-13

1.4 SPECIFICATIONS .............................................................................................................................. 1-15

1.4.1 Transmitter Receiver Computer (TRC) .............................................................................................. 1-15

1.4.2 WX-1000/SKY497 Display................................................................................................................... 1-16

1.4.3 Directional Antenna ............................................................................................................................1-16

1.5 MODIFICATIONS & SOFTWARE REVISIONS............................................................................... 1-16

1.6 INTERFACE ........................................................................................................................................ 1-17

1.7 EQUIPMENT REQUIRED NOT SUPPLIED.................................................................................... 1-17

1.8 INSTALLATION APPROVAL ............................................................................................................1-22

1.9 WARRANTY INFORMATION............................................................................................................ 1-22

1.9.1 Warranty Statement............................................................................................................................ 1-22

1.9.2 Related Policies and Procedures ......................................................................................................... 1-23

Chapter 2

INSTALLATION

2.1 INTRODUCTION .................................................................................................................................. 2-1

2.2 UNPACKING, INSPECTION AND STORAGE ..................................................................................2-1

2.3 ANTENNA LOCATION ........................................................................................................................2-2

2.4 TRC LOCATION.................................................................................................................................... 2-2

2.5 DISPLAY LOCATION ......................................................................................................................... 2-15

2.6 CABLE REQUIREMENTS AND FABRICATION ............................................................................ 2-16

2.6.1 Antenna Cables.................................................................................................................................... 2-18

2.6.2 Audio Output Cable ............................................................................................................................. 2-18

2.6.3 Data Cables .......................................................................................................................................... 2-18

2.6.4 Heading Input Cable ...........................................................................................................................2-19

2.6.5 Power Cable ......................................................................................................................................... 2-19

2.6.6 Suppression Bus Cable........................................................................................................................ 2-20

2.6.7 WX-1000/SKY497 Display and WX-1000 Processor Cable................................................................ 2-20

2.6.8 Converting Existing Aircraft Wiring from SKY497 to SKY899........................................................ 2-21

2.7 AIRCRAFT DISCRETE INPUTS .......................................................................................................2-22

2.7.1 Audio Inhibit (Terrain Warning System - GPWS)............................................................................. 2-22

2.7.2 Landing Gear ....................................................................................................................................... 2-22

2.7.3 SKYWATCH/Stormscope Mode Switch .............................................................................................. 2-22

2.7.4 Squat Switch (Weight-On-Wheels) ..................................................................................................... 2-22

2.7.5 ON/OFF Power Switch ........................................................................................................................ 2-23

2.8 ALTERNATE DISPLAY...................................................................................................................... 2-24

2.9 ARINC-429 ........................................................................................................................................... 2-24

2.9.1 General Sensor Inputs......................................................................................................................... 2-24

2.9.2 Mode S Transponder I/O (future option)............................................................................................ 2-24

2.9.3 Alternate Display Output.................................................................................................................... 2-25

2.9.4 Future Option ......................................................................................................................................2-25

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Paragraph Page

Chapter 2

INSTALLATION

2.10 AUDIO (ALERT) OUTPUT ................................................................................................................ 2-25

2.11 BAROMETRIC (UNCORRECTED) ALTITUDE INPUTS ............................................................... 2-25

2.11.1 Gilham Code (Encoding Altimeter) .................................................................................................... 2-26

2.11.2 ADC (ARINC-429) ............................................................................................................................... 2-26

2.12 GPS (ARINC-429)................................................................................................................................ 2-26

2.13 HEADING INPUT............................................................................................................................... 2-26

2.13.1 Compass Synchro (XYZ)...................................................................................................................... 2-26

2.13.2 AHRS (Attitude Heading and Reference System)............................................................................. 2-27

2.14 LAMP OUTPUTS (ABV and BLW) .................................................................................................... 2-27

2.15 OPERATIONAL MODE OUTPUT (optional) .................................................................................... 2-27

2.16 POWER INPUT ................................................................................................................................... 2-27

2.17 RADIO ALTIMETER (optional) ......................................................................................................... 2-27

2.17.1 Analog .................................................................................................................................................. 2-28

2.17.2 ARINC-429........................................................................................................................................... 2-28

2.18 SERIAL DATA..................................................................................................................................... 2-28

2.19 SOFT-KEYS......................................................................................................................................... 2-28

2.20 SUPPRESSION BUS I/O .................................................................................................................... 2-28

2.21 SYSTEM CONFIGURATION MODULE........................................................................................... 2-28

2.22 WX-1000/SKY497 DISPLAY (OPTIONAL) ....................................................................................... 2-30

2.23 WX-1000 PROCESSOR (OPTIONAL)................................................................................................2-30

2.24 ANTENNA INSTALLATION ............................................................................................................. 2-31

2.25 TRC MOUNTING TRAY INSTALLATION....................................................................................... 2-32

2.26 TRC INSTALLATION......................................................................................................................... 2-34

2.27 MOUNTING the WX-1000/SKY497 DISPLAY.................................................................................. 2-36

2.27.1 Panel Cutout........................................................................................................................................ 2-36

2.27.2 Display Installation............................................................................................................................. 2-37

Chapter 3

INSTALLATION CHECKOUT

3.1 INTRODUCTION.................................................................................................................................. 3-1

3.2 CONTROLS ........................................................................................................................................... 3-1

3.3 CHECKOUT PROCEDURE ................................................................................................................. 3-2

3.3.1 System Setup ......................................................................................................................................... 3-3

3.3.2 System Setup Verification and Operation ........................................................................................... 3-5

3.4 SELF TEST............................................................................................................................................ 3-7

4.1 INTRODUCTION.................................................................................................................................. 4-1

4.2 CONTINUED AIRWORTHINESS ....................................................................................................... 4-1

4.3 PERIODIC MAINTENANCE ............................................................................................................... 4-1

4.3.1 WX-1000/SKY497 Display .................................................................................................................... 4-1

4.3.2 TRC ........................................................................................................................................................ 4-1

4.3.3 Antenna.................................................................................................................................................. 4-1

4.4 SERVICE MENU .................................................................................................................................. 4-2

4.4.1 Setup ...................................................................................................................................................... 4-3

4.4.1.1 Aircraft Type.......................................................................................................................................... 4-3

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Chapter 4

MAINTENANCE

4.4.1.2 Antenna System..................................................................................................................................... 4-4

4.4.1.3 Audio Level ............................................................................................................................................ 4-4

4.4.1.4 Communication Ports ............................................................................................................................ 4-4

4.4.1.5 Avionics Equipment............................................................................................................................... 4-6

4.4.2 Information ............................................................................................................................................4-8

4.4.2.1 Software Version.................................................................................................................................... 4-9

4.4.2.2 System Log ............................................................................................................................................. 4-9

4.4.2.3 Data Monitor........................................................................................................................................ 4-10

4.4.3 Calibration ........................................................................................................................................... 4-12

4.4.4 Ground Test ......................................................................................................................................... 4-12

4.5 TROUBLESHOOTING ....................................................................................................................... 4-17

4.6 ERROR MESSAGES ...........................................................................................................................4-18

4.7 TRC899/WX-1000 ADAPTER PLUG ..................................................................................................4-20

4.8 DISPOSITION OF FAILED ITEMS................................................................................................... 4-21

Appendix A

SKY899 INTERFACE SIGNAL & CABLE CHARACTERISTICS

A.1 INTRODUCTION ................................................................................................................................. A-1

A.2 ELECTRICAL CHARACTERISTICS .................................................................................................. A-1

A.3 ARINC-429 LABELS .......................................................................................................................... A-11

Appendix B

ENVIRONMENTAL QUALIFICATION FORM

B.1 TRC899 ENVIRONMENTAL QUALIFICATION FORM .................................................................. B-1

B.2 NY156 & NY164 ENVIRONMENTAL QUALIFICATION FORM.................................................... B-2

B.3 WX-1000/SKY497 DISPLAY ENVIRONMENTAL QUALIFICATION FORM ................................ B-3

Appendix C

INSTALLATION CHECKOUT USING THE TCAS-201 RAMP TEST SET

C.1 INTRODUCTION ................................................................................................................................. C-1

C.2 CONTROLS........................................................................................................................................... C-1

C.3 CHECKOUT PROCEDURE................................................................................................................. C-2

Appendix D

INSTALLATION CHECKOUT USING THE TIC T-49C FLIGHTLINE TESTER

D.1 INTRODUCTION ................................................................................................................................. D-1

D.2 CONTROLS........................................................................................................................................... D-1

D.3 CHECKOUT PROCEDURE................................................................................................................. D-2

USING THE TERMINAL DEVICE ................................................................................................................. E-1

Appendix E

USING THE TERMINAL DEVICE

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Appendix F

INSTALLATION CHECKOUT USING AN ALTERNATE DISPLAY

F.1 INTRODUCTION.................................................................................................................................. F-1

F.2 CONTROLS ........................................................................................................................................... F-1

F.3 CHECKOUT PROCEDURE .................................................................................................................F-1

F.4 SELF TEST ............................................................................................................................................ F-5

LIST OF ILLUSTRATIONS

Figure Page

1-1 Vertical Display Modes ......................................................................................................................... 1-4

1-2 SKY899 System Block Diagram ........................................................................................................... 1-5

1-3 Standard TRC Mounting Tray (P/N 805-10870-001) .......................................................................... 1-8

1-4 Ruggedized TRC Mounting Tray (P/N 805-10870-003)....................................................................... 1-9

1-5 P1 Connector Dimensions (Reference Only)........................................................................................ 1-9

1-6 TRC899 Transmitter Receiver Computer (TRC)............................................................................... 1-10

1-7 System Configuration Module............................................................................................................ 1-10

1-8 WX-1000/SKY497 Display Equipment Tag ....................................................................................... 1-11

1-9 WX-1000/SKY497 Display .................................................................................................................. 1-12

1-10 NY156/NY164 Directional Antenna................................................................................................... 1-14

2-1 Directional Antenna Mounting Location ............................................................................................. 2-2

2-2 Interconnect Wiring Without WX-1000 ............................................................................................... 2-3

2-3 Interconnect Wiring With WX-1000..................................................................................................... 2-7

2-4 Interconnect Wiring With Alternate Display .................................................................................... 2-11

2-5 Heading Input Cable........................................................................................................................... 2-18

2-6 Display Cable....................................................................................................................................... 2-20

2-7 Above and Below External Lamps ..................................................................................................... 2-26

2-8 System Configuration Module............................................................................................................ 2-28

2-9 Typical Location of Configuration Module (Inside Backshell) ......................................................... 2-29

2-10 Antenna Mounting Holes.................................................................................................................... 2-31

2-11 Directional Antenna Installation ....................................................................................................... 2-31

2-12 Mounting Holes for Standard Mount Tray, P/N 805-10870-001 ...................................................... 2-32

2-13 Mounting Holes for Ruggedized Mount Tray, P/N 805-10870-003 .................................................. 2-33

2-14 TRC899 Installation............................................................................................................................ 2-34

2-15 Instrument Panel Cutout and Mounting Holes................................................................................. 2-35

2-16 Display Installation............................................................................................................................. 2-36

3-1 Controls.................................................................................................................................................. 3-1

3-2 Start-up Screen...................................................................................................................................... 3-2

3-3 Standby Screen...................................................................................................................................... 3-3

3-4 Typical Patch Antenna Tripod Mount.................................................................................................. 3-6

3-5 Self Test Screen..................................................................................................................................... 3-8

4-1 Service Menu (Terminal Emulation Program)....................................................................................4-2

4-2 Service Menu (WX-1000/SKY497 Display) .......................................................................................... 4-2

4-3 Compact Flash Insertion Instructions ............................................................................................... 4-16

4-4 Service Menu Tree (Sheet 1 of 3)........................................................................................................ 4-17

4-4 Service Menu Tree (Sheet 2 of 3)........................................................................................................ 4-18

4-4 Service Menu Tree (Sheet 3 of 3)........................................................................................................ 4-19

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LIST OF ILLUSTRATIONS

Figure Page

4-5 Adapter Plug Assembly ....................................................................................................................... 4-24

A-1 P1 Connector Pin Identifiers.............................................................................................................. A-11

C-1 Controls ................................................................................................................................................. C-1

C-2 Start-Up Screen .................................................................................................................................... C-3

C-3 Standby Screen ..................................................................................................................................... C-3

D-1 Controls ................................................................................................................................................. D-1

D-2 Start-Up Screen .................................................................................................................................... D-2

D-3 Standby Screen ..................................................................................................................................... D-3

F-1 SKYWATCH Startup Screen on Terminal Device...............................................................................F-2

F-2 External Annunciator Operation..........................................................................................................F-3

F-3 Typical Patch Antenna Tripod Mount ..................................................................................................F-4

LIST OF TABLES

Table Page

1-1 SKY899 System...................................................................................................................................... 1-6

1-2 TRC Installation Kit P/N 817-11900-xxx ............................................................................................. 1-7

1-3 WX-1000/SKY497 Display Installation Kit P/N 817-10802-001 ....................................................... 1-11

1-4 Airframe Installation Kits................................................................................................................... 1-13

1-5 Directional Antenna Installation Kit 817-10009-xxx ........................................................................ 1-14

1-6 TRC899 Software Revisions................................................................................................................ 1-17

1-7 Minimum Interface Equipment Required.......................................................................................... 1-17

1-8 Directional Antenna SIGMA and DELTA Port Cable Vendors ........................................................ 1-18

1-9 Cable to Connector Reference............................................................................................................. 1-19

1-10 Heading Input Cable Vendors ............................................................................................................1-20

1-11 Display Cable Vendors ........................................................................................................................ 1-22

2-1 Alternate Display Drivers ................................................................................................................... 2-25

2-2 WX-1000/SKY497 Display Connection............................................................................................... 2-30

2-3 WX-1000 Processor Connection .......................................................................................................... 2-30

4-1 Fault Isolation...................................................................................................................................... 4-20

4-2 Installation Related Error Messages.................................................................................................. 4-21

4-3 Informational Error Messages............................................................................................................ 4-22

A-1 ARINC-429 Input Labels (Rx)............................................................................................................ A-13

A-2 ARINC-429 Output Labels (Tx) ......................................................................................................... A-14

C-1 IFR Systems TCAS-201 Ramp Test Set Setup Data .......................................................................... C-2

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CHAPTER 1

GENERAL INFORMATION

1.1 INTRODUCTION

This section contains a functional description of the BFGoodrich Avionics Systems SKY899 traffic alert/advisory system sensor, describes the various hardware and software configurations, outlines the main features of the system, and provides a system block diagram. The SKY899 is a new generation traffic alert/advisory system that has different inputs and outputs and it requires different wiring than the SKY497. Connector P1 is keyed differently to prevent connection to the wrong TRC.

NOTES

1. The SKY899 is designed to be installed as a TCAS I traffic alert system or as a TAS traffic advisory system. The system installation differences are as follows:

• TCAS I installations requires an alternate display device (i.e., EFIS, MFD, IVSI, weather

radar indicator) FAA approved for displaying TCAS I information and the antenna must be an NY156 directional antenna.

• TAS installations can have an alternate display device, the WX-1000/SKY497 display, or

both as the primary means displaying traffic information. Either the NY156 or NY164 directional antenna can be used.

2. Contact Field Service Engineering at 1-800-453-0288 or 1-616-949-6600 for approved displays and software version requirements of the TRC899.

3. The SKY899 does not track intruder aircraft approaching at a closure rate greater than 1200 knots.

4. This section provides installation information for the SKY899 using the WX1000/SKY497 Display. If using an alternate display device refer to manufacturer instructions for installation details.

5. When interfacing to a weather radar indicator via the BFGoodrich Avionics Systems RGC250 (Radar Graphics Computer) refer to the RGC250 Installation Manual for installation instructions. RGC250 must have software version 1.5 or later.

6. When an alternate display device is installed the service menu can not be accessed via the display, therefore a terminal device (i.e., laptop) is required for system setup and post-installation checkout (refer to appendix E).

7. When planning ARINC-429 receiver interfaces note that:

• The equipment connected to receive channels 1 and 2 must be the same speed

(12.5 or 100 kHz).

• The equipment connected to receive channels 3 and 4 must be the same speed

(12.5 or 100 kHz).

• Channel 5 receiver is independent of the other receivers and can be set to 12.5 or 100 kHz.

8. In order to use ADS-B SKYWATCH HP requires a GPS input that is GAMA or ARINC-743A compliant.

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1.2 FUNCTIONAL DESCRIPTION

The BFG Avionics Systems SKYWATCH® HP SKY899 is a new generation airborne traffic alert/advisory system that increases the active-mode surveillance range over the SKY497 system from 20 nmi to 35 nmi and adds Automatic Dependent Surveillance-Broadcast (ADS-B) surveillance mode. The SKY899 continuously monitors the dedicated data link frequency (1090 MHz) for ADS-B mode S extended squitter messages within 50 nmi. The ADS-B message contains navigational information about the intruder aircraft including GPS position, ident, ground speed, and intent. The SKY899 uses this navigational information along with its own aircraft GPS navigation data to calculate the relative position of the intruder to augment its active ATCRBS surveillance of the intruder. ADS-B surveillance enhances the traffic alert/advisory abilities by increasing the accuracy of the active-mode surveillance. The SKY899 does not require a mode S transponder, ADS-B capable or otherwise to perform its ADS-B surveillance.

The SKY899 advises the flight crew where to look for aircraft that may pose a collision threat. It is intended for use by corporate and general aviation aircraft. SKY899 alerts the flight crew to nearby transponder equipped aircraft and assists the pilot in the visual acquisition of aircraft that may represent a danger. Traffic information out to a selected range is graphically displayed on the display. Using shapes (i.e., Traffic Advisory = solid circle; Other Traffic = open diamond) and text, the display shows the relative position of threat aircraft.

1.3 PHYSICAL DESCRIPTION

The SKY899 System consists of the following main components:

• Transmitter Receiver Computer

• System Configuration Module

• Alternate Display (or optional monochrome WX-1000/SKY497 display)

• Directional Antenna, NY156 or NY164 (depending on TCAS I or TAS installation)

SKY899 is an active system that operates as an aircraft-to-aircraft interrogation device. The SKY899 equipment interrogates transponders in the surrounding airspace similar to ground based radars. When replies to these active interrogations are received, the responding aircraft’s range, altitude, and closure rates are computed to plot traffic location and predict collision threats. The effective active range is approximately 20 nmi. The SKY899 does not transmit ADS-B interrogations, in order to transmit your aircraft position you must have a mode S transponder capable of ADS-B interrogations.

Figure 1-1 shows the SKY899 vertical display modes used to display intruding aircraft. The unrestricted altitude of the surveillance zone is ±10,000 ft, but the display is only capable of showing to ±9,900 ft. A simplified block diagram of the system and their relationships is shown in figure 1-2.

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Major differences between SKYWATCH and SKYWATCH HP are listed below:

1.3.1 TRC899 Transmitter Receiver Computer P/N 805-11900-xxx

The TRC is mounted in a mounting tray supplied with the installation kit (see table 1-2). The standard tray (figure 1-3) will meet the requirements for fixed wing aircraft. A ruggedized version of the tray (figure 1-4) is required for rotorcraft installations.

To meet different space requirements, the I/O signal connector (P1) will accommodate either a straight or right-angle backshell. TRC installation kits (see table 1-2) include either a straight backshell or right-angle backshell (see figure 1-5).

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Table 1-2. TRC Installation Kit P/N 817-11900-xxx

KIT P/N DESCRIPTION QUANTITY PART NUMBER

817-11900-001 For Installation on Fixed-Wing Aircraft with Straight 1.5 inch

(3.8 cm) Backshell Consists of:

Standard Mounting Tray Assembly 1 805-10870-001

1.5" (3.8 cm) Straight Backshell 1 613-10039-001 I/O Connector, 100-Position, Female, (Mil-C-38999 Series III) 1 605-10251-001

(Includes #22D Crimp Terminals) Spare Terminals for I/O Connector 10 M39029/56-348 Power Connector, 3-Position, Straight Plug 1 MS3126F12-3S

(Includes #16 Crimp Terminals) Spare Terminals for Power Connector (M39029/32-247) 2 607-10018-001 System Configuration Module Assembly 1 814-18005-001

817-11900-002 For Installation on Fixed-Wing Aircraft with Straight 2.5 inch

(6.4 cm) Backshell Consists of:

Standard Mounting Tray Assembly 1 805-10870-001

2.5" (6.4 cm)Straight Backshell 1 613-10042-001 I/O Connector, 100-Position, Female, (Mil-C-38999 Series III) 1 605-10251-001

(Includes #22D Crimp Terminals) Spare Terminals for I/O Connector 10 M39029/56-348 Power Connector, 3-Position, Straight Plug 1 MS3126F12-3S

(Includes #16 Crimp Terminals) Spare Terminals for Power Connector (M39029/32-247) 2 607-10018-001 System Configuration Module Assembly 1 814-18005-001

817-11900-003 For Installation on Fixed-Wing Right-Angle (90°) Backshell

Consists of:

Standard Mounting Tray Assembly 1 805-10870-001 Right-Angle (90°) Backshell 1 613-10043-001 I/O Connector, 100-Position, Female, (Mil-C-38999 Series III) 1 605-10251-001

(Includes #22D Crimp Terminals) Spare Terminals for I/O Connector 10 M39029/56-348 Power Connector, 3-Position, Straight Plug 1 MS3126F12-3S

(Includes #16 Crimp Terminals) Spare Terminals for Power Connector (M39029/32-247) 2 607-10018-001 System Configuration Module Assembly 1 814-18005-001

817-11900-004 For Installation on Rotorcraft with 2.5 inch (6.4 cm) Backshell

Ruggedized Mounting Tray Assembly 1 805-10870-003

2.5" (6.4 cm)Straight Backshell 1 613-10042-001 I/O Connector, 100-Position, Female, (Mil-C-38999 Series III) 1 605-10251-001

(Includes #22D Crimp Terminals) Spare Terminals for I/O Connector 10 M39029/56-348 Power Connector, 3-Position, Straight Plug 1 MS3126F12-3S

(Includes #16 Crimp Terminals) Spare Terminals for Power Connector (M39029/32-247) 2 607-10018-001 System Configuration Module Assembly 1 814-18005-001

817-11900-005 For Installation on Rotorcraft with Right-Angle (90°) Backshell

Consists of:

Ruggedized Mounting Tray Assembly 1 805-10870-003 Right-Angle (90°) Backshell 1 613-10043-001 I/O Connector, 100-Position, Female, (Mil-C-38999 Series III) 1 605-10251-001

(Includes #22D Crimp Terminals) Spare Terminals for I/O Connector 10 M39029/56-348 Power Connector, 3-Position, Straight Plug 1 MS3126F12-3S

(Includes #16 Crimp Terminals) Spare Terminals for Power Connector (M39029/32-247) 2 607-10018-001 System Configuration Module Assembly 1 814-18005-001

1-7

Rev. A

Preliminary

SKY899

Installation Manual

RETAINER CUPS

HOLD-DOWN KNOBS

(2-PLACES)

DIMENSIONS ARE IN INCHES (MILLIMETERS)

NOTE

REAR HOLD-DOWN PINS

(2-PLACES)

(

)

3.37 (85.6) MAX.

(

)

(

)

(

4.15

(105.4)

MAX.

)

1-8 Rev. A

)

(

)

Figure 1-3. Standard TRC Mounting Tray (P/N 805-10870-001)

Preliminary

SKY899

Installation Manual

DIMENSIONS ARE IN INCHES (MILLIMETERS)

NOTE

DOES NOT INCLUDE SCREW

COG

)

(

)

HEADS

)

(

3.66 (93.0) MAX.

)

(

)

(

)

(

Figure 1-4. Ruggedized TRC Mounting Tray (P/N 805-10870-003)

DIMENSIONS ARE IN INCHES (MILLIMETERS)

4.75

(120.7)

REF.

NOTE

4.25

(108.0)

REF.

3.25

(82.6)

REF.

STRAIGHT

BACKSHELL

P/N 613-10042-001

Figure 1-5. P1 Connector Dimensions (Reference Only)

SPLIT ELBOW

90° BACKSHELL

P/N 613-10043-001

1-9

Rev. A

Preliminary

SKY899

Installation Manual

4.15 - REF (105.4)

DIMENSIONS ARE IN INCHES (MILLIMETERS)

NOTE

)

7.62

(193.0)

MAX.

4.15

(105.4)

(

)

2 Y

)

(

)

(

)

Figure 1-6. TRC899 Transmitter Receiver Computer (TRC)

1.3.2 System Configuration Module P/N 814-18005-001

The system configuration module is used to store aircraft installation dependent information via the service menu. The system configuration is read from the module during turn-on. The module is included in the installation kit and is designed to be installed inside the backshell of connector P1.

1-10 Rev. A

Preliminary

SKY899

Installation Manual

1.3.3 Display (Alternate or WX-1000/SKY497 Display P/N 78-8060-5900-x)

The display used is installation dependent. If installing to meet the requirements for a TCAS I installation an alternate display device (i.e., EFIS, MFD, IVSI, weather radar indicator) approved for displaying TCAS I information is required. If installing to meet requirements for a TAS installation an alternate display device, the WX-1000/SKY497 display, or both can be used as primary means for displaying traffic information.

When interfaced to both displays (alternate display and WX-1000/SKY497 display),

display functions can be linked together or separate depending on the capabilities of the alternate display. When installed with an alternate display device only, the service menu cannot be accessed via the display, therefore a terminal device (i.e., laptop) is required for system setup and post-installation checkout (see appendix F). If both displays are connected the service menu can be accessed by the WX-1000/SKY497 display only.

The SKY899 is designed to transmit traffic information to the alternate display device via our ARINC-429 bus interface (100 kHz fixed speed). Refer to display manufacturer instructions for installation details.

WX-1000/SKY497 Display P/N 78-8060-5900-x. To operate with SKYWATCH HP, existing WX-1000 displays must conform to TSO-C113. If the equipment tag on the back of the unit (see figure 1-7) does not identify SKYWATCH and TSO-C113, return the display to the factory for modification. To schedule workload and ensure a quick turn around, a return authorization will be required. Call BFG Avionics Systems Customer Service (1-800-453-0288 or 1-616-949-6600) for details.

Stormscope

Weather Mapping Systems

Series II

TRAFFIC ADVISORY SYSTEM

WX-1000 / SKY497 DISPLAY

78-8060-5900-9 TSO C110a, C113

Pat. USA 4,023,408;U.K. 1,529,624; Germany 26-00-658; Others Pend.

SERIAL NO.

ace

erosp

2.3lb. 1.0kg.

BFGoodrich Avionics Systems, Inc. Grand Rapids, MI USA

TAG MUST IDENTIFY

SKYWATCH AND TSO-C113.

Figure 1-7. WX-1000/SKY497 Display Equipment Tag

The display unit mounts in a standard 3ATI panel cutout. All connections to the display are made through a single 25-position male D-subminiature connector on the back panel. Figure 1-8 depicts the indicator dimensions. The last digit of the part number identifies the different versions (refer to para 1.4.2). Table 1-3 lists the contents of an installation kit supplied with each unit.

Table 1-3. WX-1000/SKY497 Display Installation Kit P/N 817-10802-001

QUANTITY PART NUMBER DESCRIPTION

4 26-1001-6374-5 Screw, Machine, 6-32 x 3/4 in. Phillips Pan Head, Black Oxide 1 26-1003-5633 Connector, 25 Position Recpt. Shell 1 26-1006-2426-6 Connector Backshell, DB25 2 26-1006-1089-3 Connector Lock Post Assembly

25 26-1003-4274-9 Connector Socket, Screw Machine (M39029/63-368)

1-11

Rev. A

Preliminary

SKY899

Installation Manual

3.37

(85.6)

0.55

(14.0)

NOTE

C.G.

3.37

(85.6)

DIMENSIONS ARE IN INCHES (MILLIMETERS)

3.89

(98.8)

3.18

(80.8)

J101

3.18

(80.8)

1-12 Rev. A

0.17 ±0.02

(4.3 ±0.5)

0.08

(2.0)

C.G.

3.40

(86.4)

8.07

(205.0)

P101

1.30

(33.0)

Figure 1-8. WX-1000/SKY497 Display

Preliminary

SKY899

Installation Manual

1.3.4 Directional Antenna (NY156 P/N 805-10003-001 or NY164 P/N 805-10890-001)

The directional antenna is a teardrop-shaped antenna. Connections are made through two TNC and one BNC connector. The antenna is sealed against environmental extremes and is non-repairable. To ensure a tight seal between the airframe and antenna, an O-ring seal (i.e., an O-ring groove for an MS28775-044 Oring) has been incorporated into the design. An O-ring is supplied with each antenna and must be installed when mounting the antenna.

To fit specific airframes, a special adapter plate is also required. The adapter plate is included in the installation kit shipped with each system. Refer to table 1-4 for a list of installation kits associated with various airframes. For aircraft not listed, contact the aircraft manufacturer for information relative to the radius of the area where the antenna is to be mounted. Table 1-5 lists the contents of each installation kit. The installation kits differ only in the size of the special airframe adapter plate. Figure 1-9 depicts the antenna dimensions.

Table 1-4. Airframe Installation Kits

INSTALLATION KIT

MANUFACTURER AIRFRAME

AEROSPATIALE ATR-42 817-10009-001

AGUSTA A109 817-10009-006

BAE/RAYTHEON HAWKER 400, 600, 700, 800, and 1000 817-10009-004

BEECH

BELL 206, 407, 427 817-10009-006

CANADAIR CHALLENGER 600 and 601 817-10009-005

CESSNA CITATION III, VI, VII

COMMANDER 114 817-10009-006

DASSAULT FALCON 10, 20, 50

DEHAVILLAND Dash 7/8 817-10009-001

EMBREAR EMB 110, 120 817-10009-001

EUROCOPTER EC135 817-10009-006

FAIRCHILD METROLINER, METROLINER III, MERLIN 817-10009-001

FOKKER F28 817-10009-003

GULFSTREAM G-I, G-II, and G-III 817-10009-001

IAI WESTWIND 1125 817-10009-001

LEARJET LEARJET 31, 35, 36, 55, and 60 817-10009-004

MITSUBISHI MU-2 817-10009-002

MOONEY M20 817-10009-006

PILATIS PC-12 817-10009-001

PIPER CHEYENNE 400LS

SAAB SF-340 817-10009-001

SABRELINER SABRE 65 817-10009-001

SHORTS 360 817-10009-001

SIKORSKY S-76 817-10009-006

SOCATA TBM-700

BEECHJET, KING AIR 90, 100, 200, 300, and 350

BARON 33, 35, 36, 55, 58, BE-99, 1300, & 1900C/D

CITATIONJET, CITATION I, II, V 182, 210, 337, 401, 414, 425, 441

FALCON 900

NAVAJO

MIRAGE, MALIBU

SARATOGA, SENECA

TB20

PART NUMBER

817-10009-001 817-10009-002

817-10009-001 817-10009-004 817-10009-006

817-10009-001 817-10009-005

817-10009-001

817-10009-002

817-10009-005

817-10009-006

817-10009-001

817-10009-006

1-13

Rev. A

Preliminary

SKY899

Installation Manual

Table 1-5. Directional Antenna Installation Kit 817-10009-xxx

SUPPLIED PARTS *

KIT PART NUMBER PART NUMBER DESCRIPTION QUANTITY

817-10009-001 800-10066-001 Special Adapter Plate, 40 Inch (101.6 cm) Radius 1 817-10009-002 800-10066-002 Special Adapter Plate, 63 Inch (160.0 cm) Radius 1 817-10009-003 800-10066-004 Special Adapter Plate, 80 Inch (203.2 cm) Radius 1 817-10009-004 800-10066-003 Special Adapter Plate, 32 Inch (81.3 cm) Radius 1 817-10009-005 800-10066-005 Special Adapter Plate, 47 Inch (119.4 cm) Radius 1

817-10009-006 (No Adapter Plate)

100-10022-001* 101-10027-001*

Screw, 10-32 x 1 PPH SS (MS51958-67) Stop Nut, 10-32 (MS21044C3)

* Hardware supplied with all kits.

4 4

DIMENSIONS ARE IN INCHES (MILLIMETERS)

NOTE

FWD

DO NOT PAINT

FORWARD

6.23 ±0.08

(158.2 ±2.0)

1.30

(33.0)

1-14 Rev. A

0.725

(18.4)

SUM PORT (Blue Band)

PROBE PORT

(Black Band)

5.06

(128.5)

11.12

(282.4)

DIFFERENCE PORT

(Red Band)

5.71

(145.0)

0.45

(11.4)

Figure 1-9. NY156/NY164 Directional Antenna

Preliminary

Installation Manual

1.4 SPECIFICATIONS

1.4.1 Transmitter Receiver Computer (TRC)

SKY899

PART NUMBER:

SIZE:

WEIGHT:

OPERATING TEMPERATURE:

STORAGE TEMPERATURE:

OPERATING ALTITUDE:

COOLING:

POWER REQUIREMENTS:

TRACKING CAPABILITY:

SURVEILLANCE RANGE:

DISPLAY RANGES:

805-11900-001 - TRC899

Approximately 12.52 inches (31.90 cm) Deep Approximately 3.56 inches (9.04 cm) Wide Approximately 7.62 inches (19.36 cm) High

Approximately 8.88 lb (4.03 kg) Not Including Mounting Tray Approximately 9.76 lb (4.43 kg) With Standard Mounting Tray Approximately 10.89 lb (4.94 kg) With Ruggedized Mounting Tray

-55 to +70 degrees Celsius (-67 to +158 degrees Fahrenheit)

-55 to +85 degrees Celsius (-67 to +185 degrees Fahrenheit)

55,000 feet (Maximum)

Conduction and Forced Air (Internal Fan) Convection

18 to 32 V dc, 2 Amps @ + 28 V dc(Maximum)

Up to 35 intruder aircraft (displays only the 8 highest priority aircraft)

Horizontal tracking radius:

35 nmi Maximum ATCRBS Surveillance 50 nmi Maximum ADS-B Surveillance

Relative altitude tracking range:

±10,000 ft maximum

Horizontal display ranges:

2, 6 & 15 nmi (WX-1000/SKY497 Display)

Relative altitude display ranges:

±2,700 ft (normal mode) +9,000 ft to -2,700 ft (above mode/look up) +2,700 ft to -9,000 ft (below mode/look down) +9,900 ft to -9,900 ft (unrestricted)

RANGE ACCURACY:

BEARING ACCURACY:

ALTITUDE ACCURACY:

CERTIFICATION: *

RTCA COMPLIANCE:

± 0.05 nmi (Typical)

With NY156 Antenna - 5° RMS (Typical) 30° Peak Error With NY164 Antenna - 7° RMS (Typical) 30° Peak Error

±200 ft

USA (FAA) TSO C118 (TCAS I) & C147 (TAS) Refer to FSAW 98-04B for Flight Standards

Service policy concerning follow-on field approvals.

Software DO178-B Level D

DO-160D Category F2XBAB[(SBM)(UG)]XXXXXXZBABARRLXXXXXXA

* Listed are current certifications at time of publication, contact Field Service Engineering at 1-800-453-

0288 or 1-616-949-6600 for latest certification information.

Rev. A

1-15

Preliminary

1.4.2 WX-1000/SKY497 Display

PART NUMBER DEFINITION:

78-8060-5900-8 (Black Bezel) 78-8060-5900-9 (Gray Bezel)

SIZE:

Height: 3.37 inches (8.56 cm) Width: 3.37 inches (8.56 cm) Depth: 8.24 inches (20.92 cm)

WEIGHT:

2.3 lb (1.0 kg)

OPERATING TEMPERATURE:

-20 to +55 degrees Celsius (-4 to +131 degrees Fahren heit)

STORAGE TEMPERATURE:

-55 to +70 degrees Celsius (-67 to +158 degrees Fahrenheit)

OPERATING ALTITUDE:

55,000 feet (Maximum)

TSO COMPLIANCE:

C110a & C113

SKY899

Installation Manual

RTCA COMPLIANCE:

DO-160C F1-CA(NBM)XXXXXXZXXXZUAXXXXXX

POWER REQUIREMENTS:

+15/-15 V dc, 0.7 A (Maximum)

1.4.3 Directional Antenna

PART NUMBER: 805-10003-001 (NY156)

805-10890-001 (NY164)

SIZE: 1.3 inches (3.25 cm) high

6.23 in (15.82 cm) wide

11.12 in (27.94 cm) deep

WEIGHT: 2.3 lb (1.04 kg)

SPEED: Rated to 600 knots (0.9 Mach) @ 25,000 feet.

FREQUENCY: 1030-1090 MHz

TSO CATEGORY: C118

ENVIRONMENTAL CATEGORY: DO-160C F2-AC(CLM)XSFDFSXXXXXXXL(2A)X

FINISH: Gloss white Skydrol resistant polyurethane paint

1.5 MODIFICATIONS & SOFTWARE REVISIONS

Modifications (MODS) and software revisions for the TRC899 are identified by an entry on the S/N & I.D. tag. The system software revision is a collective designator for all software/firmware installed within the TRC899. software versions are listed below.

SKY HP software version can be verified via the service menu. Hardware modifications and

Hardware Modifications - None at the time of publication.

1-16 Rev. A

Preliminary

SKY899

Installation Manual

Table 1-6. TRC899 Software Revisions

SYSTEM

REVISION

1.00 1.00 Original production release.

1.6 INTERFACE

The electrical characteristics of all input and output signals are detailed in Appendix A. Listed below in table 1-7 is the minimum equipment required to interface with the SKY899. See chapter 2 for details.

SURVEILLANCE

MODE

SKY HP

VERSION

DESCRIPTION

Table 1-7. Minimum Interface Equipment Required

AVIONICS EQUIPMENT

GPS NAV

MAGNETIC HEADING

RADIO ALTITUDE

SQUAT SWITCH (WOW)

BAROMETRIC ALTITUDE

LANDING GEAR SWITCH

SUPPRESSION BUS

(PUSHBUTTONS)

PILOT CONTROLS

EXTERNAL LAMPS

AUDIO INHIBIT (GPWS)

AUDIO SYSTEMS

ATCRBS

(Active Only)

ATCRBS & ADS-B X X

Required.

① Optional but will enhance performance. (See paragraphs 2.7 thru 2.23 for details.) ② Required if Terrain Warning System (GPWS) is installed. ③ Only if Alternate Display requires it, see display manufacturer's instructions.

1.7 EQUIPMENT REQUIRED BUT NOT SUPPLIED

Antenna Cables The installer will supply all antenna cables and connectors. The directional

Use of any cable not meeting BFGoodrich Avionics Systems specifications voids all system warranties.

①

antenna requires three cable assemblies; sum (Sigma Port), bit probe (Probe Port) and difference (Delta Port). Cable attenuation for the sum and difference ports must not exceed 2.5 dB. Table 1-8 identifies U. S. vendors who sell approved cables by the foot. Table 1-9 provides a cable to connector cross-reference.

RG142B or equivalent may be used for the bit probe cable. Attenuation for the bit probe cable must not exceed 6 dB.

①①

①

NOTE

①

②③ ③

1-17

Rev. A

Preliminary

SKY899

Installation Manual

Table 1-8. Directional Antenna SIGMA and DELTA Port Cable Vendors

Electrical & Mechanical Technologies (EMTEQ)

1-888-679-6170

262-679-6170

FAX 262-679-6175

Attenuation

Part Number

PFLX195-100 10.81 2.7 21.8 0.50 PFLX240-100 9.76 4.5 25.0 0.75 PFLX340-100 6.3 7.2 38.2 0.88

Part Number

352001 12.2 2.7 15 0.81 311601 8.7 5.5 26 1.15 311201 5.56 8.5 41 1.59 310801 3.63 16.1 63 2.26

Part Number

S33141 7.2 6.5 32 1.5 S55122 5.7 8.2 40 1.6 S22089 3.8 18 61 2.5

(dB/100 ft 1.0 gHz)

Attenuation

(dB/100 ft 1.0 gHz)

Attenuation

(dB/100 ft 1.0 gHz)

Weight (lb) (per 100 ft)

Electronic Cable Specialists

1-800-327-9473

414-421-5300

FAX 414-421-5301

Weight (lb) (per 100 ft)

PIC Wire and Cable

1-800-742-3191

262-246-0500

FAX 262-246-0450

Weight (lb) (per 100 ft)

Maximum Length

(ft)

Maximum Length

(ft)

Maximum Length

(ft)

Minimum Bend

Radius (in)

Minimum Bend

Radius (in)

Minimum Bend

Radius (in)

If cable weight is not a consideration, select lowest loss cable. Contact cable vendors before installation. New low-loss light-weight cables may be available.

1-18 Rev. A

Preliminary

SKY899

Installation Manual

Table 1-9. Cable to Connector Reference

Electrical & Mechanical Technologies (EMTEQ)

1-888-679-6170

262-679-6170

FAX 262-679-6175

Cable Part Number TNC Straight TNC Right Angle BNC Straight BNC Right Angle

PFLX195-100 TMS195-1 TMR195-1 BMS195-1 BMR195-1 PFLX240-100 TMS240-1 TMR240-1 BMS240-1 BMR240-1 PFLX340-100 TMS340-1 TMR340-1 BMS340-1 BMR340-1

Electronic Cable Specialists

1-800-327-9473

414-421-5300

FAX 414-421-5301

Cable Part Number TNC Straight TNC Right Angle BNC Straight BNC Right Angle

311601 CTS922 CTR922 CBS922 CBR922 311201 CTS122 CTR122 CBS122 CBR122 310801 CTS022 CTR022 CBS022 CBR022 352001 CTS3522 CTR3522 CBS3522 CBR3522

PIC Wire and Cable

1-800-742-3191

262-246-0500

FAX 262-246-0450

Cable Part Number TNC Straight TNC Right Angle BNC Straight BNC Right Angle

S33141 190308 190309 190312 190313 S55122 190608 190609 190612 190613 S22089 190408 190409 190412 190413

Antenna Sealant For pressurized aircraft, use a sealant that meets the requirements of SAE

AMS-S-8802 such as Flamemaster® CS3204 class B. For non-pressurized aircraft, use a non-corrosive sealant that meets the physical requirements of MIL-A-46146 such as General Electric RTV162.

Circuit Breaker 5 Amp

Connector Installation Antenna Cables See table 1-8.

Tool M22520/5-01 Die M22520/5-19 (EMTEQ Cable PFLX195-100) Die M22520/5-43 (EMTEQ Cable PFLX240-100) Die M22520/5-35 (EMTEQ Cable PFLX340-100) Die M22520/5-19 (ECS Cable 311601)

P1 Interconnect Crimping Tool M22520/2-01

Die M22520/5-61 (ECS Cable 311201) Die M22520/5-21 (ECS Cable 310801) Die 190318 (PIC Cable S33141) Die 190418 (PIC Cable S22089) Die 190618 (PIC Cable S55122)

Positioner M22520/2-07 Insertion MS27495 A22M

Removal MS27495 R22M

1-19

Rev. A

Preliminary

SKY899

Installation Manual

Connector Installation (Continued)

P8 Power Crimping Tool M22520/1-01

Positioner M22520/1-02 Insertion MS24256A16 Removal MS24356R16

P101 Display Crimping Tool M22520/2-01

Positioner M22520/2-08 Insertion/Removal M81969/1-02

Data Cables RS-232, RS-422, and ARINC-429 data cables are #22 AWG (minimum)

twisted, shielded cables.

Flightline Tester Either the BFG TT391 Flightline Tester, IFR Systems TCAS-201 (with

TCAS I firmware) Ramp Test Set (Appendix C), or TIC T-49C Flightline Tester (Appendix D). The test set is required to do the post installation checkout.

Heading Input Cable This cable provides aircraft heading information to the SKY899. Cable that

meets the specification for SKY899 installation is available from suppliers listed in table 1-10.

Table 1-10. Heading Input Cable Vendors

COMPANY

Dallas Avionics 1-800-527-2581 214-320-9776 FAX 214-320-1057

CABLE

P/N

WX-5 (6.84 lb/ 100 ft)

Lamps (external annunciators)

Electronic Cable Specialists 1-800-327-9473 414-421-5300 FAX 414-521-5301

A.E. Petsche 817-461-9473 FAX 817-277-2887

EDMO Distributors 1-800-235-3300 805-295-6689 FAX 1-800-828-0623 FAX 805-295-6703

3N6607 (7.5 lb/ 100 ft)

TZGYR (6.84 lb/ 100 ft)

WX-1000 SYNCHRO

PIC Wire and Cable 1-800-742-3191 262-246-0500 FAX 262-246-0450

External annunciators are required when using an alternate display that is not capable of displaying above and below vertical modes. Lamp outputs are switched to ground when active (LP1OUT & LP2OUT). Lamps should be labeled ABV and BLW. An optional operation mode lamp can be installed to show system has been switched from standby into operation mode. Refer to paragraph 2.14, 2.15 and A.2. Lamps can be 12V or 28V with maximum current 300 mA

WM25807 (7.2 lb/ 100 ft)

1-20 Rev. A

+ 105 hidden pages

L 3 Communications Avionics Systems TRC899 User Manual

Specifications and Main Features

Frequently Asked Questions

User Manual

ABOUT THIS MANUAL

LIST OF EFFECTIVE PAGES

FOREWORD

TABLE OF CONTENTS

1.1 INTRODUCTION

1.2 FUNCTIONAL DESCRIPTION

1.3 PHYSICAL DESCRIPTION

1.3.1 TRC899 Transmitter Receiver Computer P/N 805-11900-xxx

1.3.2 System Configuration Module P/N 814-18005-001

1.3.3 Display (Alternate or WX-1000/SKY497 Display P/N 78-8060-5900-x)

1.3.4 Directional Antenna (NY156 P/N 805-10003-001 or NY164 P/N 805-10890-001)

1.4 SPECIFICATIONS

1.4.1 Transmitter Receiver Computer (TRC)

1.4.2 WX-1000/SKY497 Display

1.5 MODIFICATIONS & SOFTWARE REVISIONS

1.6 INTERFACE

1.7 EQUIPMENT REQUIRED BUT NOT SUPPLIED