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 or figure number, and the page number.
Send your comments to:Rockwell Collins, Inc.
400 Collins Road NE, M/S 153-250
Cedar Rapids, IA 52498-0001
nuals@rockwellcollins.com
ins, Inc.
onse Center
ad NE, M/S 133-100
IA 52498-0001
For product or
ders or inquiries,please contact:
EMAIL: techma
Rockwell Coll
Customer Resp
400 Collins Ro
Cedar Rapids,
.
T-2
TELEPHONE: 1.8
INTERNATIONAL
FAX NO: 319.295
EMAIL: respons
e@rockwellcollins.com
88.265.5467
: 1.319.265.5467
.4941
523-0809018
INSERT LATEST CHANG ED PAGES. DESTROY SUPERSEDED PAGES.
LIST OF EFFECTIVE PAGES
Dates of issue for original and changed pages are:
NOTE:The portion of the text affected by the changes is indicated by a vertical line
in the outer margins of the page. Changes to illustrations are ind icated by
shaded or screened areas, or by miniature pointing hands.
Original0 ...........29 May2009
TOTAL NUM BER OF PAGES IN THIS PUBLICATION IS 210 CONSISTING OF THE FOLLOWING:
This Installation Manual (IM) provides installation information regarding the TSS-4100 Traffic Surveillance System and its related
equipment.
OW TO USE THE MANUAL.
2. H
This IM is written to Air Transport Association (ATA) Specification 100 standards and contains the chapters outlined below:
2.1. C
General Information chapter describes the purpose and technical properties of the Traffic Surveillance System LRUs.
hapter 1.
2.2. C
System Components chapter describes each LRU separately and in detail. First the LRU is described as it relates to the rest of the
Traffic Surveillance System. Then the LRU is described as a stand alone piece of avionics equipment.
2.3. C
Operation ch a pter provides a description of the operating controls and displays that are available in the Traffic Surveillance System.
2.4. C
Maintenance chapter provides flight line maintenance instructions for the Traffic Surveillance System. This includes theory of operation.
2.5. A
Appendices describe very detailed information about the avionics system.
1.APPENDIX A Faults and Warnings
2.APPENDIX B Maintenance Words
3.APPENDIX C Buses and Other Interfaces
4.APPENDIX D Equipment Characteristics
5.APPENDIX E Interconnect Diagram
3. A
The list that follows shows the abbreviations, acronyms, and mnemonics that are used in this publication to describe the avionics
system.
T
ABSAbsolute
ACASAirborne Collision Avoidance System
ADCAir Data Computer
ADLPAircraft Data Link Processor (MODE-S)
ADSAir Data System
ADS-BAutomatic Dependent Surveillance-Broadcast
AFDAdaptive Flight Display
AHCAttitude Heading Computer
ALTAltitude
ANTAntenna
ARINCDigital Database Protocols
ATCA i r TrafficControl
ATCRBSAir Traffic Control Radar Beacon System
hapter 2.
hapter 3.
hapter 4.
PPENDICES .
CRONYMS, ABBREVIATIONS, AND MNEMONICS.
ERMMEANING
ix
introduction523-0809018
AUTOAutomatic
BITEBuilt-In Test Equipment
BNRBinary
CDUControl Display Unit
CPNCollins Part Number
CRCCyclic Redundancy Check
DCPDisplay Control Panel
DCUData Concentrator Unit
DPSKDifferential Phase Shift Keying
ECUExternal Compensation Unit
EFISElectronic Flight Instrument System
ESDSElectrostatic Discharge Sensitive
FMSFlight Management System
GPSGlobal Positioning System
HAEHeight Above Ellipsoid
HDGHeading
HgMillimeters of Mercury
HIRFHigh Intensity Radiated Field
HSIHorizontal Situation Indicator
HVHigh-Voltage
IAPSIntegrated Avionics Processor System
IRSInertial Reference System
LRULine Replaceable Unit
MCUModular Concept Unit
MFDMultifunction Display
msMilli second
MSLMean Sea Level
NANot Applicable
NVRAMNon-Volatile RAM
PAMPulse Amplitude Modulation
PFDPrimary Flight Display
PPOSPresent Position
RATCAS Resolution Advisory
RAMRandom Access Memory
RELRelative
RIURadio Interface Unit
ROMRead Only Memory
RTURadio Tuning Unit
SDISource Destination Identifier
SLSSide-Lobe-Suppression
STBYStandby
STCSupplemental Type Certificate
TATraffic Advisory
TBDTo Be Determined
TCType Certificate
TCASTraffic Alert Collision Avoidance System
TDRTransponder
TFCTraffic
TRETCAS II Directional Antenna
TSOTechnical Standard Order
TSATraffic Surveillance Antenna
TSSTraffic Surveillance System
TSSATraffic Surveillance System Applicatio n
TSMTraffic Surveillance Mount
TTCTCAS Transponder Control
TXTransmit
x
To submit comments regarding this manual, please contact:
Rockwell Collins, Inc.
400 Collins Rd NE
Cedar Rapids, IA 52498-0001
Attn: Technical Operations M/S 153-250
or send email to: techmanuals@rockwellcollins.com
introduction523-0809018
xi/(xii Blank)
523-0809018
SAFETY SUMMARY
1. GENERAL SAFETY INSTRUCTIONS.
This manual describes physical and chemical processes which may cause injury or death to personnel or damage to equipment if
not properly followed. This safety summary includes general safety precautions and instruction that must be understood and applied
during operation and maintenance to make sure personnel safety and protection of equipment. Prior to performing any task, the
WARNING, CAUTIONS, and NOTES included in that task shall be reviewed and understood.
2. W
ARNING, CAUTIONS AND NOTES.
WARNINGS and CAUTIONS are used in this manual to highlight operating or maintenance procedures, practices, conditions or
statements which are considered essential to protection of personnel (WARNING) or equipment (CAUTION). WARNINGS and
CAUTIONS immediately precede the s tep or procedure to which they apply. WARNINGS and CAUTIONS consist of four parts:
heading (WARNINGS, CAUTIONS or Icon [HAZARDOUS MATERIALS WARNING ]), a statement of the hazard, minimum
precautions, and possible result if disregarded. NOTES are u sed in this manual to highlight operating o r maintenance procedures,
practices, conditions or statements which are not essential to protection of personnel or equipment. NOTES may precede or follow
the s tep or procedure, depending upon the information to be highlighted. The headings used and definitions are as follo ws.
Highlights an essential operating or maintenance procedure, practice, condition, or statement, etc. which if not
strictly observed, could result in injury to, or death of, personnel or long term health hazards.
Highlights a
strictly observed, could result in damage to, or destruction of, equipment or loss of mission effectiveness.
n essential operating or maintenance procedure, practice, condition, or statement, etc. which if not
NOTE
Highlights an essential operating or maintenance procedure, condition, or statement.
xiii/(xiv Blank)
523-0809018
CHAPTER 1
General Information
1.1. INTRODUCTION.
This publication provides all the specifications, principles of operation, and information necessary to install, test, and troubleshoot
the TSS-4100 Traffic Surveillance System (TSS). The three major functions of the TSS-4100 follow:
• The TSS-4100 is a Mode S transponder that replies to directed and all-call interrogations.
• The TSS-4100 is a Traffic Alert Collision Avoidance Sy stem (TCAS) II, change 7 unit. It monitors the area around the aircraft
for potential airspace conflicts.
• When enabled, the TSS-4100 is also an Automatic Dependent Surveillance-Broadcast (ADS-B) transmitter/receiver u nit. It transmits the aircraft position, v e locity, and identification. It also processes the transmissions of other ADS-B equipped aircraft.
1.2. E
The Equipment Covered table shows the system avionics, mount, and avionics software. Associated equipment shows closely related
avionics. Refer to Figure 1-1 for the hardware of a typical single Traffic Surveillance System.
1.2.1. E
Refer to Table 1-1 for a complete list of the Rockwe ll Collins avionics equipment covered in this manual.
QUIPMENT.
quipment Covered.
Table 1-1. Equipment Covered.
UNITDESCRIPTIONCOLLINS PART
NUMBER
TSS-4100Traffic Surveillance System822-2132-0011
TSSA-4100 Traffic Surveillance System Application810-0052-0011
TSM-4100Traffic Surveillance Mount866-0128-0201
ECU-3000External Compensation Unit
-802: TCAS II, EHS Mode S Transponder
-803: TCAS II, EHS Mode S Transponder, ADS-B
Out
TSA-4100Traffic Surveillance Antenna
-101: Baseline antenna; short connectors
822-1200-80X1
866-0016-X011+1
STANDARD
QUANTITY
OPTIONAL
QUANTITY
-001: Optional replacement; long connectors
TRE-930Omnidirectional Antenna866-5019-0101-1
1-1
general information523-0809018
Table 1-2. Associated Equipment.
UNITDESCRIPTIONCOLLINS PART
NUMBER
STANDARD
QUANTITY
OPTIONAL
QUANTITY
NOTE
Information for the TDR-94D and ANT-42 is for reference only. Refer to the Pro Line II Comm/Nav/Pulse System Installation Manual, Collins Part Number (CPN) 523-0772719.
TDR-94DAir Traffic Control Radar Beacon System (ATCRBS)
Mode S Transponder: -008, -108, -308, -309, -408,
or -409.
ANT-42Mode S omnidirectional antenna. Used with
TDR-94D.
1.2.1.1. In addition to the Avionics, the TSS-4100 Mode S Address Programming Tool, CPN 811-3937-002, is covered in chapter
4 of this installation manual. This is used to program the Mode S Address for use by the TSS-4100.
622-9210-X0X1
622-6591-0012
1-2
general information523-0809018
Figure 1-1. Typical Single Traffic Surveillance System
1-3
general information523-0809018
1.3. SYSTEM OVERVIEW.
This section gives an overview of the Traffic Surveillance System.
1.3.1. S
ystem Block Diagram.
NOTE
Most units report maintenance informatio n in a diagnostic word to the built-in diagnostic system. This section does
not refer to these diagnostic words. Refer to the maintenance section of this manual for diagnostic information.
The system schematics are not intended to replace bench level repair coverage. Component level coverage i s
provided in the applicable repair manual.
Refer to Figure 1-2 for a block diagram of a typical Traffic Surveillance System with Radio Interface Uni t (RIU). Refer to Figure
1-3 for a block diagram o f a typical Traffic Surveillance System without RIUs. Heavy solid-black borders identify all system units.
The slashed border outlines identify the interfacing units.
1-4
general information523-0809018
Figure 1-2. Typical Traffic Surveillance System with RIUs, Block Diagram
1-5/(1-6 Blank)
general information523-0809018
Figure 1-3. Typical Traffic Surveillance System without RIUs, Block Diagram
1-7/(1-8 Blank)
general information523-0809018
1.4. COMPONENT DESCRIPTIONS.
The Traffic Surveillance System fully integrates with an airplane transponder and TCAS control system. The Traffic Surveillance
System includes the Line R eplaceable Units (LRU) that follow:
• One TSS-4100 Traffic Surveillance System LRU
• TSSA-4100 Traffic Surveillance System Application (TSSA) software
• One ECU-3000 External Compensation Unit (ECU)
• One upper TSA-4100 Traffic Surveillance Antenna (TSA)
• One lower TRE-930 L-Band Omnidirectional TCAS Antenna (TRE)
• One TSM-4100 Traffic Surveillance Mount (TSM) with monitored cooling fan
•OneAirTraffic Control (ATC) Mode-S Transponder (TDR)
• Two ANT-42 L-Band Transponder Omnidirectional Antennas (ANT)
• A transponder/TCAS control unit
•Atrafficdisplay
• An aural alert system.
The LRU overviews below describe each unit in the Traffic Surveillance System.
1.4.1. T
SS-4100 Traffic Surveillance System.
The TSS-4100 is the main component of the Traffic Surveillance System. The TSS-4100 operates on 28-V dc. It contains al l circuits
necessary for computing, transmitting, and receiving functions of the Traffic Surveillance System and interfacing with a stand-alone
transponder, other aircraft sensors (for example, Air Data Computer (ADC), Inertial Reference System (IRS), Global Positioning
System (GPS), etc.), antennas, controls, and displays.
1.4.1.1. The TSSA-4100 Traffic Surveillance System Application is necessary s oftware for the TSS-4100. The TSSA-4100 files
are field loadable.
1.4.2. E
The ECU is used to hold all of the aircraft and unit configuration d ata necessary for the TSS-4100 to operate properly. This simplifies
the wiring for the Traffic Surveillance System. For example, instead of program pins for the Mode S address, maximum aircraft
altitude, and bus speeds that must be wired and tested for every aircraft, a simple fi le is dataloaded through the TSS and stored in
the ECU.
1.4.3. T
The TDR-94D Du plex ATC/Mode S Transponder o perates on 28-V dc. The TDR-94D has the capability of operating with Mode S
interrogators. The Mode S capability permits sending and receiving messages via the interrogation/reply data link.
1.4.4. T
The TSA-4100 directional antenna is the top antenna for the TSS. It is also optionally used as the lower antenna for the TSS. It has
four passive antenna elements for directionality and is mounted on the outside of the aircraft fuselage.
1.4.5. T
The TRE-930 omnidirectional antenna is an optional lower antenna for the TSS.
1.4.6. A
Two ANT-42 omnidirectional antennas, one upper and one lower antenna, connect to the TDR-94D mode S transponder.
CU-3000 External Compensation Unit.
DR-94D ATC/Mode S Transponder.
SA-4100 Directional Antenna.
RE-930 Omnidirectional Antenna.
NT-42 Omnidirectional Antenna.
1.4.7. T
The TSM-4100, or Traffic Surveillance Mount, is a standard 4 Modular Concept Unit (MCU) mount with a fan that can be controlled
and monitored.
SM-4100 Traffic Surveillance Mount.
1-9/(1-10 Blank)
Loading...
+ 184 hidden pages
You need points to download manuals.
1 point = 1 manual.
You can buy points or you can get point for every manual you upload.