User Manual
Table Of Contents
- TSS-4100 Integrated TCAS, Transponder, and ADS-B Traffic Surveillance System
- TITLE PAGE
- LIST OF EFFECTIVE PAGES
- TABLE OF CONTENTS
- LIST OF ILLUSTRATIONS
- LIST OF TABLES
- INTRODUCTION
- SAFETY SUMMARY
- 1 General Information
- 2 System Components
- 2.1 INTRODUCTION.
- 2.2 COMPONENT DESCRIPTIONS.
- 2.3 ANT-42 34-54-00.
- 2.4 L-BAND ANTENNA, ANT-42, DATA.
- 2.5 ECU-3000 34-54-00.
- 2.6 EXTERNAL CONTROL UNIT , ECU-3000, DATA.
- 2.7 TDR-94D 34-54-00.
- 2.8 MODE S TRANSPONDER, TDR-94D, DATA.
- 2.9 TRE-930 34-54-00.
- 2.10 ANTENNA, TRE-930, DATA.
- 2.11 TSA-4100 34-54-00.
- 2.12 ANTENNA, TSA-4100, DATA.
- 2.13 TSS-4100 34-43-00.
- 2.14 TRAFFIC SURVEILLANCE SYSTEM, TSS-4100, DATA.
- 3 Operation
- 4 Maintenance
- 4.1 INTRODUCTION.
- 4.2 MAINTENANCE SCHEDULE.
- 4.3 CONVERSION FROM TTR/TDR TO TSS SYSTEM.
- 4.4 DATA LOADING.
- 4.5 TSS-4100 MODE S ADDRESS PROGRAMMING TOOL.
- 4.6 LED INDICATORS.
- 4.7 TEST EQUIPMENT AND POWER REQUIREMENTS.
- 4.8 TESTING AND TROUBLESHOOTING.
- 4.8.1 Pre-installation Testing.
- 4.8.2 TCAS Self Test.
- 4.8.3 Equipment Setup.
- 4.8.4 Radio Altitude System Failure Tests.
- 4.8.5 Pressure Altitude System Failure Tests.
- 4.8.6 Range and Bearing Test.
- 4.8.7 TCAS RA Test.
- 4.8.8 Transponder Tests.
- 4.8.9 ADS-B Transmit Ground Test.
- 4.8.10 Transponder/TCAS Suppression Bus Issues.
- 4.9 INITIAL INSTALLATION CHECK OUT PROCEDURE.
- 4.10 RETURN TO SERVICE TEST PROCEDURE.
- 4.11 INSPECTION/CHECK.
- APPENDIX A Faults and Warnings
- APPENDIX B Maintenance Words
- APPENDIX C Buses and Other Interfaces
- APPENDIX D Equipment Characteristics
- APPENDIX E Interconnect Diagram
- BACK COVER
maintenance 523-0 809018
Display Range (approx) Display Aural
12 nmi Other Traffic Symbol None
9 nmi TA Symbol TRAFFIC, TRAFFIC
6 nmi RA Symbol CLIMB, CLIMB
4.9.2.5.3. Scenario 2a: Climb RA just below maximum climb altitude. Scenario 2a and 2b are tests intended to ensure that
the max imum cl imb altitude is p r operly programmed and read by TCAS.
a. Set airplane u nder test (UUT) simulated altitude to 50 ft below (+/- 10 ft) the maximum clim b altitude (NOTE 2). Set the radio
altimeter to the maximum s etting.
b. Set the following values as necessary:
• TCAS Type: TCAS II
• Intruder Type: Mode S
• Range at Start: 15.00 n mi
• Range Rate: +720 kts
• Altitude at Start: Set to 50 ft below the UUT altitude (or e qual to 100 ft below the maximum climb altitude)
• Altitude Rate: 0.
c. Start the scenario.
d. Monitor the TCAS display and audio system for correct presentation as follows (NOTE 1):
Display Range (approx) Display Aural
If the maximum climb altitude is set between 10,000 and 20,000 ft:
12 nmi Other Traffic Symbol None
9 nmi TA Symbol TRAFFIC, TRAFFIC
6 nmi RA Symbol CLIMB, CLIMB
If the maximum climb altitude is set to 20,000 ft or more:
12 nmi Other Traffic Symbol None
9.6 nmi TA Symbol TRAFFIC, TRAFFIC
7 nmi RA Symbol CLIMB, CLIMB
4.9.2.5.4. Scenario 2b: Descend RA just above the maximum climb altitude. Scenario 2a and 2b are tests intended to
ensure that the maximum climb altitude is properly programmed an d read by TCAS.
a. Set airplane under test (UUT) simulated altitude to 50 ft above (+/- 10 ft) the maximum climb altitude (N OTE 2). Set the radio
altimeter to the maximum s etting.
b. Set the following values as necessary:
• TCAS Type: TCAS II
• Intruder Type: Mode S
• Range at Start: 15.00 n mi
• Range Rate: +720 kts
• Altitude at Start: Set to 50 ft below the UUT altitude (or equal to the maximum climb altitud e )
• Altitude Rate: 0.
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