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
appendix D 523-0809018
Table D-5. ECU-3000 Environmental Qualification Form.
CONDITIONS
DO-160E SECTION
AND REV
EQUIPMENT QUALIFICATIONS
CATEGORIES OF CONDUCTED TESTS
Temperature and Altitude
4.0
(F2)(A2)V
- Temperature
- Low Operating Temperature F2 –55 °C (–67 °F)
- High Operating Temperature F2 +70 °C (+158 °F)
- Low Storage Temperature F2 –55 °C (–67 °F)
- High Storage T
emperature
F2 +85 °C (+185 °
F)
- High (Short Time) Operating Temperature F2 + 70 °C (+158 °F)
- Altitude F2 16 800 m (55 000 ft)
- In-Flight Loss of Cooling
V
- Decompression
A2
- Over pressure A2
Temperature Variation 5.0 A
Humidity 6.0
B
Shock 7.0
B
- Operational Tested at 6 g pea
k
- Crash Safety Tested at 20 g peak
Vibration
8.0
Equipment Tested to Cat R curves BB1, Cat S
curves CLM and Cat H curve R
Explosion Proofness 9.0
E
Waterproofnes
s10.0
Y
Fluids Susceptibility
11.0
X
Sand and Dust
12.0
X
Fungus Resistance
13.0
X
Salt Spray
14.0
X
Magnetic Effect
15.0
Z
Power Input
16.0 AB
Voltage Spike 17.0 A
Audio Frequency Conducted Susceptibility 18.0
Z
Induced Signa
l Susceptibility 19.0 CC
Radio Frequency Susceptibility
20.0
RR
Emission of Radio Frequency Energy
21.0
M
Lightning Induced Transient Susceptibility
22.0
X
Lightning Direct Effects
23.0
X
Icing
24.0 A
Electrostatic Discharge
25.0 A
D-4