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1150 18 th Street, NW, Suite 910 Wa
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FOREWORD This document was prepared
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TABLE OF CONTENTS 1 PURPOSE AND SCO
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3.2.25 Status of MCP/FCU Mode Bits
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APPENDICES Appendix A Acronyms and
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Table 3.4.3.1b: Interoperability Ra
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1 PURPOSE AND SCOPE 1.1 Introductio
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� Enabling aircraft in oceanic ai
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is minimizing the latency between t
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uses of TCAS and ASA, and in partic
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provision is still the controller's
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The ADS-B system scope is the middl
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2 Operational Requirements 2.1 Gene
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The following subsections describe
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Airborne Situational Awareness (AIR
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Notes for Table 2-7: 1. The airborn
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Notes for Table 2-8: 1. System must
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this new distance-based longitudina
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� Mechanisms for aircraft-aircraf
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the lead and other proximate aircra
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environment there is a need to supp
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Operational Scenarios Blind Taxi: T
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Table 2-9(b): Additional Expected C
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Scenario � NRA - 5 NM EnRoute Tab
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Aircraft type classification, statu
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3 ADS-B and Airborne Systems Defini
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Participant - N Participant - 2 Par
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ADS-B Message Generation Function A
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certification process. The distribu
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own-aircraft’s air crew). This eq
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Class C2: Ground ATS Receive-Only A
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3.1.3 CDTI Subsystem Description Th
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. Approach Control Service 2. Fligh
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3.1.4.2.1 ADS-R Service Figure 3-8:
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USER AIR INTERFACE ADS-B MESSAGES R
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3.1.4.2.1.4 ADS-R in Enroute and Te
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TIS‐B Non‐Equipped UAT FIS‐B
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available for a Mode S track (typic
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Three squitters (even position, odd
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TIS-B Message Encoding Used Based o
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The TIS-B/ADS-R Service Status mess
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3.1.4.3.1.2.2 TIS-B Position Update
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UAT transmissions shall be randomiz
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The nominal message transmission ra
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UAT transmissions shall be randomiz
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aircraft/vehicle addresses shall {2
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3.2.2.4 Mode 3/A Code Since the Mod
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Table 3.2.4.1a: Dimensions of Defin
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3.2.4.2 Altitude means to indicate
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3.2.7 Heading 4. Pure barometric ra
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3.2.8.6 UAT Receive Capability The
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SDA Value (decimal) (binary) 0 00 T
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Table 3.2.9.6B: Longitudinal Axis G
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It is recommended that the coded re
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Table 3.2.12a: Navigation Accuracy
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3.2.16 Geometric Vertical Accuracy
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101 of the airplane during certain
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3.2.24 Selected Heading Field a. Th
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105 a. The ADS-B Transmitting Subsy
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Figure 3-15: End to End ASA System
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3.3.1.2.2 Interface A2 3.3.1.2.3 In
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111 The CDTI function may translate
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113 The update interval of ADS-R or
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data extrapolated to a common time
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Source Info Category Information El
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If the ASSAP determines that multip
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121 The operating range of display
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3.4.2.9 Multi-Function Display (MFD
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3.4.3 Subsystem Requirements for AD
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Table 3.4.3.1b: Interoperability Ra
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Equipage Class � B0 Aircraft R�
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- Page 149 and 150: Table 3.4.3.3.1.3a: Summary of TS R
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- Page 163 and 164: . ADS-B participants that are known
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- Page 175 and 176: 3.5.1.6 Air Referenced Velocity (AR
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- Page 181 and 182: alternate position sources may not
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- Page 189 and 190: application-unique processing and d
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- Page 227 and 228: C Derivation of Link Quality Requir
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Appendix F Page F-12 1 0.9 0.8 0.7
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Appendix F Page F-14 © 20xx RTCA,
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Appendix G Page G-2 North Position
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Appendix G Page G-4 ARV information
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Appendix G Page G-6 � 20xx, RTCA,