Minimum Aviation System Performance Standards for Aircraft ...

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Equipage Class � A0 Minimum R�10 NM A1 Basic R�20 NM A2 Enhanced R�40 NM A3 Extended R�90 NM Notes: Table 3.4.3.2a: Interactive Aircraft/Vehicle Equipage Type Operational Capabilities Domain � Terminal, En Route, Oceanic Approach Airport Surface Data Required to Support Operational Capability Transmit Receive SV MS SV MS SV MS TS SV MS TS SV MS SV MS SV MS TS SV MS TS R �10 NM e.g., Enhanced Visual Acquisition Support Perform Support R �20 NM Perform 1. SV= State Vector Report; MS = Mode Status Report; TS = Target State Report. R �40 NM Support Perform Support R �90 NM Perform R �10 NM e.g., Enhanced Visual Approach Support Perform R �5 NM e.g., Airport Surface Situation Awareness Yes Yes Yes No No No No No No No Yes Yes Yes Yes Yes Yes No No No No Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes No No Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes 2. A transmitting ADS-B participant supports an application by broadcasting the required data that receiving ADS-B participants need for that application. 3. A receiving ADS-B participant performs an application by processing received messages from transmitting ADS-B participants that support that application. 4. Operation in airspace with high closure rates may require longer range. 5. Class A2 and A3 users may equip for low visibility taxi following. 6. Class A1 equipment may optionally support TS reports. 7. MS reports contain time-critical report elements that, when their values change, need to be updated at higher rates than that of the MS reports. See §3.5.4.1, §3.5.8.5, and §3.5.8.6 for details.) © 20xx, RTCA, Inc. Support Perform
Equipage Class � B0 Aircraft R�10 NM B1 Aircraft R�20 NM B2 Ground Vehicle B3 Fixed Obstacle C1 ATS En route & Terminal C2 Approach & Surface C3 Flight Following Notes: Table 3.4.3.2b: Broadcast and Receive Only Equipage Type Operational Capabilities Domain � Terminal, En Route, and Oceanic / Remote Non-Radar Approach Data Required to Support Operational Capability Transmit Receive SV MS SV MS SV MS SV MS No No No R � 10 NM e.g., Enhanced Visual Acquisition Support Perform R � 20 NM Support Perform R � 40 NM Support Perform R � 90 NM Support Perform R � 10 NM e.g., Enhanced Visual Approach Support Perform Airport Surface R � 5 NM e.g., Airport Surface Situation Awareness SupPerportform No Yes No Yes No No No No No No No Yes No No Yes No Yes No No No No No No No Yes No No Yes No Yes No No No No No No No Yes No No Yes No Yes No No No No No No No Yes No SV MS TS SV MS TS SV MS No Yes No Yes No Yes No Yes No No No No No Yes No Yes No No No No No Yes No Yes No Yes No No No No No No No No No No 1. SV= State Vector; MS = Mode Status; TS = Target State Report 2. A transmitting ADS-B participant supports an application by broadcasting the required data that receiving ADS-B participants need for that application. 3. A receiving ADS-B participant performs an application by processing received messages from transmitting ADS-B participants that support that application. � 20xx, RTCA, Inc.
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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
Page 89 and 90: UAT transmissions shall be randomiz
Page 91 and 92: aircraft/vehicle addresses shall {2
Page 93 and 94: 3.2.2.4 Mode 3/A Code Since the Mod
Page 95 and 96: Table 3.2.4.1a: Dimensions of Defin
Page 97 and 98: 3.2.4.2 Altitude means to indicate
Page 99 and 100: 3.2.7 Heading 4. Pure barometric ra
Page 101 and 102: 3.2.8.6 UAT Receive Capability The
Page 103 and 104: SDA Value (decimal) (binary) 0 00 T
Page 105 and 106: Table 3.2.9.6B: Longitudinal Axis G
Page 107 and 108: It is recommended that the coded re
Page 109 and 110: Table 3.2.12a: Navigation Accuracy
Page 111 and 112: 3.2.16 Geometric Vertical Accuracy
Page 113 and 114: 101 of the airplane during certain
Page 115 and 116: 3.2.24 Selected Heading Field a. Th
Page 117 and 118: 105 a. The ADS-B Transmitting Subsy
Page 119 and 120: Figure 3-15: End to End ASA System
Page 121 and 122: 3.3.1.2.2 Interface A2 3.3.1.2.3 In
Page 123 and 124: 111 The CDTI function may translate
Page 125 and 126: 113 The update interval of ADS-R or
Page 127 and 128: data extrapolated to a common time
Page 129 and 130: Source Info Category Information El
Page 131 and 132: If the ASSAP determines that multip
Page 133 and 134: 121 The operating range of display
Page 135 and 136: 3.4.2.9 Multi-Function Display (MFD
Page 137 and 138: 3.4.3 Subsystem Requirements for AD
Page 139: Table 3.4.3.1b: Interoperability Ra
Page 143 and 144: Table 3.4.3.3.1.1a shows accuracy v
Page 145 and 146: 2. The analysis in RTCA DO-242A, Ap
Page 147 and 148: 2. The 90 NM range requirement appl
Page 149 and 150: Table 3.4.3.3.1.3a: Summary of TS R
Page 151 and 152: Instaneous air count 800 700 600 50
Page 153 and 154: Growth Factor GNY( ma �� ) ( 1
Page 155 and 156: Where the ADS-B System is used as a
Page 157 and 158: eliability required for the intende
Page 159 and 160: its component information is receiv
Page 161 and 162: c. Lighter Than Air d. Unmanned Aer
Page 163 and 164: . ADS-B participants that are known
Page 165 and 166: 3.5.1.3.6 Geometric Altitude Field
Page 167 and 168: 3. For operations at some airports,
Page 169 and 170: MS Elem. # Table 3.5.1.4: Mode Stat
Page 171 and 172: 3.5.1.4.5 Emitter Category Field An
Page 173 and 174: 3.5.1.4.11 Navigation Accuracy Cate
Page 175 and 176: 3.5.1.6 Air Referenced Velocity (AR
Page 177 and 178: 3.5.1.6.7 Heading Valid Field The
Page 179 and 180: 3.5.1.7.9 MCP/FCU Mode Indicator: V
Page 181 and 182: alternate position sources may not
Page 183 and 184: 3.6.4 TCAS The heading data will in
Page 185 and 186: 3.6.5.3 Reference Datum The airport
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Page 189 and 190: application-unique processing and d
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Figure 4-2: Example for SURF IA Ind
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Appendix A Page A-2 ©20xx, RTCA, I
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Appendix A Page A-8 A.2 Definitions
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Appendix A Page A-10 Air/Ground Sta
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Appendix A Page A-12 Collision Avoi
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Appendix A Page A-14 Extended Displ
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Appendix A Page A-16 Latency Compen
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Appendix A Page A-18 Regime - Divis
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Appendix A Page A-20 Target State R
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Appendix A Page A-22 DO-3xx Reqmts
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Appendix A Page A-24 DO-3xx Reqmts
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Appendix B Page B-2 [15] RTCA, Traf
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Appendix B Page B-4 [44] RTCA, Safe
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C Derivation of Link Quality Requir
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C.3.4 Altitude Accuracy The fundame
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Appendix F Page F-2 F.1.2 ADS-B Tra
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Appendix F Page F-4 F.2.2 Design Al
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Appendix F Page F-6 F.3.2 Performan
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Appendix F Page F-8 © 20xx RTCA, I
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Appendix F Page F-10 © 20xx RTCA,
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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,
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