Minimum Aviation System Performance Standards for Aircraft ...

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18 Table 2-7: ADS-B Transmit Sources – Minimum Required Performance vs ADS-B In Application Requirements 1 SA Applications 2 "Enhanced SA" Applications 3 Spacing Applications 4 Delegated Separation Applications 5 Self Separation Airborne Approach Surface Oceanic Approach Surface EnRoute / Terminal EnRoute / Terminal EnRoute / Terminal AIRB VSA SURF ITP CAVS SURF IA FIM-S FIM-DS ICSPA DS-C/P DSWRM FC Self Sep TRANSMIT SOURCES DO-319 DO-314 DO-322 DO-312 CEDS DO-323 DO-328 A. Airborne Platforms Accuracy (NACP) 8 5 6 7 / 9 (5) 5 9 / 10 / 11 6 / 7 9 Integrity (NIC) 7 N / A 6 N / A 5 N / A 5 / 7 9 Vel Acc (NACV) 1 1 1 2 1 1 1 3 Src Integ Lvl (SIL) 3 N / A 1 N / A 2 2 2 2 Sys Design Assur (SDA) 2 1 1 1 / 2 (3) 2 2 2 TBD DO-289 Apndx J Flight ID Yes N / A Required N / A Required N / A Required Required B. Ground Segment: ADS-R Accuracy (NACP) 9 max 5 6 7 / 9 (5) N / A 9 / 10 / 11 6 / 7 9 Integrity (NIC) 8 max N / A 6 N / A N / A N / A 5 / 7 9 Vel Acc (NACV) 1 1 1 2 N / A 1 1 3 Src Integ Lvl (SIL) 3 N / A 1 N / A N / A 2 2 2 Sys Design Assur (SDA) 2 1 1 1 / 2 (3) N / A 2 2 TBD Flight ID Yes N / A Required N / A N / A N / A Required Required C. Ground Segment: TIS-B TIS-B as currently implemented was not intended to support these applications. Accuracy (NACP) 5 / 6 / 9 (2) 5 6 7 / 9 (5) N / A 9 / 10 / 11 6 / 7 9 Integrity (NIC) 0 N / A 6 N / A N / A N / A 5 / 7 9 Vel Acc (NACV) 0 1 1 2 N / A 1 1 3 Src Integ Lvl (SIL) 0 N / A 1 N / A N / A 2 2 2 Sys Design Assur (SDA) 2 (4) 1 1 1 / 2 (3) N / A 2 2 TBD Flight ID No N / A Required N / A N / A N / A Required Required Legend: Green = Source meets application’s requirements Red = Source does not meet application’s requirements Yellow = Source does not meet application’s requirements but one or more mitigation methods are available. © 20xx, RTCA, Inc.
Notes for Table 2-7: 1. The airborne source’s performance levels (in Group A) are from the FAA Final ADS-B Out Rule and Advisory Circular AC 20-165 (Refs TBD). The ADS-R (in Group B) and TIS-B (in Group C) performance levels are from the latest version of the SBS Air ICD SRT Revision 01 (Ref TBD). 2. TIS-B NACP values for the En Route & Terminal Environments are ≥5. TIS-B NACP values are for airborne (6) & surface (9) targets in the Surface Environment. 3. FAA TSO-C195 states applications' Hazard Level for ownship when airborne or on surface > 80 knots = Major (SDA=2), Hazard Level for ownship < 80 knots = Minor (SDA=1). 4. TIS-B Service does not broadcast a SDA value but the SBS Air ICD defines TIS-B service SDA equivalent to 2. 5. SURF surface targets require NACP ≥ 9, SURF airborne targets require NACP = 7 or 9 depending on parallel runway spacing. © 20xx, RTCA, Inc. 19
Page 1 and 2: 1150 18 th Street, NW, Suite 910 Wa
Page 3 and 4: FOREWORD This document was prepared
Page 5 and 6: TABLE OF CONTENTS 1 PURPOSE AND SCO
Page 7 and 8: 3.2.25 Status of MCP/FCU Mode Bits
Page 9 and 10: APPENDICES Appendix A Acronyms and
Page 11 and 12: Table 3.4.3.1b: Interoperability Ra
Page 13 and 14: 1 PURPOSE AND SCOPE 1.1 Introductio
Page 15 and 16: � Enabling aircraft in oceanic ai
Page 17 and 18: is minimizing the latency between t
Page 19 and 20: uses of TCAS and ASA, and in partic
Page 21 and 22: provision is still the controller's
Page 23 and 24: The ADS-B system scope is the middl
Page 25 and 26: 2 Operational Requirements 2.1 Gene
Page 27 and 28: The following subsections describe
Page 29: Airborne Situational Awareness (AIR
Page 33 and 34: Notes for Table 2-8: 1. System must
Page 35 and 36: this new distance-based longitudina
Page 37 and 38: � Mechanisms for aircraft-aircraf
Page 39 and 40: the lead and other proximate aircra
Page 41 and 42: environment there is a need to supp
Page 43 and 44: Operational Scenarios Blind Taxi: T
Page 45 and 46: Table 2-9(b): Additional Expected C
Page 47 and 48: Scenario � NRA - 5 NM EnRoute Tab
Page 49 and 50: Aircraft type classification, statu
Page 51 and 52: 3 ADS-B and Airborne Systems Defini
Page 53 and 54: Participant - N Participant - 2 Par
Page 55 and 56: ADS-B Message Generation Function A
Page 57 and 58: certification process. The distribu
Page 59 and 60: own-aircraft’s air crew). This eq
Page 61 and 62: Class C2: Ground ATS Receive-Only A
Page 63 and 64: 3.1.3 CDTI Subsystem Description Th
Page 65 and 66: . Approach Control Service 2. Fligh
Page 67 and 68: 3.1.4.2.1 ADS-R Service Figure 3-8:
Page 69 and 70: USER AIR INTERFACE ADS-B MESSAGES R
Page 71 and 72: 3.1.4.2.1.4 ADS-R in Enroute and Te
Page 73 and 74: TIS‐B Non‐Equipped UAT FIS‐B
Page 75 and 76: available for a Mode S track (typic
Page 77 and 78: Three squitters (even position, odd
Page 79 and 80: TIS-B Message Encoding Used Based o
Page 81 and 82:
The TIS-B/ADS-R Service Status mess
Page 83 and 84:
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
Page 139 and 140:
Table 3.4.3.1b: Interoperability Ra
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Equipage Class � B0 Aircraft R�
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Table 3.4.3.3.1.1a shows accuracy v
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2. The analysis in RTCA DO-242A, Ap
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2. The 90 NM range requirement appl
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Table 3.4.3.3.1.3a: Summary of TS R
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Instaneous air count 800 700 600 50
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Growth Factor GNY( ma �� ) ( 1
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Where the ADS-B System is used as a
Page 157 and 158:
eliability required for the intende
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its component information is receiv
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c. Lighter Than Air d. Unmanned Aer
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. ADS-B participants that are known
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3.5.1.3.6 Geometric Altitude Field
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3. For operations at some airports,
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MS Elem. # Table 3.5.1.4: Mode Stat
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3.5.1.4.5 Emitter Category Field An
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3.5.1.4.11 Navigation Accuracy Cate
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3.5.1.6 Air Referenced Velocity (AR
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3.5.1.6.7 Heading Valid Field The
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3.5.1.7.9 MCP/FCU Mode Indicator: V
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alternate position sources may not
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3.6.4 TCAS The heading data will in
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3.6.5.3 Reference Datum The airport
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This Page Intentionally Left Blank.
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application-unique processing and d
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Figure 4-2: Example for SURF IA Ind
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This Page Intentionally Left Blank.
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This page intentionally left blank.
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Appendix A Page A-2 ©20xx, RTCA, I
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Page 201 and 202:
Page 203 and 204:
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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Page 223 and 224:
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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The Page Intentionally Left Blank.
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Page 235 and 236:
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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Page 251 and 252:
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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