Minimum Aviation System Performance Standards for Aircraft ...

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Copies of this document may be obtained from RTCA, Inc. 1150 18 th Street, NW, Suite 910 Washington, DC 20036, USA Telephone: 202-833-9339 Facsimile: 202-833-9434 Internet: www.rtca.org Please call RTCA for price and ordering information
FOREWORD This document was prepared by RTCA Special Committee 186 (SC-186), and was approved for publication by the RTCA Program Management Committee (PMC) on Month Day, 20xx. RTCA, Incorporated is a not-for-profit corporation formed to advance the art and science of aviation and aviation electronic systems for the benefit of the public. The organization functions as a Federal Advisory Committee and develops consensus based recommendations on contemporary aviation issues. RTCA’s objectives include but are not limited to: � Coalescing aviation system user and provider technical requirements in a manner that helps government and industry meet their mutual objectives and responsibilities; � Analyzing and recommending solutions to the system technical issues that aviation faces as it continues to pursue increased safety, system capacity and efficiency; � Developing consensus on the application of pertinent technology to fulfill user and provider requirements, including development of minimum operational performance standards for electronic systems and equipment that support aviation; and � Assisting in developing the appropriate technical material upon which positions for the International Civil Aviation Organization and the International Telecommunications Union and other appropriate international organizations can be based. The organization’s recommendations are often used as the basis for government and private sector decisions as well as the foundation for many Federal Aviation Administration Technical Standard Orders. Since RTCA is not an official agency of the United States Government, its recommendations may not be regarded as statements of official government policy unless so enunciated by the U.S. government organization or agency having statutory jurisdiction over any matters to which the recommendations relate.
Page 1: 1150 18 th Street, NW, Suite 910 Wa
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 and 30: Airborne Situational Awareness (AIR
Page 31 and 32: Notes for Table 2-7: 1. The airborn
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
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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:
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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
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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
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
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3.2.4.2 Altitude means to indicate
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3.2.7 Heading 4. Pure barometric ra
Page 101 and 102:
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
Page 109 and 110:
Table 3.2.12a: Navigation Accuracy
Page 111 and 112:
3.2.16 Geometric Vertical Accuracy
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101 of the airplane during certain
Page 115 and 116:
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
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 and 140:
Table 3.4.3.1b: Interoperability Ra
Page 141 and 142:
Equipage Class � B0 Aircraft R�
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Table 3.4.3.3.1.1a shows accuracy v
Page 145 and 146:
2. The analysis in RTCA DO-242A, Ap
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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
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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
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
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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
Page 187 and 188:
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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
Page 227 and 228:
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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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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