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  • ARINC 702A : 2014

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    ADVANCED FLIGHT MANAGEMENT COMPUTER SYSTEM

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  15-12-2014

    Publisher:  Aeronautical Radio Inc.

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    Table of Contents - (Show below) - (Hide below)

    1.0 INTRODUCTION AND DESCRIPTION
    1.1 Purpose and Scope
    1.2 Relationship to Other Documents
    1.3 Functional Overview
    1.4 Flight Management Computer Description
    1.5 Interchangeability
    1.6 Regulatory Approval
    1.7 Integrity and Availability
    1.8 Reliability
    1.9 Testability and Maintainability
    1.10 Flight Simulators
    2.0 INTERCHANGEABILITY STANDARDS
    2.1 Introduction
    2.2 Form Factor, Connectors, and Index Pin Coding
    2.3 Standard Interwiring
    2.4 Power Circuit
    2.5 Standardized Signaling
    2.6 Environmental Conditions
    2.7 Cooling
    2.8 Weights
    2.9 Grounding and Bonding
    3.0 SYSTEM DESIGN CONSIDERATIONS
    3.1 System Configurations
    3.3 System Response to Power Interrupts
    3.4 FMC Accuracy and Performance
    3.5 Dual System Design Considerations
    4.0 FLIGHT MANAGEMENT FUNCTION
    4.1 Introduction
    4.2 Functional Initialization and Activation
    4.3 Functional Description
    5.0 STANDARD INTERFACES
    5.1 FMC Digital Data Input Ports
    5.2 FMC Digital Data Outputs
    5.3 Discrete Inputs and Outputs
    5.4 FMC/FMC Intersystem Communications
    5.5 Ethernet Interface (ARINC 646)
    6.0 CONTROL DISPLAY UNIT INTERFACE
    6.1 General
    6.2 Standby Navigation
    6.3 Self Test
    6.4 MCDU Annunciators
    6.5 MCDU Alerting
    6.6 MCU Color and Font Usage
    7.0 ELECTRONIC FLIGHT INSTRUMENT
         SYSTEM INTERFACE
    7.1 Introduction
    7.2 FMC Outputs to EFI
    7.3 FMC Inputs From EFI
    7.4 EFI Design Features
    7.5 FMC Design Features
    7.6 Interface Design
    8.0 COMMUNICATIONS MANAGEMENT UNIT INTERFACE
    8.1 General
    9.0 DATA BASE STORAGE CONSIDERATIONS
    9.1 Introduction
    9.2 Navigation Data Base
    9.3 Airline Modifiable Information (AMI) Data Base
    9.4 Performance Data Base
    9.5 Magnetic Variation Data Base
    9.6 Terrain and Obstacle Data
    9.7 Airport Surface Map Data
    9.8 Configuration Data Base
    9.0 DATA BASE STORAGE CONSIDERATIONS
    9.1 Introduction
    9.2 Navigation Data Base
    9.3 Airline Modifiable Information (AMI) Data Base
    9.4 Performance Data Base
    9.5 Magnetic Variation Data Base
    9.6 Terrain and Obstacle Data
    9.7 Airport Surface Map Data
    9.8 Configuration Data Base
    10.0 BUILT-IN TEST AND MAINTENANCE PROVISIONS
    ATTACHMENTS
    ATTACHMENT 1 - FLIGHT MANAGEMENT SYSTEM
    ATTACHMENT 2-1 - FMC CONNECTOR POSITIONING
    ATTACHMENT 2-2 - STANDARD INTERWIRING
    ATTACHMENT 2-3 - NOTES APPLICABLE TO THE STANDARD
                     INTERWIRING
    ATTACHMENT 2-4 - CONNECTOR INSERT LAYOUT
    ATTACHMENT 3 - (SECTION INTENTIONALLY LEFT BLANK)
    ATTACHMENT 4 - DATA INPUT/OUTPUT - FMC OUTPUTS
    ATTACHMENT 5 - ENVIRONMENTAL TEST CATEGORIES
    ATTACHMENT 6 - FMC/EFI INTERFACE
    ATTACHMENT 7 - FMC/DATA LINK INTERFACE
    ATTACHMENT 8 - CODING EXAMPLES OF TRAJECTORY INTENT
                   DATA FILES
    APPENDICES
    APPENDIX A - REFERENCED DOCUMENTS
    APPENDIX B - ACRONYMS

    Abstract - (Show below) - (Hide below)

    Describes the characteristics of an advanced Flight Management Computer System (FMS) specifically designed for installation in new generation aircraft.

    General Product Information - (Show below) - (Hide below)

    Document Type Standard
    Publisher Aeronautical Radio Inc.
    Status Current
    Supersedes

    Standards Referencing This Book - (Show below) - (Hide below)

    RTCA DO 305 : A2012 FUTURE AIR NAVIGATION SYSTEM 1/A - AERONAUTICAL TELECOMMUNICATION NETWORK INTEROPERABILITY STANDARD (FANS 1/A - ATN B1 INTEROP STANDARD)
    ARINC 653 : 1997 SUPP 1 AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE
    ARINC 724B : 1987 SUPP 6 AIRCRAFT COMMUNICATIONS ADDRESSING AND REPORTING SYSTEM (ACARS)
    RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
    ARINC 743B : 2009 GLOBAL NAVIGATION SATELLITE SYSTEM (GNSS) LANDING SYSTEM SENSOR UNIT (GLSSU)
    RTCA DO 212 : 1992 MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR AIRBORNE AUTOMATIC DEPENDENT SURVEILLANCE (ADS) EQUIPMENT
    ARINC 661 : 2002 SUPP 6 COCKPIT DISPLAY SYSTEM INTERFACES TO USER SYSTEMS
    ARINC 610B : 2001 GUIDANCE FOR USE OF AVIONICS EQUIPMENT AND SOFTWARE IN SIMULATORS
    ARINC 739A : 1996 SUPP 1 MULTI-PURPOSE CONTROL AND DISPLAY UNIT
    ARINC 701 : 1979 SUPP 1 FLIGHT CONTROL COMPUTER SYSTEM
    ARINC 737 : 1984 SUPP 1 ON-BOARD WEIGHT & BALANCE SYSTEM
    RTCA DO 340 : 2012 CONCEPT OF USE FOR AERONAUTICAL INFORMATION SERVICES (AIS) AND METEOROLOGICAL (MET) DATA LINK SERVICES
    RTCA DO 258 : A2005 INTEROPERABILITY REQUIREMENTS FOR ATS APPLICATIONS USING ARINC 622 DATA COMMUNICATIONS
    RTCA DO 324 : 2010 SAFETY AND PERFORMANCE REQUIREMENTS (SPR) FOR AERONAUTICAL INFORMATION SERVICES (AIS) AND METEOROLOGICAL (MET) DATA LINK SERVICES
    ARINC 705 : 1979 SUPP 5 ATTITUDE AND HEADING REFERENCE SYSTEM
    RTCA DO 283 : B2015 MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR REQUIRED NAVIGATION PERFORMANCE FOR AREA NAVIGATION
    RTCA DO 306 : 2007 CHG NOT 1 11 SAFETY AND PERFORMANCE STANDARD FOR AIR TRAFFIC DATA LINK SERVICES IN OCEANIC AND REMOTE AIRSPACE (OCEANIC SPR STANDARD)
    ARINC 660B : 2014 CNS/ATM AVIONICS ARCHITECTURES SUPPORTING NEXTGEN/SESAR CONCEPTS
    ARINC 743A : 1992 SUPP 5 GNSS SENSOR
    ARINC 706 : 1979 SUPP 4 MARK 5 SUBSONIC AIR DATA SYSTEM
    RTCA DO 308 : 2007 OPERATIONAL SERVICES AND ENVIRONMENT DEFINITION (OSED) FOR AERONAUTICAL INFORMATION SERVICES (AIS) AND METEOROLOGICAL (MET) DATA LINK SERVICES
    ARINC 725 : 1979 SUPP 2 ELECTRONIC FLIGHT INSTRUMENTS (EFI)
    ARINC 758 : 1996 SUPP 3 COMMUNICATIONS MANAGEMENT UNIT (CMU) MARK 2
    ARINC 429 : 2001 ELECTRONIC DISKETTE COPY OF DATA LABELS IN MICROSOFT WORD AND EXCEL FORMATS
    ARINC 646 : 1995 ETHERNET LOCAL AREA NETWORK (ELAN)
    RTCA DO 328 : A2015 SAFETY, PERFORMANCE AND INTEROPERABILITY REQUIREMENTS DOCUMENTS FOR AIRBORNE SPACING-FLIGHT DECK INTERVAL MANAGEMENT (ASPA-FIM)
    ARINC 744A : 1993 SUPP 1 FULL-FORMAT PRINTER WITH GRAPHICS CAPABILITY
    ARINC 744 : 1990 FULL-FORMAT PRINTER
    RTCA DO 236 : C2013 CHG 1 2014 MINIMUM AVIATION SYSTEM PERFORMANCE STANDARDS: REQUIRED NAVIGATION PERFORMANCE FOR AREA NAVIGATION
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