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  • FAA AC 20-185 : 2015

    Current The latest, up-to-date edition.
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    AIRWORTHINESS APPROVAL OF SYNTHETIC VISION GUIDANCE SYSTEM

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  01-01-2015

    Publisher:  Federal Aviation Administration

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

    INTRODUCTION
    CHAPTER 2 - AIRWORTHINESS PACKAGE
    CHAPTER 3 - INTRODUCTION TO SYNTHETIC VISION GUIDANCE
                SYSTEM (SVGS)
    CHAPTER 4 - SVGS SYSTEM CRITERIA
    CHAPTER 5 - SVGS PERFORMANCE VERIFICATION
    APPENDIX A - SAMPLE AIRPLANE FLIGHT MANUAL (AFM)
                 SUPPLEMENT
    APPENDIX B - DEFINITIONS AND DOCUMENT ORDERING
    APPENDIX C - RELATED PUBLICATIONS
    APPENDIX D - ADVISORY CIRCULAR FEEDBACK FORM

    Abstract - (Show below) - (Hide below)

    Gives applicants with guidance for obtaining airworthiness approval for equipment installation of a Synthetic Vision Guidance System (SVGS) in aircraft.

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

    Document Type Standard
    Publisher Federal Aviation Administration
    Status Current

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

    FAA AC 27-1 : 2008 CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT
    RTCA DO 200B : 2015 STANDARDS FOR PROCESSING AERONAUTICAL DATA
    FAA AC 23.1311-1 : 2011 INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES
    RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
    RTCA DO-201A : 2000 STANDARDS FOR AERONAUTICAL INFORMATION
    FAA AC 25-11 : 2014 ELECTRONIC FLIGHT DISPLAYS
    FAA AC 25.1329-1 : 2016 APPROVAL OF FLIGHT GUIDANCE SYSTEMS
    FAA AC 20-167 : 2016 AIRWORTHINESS APPROVAL OF ENHANCED VISION SYSTEM, SYNTHETIC VISION SYSTEM, COMBINED VISION SYSTEM, AND ENHANCED FLIGHT VISION SYSTEM EQUIPMENT
    FAA AC 25-23 : 0 AIRWORTHINESS CRITERIA FOR THE INSTALLATION APPROVAL OF A TERRAIN AWARENESS AND WARNING SYSTEM (TAWS) FOR PART 25 AIRPLANES
    RTCA DO 254 : 2000 DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
    FAA AC 25-19 : 2011 CERTIFICATION MAINTENANCE REQUIREMENTS
    FAA AC 20-153 : 2016 ACCEPTANCE OF AERONAUTICAL DATA PROCESSES AND ASSOCIATED DATABASES
    FAA AC 25.1302-1 : 2013 INSTALLED SYSTEMS AND EQUIPMENT FOR USE BY THE FLIGHTCREW
    FAA AC 23-18 : 0 INSTALLATION OF TERRAIN AWARENESS AND WARNING SYSTEM (TAWS) APPROVED FOR PART 23 AIRPLANES
    FAA AC 25.1523-1 : 0 MINIMUM FLIGHTCREW
    FAA AC 23.1523 : 2005 MINIMUM FLIGHT CREW
    FAA AC 23.1309-1 : 2011 SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
    FAA AC 20-163 : 2009 DISPLAYING GEOMETRIC ALTITUDE RELATIVE TO MEAN SEA LEVEL
    SAE AS 8055A : 2015 MINIMUM PERFORMANCE STANDARD FOR AIRBORNE HEAD UP DISPLAY (HUD)
    FAA AC 120-29 : 0 CRITERIA FOR APPROVAL OF CATEGORY 1 AND CATEGORY 2 WEATHER MINIMA FOR APPROACH
    RTCA DO 276 : C2015 USER REQUIREMENTS FOR TERRAIN AND OBSTACLE DATA
    FAA AC 25.1309-1 : 0 SYSTEM DESIGN AND ANALYSIS
    FAA AC 20-138 : 2014 AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION SYSTEMS
    RTCA DO 359 : 2015 MINIMUM AVIATION SYSTEM PERFORMANCE STANDARD (MASPS) FOR SYNTHETIC VISION GUIDANCE SYSTEMS
    SAE AS 8034 : 2011 MINIMUM PERFORMANCE STANDARD FOR AIRBORNE MULTIPURPOSE ELECTRONIC DISPLAYS
    FAA AC 29-1 : 0 APPROVAL BASIS FOR AUTOMATIC STABILIZATION EQUIPMENT (ASE) INSTALLATIONS IN ROTORCRAFT
    FAA AC 25.1322-1 : 2010 FLIGHTCREW ALERTING
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