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  • FAA AC 20-156 : 2006

    Current The latest, up-to-date edition.

    AVIATION DATABUS ASSURANCE

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  01-01-2006

    Publisher:  Federal Aviation Administration

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

    1. PURPOSE
    2. MOTIVATION FOR GUIDANCE
    3. SAFETY REQUIREMENTS
    4. DATA INTEGRITY REQUIREMENTS
    5. DATABUS PERFORMANCE REQUIREMENTS
    6. SOFTWARE AND HARDWARE ASSURANCE REQUIREMENTS
    7. ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS
    8. VERIFICATION AND VALIDATION REQUIREMENTS
    9. CONFIGURATION MANAGEMENT REQUIREMENTS
    10. SECURITY ASSURANCE REQUIREMENTS
    11. PROCEDURES FOR MEETING REQUIREMENTS
    12. RELATED DOCUMENTS AND HOW TO GET THEM

    Abstract - (Show below) - (Hide below)

    Provides means to gain Federal Aviation Administration (FAA) approval of your aviation databus by showing the databus design performs its intended function and satisfies the applicable airworthiness requirements when installed on an aircraft or aircraft engine.

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

    Document Type Standard
    Publisher Federal Aviation Administration
    Status Current

    Standards Referenced By This Book - (Show below) - (Hide below)

    FAA AC 20-170 : 2013 INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153
    MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
    FAA AC 00-66 : 2015 SELECTION OF CYCLIC REDUNDANCY CODE AND CHECKSUM ALGORITHMS TO ENSURE CRITICAL DATA INTEGRITY
    ARINC 825 : 2015 GENERAL STANDARDIZATION OF CAN (CONTROLLER AREA NETWORK) BUS PROTOCOL FOR AIRBORNE USE
    SAE ARP 6461 : 2013 GUIDELINES FOR IMPLEMENTATION OF STRUCTURAL HEALTH MONITORING ON FIXED WING AIRCRAFT

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

    FAA AC 27-1 : 2008 CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT
    FAA AC 21-16 : 2011 RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT"
    RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
    FAA AC 20-136 : 2011 AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
    FAA AC 33.28-2 : 2003 GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, RECIPROCATING ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS
    SAE ARP 4754 : 2010 GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
    RTCA DO 254 : 2000 DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
    FAA AC 20-152 : 2005 RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
    SAE ARP 4761 : 1996 GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT
    FAA AC 23.1309-1 : 2011 SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
    FAA AC 29-2 : 2008 CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT
    FAA AC 25.1309-1 : 0 SYSTEM DESIGN AND ANALYSIS
    FAA AC 20-115 : 2017 AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
    FAA AC 33.75-1 : 2007 GUIDANCE MATERIAL FOR 14 CFR SECTION 33.75, SAFETY ANALYSIS
    FAA AC 33.28-1 : 0 COMPLIANCE CRITERIA FOR 14 CFR SECTION 33.28, AIRCRAFT ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS
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