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  • FAA AC 20-152 : 2005

    Current The latest, up-to-date edition.

    RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  01-01-2005

    Publisher:  Federal Aviation Administration

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

    1 PURPOSE
    2 WHY USE RTCA/DO-254?
    3 WHO CAN USE RTCA/DO-254?
    4 FUTURE CHANGES OR REVISIONS
    5 RELATED DOCUMENTS

    Abstract - (Show below) - (Hide below)

    Applies to manufacturers and installers of products or appliances incorporating complex custom micro-coded components with hardware design assurance levels of A, B, and C. Provides a means to gain Federal Aviation Administration (FAA) approval by showing the equipment design is appropriate for its intended function.

    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 20-174 : 2011 DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
    FAA 8110.105 : 2017 SIMPLE AND COMPLEX ELECTRONIC HARDWARE APPROVAL GUIDANCE
    FAA AC 20-170 : 2013 INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153
    FAA AC 23.1311-1 : 2011 INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES
    SAE ARP 5794 : 2014 CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD
    FAA AC 20-169 : 2010 GUIDANCE FOR CERTIFICATION OF MILITARY AND SPECIAL MISSION MODIFICATIONS AND EQUIPMENT FOR COMMERCIAL DERIVATIVE AIRCRAFT (CDA)
    FAA AC 20-184 : 2015 GUIDANCE ON TESTING AND INSTALLATION OF RECHARGEABLE LITHIUM BATTERY AND BATTERY SYSTEMS ON AIRCRAFT
    FAA AC 20-173 : 2011 INSTALLATION OF ELECTRONIC FLIGHT BAG COMPONENTS
    FAA AC 25-11 : 2014 ELECTRONIC FLIGHT DISPLAYS
    SAE AS 6163 : 2015 TEMPERATURE CONTROLLED CONTAINER - PERFORMANCE REQUIREMENTS AND TEST PARAMETERS
    FAA AC 20-177 : 2012 DESIGN AND INSTALLATION GUIDANCE FOR AN AIRBORNE SYSTEM FOR NON-REQUIRED TELECOMMUNICATION SERVICE IN NON-AERONAUTICAL FREQUENCY BANDS
    FAA AC 00-66 : 2015 SELECTION OF CYCLIC REDUNDANCY CODE AND CHECKSUM ALGORITHMS TO ENSURE CRITICAL DATA INTEGRITY
    MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
    SAE ARP 1070E : 2019 DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY
    FAA AC 20-156 : 2006 AVIATION DATABUS ASSURANCE
    SAE ARP 1070 : 2014 DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY
    FAA AC 25.1329-1 : 2016 APPROVAL OF FLIGHT GUIDANCE SYSTEMS
    FAA AC 20-183 : 2014 LASER AIRWORTHINESS INSTALLATION GUIDANCE
    FAA AC 23.1309-1 : 2011 SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
    FAA AC 20-138 : 2014 AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION SYSTEMS
    FAA AC 20-150 : 2014 AIRWORTHINESS APPROVAL OF SATELLITE VOICE (SATVOICE) EQUIPMENT SUPPORTING AIR TRAFFIC SERVICE (ATS) COMMUNICATION
    SAE ARP 6461 : 2013 GUIDELINES FOR IMPLEMENTATION OF STRUCTURAL HEALTH MONITORING ON FIXED WING AIRCRAFT

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

    RTCA DO 254 : 2000 DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
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