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  • FAA 8110.49 : 2011

    Current The latest, up-to-date edition.

    SOFTWARE APPROVAL GUIDELINES

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  01-01-2011

    Publisher:  Federal Aviation Administration

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

    Chapter 1 - General Information
    Chapter 2 - Software Review Process
    Chapter 3 - [Reserved]
    Chapter 4 - Software Conformity Inspection
    Appendix A - Level of Involvement Worksheets
    Appendix B - Directive Feedback Information

    Abstract - (Show below) - (Hide below)

    Specifies Aircraft Certification Service (AIR) offices and designees on how to apply RTCA/DO-178B and RTCA/DO-178C, herein called RTCA/DO-178B/C for approving software used in airborne computers.

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

    Development Note Supersedes FAA N 8110.85, FAA N 8110.86, FAA N 8110.87, FAA N 8110.88, FAA N 8110.89, FAA N 8110.90, FAA N 8110.91, FAA N 8110.92, FAA N 8110.93, FAA N 8110.94, FAA N 8110.95 (12/2003) Supersedes FAA N 8110.110. (11/2011)
    Document Type Standard
    Publisher Federal Aviation Administration
    Status Current
    Supersedes

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

    FAA 8110.105 : 2017 SIMPLE AND COMPLEX ELECTRONIC HARDWARE APPROVAL GUIDANCE
    FAA AC 23.1311-1 : 2011 INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES
    FAA AC 25-11 : 2014 ELECTRONIC FLIGHT DISPLAYS
    FAA 8110.55 : 2016 HOW TO EVALUATE AND ACCEPT PROCESSES FOR AERONAUTICAL DATABASE SUPPLIERS
    FAA N 8110.110 : 2010 SOFTWARE APPROVAL GUIDE LINES, CONTINUED
    FAA AC 00-66 : 2015 SELECTION OF CYCLIC REDUNDANCY CODE AND CHECKSUM ALGORITHMS TO ENSURE CRITICAL DATA INTEGRITY
    FAA AC 43-216 : 2017 SOFTWARE MANAGEMENT DURING AIRCRAFT MAINTENANCE
    FAA 8110.4 : 2011 TYPE CERTIFICATION

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

    FAA AC 27-1 : 2008 CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT
    RTCA DO 330 : 2011 SOFTWARE TOOL QUALIFICATION CONSIDERATIONS
    RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
    FAA AC 21-43 : 2015 PRODUCTION UNDER 14 CFR PART 21, SUBPARTS F, G, K, AND O
    FAA AC 33.28-2 : 2003 GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, RECIPROCATING ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS
    FAA 8110.4 : 2011 TYPE CERTIFICATION
    FAA AC 33.28-3 : 2014 GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, ENGINE CONTROL SYSTEMS
    FAA AC 23.1309-1 : 2011 SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
    RTCA DO 248 : C2011 SUPPORTING INFORMATION FOR DO-178C AND DO-278A
    FAA AC 29-2 : 2008 CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT
    RTCA DO 333 : 2011 FORMAL METHODS SUPPLEMENT TO DO-178C AND DO-278A
    FAA AC 25.1309-1 : 0 SYSTEM DESIGN AND ANALYSIS
    RTCA DO 331 : 2011 MODEL-BASED DEVELOPMENT AND VERIFICATION SUPPLEMENT TO DO-178C AND DO-278A
    FAA AC 20-115 : 2017 AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
    FAA 8040.4 : 2012 SAFETY RISK MANAGEMENT POLICY
    RTCA DO 332 : 2011 OBJECT-ORIENTED TECHNOLOGY AND RELATED TECHNIQUES SUPPLEMENT TO DO-178C AND DO-278A
    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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