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  • RTCA DO 178 : C2011

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    SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION

    Available format(s):  Hardcopy

    Language(s):  English

    Published date:  13-12-2011

    Publisher:  Radio Technical Commission for Aeronautics

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

    1.0 Introduction
    1.1 Purpose
    1.2 Scope
    1.3 Relationship to other documents
    1.4 How to use this document
    1.5 Document overview
    2.0 System aspects relating to software development
    2.1 Information flow between system and software
           life cycle processes
    2.2 Failure condition and software level
    2.3 System architectural considerations
    2.4 System considerations for user-modifiable
           software, option-selectable software and
           commercial off-the-shelf software
    2.5 System design considerations for field-loadable
           software
    2.6 System requirements considerations for software
           verification
    2.7 Software considerations in system verification
    3.0 Software life cycle
    3.1 Software life cycle processes
    3.2 Software life cycle definition
    3.3 Transition criteria between processes
    4.0 Software planning process
    4.1 Software planning process objectives
    4.2 Software planning process activities
    4.3 Software plans
    4.4 Software life cycle environment planning
    4.5 Software development standards
    4.6 Review and assurance of the software planning
           process
    5.0 Software development processes
    5.1 Software requirements process
    5.2 Software design process
    5.3 Software coding process
    5.4 Integration process
    5.5 Traceability
    6.0 Software verification process
    6.1 Software verification process objectives
    6.2 Software verification process activities
    6.3 Software reviews and analyses
    6.4 Software testing process
    7.0 Software configuration management process
    7.1 Software configuration management process
           objectives
    7.2 Software configuration management process
           activities
    7.3 Data control categories
    8.0 Software quality assurance process
    8.1 Software quality assurance process objectives
    8.2 Software quality assurance process activities
    8.3 Software conformity review
    9.0 Certification liaison process
    9.1 Means of compliance and planning
    9.2 Compliance substantiation
    9.3 Minimum software life cycle data that is
           submitted to certification authority
    9.4 Software life cycle data related to type design
    10.0 Overview of aircraft and engine certification
    10.1 Certification basis
    10.2 Software aspects of certification
    10.3 Compliance determination
    11.0 Software life cycle data
    11.1 Plan for software aspects of certification
    11.2 Software development plan
    11.3 Software verification plan
    11.4 Software configuration management plan
    11.5 Software quality assurance plan
    11.6 Software requirements standards
    11.7 Software design standards
    11.8 Software code standards
    11.9 Software requirements data
    11.10 Design description
    11.11 Source code
    11.12 Executable object code
    11.13 Software verification cases and procedures
    11.14 Software verification results
    11.15 Software life cycle environment configuration
           index
    11.16 Software configuration index
    11.17 Problem reports
    11.18 Software configuration management records
    11.19 Software quality assurance records
    11.20 Software accomplishment summary
    12.0 Additional considerations
    12.1 Use of previously developed software
    12.2 Tool qualification
    12.3 Alternative methods
    Annex A Process objectives and outputs by software
             level
    Annex B Acronyms and glossary of terms
    Appendix A Background of document DO-178
    1.0 Prior document version history
    2.0 RTCA/EUROCAE committee activities in the
                production of this document
    3.0 Summary of differences between DO-178B and
                DO-178A
    Appendix B Committee membership
    Appendix C Index of terms
    Appendix D Improvement suggestion form
    Figures
    1-1 Document overview
    2-1 System safety-related information flow between
          system and software life cycle processes
    3-1 Example of software project using four different
          development sequences
    6-1 Software testing process
    Tables
    7-1 SCM process objectives associated with CC1 and CC2
          data
    A-1 Software planning process
    A-2 Software development processes
    A-3 Verification of outputs of software requirements
          process
    A-4 Verification of outputs of software design process
    A-5 Verification of outputs of software coding and
          integration processes
    A-6 Testing of outputs of integration process
    A-7 Verification of verification process results
    A-8 Software configuration management process
    A-9 Software quality assurance process
    A-10 Certification liaison process

    Abstract - (Show below) - (Hide below)

    Specifies recommendations for the production of software for airborne systems and equipment that performs its intended function with a level of confidence in safety that complies with airworthiness requirements.

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

    Committee SC-205
    Document Type Standard
    Publisher Radio Technical Commission for Aeronautics
    Status Current

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

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    FAA AC 20-153 : 2016 ACCEPTANCE OF AERONAUTICAL DATA PROCESSES AND ASSOCIATED DATABASES
    SAE AS 6019 : 2012 ARC FAULT CIRCUIT BREAKER (AFCB), AIRCRAFT, TRIP-FREE 28 VDC
    SAE AS 8055A : 2015 MINIMUM PERFORMANCE STANDARD FOR AIRBORNE HEAD UP DISPLAY (HUD)
    S.R. CWA 17044:2016 AEROSPACE SERIES - MODULES FOR ELECTRO-MECHANICAL ACTUATORS IN AIRCRAFT
    I.S. EN 9115:2013 QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE ORGANIZATIONS - DELIVERABLE SOFTWARE (SUPPLEMENT TO EN 9100)
    ARINC 822-1 : 2008 AIRCRAFT/GROUND IP COMMUNICATION
    SAE ARP 94910 : 2012 AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR
    ARINC 708A : 1999 AIRBORNE WEATHER RADAR WITH FORWARD LOOKING WINDSHEAR DETECTION CAPABILITY
    SAE AS 6858 : 2017 INSTALLATION OF FUEL CELL SYSTEMS IN LARGE CIVIL AIRCRAFT
    NASA STD 8719.13B : 2004 **DUPLICATE RECORD**
    DEFSTAN 00-55(PT1)/4(2016) : 2016 REQUIREMENTS FOR SAFETY OF PROGRAMMABLE ELEMENTS (PE) IN DEFENCE SYSTEMS - PART 1: REQUIREMENTS AND GUIDANCE
    VDI 4007:2012-06 RELIABILITY GOALS - DETERMINATION, CHECK, REVIEW, CERTIFICATE
    SAE ARP 1907 : 2016 AUTOMATIC BRAKING SYSTEMS
    SAE ARP 1839 : 2015 A GUIDE TO AIRCRAFT TURBINE ENGINE VIBRATION MONITORING SYSTEMS
    ARINC 832 : 2016 CABIN EQUIPMENT INTERFACES, 4GCN CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM, CABIN DISTRIBUTION SYSTEM
    10/30203853 DC : 0 BS ISO 22072 - AEROSPACE - ELECTROHYDROSTATIC ACTUATOR (EHA) - CHARACTERISTICS TO BE DEFINED IN PROCUREMENT SPECIFICATIONS
    A A 58055 : 0 INDICATOR, ATTITUDE, THREE INCH, SOLID STATE, SELF-CONTAINED
    FAA AC 120-86 : 2005 AIRCRAFT SURVEILLANCE SYSTEMS AND APPLICATIONS
    FAA AC 20-167 : 2016 AIRWORTHINESS APPROVAL OF ENHANCED VISION SYSTEM, SYNTHETIC VISION SYSTEM, COMBINED VISION SYSTEM, AND ENHANCED FLIGHT VISION SYSTEM EQUIPMENT
    FAA 8110.49 : 2011 SOFTWARE APPROVAL GUIDELINES
    ARINC 744A-1 : 1994 FULL-FORMAT PRINTER WITH GRAPHICS CAPABILITY
    ASTM F 2538 : 2007 Standard Practice for Design and Manufacture of Reciprocating Compression Ignition Engines for Light Sport Aircraft
    SAE AIR 6464 : 2013 EUROCAE/SAE WG80/AE-7AFC HYDROGEN FUEL CELLS AIRCRAFT FUEL CELL SAFETY GUIDELINES
    17/30309594 DC : 0 BS IEC 62138 - NUCLEAR POWER PLANTS - INSTRUMENTATION AND CONTROL SYSTEMS IMPORTANT TO SAFETY - SOFTWARE ASPECTS FOR COMPUTER-BASED SYSTEMS PERFORMING CATEGORY B OR C FUNCTIONS
    MIL STD 1798 : C MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM
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    FAA AC 20-161 : 2008 AIRCRAFT ONBOARD WEIGHT AND BALANCE SYSTEMS
    RG.AERO 00044 : 2014 ARP4754A/ED-79A APPLICATION GUIDE
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    FAA AC 20-159 : 2007 OBTAINING DESIGN AND PRODUCTION APPROVAL OF AIRPORT MOVING MAP DISPLAY APPLICATIONS INTENDED FOR ELECTRONIC FLIGHT BAG SYSTEMS
    ARINC 611-1 : 1999 GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY SYSTEMS
    ARINC 636 : 1993 ON-BOARD LOCAL AREA NETWORK
    PREN 4838-001 : DRAFT 2016 CORR 17 AEROSPACE SERIES - ARC FAULT CIRCUIT BREAKERS, SINGLE-POLE, TEMPERATURE COMPENSATED, RATED CURRENT 3 A TO 25 A 115 V A.C. 400 HZ CONSTANT FREQUENCY - PART 001: TECHNICAL SPECIFICATION
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    FAA N 8110.110 : 2010 SOFTWARE APPROVAL GUIDE LINES, CONTINUED
    UNI EN 9115 : 2013 QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE ORGANIZATIONS - DELIVERABLE SOFTWARE (SUPPLEMENT TO EN 9100)
    SAE ARP 1595 : 2013(R2019) DESIGN AND VERIFICATION OF AIRCRAFT NOSE WHEEL STEERING SYSTEMS
    CAN/CSA-ISO/IEC TR 24718:2006(R2016) INFORMATION TECHNOLOGY - PROGRAMMING LANGUAGES - GUIDE FOR THE USE OF THE ADA RAVENSCAR PROFILE IN HIGH INTEGRITY SYSTEMS
    SAE ARP 5873 : 2015 LED PASSENGER READING LIGHT ASSEMBLY
    I.S. EN 16603-40:2014 SPACE ENGINEERING - PART 40: SOFTWARE
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    SAE AIR 6027 : 2017 CONSIDERATIONS FOR SAFE STORE OPERATION ON MANNED AND UNMANNED VEHICLES
    SAE ARP 5287 : 2008 OPTICAL MEASUREMENT PROCEDURES FOR AIRBORNE HEAD UP DISPLAY (HUD)
    SAE JA 1003 : 2012 SOFTWARE RELIABILITY PROGRAM IMPLEMENTATION GUIDE
    SAE ARP 9034 : 2015 A PROCESS STANDARD FOR THE STORAGE, RETRIEVAL AND USE OF THREE-DIMENSIONAL TYPE DESIGN DATA
    CAN/CSA-ISO/IEC/IEEE 29119-4:16 Software and systems engineering Software testing Part 4: Test techniques (Adopted ISO/IEC/IEEE 29119-4:2015, first edition, 201 5-12-01)
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    AOP 52 : 2016 GUIDANCE ON SOFTWARE SAFETY DESIGN AND ASSESSMENT OF MUNITION-RELATED COMPUTING SYSTEMS
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