Name: RTCA DO 178 : C2011
Brand: RTCA
Price: 522.00 USD

SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION

Available format(s)

Hardcopy

Language(s)

English

Published date

12-13-2011

Publisher

Radio Technical Commission for Aeronautics

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

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.

Committee	SC-205
DocumentType	Standard
Pages	0
PublisherName	Radio Technical Commission for Aeronautics
Status	Current

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ARINC 764 : 2005	HEAD-UP DISPLAY (HUD) SYSTEM
AOP 52 : 2016	GUIDANCE ON SOFTWARE SAFETY DESIGN AND ASSESSMENT OF MUNITION-RELATED COMPUTING SYSTEMS
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ASTM F 2538 : 2007 : REV A : R2010	Standard Practice for Design and Manufacture of Reciprocating Compression Ignition Engines for Light Sport Aircraft
NASA GB 8719.13 : 0	NASA SOFTWARE SAFETY GUIDEBOOK
DEFSTAN 00-970(PT1)SEC3/15(2015) : 2015	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE
MIL-HDBK-516 Revision C:2014	AIRWORTHINESS CERTIFICATION CRITERIA
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ARINC 542A : 1988	DIGITAL FLIGHT DATA RECORDER
FAA AC 120-76 : 2017	AUTHORIZATION FOR USE OF ELECTRONIC FLIGHT BAGS
FAA AC 25-28 : 2014	COMPLIANCE OF TRANSPORT CATEGORY AIRPLANES WITH CERTIFICATION REQUIREMENTS FOR FLIGHT IN ICING CONDITIONS
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ARINC 758-3:2011	COMMUNICATIONS MANAGEMENT UNIT (CMU) MARK 2
ARINC 652 : 1993	GUIDANCE FOR AVIONICS SOFTWARE MANAGEMENT
PREN 4839-001 : DRAFT 2016	AEROSPACE SERIES - ARC FAULT CIRCUIT BREAKERS, THREE-POLE, TEMPERATURE COMPENSATED, RATED CURRENT 3 A TO 25 A 115 V A.C. 400 HZ CONSTANT FREQUENCY - PART 001: TECHNICAL SPECIFICATION
BS ISO 22072:2011	Aerospace. Electrohydrostatic actuator (EHA). Characteristics to be defined in procurement specifications
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RG.AERO 00028 : 2005	ED-80/RTCA DO254 APPLICATION GUIDE
ARINC 615A-3 : 2007	SOFTWARE DATA LOADER USING ETHERNET INTERFACE
FAA AC 20-156 : 2006	AVIATION DATABUS ASSURANCE
ARINC 664-7 : 2009	AIRCRAFT DATA NETWORK - PART 7: AVIONICS FULL-DUPLEX SWITCHED ETHERNET NETWORK
SAE ARP 5120 : 2016	AIRCRAFT GAS TURBINE ENGINE HEALTH MANAGEMENT SYSTEM DEVELOPMENT AND INTEGRATION GUIDE
ARINC 809-3 : 2014	3GCN - SEAT DISTRIBUTION SYSTEM
SAE AIR 5924 : 2013	GUIDELINES FOR THE INTEGRATION OF ELECTRONIC ENGINE CONTROL SYSTEMS FOR TRANSPORT CATEGORY (PART 25) AND GENERAL AVIATION (PART 23) AIRCRAFT
SAE ARP 1070 : 2014	DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY
ARINC 628P2-9:2017	CABIN EQUIPMENT INTERFACES - PART 2: CABIN MANAGEMENT AND ENTERTAINMENT SYSTEMS - SEAT INTERFACES
ARINC 644A : 1996	PORTABLE MULTI-PURPOSE ACCESS TERMINAL (PMAT)
IEEE 730-2014 REDLINE	IEEE Standard for Software Quality Assurance Processes
DEFSTAN 00-56(PT2)/3(2004) : INTERIM	SAFETY MANAGEMENT REQUIREMENTS FOR DEFENCE SYSTEMS - PART 2: GUIDANCE ON ESTABLISHING A MEANS OF COMPLYING WITH PART 1
ARINC 628P4A-3: 2005	CABIN EQUIPMENT INTERFACES - PART 4A: CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM - CABIN DISTRIBUTION SYSTEM - DAISY CHAIN
FAA AC 25-15 : 1989	APPROVAL OF FLIGHT MANAGEMENT SYSTEMS IN TRANSPORT CATEGORY AIRPLANES
ISO/IEC/IEEE 29119-4:2015	Software and systems engineering Software testing Part 4: Test techniques
ISO/IEC TR 19759:2015	Software Engineering Guide to the software engineering body of knowledge (SWEBOK)
S.R. CR 12804:1997	CONCEPTUAL MODEL AND TAXONOMY FOR INFORMATION SYSTEMS ENGINEERING
ASTM F 3269 : 2017	Standard Practice for Methods to Safely Bound Flight Behavior of Unmanned Aircraft Systems Containing Complex Functions
FAA AC 25.1329-1 : 2016	APPROVAL OF FLIGHT GUIDANCE SYSTEMS
FAA AC 20-73 : 2006	AIRCRAFT ICE PROTECTION
FAA N 8000.326 : 2006	GUIDELINES FOR AIRWORTHINESS AND OPERATIONAL APPROVAL AND PROCEDURE DESIGN FOR NON-14 CFR PART 97 RNP SAAAR APPROACH PROCEDURES
16/30320046 DC : 0	BS ISO 26262-8 - ROAD VEHICLES - FUNCTIONAL SAFETY - PART 8: SUPPORTING PROCESSES
FAA AC 20-183 : 2014	LASER AIRWORTHINESS INSTALLATION GUIDANCE
ISO 22072:2011	Aerospace — Electrohydrostatic actuator (EHA) — Characteristics to be defined in procurement specifications
09/30202071 DC : 0	BS EN 9115 - QUALITY MANAGEMENT SYSTEMS REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE ORGANIZATIONS - REQUIREMENTS FOR DELIVERABLE SOFTWARE
FAA AC 20-131 : 0	AIRWORTHINESS APPROVAL OF TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEMS (TCAS 2) AND MODE S TRANSPONDERS
ARINC 763A : 2008	MARK 2 NETWORK SERVER SYSTEM (NSS) - FORM AND FIT DEFINITION
SAE ARP 6137 : 2015	TIRE PRESSURE MONITORING SYSTEMS (TPMS) FOR AIRCRAFT
FAA AC 20-185 : 2015	AIRWORTHINESS APPROVAL OF SYNTHETIC VISION GUIDANCE SYSTEM
FAA AC 23.1309-1 : 2011	SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
FAA AC 90-101 : 2011	APPROVAL GUIDANCE FOR RNP PROCEDURES WITH AR
FAA AC 20-138 : 2014	AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION SYSTEMS
BS ISO/IEC/IEEE 29119-4:2015	Software and systems engineering. Software testing Test techniques
09/30179109 DC : 0	BS ISO 26262-8 - ROAD VEHICLES - FUNCTIONAL SAFETY - PART 8: SUPPORTING PROCESSES
DEFSTAN 66-31(PT5)/1(2007) : 2007	BASIC REQUIREMENTS & TESTS FOR ELECTRONIC & ELECTRICAL TEST & MEASUREMENT EQUIPMENT - PART 5: CONTRACTOR REQUIREMENTS - LAND USE APPLICATION
ARINC 744 : 1990	FULL-FORMAT PRINTER
FAA AC 20-150 : 2014	AIRWORTHINESS APPROVAL OF SATELLITE VOICE (SATVOICE) EQUIPMENT SUPPORTING AIR TRAFFIC SERVICE (ATS) COMMUNICATION
ARINC 667-2: 2017	GUIDANCE FOR THE MANAGEMENT OF FIELD LOADABLE SOFTWARE
CSA ISO/IEC TR 24718 : 2006	INFORMATION TECHNOLOGY - PROGRAMMING LANGUAGES - GUIDE FOR THE USE OF THE ADA RAVENSCAR PROFILE IN HIGH INTEGRITY SYSTEMS
ARINC 660 : 1995	CNS/ATM AVIONICS, FUNCTIONAL ALLOCATION AND RECOMMENDED ARCHITECTURES
SAE AS 5681 : 2016	MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR REMOTE ON-GROUND ICE DETECTION SYSTEMS
SAE ARP 6461 : 2013	GUIDELINES FOR IMPLEMENTATION OF STRUCTURAL HEALTH MONITORING ON FIXED WING AIRCRAFT
ISO/IEC TR 24772:2013	Information technology Programming languages Guidance to avoiding vulnerabilities in programming languages through language selection and use
FAA AC 20-121 : A	AIRWORTHINESS APPROVAL OF LORAN-C NAVIGATION SYSTEMS FOR USE IN THE U.S. NATIONAL AIRSPACE SYSTEM (NAS) AND ALASKA
ARINC 664-5 : 2005	AIRCRAFT DATA NETWORK - PART 5: NETWORK DOMAIN CHARACTERISTICS AND INTERCONNECTION
ARINC 771 : 2016	LOW-EARTH ORBITING AVIATION SATELLITE COMMUNICATION SYSTEM
SAE ARP 5415 : 2008	USER'S MANUAL FOR CERTIFICATION OF AIRCRAFT ELECTRICAL/ELECTRONIC SYSTEMS FOR THE INDIRECT EFFECTS OF LIGHTNING
PREN 9115 : 200P1	QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE ORGANIZATIONS - DELIVERABLE SOFTWARE (SUPPLEMENT TO EN 9100)
SAE AIR 4367 : 2012	AIRCRAFT INFLIGHT ICE DETECTORS AND ICING RATE MEASURING INSTRUMENTS
ARINC 628-4C : 2005	CABIN EQUIPMENT INTERFACES (CEI) - PART 4C: CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM - CABIN DISTRIBUTION SYSTEM - 2[ND] GENERATION - DAISY CHAIN
FAA AC 20-172 : 2015	AIRWORTHINESS APPROVAL FOR ADS-B IN SYSTEMS AND APPLICATIONS
ARINC 808 : 2010	3GCN - CABIN DISTRIBUTION SYSTEM
SAE ARP 1270 : 2015	AIRCRAFT CABIN PRESSURIZATION CRITERIA
FAA 8150.1 : 2017	TECHNICAL STANDARD ORDER PROGRAM
ARINC 445 : 2014	GUIDANCE FOR CONFIGURATION AND CONTROL OF LOADABLE SOFTWARE PARTS IN FLIGHT SIMULATION TRAINING DEVICES
ARINC 702A : 2014	ADVANCED FLIGHT MANAGEMENT COMPUTER SYSTEM
ARINC 651-1 : 1997	DESIGN GUIDANCE FOR INTEGRATED MODULAR AVIONICS
ARINC 664P3-2:2009	AIRCRAFT DATA NETWORK - PART 3: INTERNET-BASED PROTOCOLS AND SERVICES
ARINC 738A : 1999	AIR DATA AND INERTIAL REFERENCE SYSTEM (ADIRS)
ARINC 629-1-5 : 1999	MULTI-TRANSMITTER DATA BUS - PART 1: TECHNICAL DESCRIPTION
DEFSTAN 00-22/1(1986) : 1986 AMD 1	FIRMWARE MANAGEMENT
FAA AC 20-145 : 2003	GUIDANCE FOR INTEGRATED MODULAR AVIONICS (IMA) THAT IMPLEMENT TSO-C153 AUTHORIZED HARDWARE ELEMENTS
FAA AC 135-14 : 2015	HELICOPTER AIR AMBULANCE OPERATIONS
EN 9115:2013	Quality Management Systems - Requirements for Aviation, Space and Defense Organizations - Deliverable Software (Supplement to EN 9100)
CR 12804 : 1997	CONCEPTUAL MODEL AND TAXONOMY FOR INFORMATION SYSTEMS ENGINEERING