RTCA DO 178 : C2011
Current
Current
The latest, up-to-date edition.
SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
Available format(s)
Hardcopy
Language(s)
English
Published date
13-12-2011
Important note : All end users must be registered with an Account prior to user licenses being assigned.
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
|
| PD ISO/IEC TR 19759:2016 | Software Engineering. Guide to the software engineering body of knowledge (SWEBOK) |
| DEFSTAN 00-56(PT2)/4(2007) : 2007 | SAFETY MANAGEMENT REQUIREMENTS FOR DEFENCE SYSTEMS - PART 2: GUIDANCE ON ESTABLISHING A MEANS OF COMPLYING WITH PART 1 |
| ARINC 628-4B : 1999 | CABIN EQUIPMENT INTERFACES - PART 4B: CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM CABIN DISTRIBUTION SYSTEM - STAR WIRING |
| FAA AC 20-115 : 2017 | AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( ) |
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| SAE AS 5506/1 : 2015 | SAE ARCHITECTURE ANALYSIS AND DESIGN LANGUAGE (AADL) ANNEX VOLUME 1: ANNEX A: ARINC653 ANNEX, ANNEX C: CODE GENERATION ANNEX, ANNEX E: ERROR MODEL ANNEX |
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| ARINC 756-3 : 2004 | GNSS NAVIGATION AND LANDING UNIT (GNLU) |
| ISO 26262-8:2011 | Road vehicles Functional safety Part 8: Supporting processes |
| FAA AC 20-174 : 2011 | DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
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| UNE-EN 9115:2013 | Quality Management Systems - Requirements for Aviation, Space and Defense Organizations - Deliverable Software (Supplement to EN 9100) |
| FAA AC 23-15 : 2003 | SMALL AIRPLANE CERTIFICATION COMPLIANCE PROGRAM |
| DEFSTAN 00-55(PT2)/2(1997) : 1997 ERRATUM 1997 | REQUIREMENTS FOR SAFETY RELATED SOFTWARE IN DEFENCE EQUIPMENT - PART 2: GUIDANCE |
| ARINC 658 : 2017 | INTERNET PROTOCOL SUITE (IPS) FOR AERONAUTICAL SAFETY SERVICES - ROADMAP DOCUMENT |
| 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 |
| FAA AC 107-2 : 2016 | SMALL UNMANNED AIRCRAFT SYSTEMS (SUAS) |
| FAA AC 120-96 : 2016 | OPERATIONS CONTROL CENTER (OCC) FOR HELICOPTER AIR AMBULANCE (HAA) OPERATIONS |
| ARINC 704-7 : 1999 | INERTIAL REFERENCE SYSTEM |
| 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 |
| BS ISO/IEC 14598-4:1999 | Information technology. Software production evaluation Process for acquirers |
| SAE AS 9006 : 2013 | DELIVERABLE AEROSPACE SOFTWARE SUPPLEMENT FOR AS9100A - QUALITY MANAGEMENT SYSTEMS - AEROSPACE - REQUIREMENTS FOR SOFTWARE |
| TR 9109 : 1 | AEROSPACE SERIES - GUIDELINES FOR SOFTWARE QUALITY MANAGEMENT |
| SAE AIR 1839 : 2017 | A GUIDE TO AIRCRAFT TURBINE ENGINE VIBRATION MONITORING SYSTEMS |
| ARMP-9 : 2009 | GUIDE TO THE MANAGEMENT OF SOFTWARE R&M |
| SAE ARD 5296 : 2002 | REQUIREMENTS FOR THE AVIONICS ARCHITECTURE DESCRIPTION LANGUAGE (AADL) |
| BS ISO 26262-8:2011 | Road vehicles. Functional safety Supporting processes |
| SAE AS 8054 : 1996 | AIRBORNE ENGINE VIBRATION MONITORING (EVM) SYSTEM, GUIDELINES FOR PERFORMANCE STANDARD FOR |
| ARINC 704A : 1999 | INERTIAL REFERENCE SYSTEM |
| ARINC 768-2 : 2011 | INTEGRATED SURVEILLANCE SYSTEM (ISS) |
| ASTM F 2538 : 2007 : REV A | Standard Practice for Design and Manufacture of Reciprocating Compression Ignition Engines for Light Sport Aircraft |
| FAA AC 25.703-1 : 0 | TAKEOFF CONFIGURATION WARNING SYSTEMS |
| ARINC 714A : 2015 | MARK 4 AIRBORNE SELECTIVE CALLING (SELCAL) |
| ARINC 760-1 : 2000 | GNSS NAVIGATION UNIT (GNU) |
| SAE ARP 1834 : 1997(S2018) | FAULT/FAILURE ANALYSIS FOR DIGITAL SYSTEMS AND EQUIPMENT |
| DEFSTAN 00-55(PT1)/2(1997) : 1997 | REQUIREMENTS FOR SAFETY RELATED SOFTWARE IN DEFENCE EQUIPMENT - PART 1: REQUIREMENTS |
| ARINC 653-0 : 2015 | AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE - PART 0: OVERVIEW OF ARINC 653 |
| SAE ARP 6803 : 2016 | IVHM CONCEPTS, TECHNOLOGY AND IMPLEMENTATION OVERVIEW |
| DEFSTAN 66-31(PT5)/2(2008) : 2008 | BASIC REQUIREMENTS & TESTS FOR ELECTRONIC & ELECTRICAL TEST & MEASUREMENT EQUIPMENT - PART 5: CONTRACTOR REQUIREMENTS - LAND USE APPLICATION |
| ASTM F 2689 : 2008 | Standard Practice for Design and Manufacture of Reciprocating Spark Ignition Engines for Unmanned Aircraft Systems (Withdrawn 2014) |
| DEFSTAN 00-970(PT1)SEC3/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| DEFSTAN 00-970(PT1)SEC3/4(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 3 - STRUCTURE |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-55(PT1)/3(2014) : 2014 | REQUIREMENTS FOR SAFETY OF PROGRAMMABLE ELEMENTS (PE) IN DEFENCE SYSTEMS - PART 1: REQUIREMENTS AND GUIDANCE |
| DEFSTAN 00-970(PT1)SEC3/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 66-31(PT1)/2(2008) : 2008 | BASIC REQUIREMENTS AND TESTS FOR ELECTRONIC AND ELECTRICAL TEST AND MEASUREMENT EQUIPMENT - PART 1: INTRODUCTION AND GUIDE TO THE SPECIFICATION AND SELECTION OF TEST AND MEASUREMENT EQUIPMENT BY THE PROCURING AUTHORITY |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT1)SEC3/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| DEFSTAN 00-970(PT1)SEC3/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| DEFSTAN 00-56(PT1)/5(2014) : 2014 | SAFETY MANAGEMENT REQUIREMENTS FOR DEFENCE SYSTEMS - PART 1: REQUIREMENTS AND GUIDANCE |
| DEFSTAN 00-970(PT1)SEC3/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| DEFSTAN 00-970(PT1)SEC3/14(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 66-31(PT3)/2(2008) : 2008 | BASIC REQUIREMENTS & TESTS FOR ELECTRONIC & ELECTRICAL TEST & MEASUREMENT EQUIPMENT - PART 3: CONTRACTOR REQUIREMENTS - AIR USE APPLICATION |
| DEFSTAN 00-56(PT2)/2(1996) : 1996 | SAFETY MANAGEMENT REQUIREMENTS FOR DEFENCE SYSTEMS - PART 2: GUIDANCE |
| DEFSTAN 00-970(PT1)SEC3/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3 - STRUCTURE |
| DEFSTAN 00-970(PT1)SEC3/5(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 3: STRUCTURE |
| DEFSTAN 66-31(PT3)/1(2007) : 2007 | BASIC REQUIREMENTS & TESTS FOR ELECTRONIC & ELECTRICAL TEST & MEASUREMENT EQUIPMENT - PART 3: CONTRACTOR REQUIREMENTS - AIR USE APPLICATION |
| DEFSTAN 00-970(PT1)SEC3/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3 - STRUCTURE |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 66-31(PT1)/1(2007) : 2007 | BASIC REQUIREMENTS & TESTS FOR ELECTRONIC & ELECTRICAL TEST & MEASUREMENT EQUIPMENT - PART 1: INTRODUCTION AND GUIDE TO THE SPECIFICATION AND SELECTION OF TEST AND MEASUREMENT EQUIPMENT BY THE PROCURING AUTHORITY |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-56(PT1)/6(2015) : 2015 | SAFETY MANAGEMENT REQUIREMENTS FOR DEFENCE SYSTEMS - PART 1: REQUIREMENTS AND GUIDANCE |
| DEFSTAN 00-970(PT1)SEC3/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| ARINC 664P8-1 : 2010 | Aircraft Data Network, Part 8, Interoperation with Non-IP Protocols and Services |
| ARINC 765 : 2003 | ETHERNET SWITCH UNIT (ESU) |
| SAE ARP 6253 : 2017 | LEDS AND AIRCRAFT APPLICATIONS |
| ASTM F 3201 : 2016 | Standard Practice for Ensuring Dependability of Software Used in Unmanned Aircraft Systems (UAS) |
| ARINC 609 : 1987 | DESIGN GUIDANCE FOR AIRCRAFT ELECTRICAL POWER SYSTEMS |
| FAA AC 90-96 : 2010 | APPROVAL OF U.S. OPERATORS AND AIRCRAFT TO OPERATE UNDER INSTRUMENT FLIGHT RULES (IFR) IN EUROPEAN AIRSPACE DESIGNATED FOR BASIC AREA NAVIGATION (B-RNAV)/RNAV 5 AND PRECISION AREA NAVIGATION (P-RNAV) |
| DEFSTAN 00-54(PT1)/1(1999) : 1999 | REQUIREMENTS FOR SAFETY RELATED ELECTRONIC HARDWARE IN DEFENCE EQUIPMENT - PART 1: REQUIREMENTS |
| DEFSTAN 00-54(PT2)/1(1999) : 1999 | REQUIREMENTS FOR SAFETY RELATED ELECTRONIC HARDWARE IN DEFENCE EQUIPMENT - PART 2: GUIDANCE |
| DEFSTAN 66-31(PT4)/1(2007) : 2007 | BASIC REQUIREMENTS & TESTS FOR ELECTRONIC & ELECTRICAL TEST & MEASUREMENT EQUIPMENT - PART 4: CONTRACTOR REQUIREMENTS - NAVAL USE APPLICATION |
| ARINC 781:2017 | MARK 3 AVIATION SATELLITE COMMUNICATIONS SYSTEMS |
| ASTM F 3238 : 2017 | Standard Specification for Design and Installation of an Infrared (IR) Searchlight System (USA) |
| SAE ARP 6275 : 2014 | DETERMINATION OF COST BENEFITS FROM IMPLEMENTING AN INTEGRATED VEHICLE HEALTH MANAGEMENT SYSTEM |
| ARINC 629 : 90 SUPP 5 | MULTI TRANSMITTER DATA BUS - TECHNICAL DESCRIPTION |
| ARINC 660A : 2001 | CNS/ATM AVIONICS, FUNCTIONAL ALLOCATION AND RECOMMENDED ARCHITECTURES |
| FAA AC 90-105 : 2016 | APPROVAL GUIDANCE FOR RNP OPERATIONS AND BAROMETRIC VERTICAL NAVIGATION IN THE U.S. NATIONAL AIRSPACE SYSTEM AND IN OCEANIC AND REMOTE CONTINENTAL AIRSPACE |
| SAE AIR5691A : 2017 | GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY INDICATING SYSTEMS |
| CSA ISO/IEC TR 24718 : 2006 : R2011 | INFORMATION TECHNOLOGY - PROGRAMMING LANGUAGES - GUIDE FOR THE USE OF THE ADA RAVENSCAR PROFILE IN HIGH INTEGRITY SYSTEMS |
| FAA AC 20-173 : 2011 | INSTALLATION OF ELECTRONIC FLIGHT BAG COMPONENTS |
| FAA AC 25-11 : 2014 | ELECTRONIC FLIGHT DISPLAYS |
| ARINC 646 : 1995 | ETHERNET LOCAL AREA NETWORK (ELAN) |
| PD CR 13694:1999 | Health informatics. Safety and security related software quality standards for healthcare (SSQS) |
| SAE AS 6163 : 2015 | TEMPERATURE CONTROLLED CONTAINER - PERFORMANCE REQUIREMENTS AND TEST PARAMETERS |
| FAA AC 00-69 : 2017 | BEST PRACTICES FOR AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( ) |
| SAE ARP 6259 : 2016 | LED REPLACEMENT FOR INCANDESCENT/HALOGEN BULBS OR FLUORESCENT LAMPS TRANSPORT CATEGORY AIRCRAFT AND ROTORCRAFT |
| FAA AC 25.1419-1 : 0 | CERTIFICATION OF TRANSPORT CATEGORY AIRPLANES FOR FLIGHT IN ICING CONDITIONS |
| FAA AC 20-148 : 2004 | REUSABLE SOFTWARE COMPONENTS |
| FAA 8110.55 : 2016 | HOW TO EVALUATE AND ACCEPT PROCESSES FOR AERONAUTICAL DATABASE SUPPLIERS |
| ARINC 632 : 1994 | GATE-AIRCRAFT TERMINAL ENVIRONMENT LINK (GATELINK) - GROUND SIDE |
| 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 Base Document:1996 | 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 Revision C:2013 | MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM |
| FAA AC 20-165 : 2015 | AIRWORTHINESS APPROVAL OF AUTOMATIC DEPENDENT SURVEILLANCE - BROADCAST OUT SYSTEMS |
| FAA AC 20-161 : 2008 | AIRCRAFT ONBOARD WEIGHT AND BALANCE SYSTEMS |
| RG.AERO 00044 : 2014 | ARP4754A/ED-79A APPLICATION GUIDE |
| FAA AC 25.1419-2 : 2009 | COMPLIANCE WITH THE ICE PROTECTION REQUIREMENTS OF SECTION 25.1419(E), (F), (G), AND (H) |
| SAE AS 5116 : 2003 | MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR GROUND ICE DETECTION SYSTEMS |
| 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 |
| SAE ARP 5580 : 2012 | RECOMMENDED FAILURE MODES AND EFFECTS ANALYSIS (FMEA) PRACTICES FOR NON-AUTOMOBILE APPLICATIONS |
| 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 |
| ARINC 659 : 1993 | BACKPLANE DATA BUS |
| 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) |
| SAE AS 5498 : 2017 | MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR INFLIGHT ICING DETECTION SYSTEMS |
| DEFSTAN 66-31(PT4)/2(2008) : 2008 | BASIC REQUIREMENTS & TESTS FOR ELECTRONIC & ELECTRICAL TEST & MEASUREMENT EQUIPMENT - PART 4: CONTRACTOR REQUIREMENTS - NAVAL USE APPLICATION |
| ARINC 764 : 2005 | HEAD-UP DISPLAY (HUD) SYSTEM |
| AOP 52 : 2016 | GUIDANCE ON SOFTWARE SAFETY DESIGN AND ASSESSMENT OF MUNITION-RELATED COMPUTING SYSTEMS |
| ARINC 613 : 1988 | GUIDANCE FOR USING THE ADA PROGRAMMING LANGUAGE IN AVIONIC SYSTEMS |
| ARINC 675 : 2017 | GUIDANCE FOR THE MANAGEMENT OF AIRCRAFT SUPPORT DATA |
| FAA AC 00-66 : 2015 | SELECTION OF CYCLIC REDUNDANCY CODE AND CHECKSUM ALGORITHMS TO ENSURE CRITICAL DATA INTEGRITY |
| 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 |
| ARINC 664-1 : 2006 | AIRCRAFT DATA NETWORK - PART 1: SYSTEMS CONCEPTS AND OVERVIEW |
| BS 7925-2:1998 | Software testing Software component testing |
| SAE AIR 5372 : 2014 | INFORMATION ON BRAKE-BY-WIRE (BBW) BRAKE CONTROL SYSTEMS |
| FAA AC 43-216 : 2017 | SOFTWARE MANAGEMENT DURING AIRCRAFT MAINTENANCE |
| SAE AS 9115 : 2017 | QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE, AND DEFENSE ORGANIZATIONS - DELIVERABLE SOFTWARE (SUPPLEMENT TO 9100:2016) |
| SAE ARP 6154 : 2017 | AEROSPACE FLUID POWER ELECTROHYDROSTATIC MODULE, DESIGN, PERFORMANCE AND TEST RECOMMENDATIONS |
| 16/30244282 DC : 0 | BS EN 9115 - QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE ORGANIZATIONS - DELIVERABLE SOFTWARE (SUPPLEMENT TO EN 9100) |
| 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 |
| PD ISO/IEC TR 24772:2013 | Information technology. Programming languages. Guidance to avoiding vulnerabilities in programming languages through language selection and use |
| BS EN 9115:2013 | Quality Management Systems. Requirements for Aviation, Space and Defense Organizations. Deliverable Software (Supplement to EN 9100) |
| FAA AC 20-151 : 2017 | AIRWORTHINESS APPROVAL OF TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEMS (TCAS 2), VERSIONS 7.0 & 7.1 AND ASSOCIATED MODE S TRANSPONDERS |
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| 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 |
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| 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 | 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) |
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| ASTM F 3269 : 2017 | Standard Practice for Methods to Safely Bound Flight Behavior of Unmanned Aircraft Systems Containing Complex Functions |
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| ISO 22072:2011 | Aerospace — Electrohydrostatic actuator (EHA) — Characteristics to be defined in procurement specifications |
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| ARINC 763A : 2008 | MARK 2 NETWORK SERVER SYSTEM (NSS) - FORM AND FIT DEFINITION |
| SAE ARP 6137 : 2015 | TIRE PRESSURE MONITORING SYSTEMS (TPMS) FOR AIRCRAFT |
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| BS ISO/IEC/IEEE 29119-4:2015 | Software and systems engineering. Software testing Test techniques |
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| ARINC 744 : 1990 | FULL-FORMAT PRINTER |
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| 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 |
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| ISO/IEC TR 24772:2013 | Information technology Programming languages Guidance to avoiding vulnerabilities in programming languages through language selection and use |
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| 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 |
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| ARINC 808 : 2010 | 3GCN - CABIN DISTRIBUTION SYSTEM |
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| FAA 8150.1 : 2017 | TECHNICAL STANDARD ORDER PROGRAM |
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| 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 |
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