FAA AC 20-170 : 2013
Current
The latest, up-to-date edition.
INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153
Hardcopy , PDF
English
01-01-2013
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Chapter 1 - RTCA-DO-297 as an Acceptable Means of Compliance
Chapter 2 - Acceptance And Incremental Acceptance
Chapter 3 - Obtaining an IMA Component Acceptance Letter
Chapter 4 - Reuse of IMA Components
Chapter 5 - Configuration Management of an IMA System
Chapter 6 - IMA Recovery Features
Chapter 7 - Topics Not Covered by RTCA/DO-297
Chapter 8 - Use Of TSO Authorized Components In IMA Systems
Appendix A - Environmental Qualification Guidance for TSO-C153
Appendix B - Sample IMA Component Acceptance Cover Letter
Appendix C - Sample Acceptance Letter
Appendix D - Related Documents And How To Get Them
Appendix E - Glossary
Appendix F - Acronyms
Appendix G - Partial List of Functional TSOs
Appendix H - SAE ARP 4754 to ARP 4754A Cross-Reference Matrix
Explains how to obtain Federal Aviation Administration (FAA) airworthiness approval for the development, verification, and integration of an integrated modular avionics (IMA) system for installation into an aircraft or engine.
| DevelopmentNote |
Supersedes FAA AC 20-145. (11/2010)
|
| DocumentType |
Standard
|
| Pages |
66
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 27-1 : 2008 | CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT |
| FAA AC 23.1311-1 : 2011 | INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES |
| FAA AC 21-16 : 2011 | RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT" |
| RTCA DO 178 : C2011 | SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
| FAA AC 20-88 : A | GUIDELINES ON THE MARKING OF AIRCRAFT POWERPLANT INSTRUMENTS (DISPLAYS) |
| FAA AC 20-174 : 2011 | DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
| FAA AC 25-11 : 2014 | ELECTRONIC FLIGHT DISPLAYS |
| FAA AC 20-136 : 2011 | AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION |
| FAA AC 33.28-2 : 2003 | GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, RECIPROCATING ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS |
| SAE ARP 4754 : 2010 | GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
| FAA AC 20-158 : 2014 | THE CERTIFICATION OF AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEMS FOR OPERATION IN THE HIGH-INTENSITY RADIATED FIELDS (HIRF) ENVIRONMENT |
| RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
| FAA AC 20-152 : 2005 | RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
| FAA AC 20-156 : 2006 | AVIATION DATABUS ASSURANCE |
| SAE ARP 4761 : 1996 | GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
| FAA AC 20-145 : 2003 | GUIDANCE FOR INTEGRATED MODULAR AVIONICS (IMA) THAT IMPLEMENT TSO-C153 AUTHORIZED HARDWARE ELEMENTS |
| FAA AC 23.1309-1 : 2011 | SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES |
| FAA AC 120-76 : 2017 | AUTHORIZATION FOR USE OF ELECTRONIC FLIGHT BAGS |
| FAA AC 29-2 : 2008 | CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT |
| FAA AC 120-64 : 0 | OPERATIONAL USE AND MODIFICATION OF ELECTRONIC CHECKLISTS |
| FAA AC 25.1309-1 : 0 | SYSTEM DESIGN AND ANALYSIS |
| FAA AC 25.1701-1 : 2007 | CERTIFICATION OF ELECTRICAL WIRING INTERCONNECTION SYSTEMS ON TRANSPORT CATEGORY AIRPLANES |
| FAA AC 20-115 : 2017 | AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( ) |
| FAA AC 33.75-1 : 2007 | GUIDANCE MATERIAL FOR 14 CFR SECTION 33.75, SAFETY ANALYSIS |
| RTCA DO 297 : 2005 | Integrated Modular Avionics (IMA) Development Guidance and Certification Considerations<br> |
| FAA AC 20-148 : 2004 | REUSABLE SOFTWARE COMPONENTS |
| 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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