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FAA AC 20-170 : 2010

NA

NA

Status of Standard is Unknown

INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2010

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.

DocumentType
Standard
Pages
64
PublisherName
Federal Aviation Administration
Status
NA
Supersedes

FAA AC 20-115 : 2017 AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
FAA AC 20-174 : 2011 DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
FAA AC 23.1311-1 : 2011 INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES
FAA AC 25-11 : 2014 ELECTRONIC FLIGHT DISPLAYS
FAA AC 00-69 : 2017 BEST PRACTICES FOR AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
FAA AC 00-66 : 2015 SELECTION OF CYCLIC REDUNDANCY CODE AND CHECKSUM ALGORITHMS TO ENSURE CRITICAL DATA INTEGRITY
FAA AC 20-138 : 2014 AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION SYSTEMS

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