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FAA AC 20-170:2010

FAA AC 20-170:2010 Integrated Modular Avionics Development, Verification, Integration, And Approval Using Rtca/Do-297 And Technical Standard Order-C153 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 i

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Table of Contents

Chapter1-RTCA-DO-297asanAcceptableMeansofCompliance
Chapter2-AcceptanceAndIncrementalAcceptance
Chapter3-ObtaininganIMAComponentAcceptanceLetter
Chapter4-ReuseofIMAComponents
Chapter5-ConfigurationManagementofanIMASystem
Chapter6-IMARecoveryFeatures
Chapter7-TopicsNotCoveredbyRTCA/DO-297
Chapter8-UseOfTSOAuthorizedComponentsInIMASystems
AppendixA-EnvironmentalQualificationGuidanceforTSO-C153
AppendixB-SampleIMAComponentAcceptanceCoverLetter
AppendixC-SampleAcceptanceLetter
AppendixD-RelatedDocumentsAndHowToGetThem
AppendixE-Glossary
AppendixF-Acronyms
AppendixG-PartialListofFunctionalTSOs

Abstract

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.

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