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  • FAA AC 20-145 : 2003

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    GUIDANCE FOR INTEGRATED MODULAR AVIONICS (IMA) THAT IMPLEMENT TSO-C153 AUTHORIZED HARDWARE ELEMENTS

    Available format(s): 

    Superseded date:  28-10-2010

    Language(s): 

    Published date:  12-01-2013

    Publisher:  Federal Aviation Administration

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    Table of Contents - (Show below) - (Hide below)

    1 PURPOSE
    2 RELATED DOCUMENTS
       a Code of Federal Regulations
       b FAA Technical Standard Orders (TSO)
       c FAA Policy Documents
       d FAA Advisory Circulars (AC)
       e RTCA, Inc. Documents
       f SAE Documents
    3 DEFINITIONS
    4 ACRONYMS
    5 SCOPE
    6 BACKGROUND
    7 DOCUMENT OVERVIEW
    8 IMA SYSTEM APPROVALS AND AUTHORIZATIONS
       a TSO-C153 Authorization
       b Functional TSO Authorization
       c Installation Approval
    9 SAFETY ASSESSMENT PROCESS GUIDANCE
    10 CONFIGURATION MANAGEMENT GUIDANCE
    11 ELECTRONIC IDENTIFICATION GUIDANCE
    12 SOFTWARE GUIDANCE
       a Software Assurance
       b Software Levels
       c Field-Loadable Software (FLS)
       d Partitioning and Protection
       e Software Reuse
    13 ELECTRONIC HARDWARE GUIDANCE
    14 IMA DESIGN GUIDANCE
       a Electrical Power for IMA Systems
       b Recovery Features
       c Built-In Test (BIT)
       d Maintenance Diagnostics
       e Failure Detection and Annunciation
       f Functional Partitioning
       g Functional Isolation
       h Intentional Transmitters
       i Visual and Aural Alerting
    15 ENVIRONMENTAL QUALIFICATION GUIDANCE
    Figure 15-1 RTCA/DO-160D Environmental Qualification
                Requirements
    16 HUMAN FACTORS AND FLIGHT CREW INTERFACE GUIDANCE
       a Human Factors Background
       b Potential Human Factors and Flight Crew Interface
         Issues with IMA Systems
       c Testing Considerations for Human Factors and Flight
         Crew Interface Issues
       d Methods of Compliance with Controls Regulations
    17 TESTING PRACTICES
       a IMA Hardware Element Testing
       b Individual System Testing
       c IMA System Integration Testing
       d Aircraft Ground Testing
       e Aircraft Flight Testing
       f Configuration Control During Flight Testing
    18 ROLES AND RESPONSIBILITIES OF IMA SYSTEM APPLICANTS
       a TSO-C153 Applicant Roles and Responsibilities
       b Functional TSO Applicant Roles and Responsibilities
       c TC, STC, ATC, ASTC Applicant Roles and Responsibilities
    19 ADDITIONAL GUIDANCE FOR THIRD-PARTY MANUFACTURERS
    20 AIRWORTHINESS CONSIDERATIONS
       a Initial Installation
       b Follow-on Installations
       c Change Impact Analysis
       d Change Classification
    21 MAINTENANCE AND CONTINUED AIRWORTHINESS GUIDANCE
       a Maintenance Instructions
       b Maintenance Diagnostics
       c Master Minimum Equipment List (MMEL)
    APPENDIX 1 PARTIAL LIST OF FUNCTIONAL TSOs

    Abstract - (Show below) - (Hide below)

    Provides an acceptable means, but not the only means, to obtain Federal Aviation Administration's (FAA) airworthiness approval for the installation of an Integrated Modular Avionics (IMA) System that uses hardware elements authorized under Technical Standard Order (TSO)-C153, Integrated Modular Avionics Hardware Elements.

    General Product Information - (Show below) - (Hide below)

    Document Type Standard
    Publisher Federal Aviation Administration
    Status Superseded
    Superseded By

    Standards Referenced By This Book - (Show below) - (Hide below)

    FAA AC 20-170 : 2013 INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153
    FAA N 8110.110 : 2010 SOFTWARE APPROVAL GUIDE LINES, CONTINUED
    MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA

    Standards Referencing This Book - (Show below) - (Hide below)

    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 25-11 : 2014 ELECTRONIC FLIGHT DISPLAYS
    FAA 8110.4 : 2011 TYPE CERTIFICATION
    SAE ARP 4754 : 2010 GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
    RTCA DO 254 : 2000 DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
    SAE ARP 4761 : 1996 GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT
    FAA AC 23.1309-1 : 2011 SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
    FAA AC 21-40 : 2007 GUIDE FOR OBTAINING A SUPPLEMENTAL TYPE CERTIFICATE
    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 20-115 : 2017 AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
    FAA 8150.1 : 2017 TECHNICAL STANDARD ORDER PROGRAM
    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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