• ARINC 608A : 1993

    Current The latest, up-to-date edition.

    DESIGN GUIDANCE FOR AVIONICS TEST EQUIPMENT - PART 1: SYSTEM DESCRIPTION

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  15-01-1993

    Publisher:  Aeronautical Radio Inc.

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

    1.0 INTRODUCTION
    1.1 Purpose of This Document
    1.2 Advantages
    1.3 Objectives
    1.4 Goals
    1.5 Background
    1.6 Relationship to ARINC Specification 608
    1.7 Compatibility With Other Systems
    2.0 SYSTEM CONCEPT
    2.1 Introduction
    2.2 Test System Hardware
    2.3 Test System Software
    3.0 TEST SYSTEM FUNCTIONS
    3.1 Introduction
    3.2 Operator Interface
    3.3 Hardware Interface
    3.4 Automatic Test Control
    3.5 Manual Test Control
    3.6 Test Program Development
    4.0 TEST SYSTEM DESIGN GUIDELINES
    4.1 Introduction
    4.2 Test Control Computer and Operating System
    4.3 Test System Interfaces
    4.4 Switching
    4.5 Digital Test
    4.6 Radio Frequency (RF) Test
    4.7 Specialized Testing
    4.8 Test System Resources
    APPENDICES
    A Glossary
    B Example Software Architecture
    C Standard Interface Modules
    D Standard Interface Functional Description
    E Receiver Modules (No. 1 thru 21)
    F Standard Interface Mechanical Specification
    G Dynamic Digital Data Module
    H ATE Cabling and Grounding Guidelines
    I ARINC 629 Data Bus Testing
    J Test Unit Adapter (TUA) Identification
    K User-Defined Module

    Abstract - (Show below) - (Hide below)

    Defines standard avionics test system concept that will reduce the cost of test and repair of avionics equipment.

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

    Document Type Standard
    Publisher Aeronautical Radio Inc.
    Status Current

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

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