Name: ARINC 608A : 1993
Brand: ARINC
Price: 403.00 USD

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

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-15-1993

Publisher

Aeronautical Radio Inc.

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

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

DocumentType	Standard
Pages	171
PublisherName	Aeronautical Radio Inc.
Status	Current

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