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ARINC 655 : 1999

Current
Current

The latest, up-to-date edition.

REMOTE DATA CONCENTRATOR (RDC) GENERIC DESCRIPTION
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

04-01-1999

1.0 Introduction
1.1 Purpose of this Document
1.2 Generic Description
1.3 Interoperability
1.4 Relationships to ARINC 651
1.5 Reference Documents
1.6 Regulatory Approval
2.0 Architectural Considerations
2.1 Introduction
2.2 Equipment Interoperability
2.3 Architecture Considerations
2.4 Architecture Tradeoffs
2.5 Hardware Architecture
2.6 Software Architecture
3.0 Functional Characteristics
3.1 Introduction
3.3 General Capabilities
3.4 Initialization
4.0 Physical Attributes
4.1 Introduction
4.2 Environmental Conditions
4.3 Cooling
4.4 Type, Size and Weight
4.5 Connectors
5.0 Electrical Interface
5.1 Introduction
5.2 Electrical Bonding and Grounding
5.3 Power
5.4 RDC Internal Discretes
5.5 Test and Maintenance Bus
5.6 Other Interfaces
5.7 Standard Interwiring
6.0 Data Bus and I/O Functional Interfaces
6.1 ARINC 629 Data Bus Interfaces
6.2 ARINC 429 Data Bus Interfaces
6.3 Discrete Input Resources Interface
6.4 Discrete Output Resources Interface
6.5 Analog Input Resources Interface
6.6 Analog Output Resources Interface
7.0 Supportability
7.1 Reliability
7.2 Maintainability
7.3 Testability
8.0 Software
8.1 Introduction
8.2 Software Development
8.3 Software Programming
Attachments
1. RDC - Interface Block Diagram
2. RDC - Configuration Examples
Appendices
A RDC Connector Definition
B Glossary

Gives guide for the design and implementation of a Remote Data Concentrator (RDC) in aircraft installations. Represents the consensus of airlines, airframe manufacturers and avionics suppliers that are involved in preparing this document.

DocumentType
Standard
Pages
65
PublisherName
Aeronautical Radio Inc.
Status
Current

MIL-W-22759 Revision E:1990 WIRE, ELECTRIC, FLUOROPOLYMER-INSULATED, COPPER OR COPPER ALLOY
ARINC 653 : 1997 SUPP 1 AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE
ARINC 608A : 1993 DESIGN GUIDANCE FOR AVIONICS TEST EQUIPMENT - PART 1: SYSTEM DESCRIPTION
ARINC 652 : 1993 GUIDANCE FOR AVIONICS SOFTWARE MANAGEMENT
ARINC 654 : 1994 ENVIRONMENTAL DESIGN GUIDELINES FOR INTEGRATED MODULAR AVIONICS PACKAGING AND INTERFACES
SAE ARP 4754 : 2010 GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
MIL C 17 : G CABLES, RADIO FREQUENCY, FLEXIBLE AND SEMIRIGID, GENERAL SPECIFICATION FOR
ARINC 629 : 90 SUPP 5 MULTI TRANSMITTER DATA BUS - TECHNICAL DESCRIPTION
SAE ARP 4761 : 1996 GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT
MIL-HDBK-217 Revision F:1991 RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT
MIL-STD-1344 Revision A:1977 TEST METHODS FOR ELECTRICAL CONNECTORS
ARINC 429 : 2001 ELECTRONIC DISKETTE COPY OF DATA LABELS IN MICROSOFT WORD AND EXCEL FORMATS
MIL-STD-1629 Revision A:1980 PROCEDURES FOR PERFORMING A FAILURE MODE, EFFECTS AND CRITICALITY ANALYSIS
ARINC 650 : 1994 INTEGRATED MODULAR AVIONICS PACKAGING AND INTERFACES
ARINC 609 : 1987 DESIGN GUIDANCE FOR AIRCRAFT ELECTRICAL POWER SYSTEMS

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