ARINC 655 : 1999
Current
The latest, up-to-date edition.
REMOTE DATA CONCENTRATOR (RDC) GENERIC DESCRIPTION
Hardcopy , PDF
English
05-04-1999
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 ARP4754A | 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 ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING 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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