ARINC 728 : 1979
Current
The latest, up-to-date edition.
AVIONICS REFRIGERATION COOLING SYSTEM
Hardcopy , PDF
English
31-10-1979
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1.0 GENERAL CONSIDERATIONS
1.1 Background
1.2 Objective
1.3 Scope
1.4 Nomenclature and Definitions
1.5 Applicable Documents
2.0 INTERCHANGEABILITY
2.1 Configuration
2.2 Capacity
2.3 Form Factor
2.4 Interwiring
2.5 Power
2.6 Environmental Conditions
2.7 System Components Other than ARU
2.8 Grounding and Bonding
2.9 Annunciation
2.10 ARU Orientation
3.0 DESIGN CRITERIA AND GUIDANCE
3.1 General
3.2 Description
3.3 Temperature
3.4 Performance
3.5 Interfaces
3.6 Maintainability
3.7 Qualification Tests
ATTACHMENTS
1 Notes Applicable to Standard Interwiring
2 Standard Interwiring
3 ARCS System Simplified Schematic
4 (ARU Envelope) Diagram
5 Environmental Test Categories
APPENDICES
1 Chronology and Bibliography
Gives: 1) A total system description, 2) The mechanical, electrical, environmental, and pneumatic interfaces between a 4 ton avionics refrigeration cooling unit and any aircraft (excluding fans), and 3) System Interwiring for electrical signaling.
| DocumentType |
Standard
|
| Pages |
18
|
| PublisherName |
Aeronautical Radio Inc.
|
| Status |
Current
|
| SAE AIR64B | ELECTRICAL AND ELECTRONIC EQUIPMENT COOLING IN COMMERCIAL TRANSPORTS |
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