ARINC 777-2 : 2010
Current
The latest, up-to-date edition.
RECORDER INDEPENDENT POWER SUPPLY (RIPS)
Hardcopy , PDF
English
11-10-2010
1.0 INTRODUCTION AND DESCRIPTION
1.1 Purpose and Scope
1.2 Organization of this Document
1.3 Relationship to Other Documents
1.4 Functional Overview
1.5 Significance of Commentary, Attachments, and Appendices
2.0 INTERCHANGEABILITY STANDARDS
2.1 Interchangeability Objectives
2.2 Form Factor and Connector
2.3 Power
2.4 Standard Interwiring
2.5 Environmental Conditions
2.6 Cooling
2.7 Weight
2.8 Grounding and Bonding
3.0 SYSTEM DESIGN CONSIDERATIONS
3.1 General
3.2 Timings
3.3 Output Power
3.4 Output Control
3.5 Discrete Outputs
3.6 Relay 'Dry Contact' Outputs
3.7 Discrete Inputs
3.8 RIPS Bypass Diode
3.9 RIPS Input and Output Power Returns
3.10 Installation
4.0 PROVISIONS FOR TEST
4.1 Built-In Test Equipment
ATTACHMENTS
ATTACHMENT 1 - SYSTEM BLOCK DIAGRAMS
ATTACHMENT 2 - STANDARD INTERWIRING
ATTACHMENT 3 - CONNECTOR PIN FUNCTION
ATTACHMENT 5 - RIPS OUTLINE DRAWINGS
APPENDIX A - POLICY ON THE USE OF SHOULD AND SHALL
ARINC Standard - Errata Report
APIM
This document contains the physical form and fit dimensions, the electrical interface definition, and a description of the functions, operations, and interfaces of the Recorder Independent Power Supply (RIPS) for the Cockpit Voice Recorder (CVR) or crash survivable recorder units that combine voice with other recording functions.
DocumentType |
Standard
|
Pages |
54
|
PublisherName |
Aeronautical Radio Inc.
|
Status |
Current
|
ARINC 413A : 1976 | GUIDANCE FOR AIRCRAFT ELECTRICAL POWER UTILIZATION AND TRANSIENT PROTECTION |
ARINC 757A : 2011 SUPP 1 | COCKPIT VOICE RECORDER (CVR) |
ARINC 609 : 1987 | DESIGN GUIDANCE FOR AIRCRAFT ELECTRICAL POWER SYSTEMS |
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