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SAE ARP 5007 : 2012

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

DEVELOPMENT PROCESS - AEROSPACE FLY-BY-WIRE ACTUATION SYSTEM
Available format(s)

Hardcopy , PDF

Superseded date

10-17-2020

Language(s)

English

Published date

04-26-2012

FOREWORD
1. SCOPE
2. REFERENCES
3. SYSTEM DEVELOPMENT PHASES
4. SYSTEM REQUIREMENTS ANALYSIS
5. ELECTRONICS AND ACTUATOR REQUIREMENTS
6. PRELIMINARY DESIGN
7. DETAILED DESIGN
8. DEVELOPMENT/FABRICATION
9. ACTUATION SYSTEM INTEGRATION

Provides a description of a process for development of fly-by-wire actuation systems. Included are (1) the development of requirements for the servo-actuator hardware and the electronics hardware and software, (2) actuator and servo-electronics interface definitions and, (3) the required communications and interactions between the servo-actuator and the servo-electronics designers.

Committee
A-6A3
DocumentType
Standard
Pages
26
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

SAE AIR 4543/1A : 2017 AEROSPACE HYDRAULICS AND ACTUATION LESSONS LEARNED
SAE ARP 5724 : 2013 AEROSPACE - TESTING OF ELECTROMECHANICAL ACTUATORS, GENERAL GUIDELINES FOR

SAE AIR 4094 : 2016 AIRCRAFT FLIGHT CONTROL SYSTEMS DESCRIPTIONS
SAE ARP 4386 : 2010 TERMINOLOGY AND DEFINITIONS FOR AEROSPACE FLUID POWER, ACTUATION AND CONTROL TECHNOLOGIES
SAE AIR 4922A : 2015 PRIMARY FLIGHT CONTROL HYDRAULIC ACTUATION SYSTEM INTERFACE DEFINITION

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US$147.50
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