Table of Contents

1 Scope
  1.1 Purpose
  1.2 Product Classification
  1.3 Field of Application
2 References
  2.1 Applicable Documents
  2.2 Definitions and Abbreviations
3 Technical Requirements
  3.1 General
  3.2 Design
  3.3 Processes, Construction/Assembly Requirements
  3.4 Performance
  3.5 Installation/Maintenance Requirements
  3.6 Documentation
4 Quality Assurance Provisions
  4.1 General
  4.2 Test Requirements
  4.3 Classification of Tests
  4.4 Test Procedures
  4.5 Test Conditions
  4.6 Acceptance Test Methods
  4.7 Preproduction Test Methods
  4.8 Qualification Test Methods
  4.9 Test Reports, Design Changes and Approval Data
  4.10 Preproduction and Qualification Test Failures
5 Preparation For Delivery
  5.1 Preservation For Delivery
  5.2 Packing
  5.3 Marking of Shipment
6 Notes
Appendix A Technical Notes and Comments
Figure
Tables

Abstract

Specifies a framework and suggested procedures or values for requirements for the design, performance, and test of hydraulically powered servo actuators for use in aircraft flight control systems.

General Product Information

Published
Document Type	Standard
Status	Current
Publisher	SAE International
Pages
ISBN
Committee	A-6