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  • SAE ARP 1281 : 2002

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    ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR

    Available format(s): 

    Language(s): 

    Published date:  12-09-2002

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

    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 - (Show below) - (Hide below)

    This aerospace recommended practice provides a framework and suggested procedures or values for requirements for the design, performance, and test of hydraulically powered servoactuators for use in aircraft flight control systems.

    General Product Information - (Show below) - (Hide below)

    Committee A-6B1
    Document Type Revision
    Publisher SAE International
    Status Current

    Standards Referenced By This Book - (Show below) - (Hide below)

    ISO 8625-1:2018 Aerospace — Fluid systems — Vocabulary — Part 1: General terms and definitions related to pressure
    SAE ARP 4493 : 2013 AEROSPACE - DIRECT DRIVE SERVOVALVES
    SAE ARP 4925 : 2014 AEROSPACE DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT HELICOPTER HYDRAULIC SYSTEMS
    SAE ARP 94910 : 2012 AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR
    SAE AS 94900 : 2007 AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR
    17/30342695 DC : 0 BS ISO 8625-1 - AEROSPACE - FLUID SYSTEMS - VOCABULARY - PART 1: GENERAL TERMS AND DEFINITIONS RELATED TO PRESSURE
    MIL-DTL-9490 Revision E:2008 FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    SAE ARP 5724 : 2013 AEROSPACE - TESTING OF ELECTROMECHANICAL ACTUATORS, GENERAL GUIDELINES FOR
    SAE AIR 4982 : 2014 AEROSPACE FLY-BY-LIGHT ACTUATION SYSTEMS
    SAE ARP 4752 : 2013 AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS
    SAE ARP 988 : 2016 ELECTROHYDRAULIC MECHANICAL FEEDBACK SERVOACTUATORS

    Standards Referencing This Book - (Show below) - (Hide below)

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    SAE AS 8976 : 2012 BEARINGS, PLAIN, SELF-ALIGNING, ALL METAL, GENERAL SPECIFICATION FOR
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    SAE AMS QQ C 320 : 2000 CHROMIUM PLATING (ELECTRODEPOSITED)
    MIL STD 130 : N IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
    MIL-PRF-46170 Revision E:2013 HYDRAULIC FLUID, RUST INHIBITED, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, NATO CODE NO. H-544
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    NASM20995:2012 WIRE, SAFETY OR LOCK
    SAE AS 8879 : 2004 SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER
    SAE AS 39901 : 2012 BEARINGS, ROLLER, NEEDLE, AIRFRAME, ANTIFRICTION, INCH
    MIL STD 882 : E STANDARD PRACTICE FOR SYSTEM SAFETY
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    MIL A 8625 : F ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
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    ASTM E 1444 : 2005 Standard Practice for Magnetic Particle Testing
    MS 21343 : 0 BOSS SPACING HYDRAULIC DESIGN STANDARD FOR
    SAE AS 8775 : 1998 HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR
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    MIL STD 100 : G ENGINEERING DRAWINGS
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    SAE AS 33649 : 2000 BOSSES, FLUID CONNECTION, INTERNAL STRAIGHT THREAD
    NASM24665:2016 PIN, COTTER (SPLIT)
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