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  • SAE AS 94900 : 2007

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR

    Available format(s): 

    Superseded date:  19-10-2019

    Language(s): 

    Published date:  01-01-2007

    Publisher:  SAE International

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

    1. SCOPE
    2. REFERENCES
    3. REQUIREMENTS
    4. QUALITY ASSURANCE PROVISIONS

    Abstract - (Show below) - (Hide below)

    Establishes general performance, design, test, development and quality assurance requirements for the Flight Control Systems of military piloted aircraft. Flight Control Systems (FCS) include all components used to transmit flight control commands from the pilot or other sources to appropriate force and moment producers.

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

    Committee A-6A3
    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By
    Supersedes

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

    SAE ARP 94910 : 2012 AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR
    SAE AIR 5992 : 2015 DESCRIPTIONS OF SYSTEMS INTEGRATION TEST RIGS (IRON BIRDS) FOR AEROSPACE APPLICATIONS
    SAE ARP 5812 : 2017 ACTUATORS, LINEAR MECHANICAL, GENERAL SPECIFICATION GUIDE
    MIL HDBK 516 : C AIRWORTHINESS CERTIFICATION CRITERIA
    SAE ARP 5770 : 2012 MECHANICAL CONTROL DESIGN GUIDE
    SAE ARP 5764 : 2013(R2018) AEROSPACE ACTIVE INCEPTOR SYSTEMS FOR AIRCRAFT FLIGHT AND ENGINE CONTROLS

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

    ASTM B 438/B438M : 2005 Specification for Bronze Powder Metallurgy (P/M) Bearing (Oil-Impregnated)
    MIL A 8865 : B AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS
    MIL-DTL-18375H: 2005 WIRE ROPE, FLEXIBLE, CORROSION-RESISTING, NONMAGNETIC, FOR AIRCRAFT CONTROL
    MIL PRF 7958 : D PUSH-PULL CONTROLS, FLEXIBLE AND RIGID
    MIL I 8500 : D INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES
    MIL STD 1530 : D AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP)
    SAE AS 8976 : 2012 BEARINGS, PLAIN, SELF-ALIGNING, ALL METAL, GENERAL SPECIFICATION FOR
    SAE AS 15002 : 2010 FITTING, LUBRICATION, HYDRAULIC, SURFACE CHECK, STRAIGHT THREADS, STEEL, TYPE 2
    MS 33736 : D TURNBUCKLE ASSEMBLIES, CLIP LOCKING OF
    MIL STD 704 : F AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    SAE AS 81820 : 2014 BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, LOW SPEED OSCILLATION
    MIL STD 130 : N IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
    MIL H 8890 : 0 HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG]
    IEEE 12207.1 : 1997 INDUSTRY IMPLEMENTATION OF INTERNATIONAL STANDARD ISO/IEC 12207:1995 (ISO/IEC 12207) STANDARD FOR INFORMATION TECHNOLOGY - SOFTWARE LIFE CYCLE PROCESSES - LIFE CYCLE DATA
    MIL DTL 781 : J TERMINAL, WIRE ROPE SWAGING, GENERAL SPECIFICATION FOR
    NASM 33588 : 0 NUT, SELF-LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR
    SAE ARP 1281 : 2002 ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR
    SAE AS 7949 : 2004 BEARINGS, BALL, AIRFRAME, ANTIFRICTION, GENERAL STANDARD
    MIL DTL 83420 : P WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
    MIL STD 810 : G ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL H 8891 : A HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR
    MIL A 87229 : 0 AUXILIARY POWER SYSTEMS, AIRBORNE
    SAE ARP 4754 : 2010 GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
    MIL DTL 6193 : E JOINTS, UNIVERSAL, PLAIN, LIGHT AND HEAVY DUTY, GENERAL SPECIFICATION FOR
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    MIL A 8870 : C AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
    SAE AMS A 22771 : 2012 ALUMINUM ALLOY FORGINGS, HEAT TREATED
    MIL HDBK 781 : A RELIABILITY TEST METHODS, PLANS, AND ENVIRONMENTS FOR ENGINEERING DEVELOPMENT, QUALIFICATION AND PRODUCTION
    MIL M 38510 : J MICROCIRCUITS, SPECIFICATION FOR
    SAE AS 5440 : 2011 HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR
    MIL HDBK 454 : B GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT
    SAE AS 6038 : 2011 BEARINGS, BALL, BELLCRANK, ANTIFRICTION, AIRFRAME
    SAE ARP 4493 : 2013 AEROSPACE - DIRECT DRIVE SERVOVALVES
    MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
    MIL STD 7080 : 0 SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT
    SAE AS 56761 : 1999 SPLICING; CABLE TERMINAL, PROCESS FOR, AIRCRAFT
    NASM 33540 : 2003 SAFETY WIRING, SAFETY CABLING, COTTER PINNING, GENERAL PRACTICES FOR
    SAE ARP 4761 : 1996 GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT
    MIL STD 464 : C ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
    MIL DTL 6117 : L WIRE ROPE ASSEMBLIES, AVIATION, SWAGED TYPE
    SAE AMS STD 2175 : 1998 CASTINGS, CLASSIFICATION AND INSPECTION OF
    SAE AS 7997A : 1999(S2018) MOTORS, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT - GENERAL SPECIFICATION FOR
    MIL PRF 5503 : G ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR
    JSSG 2001 : B AIR VEHICLE
    MIL STD 882 : E STANDARD PRACTICE FOR SYSTEM SAFETY
    SAE AS 6039 : 2009 BEARINGS, BALL, ROD END, DOUBLE ROW, SELF-ALIGNING
    MIL M 8609 : B MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL STD 461 : G REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    NASM 33602 : 0 BOLTS, SELF-RETAINING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY, DESIGN AND USAGE REQUIREMENTS FOR
    MIL STD 203 : G AIRCREW STATION CONTROLS AND DISPLAYS FOR FIXED WING AIRCRAFT
    IEEE 12207.0 : 1996 INTERNATIONAL STANDARD ISO/IEC 12207:1995 (ISO/IEC 12207) STANDARD FOR INFORMATION TECHNOLOGY - SOFTWARE LIFE CYCLE PROCESSES
    MIL STD 1773 : 0 FIBER OPTICS MECHANIZATION OF AN AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS
    MIL DTL 8878 : L TURNBUCKLES, POSITIVE SAFETYING, GENERAL SPECIFICATION FOR
    MIL A 8867 : C AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
    MIL-DTL-7034F:2005 PULLEYS, GROOVE, ANTIFRICTION BEARING, GREASE LUBRICATED, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL A 8861 : B AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
    FAA AC 120-29 : 0 CRITERIA FOR APPROVAL OF CATEGORY 1 AND CATEGORY 2 WEATHER MINIMA FOR APPROACH
    SAE ARP 4895 : 2006 FLIGHT CONTROL ACTUATORS - DYNAMIC SEALS, COLLECTION OF DUTY CYCLE DATA
    SAE AS 8775 : 1998 HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR
    SAE AS 35411 : 2010 FITTINGS, LUBRICATION
    SAE ARP 988 : 2016 ELECTROHYDRAULIC MECHANICAL FEEDBACK SERVOACTUATORS
    MIL S 8512 : D SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF
    SAE AS 50881 : 2015 WIRING AEROSPACE VEHICLE
    MIL M 7969 : C MOTOR, ALTERNATING CURRENT, 400 CYCLE, 115/200 VOLT SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL STD 1472 : G HUMAN ENGINEERING
    NASM 24665 : 0 PIN, COTTER (SPLIT)
    SAE AMS F 7190 : 2016 FORGING, STEEL, FOR AIRCRAFT/AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS
    MIL HDBK 838 : 0 LUBRICATION OF MILITARY EQUIPMENT
    SAE ARP 4386 : 2010 TERMINOLOGY AND DEFINITIONS FOR AEROSPACE FLUID POWER, ACTUATION AND CONTROL TECHNOLOGIES
    ARINC 429 : 2001 ELECTRONIC DISKETTE COPY OF DATA LABELS IN MICROSOFT WORD AND EXCEL FORMATS
    MIL HDBK 470 : A DESIGNING AND DEVELOPING MAINTAINABLE PRODUCTS AND SYSTEMS - VOLUME 1
    MIL STD 202 : H ELECTRONIC AND ELECTRICAL COMPONENT PARTS
    SAE ARP 4058 : 2007 GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS
    MIL HDBK 516 : C AIRWORTHINESS CERTIFICATION CRITERIA
    NASM 15981 : 0 FASTENERS, EXTERNALLY THREADED, SELF-LOCKING DESIGN AND USAGE LIMITATIONS FOR
    SAE ARP 490 : 2008 ELECTROHYDRAULIC SERVOVALVES
    IEEE 12207.2 : 1997
    JSSG 2006 : 0 JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
    SAE AIR 1083 : 2012 AIRBORNE HYDRAULIC AND CONTROL SYSTEM SURVIVABILITY FOR MILITARY AIRCRAFT
    SAE AS 5643 : 2016 IEEE-1394B INTERFACE REQUIREMENTS FOR MILITARY AND AEROSPACE VEHICLE APPLICATIONS
    MIL A 8860 : B AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
    MIL STD 1553 : B DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA
    MIL-C-81774A:1973 CONTROL PANEL, AIRCRAFT, GENERAL REQUIREMENTS FOR
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