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  • MIL DTL 9490 : E

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    FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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

    1. SCOPE
    2. APPLICABLE DOCUMENTS
    3. REQUIREMENTS
    4. VERIFICATION
    5. PACKAGING
    6. NOTES
    ALPHABETICAL INDEX

    Abstract - (Show below) - (Hide below)

    Specifies general performance, design, develop, and quality assurance requirements for the flight control systems of manned piloted aircraft.

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

    Committee FSC 15GP
    Development Note Inactive for New Design. Supersedes MIL F 9490 (D). (05/2008)
    Document Type Standard
    Product Note NEW CHILD NOT 1 2019 IS NOW ADDED
    Publisher US Military Specs/Standards/Handbooks
    Status Current

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

    DEFSTAN 00-970(PT1)SEC3/15(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE
    DEFSTAN 00-970(PT1)SEC3/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE
    DEFSTAN 00-970(PT1)SEC3/13(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE
    DEFSTAN 00-970(PT1)SEC3/14(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE

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

    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
    SAE AMS A 21180 : 2011 ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH
    SAE AMS 5676 : 2011 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, WELDING WIRE, 80NI - 20CR
    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
    MIL F 8785 : C FLYING QUALITIES OF PILOTED AIRPLANES
    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]
    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 AMS 2175 : 2010 CASTINGS, CLASSIFICATION AND INSPECTION OF
    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 M 7997 : C MOTOR, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT GENERAL SPECIFICATION FOR
    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
    DOT/FAA/AR-MMPDS-01 : 20030131 METALLIC MATERIALS PROPERTIES DEVELOPMENT AND STANDARDIZATION (MMPDS)
    MIL DTL 6193 : E JOINTS, UNIVERSAL, PLAIN, LIGHT AND HEAVY DUTY, GENERAL SPECIFICATION FOR
    MIL A 8870 : C AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
    SAE AMS A 22771 : 2012 ALUMINUM ALLOY FORGINGS, HEAT TREATED
    MIL T 5677 : B THIMBLE, WIRE CABLE, AIRCRAFT
    MIL M 38510 : J MICROCIRCUITS, SPECIFICATION FOR
    SAE AS 5440 : 2011 HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR
    NASM 25049 : REV 1 KNOBS, CONTROL, ELECTRONIC EQUIPMENT, GENERAL SPECIFICATION FOR
    MIL HDBK 454 : B GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT
    SAE AS 6038 : 2011 BEARINGS, BALL, BELLCRANK, ANTIFRICTION, AIRFRAME
    MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
    MIL STD 7080 : 0 SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT
    SAE AMS 4965 : 2014 TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL 4.0V, SOLUTION HEAT TREATED AND AGED
    SAE AS 56761 : 1999 SPLICING; CABLE TERMINAL, PROCESS FOR, AIRCRAFT
    NASM 33540 : 2003 SAFETY WIRING, SAFETY CABLING, COTTER PINNING, GENERAL PRACTICES FOR
    MIL STD 464 : C ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
    MIL DTL 6117 : L WIRE ROPE ASSEMBLIES, AVIATION, SWAGED TYPE
    MIL PRF 5503 : G ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR
    SAE AS 8879 : 2004 SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER
    MS 33572 : C INSTRUMENT, PILOT, FLIGHT, BASIC, STANDARD ARRANGEMENT FOR HELICOPTERS
    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
    SAE ARP 1961 : 2016 GEARBOX - AIRFRAME MOUNTED ACCESSORY
    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 AS 8775 : 1998 HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR
    MIL A 8866 : C AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
    SAE AS 35411 : 2010 FITTINGS, LUBRICATION
    SAE ARP 988 : 2016 ELECTROHYDRAULIC MECHANICAL FEEDBACK SERVOACTUATORS
    SAE AS 50881 : 2015 WIRING AEROSPACE VEHICLE
    MIL M 7969 : C MOTOR, ALTERNATING CURRENT, 400 CYCLE, 115/200 VOLT SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR
    JSSG 2009 : A AIR VEHICLE SUBSYSTEMS (JOINT SERVICE SPECIFICATION GUIDE)
    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
    NASM 15981 : 0 FASTENERS, EXTERNALLY THREADED, SELF-LOCKING DESIGN AND USAGE LIMITATIONS FOR
    SAE ARP 490 : 2008 ELECTROHYDRAULIC SERVOVALVES
    MIL P 8564 : D PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG]
    JSSG 2006 : 0 JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
    MIL HDBK 17/1 : F COMPOSITE MATERIALS HANDBOOK - VOLUME 1: POLYMER MATRIX COMPOSITES GUIDELINES FOR CHARACTERIZATION OF STRUCTURAL MATERIALS
    MIL A 8860 : B AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
    MIL STD 1553 : B DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA
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