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  • MIL H 8891 : A

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    HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR

    Available format(s):  Hardcopy, PDF

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    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Covers design and installation requirements for manned flight vehicle hydraulic systems.

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

    Committee FSC 1650
    Development Note A NOTICE 1 - Notice of Inactivation for New Design. A NOTICE 2 - Notice of Validation but remains Inactive for New Design. (02/2008)
    Document Type Standard
    Product Note New child NOT 3 2019 is now added
    Publisher US Military Specs/Standards/Handbooks
    Status Current

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

    SAE ARP 5794 : 2014 CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD
    DEFSTAN 00-970(PT0)/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/14(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/13(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    DEFSTAN 00-970(PT0)/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    MIL H 5440 : H HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR
    MIL R 8931 : A RESERVOIRS, AIRCRAFT AND MISSILE, HYDRAULIC SEPARATED TYPE
    MIL P 5994 : D PUMP, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY, GENERAL SPECIFICATION FOR
    MIL T 5522 : D TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
    MIL S 8512 : D SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF
    MIL H 8890 : 0 HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG]
    MIL B 8075 : D BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF
    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
    SAE AIR 5992 : 2015 DESCRIPTIONS OF SYSTEMS INTEGRATION TEST RIGS (IRON BIRDS) FOR AEROSPACE APPLICATIONS
    SBAC TS 103 : 2 RECOMMENDATIONS FOR DESIGN CONSIDERATIONS FOR AIRCRAFT HYDRAULIC SYSTEMS
    MIL S 8812 : D STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR
    MIL P 19692 : E PUMPS, HYDRAULIC, VARIABLE FLOW, GENERAL SPECIFICATION FOR
    MIL I 18373 : B INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF
    SAE AS 19692 : 2016 AEROSPACE - MILITARY TYPE VARIABLE DELIVERY, PRESSURE COMPENSATED HYDRAULIC PUMP
    MIL DTL 9490 : E FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    DIN 65178-1:1985-12 AEROSPACE; CONFIGURATION AND INSTALLATION OF FLUID PIPELINES; SURVEY AND DEFINITIONS
    SAE AS 5994 : 2013 PUMP UNITS, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY

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

    MIL T 5522 : D TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
    MIL V 81940 : B VALVE, SAMPLING AND BLEED, HYDRAULIC, TYPE LI SYSTEMS
    MIL F 8785 : C FLYING QUALITIES OF PILOTED AIRPLANES
    MIL H 8890 : 0 HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG]
    MIL T 6845 : D TUBING, STEEL, CORROSION-RESISTANT (304) AEROSPACE VEHICLE HYDRAULIC SYSTEM 1/8 HARD CONDITION
    MIL M 7997 : C MOTOR, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT GENERAL SPECIFICATION FOR
    SAE ARP 243 : 1993 NOMENCLATURE, AIRCRAFT HYDRAULIC AND PNEUMATIC SYSTEMS
    MIL B 8584 : C BRAKE SYSTEMS, WHEEL, AIRCRAFT, DESIGN OF
    AN 929 : 0014 CAP INSERT, ASSEMBLY, PRESSURE SEAL, FLARED TUBE FITTING
    SAE AIR 1362 : 2016 AEROSPACE HYDRAULIC FLUIDS PHYSICAL PROPERTIES
    MS 33656 : J FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL
    MIL P 5994 : D PUMP, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY, GENERAL SPECIFICATION FOR
    MIL F 9490 : D FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    SAE ARP 994 : 2016 DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS
    MIL V 25675 : B VALVE, CHECK, MINIATURE, HYDRAULIC, AIRCRAFT AND MISSILE
    MS 33583 : C TUBING END, DOUBLE FLARE, STANDARD DIMENSIONS FOR
    MS 33584 : C TUBING END, STANDARD DIMENSIONS FOR FLARED
    MIL F 8815 : D FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC LINE, 15 MICRON ABSOLUTE AND 5 MICRON ABSOLUTE, TYPE 11 SYSTEMS; GENERAL SPECIFICATION FOR
    SAE AS 1290 : 2011 GRAPHIC SYMBOLS FOR AIRCRAFT HYDRAULIC AND PNEUMATIC SYSTEMS
    SAE ARP 584D : 2012 COILED TUBING - CORROSION RESISTANT STEEL, HYDRAULIC APPLICATIONS, AEROSPACE
    MIL P 19692 : E PUMPS, HYDRAULIC, VARIABLE FLOW, GENERAL SPECIFICATION FOR
    MS 33611 : A TUBE BEND RADII
    MIL G 8348 : H GAGE, ASSEMBLIES, AIR PRESSURE, DIAL INDICATING CHUCK TYPE SELF CONTAINED
    MIL H 5440 : H HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR
    MIL R 8931 : A RESERVOIRS, AIRCRAFT AND MISSILE, HYDRAULIC SEPARATED TYPE
    MIL C 85052 : A CLAMP LOOP, CUSHION, GENERAL SPECIFICATION FOR
    FED STD 791 : D TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS
    MIL F 18372 : 0 FLIGHT CONTROL SYSTEMS, DESIGN, INSTALLATION AND TEST OF, AIRCRAFT (GENERAL SPECIFICATION FOR)
    MIL STD 1247 : D MARKINGS, FUNCTIONS AND HAZARDS DESIGNATIONS OF HOSE, PIPE, AND TUBE LINES FOR AIRCRAFT MISSILE, AND SPACE SYSTEMS
    MIL B 5087 : B BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
    MIL W 5088 : L WIRING, AEROSPACE VEHICLE
    AN 6240 : 0002 FILTER - HYDRAULIC REPLACEABLE ELEMENT VENT TYPE
    MS 21344 : A FITTING INSTALLATION OF FLARED TUBE STRAIGHT THREADED CONNECTORS DESIGN STANDARD FOR
    MIL F 7179 : G FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM
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