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  • MIL-H-8775 Revision D:1976

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR

    Available format(s):  PDF

    Superseded date:  01-07-1998

    Language(s): 

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Covers requirements common to most hydraulic components used in aeronautical hydraulic systems.

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

    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Superseded
    Superseded By

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

    DEFSTAN 00-970(PT1)SEC6/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/13(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    MIL C 25427 : A COUPLING ASSEMBLY, HYDRAULIC, SELF-SEALING, QUICK DISCONNECT
    MIL-V-29592 Base Document:1993 VALVE, AIR VENT, AUTOMATIC, HYDRAULIC, LOW PRESSURE TYPE II SYSTEMS, GENERAL SPECIFICATION FOR
    MIL V 81940 : B VALVE, SAMPLING AND BLEED, HYDRAULIC, TYPE LI SYSTEMS
    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
    DEFSTAN 00-970(PT1)SEC6/14(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    MIL-V-47308 Revision A:1991 VALVE, SERVO, HYDRAULIC FLOW CONTROL
    DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    MIL F 83861 : B FILTER ELEMENTS, NONCLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE, TYPE 1I, SYSTEMS GENERAL SPECIFICATION FOR
    DEFSTAN 00-970(PT7)SEC2/SUPP6/6(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F)
    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)/7(2011) : 2011 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)/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    MIL V 5523 : D VALVE, RELIEF, HYDRAULIC PRESSURE
    DEFSTAN 00-970(PT0)/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    MIL F 9490 : D FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    DEFSTAN 00-970(PT1)SEC6/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    MIL F 83870 : A FILTER ELEMENT, FLUID PRESSURE, TRANSMISSION, AIRCRAFT DISPOSABLE, 20 MICRON ABSOLUTE
    MIL-V-19067 Revision A:1957 VALVE, CHECK, CONTROLLABLE, HYDRAULIC, AIRCRAFT TYPE 11 SYSTEMS
    DEFSTAN 00-970(PT7)SEC2/SUPP6/5(2015) : INTERIM DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F)
    MIL-H-5440 Revision H:1993 HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR
    MIL-A-19736 Revision A:1960 AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR
    MIL-R-8931 Revision A:1994 RESERVOIRS, AIRCRAFT AND MISSILE, HYDRAULIC SEPARATED TYPE
    MIL-P-5994 Revision D:1972 PUMP, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY, GENERAL SPECIFICATION FOR
    MIL F 83860 : C FILTER ELEMENTS, NONCLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 MICRON ABSOLUTE, TYPE II, SYSTEMS, GENERAL SPECIFICATION FOR
    MIL V 19068 : A VALVE, SHUTTLE, HYDRAULIC, AIRCRAFT, TYPE 11 SYSTEMS
    MIL-F-24666 Base Document:1986 FILTER ELEMENT, SHIP FUEL SYSTEM PREFILTER, NONCLEANABLE, HIGH EFFICIENCY
    DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    MIL B 8075 : D BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF
    DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT
    SAE AS 838 : 2013 AIRCRAFT HYDRAULIC STARTER/PUMPS
    SAE AS 55151 : 2001 PUMP, HYDRAULIC, RAM, HAND DRIVEN
    SAE AS 25427 : 2015 COUPLING ASSEMBLY, HYDRAULIC, SELF-SEALING, QUICK DISCONNECT
    MIL F 5508 : B FUSE, AIRCRAFT AUTOMATIC QUANTITY MEASURING HYDRAULIC
    MIL-S-8812 Revision D:1975 STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR
    MIL-M-7997 Revision C:1981 MOTOR, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT GENERAL SPECIFICATION FOR
    DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    DEFSTAN 00-970(PT1)SEC6/6(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    SAE AS 4251 : 2013 COUPLING ASSEMBLIES, NON-LOCKING PROBE STYLE, SELF-ALIGNING, SELF-SEALING DISCONNECTS
    SAE AS 7997:1999 MOTORS, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT - GENERAL SPECIFICATION FOR
    MIL-R-5520 Revision C:1964 RESERVOIRS, AIRCRAFT, HYDRAULIC, NON-SEPARATED TYPE
    SAE AS 6026 : 2013 CONTROL UNIT, PRESSURE GENERATING, MANUALLY OPERATED, AIRCRAFT HYDRAULIC BRAKE SYSTEM
    SAE AS 1896 : 2013 COUPLING ASSEMBLY, SELF-SEALING, ONE SIDE ONLY, HYDRAULIC
    MIL-V-19069 Revision B:1986 Valve, Check, Hydraulic, Aircraft, Type II Systems
    MIL-P-19692 Revision E:1994 PUMPS, HYDRAULIC, VARIABLE FLOW, GENERAL SPECIFICATION FOR
    DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT
    MIL-T-18232 Revision B:1968 TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR
    MIL A 8897 : A ACCUMULATORS, HYDRAULIC CYLINDRICAL, 3,000 PSI AIRCRAFT TYPE 11 SYSTEMS
    MIL A 5503 : E ACTUATOR, AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR
    MIL A 5498 : D ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT
    MIL F 81836 : A SUPP 1 FILTER AND DISPOSABLE ELEMENT, FLUID PRESSURE, HYDRAULIC, 3 MICRON ABSOLUTE
    DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    MIL R 25534 : A NOTICE 1 ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR
    MIL-F-5504 Revision B:1958 Filters and Filter Elements, Fluid Pressure, Hydraulic Micronic Type
    MIL-T-25307 Revision D:1985 TRANSMITTER, PRESSURE, HYDRAULIC, TYPE MJ-1
    MIL R 25532 : A ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR
    MIL J 5513 : C JOINT, HYDRAULIC SWIVEL
    MIL-W-5013 Revision L:1991 WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR
    SAE AIR 4543 : 2017 AEROSPACE HYDRAULICS AND ACTUATION LESSONS LEARNED
    SAE AS 5994A:2000(S2013) PUMP UNITS, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY

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

    MS28772 Revision B:1971 PACKING D, RING, SHOCK STRUT
    MIL HDBK 5 : G_VOL2 METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES
    MS33540 Revision J:1986 SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR
    MIL-STD-129 Revision R:2014 Military Marking for Shipment and Storage
    MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL-STD-130 Revision N:2007 IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
    MIL F 81836 : A SUPP 1 FILTER AND DISPOSABLE ELEMENT, FLUID PRESSURE, HYDRAULIC, 3 MICRON ABSOLUTE
    MIL-H-25475 Revision B:1971 HYDRAULIC SYSTEM, MISSILE, DESIGN, INSTALLATION TESTS AND DATE REQUIREMENTS, GENERAL REQUIREMENTS FOR
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL I 6866 : B INSPECTION, PENETRANT METHOD OF
    NAS1638:2011 CLEANLINESS REQUIREMENTS OF PARTS USED IN HYDRAULIC SYSTEMS
    MS27595 Revision E:2006 RETAINER, PACKING BACKUP, CONTINUOUS RING, POLYTETRAFLUOROETHYLENE
    MS33515 Revision J:1973 FITTING END, STANDARD DIMENSIONS FOR BULKHEAD FLARELESS TUBE CONNECTIONS
    ASME B46.1 : 2009 SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY)
    MS28774 Revision M:2009 RETAINER, PACKING BACKUP, SINGLE TURN, POLYTETRAFLUOROETHYLENE
    MIL-STD-889 Revision C:2016 DISSIMILAR METALS
    MS28778 Revision C:1984 PACKING, PREFORMED, STRAIGHT THREAD TUBE FITTING BOSS
    MS28775 Revision E:1984 PACKING, PREFORMED, HYDRAULIC, PLUS 275 DEG. F. (O RING)
    MS33656 Revision J:1987 FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL
    QQ-C-320 Revision B:1974 CHROMIUM PLATING (ELECTRODEPOSITED)
    MS28782 Revision E:2006 RETAINER, PACKING, BACK-UP, TEFLON
    MIL C 38999 : J CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET THREADED & BREECH COUPLING) ENVIRONMENT RESISTANT, REMOVABLE CRIMP & HERMETIC SOLDER CONTACTS
    MIL-T-10727 Revision C:1989 TIN PLATING, ELECTRODEPOSITED OR HOT-DIPPED FOR FERROUS AND NONFERROUS METALS
    QQ-S-365 Revision D:1985 SILVER PLATING, ELECTRODEPOSITED, GENERAL REQUIREMENTS FOR
    MIL-G-5514 Revision G:1993 GLAND DESIGN, PACKINGS, HYDRAULIC GENERAL REQUIREMENTS FOR
    MS20995 Revision E:1974 WIRE, SAFETY OR LOCK
    MIL-R-8791 Revision D:1982 RETAINER, PACKING, HYDRAULIC, AND PNEUMATIC, TETRAFLUOROETHYLENE RESIN
    MIL H 83282 : C HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, AIRCRAFT, METRIC, NATO CODE NUMBER H 537
    MIL H 6083 : E HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION
    MIL-STD-143 Revision B:1969 STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
    MIL-C-83982 Base Document:1974 COMPOUND, SEALING, FLUID RESISTANT
    MIL-M-8609 Revision B:1965 MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    MIL-I-6868 Revision E:1976 INSPECTION PROCESS, MAGNETIC PARTICLE
    MIL C 5541 : E CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS
    MIL-S-8879 Revision C:1991 SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR
    MIL A 8625 : F ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
    MS21343 Base Document:1971 BOSS SPACING HYDRAULIC DESIGN STANDARD FOR
    MS28783 Revision F:2006 RING, GASKET, BACK-UP, PTFE
    MIL S 81733 : C SEALING AND COATING COMPOUND CORROSION INHIBITIVE
    MIL-STD-100 Revision G:1997 ENGINEERING DRAWINGS
    MIL-M-7969 Revision C:1965 Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for
    MIL-STD-490 Revision A:1985 SPECIFICATION PRACTICES
    MIL C 5015 : G CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR
    MIL-H-5440 Revision H:1993 HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR
    MIL H 5606 : G HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE
    MIL-STD-462 Revision D:1993 MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS
    AND10476 : 0002 WASHER - LIMITATIONS ON USAGE OF LOCK
    MIL C 26074 : E COATINGS, ELECTROLESS NICKEL, REQUIREMENTS FOR
    MIL-C-5501 Revision G:1989 CAP AND PLUG, PROTECTIVE, DUST AND MOISTURE SEAL
    QQ-P-416 Revision F:1991 PLATING, CADMIUM (ELECTRODEPOSITED)
    MIL-P-83461 Revision B:1980 PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, IMPROVED PERFORMANCE AT 275 DEGREES F (135 DEGREES C)
    FED-STD-791 Revision D:2007 TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS
    MS33514 Revision G:1990 FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (ASG)
    MIL G 81322 : E GREASE, AIRCRAFT, GENERAL PURPOSE, SIDE TEMPERATURE RANGE, NATO CODE NUMBER G-395
    MIL-F-27656 Revision C:1987 FILTER UNIT, FLUID, PRESSURE MXU-4O8/M, ABSOLUTE 5 MICRON, HYDRAULIC
    MIL-STD-785 Revision B:1980 RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION
    QQ-N-290 Revision A:1971 NICKEL PLATING (ELECTRODEPOSITED)
    MS33547 Revision C:1957 PIN, SPRING, FUNCTIONAL LIMITATIONS OF (ASG)
    AN6230 Revision 9:1982 GASKET "O"-RING HYDRAULIC
    MIL-HDBK-221 Base Document:1965 FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES
    MS21344 Revision A:2016 FITTING INSTALLATION OF FLARED TUBE STRAIGHT THREADED CONNECTORS DESIGN STANDARD FOR
    MIL-STD-463 Revision A:1977 DEFINITION AND SYSTEM OF UNITS, ELECTROMAGNETIC INTERFERENCE TECHNOLOGY
    MS21209 Revision E:1978 INSERT SCREW THREAD COARSE AND FINE SCREW LOCKING HELICAL COIL CRES
    MIL-STD-961 Revision E:2003 DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT
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