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  • MIL-H-5440 Revision H:1993

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR

    Available format(s):  PDF

    Superseded date:  01-04-1998

    Language(s): 

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Gives requirements for types I and II hydraulic systems as follows; -54deg to +71degC (-65deg to +160degF), and -54deg to +135degC (-65deg to +275degF) temperature range.

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

    Committee FSC 1650
    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    Status Superseded
    Superseded By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
    MIL-I-83294 Base Document:1971 INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR
    DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    MIL P 5516 : C PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, 160 DEGREES F
    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
    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)
    MIL-C-8603 Revision B:1984 CLAMPS, LOOP TYPE, AND STRAPS, SUPPORT
    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
    MIL-H-8775 Revision D:1976 HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR
    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
    MIL F 5508 : B FUSE, AIRCRAFT AUTOMATIC QUANTITY MEASURING HYDRAULIC
    DEFSTAN 00-970(PT1)SEC6/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    MIL-H-8891 Revision A:1978 HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR
    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-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 V 6164 : E VALVE, AIRCRAFT, AIR HIGH PRESSURE
    MIL-T-5522 Revision D:1975 TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
    MIL-S-8512 Revision D:1974 SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF
    MIL-T-26017 Revision C:1972 TEST STAND, HYDRAULIC SYSTEM COMPONENTS, TYPE MK-3A (STAND, TEST, AIRCRAFT HYDRAULIC SYSTEM, ELECTRIC MOTOR DRIVEN, TYPE MK-3A)
    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 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 AIR 4713 : 2013 AEROSPACE - CHLORINATED SOLVENT CONTAMINATION OF MIL-H-5606/MIL-H-83282 VEHICLE HYDRAULIC SYSTEMS
    SAE AS 5994A:2000(S2013) PUMP UNITS, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY
    SAE AIR 4922A : 2015 PRIMARY FLIGHT CONTROL HYDRAULIC ACTUATION SYSTEM INTERFACE DEFINITION
    SBAC TS 103 : 2 RECOMMENDATIONS FOR DESIGN CONSIDERATIONS FOR AIRCRAFT HYDRAULIC SYSTEMS
    MIL-V-5527 Revision A:1951 VALVE, AIRCRAFT, HYDRAULIC THERMAL EXPANSION RELIEF
    MIL-S-8812 Revision D:1975 STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS 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
    MIL-T-7081 Revision D:1965 TUBE, ALUMINUM ALLOY, SEAMLESS, ROUND, DRAWN, 6061, AIRCRAFT HYDRAULIC QUALITY
    MIL-I-8673 Base Document:1955 INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS
    MIL-P-19692 Revision E:1994 PUMPS, HYDRAULIC, VARIABLE FLOW, GENERAL SPECIFICATION FOR
    MIL-F-5509 Revision D:1978 FITTING, FLARED TUBE, FLUID CONNECTION
    MIL I 18373 : B INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF
    MIL PRF 46821 : C LOADER-TRANSPORTER, GUIDED MISSILE - XM501E3 (IMPROVED HAWK)
    MIL-R-5520 Revision C:1964 RESERVOIRS, AIRCRAFT, HYDRAULIC, NON-SEPARATED TYPE
    MIL-P-5238 Revision C:1974 PUMP, CENTRIFUGAL, FUEL BOOSTER, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-P-87175 Base Document:1982 PACKING, PREFORMED, PETROLEUM, HYDRAULIC FLUID RESISTANT, PHOSPHONITRILIC FLUOROELASTOMER
    DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    SAE AS 6026 : 2013 CONTROL UNIT, PRESSURE GENERATING, MANUALLY OPERATED, AIRCRAFT HYDRAULIC BRAKE SYSTEM
    MIL-V-19069 Revision B:1986 Valve, Check, Hydraulic, Aircraft, Type II Systems
    SAE AS 1896 : 2013 COUPLING ASSEMBLY, SELF-SEALING, ONE SIDE ONLY, HYDRAULIC
    DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT
    MIL-W-5013 Revision L:1991 WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-DTL-46821 Revision D:1998 LOADER-TRANSPORTER, GUIDED MISSILE: XM501E3 (IMPROVED HAWK)
    SAE ARP 1897 : 2013 CLAMP SELECTION AND INSTALLATION GUIDE
    SAE AS 25427 : 2015 COUPLING ASSEMBLY, HYDRAULIC, SELF-SEALING, QUICK DISCONNECT
    MIL A 5503 : E ACTUATOR, AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR
    MIL-P-83461 Revision B:1980 PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, IMPROVED PERFORMANCE AT 275 DEGREES F (135 DEGREES C)
    MIL A 5498 : D ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT
    DIN 9370:1985-04 AEROSPACE; TUBES; CLASSIFICATION, PRESSURE TERMS, CALCULATION AND DESIGN CRITERIA
    DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DIN 65178-1:1985-12 AEROSPACE; CONFIGURATION AND INSTALLATION OF FLUID PIPELINES; SURVEY AND DEFINITIONS
    MIL R 25532 : A ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR
    MIL-C-18244 Revision A:1962 CONTROL AND STABILIZATION SYSTEMS, AUTOMATIC, PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    SAE ARP 4943 : 2008 GROUND SUPPORT EQUIPMENT HYDRAULIC SYSTEMS, DESIGN AND INSTALLATION, RECOMMENDED PRACTICES FOR
    SAE AIR 4543 : 2017 AEROSPACE HYDRAULICS AND ACTUATION LESSONS LEARNED
    SAE AS 838 : 2013 AIRCRAFT HYDRAULIC STARTER/PUMPS

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

    MIL-T-5522 Revision D:1975 TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
    MIL-R-83248 Revision C:1994 RUBBER, FLUOROCARBON ELASTOMER, HIGH TEMPERATURE, FLUID, AND COMPRESSION SET RESISTANT
    SAE AS 4396 : 2013 FITTING END, BULKHEAD, FLARED TUBE CONNECTION, DESIGN STANDARD
    MIL F 83296 : 0 FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, HIGH PRESSURE (3,000 PSI HYDRAULIC AND PNEUMATIC)
    MIL V 81940 : B VALVE, SAMPLING AND BLEED, HYDRAULIC, TYPE LI SYSTEMS
    SAE ARP 603 : 1985 IMPULSE TESTING OF HYDRAULIC HOSE, TUBING, AND FITTING ASSEMBLIES
    MIL H 46170 : B HYDRAULIC FLUID, RUST INHIBITED, FIRE-RESISTANT, SYNTHETIC HYDROCARBON BASE
    MIL-F-8785 Revision C:1980 FLYING QUALITIES OF PILOTED AIRPLANES
    MIL F 81836 : A SUPP 1 FILTER AND DISPOSABLE ELEMENT, FLUID PRESSURE, HYDRAULIC, 3 MICRON ABSOLUTE
    SAE AS 1975 : 2016 Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems
    MIL-STD-1844 Base Document:1984 GAS CHROMATOGRAPHY METHOD FOR DETERMINATION OF TRACE CHLORINATED SOLVENTS IN HYDRAULIC FLUID
    MIL H 83298 : A HOSE, TETRAFLUOROETHYLENE, HIGH TEMPERATURE, HIGH PRESSURE (3000 PSI) HYDRAULIC AND PNEUMATIC
    SAE ARP 4146D : 2012 COILED TUBING - TITANIUM ALLOY, HYDRAULIC APPLICATIONS, AEROSPACE
    MIL-T-6845 Revision D:1985 TUBING, STEEL, CORROSION-RESISTANT (304) AEROSPACE VEHICLE HYDRAULIC SYSTEM 1/8 HARD CONDITION
    SAE ARP 4553 : 2008 AEROSPACE - ACCUMULATOR, HYDRAULIC, SELF-DISPLACING
    SAE AS 4201 : 1998 PORT - RING LOCKED FLUID CONNECTION TYPE, 8000 PSI DESIGN STANDARD
    MIL H 27267 : B HOSE TETRAFLUOROETHYLENE, HIGH TEMPERATURE, MEDIUM PRESSURE
    MIL-C-85449-1 Revision B:1987 CLAMP ASSEMBLY, SADDLE TYPE, CUSHIONED, NBR RUBBER, 321 CRES, 275 DEG. F, FUEL RESISTANT, GENERAL PURPOSE
    MIL J 5513 : C JOINT, HYDRAULIC SWIVEL
    MIL C 25427 : A COUPLING ASSEMBLY, HYDRAULIC, SELF-SEALING, QUICK DISCONNECT
    MIL-M-7997 Revision C:1981 MOTOR, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT GENERAL SPECIFICATION FOR
    MIL-R-83485 Base Document:1976 RUBBER, FLUOROCARBON ELASTOMER, IMPROVED PERFORMANCE AT LOW TEMPERATURES
    SAE AS 1300 : 2014 PORT - RING LOCKED FLUID CONNECTION TYPE, STANDARD DIMENSIONS FOR
    MIL V 19068 : A VALVE, SHUTTLE, HYDRAULIC, AIRCRAFT, TYPE 11 SYSTEMS
    MIL-H-8891 Revision A:1978 HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR
    MIL H 25579 : E HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR
    MIL-C-85449-3 Revision B:1987 CLAMP ASSEMBLY, SADDLE TYPE, CUSHIONED, SILICONE FABRIC, REINFORCED 321 CRES, 500 DEG. F, GENERAL PURPOSE
    MIL-V-5525 Revision C:1959 VALVES AIRCRAFT POWER BRAKE
    MIL-B-8584 Revision C:1970 BRAKE SYSTEMS, WHEEL, AIRCRAFT, DESIGN OF
    MS14169 Revision C:1980 CIRCULAR SPLINE AND ADAPTER DETAILS ENGINE DRIVEN ACCESSORIES
    SAE AMS 5561 : 2012 STEEL, CORROSION AND HEAT-RESISTANT, WELDED AND DRAWN OR SEAMLESS AND DRAWN TUBING, 9.0MN - 20CR - 6.5NI - 0.28N, HIGH-PRESSURE HYDRAULIC
    MS27595 Revision E:2006 RETAINER, PACKING BACKUP, CONTINUOUS RING, POLYTETRAFLUOROETHYLENE
    MIL S 9395 : F SWITCHES, PRESSURE, [ABSOLUTE, GAGE AND DIFFERENTIAL] GENERAL SPECIFICATION FOR
    MIL-V-5527 Revision A:1951 VALVE, AIRCRAFT, HYDRAULIC THERMAL EXPANSION RELIEF
    MIL-P-83461-2 Base Document:1991 PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT IMPROVED PERFORMANCE AT 275 DEGREE F FOR USE IN BOSS FITTINGS, SIZES AND TOLERANCES
    MIL-STD-2069 Base Document:1961 REQUIREMENTS FOR AIRCRAFT NONNUCLEAR SURVIVABILITY PROGRAM
    MIL F 27272 : B FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR
    MS33656 Revision J:1987 FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL
    MIL-F-8815-6 Revision B:1976 FILTER ELEMENTS, NON-CLEANABLE, FLUID PRESSURE, HYDRAULIC LINE 3000 PSI 5 MICRON ABSOLUTE MINUS 65 DEGREES TO PLUS 275 DEGREES F
    MIL-P-5994 Revision D:1972 PUMP, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY, GENERAL SPECIFICATION FOR
    MIL-F-85720 Base Document:1985 FITTING, TUBE, FLUID SYSTEMS, SEPARABLE, HIGH PRESSURE, DYNAMIC BEAM, SEAL, GENERAL SPECIFICATION FOR
    MIL F 9490 : D FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-G-5514 Revision G:1993 GLAND DESIGN, PACKINGS, HYDRAULIC GENERAL REQUIREMENTS FOR
    MIL-R-8791 Revision D:1982 RETAINER, PACKING, HYDRAULIC, AND PNEUMATIC, TETRAFLUOROETHYLENE RESIN
    SAE ARP 994 : 2016 DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS
    MIL H 83282 : C HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, AIRCRAFT, METRIC, NATO CODE NUMBER H 537
    MIL V 25675 : B VALVE, CHECK, MINIATURE, HYDRAULIC, AIRCRAFT AND MISSILE
    MS33583 Revision C:1993 TUBING END, DOUBLE FLARE, STANDARD DIMENSIONS FOR
    SAE AMS 4945 : 2014 TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC 3AL - 2.5V, CONTROLLED CONTRACTILE STRAIN RATIO COLD WORKED, STRESS RELIEVED
    SAE ARP 1192 : B1987 (R1991) PROCEDURE FOR CALIBRATION AND VERIFICATION OF LIQUIDBORNE PARTICLE COUNTER - AN ABSOLUTE STANDARD
    MIL-H-8775 Revision D:1976 HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR
    MIL-STD-2089 Base Document:1981 AIRCRAFT NONNUCLEAR SURVIVABILITY TERMS
    MS33584 Revision C:1990 TUBING END, STANDARD DIMENSIONS FOR FLARED
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    MS33611 Revision A:1983 TUBE BEND RADII
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    MIL H 5606 : G HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE
    MS14184 Revision A:1980 NON-METALLIC SHAFT COUPLING DETAILS ENGINE DRIVEN ACCESSORIES
    MIL C 85052/3 : B CLAMP, LOOP, TUBE 17-7 PH CRES, 500 DEG., F
    SAE ARP 598 : 2016 AEROSPACE MICROSCOPIC SIZING AND COUNTING OF PARTICULATE CONTAMINATION FOR FLUID POWER SYSTEMS
    MIL-R-8931 Revision A:1994 RESERVOIRS, AIRCRAFT AND MISSILE, HYDRAULIC SEPARATED TYPE
    SAE ARP 1383 : 2013 AEROSPACE - IMPULSE TESTING OF HYDRAULIC COMPONENTS
    MIL C 85052 : A CLAMP LOOP, CUSHION, GENERAL SPECIFICATION FOR
    MIL-P-83461 Revision B:1980 PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, IMPROVED PERFORMANCE AT 275 DEGREES F (135 DEGREES C)
    MIL-V-19069 Revision B:1986 Valve, Check, Hydraulic, Aircraft, Type II Systems
    FED-STD-791 Revision D:2007 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-C-85449 Base Document:1981 CLAMP ASSEMBLY, SADDLE TYPE, CUSHION, GENERAL SPECIFICATION FOR
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    MIL-V-29592 Base Document:1993 VALVE, AIR VENT, AUTOMATIC, HYDRAULIC, LOW PRESSURE TYPE II SYSTEMS, GENERAL SPECIFICATION FOR
    MIL-B-5087 Revision B:1964 BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
    MIL A 5503 : E ACTUATOR, AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR
    MIL-W-5088 Revision L:1991 Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
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    MIL-T-7081 Revision D:1965 TUBE, ALUMINUM ALLOY, SEAMLESS, ROUND, DRAWN, 6061, AIRCRAFT HYDRAULIC QUALITY
    MIL-F-85421 Revision B:1986 FITTINGS, TUBE, FLUID SYSTEMS, SEPARABLE, BEAM SEAM, 3000/4000 PSI - GENERAL SPECIFICATION FOR
    MS21344 Revision A:2016 FITTING INSTALLATION OF FLARED TUBE STRAIGHT THREADED CONNECTORS DESIGN STANDARD FOR
    MIL-F-7179 Revision G:1993 FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM
    MIL-P-83461-1 Revision B:1989 PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT IMPROVED PERFORMANCE OF 275 DEG. F (135 DEG. C) SIZES AND TOLERANCES
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