MIL-H-5440 Revision H:1993

Superseded

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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Superseded date: 01-04-1998

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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.

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Committee	FSC 1650
Document Type	Standard
ISBN
Pages
Published
Publisher	US Military Specs/Standards/Handbooks
Status	Superseded
Superseded By	SAE AS 5440 : 2011

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 5994 : 2013	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	VALVES, 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 DEGREES 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
SAE AIR 4057 : 2012	SECONDARY FILTERS FOR FLUID SYSTEM RELIABILITY
MIL-STD-1472 Revision G:2012	HUMAN ENGINEERING
MIL C 85052/1 : B	CLAMP, LOOP TUBE 17-7 PH CRES, 275 DEG., F, FUEL AND PETROLEUM BASED HYDRAULIC FLUID RESISTANT
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
MIL-V-19067 Revision A:1957	VALVE, CHECK, CONTROLLABLE, HYDRAULIC, AIRCRAFT TYPE 11 SYSTEMS
SAE AS 1339 : 2012	HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 3000 PSI, 400 DEGREES F, LIGHTWEIGHT, HYDRAULIC AND PNEUMATIC
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 F 5508 : B	FUSE, AIRCRAFT AUTOMATIC QUANTITY MEASURING HYDRAULIC
SAE AS 4059F : 2013	AEROSPACE FLUID POWER - CONTAMINATION CLASSIFICATION FOR HYDRAULIC FLUIDS
MIL-P-19692 Revision E:1994	PUMPS, HYDRAULIC, VARIABLE FLOW, GENERAL SPECIFICATION FOR
MS33611 Revision A:1983	TUBE BEND RADII
SAE AS 4251 : 2013	COUPLING ASSEMBLIES, NON-LOCKING PROBE STYLE, SELF-ALIGNING, SELF-SEALING DISCONNECTS
MIL G 8348 : H	GAGE, ASSEMBLIES, AIR PRESSURE, DIAL INDICATING CHUCK TYPE SELF CONTAINED
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	VALVES, 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
SAE AS 604 : 2012	HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 3000 PSI, 400 DEGREES F, HEAVYWEIGHT, HYDRAULIC
MIL-STD-1247 Revision D:2009	MARKINGS, FUNCTIONS AND HAZARDS DESIGNATIONS OF HOSE, PIPE, AND TUBE LINES FOR AIRCRAFT MISSILE, AND SPACE SYSTEMS
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
MIL H 85800 : 0	HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID FIBER REINFORCED, 5000 & 8000 PSI, GENERAL SPECIFICATION FOR
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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