MIL-PRF-87257 Revision C:2017
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE
Available format(s)
PDF
Superseded date
19-05-2022
Superseded by
Language(s)
English
Publisher
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
Specifies the characteristics and provides the requirements for a synthetic hydrocarbon base hydraulic fluid for use in the -54 degrees C to +200 degrees C temperature range in aircraft and missile hydraulic systems.
| Committee |
FSC 9150
|
| DevelopmentNote |
Supersedes MIL H 87257 (04/2004)
|
| DocumentType |
Standard
|
| Pages |
15
|
| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| SAE ARP 4493 : 2013 | AEROSPACE - DIRECT DRIVE SERVOVALVES |
| MIL-DTL-32480 Base Document:2014 | Adapter, Hydraulic and Pneumatic, Flareless Tube Fitting to ORFS Connectors, 1500 to 3000 PSI and Minus 65 Degrees Fahrenheit to Plus 250 Degrees Fahrenheit, General Specification for |
| MIL-DTL-5515 Revision F:2013 | PUMP, HYDRAULIC, RAM, HAND DRIVEN |
| MIL-PRF-32104 Base Document:2010 | MOBILE HYDRAULIC OIL DISPENSER |
| MIL-STD-290 Revision H:2013 | PACKAGING AND MARKING OF PETROLEUM AND RELATED PRODUCTS |
| MIL-DTL-8815-31 Base Document:2009 | FILTER ELEMENTS, NON-CLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 3,000 PSI, 5 MICRON ABSOLUTE, -65 DEGREES F TO 275 DEGREES F |
| MIL-DTL-32372 Revision A:2016 | Fitting, Adapter, Hydraulic and Pneumatic, NPTF to ORFS Connectors, 1500 to 3000 PSI and -65°F to 250°F |
| MIL-PRF-22750 Revision G:2011 | COATING, EPOXY, HIGH-SOLIDS |
| MIL-DTL-32554 Base Document:2016 | STRAPS, TIE-DOWN, ADJUSTABLE, NON-METALLIC, CABLE BUNDLING, GENERAL SPECIFICATION FOR |
| SAE AMS 3400 : 2017 | FLUID, REFERENCE FOR TESTING POLYALPHAOLEFIN (PAO) RESISTANT MATERIAL |
| MIL-PRF-32177 Revision A:2012 | CLEANING COMPOUND, NONSKID |
| MIL-DTL-25038 Revision J:2012 | WIRE, ELECTRICAL, HIGH TEMPERATURE, FIRE RESISTANT, AND FLIGHT CRITICAL |
| SAE ARP 5632 : 2016 | ROTORCRAFT: APPLICATION OF EXISTING AIRCRAFT DESIGNED TIRES, WHEELS AND BRAKES |
| SAE AIR 810 : 2013 | DEGRADATION LIMITS OF HYDROCARBON-BASED HYDRAULIC FLUIDS, MIL-PRF-5606, MIL-PRF-83282, AND MIL-PRF-87257 USED IN HYDRAULIC TEST STANDS |
| SAE AS 83461/2 : 2016 | STRAIGHT THREAD TUBE FITTING BOSS O-RING MOLDED FROM AMS-P-83461 RUBBER |
| SAE AS 83485 : 2016 | O-RING MOLDED FROM AMS7287 MATERIAL |
| SAE AIR 5693 : 2014 | COMPATIBILITY OF PTFE HOSE ASSEMBLIES WITH TYPICAL FLUIDS FOUND IN AEROSPACE APPLICATIONS |
| MIL-DTL-83797 Revision C:2008 | HOSE, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
| MIL-DTL-8790 Revision F:2007 | Hose Assemblies, Rubber, Hydraulic, High Pressure 3,000 PSI, Operating Temperature Range -65 Degrees F to +275 Degrees F, Field Attachable |
| MIL-DTL-24640 Revision C:2011 | CABLES, LIGHTWEIGHT, LOW SMOKE, ELECTRIC, FOR SHIPBOARD USE, GENERAL SPECIFICATION FOR |
| MIL-DTL-83796 Revision B:2008 | HOSE ASSEMBLY, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
| MIL-DTL-5523 Revision E:2011 | VALVE; RELIEF, HYDRAULIC PRESSURE |
| MIL-DTL-32330 Revision A:2015 | Hose Assembly, Conductive Polytetrafluoroethylene Tube, Smooth Bore, Flared and Flareless, Tube to Hose, with Swivel Nut |
| MIL-DTL-25579 Revision H:2014 | Hose Assembly, Polytetrafluoroethylene, High Temperature, Medium Pressure, General Specification for |
| MIL-DTL-8788 Revision G:2015 | Hose, Rubber, Hydraulic, High Pressure 3,000 PSI, Operating Temperature Range -65 Degrees F to +160 Degrees F |
| MIL-DTL-27267 Revision D:2012 | Hose, Cres Wire Reinforced, Polytetrafluoroethylene, Four Hundred Fifty Degree Fahrenheit, Medium Pressure |
| SAE AS 83461/1 : 2016 | M83461 O-RING MOLDED FROM AMS-P-83461 RUBBER |
| A-A-59935 Base Document:2013 | Conical Seal, Crush, 37 Degree Flared Tube Fitting, General Requirements for |
| MIL-PRF-5503 Revision G:2013 | ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
| MIL-PRF-6083 Revision G:2013 | HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION |
| MIL-DTL-25427 Revision B:2009 | COUPLING ASSEMBLY, HYDRAULIC, SELF SEALING, QUICK DISCONNECT, GENERAL SPECIFICATION FOR |
| MIL-DTL-32435 Base Document:2013 | Hose, Polytetrafluoroethylene, Convoluted, 450 Degrees F, Medium Pressure |
| MIL-PRF-8932 Revision B:1998 | SWITCHES, PRESSURE, BULKHEAD MOUNTED, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-DTL-83296 Revision B:2009 | Fittings, Corrosion Resistant Steel, High Temperature, High Pressure (3000 PSI), Hydraulic and Pneumatic, General Specification for |
| 16/30354036 DC : 0 | BS EN 4854-3 - AEROSPACE SERIES - BEARINGS, SPHERICAL PLAIN, IN CORROSION RESISTING STEEL WITH SELF-LUBRICATING LINER, LOW STARTING TORQUE AND LOW FRICTION COEFFICIENT, ELEVATED DUTY CYCLES UNDER LOW OSCILLATIONS AT DIFFERENT OPERATING CONDITIONS - PART 3: TECHNICAL SPECIFICATION |
| MIL-DTL-83298 Revision C:2009 | Hose, Conductive Polytetrafluoroethylene Tube, High Temperature, High Pressure (3000 PSI), Hydraulicand Pneumatic |
| MIL-DTL-8815-32 Base Document:2010 | FILTER ELEMENTS, NON-CLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 3000 PSI, 5 MICRON ABSOLUTE, -65 DEGREES F TO 275 DEGREES F, H-60 AIRCRAFT |
| SAE AIR 5358 : 2016 | LANDING GEAR SHOCK STRUT HYDRAULIC FLUID |
| MIL-DTL-81381 Revision C:2005 | WIRE, ELECTRIC, POLYIMIDE-INSULATED, COPPER OR COPPER ALLOY |
| SAE AS 83248/1 : 2016 | O-RING MOLDED FROM AMS7276 MATERIAL |
| MIL-PRF-27601 Revision C:1998 | HYDRAULIC FLUID, FIRE RESISTANT, HYDROGENATED POLYALPHAOLEFIN BASE, HIGH TEMPERATURE, FLIGHT VEHICLE, METRIC |
| MIL-DTL-32464 Revision A:2017 | FITTINGS, ADAPTER, HYDRAULIC AND PNEUMATIC, 37 DEGREES SPHERICAL TO ANPT CONNECTORS, 1500 TO 3000 PSI, GENERAL SPECIFICATION FOR |
| SAE AS 5960 : 2013 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC BRAID REINFORCED, 5080 PSI (35000 KPA), 400 DEGREES F (204 DEGREES C), AIRCRAFT HYDRAULIC SYSTEMS |
| MIL-DTL-32371 Base Document:2012 | Fittings, Adapter, Hydraulic and Pneumatic, Spherical to ORFS Connectors, 1500 to 3000 PSI, General Specification for |
| MIL-DTL-64154 Revision B:2008 | LAMINATE: FIBERGLASS-FABRIC-REINFORCED, PHENOLIC |
| SAE AIR 1362 : 2016 | AEROSPACE HYDRAULIC FLUIDS PHYSICAL PROPERTIES |
| SAE AS 5466 : 2012 | AEROSPACE - GENERAL REQUIREMENTS FOR HYDRAULIC FUSE - QUANTITY MEASURING |
| SAE AS 620 : 2012 | HOSE ASSEMBLIES, CONVOLUTED POLYTETRAFLUOROETHYLENE METALLIC REINFORCED, HIGH TEMPERATURE, MEDIUM PRESSURE, AIRCRAFT |
| SAE AIR 81 : 2016 | IMPORTANCE OF PHYSICAL AND CHEMICAL PROPERTIES OF AIRCRAFT HYDRAULIC FLUIDS |
| SAE ARP 4945 : 2013 | AEROSPACE-SOLENOID VALVE, HYDRAULIC, THREE WAY, TWO POSITION, DIRECT ACTING |
| SAE AS 83248/2 : 2016 | O-RING MOLDED FROM AMS7259 MATERIAL |
| SAE AS 683 : 2012 | INSTALLATION PROCEDURES AND TORQUES FOR FLUID CONNECTIONS |
| SAE AIR 786 : 2014 | ELASTOMER COMPATIBILITY CONSIDERATIONS RELATIVE TO ELASTOMERIC SEALANT SELECTION |
| SAE AS 614 : 2017 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 4000 PSI, 400 DEGREES F, HEAVY DUTY, HYDRAULIC AND PNEUMATIC |
| SAE AIR 1228 : 2009 | STANDARD IMPULSE MACHINE EQUIPMENT AND OPERATION |
| MIL-DTL-13444 Revision H:2006 | Hose and Hose Assemblies, Rubber: Fuel and Oil |
| MIL-DTL-26633 Revision F:2014 | Hose Assembly, Nonconductive, Polytetrafluoroethylene, Oxygen |
| SAE ARP 994 : 2016 | DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS |
| MIL-DTL-8794 Revision F:2007 | HOSE, SYNTHETIC RUBBER - HYDRAULIC FLUID, FUEL, AND OIL RESISTANT |
| SAE AS 5258 : 2012 | INSULATING COMPONENT, MOLDED, ELECTRICAL, HEAT SHRINKABLE, CONNECTOR AND CABLE ACCESSORY, SEALING STRAIN RELIEF, GENERAL SPECIFICATION FOR |
| MIL-PRF-32058 Revision B:2017 | CHOCK, WHEEL-TRACK - AVIATION, ADJUSTABLE ROPE TYPE |
| MIL-DTL-19068 Revision B:2006 | VALVES, SHUTTLE, HYDRAULIC, AIRCRAFT, TYPE 2 SYSTEMS |
| SAE AS 5958 : 2017 | FITTINGS, AXIALLY SWAGED TUBE WITH FLARELESS SEPARABLE, FLUID SYSTEM FOR OPERATING PRESSURES UP TO AND INCLUDING 5080 PSI (35 000 KPA), SPECIFICATION FOR |
| MIL-DTL-5593 Revision E:2006 | HOSE, AIRCRAFT, LOW PRESSURE AIR AND VACUUM, FLEXIBLE |
| SAE AS 4459 : 2013 | FITTINGS, TUBE, FLUID SYSTEM 3000 PSIG (21000 KPA) RATED PRESSURE, EXTERNALLY SWAGED, SPECIFICATION FOR |
| SAE ARP 5311 : 2016 | AEROSPACE-INTERFACE DEFINITION FOR MECHANICAL ACTUATION SUBSYSTEMS |
| MIL-DTL-32234 Base Document:2007 | CONNECTORS, ELECTRICAL, ULTRA HIGH DENSITY, MODULAR, BLADE AND FORK, EIGHT ROW, GENERAL SPECIFICATION FOR |
| MIL-DTL-53030 Revision B Interim Revision:2003 | Primer Coating, Epoxy, Water Based, Lead and Chromate Free |
| MIL-PRF-83860 Revision D:2013 | FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 MICRON ABSOLUTE |
| MIL-DTL-32460 Revision A:2017 | ADAPTER, HYDRAULIC AND PNEUMATIC, 37 DEGREES FLARE TUBE FITTING TO ORFS CONNECTORS, 1500 TO 3000 PSI AND -65 DEGREES F TO 250 DEGREES F, GENERAL SPECIFICATION FOR |
| MIL-DTL-83798 Revision D:2008 | FITTING, RUBBER HOSE, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
| MIL-DTL-8795 Revision G:2014 | Hose Assemblies, Elastomeric, Hydraulic, Fuel, Coolant, and Oil Resistant, General Specification for |
| MIL-DTL-53030 Revision D:2011 | Primer Coating, Epoxy, Water Based, Lead and Chromate Free |
| MIL-STD-3004 Revision D:2014 | QUALITY ASSURANCE/SURVEILLANCE FOR FUELS, LUBRICANTS AND RELATED PRODUCTS |
| SAE AS 604 : 2012 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 3000 PSI, 400 DEGREES F, HEAVYWEIGHT, HYDRAULIC |
| SAE AS 2078 : 2015 | TEST METHODS, HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE (PTFE) |
| PREN 4854-3 : 200P1 | AEROSPACE SERIES - BEARINGS, SPHERICAL PLAIN, IN CORROSION RESISTING STEEL WITH SELF-LUBRICATING LINER, LOW STARTING TORQUE AND LOW FRICTION COEFFICIENT, ELEVATED DUTY CYCLES UNDER LOW OSCILLATIONS AT DIFFERENT OPERATING CONDITIONS - PART 3: TECHNICAL SPECIFICATION |
| SAE MA 1339 : 2015 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 21,000 KPA, 204 DEGREE C, LIGHTWEIGHT, HYDRAULIC AND PNEUMATIC, METRIC |
| SAE ARP 1595 : 2013(R2019) | DESIGN AND VERIFICATION OF AIRCRAFT NOSE WHEEL STEERING SYSTEMS |
| SAE AIR 1922 : 2017 | AEROSPACE - SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE |
| SAE AIR 5005 : 2015 | AEROSPACE - COMMERCIAL AIRCRAFT HYDRAULIC SYSTEMS |
| SAE AS 1975 : 2016 | Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems |
| SAE AS 1709 : 2014 | COUPLING ASSEMBLY, HYDRAULIC SELF SEALING, QUICK DISCONNECT |
| SAE AS 18280 : 2017 | FITTINGS, 24 DEGREES CONE FLARELESS, FLUID CONNECTION, 3000 PSI |
| SAE AS 6235 : 2015 | FACE SEAL GLAND DESIGN, STATIC, O-RING AND OTHER SEALS FOR AEROSPACE HYDRAULIC AND PNEUMATIC APPLICATIONS |
| MIL-PRF-6164 Revision G:2012 | VALVE; AIRCRAFT, PNEUMATIC, HIGH-PRESSURE CHARGING |
| SAE ARP 5796 : 2013 | FLIGHT CRITICAL CONTROL VALVES, MILITARY AIRCRAFT |
| MIL-DTL-32434 Base Document:2013 | Hose Assembly, Polytetrafluoroethylene, Convoluted, High Temperature, Medium Pressure, General Specification for |
| SAE ARP 1281 : 2002 | ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
| MIL-DTL-5498 Revision G:2013 | ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
| SAE ARP 6154 : 2017 | AEROSPACE FLUID POWER ELECTROHYDROSTATIC MODULE, DESIGN, PERFORMANCE AND TEST RECOMMENDATIONS |
| SAE AIR 1083 : 2012 | AIRBORNE HYDRAULIC AND CONTROL SYSTEM SURVIVABILITY FOR MILITARY AIRCRAFT |
| SAE AIR 5829 : 2008 | AIR IN AIRCRAFT HYDRAULIC SYSTEMS |
| MIL-PRF-32287 Revision A:2011 | PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT |
| MIL-DTL-83733 Revision E:2006 | CONNECTORS, ELECTRICAL MINIATURE, RECTANGULAR TYPE, RACK TO PANEL, ENVIRONMENT RESISTING, 200 DEGREES C TOTAL CONTINUOUS OPERATING TEMPERATURE, GENERAL SPECIFICATION FOR |
| MIL-DTL-5070 Revision F:2006 | ADAPTER, HOSE TO TUBE, PIPE AND FLANGE, REUSABLE - HYDRAULIC, FUEL, AND OIL LINES, GENERAL SPECIFICATION FOR |
| MIL-PRF-83861 Revision D:2013 | FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE |
| MIL-DTL-8789 Revision G:2015 | FITTING END, ATTACHABLE, HYDRAULIC, HIGH PRESSURE (3,000 PSI), GENERAL SPECIFICATION FOR |
| MIL-PRF-46170 Revision E:2013 | HYDRAULIC FLUID, RUST INHIBITED, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, NATO CODE NO. H-544 |
| MIL PRF 0032287 : 0 | PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT |
| MIL-PRF-5606 Revision H:2002 | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE |
| SAE AS 595 : 2015 | AEROSPACE - CIVIL TYPE VARIABLE DELIVERY, PRESSURE COMPENSATED, HYDRAULIC PUMP |
| SAE AS 1339 : 2017 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 3000 PSI, 400 DEGREES F, LIGHTWEIGHT, HYDRAULIC AND PNEUMATIC |
| SAE AS 5729 : 2016 | O-RING MOLDED FROM AMS7379 (FLUOROCARBON) MATERIAL |
| SAE AS 1227 : 2013 | HOSE ASSEMBLY, CONVOLUTED POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, LOW PRESSURE, UP TO 400 DEGREES F, AIRCRAFT |
| SAE ARP 5891 : 2014 | ACHIEVING CLEANLINESS STANDARDS FOR AIRCRAFT HYDRAULIC SYSTEMS DURING MANUFACTURE |
| SAE ARP 4763 : 2017 | AEROSPACE - GENERAL REQUIREMENTS FOR HYDRAULIC RELIEF VALVES |
| MIL-DTL-9129 Revision G:2014 | Discharges, Electrostatic General Specification for |
| SAE ARP 1311 : 2015 | LANDING GEAR STRUCTURES AND MECHANISMS |
| SAE AIR 4094 : 2016 | AIRCRAFT FLIGHT CONTROL SYSTEMS DESCRIPTIONS |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| MIL-DTL-28804 Revision D:1998 | CONNECTORS, PLUG AND RECEPTACLE, ELECTRIC, RECTANGULAR, HIGH DENSITY, POLARIZATION CENTER JACKSCREW - GENERAL SPECIFICATION FOR |
| MIL DTL 17 : J | CABLES, RADIO FREQUENCY, FLEXIBLE AND SEMIRIGID, GENERAL SPECIFICATION FOR |
| MIL-DTL-8815-33 Base Document:2011 | FILTER ELEMENTS, NON-CLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 3500 PSI, 5 MICRON ABSOLUTE, -65 DEGREES F TO 275 DEGREES F, AVIATION GROUND POWER UNIT (AGPU) |
| SAE AS 5467 : 2016 | GENERAL REQUIREMENTS FOR HYDRAULIC FUSE - FLOW RATE |
| SAE ARP 4925 : 2014 | AEROSPACE DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT HELICOPTER HYDRAULIC SYSTEMS |
| SAE ARP 4752 : 2013 | AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS |
| SAE AIR 5490 : 2016 | CARBON BRAKE CONTAMINATION AND OXIDATION |
| SAE AS 5951 : 2017 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA-ARAMID REINFORCED, 5080 PSI (35,000 KPA), 275 DEGREES F (135 DEGREES C), AIRCRAFT HYDRAULIC SYSTEMS |
| SAE AS 4941 : 2015 | AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS |
| SAE AS 4623 : 2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA-ARAMID REINFORCED, 3,000 PSI, 275 DEGREES F, HEAVY DUTY, AIRCRAFT HYDRAULIC SYSTEMS |
| SAE AIR 4543 : 2017 | AEROSPACE HYDRAULICS AND ACTUATION LESSONS LEARNED |
| SAE AS 6116 : 2016 | ALUMINUM FITTINGS, AXIALLY SWAGED TUBE WITH FLARELESS SEPERABLE, FLUID SYSTEM, UP TO 1500 PSI (10340 KPA) MAXIMUM, SPECIFICATION FOR |
| SAE ARP4912C:2017 | DESIGN RECOMMENDATIONS FOR SPARE SEALS IN LANDING GEAR SHOCK STRUTS |
| MIL-STD-1568 Revision D:2015 | Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
| SAE ARP 988 : 2016 | ELECTROHYDRAULIC MECHANICAL FEEDBACK SERVOACTUATORS |
| SAE AS 1946 : 2015 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, UP TO 1500 PSI AND 450 DEGREES F, HYDRAULIC AND PNEUMATIC |
| ASTM D 892 : 2013-07 | TEST METHOD FOR FOAMING CHARACTERISTICS OF LUBRICATING OILS |
| MIL-PRF-6083 Revision G:2013 | HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION |
| ASTM D 4898 : 2016 : REDLINE | Standard Test Method for Insoluble Contamination of Hydraulic Fluids by Gravimetric Analysis |
| MIL-PRF-46170 Revision E:2013 | HYDRAULIC FLUID, RUST INHIBITED, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, NATO CODE NO. H-544 |
| SAE AMS 3400 : 2017 | FLUID, REFERENCE FOR TESTING POLYALPHAOLEFIN (PAO) RESISTANT MATERIAL |
| MIL-PRF-5606 Revision H:2002 | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE |
| MIL-PRF-680 Revision C:2010 | DEGREASING SOLVENT |
| ASTM D 4636 : 2017 : REDLINE | Standard Test Method for Corrosiveness and Oxidation Stability of Hydraulic Oils, Aircraft Turbine Engine Lubricants, and Other Highly Refined Oils |
| ISO 11500:2008 | Hydraulic fluid power — Determination of the particulate contamination level of a liquid sample by automatic particle counting using the light-extinction principle |
| ASTM D 972 : 2016 : REDLINE | Standard Test Method for Evaporation Loss of Lubricating Greases and Oils |
| ASTM D 4289 : 2014-02 | TEST METHOD FOR ELASTOMER COMPATIBILITY OF LUBRICATING GREASES AND FLUIDS |
| ISO 11171:2016 | Hydraulic fluid power Calibration of automatic particle counters for liquids |
| ASTM D 5949 : 2016 : REDLINE | Standard Test Method for Pour Point of Petroleum Products (Automatic Pressure Pulsing Method) |
| MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
| SAE AS 4059F : 2013 | AEROSPACE FLUID POWER - CONTAMINATION CLASSIFICATION FOR HYDRAULIC FLUIDS |
| ASTM D 5306 : 1992 : R2018 | Standard Test Method for Linear Flame Propagation Rate of Lubricating Oils and Hydraulic Fluids |
| FED-STD-791 Revision D:2007 | TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS |
| SD 6 : 20140201 | PROVISIONS GOVERNING QUALIFICATION: QUALIFIED PRODUCTS LIST AND QUALIFIED MANUFACTURERS LISTS |
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