MIL-PRF-83282 Revision D:1997
Current
Current
The latest, up-to-date edition.
HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537
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Important note : Users cannot be edited or removed once added to your Multi user PDF.Covers requirements for hydraulic fluid with a synthetic hydrocarbon-base used in temperatures of -40 Deg C to +250 Deg C. The Hydraulic fluid is identified by NATO Code Number H-537.
| Committee |
FSC 9150
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| DevelopmentNote |
SUPERSEDING MIL-H-83282
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| DocumentType |
Standard
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| Pages |
23
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| ProductNote |
NEW CHILD NOT 1 2019 IS NOW ADDED
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Current
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| Supersedes |
| MIL-PRF-32239 Revision A:2014 | COATING SYSTEM, ADVANCED PERFORMANCE, FOR AEROSPACE APPLICATIONS |
| MIL-PRF-29608 Revision C:2016 | CLEANING AND CLEANING-LUBRICATING COMPOUNDS, ELECTRICAL CONTACT |
| SAE AS4841B | Fittings, 37° Internal Flare, Fluid Connection, Procurement Specification |
| SAE ARP4493A | Aerospace - Direct Drive Servovalves |
| MIL-DTL-5515 Revision F:2013 | PUMP, HYDRAULIC, RAM, HAND DRIVEN |
| 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-PRF-32104 Base Document:2010 | MOBILE HYDRAULIC OIL DISPENSER |
| SAE AS85560B | Bearings, Fiber Reinforced Plastic, Sleeve, Plain and Flanged, Self-Lubricating; General Specification For |
| 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-PRF-24667 Revision C:2008 | COATING SYSTEM, NON-SKID, FOR ROLL, SPRAY, OR SELF-ADHERING APPLICATION |
| MIL-PRF-32405 Base Document:2013 | CLEANER, HAND WIPE, FOR AVIATION AND MISSILE SYSTEMS, METALLIC SUBSTRATES, LOW OR EXEMPT VOC |
| 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-DTL-85052 Revision B:2005 | CLAMP, LOOP, CUSHION, GENERAL SPECIFICATION FOR |
| MIL-PRF-83383 Revision F:2017 | Circuit Breakers, Remote Control, Thermal, Trip Free General Specification For |
| SAE AIR 5479 : 2017 | ENVIRONMENTALLY COMPLIANT PROCESSES FOR LANDING GEAR |
| MIL-PRF-22750 Revision G:2011 | COATING, EPOXY, HIGH-SOLIDS |
| MIL-PRF-85322 Revision C:2014 | COATING, ELASTOMERIC, POLYURETHANE, RAIN-EROSION |
| MIL-PRF-32577 Base Document:2017 | Coating System, Nonskid, Metallic Thermal Spray Application |
| MIL-DTL-9395-31 Revision E:2006 | SWITCHES, PRESSURE, (GAGE), TYPE 2, 5 AMPERES |
| MIL-DTL-32554 Base Document:2016 | STRAPS, TIE-DOWN, ADJUSTABLE, NON-METALLIC, CABLE BUNDLING, GENERAL SPECIFICATION FOR |
| SAE AMS3400 | Fluid, Reference for Testing Polyalphaolefin (PAO) Resistant Material |
| MIL-DTL-25038 Revision J:2012 | WIRE, ELECTRICAL, HIGH TEMPERATURE, FIRE RESISTANT, AND FLIGHT CRITICAL |
| SAE ARP5632 | Rotorcraft: Application of Existing Aircraft Designed Tires, Wheels and Brakes |
| SAE ARP4945A | Aerospace-Solenoid Valve, Hydraulic, Three Way, Two Position, Direct Acting |
| SAE AMSC27725D | Coating, Corrosion Preventative, for Aircraft Integral Fuel Tanks for Use to 250 °F (121 °C) |
| SAE AS83485A | O-RING MOLDED FROM AMS7287 MATERIAL |
| SAE AMS3255B | Sealing Tape, Sheet, or Gasket, Polytetrafluoroethylene, Expanded (EPTFE) Oil and Water Resistant |
| SAE AIR5693 | Compatibility of PTFE Hose Assemblies With Typical Fluids Found in Aerospace Applications |
| SAE AMS3379 | Sealing Compound, Polysulfide Rubber Preformed Strips for Sealing Removable Doors, Skins, and Panels |
| SAE J1779_201305 | Ship Systems and Equipment - Hydraulic System Design Criteria for Marine Vehicles |
| MIL-DTL-83797 Revision C:2008 | HOSE, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
| MIL-DTL-27272 Revision D:2015 | Fittings, Polytetrafluoroethylene Hose, High-Temperature, Medium-Pressure, General Specification for |
| MIL-PRF-83812 Revision D:2011 | FORKLIFT, TRUCK, 10,000 AND 13,000 POUND CAPACITY, ADVERSE TERRAIN |
| MIL-STD-2088 Revision B:2007 | BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT |
| 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-PRF-32542 Base Document:2016 | TRUCK, FORKLIFT, 4,000 AND 6,200 LB. CAPACITY, FRONT/SIDE LOADING, NON-PNEUMATIC, INTERNAL COMBUSTION ENGINE |
| MIL-DTL-24640 Revision C:2011 | CABLES, LIGHTWEIGHT, LOW SMOKE, ELECTRIC, FOR SHIPBOARD USE, GENERAL SPECIFICATION FOR |
| MIL-DTL-7788 Revision H:2011 | PANELS, INFORMATION, INTEGRALLY ILLUMINATED |
| 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-24694 Revision A:2011 | VALVE, HYDRAULIC RELIEF, 1.5 - 35 BARS (22 - 500 POUNDS PER SQUARE INCH) CARTRIDGE TYPE, GENERAL SPECIFICATION FOR (METRIC) |
| 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 |
| MIL-PRF-83830 Revision C:2014 | TRUCK, FORKLIFT, ROUGH TERRAIN, DIESEL ENGINE DRIVEN, 25,000 POUND CAPACITY AT A 48 INCH LOAD CENTER |
| P-W-2891 Revision A:2002 | WIPE SOLVENTS, EXEMPT AND NON-EXEMPT |
| SAE AS81934B | Bearings, Sleeve, Plain and Flanged, Self-Lubricating |
| 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-83817 Revision C:2017 | TRUCK, LIFT, FORK, 4,000 POUND CAPACITY, VARIABLE REACH, ROUGH TERRAIN |
| MIL-PRF-8932 Revision B:1998 | SWITCHES, PRESSURE, BULKHEAD MOUNTED, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-PRF-85570 Revision E:2012 | CLEANING COMPOUNDS, AIRCRAFT, EXTERIOR |
| MIL-DTL-83296 Revision B:2009 | Fittings, Corrosion Resistant Steel, High Temperature, High Pressure (3000 PSI), Hydraulic and Pneumatic, General Specification for |
| NASA KSC SPEC F 0006 : 2009 | HEAT AND BLAST PROTECTION COATING MATERIALS AND APPLICATION METHODS, SPECIFICATION FOR |
| MIL-PRF-32348 Base Document:2010 | POWDER COATING, CAMOUFLAGE CHEMICAL AGENT RESISTANT SYSTEMS |
| 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 AS 83248/1 : 2016 | O-RING MOLDED FROM AMS7276 MATERIAL |
| MIL-PRF-23377 Revision K:2012 | PRIMER COATINGS: EPOXY, HIGH-SOLIDS |
| 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 |
| MIL-DTL-9395-39 Revision D:2010 | SWITCHES, PRESSURE, (GAUGE) TYPE 2, LOW LEVEL TO 5 AMPERES |
| SAE AS5960B | Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35 000 kPa), 400 °F (204 °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 |
| MIL-PRF-81352 Revision C:2005 | COATINGS, AIRCRAFT TOUCH-UP |
| SAE AIR1362C | Aerospace Hydraulic Fluids Physical Properties |
| SAE AMS 2980/1 : 2014 | CARBON FIBER FABRIC AND EPOXY RESIN WET LAY-UP REPAIR MATERIAL - PART 1 - GENERAL REQUIREMENTS |
| SAE AS 5466 : 2012 | AEROSPACE - GENERAL REQUIREMENTS FOR HYDRAULIC FUSE - QUANTITY MEASURING |
| SAE AS620G | Hose Assemblies, Convoluted Polytetrafluoroethylene Metallic Reinforced, High Temperature, Medium Pressure, Aircraft |
| SAE AMS3143B | Powder Coating Material |
| SAE AIR81D | Importance of Physical and Chemical Properties of Aircraft Hydraulic Fluids |
| SAE AS85421A | Fittings, Tube, Fluid Systems, Separable, Beam Seal, 3000/4000 psi, General Specification For |
| SAE AS83461/2B | STRAIGHT THREAD TUBE FITTING BOSS O-RING MOLDED FROM AMS-P-83461 RUBBER |
| SAE AS 83248/2 : 2016 | O-RING MOLDED FROM AMS7259 MATERIAL |
| SAE AS4157B | Coupling Assemblies, Hydraulic, Self-Sealing, Quick Disconnect 8000 Pounds Per Square Inch, Gage |
| SAE AS1975G | Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems |
| SAE AS683D | Installation Procedures and Torques for Fluid Connections |
| SAE AS 1701 : 2017 | LUBRICANT, SOLID FILM |
| SAE AS614D | Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 4000 psi, 400 °F, Heavy Duty, Hydraulic and Pneumatic |
| SAE AS82819 | Bearings, Plain, Self-Aligning, Self-Lubricating, 300 cpm Oscillation (13 fpm), -65 to +160 °F (-54 to +71 °C), Liners Less Than 0.015 inches |
| SAE AIR 1228 : 2009 | STANDARD IMPULSE MACHINE EQUIPMENT AND OPERATION |
| SAE ARP5796 | Flight Critical Control Valves, Military Aircraft |
| 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 AMS7254B | Perfluoroether Elastomer |
| MIL-DTL-9395-40 Revision C:2006 | SWITCHES, PRESSURE, (GAGE), TYPE 2, LOW LEVEL TO 5 AMPERE |
| MIL-DTL-8794 Revision F:2007 | HOSE, SYNTHETIC RUBBER - HYDRAULIC FLUID, FUEL, AND OIL RESISTANT |
| SAE AIR5005A | Aerospace - Commercial Aircraft Hydraulic Systems |
| 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 AS5958F | Fittings, Axially Swaged Tube with Flareless Separable, Fluid System for Operating Pressures up to and Including 5080 psi (35000 kPa), Specification for |
| MIL-DTL-5593 Revision E:2006 | HOSE, AIRCRAFT, LOW PRESSURE AIR AND VACUUM, FLEXIBLE |
| SAE AS4459B | Fittings, Tube, Fluid System 3000 psig (21 000 kPa) Rated Pressure, Externally Swaged, Specification For |
| SAE ARP 5311 : 2016 | AEROSPACE-INTERFACE DEFINITION FOR MECHANICAL ACTUATION SUBSYSTEMS |
| 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-PRF-87257 Revision C:2017 | HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE |
| 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 |
| MIL-PRF-85285 Revision E:2012 | COATING: POLYURETHANE, AIRCRAFT AND SUPPORT EQUIPMENT |
| MIL-PRF-32295 Revision B:2017 | CLEANER, NON-AQUEOUS, LOW-VOC, HAP-FREE |
| MIL-PRF-32597 Base Document:2018 | CLEANER, POLYMER AND POLYMER MATRIX COMPOSITE (PMC) MATERIAL, NON-AQUEOUS, HAP-FREE |
| MIL-DTL-9395-5 Revision F:2014 | SWITCHES, PRESSURE, (GAGE), TYPE 2, SPST, 5 AMPERES |
| JSSG-2001 Revision B:2004 | Air Vehicle |
| MIL-PRF-32306 Base Document:2008 | HOSE ASSEMBLY, PREFORMED FLEXIBLE, VIBRATION AND MOTION ISOLATION |
| SAE AS81819A | Bearings, Plain, Self-Aligning, Self-Lubricating, High Speed Oscillation -65 to +160 °F General Specification For |
| SAE AS5127B | Aerospace Standard Test Methods for Aerospace Sealants Methods for Preparing Aerospace Sealant Test Specimens |
| SAE AS604E | Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 3000 psi, 400 °F, Heavyweight, Hydraulic |
| SAE MA1339 | Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 21,000 kPa, 204 °C, Lightweight, Hydraulic and Pneumatic, Metric |
| SAE AIR 5565 : 2017 | HISTORICAL DESIGN INFORMATION OF AIRCRAFT LANDING GEAR AND CONTROL ACTUATION SYSTEMS |
| SAE AS6449C | Solid Film Lubricant |
| SAE ARP 5936 : 2016 | LANDING GEAR STORAGE |
| SAE AIR 1922 : 2017 | AEROSPACE - SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE |
| SAE AS4842A | Fittings and Bosses, Pipe Threaded, Fluid Connection |
| SAE ARP5891 | Achieving Cleanliness Standards for Aircraft Hydraulic Systems During Manufacture |
| MIL-STD-2073-1 Revision E:2008 | STANDARD PRACTICE FOR MILITARY PACKAGING |
| SAE AS1709A | Coupling Assembly, Hydraulic Self Sealing, Quick Disconnect |
| SAE AS18280F | Fittings, 24° Cone Flareless, Fluid Connection, 3000 psi |
| SAE AS6235A | 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 |
| MIL-PRF-32181 Revision B:2015 | TRUCK, FORKLIFT, 4,000 AND 6,200 POUND CAPACITY, LOADING, INTERNAL COMBUSTION ENGINE |
| SAE J517_201710 | Hydraulic Hose |
| SAE AS83461/1B | M83461 O-RING MOLDED FROM AMS-P-83461 RUBBER |
| SAE AMS3266A | Sealing Compound, Polythioether Elastomeric Two-Part Electrically Conductive |
| 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-STD-3035 Base Document:2013 | DESIGN CRITERIA STANDARD - USAF AIRCRAFT ARRESTING SYSTEMS |
| SAE ARP6154 | Aerospace Fluid Power Electrohydrostatic Module, Design, Performance and Test Recommendations |
| SAE AIR 1083 : 2012 | AIRBORNE HYDRAULIC AND CONTROL SYSTEM SURVIVABILITY FOR MILITARY AIRCRAFT |
| MIL-PRF-32287 Revision A:2011 | PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT |
| MIL-PRF-83861 Revision D:2013 | FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE |
| MIL-PRF-29602 Revision A:2005 | CLEANING COMPOUNDS, PARTS WASHER AND SPRAY CABINET |
| MIL-DTL-5070 Revision F:2006 | ADAPTER, HOSE TO TUBE, PIPE AND FLANGE, REUSABLE - HYDRAULIC, FUEL, AND OIL LINES, GENERAL SPECIFICATION FOR |
| MIL-STD-2161 Revision C:2014 | Paint Schemes and Exterior Markings for U.S. Navy and Marine Corps Aircraft |
| 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 |
| ISO 8829-1:2009 | Aerospace Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Part 1: Metallic (stainless steel) braid |
| SAE AS595D | Aerospace – Civil Type Variable Delivery, Pressure Compensated, Hydraulic Pump |
| SAE ARP1280B | Aerospace - Application Guide for Hydraulic Power Transfer Units |
| SAE AS85720B | Fittings, Tube, Fluid Systems, Separable, High Pressure Beam Seal, 5000/8000 psi, General Specification For |
| SAE AS4843A | Fittings, Beaded, Fluid Connection |
| SAE AS5272E | Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting, Procurement Specification |
| SAE AS4604B | Hose Assembly, 3000 psi, Polytetrafluoroethylene, Metallic Reinforced, 400 °F, Heavy Duty, Aircraft Hydraulic Systems |
| SAE AIR810D | Degradation Limits of Hydrocarbon-Based Hydraulic Fluids, MIL-PRF-5606, MIL-PRF-83282, and MIL-PRF-87257 Used in Hydraulic Test Stands |
| SAE AS2078A | Test Methods, Hose Assemblies, Polytetrafluoroethylene (PTFE) |
| SAE AS1339H | Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 3000 psi, 400 °F, Lightweight, Hydraulic and Pneumatic |
| SAE AS5729A | O-RING MOLDED FROM AMS7379 (FLUOROCARBON) MATERIAL |
| SAE AS1227C | Hose Assembly, Convoluted Polytetrafluoroethylene, Metallic Reinforced, Low Pressure, Up to 400 °F, Aircraft |
| SAE AS603B | Impulse Testing of Hydraulic Hose, Tubing, and Fitting Assemblies |
| SAE AMS3603A | Protective Film, High Performance, Polymeric Pressure Sensitive Adhesive, for Aircraft Exterior Applications |
| SAE ARP4763 | Aerospace - General Requirements for Hydraulic Relief Valves |
| MIL-PRF-83818 Revision C:2015 | TRUCK, FORKLIFT, 4,000 AND 6,200 POUND CAPACITY, FRONT/SIDE LOADING, INTERNAL COMBUSTION ENGINE |
| MIL-DTL-24630 Revision A:2014 | Valves, Check, In-line, for Hydraulic Fluid and Lubricating Oil Fluid, General Specification for |
| MIL-PRF-81733 Revision D:1998 | SEALING AND COATING COMPOUND, CORROSION INHIBITIVE |
| BS ISO 8829-1:2009 | Aerospace. Test methods for polytetraflouroethylene (PTFE) inner-tube hose assemblies Metallic (stainless steel) braid |
| SAE ARP1311C | Landing Gear Structures and Mechanisms |
| SAE AIR4094A | Aircraft Flight Control Systems Descriptions |
| SAE AMS3970/1A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements |
| SAE AIR 5829 : 2008 | AIR IN AIRCRAFT HYDRAULIC SYSTEMS |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| MIL-DTL-9395-33 Revision C:2006 | SWITCHES, PRESSURE, (DIFFERENTIAL), TYPE 3, 5 AMPERES |
| MIL-DTL-9395-38 Revision C:2006 | SWITCHES, PRESSURE, (GAGE) TYPE 2, LOW LEVEL TO 5 AMPERES |
| MIL-DTL-5500 Revision G:2014 | CAP, HIGH PRESSURE AIR VALVE |
| MIL-PRF-85582 Revision E:2012 | PRIMER COATINGS: EPOXY, WATERBORNE |
| MIL-PRF-32470 Base Document:2013 | TRUCK, FORKLIFT, 10,000 LB CAPACITY, VARIABLE REACH, ROUGH TERRAIN |
| MIL-DTL-83420 Revision P:2017 | WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR |
| MIL-PRF-87937 Revision D:2001 | CLEANING COMPOUND, AEROSPACE EQUIPMENT |
| 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 ARP4925B | Aerospace Design and Installation of Commercial Transport Helicopter Hydraulic Systems |
| SAE AIR5490A | Carbon Brake Contamination and Oxidation |
| SAE ARP4752B | Aerospace - Design and Installation of Commercial Transport Aircraft Hydraulic Systems |
| SAE AMS3277J | Sealing Compound, Polythioether Rubber Fast Curing for Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C) |
| SAE AMS3144 | Primer, Anodic Electrodeposition for Aircraft Applications |
| SAE AS5951D | Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 5080 psi (35000 kPa), 275 °F (135 °C), Aircraft Hydraulic Systems |
| SAE AS4941B | Aerospace - General Requirements for Commercial Aircraft Hydraulic Components |
| SAE AS4875A | Fittings, Straight Threaded Boss or Flanged, Fluid Connection |
| SAE AS4623E | Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3,000 psi, 275 °F, Heavy Duty, Aircraft Hydraulic Systems |
| SAE AS83819 | Bearings, Plain, Self-Aligning, Self-Lubricating, 1400 cpm (15 fpm), Oscillation, -65 to +160 °F (-54 to +71 °C) |
| SAE AS85052A | Clamp Assembly, Loop Type, Cushioned, General Specification For |
| SAE AIR4543C | Aerospace Hydraulics and Actuation Lessons Learned |
| SAE AS6116A | Aluminum Fittings, Axially Swaged Tube with Flareless Separable, Fluid System Up to 1500 psi (10340 kPa) Maximum, Specification for |
| MIL-STD-1568 Revision D:2015 | Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
| SAE ARP4912C:2017 | DESIGN RECOMMENDATIONS FOR SPARE SEALS IN LANDING GEAR SHOCK STRUTS |
| SAE AS7510 | Coupling Assembly, Threadless, Flexible, Self-Locking, Fixed Cavity, High Conductivity, Self-Bonding, Part Specification |
| SAE AS81820D | Bearings, Plain, Self-Aligning, Self-Lubricating, Low Speed Oscillation |
| SAE AMS3167B | Solvents, Wipe for Cleaning Prior to Application of Primer and Top Coat Materials, or Sealing Compounds |
| SAE AIR786B | Elastomer Compatibility Considerations Relative to Elastomeric Sealant Selection |
| SAE AS1946E | Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, Up to 1500 psi and 450 °F, Hydraulic and Pneumatic |
| SAE J2333_201305 | Ship Systems and Equipment - Hydraulic Systems - Filter Selection Parameters |
| ASTM D 892 : 2013-07 | TEST METHOD FOR FOAMING CHARACTERISTICS OF LUBRICATING OILS |
| ASTM D 4898 : 2016 : REDLINE | Standard Test Method for Insoluble Contamination of Hydraulic Fluids by Gravimetric Analysis |
| MIL H 87257 : 0 | HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT & MISSILE |
| 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 |
| SAE AMS3217/2C | Test Slabs, Acrylonitrile Butadiene (NBR-L) Low Acrylonitrile, 65 - 75 |
| MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
| 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 |
| ASTM E 659 : 2015 : REDLINE | Standard Test Method for Autoignition Temperature of Chemicals |
| ASTM D 1744 : 2013 | Standard Test Method for Determination of Water in Liquid Petroleum Products by Karl Fischer Reagent (Withdrawn 2016) |
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