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
Available format(s)
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Publisher
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 |
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MIL-DTL-64154 Revision B:2008 | LAMINATE: FIBERGLASS-FABRIC-REINFORCED, PHENOLIC |
MIL-PRF-81352 Revision C:2005 | COATINGS, AIRCRAFT TOUCH-UP |
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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 |
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SAE AS 83461/2 : 2016 | STRAIGHT THREAD TUBE FITTING BOSS O-RING MOLDED FROM AMS-P-83461 RUBBER |
SAE AS 83248/2 : 2016 | O-RING MOLDED FROM AMS7259 MATERIAL |
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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 AIR 5005 : 2015 | 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 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-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 AS 81819 : 2010 | BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, HIGH SPEED OSCILLATION -65 TO +160 DEGREES F GENERAL SPECIFICATION FOR |
SAE AS 5127 : 2013 | AEROSPACE STANDARD TEST METHODS FOR AEROSPACE SEALANTS METHODS FOR PREPARING AEROSPACE SEALANT TEST SPECIMENS |
SAE AS 604 : 2012 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 3000 PSI, 400 DEGREES F, HEAVYWEIGHT, HYDRAULIC |
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SAE AS 6449 : 2017 | SOLID FILM LUBRICANT |
SAE ARP 5936 : 2016 | LANDING GEAR STORAGE |
SAE AIR 1922 : 2017 | AEROSPACE - SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE |
SAE AS 4842 : 2016 | FITTINGS AND BOSSES, PIPE THREADED, FLUID CONNECTION |
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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 |
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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 AS 595 : 2015 | AEROSPACE - CIVIL TYPE VARIABLE DELIVERY, PRESSURE COMPENSATED, HYDRAULIC PUMP |
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SAE AS 4604 : 2003 | HOSE ASSEMBLY, 3000 PSI, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 400 DEGREES F, HEAVY DUTY, AIRCRAFT HYDRAULIC SYSTEMS |
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 |
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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 AS 603 : 2015 | IMPULSE TESTING OF HYDRAULIC HOSE, TUBING, AND FITTING ASSEMBLIES |
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SAE ARP 4763 : 2017 | 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 |
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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 ARP 1595 : 2013(R2019) | DESIGN AND VERIFICATION OF AIRCRAFT NOSE WHEEL STEERING SYSTEMS |
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 AIR 5490 : 2016 | CARBON BRAKE CONTAMINATION AND OXIDATION |
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SAE AMS 3277 : 2015 | SEALING COMPOUND, POLYTHIOETHER RUBBER, FAST CURING FOR INTEGRAL FUEL TANKS AND GENERAL PURPOSE, INTERMITTENT USE TO 360 DEGREES F (182 DEGREES C) |
SAE AMS 3144 : 2012 | PRIMER, ANODIC ELECTRODEPOSITION FOR AIRCRAFT APPLICATIONS |
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 4875 : 2016 | FITTINGS, STRAIGHT THREADED BOSS OR FLANGED, FLUID CONNECTION |
SAE AS 4623 : 2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA-ARAMID REINFORCED, 3,000 PSI, 275 DEGREES F, HEAVY DUTY, AIRCRAFT HYDRAULIC SYSTEMS |
SAE AS 83819 : 2013 | BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, 1400 CPM (15 FPM), OSCILLATION, -65 TO +160 DEGREES F (-54 TO +71 DEGREES C) |
SAE AS 85052 : 2015 | CLAMP ASSEMBLY, LOOP TYPE, CUSHIONED, GENERAL SPECIFICATION FOR |
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 |
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 AS 7510 : 2017 | COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, SELF-LOCKING, FIXED CAVITY, HIGH CONDUCTIVITY, SELF-BONDING, PART SPECIFICATION |
SAE AS 81820 : 2014 | BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, LOW SPEED OSCILLATION |
SAE AMS 3167 : 2005 | SOLVENTS, WIPE FOR CLEANING PRIOR TO APPLICATION OF PRIMER AND TOP COAT MATERIALS, OR SEALING COMPOUNDS |
SAE AIR 786 : 2014 | ELASTOMER COMPATIBILITY CONSIDERATIONS RELATIVE TO ELASTOMERIC SEALANT SELECTION |
SAE AS 1946 : 2015 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, UP TO 1500 PSI AND 450 DEGREES F, HYDRAULIC AND PNEUMATIC |
SAE J 2333 : 2013 | 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 AMS 3217/2 : 2012 | 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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