MIL H 83282 : C
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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, SYNTHETIC HYDROCARBON BASE, AIRCRAFT, METRIC, NATO CODE NUMBER H 537
Available format(s)
PDF
Superseded date
30-09-1997
Superseded by
Language(s)
English
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Describes aircraft missile hydraulic systems synthetic hydrocarbon base fluid for -40deg to +205degC temperature range use.
| Committee |
FSC 9150
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| DocumentType |
Standard
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| Pages |
34
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| SupersededBy |
| SAE MA2094 | Test Methods for Tube-Fitting Assemblies, Metric (ISO 10583) |
| AFGS-87213 Revision B:1993 | DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED |
| SAE MA4098 | Hose Assembly, Polytetrafluoroethylene, Heavy Duty, Metallic Reinforced, 204 °C, 35 000 kPa Hydraulic and Pneumatic, Metric |
| MIL-J-26149 Revision E:1988 | Jack, Hydraulic, Aircraft Maintenance, General Specification for |
| MMM-A-132 Revision B:1994 | ADHESIVES, HEAT RESISTANT, AIRFRAME STRUCTURAL, METAL TO METAL |
| MIL-A-85705 Revision A:1987 | ADHESIVE, AIRCRAFT, FOR STRUCTURAL REPAIR |
| MIL-HDBK-267 Revision A:1987 | GUIDE FOR SELECTION OF LUBRICANTS & HYDRAULIC FLUIDS FOR USE IN SHIPBOARDS EQUIPMENT |
| 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 H 87257 : 0 | HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT & MISSILE |
| 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 |
| SAE AS4388 | Hose Assembly PTFE Heavy Duty, -65 To 400 °F (-55 To 204 °C) 8000 psi (56 000 kPa) Hydraulic and Pneumatic |
| MIL F 83861 : B | FILTER ELEMENTS, NONCLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE, TYPE 1I, SYSTEMS GENERAL SPECIFICATION FOR |
| MIL-F-85421 Revision B:1986 | FITTINGS, TUBE, FLUID SYSTEMS, SEPARABLE, BEAM SEAM, 3000/4000 PSI - GENERAL SPECIFICATION FOR |
| MIL-PRF-29598 Base Document:1996 | FILM, PROTECTIVE, LEADING EDGE (PRESSURE-SENSITIVE) |
| MIL C 85322 : B | COATING ELASTOMERIC, POLYURETHANE, RAIN EROSION RESISTANT, FOR EXTERIOR AIRCRAFT USE |
| MIL P 85582 : B | PRIMER COATINGS: EPOXY, WATERBORNE |
| MIL H 8790 : D | HOSE ASSEMBLY, RUBBER HYDRAULIC HIGH PRESSURE [3,000 PSI] |
| MIL H 27267 : B | HOSE TETRAFLUOROETHYLENE, HIGH TEMPERATURE, MEDIUM PRESSURE |
| MIL P 53030 : A | PRIMER COATING, EPOXY, WATER REDUCIBLE, LEAD & CHROMATE FREE |
| MIL D 87213 : 0 | DISPLAYS/OPTICALLY GENERATED REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
| ASTM D 5306 : 1992 : R2002 : EDT 1 | Standard Test Method for Linear Flame Propagation Rate of Lubricating Oils and Hydraulic Fluids |
| ASTM F 1387 : 1999 | Standard Specification for Performance of Piping and Tubing Mechanically Attached Fittings |
| BS EN 2608:2005 | Aerospace series. Installation and removal requirements for 8° 30\' adaptors, threaded, with lockring |
| MIL H 25579 : E | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL-A-81973 Base Document:1974 | AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR |
| MIL V 24630 : 0 | VALVES, CHECK, IN-LINE, FOR HYDRAULIC FLUID AND LUBRICATING OIL FLUID |
| MIL-H-8775 Revision D:1976 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
| MIL-C-5501 Revision G:1989 | CAP AND PLUG, PROTECTIVE, DUST AND MOISTURE SEAL |
| MIL-D-28728 Revision B:1986 | DIAL, CONTROL, MULTI-TURN COUNTERS, GENERAL SPECIFICATION FOR |
| SAE AMS 3109 : 2014 | PRIMER, ADHESIVE, ELECTRODEPOSITED -55 TO +82 DEGREES C (-67 TO +180 DEGREES F) |
| MIL-R-85111 Revision A:1980 | RECOVERY ASSIST SECURING AND TRAVERSING SYSTEM FOR LAMPS MK 111 HELICOPTER |
| SAE AS4444 | Fittings, 24° Cone Flareless, Fluid Connection, 5000 psi |
| SAE AMSP25732 | Packaging, Preformed, Petroleum Hydraulic Fluid Resistant, Limited Service at 275°F (135°C) |
| MIL-PRF-25675 Revision C:1997 | VALVES, CHECK, MINIATURE, HYDRAULIC, AIRCRAFT AND MISSILE |
| MIL-STD-726 Revision H:1985 | PACKAGING REQUIREMENTS CODE |
| MIL S 9395/39 : B | SWITCH, PRESSURE, [GAGE] TYPE 11 LOW LEVEL TO 5 AMPERES |
| MIL-H-5440 Revision H:1993 | HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
| MIL-R-8931 Revision A:1994 | RESERVOIRS, AIRCRAFT AND MISSILE, HYDRAULIC SEPARATED TYPE |
| MIL-B-85598 Base Document:1988 | BEARINGS, ELASTOMERIC GENERAL SPECIFICATION FOR |
| MIL F 83860 : C | FILTER ELEMENTS, NONCLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 MICRON ABSOLUTE, TYPE II, SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL H 46170 : B | HYDRAULIC FLUID, RUST INHIBITED, FIRE-RESISTANT, SYNTHETIC HYDROCARBON BASE |
| A-A-50542 Revision A:1994 | COATING SYSTEM, REFLECTIVE, SLIP-RESISTANT, CHEMICAL RESISTANT URETHANE FOR MAINTENANCE FACILITY FLOORS |
| SAE MA620 | Hose Assemblies, Convoluted Polytetrafluoroethylene Metallic Reinforced, High Temperature, Medium Pressure, Aircraft Metric |
| TT-P-2756 Revision A:1996 | POLYURETHANE COATING - SELF-PRIMING TOPCOAT, LOW VOLATILE ORGANIC COMPOUND (VOC) CONTENT |
| MIL W 83420 : E | WIRE, ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL |
| MIL-L-8937 Revision D:1982 | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING, [NATO CODE NUMBER S 1738] |
| SAE AIR4713A | Aerospace - Chlorinated Solvent Contamination of MIL-H-5606/MIL-H-83282 Vehicle Hydraulic Systems |
| SAE ARP1185B | Flexure Testing of Hydraulic Tubing Joints and Fittings |
| SAE AIR4922A | Primary Flight Control Hydraulic Actuation System Interface Definition |
| ASTM D 5306 : 1992 : R2018 | Standard Test Method for Linear Flame Propagation Rate of Lubricating Oils and Hydraulic Fluids |
| MIL-H-38360 Revision B:1966 | HOSE, ASSEMBLIES, TETRAFLUOROETHYLENE, HIGH-TEMPERATURE, HIGH PRESSURE, 3000 PSI HYDRAULIC AND PNEUMATIC |
| MIL-F-18280 Revision F:1995 | FITTING, FLARELESS TUBE, FLUID CONNECTION |
| MIL-M-7997 Revision C:1981 | Motor, Aircraft Hydraulic, Constant Displacement General Specification for |
| MIL-C-83873 Revision A:1993 | CLEANING COMPOUND, PRECOATING SURFACE, AIRCRAFT & AEROSPACE GROUND EQUIPMENT (AGE) |
| SAE AS4251 | Coupling Assemblies, Non-Locking Probe Style, Self-Aligning, Self-Sealing Disconnects |
| MIL-S-87241 Base Document:1985 | SIMULATOR, FLIGHT (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
| MIL-B-81820 Revision F:1994 | BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, LOW SPEED OSCILLATION, GENERAL SPECIFICATION FOR |
| MIL-P-46111 Revision C:1978 | PLASTIC FOAM, POLYURETHANE (FOR USE IN AIRCRAFT) |
| MIL-HDBK-692 Revision B:1983 | A Guide to the Selection of Rubber O-Rings |
| MIL-B-81819 Revision B:1987 | BEARING, PLAIN, (SLIDING SPHERICAL, SLEEVE & THRUST) SELF LUBRICATING, HIGH SPEED OSCILLATION, GENERAL SPECIFICATION FOR |
| MIL-C-87987 Base Document:1989 | CRANE, HYDRAULIC, WHEEL MOUNTED, 7.5 & 15 TON CAPACITIES |
| SAE AS7997 | Motors, Aircraft Hydraulic, Constant Displacement General Specification For |
| MIL-P-87175 Base Document:1982 | PACKING, PREFORMED, PETROLEUM, HYDRAULIC FLUID RESISTANT, PHOSPHONITRILIC FLUOROELASTOMER |
| SAE AS4510 | Fittings, Weld, Fluid Connection, 5000 psi |
| SAE MA2150 | Clamps, Loop or P Style, Single Point Mount, Multiple Shapes, Metric |
| SAE AS4098A | Hose Assembly, Polytetrafluoroethylene, Heavy Duty, Metallic Reinforced, 400 °F, 5000 psi Hydraulic and Pneumatic |
| ASTM D 5306 : 1992 : R2007 | Standard Test Method for Linear Flame Propagation Rate of Lubricating Oils and Hydraulic Fluids |
| ASTM F 1387 : 1999 : R2012 | Standard Specification for Performance of Piping and Tubing Mechanically Attached Fittings |
| MIL-L-23398 Revision D:1985 | LUBRICANT, SOLID FILM, AIR DRYING, CORROSION INHIBITING, NATO CODE NUMBER S 749 |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| MIL-B-85560 Base Document:1983 | BEARING, FIBER REINFORCED PLASTIC, SLEEVE, PLAIN AND FLANGED, SELF LUBRICATING GENERAL SPECIFICATION FOR |
| SAE AS1896A | Coupling Assembly, Self-Sealing, One Side Only, Hydraulic |
| NASA MSFC SPEC 708 : 2007 | SPECIFICATION FOR IDENTIFICATION MARKERS FOR SPACE SYSTEMS ELECTRICAL HARNESSES |
| BWB TL 4330-0020 : 1ED 1996 | FILTER ELEMENT |
| MIL-STD-1290 Revision A:1988 | LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE |
| MIL-F-8815-24 Revision C:1993 | FILTER ELEMENT, NON-CLEANABLE, FLUID PRESSURE, HYDRAULIC LINE 3000 PSI 5 MICRON ABSOLUTE, 65 DEGREES TO 275 DEGREES F 14 AND F 18 AIRCRAFT 84 GPM |
| MIL H 83797 : 0 | HOSE, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
| NASA MSFC PROC 1301 : 1986 | GUIDELINES FOR THE IMPLEMENTATION OF REQUIRED MATERIALS CONTROL PROCEDURES |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| MIL-PRF-29607 Base Document:1996 | CLEANING COMPOUND, AVIONICS COMPONENTS, NON-OZONE DEPLETING |
| MIL C 87937 : B | CLEANING COMPOUND, AEROSPACE EQUIPMENT |
| SAE MA2007A | Hose Assembly, Tetrafluoroethylene, Lightweight, 204 °C, 21 000 kPa Hydraulic, Metric |
| SAE ARP1897 | Clamp Selection and Installation Guide |
| SAE MA1975 | Hose Assemblies, Polytetrafluoroethylene, Aramid Reinforced, 135 °C, Standard Duty, 28 000/21 000 kPa, Hydraulic, Aircraft Systems |
| SAE AS4401 | Separable Fittings, Permanent Fittings, Tubing, Fluid Systems 8000 psi Qualification Test Standard For |
| SAE MA4510 | Fittings, Weld, Fluid Connection, 35 000 kPa, Metric |
| SAE MA2151 | Clamp Assemblies, Saddle or Omega Style, Two Point Mount, Multiple Shapes, Metric |
| ASTM D 5306 : 1992 : R1997 | Standard Test Method for Linear Flame Propagation Rate of Lubricating Oils and Hydraulic Fluids |
| ASTM F 1387 : 1999 : R2005 | Standard Specification for Performance of Piping and Tubing Mechanically Attached Fittings |
| BS EN 2350:1991 | Circuit breakers. Technical specification |
| EN 2608:2005 | Aerospace series - Installation and removal requirements for 8° 30' adaptors, threaded, with lockring |
| EN 2350:1990 | Aerospace series - Circuit breakers - Technical specification |
| MIL C 85285 : C | |
| MIL A 5503 : E | ACTUATOR, AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
| MIL-B-81934 Revision B:1991 | BEARING, SLEEVE, PLAIN AND FLANGED, SELF LUBRICATING |
| MIL H 85800 : 0 | HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID FIBER REINFORCED, 5000 & 8000 PSI, GENERAL SPECIFICATION FOR |
| MIL H 27601 : B | HYDRAULIC FLUID, FIRE RESISTANT, HYDROGENATED POLYALPHAOLEFIN BASE, HIGH TEMPERATURE, FLIGHT VEHICLE, METRIC |
| MIL-P-83461 Revision B:1980 | PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, IMPROVED PERFORMANCE AT 275 DEGREES F (135 DEGREES C) |
| MIL-F-85720 Base Document:1985 | FITTING, TUBE, FLUID SYSTEMS, SEPARABLE, HIGH PRESSURE, DYNAMIC BEAM, SEAL, GENERAL SPECIFICATION FOR |
| MIL H 83298 : A | HOSE, TETRAFLUOROETHYLENE, HIGH TEMPERATURE, HIGH PRESSURE (3000 PSI) HYDRAULIC AND PNEUMATIC |
| MIL-PRF-62495 Revision B:1997 | POWER UNIT, HYDRAULIC |
| MIL A 5498 : D | ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
| MIL F 81836 : A SUPP 1 | FILTER AND DISPOSABLE ELEMENT, FLUID PRESSURE, HYDRAULIC, 3 MICRON ABSOLUTE |
| MIL P 7788 : F | PANEL, INFORMATION INTEGRALLY ILLUMINATED |
| TT-P-2760 Revision A:1994 | PRIMER COATING; POLYURETHANE, ELASTOMERIC |
| SAE AIR4298 | Impulse Test Machine, Sine Wave, Equipment and Operation of |
| MIL P 23377 : G | PRIMER COATING, EPOXY, HIGH SOLIDS |
| MIL-R-5049 Revision D:1989 | RING, WIPER, PISTON ROD |
| MIL C 85570 : B (1) | CLEANING COMPOUND, AIRCRAFT, EXTERIOR |
| SAE AMS3263A | Sealing Compound, Polythioether, Ambient Cure or Immediate Heat Cure For Aircraft Structures, Fuel Resistant with Intermittent Use to 400°CF (204°CC) |
| PREN 2608 : 200P1 | AEROSPACE SERIES - INSTALLATION AND REMOVAL REQUIREMENTS FOR 8 DEGREES 30 MINUTES ADAPTORS, THREADED WITH LOCKRING |
| SAE ARP 4943 : 2008 | GROUND SUPPORT EQUIPMENT HYDRAULIC SYSTEMS, DESIGN AND INSTALLATION, RECOMMENDED PRACTICES FOR |
| SAE MA2079 | Hose Assembly, Convoluted Polytetrafluoroethylene, High Temperature, Medium Pressure, Aircraft, Metric |
| SAE AS5363A | Electromechanical Power Controller/Relay, General Specification For |
| SAE MA4623 | Hose Assembly, Polytetrafluoroethylene, Para Aramid Reinforced Heavy-Duty, 21 000 kPa, 135 °C, Aircraft Hydraulic Systems, Metric |
| ASTM D 5306 : 1992 : R2013 | Standard Test Method for Linear Flame Propagation Rate of Lubricating Oils and Hydraulic Fluids |
| I.S. EN 2350:1991 | AEROSPACE SERIES - CIRCUIT BREAKERS - TECHNICAL SPECIFICATION |
| FED-STD-313 Revision D:1996 | MATERIAL SAFETY DATA, TRANSPORTATION DATA AND DISPOSAL DATA FOR HAZARDOUS MATERIALS FURNISHED TO GOVERNMENT ACTIVITIES |
| PPP-C-96 Revision E:1992 | CAN, METAL, 28 GAGE AND LIGHTER |
| ASTM D 892 : 2013-07 | TEST METHOD FOR FOAMING CHARACTERISTICS OF LUBRICATING OILS |
| MIL-STD-290 Revision H:2013 | PACKAGING AND MARKING OF PETROLEUM AND RELATED PRODUCTS |
| 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 |
| 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 |
| MIL-STD-105 Revision E:1989 | SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES |
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