MIL H 25579 : E
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR
Available format(s)
PDF
Superseded date
25-09-2003
Language(s)
English
Publisher
Outlines specifications for such hose assemblies, for use in fuel, water-alcohol, lubricating oil, hydraulic and pneumatic systems.
DocumentType |
Standard
|
Pages |
30
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
Superseded
|
SupersededBy |
MIL-I-83294 Base Document:1971 | INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR |
JSGS-87231 Revision A:1995 | ENGINES, AIRCRAFT, TURBINE |
MIL-P-26292 Revision C:1969 | PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF |
MIL-E-17341 Revision C:1970 | ENGINE, GAS TURBINE, PROPULSION & AUXILIARY NAVAL SHIPBOARD |
MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
MIL-T-46603 Revision A:1969 | THRUSTER, CARTRIDGE ACTUATED, M19, ASSEMBLY |
MIL-H-25475 Revision B:1971 | HYDRAULIC SYSTEM, MISSILE, DESIGN, INSTALLATION TESTS AND DATE REQUIREMENTS, GENERAL REQUIREMENTS FOR |
MIL-T-46604 Revision B:1993 | THRUSTER, CARTRIDGE ACTUATED, M13, ASSEMBLY |
MIL-C-60224 Base Document:1965 | CARTRIDGE, INITIATOR, XM201 ASSEMBLY |
MIL-C-7413 Revision B:1970 | COUPLING, QUICK DISCONNECT, AUTOMATIC SHUTOFF, GENERAL SPECIFICATION FOR |
MIL P 87220 : 0 | PROPELLANT, AND EXPLOSIVE SYSTEMS, AIRCRAFT CREW ESCAPE REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT PATTERSON, AFB OH 45433-6503 |
MIL-H-5440 Revision H:1993 | HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
MIL-C-83124 Base Document:1969 | CARTRIDGE ACTUATED DEVICES PROPELLANT ACTUATED DEVICES GENERAL DESIGN SPECIFICATION FOR |
MIL-C-60604 Revision A:1992 | CARTRIDGE, THRUSTER, M119 |
MIL-DTL-9479 Revision E:1999 | |
SAE ARP 4925 : 2014 | AEROSPACE DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT HELICOPTER HYDRAULIC SYSTEMS |
MIL-I-18802 Revision A:1962 | INSTALLATION OF FUEL AND OIL LINES, AIRCRAFT |
MIL-I-60221 Base Document:1965 | INITIATOR, CARTRIDGE ACTUATED, XM98 ASSEMBLY |
MIL-I-48404 Base Document:1973 | INITIATOR, PROPELLANT ACTUATED, DELAY, JAU-9/A ASSEMBLY |
MIL-C-14810 Base Document:1969 | CARTRIDGE, DELAY, XM86, ASSEMBLY |
MIL-DTL-50714 Revision C:2004 | INITIATOR, PROPELLANT ACTUATED, DELAY, M113 ASSEMBLY |
MIL S 9479 : C | |
SAE AS 1896 : 2013 | COUPLING ASSEMBLY, SELF-SEALING, ONE SIDE ONLY, HYDRAULIC |
SAE AS 1969 : 2013 | COUPLING ASSEMBLY, SELF-HEALING, QUICK DISCONNECT FUEL AND OIL SYSTEM COMPONENTS |
MIL-I-48410 Base Document:1974 | INITIATOR, PROPELLANT ACTUATED, DELAY, JAU-4/A25 ASSEMBLY |
SAE AS 18802 : 2013 | FUEL AND OIL LINES, AIRCRAFT, INSTALLATION OF |
MIL-STD-1290 Revision A:1988 | LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE |
SAE AS 4897 : 1994 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE (PTFE), LOW PRESSURE, 450 DEGREES F AND FIREPROOF, PROCUREMENT SPECIFICATION FOR |
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SAE AS 1709 : 2014 | COUPLING ASSEMBLY, HYDRAULIC SELF SEALING, QUICK DISCONNECT |
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SAE ARP 603 : 1985 | IMPULSE TESTING OF HYDRAULIC HOSE, TUBING, AND FITTING ASSEMBLIES |
SAE AS 611F : 2010 | HOSE ASSEMBLY AND TUBING, POLYTETRAFLUOROETHYLENE, CLEANING METHODS FOR |
ASTM A 262 : 2015 : REDLINE | Standard Practices for Detecting Susceptibility to Intergranular Attack in Austenitic Stainless Steels |
MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
MIL-T-6845 Revision D:1985 | TUBING, STEEL, CORROSION-RESISTANT (304) AEROSPACE VEHICLE HYDRAULIC SYSTEM 1/8 HARD CONDITION |
MIL H 27267 : B | HOSE TETRAFLUOROETHYLENE, HIGH TEMPERATURE, MEDIUM PRESSURE |
NAS1760:2015 | FITTING END, FLARELESS ACORN, STANDARD DIMENSIONS FOR |
MS8009 Revision D:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PERMANENTLY ATTACHED FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLANGE-TO-FLANGE |
MIL P 775 : D | PACKAGING OF HOSE, HOSE ASSEMBLY, RUBBER PLASTIC, FABRIC, OR METAL [INCLUDING TUBING] AND FITTINGS, NOZZLES AND STRAINERS |
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MIL-T-8808 Revision B:1981 | TUBING, STEEL, CORROSION RESISTANT (18.8 STABILIZED) AIRCRAFT HYDRAULIC QUALITY |
MIL-A-22771 Revision D:1984 | ALUMINUM ALLOY FORGINGS, HEAT TREATED |
MS8004 Revision E:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, REUSABLE FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLANGE-TO-FLANGE |
SAE AMS 5643 : 2016 | STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, MECHANICAL TUBING, AND RINGS, 16CR - 4.0NI - 0.30CB (NB) - 4.0CU, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
SAE AMS 5743 : 2014 | STEEL, CORROSION AND HEAT-RESISTANT, BARS AND FORGINGS 15.5CR - 4.5NI - 2.9MO - 0.10N SOLUTION HEAT TREATED, SUB-ZERO COOLED, EQUALIZED, AND OVER-TEMPERED |
MIL T 5624 : R | TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5 |
SAE AS 1055 : 2013 | FIRE TESTING OF FLEXIBLE HOSE, TUBE ASSEMBLIES, COILS, FITTINGS AND SIMILAR SYSTEM COMPONENTS |
QQ-W-423 Revision B:1969 | FEDERAL SPECIFICATION - WIRE, STEEL, CORROSION RESISTING |
ASTM D 792 : 2013 : REDLINE | Standard Test Methods for Density and Specific Gravity (Relative Density) of Plastics by Displacement |
MS8000 Revision E:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, REUSABLE FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARE-TO-FLARE |
MIL F 27272 : B | FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
QQ A 225/6 : E | ALUMINUM ALLOY BAR, ROD, AND WIRE, ROLLED, DRAWN OR COLD FINISHED, 2024 |
MS8005 Revision E:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PERMANENTLY ATTACHED FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARE-TO-FLARE |
SAE ARP 908 : 2013 | TORQUE REQUIREMENTS, INSTALLATION AND QUALIFICATION TEST, HOSE AND TUBE FITTING |
MS33656 Revision J:1987 | FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL |
WW-T-700-4 Revision F:1983 | TUBE, ALUMINUM ALLOY, DRAWN, SEAMLESS, 5052 |
MIL-STD-831 Base Document:1963 | TEST REPORTS, PREPARATION OF |
SAE AIR 1228 : 2009 | STANDARD IMPULSE MACHINE EQUIPMENT AND OPERATION |
MS8007 Revision D:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PERMANENTLY ATTACHED FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARE-TO-FLANGE |
TT-S-735 Revision A:1988 | STANDARD TEST FLUIDS, HYDROCARBON |
MIL H 83282 : C | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, AIRCRAFT, METRIC, NATO CODE NUMBER H 537 |
QQ A 225/4 : E | ALUMINUM ALLOY BAR, ROD, WIRE, AND SPECIAL SHAPES, ROLLED DRAWN, OR COLD FINISHED, 2014 |
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MS8008 Revision D:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PERMANENTLY ATTACHED FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARELESS-TO-FLANGE |
MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
QQ-S-763 Revision F:1996 | STEEL BARS, WIRE, SHAPES AND FORGINGS; CORROSION 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 H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
MS21900 Revision E:1988 | ADAPTOR FLARELESS TUBE TO A FLARED TUBE |
QQ A 225/8 : E | ALUMINUM ALLOY 6061, BAR, ROD, WIRE & SPECIAL SHAPES, ROLLED, DRAWN OR COLD FINISHED |
SAE AMS5644E:1964(S2017) | STEEL, BARS AND FORGINGS, CORROSION RESISTANT, 17CR - 7NI - 1AL |
MS33514 Revision G:1990 | FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (ASG) |
MS8006 Revision D:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PERMANENTLY ATTACHED FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARELESS-TO-FLARELESS |
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