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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR
Available format(s)
PDF
Language(s)
English
Publisher
Superseded date
25-09-2003
Superseded by
£13.91
Excluding VAT
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Superseded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 (No S/S Document) |
| JSGS-87231 Revision A:1995 | Engines, Aircraft, Turbine (S/S by JSSG-2007) |
| MIL-P-26292 Revision C:1969 | PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF (NO S/S DOCUMENT) |
| MIL-E-17341 Revision C:1970 | Engine, Gas Turbine, Propulsion and 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 (NO S/S DOCUMENT) |
| MIL-H-25475 Revision B:1971 | Hydraulic Systems, Missile Design, Installation and Tests, General Requirements for (No S/S Document) |
| MIL-T-46604 Revision B:1993 | Thruster, Cartridge Actuated, M13 Assembly |
| MIL-C-60224 Base Document:1965 | Cartridge, Initiator, XM201 Assembly (No S/S Document) |
| MIL-C-7413 Revision B:1970 | Coupling, Quick Disconnect, Automatic Shutoff, General Specification for (S/S by SAE-AS7413) |
| 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, Design and Installation Requirements for (S/S by SAE-AS5440) |
| MIL-C-83124 Base Document:1969 | Cartridge Actuated Devices/Propellant Actuated Devices General Design Specification for |
| MIL-C-60604 Revision A:1992 | Cartridge, Impulse, M119 Assembly |
| MIL-DTL-9479 Revision E:1999 | Seat System, Upward Ejection, Aircraft, General Specification for |
| SAE ARP4925B | Aerospace Design and Installation of Commercial Transport Helicopter Hydraulic Systems |
| MIL-I-18802 Revision A:1962 | Installation of Fuel and Oil Lines, Aircraft (S/S by SAE-AS18802) |
| MIL-I-60221 Base Document:1965 | Initiator, Cartridge Actuated, XM98 Assembly (No S/S Document) |
| MIL-I-48404 Base Document:1973 | Initiator, Propellant Actuated, Delay, JAU-9/A Assembly (No S/S Document) |
| MIL-C-14810 Base Document:1969 | Cartridge, Delay, XM86, Assembly (No S/S Document) |
| MIL-DTL-50714 Revision C:2004 | Initiator, Propellant Actuated, Delay, M113 Assembly |
| MIL S 9479 : C | |
| SAE AS1896A | Coupling Assembly, Self-Sealing, One Side Only, Hydraulic |
| SAE AS1969 | Coupling Assembly, Self-Sealing, Quick Disconnect Fuel and Oil System Components |
| MIL-I-48410 Base Document:1974 | Initiator, Propellant Actuated, Delay, JAU-4/A25 Assembly |
| SAE AS18802 | Fuel and Oil Lines, Aircraft, Installation of |
| MIL-STD-1290 Revision A:1988 | Light Fixed and Rotary-Wing Aircraft Crash Resistance |
| SAE AS4897 | Hose Assembly, Polytetrafluoroethylene (PTFE), Low Pressure, 450 °F and Fireproof, Procurement Specification for |
| DIN 9462:1987-08 | AEROSPACE; HOSE ASSEMBLIES; SURVEY |
| SAE AS1709A | Coupling Assembly, Hydraulic Self Sealing, Quick Disconnect |
| SAE AMS5689F | Steel, Corrosion and Heat Resistant, Wire 18Cr - 10.5Ni - 0.40Ti (SAE 30321) Solution Heat Treated |
| MIL L 7808 : K (1) | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
| SAE ARP603G | Impulse Testing of Hydraulic Hose, Tubing, and Fittings Assemblies |
| SAE AS611E | 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 (S30400), AEROSPACE VEHICLE HYDRAULIC SYSTEM 1/8 HARD CONDITION (S/S BY SAE-AMS-T-6845) |
| MIL H 27267 : B | HOSE TETRAFLUOROETHYLENE, HIGH TEMPERATURE, MEDIUM PRESSURE |
| MS8009 Revision D:2016 | Hose Assembly, Polyetetrafluorethylene, 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 |
| MS8002 Revision E:2016 | Hose Assembly, Polytetrafluoroethylene, Reusable Fittings, High Temperature, Medium Pressure, Flare-to-Flange |
| MIL-T-8808 Revision B:1981 | TUBING, STEEL, CORROSION-RESISTANT (18-8 STABILIZED), AIRCRAFT HYDRAULIC QUALITY (USE SAE-AMS5556 AND SAE-AMS5557) |
| MIL-A-22771 Revision D:1984 | Aluminum Alloy Forgings, Heat Treated (S/S by SAE-AMS-A-22771) |
| MS8004 Revision E:2016 | Hose Assembly, Polytetrafluoroethylene, Reusable Fittings, High Temperature, Medium Pressure, Flange-to-Flange |
| SAE AMS5643U | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings 16Cr - 4.0Ni - 0.30Cb (Nb) - 4.0Cu Solution Heat Treated, Precipitation Hardenable |
| SAE AMS5743J | 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 AS1055D | Fire Testing of Flexible Hose, Tube Assemblies, Coils, Fittings, and Similar System Components |
| QQ-W-423 Revision B:1969 | Wire, Steel, Corrosion-Resisting (S/S by ASTM-A313 and ASTM-A580) |
| 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 ARP908C | 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 (S/S BY SAE-AS4395) |
| WW-T-700-4 Revision F:1983 | TUBE, ALUMINUM ALLOY, DRAWN, SEAMLESS, 5052 (S/S BY SAE-AMS-WW-T-700/4) |
| MIL-STD-831 Base Document:1963 | TEST REPORTS, PREPARATION OF |
| 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 (S/S BY ASTM-D471) |
| 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 |
| MS8003 Revision E:2016 | Hose Assembly, Polytetrafluoroethylene, Reusable Fittings, High Temperature, Medium Pressure, Flareless-to-Flange |
| MS8001 Revision E:2016 | Hose Assembly, Polyetrafluorothylene, Reusable Fittings, High Temperature, Medium Pressure, Flareless-to-Flareless |
| MIL-S-8879 Revision C:1991 | Screw Threads, Controlled Radius Root withIncreased Minor Diameter, General Specification for (S/S by SAE-AS8879) |
| MS8008 Revision D:2016 | Hose Assembly, Polytetrafluorethylene, 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 (S/S BY SAE-AMS-QQ-S-763) |
| 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 | ADAPTER, FLARELESS TUBE TO A FLARED TUBE (S/S BY SAE-AS21900) |
| QQ A 225/8 : E | ALUMINUM ALLOY 6061, BAR, ROD, WIRE & SPECIAL SHAPES, ROLLED, DRAWN OR COLD FINISHED |
| SAE AMS5644E | Steel, Bars and Forgings, Corrosion Resistant 17Cr - 7Ni - 1Al |
| MS33514 Revision G:1990 | FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (S/S BY SAE-AS33514) |
| MS8006 Revision D:2016 | Hose Assembly, Polytetrafluoroethylene, Permanently Attached Fittings, High Temperature, Medium Pressure, Flareless-to-Flareless |
Summarise
£13.91
Excluding VAT
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