MIL-H-25475 Revision B:1971
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
HYDRAULIC SYSTEM, MISSILE, DESIGN, INSTALLATION TESTS AND DATE REQUIREMENTS, GENERAL REQUIREMENTS FOR
Available format(s)
PDF
Withdrawn date
09-09-1993
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Details design, installation, and testing of the above systems.
| DocumentType |
Standard
|
| Pages |
36
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| MIL V 81940 : B | VALVE, SAMPLING AND BLEED, HYDRAULIC, TYPE LI SYSTEMS |
| 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 F 83861 : B | FILTER ELEMENTS, NONCLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE, TYPE 1I, SYSTEMS GENERAL SPECIFICATION FOR |
| MIL-D-8684 Revision B:1959 | DATA AND TESTS, ENGINEERING, CONTACT REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE SYSTEMS |
| MIL-H-8775 Revision D:1976 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
| MIL-R-8931 Revision A:1994 | RESERVOIRS, AIRCRAFT AND MISSILE, HYDRAULIC SEPARATED TYPE |
| MIL F 83860 : C | FILTER ELEMENTS, NONCLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 MICRON ABSOLUTE, TYPE II, SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-D-8685 Revision B:1967 | DATA AND TESTS, ENGINEERING, CONTRACT REQUIREMENTS FOR GUIDED MISSILE TARGET SYSTEMS |
| MIL-T-7081 Revision D:1965 | TUBE, ALUMINUM ALLOY, SEAMLESS, ROUND, DRAWN, 6061, AIRCRAFT HYDRAULIC QUALITY |
| MIL-F-45764 Revision C:1990 | FLUID LINES & FITTINGS FOR MISSILES & RELATED GROUND EQUIPMENT, FABRICATION & INSTALLATION OF |
| MIL-T-18232 Revision B:1968 | TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
| MIL R 25534 : A NOTICE 1 | ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR |
| MIL-STD-1606 Revision A:1983 | TECHNICAL INFORMATION REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE PROPOSALS |
| MIL R 25532 : A | ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| MIL-F-18280 Revision F:1995 | FITTING, FLARELESS TUBE, FLUID CONNECTION |
| MIL-T-6845 Revision D:1985 | TUBING, STEEL, CORROSION-RESISTANT (304) AEROSPACE VEHICLE HYDRAULIC SYSTEM 1/8 HARD CONDITION |
| MIL J 5513 : C | JOINT, HYDRAULIC SWIVEL |
| MIL C 25427 : A | COUPLING ASSEMBLY, HYDRAULIC, SELF-SEALING, QUICK DISCONNECT |
| MIL-M-7997 Revision C:1981 | Motor, Aircraft Hydraulic, Constant Displacement General Specification for |
| MIL-H-38360 Revision B:1966 | HOSE, ASSEMBLIES, TETRAFLUOROETHYLENE, HIGH-TEMPERATURE, HIGH PRESSURE, 3000 PSI HYDRAULIC AND PNEUMATIC |
| MIL-W-8160 Revision D:1961 | WIRING, GUIDED MISSILE, INSTALLATION OF, GENERAL SPECIFICATION FOR |
| MIL H 25579 : E | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL A 5498 : D | ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
| AN929 Revision 14:2017 | CAP INSERT, ASSEMBLY, PRESSURE SEAL, FLARED TUBE FITTING |
| MS24334 Revision E:1992 | COUPLING ASSEMBLY, HYDRAULIC, SELF-SEALING, FLARELESS FITTING TO INTERNAL THREAD BOSS |
| MS21919 Revision E:1981 | CLAMP, LOOP TYPE, CUSHIONED, SUPPORT |
| MS33620 Revision B:1964 | CHART, HOSE SELECTION |
| 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 |
| MS33566 Revision B:1975 | FITTING, INSTALLATION OF FLARELESS TUBE, STRAIGHT THREADED CONNECTOR |
| MIL-G-5514 Revision G:1993 | GLAND DESIGN, PACKINGS, HYDRAULIC GENERAL REQUIREMENTS FOR |
| MIL H 6083 : E | HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION |
| MS33583 Revision C:1993 | TUBING END, DOUBLE FLARE, STANDARD DIMENSIONS FOR |
| MIL-F-5509 Revision D:1978 | FITTING, FLARED TUBE, FLUID CONNECTION |
| MS33584 Revision C:1990 | TUBING END, STANDARD DIMENSIONS FOR FLARED |
| MIL-STD-100 Revision G:1997 | ENGINEERING DRAWINGS |
| MIL V 5523 : D | VALVE, RELIEF, HYDRAULIC PRESSURE |
| MS33611 Revision A:1983 | TUBE BEND RADII |
| MIL G 8348 : H | GAGE, ASSEMBLIES, AIR PRESSURE, DIAL INDICATING CHUCK TYPE SELF CONTAINED |
| MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
| MIL-STD-1247 Revision D:2009 | MARKINGS, FUNCTIONS AND HAZARDS DESIGNATIONS OF HOSE, PIPE, AND TUBE LINES FOR AIRCRAFT MISSILE, AND SPACE SYSTEMS |
| MIL-B-5087 Revision B:1964 | BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
| MIL-T-7081 Revision D:1965 | TUBE, ALUMINUM ALLOY, SEAMLESS, ROUND, DRAWN, 6061, AIRCRAFT HYDRAULIC QUALITY |
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