MIL-H-5440 Revision H:1993
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Hydraulic Systems, Aircraft, Design and Installation Requirements for (S/S by SAE-AS5440)
Available format(s)
PDF
Published date
25-05-1993
Publisher
Superseded date
01-04-1998
Superseded by
€16.67
Excluding VAT
Gives requirements for types I and II hydraulic systems as follows; -54deg to +71degC (-65deg to +160degF), and -54deg to +135degC (-65deg to +275degF) temperature range.
| DocumentType |
Standard
|
| Pages |
51
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
This specification covers the design and installation requirements for Types I and II aircraft hydraulic systems.
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| MIL V 6164 : E | VALVE, AIRCRAFT, AIR HIGH PRESSURE |
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| SAEITC TS103-2 | TS103 Recommendations for Design Considerations for Aircraft Hydraulic Systems |
| MIL-V-5527 Revision A:1951 | VALVES, AIRCRAFT, HYDRAULIC THERMAL EXPANSION RELIEF |
| MIL-S-8812 Revision D:1975 | Steering System, Aircraft General Requirements for |
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| MIL-T-7081 Revision D:1965 | TUBE, ALUMINUM ALLOY, SEAMLESS, ROUND, DRAWN 6061, AIRCRAFT HYDRAULIC QUAL ITY (S/S BY SAE-AMS-T-7081) |
| MIL-I-8673 Base Document:1955 | Installation and Test of Aircraft Flexible Weapons Systems (No S/S Document) |
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| MIL-C-18244 Revision A:1962 | Control and Stabilization Systems: Automatic, Piloted Aircraft, General Specification for |
| SAE AIR4543C | Aerospace Hydraulics and Actuation Lessons Learned |
| SAE AS838A | Aircraft Hydraulic Starter/Pumps |
| MIL-T-5522 Revision D:1975 | Test Requirementsand Methodsfor Aircraft Hydraulicand Emergency Pneumatic Systems (S/S By MIL-STD-5522) |
| MIL-R-83248 Revision C:1994 | RUBBER, FLUOROCARBON ELASTOMER, HIGH TEMPERATURE, FLUID, AND COMPRESSION SET RESISTANT (S/S BY SAE-AMS7276, SAE-AMS7259, SAE-AMS3216, AND SAE-AMS3218) |
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| MIL H 25579 : E | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL-C-85449-3 Revision B:1987 | CLAMP ASSEMBLY, SADDLE TYPE, CUSHIONED, SILICONE FABRIC, REINFORCED 321 CRES, 500 DEG. F, GENERAL PURPOSE |
| MIL-V-5525 Revision C:1959 | Valves, Aircraft Power Brake |
| MIL-B-8584 Revision C:1970 | Brake Systems, Wheel, Aircraft, Design of |
| MS14169 Revision C:1980 | Circular Spline and Adapter Details Engine Driven Accessories |
| SAE AMS5561G | Steel, Corrosion and Heat-Resistant, Welded and Drawn or Seamless and Drawn Tubing 9.0Mn - 20Cr - 6.5Ni - 0.28N High-Pressure Hydraulic |
| MS27595 Revision E:2006 | Retainer, Packing Backup, Continuous Ring, Polytetrafluoroethylene |
| MIL S 9395 : F | SWITCHES, PRESSURE, [ABSOLUTE, GAGE AND DIFFERENTIAL] GENERAL SPECIFICATION FOR |
| MIL-V-5527 Revision A:1951 | VALVES, AIRCRAFT, HYDRAULIC THERMAL EXPANSION RELIEF |
| MIL-P-83461-2 Base Document:1991 | PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT IMPROVED PERFORMANCE AT 275 DEG. F (135 DEG. C) FOR USE IN BOSS FITTINGS, SIZES AND TOLERANCES (S/S BY SAE-AMS-P-83461/2) |
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| MIL F 27272 : B | FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
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| MIL-F-8815-6 Revision B:1976 | Filter Elements, Noncleanable, Fluid Pressure, Hydraulic Line, 3000 PSI, 5 Micron Absolute, -65 Degree to +275 Degree Fahrenheit |
| MIL-P-5994 Revision D:1972 | Pump Units, Hydraulic, Electric Motor Driven, Variable Delivery, General Specification for (No S/S Document) |
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| SAE ARP 1192 : B1987 (R1991) | PROCEDURE FOR CALIBRATION AND VERIFICATION OF LIQUIDBORNE PARTICLE COUNTER - AN ABSOLUTE STANDARD |
| MIL-H-8775 Revision D:1976 | Hydraulic System Components, Aircraft and Missiles General Specification for (S/S by SAE-AS8775) |
| MIL-STD-2089 Base Document:1981 | AIRCRAFT NONNUCLEAR SURVIVABILITY TERMS (NO S/S DOCUMENT, SEE MIL-HDBK-2089 FOR GUIDANCE) |
| MS33584 Revision C:1990 | TUBING END STANDARD DIMENSIONS FOR FLARED (S/S BY SAE-AS4330) |
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| SAE ARP584C | Coiled Tubing - Corrosion Resistant Steel, Hydraulic Applications, Aerospace |
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| MIL-P-19692 Revision E:1994 | PUMPS, HYDRAULIC, VARIABLE FLOW, GENERAL SPECIFICATION FOR (S/S BY SAE-AS19692) |
| MS33611 Revision A:1983 | TUBE BEND RADII (S/S BY SAE-AS33611) |
| SAE AS4251 | Coupling Assemblies, Non-Locking Probe Style, Self-Aligning, Self-Sealing Disconnects |
| 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 |
| MS14184 Revision A:1980 | Nonmetallic Shaft-Coupling Details, Engine Driven Accessories |
| MIL C 85052/3 : B | CLAMP, LOOP, TUBE 17-7 PH CRES, 500 DEG., F |
| SAE ARP598D | Aerospace Microscopic Sizing and Counting of Particulate Contamination for Fluid Power Systems |
| MIL-R-8931 Revision A:1994 | Reservoirs,Aircraft and Missile, Hydraulic, Separated Type |
| MIL C 85052 : A | CLAMP LOOP, CUSHION, GENERAL SPECIFICATION FOR |
| MIL-P-83461 Revision B:1980 | PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, IMPROVED PERFORMANCE AT 275 DEG. F (135 DEG. C) (S/S BY SAE-AMS-P-83461) |
| MIL-V-19069 Revision B:1986 | Valve, Check, Hydraulic, Aircraft, Type II Systems |
| FED-STD-791 Revision D:2007 | Testing Method of Lubricants, Liquid Fuels, and Related Products |
| MIL F 18372 : 0 | FLIGHT CONTROL SYSTEMS, DESIGN, INSTALLATION AND TEST OF, AIRCRAFT (GENERAL SPECIFICATION FOR) |
| MIL-C-85449 Base Document:1981 | CLAMP ASSEMBLY, SADDLE TYPE, CUSHION, GENERAL SPECIFICATION FOR |
| SAE AS604E | Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 3000 psi, 400 °F, Heavyweight, Hydraulic |
| MIL-STD-1247 Revision D:2009 | Markings, Functions and Hazards Designations of Hose, Pipe, and Tube Lines for Aircraft Missile, and Space Systems |
| MIL-V-29592 Base Document:1993 | VALVE, AIR VENT, AUTOMATIC, HYDRAULIC, LOW PRESSURE TYPE II SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-B-5087 Revision B:1964 | Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464) |
| MIL A 5503 : E | ACTUATOR, AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| MIL H 85800 : 0 | HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID FIBER REINFORCED, 5000 & 8000 PSI, GENERAL SPECIFICATION FOR |
| MIL-T-7081 Revision D:1965 | TUBE, ALUMINUM ALLOY, SEAMLESS, ROUND, DRAWN 6061, AIRCRAFT HYDRAULIC QUAL ITY (S/S BY SAE-AMS-T-7081) |
| MIL-F-85421 Revision B:1986 | FITTINGS, TUBE, FLUID SYSTEMS, SEPARABLE, BEAM SEAM, 3000/4000 PSI - GENERAL SPECIFICATION FOR |
| MS21344 Revision A:2016 | Fittings - Installationof Flared Tube, Straight, Threaded Connectors, Design Standard for |
| MIL-F-7179 Revision G:1993 | Finishes, Coatings, and Sealants for the Protection of Aerospace Weapons Systems (S/S by MIL-STD-7179) |
| MIL-P-83461-1 Revision B:1989 | PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT IMPROVED PERFORMANCE AT 275 DEGREE F (135 DEGREE C) SIZES AND TOLERANCES (S/S BY SAE-AMS-P-83461/1) |
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