MIL-P-5994 Revision D:1972
Withdrawn
Pump Units, Hydraulic, Electric Motor Driven, Variable Delivery, General Specification for (No S/S Document)
05-03-1972
11-01-2013
Establishes the common requirements for variable delivery electric motor driven, hydraulic pump units, suitable for use in aircraft hydraulic systems.
| DevelopmentNote |
D NOTICE 1 - Notice of Inactivation for New Design. D NOTICE 2 - Notice of Validation but remains Inactive for New Design. (01/2008) D NOTICE 3 - Notice of Cancellation without Replacement. (11/2013)
|
| DocumentType |
Standard
|
| Pages |
34
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
This specification establishes the common requirements for variable delivery electric motor driven, hydraulic pump units, suitable for use in aircraft hydraulic systems.
| MIL-H-8891 Revision A:1978 | Hydraulic Systems, Manned Flight Vehicles, Type III Design, Installation and Data Requirements for, General Specification for |
| MIL-H-5440 Revision H:1993 | Hydraulic Systems, Aircraft, Design and Installation Requirements for (S/S by SAE-AS5440) |
| 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) |
| MS33540 Revision J:1986 | SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR (S/S BY NASM33540) |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-STD-130 Revision N:2007 | Identification Marking of U.S. Military Property |
| MIL-H-8890 Base Document:1961 | Hydraulic Components, Type III (-65 Degrees to Plus 450 Degrees F) General Specification for (ASG) |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-H-8891 Revision A:1978 | Hydraulic Systems, Manned Flight Vehicles, Type III Design, Installation and Data Requirements for, General Specification for |
| MIL-STD-2073-1 Revision E:2008 | Standard Practice for Military Packaging |
| MS27595 Revision E:2006 | Retainer, Packing Backup, Continuous Ring, Polytetrafluoroethylene |
| MIL M 7793 : F | METER, TIME TOTALIZING |
| MIL-STD-195 Base Document:1955 | MARKING OF CONNECTIONS FOR ELECTRIC ASSEMBLIES (NO S/S DOCUMENT) |
| MS28774 Revision M:2009 | Retainer, Packing Backup, Single Turn, Polytetraflouroethylene |
| MIL P 15024 : E | PLATES, TAGS AND BANDS FOR IDENTIFICATION OF EQUIPMENT |
| MIL-STD-889 Revision C:2016 | Galvanic Compatibility of Electrically Conductive Materials |
| MS28775 Revision E:1984 | PACKING, PREFORMED, HYDRAULIC, +275 DEG. F (\"O\" RING) (S/S BY SAE-AS28775) |
| QQ-C-320 Revision B:1974 | CHROMIUM PLATING (ELECTRODEPOSITED) (S/S BY SAE-AMS-QQ-C-320) |
| MIL-STD-838 Revision C:1983 | LUBRICATION OF MILITARY EQUIPMENT |
| MS28782 Revision E:2006 | Retainer, Packing, Back-up, Teflon |
| MIL-T-10727 Revision C:1989 | TIN PLATING: ELECTRODEPOSITED OR HOT-DIPPED, FOR FERROUS AND NONFERROUS METALS (S/S BY ASTM-B545, ASTM-B339) |
| QQ-S-365 Revision D:1985 | SILVER PLATING, ELECTRODEPOSITED, GENERAL REQUIREMENTS FOR (USERS MAY CONSULT ASTM-B700) |
| MIL-STD-276 Revision A:1992 | Impregnation of Porous Metal Castings and Powdered Metal Components |
| MIL-M-8609 Revision B:1965 | Motor, DC, 28 Volt System, Aircraft, General Specification for |
| MIL-STD-461 Revision G:2015 | Requirements for the Control of Electromagnetic Interference Characteristics of Subsystems and Equipment |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-H-8775 Revision D:1976 | Hydraulic System Components, Aircraft and Missiles General Specification for (S/S by SAE-AS8775) |
| MS28783 Revision F:2006 | Ring, Gasket, Back-up, PTFE |
| MIL-M-7969 Revision C:1965 | Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for |
| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF (S/S BY MIL-STD-2073-1) |
| 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-P-19692 Revision E:1994 | PUMPS, HYDRAULIC, VARIABLE FLOW, GENERAL SPECIFICATION FOR (S/S BY SAE-AS19692) |
| MIL-H-5440 Revision H:1993 | Hydraulic Systems, Aircraft, Design and Installation Requirements for (S/S by SAE-AS5440) |
| MIL-STD-202 Revision H:2015 | Electronic and Electrical Component Parts |
| MIL C 26074 : E | COATINGS, ELECTROLESS NICKEL, REQUIREMENTS FOR |
| MIL-B-5087 Revision B:1964 | Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464) |
| QQ-N-290 Revision A:1971 | NICKEL PLATING (ELECTRODEPOSITED) (S/S BY SAE-AMS-QQ-N-290) |
| MIL-STD-781 Revision D:1986 | RELIABILITY TESTING FOR ENGINEERING DEVELOPMENT, QUALIFICATION AND PRODUCTION |
| MS21344 Revision A:2016 | Fittings - Installationof Flared Tube, Straight, Threaded Connectors, Design Standard for |