SAE AS5994A
Current
Current
The latest, up-to-date edition.
PUMP UNITS, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
04-10-2013
Publisher
This specification establishes the common requirements for variable delivery electric motor driven, hydraulic pump units, suitable for use in aircraft hydraulic systems.
Committee |
A-6C4
|
DocumentType |
Standard
|
Pages |
35
|
ProductNote |
This standard is now stabilized
|
PublisherName |
SAE International
|
Status |
Current
|
Supersedes |
SAE ARP4752B | AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS |
SAE ARP4925B | AEROSPACE DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT HELICOPTER HYDRAULIC SYSTEMS |
SAE ARP 6154 : 2017 | AEROSPACE FLUID POWER ELECTROHYDROSTATIC MODULE, DESIGN, PERFORMANCE AND TEST RECOMMENDATIONS |
MIL-H-8890 Base Document:1961 | HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG] |
MIL-H-8891 Revision A:1978 | HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
MIL M 7793 : F | METER, TIME TOTALIZING |
QQ-C-320 Revision B:1974 | CHROMIUM PLATING (ELECTRODEPOSITED) |
MIL-T-10727 Revision C:1989 | TIN PLATING, ELECTRODEPOSITED OR HOT-DIPPED FOR FERROUS AND NONFERROUS METALS |
QQ-S-365 Revision D:1985 | SILVER PLATING, ELECTRODEPOSITED, GENERAL REQUIREMENTS FOR |
MIL-M-8609 Revision B:1965 | MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR |
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 |
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 |
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-5440 Revision H:1993 | HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
MIL-B-5087 Revision B:1964 | BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
QQ-N-290 Revision A:1971 | NICKEL PLATING (ELECTRODEPOSITED) |
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