PUMP UNITS, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

10-04-2013

Publisher

SAE International

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 AS 5994 : 2000

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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)