AIRCRAFT HYDRAULIC STARTER/PUMPS

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

10-28-2013

Publisher

SAE International

1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 NOTES
APPENDIX I
APPENDIX II

Establishes the common requirements for hydraulic units capable functioning as starters and as pumps suitable for use in aircraft and missiles and the methods to be used for demonstrating compliance with these requirements.

Committee	A-6C4
DocumentType	Standard
Pages	13
ProductNote	THIS VERSION IS NOW STABILIZED
PublisherName	SAE International
Status	Current
Supersedes	SAE AS 838 : 1968

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SAE AMS2474 : 2013	CHEMICAL TREATMENT FOR ALUMINUM ALLOYS, LOW ELECTRICAL RESISTANCE COATING
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SAE AMS 2406 : 2015	PLATING, CHROMIUM, HARD DEPOSIT
MIL-H-8775 Revision D:1976	HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR
MIL-P-6906 Revision B:1969	PLATE, IDENTIFICATION AIRCRAFT
MIL-STD-100 Revision G:1997	ENGINEERING DRAWINGS
MIL-P-116 Revision J:1988	PRESERVATION, METHODS OF
SAE AMS 2400 : 2013	PLATING, CADMIUM
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SAE AMS 2403 : 2015	PLATING, NICKEL, GENERAL PURPOSE
MIL-P-19692 Revision E:1994	PUMPS, HYDRAULIC, VARIABLE FLOW, GENERAL SPECIFICATION FOR
MIL-H-5440 Revision H:1993	HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR
SAE AMS 2410 : 2010	PLATING, SILVER, NICKEL STRIKE, HIGH BAKE
MIL-C-5501 Revision G:1989	CAP AND PLUG, PROTECTIVE, DUST AND MOISTURE SEAL
MIL-C-11796 Revision C:1986	CORROSION PREVENTIVE COMPOUND, PETROLATUM, HOT APPLICATION
SAE AS 478 : 2015	IDENTIFICATION MARKING METHODS
SAE AMS 2470 : 2013	ANODIC TREATMENT OF ALUMINUM ALLOYS, CHROMIC ACID PROCESS
MIL-S-7742 Revision D:1991	SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR