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  • SAE ARP 5794 : 2014

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD

    Available format(s):  Hardcopy, PDF

    Superseded date:  03-06-2018

    Language(s):  English

    Published date:  01-01-2014

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

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

    Abstract - (Show below) - (Hide below)

    Specifies the general design, testing, and safety requirements for aircraft tank mounted fuel booster pumps used for engine fuel feed, transfer, and jettison.

    General Product Information - (Show below) - (Hide below)

    Committee AE-5B
    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By

    Standards Referenced By This Book - (Show below) - (Hide below)

    SAE ARP 6385 : 2017 AIRCRAFT FUEL PUMP MECHANICAL AND ELECTRICAL SAFETY DESIGN
    SAE ARP594 : 2017 FUEL PUMP THERMAL SAFETY DESIGN
    MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA

    Standards Referencing This Book - (Show below) - (Hide below)

    SAE AMS A 21180 : 2011 ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH
    SAE ARP594 : 2016 FUEL PUMP THERMAL SAFETY DESIGN
    MIL-STD-129 Revision R:2014 Military Marking for Shipment and Storage
    SAE AMS QQ P 416 : 2016 PLATING, CADMIUM (ELECTRODEPOSITED)
    MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    FAA AC 20-136 : 2011 AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
    SAE AMS 2175 : 2010 CASTINGS, CLASSIFICATION AND INSPECTION OF
    SAE ARP 8615 : 2011 FUEL SYSTEM COMPONENTS: GENERAL SPECIFICATION FOR
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL-H-8891 Revision A:1978 HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR
    SAE ARP 4754 : 2010 GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
    FAA AC 20-158 : 2014 THE CERTIFICATION OF AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEMS FOR OPERATION IN THE HIGH-INTENSITY RADIATED FIELDS (HIRF) ENVIRONMENT
    SAE AMS 3216 : 2005 ELASTOMER: FLUOROCARBON (FKM) RUBBER HIGH-TEMPERATURE - FLUID RESISTANT LOW COMPRESSION SET 70 TO 80
    MIL-STD-31000 Revision A:2013 TECHNICAL DATA PACKAGES
    SAE ARP594 : 2016 FUEL PUMP THERMAL SAFETY DESIGN
    SAE AMS R 83485 : 2014 RUBBER, FLUOROCARBON ELASTOMER, IMPROVED PERFORMANCE AT LOW TEMPERATURES
    SAE AS 5440 : 2011 HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR
    FAA AC 20-152 : 2005 RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
    MIL-STD-889 Revision C:2016 DISSIMILAR METALS
    SAE J 1926/1 : 2016 CONNECTIONS FOR GENERAL USE AND FLUID POWER - PORTS AND STUD ENDS WITH ASME B1.1 THREADS AND O-RING SEALING - PART 1: THREADED PORT WITH O-RING SEAL IN TRUNCATED HOUSING
    MIL-STD-464 Revision C:2010 ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
    ASTM D 910 : 2017-05 SPECIFICATION FOR LEADED AVIATION GASOLINES
    SAE ARP 5316 : 2014 STORAGE OF ELASTOMER SEALS AND SEAL ASSEMBLIES WHICH INCLUDE AN ELASTOMER ELEMENT PRIOR TO HARDWARE ASSEMBLY
    SAE AS 8879 : 2004 SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER
    MIL-STD-882 Revision E:2012 STANDARD PRACTICE FOR SYSTEM SAFETY
    MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    MIL-DTL-83133 Revision J:2015 TURBINE FUEL, AVIATION, KEROSENE TYPE, JP-8 (NATO F-34), NATO F-35, AND JP-8+100 (NATO F-37)
    SAE AS 50881 : 2015 WIRING AEROSPACE VEHICLE
    SAE ARP 1401 : 2012 AIRCRAFT FUEL SYSTEM AND COMPONENT ICING TEST
    FAA AC 20-155 : 2013 INDUSTRY DOCUMENTS TO SUPPORT AIRCRAFT LIGHTNING PROTECTION CERTIFICATION
    FAA AC 25.1309-1 : 0 SYSTEM DESIGN AND ANALYSIS
    MIL-STD-202 Revision H:2015 ELECTRONIC AND ELECTRICAL COMPONENT PARTS
    SAE AMS P 5315 : 2013 ACRYLONITRILE-BUTADIENE (NBR) RUBBER FOR FUEL-RESISTANT SEALS 60 TO 70
    FAA AC 20-115 : 2017 AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
    FAA AC 25.981-1 : 2008 FUEL TANK IGNITION SOURCE PREVENTION GUIDELINES
    MIL-PRF-6855 Revision F:2009 RUBBER, SYNTHETIC, SHEETS, STRIPS, MOLDED OR EXTRUDED SHAPES, GENERAL SPECIFICATION FOR
    MIL-DTL-25988 Revision C:2006 RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, SHEETS, STRIPS, MOLDED PARTS, AND EXTRUDED SHAPES
    SAE AIR 4246 : 2012 CONTAMINANTS FOR AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT TESTING
    MIL-S-7742 Revision D:1991 SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR
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