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  • MIL-P-85315 Base Document:1979

    Current The latest, up-to-date edition.

    Pump, Ejector, Air Vehicle Fuel, General Specification For

    Available format(s):  PDF

    Language(s): 

    Published date:  30-03-1979

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Defines minimum requirements for air vehicle fuel ejector pumps, regardless of application (transfer, boost, scavenge, etc.), configuration (multiple stage, multiple nozzle, variable geometry etc.), or auxiliary features (check valves, motive flow shut off valves, negative "G" provisions, etc.).

    Scope - (Show below) - (Hide below)

    This specification defines minimum requirements for air vehicle fuel ejector pumps, regardless of application (transfer, boost, scavenge, etc.), configuration (multiple nozzle, multiple stage,variable geometry, etc.), or auxiliary features (check valves, motive flow shut off valves, negative \"G\" provisions, etc.).

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

    Development Note INACTIVE FOR NEW DESIGN 28/8/96
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Current

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

    MIL-R-83248 Revision C:1994 RUBBER, FLUOROCARBON ELASTOMER, HIGH TEMPERATURE, FLUID, AND COMPRESSION SET RESISTANT
    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-P-7105 Revision B:1965 PIPE THREADS, TAPER, AERONAUTICAL NATIONAL FORM, SYMBOL ANPT. GENERAL REQUIREMENTS FOR
    PPP-B-636 Revision J:1981 BOX, SHIPPING, FIBERBOARD
    MIL T 5624 : R TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5
    MIL S 5002 : D SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS
    MS29513 Revision C:1966 PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT, O RING
    MIL P 15024 : E PLATES, TAGS AND BANDS FOR IDENTIFICATION OF EQUIPMENT
    MIL-STD-889 Revision C:2016 DISSIMILAR METALS
    MIL C 7024 : D CALIBRATING FLUID, AIRCRAFT FUEL SYSTEM COMPONENTS
    MS33656 Revision J:1987 FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL
    MS29512 Revision C:1965 PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT TUBE FITTING 0 RING
    MS33588 Revision E:1984 NUTS, SELF LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR
    TT-S-735 Revision A:1988 STANDARD TEST FLUIDS, HYDROCARBON
    MS20995 Revision E:1974 WIRE, SAFETY OR LOCK
    MIL-G-5572 Revision F:1969 GASOLINE, AVIATION, GRADES 80/87, 100/130, 115/145
    MIL R 25988 : B RUBBER, FLUOROSILICONE ELASTOMER, OIL AND FUEL RESISTANT, SHEETS, STRIPS, MOLDED PARTS AND EXTRUDED SHAPES
    PPP-B-591 Revision B:1971 BOXES, SHIPPING, FIBERBOARD, WOOD-CLEATED
    MIL-STD-143 Revision B:1969 STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
    MIL-S-8879 Revision C:1991 SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR
    MIL A 8625 : F ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
    MIL-STD-1523 Revision A:1984 AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIAL
    MIL-A-21180 Revision D:1984 ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH
    MIL-P-116 Revision J:1988 PRESERVATION, METHODS OF
    PPP-B-601 Revision H:1989 BOXES, WOOD, CLEATED PLYWOOD
    MIL T 83133 : D TURBINE FUELS, AVIATION, KEROSENE TYPES, NATO F-34 (JP-8) AND NATO F-35
    MIL-F-8615 Revision D:1976 FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG]
    QQ-P-416 Revision F:1991 PLATING, CADMIUM (ELECTRODEPOSITED)
    PPP-B-621 Revision D:1981 BOXES, WOOD, NAILED AND LOCK CORNER
    MIL-F-27351 Base Document:1960 FLUID, CALIBRATING, HIGH FLASH POINT, AIRCRAFT FUEL SYSTEM COMPONENTS
    MIL C 6021 : H NOTICE 1 CASTINGS, CLASSIFICATION AND INSPECTION OF
    MIL-S-7742 Revision D:1991 SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR
    MIL N 25027 : G NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F
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