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  • SAE ARP 4028 : 2014

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    AIRCRAFT/ENGINE FUEL PUMP TWO PHASE (SLUGGING FLOW) INLET PERFORMANCE TEST AND EVALUATION

    Available format(s):  Hardcopy, PDF

    Superseded date:  02-05-2020

    Language(s):  English

    Published date:  01-01-2014

    Publisher:  SAE International

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

    FOREWORD
    1. SCOPE
    2. APPLICABLE DOCUMENTS
    3. TECHNICAL REQUIREMENTS/CONSIDERATIONS
    4. TECHNICAL REQUIREMENTS
    5. DETAILED REQUIREMENTS
    6. TEST DATA
    7. TEST PROCEDURE

    Abstract - (Show below) - (Hide below)

    Pertains to all engine or airframe mounted fuel pumps and controls when required by the applicable specification.

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

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    Status Superseded
    Superseded By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

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

    SAE MAP 749 : 2015 AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT ENDURANCE TEST PROCEDURE (ROOM TEMPERATURE CONTAMINATED FUEL)
    MIL T 5624 : R TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5
    ASTM D 86 : 2017-06 TEST METHOD FOR DISTILLATION OF PETROLEUM PRODUCTS AND LIQUID FUELS AT ATMOSPHERIC PRESSURE
    SAE ARP 492 : 2014 AIRCRAFT ENGINE FUEL PUMP CAVITATION ENDURANCE TEST
    SAE AIR 1326 : 1997 AIRCRAFT FUEL SYSTEM VAPOR-LIQUID RATIO PARAMETER
    MIL-G-5572 Revision F:1969 GASOLINE, AVIATION, GRADES 80/87, 100/130, 115/145
    MIL T 83133 : D TURBINE FUELS, AVIATION, KEROSENE TYPES, NATO F-34 (JP-8) AND NATO F-35
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