• SAE MA 2078 : 1992

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

    TEST METHODS, HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE (PTFE), METRIC

    Available format(s):  Hardcopy, PDF

    Superseded date:  24-04-2009

    Language(s):  English

    Published date:  01-01-1992

    Publisher:  SAE International

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

    1 SCOPE AND FIELD OF APPLICATION
    2 REFERENCES
    3 TEST ON PTFE INNER TUBES
    4 HOSE AND HOSE ASSEMBLY TESTS
    APPENDIX A TEST FLUIDS AND MATERIALS

    Abstract - (Show below) - (Hide below)

    Defines the test methods for flexible PTFE hose and hose assemblies used in aircraft fluid systems in the pressure and temperature ranges defined in MA2001.

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

    Committee G-3
    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By
    Supersedes

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

    SAE MA 2126 : 2015 HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE (PTFE), UP TO 232 DEGREES C AND 10 500 KPA PROCUREMENT SPECIFICATION, METRIC
    SAE MA 4098 : 2015 HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, HEAVY DUTY, METALLIC REINFORCED, 204 DEGREE C, 35000 KPA, HYDRAULIC AND PNEUMATIC, METRIC
    SAE MA 1339 : 2015 HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 21,000 KPA, 204 DEGREE C, LIGHTWEIGHT, HYDRAULIC AND PNEUMATIC, METRIC
    SAE MA 1975 : 2015 HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID REINFORCED, 135 DEGREE C, STANDARD DUTY, 28000/21000 KPA, HYDRAULIC, AIRCRAFT SYSTEMS
    SAE MA 620 : 2015 HOSE ASSEMBLIES, CONVOLUTED POLYTETRAFLUOROETHYLENE METALLIC REINFORCED, HIGH TEMPERATURE, MEDIUM PRESSURE, AIRCRAFT METRIC
    SAE MA 614 : 2015 HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE (PTFE), METALLIC REINFORCED, 28,000 KPA, 204 DEGREES C, HYDRAULIC, METRIC
    SAE MA 4623 : 2015 Hose Assembly, Polytetrafluoroethylene, Para Aramid Reinforced Heavy-Duty, 21 000 kPa, 135 °C, Aircraft Hydraulic Systems, Metric
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