ASTM D4305-98a(2004)e1

    Standard Test Method for Filter Flow of Aviation Fuels at Low Temperatures (Withdrawn 2010)

    Withdrawn Standard: ASTM D4305-98a(2004)e1 | Developed by Subcommittee: D02.07

    WITHDRAWN, NO REPLACEMENT


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    Withdrawn Rationale:

    This test method covers the determination of low temperature flow behavior, through a screen-type test filter, of aviation turbine fuels, which can contain separated solids as wax.

    This test method is being balloted for withdrawal with no replacement because it has been removed as a Referenced Document from Specification D1655 by Subcommittee D02.J0 due to its inability to detect contamination in jet fuel.

    Formerly under the jurisdiction of Committee D02 on Petroleum Products and Lubricants, this test method was withdrawn in May 2010.

    1. Scope

    1.1 This test method covers the determination of low temperature flow behavior, through a screen-type test filter, of aviation turbine fuels, which can contain separated solids as wax.

    1.2 Procedure A employs a 26-μm test filter and is the recommended procedure. Some existing instruments are fitted with a 42-μm filter, and Procedure B is retained to enable their continued use.

    1.3 The use of Procedure A (26-μm test filter) with fuels that have a viscosity of greater than 5.0 mm2/s (cSt) at -20°C, as determined by Test Method D 445, can affect the precision and the simulated freezing point obtained on such fuels and can give a higher (warmer) result than the conventional freezing point obtained by Test Method D 2386.

    Note 1—The principle of this test method relies on flow through a fine-mesh test filter, and, hence, the result can be affected by the viscosity of the sample. When using Procedure A, a no-flow condition is reached when crystals block the test filter or the viscosity exceeds about 14 mm2/s (cSt); sample with a viscosity of greater than 5 mm2/s (cSt) at -20°C may exceed the 14-mm2/s (cSt) threshold at a temperature before crystals are formed. If viscosity affects the result before crystals are formed, then the reported value of the no-flow temperature of the sample will always be warmer than the actual freezing point, and therefore fail-safe and an indicator of possible flow anomalies at low temperature.

    1.4 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.



    2. Referenced Documents (purchase separately) The documents listed below are referenced within the subject standard but are not provided as part of the standard.

    ASTM Standards

    D445 Test Method for Kinematic Viscosity of Transparent and Opaque Liquids (the Calculation of Dynamic Viscosity)

    D1655 Specification for Aviation Turbine Fuels

    D2386 Test Method for Freezing Point of Aviation Fuels

    D4057 Practice for Manual Sampling of Petroleum and Petroleum Products


    Referencing This Standard

    DOI: 10.1520/D4305-98AR04E01

    ASTM International is a member of CrossRef.

    Citation Format

    ASTM D4305-98a(2004)e1, Standard Test Method for Filter Flow of Aviation Fuels at Low Temperatures (Withdrawn 2010), ASTM International, West Conshohocken, PA, 2004, www.astm.org

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