Standard Test Method for Determining Filterability of Aviation Turbine Fuel

SIGNIFICANCE AND USE
5.1 This test method is intended for use in the laboratory or field in evaluating aviation turbine fuel cleanliness.  
5.2 A change in filtration performance after storage, pretreatment, or commingling can be indicative of changes in fuel condition.  
5.3 Relative filterability of fuels may vary, depending on filter porosity and structure, and may not always correlate with results from this test method.  
5.4 Causes of poor filterability in industrial/refinery filters include fuel degradation products, contaminants picked up during storage or transfer, incompatibility of commingled fuels, or interaction of the fuel with the filter media. Any of these could correlate with orifice or filter system plugging, or both.
SCOPE
1.1 This test method covers a procedure for determining the filterability of aviation turbine fuels (for other middle distillate fuels, see Test Method D6426). Note 1—ASTM specification fuels falling within the scope of this test method are Specifications D1655 and D6615 and the military fuels covered in the military specifications listed in 2.2.  
1.2 This test method is not applicable to fuels that contain undissolved water.  
1.3 The values stated in SI units are to be regarded as the standard. The values given in parentheses are for information only.  
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.

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Publication Date
14-Jun-2013
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ASTM D6824-13e1 - Standard Test Method for Determining Filterability of Aviation Turbine Fuel
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NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.
Contact ASTM International (www.astm.org) for the latest information
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Designation: D6824 − 13 An American National Standard
Standard Test Method for
1
Determining Filterability of Aviation Turbine Fuel
This standard is issued under the fixed designation D6824; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A
superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
1
ε NOTE—Editorial changes were made to 6.1.7, 10.1, and the Summary of Changes section in September 2013.
1. Scope* D6300 Practice for Determination of Precision and Bias
Data for Use in Test Methods for Petroleum Products and
1.1 This test method covers a procedure for determining the
Lubricants
filterability of aviation turbine fuels (for other middle distillate
D6426 Test Method for Determining Filterability of Middle
fuels, see Test Method D6426).
Distillate Fuel Oils
NOTE 1—ASTM specification fuels falling within the scope of this test
D6615 Specification for Jet B Wide-Cut Aviation Turbine
method are Specifications D1655 and D6615 and the military fuels
covered in the military specifications listed in 2.2.
Fuel
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2.2 Military Standards:
1.2 This test method is not applicable to fuels that contain
MIL-DTL-5624 Turbine Fuel, Aviation, Grades JP-4, JP-5,
undissolved water.
and JP-5/JP-8 ST
1.3 The values stated in SI units are to be regarded as the
MIL-DTL-25524 Turbine Fuel, Aviation, Thermally Stable
standard. The values given in parentheses are for information
MIL-DTL-38219 Turbine Fuels, Low Volatility, JP-7
only.
MIL-DTL-83133 Turbine Fuels, Aviation, Kerosine Types,
1.4 This standard does not purport to address all of the
NATO F-34 (JP-8), NATO F-35, and JP-8+100
safety concerns, if any, associated with its use. It is the
3. Terminology
responsibility of the user of this standard to establish appro-
priate safety and health practices and determine the applica-
3.1 Definitions of Terms Specific to This Standard:
bility of regulatory limitations prior to use.
3.1.1 filterability, n—a measure of the rapidity with which a
standard filter medium is plugged by insoluble matter in fuel
2. Referenced Documents
and may be described as a function of pressure or volume:
2
2.1 ASTM Standards:
3.1.1.1 filterability (by pressure), n—the pressure drop
D1655 Specification for Aviation Turbine Fuels
across a filter medium when 300 mL of fuel is passed at a rate
D4057 Practice for Manual Sampling of Petroleum and
of 20 mL/min.
Petroleum Products
3.1.1.2 filterability (by volume), n—the volume of fuel
D4176 Test Method for FreeWater and Particulate Contami-
passed when a pressure of 104 kPa (15 psig) is reached.
nation in Distillate Fuels (Visual Inspection Procedures)
3.1.1.3 Discussion—Filterability by volume is used when
D4177 Practice for Automatic Sampling of Petroleum and
less than 300 mL passes the filter at a pressure up to 104 kPa
Petroleum Products
(15 psig).
D4860 Test Method for FreeWater and Particulate Contami-
3.1.1.4 filterability quality factor (F-QF), n—a value that
nation in Middle Distillate Fuels (Clear and Bright Nu-
defines the filter plugging tendency of a fuel caused by
merical Rating)
particulates.
D5452 Test Method for Particulate Contamination in Avia-
tion Fuels by Laboratory Filtration
3.1.1.5 Discussion—The F-QF value is calculated using the
volume and pressure attained at the end of the test cycle,
according to one of two equations, depending on the outcome
1
This test method is under the jurisdiction of ASTM Committee D02 on
of the test. (See Section 10, Calculations.)
Petroleum Products, Liquid Fuels, and Lubricants and is the direct responsibility of
Subcommittee D02.J0.01 on Jet Fuel Specifications.
4. Summary of Test Method
Current edition approved June 15, 2013. Published August 2013. Originally
approved in 2002. Last previous edition approved in 2007 as D6824 – 07. DOI:
4.1 A sample is passed at a constant rate (20 mL/min)
10.1520/D6824-13E01.
through a standard porosity filter medium. The pressure drop
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
3
Standards volume information, refer to the standard’s Document Summary page on Available from Standardization Documents Order Desk, DODSSP, Bldg. 4,
the ASTM website. Section D, 700 Robbins Ave., Philadelphia, PA 19111-5098.
*A Summary of Changes section appears at the end of this standard
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
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D6824 − 13
NOTE 1—Fuel flow from reservoir through pump to container.
FIG. 1 Schematic Diagram of Filterability Apparatus
across the filter an
...

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