ASTM D6824 Standard Test Method for Determining Filterability of Aviation Turbine Fuel
1. Scope
1.1 This test method covers a procedure for determining the filterability of aviation turbine fuels.
NOTE 1 - ASTM specification fuels falling within the scope of this test method are Specification D 1655 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.
2. Referenced Documents
2.1 ASTM Standards:
D1655 Specification for Aviation Turbine Fuels
D4057 Practice for Manual Sampling of Petroleum and Petroleum Products
D4176 Test Method for Free Water and Particulate Contamination in Distillate Fuels (Visual Inspection Procedures)
D4177 Practice for Automatic Sampling of Petroleum and Petroleum Products
D4860 Test Method for Free Water and Particulate Contamination in Mid-Distillate Fuels (Clear and Bright Numerical Rating)
D5452 Test Method for Particulate Contamination in Aviation Fuels by Laboratory Filtration
D6426 Test Method for Determining Filterability of Middle Distillate Fuel Oils
D6615 Specification for Jet B Wide-Cut Aviation Turbine Fuel
E 1 Specification for ASTM Thermometers
2.2 Military Standards:
MIL-DTL-5624 Turbine Fuel, Aviation, Grades JP-4, JP-5, and JP-5/JP-8 ST
MIL-DTL-25524 Turbine Fuel, Aviation, Thermally Stable
MIL-DTL-38219 Turbine Fuels, Low Volatility, JP-7
MIL-DTL-83133 Turbine Fuels, Aviation, Kerosine Types, NATO F-34 (JP-8), NATO F-35, and JP-8+100
3. Terminology
3.1 Definitions ofTerms Specific to This Standard:
3.1.1 filterability - a measure of the rapidity with which a standard filter medium is plugged by insoluble matter in fuel and can be described in the following ways:
3.1.1.1 filterability (by pressure) - the pressure drop across a filter medium when 300 mL of fuel is passed at a rate of 20 mL/min.
3.1.1.2 filterability (by volume) - the volume of fuel passed when 104 kPa (15 psi) is reached. This method ofreport is used when less than 300 mL passes at that pressure, 104 kPa (15 psi).
3.1.1.3 filterability quality factor (F-QF) - a value that defines the filter plugging tendency of a fuel caused by particulate. The value is calculated using the volume and pressure attained at the end of the test cycle. Depending on the outcome of the test, two different equations are applied.
3.1.1.4 Discussion - Eq 1 is applied if the total sample was discharged prior to reaching the maximum pressure or Eq 2 if the maximum pressure was reached prior to discharging the entire sample. The equations proportion the results so that a continuous range of 0 to 100 is attained. Eq 1 yields values from 50 to 100, whereas Eq 2 yields values from 0 to 50. Higher values signify less particulate that can plug a filter of a given pore size and porosity.
(1) If the total sample, 300 mL, is discharged prior to reaching the maximum pressure, 104 kPa (15 psi), the F-QF is calculated by the following equation:
F-QF(300 mL at P(F) = [(15 psi - P(F))/15 psi][50] + [50]
where:
P(F) = final pressure when the total sample, 300 mL, was discharged.
(2) If the total sample is not discharged prior to reaching the maximum pressure, 104 kPa (15 psi), the F-QF is calculated by the following equation:
F - QF(V(F) at 15 psi = V(F)/6
where:
V(F) = final volume when the maximum pressure was reached.
3.1.1.5 Discussion - The final volume (V(F)) is divided by 6, since the maximum possible volume is 300 mL. By dividing by 6, the values for that test result are proportioned to fit the range from 0 to 50.
