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ASTM D2386-15e1

Historical Revision

Standard Test Method for Freezing Point of Aviation Fuels

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1.1 This test method covers the determination of the temperature below which solid hydrocarbon crystals may form in aviation turbine fuels and aviation gasoline.

Note 1: The interlaboratory program that generated the precisions for this test method did not include aviation gasoline.

1.2 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.

1.3 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. For specific warning statements, see 5.4, Section 6, and 8.3.


4.1 The freezing point of an aviation fuel is the lowest temperature at which the fuel remains free of solid hydrocarbon crystals that can restrict the flow of fuel through filters if present in the fuel system of the aircraft. The temperature of the fuel in the aircraft tank normally falls during flight depending on aircraft speed, altitude, and flight duration. The freezing point of the fuel must always be lower than the minimum operational tank temperature.

4.2 Freezing point is a requirement in Specifications D910 and D1655.

SDO ASTM: ASTM International
Document Number D2386
Publication Date June 1, 2015
Language en - English
Page Count 5
Revision Level 15e1
Supercedes
Committee D02.07
Publish Date Document Id Type View
May 1, 2019 D2386-19 Revision
Dec. 1, 2018 D2386-18 Revision
June 1, 2015 D2386-15E01 Revision
June 1, 2015 D2386-15 Revision
Jan. 1, 2006 D2386-06 Revision
July 1, 2005 D2386-05 Revision
May 10, 2003 D2386-03 Revision
Aug. 10, 2001 D2386-97 Revision
Aug. 10, 2001 D2386-01 Revision
April 15, 2012 D2386-06R12 Reaffirmation