Standard Test Method for Freezing Point of Aviation Fuels (Automatic Fiber Optical Method)

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Published date

01-04-2015

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American Society for Testing and Materials

CONTAINED IN VOL. 05.04, 2018 Specifies the determination of the temperature below which solid hydrocarbon crystals may form in aviation turbine fuels.

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

Note 1:This test method describes an alternative procedure and automatic apparatus which closely mimics the apparatus and procedure described in Test Method D2386.

1.2The measuring range of the apparatus is from –70 °C to 0 °C, however the precision statements were derived only from samples with freezing point temperatures from –60 °C to –42 °C.

Note 2:Typical aviation fuel has freezing point temperatures in the –60 °C to –40 °C range.

1.3Some results from this test method (14 % of samples included in the 2003 round robin2) incorrectly identified sample contamination where no contaminants were present in the samples (see research report2 for further information).

1.4The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.

1.5This 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 hazard statements, see Section 7.

Committee	D 02
DocumentType	Redline
Pages	9
PublisherName	American Society for Testing and Materials
Status	Current

MIL-DTL-83133 Revision J:2015	TURBINE FUEL, AVIATION, KEROSENE TYPE, JP-8 (NATO F-34), NATO F-35, AND JP-8+100 (NATO F-37)
DEFSTAN 91-91/7(2011) : 2011	TURBINE FUEL, KEROSINE TYPE, JET A-1 NATO CODE: F-35 JOINT SERVICE DESIGNATION: AVTUR
MIL-DTL-83133 Revision K:2018	TURBINE FUEL, AVIATION, KEROSENE TYPE, JP-8 (NATO F-34), NATO F-35, AND JP-8+100 (NATO F-37)
MIL-DTL-25524 Revision F:2015	TURBINE FUEL, AVIATION, THERMALLY STABLE (JPTS)
ASTM D 1655 : 2018-01	SPECIFICATION FOR AVIATION TURBINE FUELS
MIL-DTL-5624 Revision W:2016	TURBINE FUEL, AVIATION, GRADES JP-4 AND JP-5
DEFSTAN 91-91/8(2016) : 2016	TURBINE FUEL, AVIATION KEROSINE TYPE, JET A-1 NATO CODE: F-35 JOINT SERVICE DESIGNATION: AVTUR
DEFSTAN 91-091/9(2016) : 2016	TURBINE FUEL, AVIATION KEROSINE TYPE, JET A-1 NATO CODE: F-35 JOINT SERVICE DESIGNATION: AVTUR
ASTM D 8147 : 2017	Standard Specification for Special-Purpose Test Fuels for Aviation Compression-Ignition Engines

ASTM E 1 : 2014 : REDLINE	Standard Specification for ASTM Liquid-in-Glass Thermometers
ASTM D 5901 : 2003	Standard Test Method for Freezing Point of Aviation Fuels (Automated Optical Method) (Withdrawn 2010)
ASTM D 2386 : 2015	Standard Test Method for Freezing Point of Aviation Fuels
IP 16 : 2015	DETERMINATION OF THE FREEZING POINT OF AVIATION FUELS - MANUAL METHOD

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ASTM D 7154 : 2015 : REDLINE

Standard Test Method for Freezing Point of Aviation Fuels (Automatic Fiber Optical Method)

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