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ASTM D1655-16a

(Specification)

Standard Specification for Aviation Turbine Fuels

Standard Specification for Aviation Turbine Fuels

ABSTRACT
This specification covers purchases of aviation turbine fuel under contract and is intended primarily for use by purchasing agencies. This specification does not include all fuels satisfactory for reciprocating aviation turbine engines, but rather, defines the following specific types of aviation fuel for civil use: Jet A; and Jet A-1. The fuels shall be sampled and tested appropriately to examine their conformance to detailed requirements as to composition, volatility, fluidity, combustion, corrosion, thermal stability, contaminants, and additives.
SCOPE
1.1 This specification covers the use of purchasing agencies in formulating specifications for purchases of aviation turbine fuel under contract.  
1.2 This specification defines the minimum property requirements for Jet A and Jet A-1 aviation turbine fuel and lists acceptable additives for use in civil operated engines and aircrafts. Specification D1655 is directed at civil applications, and maintained as such, but may be adopted for military, government or other specialized uses.  
1.3 This specification can be used as a standard in describing the quality of aviation turbine fuel from production to the aircraft. However, this specification does not define the quality assurance testing and procedures necessary to ensure that fuel in the distribution system continues to comply with this specification after batch certification. Such procedures are defined elsewhere, for example in ICAO 9977, EI/JIG Standard 1530, JIG 1, JIG 2, API 1543, API 1595, and ATA-103.  
1.4 This specification does not include all fuels satisfactory for aviation turbine engines. Certain equipment or conditions of use may permit a wider, or require a narrower, range of characteristics than is shown by this specification.  
1.5 Aviation turbine fuels defined by this specification may be used in other than turbine engines that are specifically designed and certified for this fuel.  
1.6 This specification no longer includes wide-cut aviation turbine fuel (Jet B). FAA has issued a Special Airworthiness Information Bulletin which now approves the use of Specification D6615 to replace Specification D1655 as the specification for Jet B and refers users to this standard for reference.  
1.7 The values stated in SI units are to be regarded as standard. However, other units of measurement are included in this standard.

General Information

Status
Historical
Publication Date
31-Jul-2016
ICS
75.160.20 - Liquid fuels
Technical Committee
D02 - Petroleum Products, Liquid Fuels, and Lubricants
Drafting Committee
D02.J0.01 - Jet Fuel Specifications
Current Stage
Ref Project

Relations

Replaced By
ASTM D1655-16b - Standard Specification for Aviation Turbine Fuels
Effective Date
01-Sep-2016

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Standards Content (Sample)

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
Designation:D1655 −16a An American National Standard
Standard Specification for
1
Aviation Turbine Fuels
This standard is issued under the fixed designation D1655; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision.Anumber in parentheses indicates the year of last reapproval.A
superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
This standard has been approved for use by agencies of the U.S. Department of Defense.
1. Scope* 2. Referenced Documents
2
2.1 ASTM Standards:
1.1 Thisspecificationcoverstheuseofpurchasingagencies
D56Test Method for Flash Point by Tag Closed Cup Tester
in formulating specifications for purchases of aviation turbine
D86Test Method for Distillation of Petroleum Products and
fuel under contract.
Liquid Fuels at Atmospheric Pressure
1.2 This specification defines the minimum property re-
D93Test Methods for Flash Point by Pensky-Martens
quirements for JetAand JetA-1 aviation turbine fuel and lists
Closed Cup Tester
acceptable additives for use in civil operated engines and
D130Test Method for Corrosiveness to Copper from Petro-
aircrafts. Specification D1655 is directed at civil applications,
leum Products by Copper Strip Test
and maintained as such, but may be adopted for military,
D156Test Method for Saybolt Color of Petroleum Products
government or other specialized uses.
(Saybolt Chromometer Method)
1.3 This specification can be used as a standard in describ-
D240Test Method for Heat of Combustion of Liquid Hy-
ing the quality of aviation turbine fuel from production to the
drocarbon Fuels by Bomb Calorimeter
aircraft. However, this specification does not define the quality
D323TestMethodforVaporPressureofPetroleumProducts
assurance testing and procedures necessary to ensure that fuel
(Reid Method)
in the distribution system continues to comply with this
D381Test Method for Gum Content in Fuels by Jet Evapo-
specification after batch certification. Such procedures are
ration
defined elsewhere, for example in ICAO9977, EI/JIG Stan-
D445Test Method for Kinematic Viscosity of Transparent
dard1530, JIG1, JIG2, API1543, API1595, and ATA-103.
andOpaqueLiquids(andCalculationofDynamicViscos-
ity)
1.4 This specification does not include all fuels satisfactory
D1266TestMethodforSulfurinPetroleumProducts(Lamp
for aviation turbine engines. Certain equipment or conditions
Method)
of use may permit a wider, or require a narrower, range of
D1298Test Method for Density, Relative Density, or API
characteristics than is shown by this specification.
Gravity of Crude Petroleum and Liquid Petroleum Prod-
1.5 Aviation turbine fuels defined by this specification may
ucts by Hydrometer Method
be used in other than turbine engines that are specifically
D1319TestMethodforHydrocarbonTypesinLiquidPetro-
designed and certified for this fuel.
leum Products by Fluorescent Indicator Adsorption
1.6 This specification no longer includes wide-cut aviation D1322Test Method for Smoke Point of Kerosine and
Aviation Turbine Fuel
turbine fuel (Jet B). FAA has issued a Special Airworthiness
Information Bulletin which now approves the use of Specifi- D1405Test Method for Estimation of Net Heat of Combus-
tion of Aviation Fuels
cation D6615 to replace Specification D1655 as the specifica-
tion for Jet B and refers users to this standard for reference. D1660Method of Test for Thermal Stability of Aviation
3
Turbine Fuels (Withdrawn 1992)
1.7 The values stated in SI units are to be regarded as
D1840Test Method for Naphthalene Hydrocarbons inAvia-
standard.However,otherunitsofmeasurementareincludedin
tion Turbine Fuels by Ultraviolet Spectrophotometry
this standard.
D2276Test Method for Particulate Contaminant inAviation
1 2
This specification is under the jurisdiction of ASTM Committee D02 on For referenced ASTM standards, visit the ASTM website, www.astm.org, or
Petroleum Products, Liquid Fuels, and Lubricants and is the direct responsibility of contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
Subcommittee D02.J0.01 on Jet Fuel Specifications. Standards volume information, refer to the standard’s Document Summary page on
Current edition approved Aug. 1, 2016. Published August 2016. Originally the ASTM website.
3
approved in 1959. Last previous edition approved in 2016 as D1655–16. DOI: The last approved version of this historical standard is referenced on
10.1520/D1655-16A. www.astm.org.
*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
1

---------------------- Page: 1 ----------------------
D1655−16a
Fuel by Line Sampling D5001Test Method for Measurement of Lubricity of Avia-
D2386Test Method for Fre
...

This document is not an ASTM standard and is intended only to provide the user of an ASTM standard an indication of what changes have been made to the previous version. Because
it may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current version
of the standard as published by ASTM is to be considered the official document.
Designation: D1655 − 16 D1655 − 16a An American National Standard
Standard Specification for
1
Aviation Turbine Fuels
This standard is issued under the fixed designation D1655; 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.
This standard has been approved for use by agencies of the U.S. Department of Defense.
1. Scope*
1.1 This specification covers the use of purchasing agencies in formulating specifications for purchases of aviation turbine fuel
under contract.
1.2 This specification defines the minimum property requirements for Jet A and Jet A-1 aviation turbine fuel and lists acceptable
additives for use in civil operated engines and aircrafts. Specification D1655 is directed at civil applications, and maintained as
such, but may be adopted for military, government or other specialized uses.
1.3 This specification can be used as a standard in describing the quality of aviation turbine fuel from production to the aircraft.
However, this specification does not define the quality assurance testing and procedures necessary to ensure that fuel in the
distribution system continues to comply with this specification after batch certification. Such procedures are defined elsewhere, for
example in ICAO 9977, EI/JIG Standard 1530, JIG 1, JIG 2, API 1543, API 1595, and ATA-103.
1.4 This specification does not include all fuels satisfactory for aviation turbine engines. Certain equipment or conditions of use
may permit a wider, or require a narrower, range of characteristics than is shown by this specification.
1.5 Aviation turbine fuels defined by this specification may be used in other than turbine engines that are specifically designed
and certified for this fuel.
1.6 This specification no longer includes wide-cut aviation turbine fuel (Jet B). FAA has issued a Special Airworthiness
Information Bulletin which now approves the use of Specification D6615 to replace Specification D1655 as the specification for
Jet B and refers users to this standard for reference.
1.7 The values stated in SI units are to be regarded as standard. However, other units of measurement are included in this
standard.
2. Referenced Documents
2
2.1 ASTM Standards:
D56 Test Method for Flash Point by Tag Closed Cup Tester
D86 Test Method for Distillation of Petroleum Products and Liquid Fuels at Atmospheric Pressure
D93 Test Methods for Flash Point by Pensky-Martens Closed Cup Tester
D130 Test Method for Corrosiveness to Copper from Petroleum Products by Copper Strip Test
D156 Test Method for Saybolt Color of Petroleum Products (Saybolt Chromometer Method)
D240 Test Method for Heat of Combustion of Liquid Hydrocarbon Fuels by Bomb Calorimeter
D323 Test Method for Vapor Pressure of Petroleum Products (Reid Method)
D381 Test Method for Gum Content in Fuels by Jet Evaporation
D445 Test Method for Kinematic Viscosity of Transparent and Opaque Liquids (and Calculation of Dynamic Viscosity)
D1266 Test Method for Sulfur in Petroleum Products (Lamp Method)
D1298 Test Method for Density, Relative Density, or API Gravity of Crude Petroleum and Liquid Petroleum Products by
Hydrometer Method
D1319 Test Method for Hydrocarbon Types in Liquid Petroleum Products by Fluorescent Indicator Adsorption
1
This specification is under the jurisdiction of ASTM Committee D02 on Petroleum Products, Liquid Fuels, and Lubricants and is the direct responsibility of Subcommittee
D02.J0.01 on Jet Fuel Specifications.
Current edition approved June 1, 2016Aug. 1, 2016. Published August 2016. Originally approved in 1959. Last previous edition approved in 20152016 as
ɛ1
D1655 – 15dD1655 – 16. . DOI: 10.1520/D1655-16.10.1520/D1655-16A.
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 Standards
volume information, refer to the standard’s Document Summary page on the ASTM website.
*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
1

---------------------- Page: 1 ----------------------
D1655 − 16a
D1322 Test Method for Smoke Point of Kerosine and Aviation Turbine Fuel
D1405 Test Method for Estimation of Net Heat of Combustion of Aviation Fuels
3
D1660 Method of Test for Thermal Stability of
...

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1.4 Table of Contents:    
Section  
Scope  
1  
Referenced Documents  
2  
Terminology  
3  
Summary of Test Method  
4  
Significance and Use  
5  
Apparatus  
6  
Engine Fluids and Cleaning Solvents  
7  
Preparation of Apparatus  
8  
Engine/Stand Calibration and Non-Reference Oil Tests  
9  
Test Procedure  
10  
Calculations, Ratings, and Test Validity  
11  
Report  
12  
Precision and Bias  
13  
Annexes  
Safety Precautions  
Annex A1  
Intake Air Aftercooler  
Annex A2  
The Cummins ISB Engine Build Parts Kit  
Annex A3  
Sensor Locations and Special Hardware  
Annex A4  
External Oil System  
Annex A5  
Cummins Service Publications  
Annex A6  
Specified Units and Formats  
Annex A7  
Oil Analyses  
Annex A8  
Alternate Fuel Approval Process  
Annex A9  
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SIGNIFICANCE AND USE
5.1 Wear due to excessive friction resulting in shortened life of engine components such as fuel pumps and fuel controls has sometimes been ascribed to lack of lubricity in an aviation fuel.  
5.2 The relationship of test results to aviation fuel system component distress due to wear has been demonstrated for some fuel/hardware combinations where boundary lubrication is a factor in the operation of the component.  
5.3 The wear scar generated in the ball-on-cylinder lubricity evaluator (BOCLE) test is sensitive to contamination of the fluids and test materials, the presence of oxygen and water in the atmosphere, and the temperature of the test. Lubricity measurements are also sensitive to trace materials acquired during sampling and storage. Containers specified in Practice D4306 shall be used.  
5.4 The BOCLE test method may not directly reflect operating conditions of engine hardware. For example, some fuels that contain a high content of certain sulfur compounds can give anomalous test results.
SCOPE
1.1 This test method covers assessment of the wear aspects of the boundary lubrication properties of aviation turbine fuels on rubbing steel surfaces.  
1.1.1 This test method incorporates two procedures, one using a semi-automated instrument and the second a fully automated instrument. Either of the two instruments may be used to carry out the test.  
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 the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use.  
1.4 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

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ASTM
ASTM D4808-23(Test Method)
Standard Test Methods for Hydrogen Content of Light Distillates, Middle Distillates, Gas Oils, and Residua by Low-Resolution Nuclear Magnetic Resonance Spectroscopy

SIGNIFICANCE AND USE
5.1 The hydrogen content represents a fundamental quality of a petroleum product that has been correlated with many of the performance characteristics of that product.  
5.2 This test method provides a simple and more precise alternative to existing test methods, specifically combustion techniques (Test Methods D5291) for determining the hydrogen content on a range of petroleum products.
SCOPE
1.1 These test methods cover the determination of the hydrogen content of petroleum products ranging from atmospheric distillates to vacuum residua using a continuous wave, low-resolution nuclear magnetic resonance spectrometer. (Test Method D3701 is the preferred method for determining the hydrogen content of aviation turbine fuels using nuclear magnetic resonance spectroscopy.)  
1.2 Three test methods are included here that account for the special characteristics of different petroleum products and apply to the following distillation ranges:    
Test Method  
Petroleum Products  
Boiling Range, °C (°F)
(approximate)  
A  
Light Distillates  
15–260 (60–500)  
B  
Middle Distillates  
200–370 (400–700)  
Gas Oils  
370–510 (700–950)  
C  
Residua  
510+ (950+ )  
1.3 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. The preferred units are mass %.  
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, health, and environmental practices and determine the applicability of regulatory limitations prior to use. For specific warning statements, see Sections 7.2 and 7.4.  
1.5 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

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ASTM
ASTM D8252-23(Test Method)
Standard Test Method for Vanadium and Nickel in Crude and Residual Oil by X-ray Spectrometry

SIGNIFICANCE AND USE
5.1 This test method provides a rapid and precise elemental measurement with simple sample preparation. Typical analysis times are approximately 4 min to 5 min per sample with a preparation time of approximately 1 min to 3 min per sample.  
5.2 The quality of crude oil is related to the amount of sulfur present. Knowledge of the vanadium and nickel concentration is necessary for processing purposes as well as contractual agreements.  
5.3 The presence of vanadium and nickel presents significant risks for contamination of the cracking catalysts in the refining process.  
5.4 This test method provides a means of determining whether the vanadium and nickel content of crude meets the operational limits of the refinery and whether the metal content will have a deleterious effect on the refining process or when used as a fuel.
SCOPE
1.1 This test method covers the quantitative determination of total vanadium and nickel in crude and residual oil in the concentration ranges shown in Table 1 using X-ray fluorescence (XRF) spectrometry.  
1.2 Sulfur is measured for analytical purposes only for the compensation of X-ray absorption matrix effects affecting the vanadium and nickel X-rays. For measurement of sulfur by standard test method use Test Methods D4294, D2622 or other suitable standard test method for sulfur in crude and residual oils.  
1.3 This test method is limited to the use of X-ray fluorescence (XRF) spectrometers employing an X-ray tube for excitation in conjunction with wavelength dispersive detection system or energy dispersive high resolution semiconductor detector with the ability to separate signals of adjacent and near-adjacent elements.  
1.4 This test method uses inter-element correction factors calculated from XRF theory, the fundamental parameters (FP) approach, or best fit regression.  
1.5 Samples containing higher concentrations than shown in Table 1 must be diluted to bring the elemental concentration of the diluted material within the scope of this test method.  
1.6 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.  
1.6.1 The preferred concentrations units are mg/kg for vanadium and nickel.  
1.7 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, health, and environmental practices and determine the applicability of regulatory limitations prior to use.  
1.8 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

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