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ASTM D1655-04

(Specification)

Standard Specification for Aviation Turbine Fuels

Standard Specification for Aviation Turbine Fuels

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 specific types of aviation turbine fuel for civil use in the operation and certification of aircraft and describes fuels found satisfactory for the operation of aircraft and engines. The specification can be used as a standard in describing the quality of aviation turbine fuels from the refinery to the aircraft.
1.3 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.
1.4 Aviation turbine fuels defined by this specification may be used in other than turbine engines that are specifically designed and certified for this fuel.
1.5 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 D 6615 to replace Specification D 1655 as the specification for Jet B and refers users to this standard for reference.

General Information

Status
Historical
Publication Date
31-May-2004
ICS
75.160.20 - Liquid fuels
Technical Committee
D02 - Petroleum Products, Liquid Fuels, and Lubricants
Drafting Committee
D02.J0 - Aviation Fuels
Current Stage
Ref Project

Relations

Replaces
ASTM D1655-03a - Standard Specification for Aviation Turbine Fuels
Effective Date
01-Jun-2004
Replaced By
ASTM D1655-04a - Standard Specification for Aviation Turbine Fuels
Effective Date
01-Nov-2004
Referred By
ASTM D381-22 - Standard Test Method for Gum Content in Fuels by Jet Evaporation
Effective Date
01-Jun-2004
Referred By
ASTM D2276-22 - Standard Test Method for Particulate Contaminant in Aviation Fuel by Line Sampling
Effective Date
01-Jun-2004
Referred By
ASTM D4054-23 - Standard Practice for Evaluation of New Aviation Turbine Fuels and Fuel Additives
Effective Date
01-Jun-2004
Referred By
ASTM D7042-21a - Standard Test Method for Dynamic Viscosity and Density of Liquids by Stabinger Viscometer (and the Calculation of Kinematic Viscosity)
Effective Date
01-Jun-2004
Referred By
ASTM D6469-20 - Standard Guide for Microbial Contamination in Fuels and Fuel Systems
Effective Date
01-Jun-2004
Referred By
ASTM F3397/F3397M-21 - Standard Practice for Aeroplane Turbine Fuel System Hot Weather Operations
Effective Date
01-Jun-2004
Referred By
ASTM D6217-21 - Standard Test Method for Particulate Contamination in Middle Distillate Fuels by Laboratory Filtration<rangeref></rangeref >
Effective Date
01-Jun-2004
Referred By
ASTM D4171-22 - Standard Specification for Fuel System Icing Inhibitors
Effective Date
01-Jun-2004
Referred By
ASTM D8073-22 - Standard Test Method for Determination of Water Separation Characteristics of Aviation Turbine Fuel by Small Scale Water Separation Instrument
Effective Date
01-Jun-2004
Referred By
ASTM D7619-22 - Standard Test Method for Sizing and Counting Particles in Light and Middle Distillate Fuels, by Automatic Particle Counter
Effective Date
01-Jun-2004
Referred By
ASTM D7978-14(2019) - Standard Test Method for Determination of the Viable Aerobic Microbial Content of Fuels and Associated Water&#x2014;Thixotropic Gel Culture Method
Effective Date
01-Jun-2004
Referred By
ASTM D5677-17 - Standard Specification for Fiberglass (Glass-Fiber-Reinforced Thermosetting-Resin) Pipe and Pipe Fittings, Adhesive Bonded Joint Type, for Aviation Jet Turbine Fuel Lines
Effective Date
01-Jun-2004
Referred By
ASTM D4529-17 - Standard Test Method for Estimation of Net Heat of Combustion of Aviation Fuels
Effective Date
01-Jun-2004

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ASTM D1655-04 - Standard Specification for Aviation Turbine FuelsASTM D1655-04 - Standard Specification for Aviation Turbine Fuels
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ASTM D1655-04 - Standard Specification for Aviation Turbine Fuels
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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
An American National Standard
Designation: D 1655 – 04
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 (e) indicates an editorial change since the last revision or reapproval.
This standard has been approved for use by agencies of the Department of Defense.
1. Scope* D156 Test Method for Saybolt Color of Petroleum Prod-
ucts (Saybolt Chromometer Method)
1.1 Thisspecificationcoverstheuseofpurchasingagencies
D240 Test Method for Heat of Combustion of Liquid
in formulating specifications for purchases of aviation turbine
Hydrocarbon Fuels by Bomb Calorimeter
fuel under contract.
D323 Test Method for Vapor Pressure of Petroleum Prod-
1.2 This specification defines specific types of aviation
ucts (Reid Method)
turbine fuel for civil use in the operation and certification of
D381 Test Method for Gum Content in Fuels by Jet
aircraftanddescribesfuelsfoundsatisfactoryfortheoperation
Evaporation
of aircraft and engines. The specification can be used as a
D445 Test Method for Kinematic Viscosity of Transparent
standardindescribingthequalityofaviationturbinefuelsfrom
and Opaque Liquids (and the Calculation of Dynamic
the refinery to the aircraft.
Viscosity)
1.3 This specification does not include all fuels satisfactory
D1094 Test Method for Water Reaction of Aviation Fuels
for aviation turbine engines. Certain equipment or conditions
D1266 Test Method for Sulfur in Petroleum Products
of use may permit a wider, or require a narrower, range of
(Lamp Method)
characteristics than is shown by this specification.
D1298 TestMethodforDensity,RelativeDensity(Specific
1.4 Aviation turbine fuels defined by this specification may
Gravity), or API Gravity of Crude Petroleum and Liquid
be used in other than turbine engines that are specifically
Petroleum Products by Hydrometer Method
designed and certified for this fuel.
D1319 Test Method for Hydrocarbon Types in Liquid
1.5 This specification no longer includes wide-cut aviation
Petroleum Products by Fluorescent Indicator Adsorption
turbine fuel (Jet B). FAA has issued a Special Airworthiness
D1322 Test Method for Smoke Point of Kerosine and
Information Bulletin which now approves the use of Specifi-
Aviation Turbine Fuel
cation D 6615 to replace SpecificationD1655 as the specifi-
D1405 Test Method for Estimation of Net Heat of Com-
cation for Jet B and refers users to this standard for reference.
bustion of Aviation Fuels
2. Referenced Documents
D1552 Test Method for Sulfur in Petroleum Products
2
(High-Temperature Method)
2.1 ASTM Standards:
D1660 Method of Test for Thermal Stability of Aviation
D56 TestMethodforFlashPointbyTagClosedCupTester
3
Turbine Fuels
D86 Test Method for Distillation of Petroleum Products at
D1840 Test Method for Naphthalene Hydrocarbons in
Atmospheric Pressure
Aviation Turbine Fuels by Ultraviolet Spectrophotometry
D93 Test Methods for Flash-Point by Pensky-Martens
D2276 Test Method for Particulate Contaminant in Avia-
Closed Cup Tester
tion Fuel by Line Sampling
D129 Test Method for Sulfur in Petroleum Products (Gen-
D2386 Test Method for Freezing Point of Aviation Fuels
eral Bomb Method)
D2622 Test Method for Sulfur in Petroleum Products by
D130 Test Method for Corrosiveness to Copper from
Wavelength Dispersive X-Ray Fluorescence Spectrometry
Petroleum Products by the Copper Strip Test
D2624 Test Methods for Electrical Conductivity of Avia-
tion and Distillate Fuels
D2887 Test Method for Boiling Range Distribution of
1
This specification is under the jurisdiction of ASTM Committee D02 on
Petroleum Fractions by Gas Chromatography
PetroleumProductsandLubricantsandisthedirectresponsibilityofSubcommittee
D02.J0 on Aviation Fuels.
D3120 Test Method forTrace Quantities of Sulfur in Light
CurrenteditionapprovedJune1,2004.PublishedJuly2004.Originallyapproved
Liquid Petroleum Hydrocarbons by Oxidative Microcou-
in 1959. Last previous edition approved in 2003 as D1655–03a.
2 lometry
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.
3
Withdrawn.
*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 ----------------------
D1655–04
D3227 Test Method for (Thiol Mercaptan) Sulfur in Gaso- D5972 Test Method for Freezing Point of Aviation Fuels
line, Kerosine, Aviation Turbine, and Distillate F
...

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5.1 The combustion quality of aviation turbine fuel has traditionally been controlled in specifications by such tests as smoke point (see Test Method D1322), smoke volatility index, aromatic content of luminometer number (see Test Method D1740). Evidence is accumulating that a better control of the quality may be obtained by limiting the minimum hydrogen content of the fuel.  
5.2 Existing methods allow the hydrogen content to be calculated from other parameters or determined by combustion techniques. The method specified provides a quick, simple, and more precise alternative to these methods.
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1.1 This test method covers the determination of the hydrogen content of aviation turbine fuels.  
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5.1 This guide is intended for the developers or sponsors of new aviation gasolines or additives to describe the data requirements necessary to support the development of specifications for these new products by ASTM members. The ultimate goal of the data generated in accordance with this guide is to provide an understanding of the performance of the new fuel or additive within the property constraints and compositional bounds of the proposed specification criteria.  
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1.1 This guide provides procedures to develop data for use in research reports for new aviation gasolines or new aviation gasoline additives.  
1.2 This data is intended to be used by the ASTM subcommittee to make a determination of the suitability of the fuel for use as an aviation fuel in either a fleet-wide or limited capacity, and to make a determination that the proposed properties and criteria in the associated standard specification provide the necessary controls to ensure this fuel maintains this suitability during high-volume production.  
1.3 These research reports are intended to support the development and issuance of new specifications or specification revisions for these products. Guidance to develop ASTM International standard specifications for aviation gasoline is provided in Subcommittee J on Aviation Fuels Operating Procedures, Annex A6, “Guidelines for the Development and Acceptance of a New Aviation Fuel Specification for Spark-Ignition Reciprocating Engines.”  
1.4 The procedures, tests, selection of materials, engines, and aircraft detailed in this guide are based on industry expertise to give appropriate data for review. Because of the diversity of aviation hardware and potential variation in fuel/additive formulations, not every aspect may be encompassed and further work may be required. Therefore, additional data beyond that described in this guide may be requested by the ASTM task force, Subcommittee J, or Committee D02 upon review of the specific composition, performance, or other characteristics of the candidate fuel or additive.  
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5.1 Some acids can be present in aviation turbine fuels due either to the acid treatment during the refining process or to naturally occurring organic acids. Significant acid contamination is not likely to be present because of the many check tests made during the various stages of refining. However, trace amounts of acid can be present and are undesirable because of the consequent tendencies of the fuel to corrode metals that it contacts or to impair the water separation characteristics of the aviation turbine fuel.  
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1.1 This test method covers the determination of the acidity in aviation turbine fuel in the range from 0.000 mg/g to 0.100 mg/g KOH.  
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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.  
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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.  
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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.
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5.1 The tendency of a fuel to vaporize in automotive engine fuel systems is indicated by the vapor-liquid ratio of the fuel.  
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Note 1: When the vapor-liquid ratio is 20:1, the result is intended to be comparable to the results determined by Test Method D2533.
Note 2: This test method may also be applicable at pressures other than one atmosphere, but the stated precision may not apply.  
1.2 This test method is applicable to both gasoline and gasoline-oxygenate blends.  
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1.3.1 Exception—The values given in parentheses are provided for information only.  
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Standard Test Method for Measurement of Lubricity of Aviation Turbine Fuels by the Ball-on-Cylinder Lubricity Evaluator (BOCLE)

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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Standard Test Method for Boiling Range Distribution of Fatty Acid Methyl Esters (FAME) in the Boiling Range from 100 °C to 615 °C by Gas Chromatography

SIGNIFICANCE AND USE
5.1 The boiling range distribution of FAMES provides an insight into the composition of product related to the transesterification process. This gas chromatographic determination of boiling range can be used to replace conventional distillation methods for product specification testing with the mutual agreement of interested parties.  
5.2 Biodiesel (FAMES) exhibits a boiling point rather than a distillation curve. The fatty acid chains in the raw oils and fats from which biodiesel is produced are mainly comprised of straight chain hydrocarbons with 16 to 18 carbons that have similar boiling temperatures. The atmospheric boiling point of biodiesel generally ranges from 330 °C to 357 °C. The Specification D6751 value of 360 °C max at 90 % off by Test Method D1160 was incorporated as a precaution to ensure the fuel has not been adulterated with high boiling contaminants.
SCOPE
1.1 This test method covers the determination of the boiling range distribution of fatty acid methyl esters (FAME). This test method is applicable to FAMES (biodiesel, B100) having an initial boiling point greater than 100 °C and a final boiling point less than 615 °C at atmospheric pressure as measured by this test method.  
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1.4 Boiling range distributions obtained by this test method are not equivalent to results from low efficiency distillation such as those obtained with Test Method D86 or D1160, especially the initial and final boiling points.  
1.5 This test method uses the principles of simulated distillation methodology. See Test Methods D2887, D6352, and D7213.  
1.6 The values stated in SI units are to be regarded as standard. The values given in parentheses are for information only.  
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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Standard Test Method for Evaluation of Automotive Engine Oils for Valve-Train Wear Performance in Cummins ISB Medium-Duty Diesel Engine

SIGNIFICANCE AND USE
5.1 This test method was developed to assess the performance of a heavy-duty engine oil in controlling engine wear under operating conditions selected to accelerate soot production and valve-train wear in a turbocharged and aftercooled four-cycle diesel engine with sliding tappet followers equipped with exhaust gas recirculation hardware.  
5.2 The design of the engine used in this test method is representative of many, but not all, modern diesel engines. This factor, along with the accelerated operating conditions, shall be considered when extrapolating test results.
SCOPE
1.1 This test method, commonly referred to as the Cummins ISB Test, covers the utilization of a modern, 5.9 L, diesel engine equipped with exhaust gas recirculation and is used to evaluate oil performance with regard to valve-train wear.  
1.2 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.  
1.2.1 Exceptions—SI units are provided for all parameters except where there is no direct equivalent such as the units for screw threads, National Pipe Threads/diameters, tubing size, or where there is a sole source of supply equipment specification.  
1.2.2 See also A7.1 for clarification; it does not supersede 1.2 and 1.2.1.  
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, health, and environmental practices and determine the applicability of regulatory limitations prior to use. See Annex A1 for general safety precautions.  
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  
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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  • Standard
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    English language
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