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ASTM D910-00

(Specification)

Standard Specification for Aviation Gasolines

Standard Specification for Aviation Gasolines

SCOPE
1.1 This specification is for the use of purchasing agencies in formulating specifications for purchases of aviation gasoline under contract.  
1.2 This specification defines specific types of aviation gasolines for civil use. It does not include all gasolines satisfactory for reciprocating aviation engines. Certain equipment or conditions of use may permit a wider, or require a narrower, range of characteristics than is shown by this specification.

General Information

Status
Historical
Publication Date
09-Dec-2001
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 D910-99 - Standard Specification for Aviation Gasolines
Effective Date
10-Dec-2001
Referred By
ASTM D3343-22 - Standard Test Method for Estimation of Hydrogen Content of Aviation Fuels
Effective Date
10-Dec-2001
Referred By
ASTM D7464-20 - Standard Practice for Manual Sampling of Liquid Fuels, Associated Materials and Fuel System Components for Microbiological Testing
Effective Date
10-Dec-2001
Referred By
ASTM D6227-18(2023) - Standard Specification for Unleaded Aviation Gasoline Containing a Non-hydrocarbon Component
Effective Date
10-Dec-2001
Referred By
ASTM D4529-17 - Standard Test Method for Estimation of Net Heat of Combustion of Aviation Fuels
Effective Date
10-Dec-2001
Referred By
ASTM D7719-21a - Standard Specification for High Aromatic Content Unleaded Hydrocarbon Aviation Gasoline Test Fuel
Effective Date
10-Dec-2001
Referred By
ASTM D3144-23 - Standard Specification for Crosslinked Poly(Vinylidene Fluoride) and Poly(Vinylidene Fluoride) Copolymer Heat-Shrinkable Tubing for Electrical Insulation
Effective Date
10-Dec-2001
Referred By
ASTM D4171-22 - Standard Specification for Fuel System Icing Inhibitors
Effective Date
10-Dec-2001
Referred By
ASTM E1259-23 - Standard Practice for Evaluation of Antimicrobials in Liquid Fuels Boiling Below 390 °C
Effective Date
10-Dec-2001
Referred By
ASTM F3397/F3397M-21 - Standard Practice for Aeroplane Turbine Fuel System Hot Weather Operations
Effective Date
10-Dec-2001
Referred By
ASTM D7826-23a - Standard Guide for Evaluation of New Aviation Gasolines and New Aviation Gasoline Additives
Effective Date
10-Dec-2001
Referred By
ASTM D7960-21 - Standard Specification for Unleaded Aviation Gasoline Test Fuel Containing Non-hydrocarbon Components
Effective Date
10-Dec-2001
Referred By
ASTM D8434-21 - Standard Specification for Unleaded Aviation Gasoline Test Fuel Containing Organo-metallic Additive
Effective Date
10-Dec-2001
Referred By
ASTM F2245-23 - Standard Specification for Design and Performance of a Light Sport Airplane
Effective Date
10-Dec-2001
Referred By
ASTM D4865-19 - Standard Guide for Generation and Dissipation of Static Electricity in Petroleum Fuel Systems
Effective Date
10-Dec-2001

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ASTM D910-00 - Standard Specification for Aviation GasolinesASTM D910-00 - Standard Specification for Aviation Gasolines
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ASTM D910-00 - Standard Specification for Aviation Gasolines
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Standards Content (Sample)

NOTICE: This standard has either been superseded and replaced by a new version or discontinued.
Contact ASTM International (www.astm.org) for the latest information.
Designation: D 910 – 00 An American National Standard
Standard Specification for
1
Aviation Gasolines
This standard is issued under the fixed designation D 910; 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 (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.
2
1. Scope D 1094 Test Method for Water Reaction of Aviation Fuels
D 1266 Test Method for Sulfur in Petroleum Products
1.1 This specification is intended primarily for use by
2
(Lamp Method)
purchasing agencies in formulating specifications for purchases
D 1298 Test Method for Density, Relative Density (Specific
of aviation gasoline under contract.
Gravity), or API Gravity of Crude Petroleum and Liquid
1.2 This specification defines specific types of aviation
2
Petroleum Products by Hydrometer Method
gasolines for civil use. It does not include all gasolines
2
D 2386 Test Method for Freezing Point of Aviation Fuels
satisfactory for reciprocating aviation engines. Certain equip-
2
D 2392 Test Method for Color of Dyed Aviation Gasolines
ment or conditions of use may permit a wider, or require a
D 2622 Test Method for Sulfur in Petroleum Products by
narrower, range of characteristics than is shown by this
Wavelength Dispersive X-Ray Fluorescence Spectrom-
specification.
6
etry
2. Referenced Documents
D 2624 Test Method for Electrical Conductivity of Aviation
6
and Distillate Fuels
2.1 ASTM Standards:
D 2700 Test Method for Octane Number of Spark-Ignition
D 86 Test Method for Distillation of Petroleum Products at
5
2
Engine Fuel
Atmospheric Pressure
D 3338 Test Method for Estimation of Heat of Combustion
D 93 Test Methods for Flash-Point by Pensky-Martens
6
2
of Aviation Fuels
Closed Cup Tester
D 3341 Test Method for Lead in Gasoline—Iodine
D 130 Test Method for Detection of Copper Corrosion from
6
2
Monochloride Method
Petroleum Products by the Copper Strip Tarnish Test
D 4052 Test Method for Density and Relative Density of
D 156 Test Method for Saybolt Color of Petroleum Prod-
6
2
Liquids by Digital Density Meter
ucts (Saybolt Chromometer Method)
D 4057 Practice for Manual Sampling of Petroleum and
D 323 Test Method for Vapor Pressure of Petroleum Prod-
6
2
Petroleum Products
ucts (Reid Method)
6
D 4171 Specification for Fuel System Icing Inhibitors
D 357 Method of Test for Knock Characteristics of Motor
3
D 4306 Practice for Aviation Fuel Sampling Containers for
Fuels Below 100 Octane Number by the Motor Method
6
Tests Affected by Trace Contamination
D 381 Test Method for Gum Content in Fuels by Jet
2
D 4529 Test Method for Estimation of Net Heat of Com-
Evaporation
6
bustion of Aviation Fuels
D 614 Method of Test for Knock Characteristics of Aviation
4
D 4809 Test Method for Heat of Combustion of Liquid
Fuels by the Aviation Method
Hydrocarbon Fuels by Bomb Calorimeter (Intermediate
D 873 Test Method for Oxidation Stability of Aviation Fuels
7
2
Precision Method)
(Potential Residue Method)
D 4865 Guide for the Generation and Dissipation of Static
D 909 Test Method for Knock Characteristics of Aviation
7
5
Electricity in Petroleum Fuel Systems
Gasolines by the Supercharge Method
D 5006 Test Method for Determination of Fuel System
7
Icing Inhibitor (Ether Type) in Aviation Fuels
1
This specification is under the jurisdiction of ASTM Committee D02 on
D 5059 Test Method for Lead in Gasoline by X-Ray Spec-
Petroleum Products and Lubricants and is the direct responsibility of Subcommittee 7
troscopy
D02.J on Aviation Fuels.
D 5190 Test Method for Vapor Pressure of Petroleum Prod-
Current edition approved Dec. 10, 2000. Published January 2001. Originally
7
published as D 910 – 47 T replacing former D 615. Last previous edition ucts (Automatic Method)
D 910 – 99.
2
Annual Book of ASTM Standards, Vol 05.01.
3
Discontinued 1969. Replaced by D 2700.
4 6
Discontinued; see 1970 Annual Book of ASTM Standards. Annual Book of ASTM Standards, Vol 05.02.
5 7
Annual Book of ASTM Standards, Vol 05.05. Annual Book of ASTM Standards, Vol 05.03.
Copyright © ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959, United States.
1

---------------------- Page: 1 ----------------------
D 910
D 5191 Test Method for Vapor Pressure of Petroleum Prod- 6.2 Additives—Mandatory, shall be added to each grade of
7
ucts (Mini Method) aviation gasoline in the amount and of the composition
D 6469 Guide for Microbial Contaimination in Fuels and specified in the following list of approved materials.
8
Fuel Systems 6.2.1 Tetraethyl Lead, shall be added in the form of an
E 29 Practice for Using Significant Digits in Test Data to antiknock mixture conta
...

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5.1 The analysis of trace oxygenates in automotive spark-ignition engine fuel has become routine in certain areas to ensure compliance whenever oxygenated fuels are used. In addition, test methods to measure trace levels of oxygenates in automotive spark-ignition fuel are necessary to assess product quality.
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1.2 The ethanol blending concentration for which this test method applies ranges from 1 % to 15% by volume. Higher concentrations of ethanol coelute with methanol in the analytical column. Lower levels of ethanol, similar to the other oxygenate, can be calibrated and analyzed also. If higher ethanol concentrations are expected, the window cutting technique can be used to avoid ethanol from entering the analytical column and interfere with the determination of the other oxygenates of interest. Refer to Appendix X1 for details.  
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ASTM D3701-23(Test Method)
Standard Test Method for Hydrogen Content of Aviation Turbine Fuels by Low Resolution Nuclear Magnetic Resonance Spectrometry

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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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ASTM D7826-23b(Guide)
Standard Guide for Evaluation of New Aviation Gasolines and New Aviation Gasoline Additives

SIGNIFICANCE AND USE
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.”  
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1.6.1 Exception—Some industry standard methodologies uti...

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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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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.  
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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  
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 D5001-23(Test Method)
Standard Test Method for Measurement of Lubricity of Aviation Turbine Fuels by the Ball-on-Cylinder Lubricity Evaluator (BOCLE)

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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 Methods for Hydrogen Content of Light Distillates, Middle Distillates, Gas Oils, and Residua by Low-Resolution Nuclear Magnetic Resonance Spectroscopy

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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.  
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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 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.

  • Standard
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  • Standard
    7 pages
    English language
    sale 15% off