1、Designation: D1655 13a An American National StandardStandard Specification forAviation Turbine Fuels1This standard is issued under the fixed designation D1655; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last revisi
2、on. A number in parentheses indicates the year of last reapproval. Asuperscript 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 purch
3、asing agenciesin formulating specifications for purchases of aviation turbinefuel under contract.1.2 This specification defines specific types of aviationturbine fuel for civil use in the operation and certification ofaircraft and describes fuels found satisfactory for the operationof aircraft and e
4、ngines. The specification can be used as astandard in describing the quality of aviation turbine fuels fromthe refinery to the aircraft.1.3 This specification does not include all fuels satisfactoryfor aviation turbine engines. Certain equipment or conditionsof use may permit a wider, or require a n
5、arrower, range ofcharacteristics than is shown by this specification.1.4 Aviation turbine fuels defined by this specification maybe used in other than turbine engines that are specificallydesigned and certified for this fuel.1.5 This specification no longer includes wide-cut aviationturbine fuel (Je
6、t B). FAA has issued a Special AirworthinessInformation Bulletin which now approves the use of Specifi-cation D6615 to replace Specification D1655 as the specifica-tion for Jet B and refers users to this standard for reference.1.6 The values stated in SI units are to be regarded asstandard. No other
7、 units of measurement are included in thisstandard.2. Referenced Documents2.1 ASTM Standards:2D56 Test Method for Flash Point by Tag Closed Cup TesterD86 Test Method for Distillation of Petroleum Products atAtmospheric PressureD93 Test Methods for Flash Point by Pensky-MartensClosed Cup TesterD129 T
8、est Method for Sulfur in Petroleum Products (Gen-eral High Pressure Decomposition Device Method)D130 Test Method for Corrosiveness to Copper from Petro-leum Products by Copper Strip TestD156 Test Method for Saybolt Color of Petroleum Products(Saybolt Chromometer Method)D240 Test Method for Heat of C
9、ombustion of Liquid Hy-drocarbon Fuels by Bomb CalorimeterD323 Test Method for Vapor Pressure of Petroleum Products(Reid Method)D381 Test Method for Gum Content in Fuels by Jet Evapo-rationD445 Test Method for Kinematic Viscosity of Transparentand Opaque Liquids (and Calculation of Dynamic Viscos-it
10、y)D1266 Test Method for Sulfur in Petroleum Products (LampMethod)D1298 Test Method for Density, Relative Density, or APIGravity of Crude Petroleum and Liquid Petroleum Prod-ucts by Hydrometer MethodD1319 Test Method for Hydrocarbon Types in Liquid Petro-leum Products by Fluorescent Indicator Adsorpt
11、ionD1322 Test Method for Smoke Point of Kerosine andAviation Turbine FuelD1405 Test Method for Estimation of Net Heat of Combus-tion of Aviation FuelsD1660 Method of Test for Thermal Stability of AviationTurbine Fuels (Withdrawn 1992)3D1840 Test Method for Naphthalene Hydrocarbons in Avia-tion Turbi
12、ne Fuels by Ultraviolet SpectrophotometryD2276 Test Method for Particulate Contaminant in AviationFuel by Line SamplingD2386 Test Method for Freezing Point of Aviation FuelsD2622 Test Method for Sulfur in Petroleum Products byWavelength Dispersive X-ray Fluorescence SpectrometryD2624 Test Methods fo
13、r Electrical Conductivity of Aviationand Distillate Fuels1This specification is under the jurisdiction of ASTM Committee D02 onPetroleum Products, Liquid Fuels, and Lubricants and is the direct responsibility ofSubcommittee D02.J0.01 on Jet Fuel Specifications.Current edition approved Dec. 1, 2013.
14、Published December 2013. Originallyapproved in 1959. Last previous edition approved in 2013 as D1655 13. DOI:10.1520/D1655-13A.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards volume information
15、, refer to the standards Document Summary page onthe ASTM website.3The last approved version of this historical standard is referenced onwww.astm.org.*A Summary of Changes section appears at the end of this standardCopyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken,
16、PA 19428-2959. United States1D2887 Test Method for Boiling Range Distribution of Pe-troleum Fractions by Gas ChromatographyD2892 Test Method for Distillation of Crude Petroleum(15-Theoretical Plate Column)D3120 Test Method for Trace Quantities of Sulfur in LightLiquid Petroleum Hydrocarbons by Oxida
17、tive Microcou-lometryD3227 Test Method for (Thiol Mercaptan) Sulfur inGasoline, Kerosine, Aviation Turbine, and Distillate Fuels(Potentiometric Method)D3240 Test Method for Undissolved Water In AviationTurbine FuelsD3241 Test Method for Thermal Oxidation Stability ofAviation Turbine FuelsD3242 Test
18、Method for Acidity in Aviation Turbine FuelD3338 Test Method for Estimation of Net Heat of Combus-tion of Aviation FuelsD3343 Test Method for Estimation of Hydrogen Content ofAviation FuelsD3701 Test Method for Hydrogen Content of AviationTurbine Fuels by Low Resolution Nuclear MagneticResonance Spe
19、ctrometryD3828 Test Methods for Flash Point by Small Scale ClosedCup TesterD3948 Test Method for Determining Water Separation Char-acteristics ofAviationTurbine Fuels by Portable Separom-eterD4052 Test Method for Density, Relative Density, and APIGravity of Liquids by Digital Density MeterD4057 Prac
20、tice for Manual Sampling of Petroleum andPetroleum ProductsD4171 Specification for Fuel System Icing InhibitorsD4176 Test Method for Free Water and Particulate Contami-nation in Distillate Fuels (Visual Inspection Procedures)D4294 Test Method for Sulfur in Petroleum and PetroleumProducts by Energy D
21、ispersive X-ray Fluorescence Spec-trometryD4306 Practice for Aviation Fuel Sample Containers forTests Affected by Trace ContaminationD4529 Test Method for Estimation of Net Heat of Combus-tion of Aviation FuelsD4809 Test Method for Heat of Combustion of LiquidHydrocarbon Fuels by Bomb Calorimeter (P
22、recisionMethod)D4865 Guide for Generation and Dissipation of Static Elec-tricity in Petroleum Fuel SystemsD4952 Test Method for Qualitative Analysis for ActiveSulfur Species in Fuels and Solvents (Doctor Test)D4953 Test Method for Vapor Pressure of Gasoline andGasoline-Oxygenate Blends (Dry Method)D
23、5001 Test Method for Measurement of Lubricity of Avia-tion Turbine Fuels by the Ball-on-Cylinder LubricityEvaluator (BOCLE)D5006 Test Method for Measurement of Fuel System IcingInhibitors (Ether Type) in Aviation FuelsD5190 Test Method for Vapor Pressure of Petroleum Prod-ucts (Automatic Method) (Wi
24、thdrawn 2012)3D5191 Test Method for Vapor Pressure of Petroleum Prod-ucts (Mini Method)D5452 Test Method for Particulate Contamination in Avia-tion Fuels by Laboratory FiltrationD5453 Test Method for Determination of Total Sulfur inLight Hydrocarbons, Spark Ignition Engine Fuel, DieselEngine Fuel, a
25、nd Engine Oil by Ultraviolet FluorescenceD5972 Test Method for Freezing Point of Aviation Fuels(Automatic Phase Transition Method)D6045 Test Method for Color of Petroleum Products by theAutomatic Tristimulus MethodD6379 Test Method for Determination of Aromatic Hydro-carbon Types in Aviation Fuels a
26、nd PetroleumDistillatesHigh Performance Liquid ChromatographyMethod with Refractive Index DetectionD6469 Guide for Microbial Contamination in Fuels and FuelSystemsD6615 Specification for Jet B Wide-Cut Aviation TurbineFuelD6751 Specification for Biodiesel Fuel Blend Stock (B100)for Middle Distillate
27、 FuelsD7153 Test Method for Freezing Point of Aviation Fuels(Automatic Laser Method)D7154 Test Method for Freezing Point of Aviation Fuels(Automatic Fiber Optical Method)D7524 Test Method for Determination of Static DissipaterAdditives (SDA) in Aviation Turbine Fuel and MiddleDistillate FuelsHigh Pe
28、rformance Liquid Chromato-graph (HPLC) MethodD7566 Specification for Aviation Turbine Fuel ContainingSynthesized HydrocarbonsE29 Practice for Using Significant Digits in Test Data toDetermine Conformance with Specifications2.2 Energy Institute Standards:4IP 225 Copper Content of Aviation Turbine Fue
29、lIP 227 Silver Corrosion of Aviation Turbine FuelIP540 Determination of the existent gum content of aviationturbine fuel Jet evaporation methodIP 585 Determination of fatty acid methyl esters (FAME),derived from bio-diesel fuel, in aviation turbine fuel GC-MS with selective ion monitoring/scan detec
30、tionmethodIP 590 Determination of fatty acid methyl esters (FAME) inaviation fuelHPLC evaporative light scattering detectormethod2.3 ANSI Standard:5ANSI 863 Report of Test Results2.4 Other Standards:Defence Standard (Def Stan) 91-91 Turbine Fuel, AviationKerosine Type, Jet A-16IATA Guidance Material
31、 on Microbiological Contamination4Available from Energy Institute, 61 New Cavendish St., London, WIG 7AR,U.K., http:/www.energyinst.org.uk.5Available from American National Standards Institute (ANSI), 25 W. 43rd St.,4th Floor, New York, NY 10036.6Available from Procurement Executive DFS (Air), Minis
32、try of Defence, St.Giles Court 1, St. Giles High St., London WC2H 8LD.D1655 13a2in Aircraft Fuel Tanks Ref. No: 9680-027EN14214 Automotive fuels - Fatty acid methyl esters(FAME) for diesel engines - Requirements and testmethods8Bulletin Number 65 MSEP Protocol93. General3.1 This specification, unles
33、s otherwise provided, prescribesthe required properties of aviation turbine fuel at the time andplace of delivery.4. Classification4.1 Two types of aviation turbine fuels are provided, asfollows:4.1.1 Jet A and Jet A-1Relatively high flash point distil-lates of the kerosine type.4.2 Jet A and Jet A-
34、1 represent two grades of kerosine fuelthat differ in freezing point. Other grades would be suitablyidentified.4.3 This specification previously cited the requirements forJet B. Requirements for Jet B fuel now appear in SpecificationD6615.5. Materials and Manufacture5.1 Aviation turbine fuel is a co
35、mplex mixture predomi-nantly composed of hydrocarbons and varies depending oncrude source and manufacturing process. Consequently, it isimpossible to define the exact composition of Jet A/A-1. Thisspecification has therefore evolved primarily as a performancespecification rather than a compositional
36、 specification. It isacknowledged that this largely relies on accumulated experi-ence; therefore the specification limits aviation turbine fuels tothose made from conventional sources or by specificallyapproved processes.5.1.1 Aviation turbine fuel, except as otherwise specified inthis specification
37、, shall consist predominantly of refined hydro-carbons (see Note 1) derived from conventional sourcesincluding crude oil, natural gas liquid condensates, heavy oil,shale oil, and oil sands. The use of jet fuel blends containingcomponents from other sources is permitted only in accordancewith Annex A
38、1.NOTE 1Conventionally refined jet fuel contains trace levels ofmaterials that are not hydrocarbons, including oxygenates, organosulfur,and nitrogenous compounds.5.1.2 Fuels used in certified engines and aircraft are ulti-mately approved by the certifying authority subsequent toformal submission of
39、evidence to the authority as part of thetype certification program for that aircraft and engine model.Additives to be used as supplements to an approved fuel mustalso be similarly approved on an individual basis (see X1.2.4and X1.15.1).5.2 AdditivesMay be added to each type of aviationturbine fuel i
40、n the amount and of the composition specified inTable 2 or the following list of approved material:5.2.1 Other additives are permitted under 5.1 and 7.1. Theseinclude fuel performance enhancing additives and fuel handingand maintenance additives as found under Table 2. Thequantities and types must b
41、e declared by the fuel supplier andagreed to by the purchaser. Only additives approved by theaircraft certifying authority are permitted in the fuel on whichan aircraft is operated.5.2.1.1 Biocidal additives are available for controlled usage.Where such an additive is used in the fuel, the approval
42、statusof the additive and associated conditions must be checked forthe specific aircraft and engines to be operated.5.2.1.2 Fuel System Icing Inhibitor:(1) Diethylene Glycol Monomethyl Ether (DiEGME), con-forming to the requirements of Specification D4171, Type III,may be used in concentrations of 0
43、.10 to 0.15 volume %.(2) Test Method D5006 may be used to determine theconcentration of DiEGME in aviation fuels.5.3 Incidental MaterialsIncidental materials are chemi-cals and compositions that can occur in turbine fuels as a resultof production, processing, distribution, or storage. Table 3 listss
44、pecific materials that have an agreed limit. SpecificationD1655 does not require that each batch of fuel be analyzed forincidental materials where there is essentially no risk ofcontamination exceeding Table 3 limits. Where a supplier riskassessment suggests that incidental materials could exceedTab
45、le 3 limits, jet fuel should be confirmed to comply withTable 3 limits prior to airport supply because airports generallyare not equipped to mitigate incidental material content thatexceeds specification limits. Further guidance concerning thesematerials is presented in X1.16.5.4 Guidance material i
46、s presented in Appendix X2 con-cerning the need to control processing additives in jet fuelproduction.6. Detailed Requirements6.1 The aviation turbine fuel shall conform to the require-ments prescribed in Table 1.6.2 Test results shall not exceed the maximum or be lessthan the minimum values specifi
47、ed in Table 1. No allowanceshall be made for the precision of the test methods. Todetermine conformance to the specification requirement, a testresult may be rounded to the same number of significant figuresas in Table 1 using Practice E29. Where multiple determina-tions are made, the average result
48、, rounded in accordance withPractice E29, shall be used.7. Workmanship, Finish, and Appearance7.1 The aviation turbine fuel specified in this specificationshall be visually free of undissolved water, sediment, andsuspended matter. The odor of the fuel shall not be nauseatingor irritating. If the fue
49、l has an odor similar to that of “rottenegg,” please refer to X1.12.5 for further discussion. Nosubstance of known dangerous toxicity under usual conditionsof handling and use shall be present, except as permitted in thisspecification.7Available from International Air Transport Association (IATA), (Head Office)800 Place Victoria, PO Box 113, Montreal, H4Z 1M1, Quebec, Canada. www.iata-.8Available from European Committee for Standardization (CEN), 36 rue deStassart, B-1050, Brussels, Belgium, http:/www.cenorm.be.9Available from Joint Inspection Group (JIG), http
