MIL-DTL-25576E
ASTM D 3227
Standard Test Method for (Thiol Mercaptan) Sulfur in Gasoline,
Kerosine, Aviation Turbine, and Distillate Fuels (Potentiometric
Method) (DoD Adopted)
ASTM D 3241
Standard Test Method for Thermal Oxidation Stability of Aviation
Turbine Fuels (JFTOT Procedure) (DoD Adopted)
ASTM D 3343
Standard Test Method for Estimation of Hydrogen Content of
Aviation Fuels (DoD Adopted)
ASTM D 4045
Standard Test Method for Sulfur in Petroleum Products by
Hydrogenolysis and Rateometric Colorimetry
ASTM D 4052
Standard Test Method for Density and Relative Density of Liquids by
Digital Density Meter (DoD Adopted)
ASTM D 4057
Standard Practice for Manual Sampling of Petroleum and Petroleum
Products (DoD Adopted)
ASTM D 4177
Standard Practice for Automatic Sampling of Petroleum and
Petroleum Products (DoD Adopted)
ASTM D 5452
Standard Test Method for Particulate Contamination in Aviation
Fuels by Laboratory Filtration (DoD Adopted)
ASTM D 5453
Standard Test Method for Determination of Total Sulfur in Light
Hydrocarbons, Motor Fuels, and Oils by Ultraviolet Fluorescence
ASTM D 5623
Standard Test Method for Sulfur Compounds in Light Petroleum
Liquids by Gas Chromatography and Sulfur Selective Detection
ASTM E 29
Standard Practice for Using Significant Digits in Test Data to
Determine Conformance with Specifications (DoD Adopted)
(Copies of these documents are available online at https://www.astm.org or from the American Society for
Testing and Materials, 100 Barr Harbor Drive, West Conshohocken PA 19428-2959)
AMERICAN PETROLEUM INSTITUTE (API)
API/IP Spec 1581
Specifications and Qualification Procedures for Aviation Jet Fuel
Filter/Separators
(Copies of this document are available online at https://api-ep.api.org or from API Publications, Global
Engineering Documents, 15 Inverness Way East, M/S C303B, Englewood, CO 80112-5776)
2.4 Order of precedence. In the event of a conflict between the text of this document and the
references cited herein, the text of this document takes precedence. Nothing in this document, however,
supersedes applicable laws and regulations unless a specific exemption has been obtained.
3. REQUIREMENTS
3.1 Material. The propellant shall consist completely of hydrocarbon compounds except as
otherwise specified herein.
3.2 Chemical and physical properties. The chemical and physical properties of the propellant
shall conform to those listed in Table I when tested in accordance with applicable test methods.
3
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