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ASTM-D7566 2009

$44.96

D7566-09 Standard Specification for Aviation Turbine Fuel Containing Synthesized Hydrocarbons

Published By Publication Date Number of Pages
ASTM 2009 18
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1.1 This specification covers the manufacture of aviation turbine fuel that consists of conventional and synthetic blending components.

1.2 This specification applies only at the point of batch origination. Aviation turbine fuel manufactured, certified and released to all the requirements of this specification, meets the requirements of Specification D 1655 and shall be regarded as Specification D 1655 turbine fuel. Once released to this specification (D 7566) the requirements of this specification are no longer applicable: any recertification shall be done to D 1655 . Field blending of synthesized paraffinic kerosine (SPK) with D 1655 fuel (which may on the whole or in part have originated as D 7566 fuel) shall be considered batch origination in which case all of the requirements of this specification (D 7566) apply, however the fuel shall be regarded as D 1655 turbine fuel after certification and release.

1.3 This specification defines specific types of aviation turbine fuel that contain synthesized hydrocarbons for civil use in the operation and certification of aircraft and describes fuels found satisfactory for the operation of aircraft and engines. The specification is intended to be used as a standard in describing the quality of aviation turbine fuels and synthetic blending components at the place of manufacture but can be used to describe the quality of aviation turbine fuels for contractual transfer at all points in the distribution system.

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 While aviation turbine fuels defined by this specification can be used in applications other than aviation turbine engines, requirements for such other applications have not been considered in the development of this specification.

1.6 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.

1.7 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 and health practices and determine the applicability of regulatory limitations prior to use.

PDF Catalog

PDF Pages PDF Title
1 Scope
Referenced Documents
3 General
Terminology
Classification
Materials and Manufacture
Detailed Requirements
4 TABLE 1
5 TABLE 1
TABLE 2
6 Workmanship, Finish and Appearance
Sampling
Report
Test Methods
Keywords
7 A1. HYDROPROCESSED SYNTHESIZED PARAFFINIC KEROSINE
A1.1 Scope
A1.2 General
A1.3 Terminology
A1.4 Materials and Manufacture
A1.5 Detailed Batch Requirements
A1.6 Other Detailed Requirements
8 TABLE A1.1
TABLE A1.2
9 X1. PERFORMANCE CHARACTERISTICS OF AVIATION TURBINE FUELS
X1.1 Introduction
X1.2 Significance and Use
X1.3 Thermal Stability
TABLE X1.1
10 X1.4 Combustion
X1.5 Fuel Metering and Aircraft Range
X1.6 Fuel Atomization
11 X1.7 Fluidity at Low Temperatures
X1.8 Compatibility with Elastomer and the Metals in the Fuel System and Turbine
X1.9 Fuel Storage Stability
X1.10 Fuel Lubricity
12 X1.11 Fuel Handling
X1.12 Fuel Cleanliness and Contamination
X1.13 Surfactants
13 X1.14 Cleanliness at Time of Fuel Custody Transfer at Airport
X1.15 Miscellaneous
X2. CONTROL OF PROCESSING ADDITIVES
X2.1
14 X2.2
X3. FORM FOR REPORTING INSPECTION DATA ON AVIATION TURBINE FUELS
X3.1 Introduction
X3.2 Dimensions of Standard Form
15 FIG. X3.1
16 X3.6 Instructions Applicable to All Forms
FIG. X3.2
17 X3.7 Instructions for Executing Column 4 on All Forms
FIG. X3.3
ASTM-D7566 2009
$44.96