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ASTM D7566-10a
Standard Specification for Aviation Turbine Fuel Containing Synthesized Hydrocarbons (Includes all amendments And changes 6/29/2011).
Automatically translated name:
Standard Specification for Aviation Turbine Fuel Containing Synthesized Hydrocarbons
STANDARD published on 1.7.2010
The information about the standard:
Designation standards: ASTM D7566-10a
Note: WITHDRAWN
Publication date standards: 1.7.2010
SKU: NS-38730
The number of pages: 20
Approximate weight : 60 g (0.13 lbs)
Country: American technical standard
Category: Technical standards ASTM
Annotation of standard text ASTM D7566-10a :
Keywords:
aviation turbine fuel, avtur, Jet A, Jet A-1, jet fuel, synthesized hydrocarbons, synthesized paraffinic kerosene, synthetic blending component, turbine fuel, Aviation turbine fuels, Synthesized hydrocarbons, Turbine fuels, ICS Number Code 75.160.20 (Liquid fuels)
Additional information
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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 D1655 and shall be regarded as Specification D1655 turbine fuel. Once released to this specification (D7566) the requirements of this specification are no longer applicable: any recertification shall be done to D1655. Field blending of synthesized paraffinic kerosine (SPK) with D1655 fuel (which may on the whole or in part have originated as D7566 fuel) shall be considered batch origination in which case all of the requirements of this specification (D7566) apply, however the fuel shall be regarded as D1655 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. |
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