Norme ASTM D7566-09

Spécification standard pour le carburant de turbine d'aviation contenant des hydrocarbures synthétisés
Statut
:
Remplacée
Date de publication
:
2009
Langues
:
EN
ICS
:
75.160.20 Combustibles liquides
Sommaire :

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 Once released to this specification (D 7566) the requirements of this specification are no longer applicable: any recertification shall be done to D 1655.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 fue
l) 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.

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