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ASTM D7566-19a

Historical Revision

Standard Specification for Aviation Turbine Fuel Containing Synthesized Hydrocarbons

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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, as follows:

1.2.1 Aviation turbine fuel manufactured, certified, and released to all the requirements of Table 1 of this specification (D7566), meets the requirements of Specification D1655 and shall be regarded as Specification D1655 turbine fuel. Duplicate testing is not necessary; the same data may be used for both D7566 and D1655 compliance. Once the fuel is released to this specification (D7566) the unique requirements of this specification are no longer applicable: any recertification shall be done in accordance with Table 1 of Specification D1655.

1.2.2 Field blending of synthesized paraffinic kerosine (SPK) blendstocks, as described in Annex A1 (FT SPK), Annex A2 (HEFA SPK), Annex A3 (SIP), Annex A4 synthesized paraffinic kerosine plus aromatics (SPK/A), or Annex A5 (ATJ) 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 Table 1 of this specification (D7566) apply and shall be evaluated. Short form conformance test programs commonly used to ensure transportation quality are not sufficient. The fuel shall be regarded as D1655 turbine fuel after certification and release as described in 1.2.1.

1.2.3 Once a fuel is redesignated as D1655 aviation turbine fuel, it can be handled in the same fashion as the equivalent refined D1655 aviation turbine fuel.

1.3 This specification defines the minimum property requirements for aviation turbine fuel that contain synthesized hydrocarbons and lists acceptable additives for use in civil operated engines and aircrafts. Specification D7566 is directed at civil applications, and maintained as such, but may be adopted for military, government, or other specialized uses.

1.4 This specification can be used as a standard in describing the quality of aviation turbine fuel from production to the aircraft. However, this specification does not define the quality assurance testing and procedures necessary to ensure that fuel in the distribution system continues to comply with this specification after batch certification. Such procedures are defined elsewhere, for example in ICAO 9977, EI/JIG Standard 1530, JIG 1, JIG 2, API 1543, API 1595, and ATA-103.

1.5 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.

1.6 While aviation turbine fuels defined by Table 1 of 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.

1.7 Synthetic blending components, synthetic fuels, and blends of synthetic fuels with conventional petroleum-derived fuels in this specification have been evaluated and approved in accordance with the principles established in Practice D4054.

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

1.9 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, health, and environmental practices and determine the applicability of regulatory limitations prior to use.

1.10 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.


SDO ASTM: ASTM International
Document Number D7566
Publication Date Dec. 1, 2019
Language en - English
Page Count 30
Revision Level 19a
Supercedes
Committee D02.J0.06
Publish Date Document Id Type View
Nov. 1, 2024 D7566-24D Revision
Oct. 1, 2024 D7566-24C Revision
July 1, 2024 D7566-24B Revision
March 15, 2024 D7566-24A Revision
March 1, 2024 D7566-24 Revision
Oct. 1, 2023 D7566-23B Revision
July 1, 2023 D7566-23A Revision
June 1, 2023 D7566-23 Revision
Oct. 1, 2022 D7566-22A Revision
July 1, 2022 D7566-22 Revision
July 1, 2021 D7566-21 Revision
Dec. 1, 2020 D7566-20C Revision
Sept. 1, 2020 D7566-20B Revision
July 15, 2020 D7566-20A Revision
May 1, 2020 D7566-20 Revision
Dec. 15, 2019 D7566-19B Revision
Dec. 1, 2019 D7566-19A Revision
March 1, 2019 D7566-19 Revision
Dec. 1, 2018 D7566-18A Revision
April 1, 2018 D7566-18 Revision
Dec. 1, 2017 D7566-17B Revision
Oct. 1, 2017 D7566-17A Revision
May 1, 2017 D7566-17 Revision
July 1, 2016 D7566-16B Revision
June 1, 2016 D7566-16A Revision
April 1, 2016 D7566-16 Revision
Nov. 1, 2015 D7566-15C Revision
Oct. 1, 2015 D7566-15B Revision
Aug. 15, 2015 D7566-15A Revision
June 15, 2015 D7566-15 Revision
Dec. 1, 2014 D7566-14C Revision
Oct. 1, 2014 D7566-14B Revision
June 15, 2014 D7566-14A Revision
May 15, 2014 D7566-14 Revision
May 1, 2013 D7566-13 Revision
Nov. 1, 2012 D7566-12A Revision
Oct. 1, 2012 D7566-12 Revision
July 15, 2011 D7566-11A Revision
July 1, 2011 D7566-11 Revision
July 1, 2010 D7566-10A Revision
May 1, 2010 D7566-10 Revision
Sept. 1, 2009 D7566-09 Revision