Standard Practice for Aeroplane Turbine Fuel System Hot Weather Operations

SIGNIFICANCE AND USE
4.1 This specification provides designers of general aviation aeroplanes a process for evaluating and testing a fuel system under hot weather conditions to ensure safety during flight. The specification is applicable to kerosene-type turbine engine fuels and fuel systems for traditional general aviation aeroplanes.
SCOPE
1.1 This standard practice provides requirements for performing hot weather testing as a means of compliance to Subsection 7.7 of Specification F3063/F3063M for kerosene-type turbine fuels such as Jet A and Jet A-1 (Specification D1655). The appendix provides supplemental information and considerations for turbine fuel system hot weather operation. The material was developed through open consensus of international experts in general aviation.  
1.2 An applicant intending to propose this information as Means of Compliance for a design approval must seek guidance from their respective oversight authority (for example, published guidance from applicable civil aviation authorities (CAAs)) concerning the acceptable use and application thereof. For information on which oversight authorities have accepted this standard (in whole or in part) as an acceptable Means of Compliance to their regulatory requirements hereinafter (“the Rules”), refer to the ASTM Committee F44 web page (www.astm.org/COMMITTEE/F44.htm).  
1.3 The values stated in either SI units or inch-pound units are to be regarded separately as standard. The values stated in each system are not necessarily exact equivalents; therefore, to ensure conformance with the standard, each system shall be used independently of the other, and values from the two systems shall not be combined.  
1.4 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. A specific warning is given in Section 6 on Test Setup.  
1.5 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.

General Information

Status
Published
Publication Date
31-Dec-2020
Drafting Committee
Current Stage
Ref Project

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ASTM F3397/F3397M-21 - Standard Practice for Aeroplane Turbine Fuel System Hot Weather Operations
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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.
Designation: F3397/F3397M − 21
Standard Practice for
1
Aeroplane Turbine Fuel System Hot Weather Operations
ThisstandardisissuedunderthefixeddesignationF3397/F3397M;thenumberimmediatelyfollowingthedesignationindicatestheyear
of original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval.
A superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
1. Scope 2. Referenced Documents
2
1.1 This standard practice provides requirements for per- 2.1 ASTM Standards:
forming hot weather testing as a means of compliance to D910 Specification for Leaded Aviation Gasolines
Subsection 7.7 of Specification F3063/F3063M for kerosene- D1655 Specification for Aviation Turbine Fuels
type turbine fuels such as Jet A and Jet A-1 (Specification F3063/F3063M Specification for Aircraft Fuel Storage and
D1655). The appendix provides supplemental information and Delivery
considerations for turbine fuel system hot weather operation. F3064/F3064M Specification for Aircraft Powerplant
The material was developed through open consensus of inter- Control, Operation, and Indication
national experts in general aviation. F3179/F3179M Specification for Performance of Aircraft
3
2.2 FAA Standards:
1.2 An applicant intending to propose this information as
AC 23-16A Powerplant Guide for Certification of Part 23
Means of Compliance for a design approval must seek guid-
Airplanes and Airships
ance from their respective oversight authority (for example,
CAR 3 Airplane Airwothiness – Normal, Utility, and Acro-
published guidance from applicable civil aviation authorities
batic Categories
(CAAs)) concerning the acceptable use and application
4
thereof. For information on which oversight authorities have
2.3 CRC Report:
accepted this standard (in whole or in part) as an acceptable
CRC AV-20-14 Determination of Heat of Vaporization and
Means of Compliance to their regulatory requirements herein-
Creating Enthalpy Diagrams for Several Common Jet
after (“the Rules”), refer to the ASTM Committee F44 web
Fuels
page (www.astm.org/COMMITTEE/F44.htm).
2.4 Fuel Standards:
1.3 The values stated in either SI units or inch-pound units GOST 10227 Russian Standards and Regulations: Jet Fuel
5
are to be regarded separately as standard. The values stated in Specification
each system are not necessarily exact equivalents; therefore, to MIL-DTL-5624 Detail Specification: Turbine Fuel,
6
ensure conformance with the standard, each system shall be
Aviation, Grades JP-4 and JP-5
used independently of the other, and values from the two
systems shall not be combined. 3. Terminology
1.4 This standard does not purport to address all of the
3.1 Definitions:
safety concerns, if any, associated with its use. It is the
3.1.1 fuel volatility, n—thefuel’stendencytoevaporate(that
responsibility of the user of this standard to establish appro- is, change to a vapor from a fluid).
priate safety, health, and environmental practices and deter-
3.1.2 vapor pressure, n—pressure exerted by its vapor in
mine the applicability of regulatory limitations prior to use. A
equilibrium with the liquid at a specific temperature with the
specific warning is given in Section 6 on Test Setup.
absence of air over the fuel.
1.5 This international standard was developed in accor-
dance with internationally recognized principles on standard-
ization established in the Decision on Principles for the
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
Development of International Standards, Guides and Recom-
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
Standards volume information, refer to the standard’s Document Summary page on
mendations issued by the World Trade Organization Technical
the ASTM website.
Barriers to Trade (TBT) Committee.
3
Available from Federal Aviation Administration (FAA), 800 Independence
Ave., SW, Washington, DC 20591, http://www.faa.gov.
4
Available from Coordinating Research Council (CRC), 5755 North Point
1
This practice is under the jurisdiction of ASTM Committee F44 on General Parkway, Suite 265, Alpharetta, GA 30022, https://www.crcao.org.
5
Aviation Aircraft and is the direct responsibility of Subcommittee F44.40 on Available from Russian Gost, LLC. P.O. Box 366, Alief, TX 77411, https://
Powerplant. www.russiangost.com.
6
Current edition approved Jan. 1, 2021. Published February 2021. DOI: 10.1520/ Available from DLA Document Services, Building 4/D, 700 Robbins Ave.,
F3397_F3397M-21. Philadelphia, PA 19111-5094, http://quicksearch.dla.mil.
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