ASTM F3064/F3064M-24
(Specification)Standard Specification for Aircraft Powerplant Control, Operation, and Indication
Standard Specification for Aircraft Powerplant Control, Operation, and Indication
ABSTRACT
This specification provides minimum requirements for the control, indication, and operational characteristics of propulsion systems. It was developed based on propulsion system installed on aeroplanes, but may be applicable to other applications. The applicant for a design approval must seek the individual guidance to their respective civil aviation authority (CAA) body concerning the use of this specification as part of a certification plan.
SCOPE
1.1 This specification covers minimum requirements for the control, indication, and operational characteristics of propulsion systems. It was developed based on propulsion system installed on aeroplanes, but may be applicable to other applications as well.
1.2 The applicant for a design approval must seek the individual guidance to their respective CAA body concerning the use of this standard as part of a certification plan. For information on which CAA regulatory bodies have accepted this standard (in whole or in part) as a means of compliance to their Aeroplane Airworthiness regulations (Hereinafter referred to as “the Rules”), refer to ASTM F44 webpage (www.ASTM.org/COMITTEE/F44.htm) which includes CAA website links. Annex A1 maps the Means of Compliance described in this specification to EASA CS-23, amendment 5, or later, and FAA 14 CFR Part 23, amendment 64, or later.
1.3 Units—The values stated are SI units followed by imperial units in brackets. 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.
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.
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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: F3064/F3064M − 24
Standard Specification for
1
Aircraft Powerplant Control, Operation, and Indication
This standard is issued under the fixed designation F3064/F3064M; the number immediately following the designation indicates the year
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
2.1 ASTM Standards:
1.1 This specification covers minimum requirements for the
F3060 Terminology for Aircraft
control, indication, and operational characteristics of propul-
F3061/F3061M Specification for Systems and Equipment in
sion systems. It was developed based on propulsion system
Aircraft
installed on aeroplanes, but may be applicable to other appli-
F3062/F3062M Specification for Aircraft Powerplant Instal-
cations as well.
lation
1.2 The applicant for a design approval must seek the
F3063/F3063M Specification for Aircraft Fuel Storage and
individual guidance to their respective CAA body concerning
Delivery
the use of this standard as part of a certification plan. For
F3116/F3116M Specification for Design Loads and Condi-
information on which CAA regulatory bodies have accepted
tions
this standard (in whole or in part) as a means of compliance to F3117/F3117M Specification for Crew Interface in Aircraft
their Aeroplane Airworthiness regulations (Hereinafter referred
F3233/F3233M Specification for Flight and Navigation In-
to as “the Rules”), refer to ASTM F44 webpage strumentation in Aircraft
(www.ASTM.org/COMITTEE/F44.htm) which includes CAA F3367 Practice for Simplified Methods for Addressing High-
Intensity Radiated Fields (HIRF) and Indirect Effects of
website links. Annex A1 maps the Means of Compliance
Lightning on Aircraft
described in this specification to EASA CS-23, amendment 5,
F3432 Practice for Powerplant Instruments
or later, and FAA 14 CFR Part 23, amendment 64, or later.
3
2.2 EASA Standard:
1.3 Units—The values stated are SI units followed by
CS-23 Certification Specifications for Normal-Category
imperial units in brackets. The values stated in each system are
Aeroplanes
4
not necessarily exact equivalents; therefore, to ensure confor-
2.3 FAA Documents:
mance with the standard, each system shall be used indepen-
14 CFR Part 23 Airworthiness Standards: Normal Category
dently of the other, and values from the two systems shall not
Airplanes
be combined.
AC 33.28-1 Compliance Criteria For 14 CFR §33.28, Air-
craft Engines, Electrical And Electronic Engine Control
1.4 This standard does not purport to address all of the
Systems
safety concerns, if any, associated with its use. It is the
AC 33.28-2 Guidance Material For 14 CFR §33.28, Recip-
responsibility of the user of this standard to establish appro-
rocating Engines, Electrical And Electronic Engine Con-
priate safety, health, and environmental practices and deter-
trol Systems
mine the applicability of regulatory limitations prior to use.
AC 33.28-3 Guidance Material For 14 CFR §33.28, Engine
1.5 This international standard was developed in accor-
Control Systems
dance with internationally recognized principles on standard-
ization established in the Decision on Principles for the
3. Terminology
Development of International Standards, Guides and Recom-
3.1 The following are a selection of relevant terms. See
mendations issued by the World Trade Organization Technical
Terminology F3060 for more definitions and abbreviations.
Barriers to Trade (TBT) Committee.
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
1
This specification is under the jurisdiction of ASTM Committee F44 on General Standards volume information, refer to the standard’s Document Summary page on
Aviation Aircraft and is the direct responsibility of Subcommittee F44.40 on the ASTM website.
3
Powerplant. Available from European Union Aviation Safety Agency (EASA), Konrad-
Current edition approved March 1, 2024. Published March 2024. Originally Adenauer-Ufer 3, D-50668 Cologne, Germany, https://www.easa.europa.eu.
4
approved in 2015. Last previous edition approved in 2021 as F3064/F3064M–21. Available from Federal Aviation Administration (FAA), 800 Independence
DOI: 10.1520/F3064_F3064M-24. Ave., SW, Washington, DC 20591, http://www.faa.gov.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
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F3064/F3064M − 24
3.2 Definitions: 4. Powerplant
...
This document is not an ASTM standard and is intended only to provide the user of an ASTM standard an indication of what changes have been made to the previous version. Because
it may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current version
of the standard as published by ASTM is to be considered the official document.
Designation: F3064/F3064M − 21 F3064/F3064M − 24
Standard Specification for
1
Aircraft Powerplant Control, Operation, and Indication
This standard is issued under the fixed designation F3064/F3064M; the number immediately following the designation indicates the year
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
1.1 This specification covers minimum requirements for the control, indication, and operational characteristics of propulsion
systems. It was developed based on propulsion system installed on aeroplanes, but may be applicable to other applications as well.
1.2 The applicant for a design approval must seek the individual guidance to their respective CAA body concerning the use of this
standard as part of a certification plan. For information on which CAA regulatory bodies have accepted this standard (in whole
or in part) as a means of compliance to their Aeroplane Airworthiness regulations (Hereinafter referred to as “the Rules”), refer
to ASTM F44 webpage (www.ASTM.org/COMITTEE/F44.htm) which includes CAA website links. Annex A1 maps the Means
of Compliance described in this specification to EASA CS-23, amendment 5, or later, and FAA 14 CFR Part 23, amendment 64,
or later.
1.3 Units—The values stated are SI units followed by imperial units in brackets. 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.
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.
2. Referenced Documents
2
2.1 ASTM Standards:
F3060 Terminology for Aircraft
F3061/F3061M Specification for Systems and Equipment in Aircraft
F3062/F3062M Specification for Aircraft Powerplant Installation
F3063/F3063M Specification for Aircraft Fuel Storage and Delivery
F3116/F3116M Specification for Design Loads and Conditions
F3117/F3117M Specification for Crew Interface in Aircraft
F3233/F3233M Specification for Flight and Navigation Instrumentation in Aircraft
1
This specification is under the jurisdiction of ASTM Committee F44 on General Aviation Aircraft and is the direct responsibility of Subcommittee F44.40 on Powerplant.
Current edition approved May 1, 2021March 1, 2024. Published May 2021March 2024. Originally approved in 2015. Last previous edition approved in 20202021 as
F3064/F3064M–20a. DOI: 10.1520/F3064_F3064M-21.–21. DOI: 10.1520/F3064_F3064M-24.
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or 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 the ASTM website.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
---------------------- Page: 1 ----------------------
F3064/F3064M − 24
F3367 Practice for Simplified Methods for Addressing High-Intensity Radiated Fields (HIRF) and Indirect Effects of Lightning
on Aircraft
F3432 Practice for Powerplant Instruments
3
2.2 EASA Standard:
CS-23 Certification Specifications for Normal-Category Aeroplanes
4
2.3 FAA Standard:Documents:
14 CFR Part 23 Airworthiness Standards: Normal Category Airplanes
AC 33.28-1 Compliance Criteria For 14 CFR §33.28, Aircraft Engines, Electrical And Electronic Engine Control Systems
AC 33.28-2 Guidance Material For 14 CFR §33.28, Reciprocating Engines, Electrical And Electronic Engine Control Systems
AC 33.28-3 Guidance Material For 14 CFR §33.28, Engine Control Systems
3. Terminology
3.1 The following are a selection of relevant terms. See Terminology F3060 for more definitions and abbreviations.
3.2 Definitions:
3.2.1 automatic power reserve (APR) system, n—the automatic system used only during takeoff, including al
...
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