ASTM F3064/F3064M-18

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Designation: F3064/F3064M − 15 F3064/F3064M − 18
Standard Specification for
Control, Operational Characteristics and Installation of
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Instruments and Sensors of Propulsion Systems
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.
1.3 Units—The values stated are SI units followed by imperial units in brackets. The values stated in each system may not be
exact equivalents; therefore, each system shall be used independently of the other. Combining values from the two systems may
result in non-conformance with the standard.
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 safety, health, and healthenvironmental 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
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2.1 ASTM Standards:
F3060 Terminology for Aircraft
F3062F3062/F3062M Specification for the Installation of Powerplant Systems
F3063F3063/F3063M Specification for Design and Integration of Fuel/Energy Aircraft Fuel and Energy Storage and Delivery
System Installations
F3066F3066/F3066M Specification for Aircraft Powerplant SystemsInstallation Hazard Mitigation
F3116F3116/F3116M Specification for Design Loads and Conditions
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2.2 Other Standards:
US 14 CFR (Code of Federal Regulations) Part 23 Amendment 62
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 all devices both
mechanical and electrical that sense engine failure, transmit signals, actuate fuel controls or power levers on operating engines,
including power sources, to achieve the scheduled power increase and furnish cockpit information on system operation.
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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, 2015Jan. 1, 2018. Published June 2015February 2018. Originally approved in 2015. Last previous edition approved in 2015 as
F3064/F3064M – 15. DOI: 10.1520/F3064-15.10.1520/F3064_F3064M-18.
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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.
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F3064/F3064M − 18
3.2.2 critical time interval, n—period starting at V minus one second and ending at the intersection of the engine and APR
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failure flight path line with the minimum performance all engine flight path line. The engine and APR failure flight path line
intersects the one-engine-inoperative flight path
...