ASTM F3064/F3064M-18a

Standard Specification for Aircraft Powerplant Control, Operation, and Indication

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, 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.

General Information

• Status: Historical
• Publication Date: 31-Jan-2018
• ICS: 49.140 - Space systems and operations
• Technical Committee: F44 - General Aviation Aircraft
• Drafting Committee: F44.40 - Powerplant

Standards Content (Sample)

NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.
Contact ASTM International (www.astm.org) for the latest information
Designation: F3064/F3064M −18a
Standard Specification for
1
Aircraft Powerplant Control, Operation, and Indication
ThisstandardisissuedunderthefixeddesignationF3064/F3064M;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 specification covers minimum requirements for the 2.1 ASTM Standards:
F3060 Terminology for Aircraft
control, indication, and operational characteristics of propul-
sion systems. It was developed based on propulsion system F3062/F3062M Specification for Installation of Powerplant
Systems
installed on aeroplanes, but may be applicable to other appli-
F3063/F3063M Specification for Aircraft Fuel and Energy
cations as well.
Storage and Delivery
1.2 The applicant for a design approval must seek the
F3066/F3066M Specification forAircraft Powerplant Instal-
individual guidance to their respective CAA body concerning
lation Hazard Mitigation
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 Specification for Crew Interface in Aircraft
theirAeroplaneAirworthinessregulations(Hereinafterreferred
3
2.2 Other Standards:
to as “the Rules”), refer to ASTM F44 webpage
US 14 CFR (Code of Federal Regulations) Part 23 Amend-
(www.ASTM.org/COMITTEE/F44.htm) which includes CAA
ment 62
website links.
3. Terminology
1.3 Units—The values stated are SI units followed by
imperial units in brackets. The values stated in each system 3.1 The following are a selection of relevant terms. See
may not be exact equivalents; therefore, each system shall be Terminology F3060 for more definitions and abbreviations.
used independently of the other. Combining values from the
3.2 Definitions:
two systems may result in non-conformance with the standard.
3.2.1 automatic power reserve (APR) system, n—the auto-
1.4 This standard does not purport to address all of the
matic system used only during takeoff, including all devices
safety concerns, if any, associated with its use. It is the
both mechanical and electrical that sense engine failure,
responsibility of the user of this standard to establish appro-
transmit signals, actuate fuel controls or power levers on
priate safety, health, and environmental practices and deter-
operating engines, including power sources, to achieve the
mine the applicability of regulatory limitations prior to use.
scheduled power increase and furnish cockpit information on
1.5 This international standard was developed in accor-
system operation.
dance with internationally recognized principles on standard-
3.2.2 critical time interval, n—period starting at V minus
1
ization established in the Decision on Principles for the
one second and ending at the intersection of the engine and
Development of International Standards, Guides and Recom-
APR failure flight path line with the minimum performance all
mendations issued by the World Trade Organization Technical
engine flight path line. The engine and APR failure flight path
Barriers to Trade (TBT) Committee.
line intersects the one-engine-inoperative flight path line at 122
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
1
ThisspecificationisunderthejurisdictionofASTMCommitteeF44onGeneral contact ASTM Customer Service at [e-mail]. For Annual Book of ASTM
Aviation Aircraft and is the direct responsibility of Subcommittee F44.40 on Standards volume information, refer to the standard’s Document Summary page on
Powerplant. the ASTM website.
3
Current edition approved Feb. 1, 2018. Published February 2018. Originally AvailablefromU.S.GovernmentPrintingOfficeSuperintendentofDocuments,
approved in 2015. Last previous edition approved in 2018 as F3064/F3064M – 18. 732 N. Capitol St., NW, Mail Stop: SDE, Washington, DC 20401, http://
DOI: 10.1520/F3064_F3064M-18A. www.access.gpo.gov.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

---------------------- Page: 1 ----------------------
F3064/F3064M − 18a
m [400 ft] above the takeoff surface. The engine and APR 4.1.7.2 For power-assisted valves, a means to indicate to the
failure flight path is based on the airplane’s performance and flight crew when the valve is in the fully open or fully closed
must have a positive gradient of at least 0.5 % at 122 m [400 position; or is moving between the fully open and fully closed
ft] above the takeoff surface. See Fig. 1. position.
3.2.3 selected tak
...

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 − 18 F3064/F3064M − 18a
Standard Specification for
Control, Operational Characteristics and Installation of
Instruments and Sensors of Propulsion SystemsAircraft
1
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.
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, 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
F3062/F3062M Specification for Installation of Powerplant Systems
F3063/F3063M Specification for Aircraft Fuel and Energy Storage and Delivery
F3066/F3066M Specification for Aircraft Powerplant Installation Hazard Mitigation
F3116/F3116M Specification for Design Loads and Conditions
F3117 Specification for Crew Interface in Aircraft
3
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.
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 Jan. 1, 2018Feb. 1, 2018. Published February 2018. Originally approved in 2015. Last previous edition approved in 20152018 as
F3064/F3064M – 15.F3064/F3064M – 18. DOI: 10.1520/F3064_F3064M-18.10.1520/F3064_F3064M-18A.
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or contact ASTM Customer Service at [e-mail]. For Annual Book of ASTM Standards
volume information, refer to the standard’s Document Summary page on the ASTM website.
3
Available from U.S. Government Printing Office Superintendent of Documents, 732 N. Capitol St., NW, Mail Stop: SDE, Washington, DC 20401, http://
www.access.gpo.gov.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

---------------------- Page: 1 ----------------------
F3064/F3064M − 18a
3.2.2 critical time interval, n—period starting at V minus one second and ending at the intersection of the engine and APR
1
failure flight path line with the minimum performance all engine flight path line. The engine and APR failure flight path line
intersects the one-engi
...