ASTM F3062/F3062M-19
(Specification)Standard Specification for Aircraft Powerplant Installation
Standard Specification for Aircraft Powerplant Installation
SCOPE
1.1 This specification covers minimum requirements for the installation and integration of powerplant system units.
1.2 This specification is applicable to small aeroplanes as defined in the F44 terminology standard. Use of the term airplane is used throughout this specification and will mean “small airplane.”
1.3 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 Small Aircraft Airworthiness regulations (Hereinafter referred to as “the Rules”), refer to the ASTM F44 webpage (www.ASTM.org/COMITTEE/F44.htm) which includes CAA website links.
1.4 References within this standard normally refer to documents in United States legal system. Appendix X1 cross references documents in the legal system of other countries of corresponding content.
1.5 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.
1.6 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.
1.7 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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Designation:F3062/F3062M −19
Standard Specification for
1
Aircraft Powerplant Installation
ThisstandardisissuedunderthefixeddesignationF3062/F3062M;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:
installation and integration of powerplant system units. F2339 Practice for Design and Manufacture of Reciprocat-
ing Spark Ignition Engines for Light Sport Aircraft
1.2 This specification is applicable to small aeroplanes as
F2506 Specification for Design and Testing of Light Sport
defined in the F44 terminology standard. Use of the term
Aircraft Propellers
airplane is used throughout this specification and will mean
F2538 Practice for Design and Manufacture of Reciprocat-
“small airplane.”
ing Compression Ignition Engines for Light SportAircraft
1.3 The applicant for a design approval must seek the
F2840 Practice for Design and Manufacture of Electric
individual guidance to their respective CAA body concerning
Propulsion Units for Light Sport Aircraft
the use of this standard as part of a certification plan. For
F3060 Terminology for Aircraft
information on which CAA regulatory bodies have accepted
F3063/F3063M Specification for Aircraft Fuel and Energy
this standard (in whole or in part) as a means of compliance to
Storage and Delivery
their Small Aircraft Airworthiness regulations (Hereinafter
F3066/F3066M Specification forAircraft Powerplant Instal-
referred to as “the Rules”), refer to the ASTM F44 webpage
lation Hazard Mitigation
(www.ASTM.org/COMITTEE/F44.htm) which includes CAA
F3117/F3117M Specification for Crew Interface in Aircraft
website links.
3
2.2 Code of Federal Regulations (CFR):
1.4 References within this standard normally refer to docu-
14 CFR part 23 Airworthiness Standards: Normal Category
ments in United States legal system. Appendix X1 cross
Airplanes
references documents in the legal system of other countries of
14 CFR part 33 Airworthiness Standards: Aircraft Engines
corresponding content.
14CFRpart34 FuelVentingandExhaustEmissionRequire-
ments for Turbine Engine Powered Airplanes
1.5 Units—The values stated are SI units followed by
14 CFR part 35 Airworthiness Standards: Propellers
imperial units in brackets. The values stated in each system
4
may not be exact equivalents; therefore, each system shall be
2.3 Federal Aviation Administration (FAA) Publications:
used independently of the other. Combining values from the
AC 23-8C Flight Test Guide for Certification of Part 23
two systems may result in non-conformance with the standard.
Airplanes
CAR 13 Aircraft Engine Airworthiness
1.6 This standard does not purport to address all of the
TSO-C77 Technical Standard Order – Gas Turbine Auxil-
safety concerns, if any, associated with its use. It is the
liary Power Units
responsibility of the user of this standard to establish appro-
5
priate safety, health, and environmental practices and deter-
2.4 JAA Documents:
mine the applicability of regulatory limitations prior to use.
JAR-E Engines
1.7 This international standard was developed in accor-
JAR-P Propellers
dance with internationally recognized principles on standard-
JAR-22 Sailplanes and Powered Sailplanes
ization established in the Decision on Principles for the
Development of International Standards, Guides and Recom-
mendations issued by the World Trade Organization Technical
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
Barriers to Trade (TBT) Committee. 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.
1 3
ThisspecificationisunderthejurisdictionofASTMCommitteeF44onGeneral Available from U.S. Government Publishing Office, 732 N. Capitol St., NW,
Aviation Aircraft and is the direct responsibility of Subcommittee F44.40 on Washington, DC 20401, https://www.gpo.gov.
4
Powerplant. Available from Federal Aviation Administration (FAA), 800 Independence
Current edition approved Feb. 1, 2019. Published March 2019. Originally Ave., SW, Washington, DC 20591, https://www.faa.gov.
5
approved in 2015. Last previous edition approved in 2018 as F3062/F3062M–18. Available from Global Engineering Documents, 15 Inverness Way, East
DOI: 10.1520/F3062_F3062M–19. Englewood, CO 80112-5704, https://global.ihs.com.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
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F3062/F3062M−19
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2.5
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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: F3062/F3062M − 18 F3062/F3062M − 19
Standard Specification for
1
Aircraft Powerplant Installation
This standard is issued under the fixed designation F3062/F3062M; 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 installation and integration of powerplant system units.
1.2 This specification is applicable to small aeroplanes as defined in the F44 terminology standard. Use of the term airplane is
used throughout this specification and will mean “small airplane.”
1.3 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 Small Aircraft Airworthiness regulations (Hereinafter referred to as “the Rules”), refer
to the ASTM F44 webpage (www.ASTM.org/COMITTEE/F44.htm) which includes CAA website links.
1.4 References within this standard normally refer to documents in United States legal system. Appendix X1 cross references
documents in the legal system of other countries of corresponding content.
1.5 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.
1.6 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.
1.7 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:
F2339 Practice for Design and Manufacture of Reciprocating Spark Ignition Engines for Light Sport Aircraft
F2506 Specification for Design and Testing of Light Sport Aircraft Propellers
F2538 Practice for Design and Manufacture of Reciprocating Compression Ignition Engines for Light Sport Aircraft
F2840 Practice for Design and Manufacture of Electric Propulsion Units for Light Sport Aircraft
F3060 Terminology for Aircraft
F3063/F3063M Specification for Aircraft Fuel and Energy Storage and Delivery
F3066/F3066M Specification for Aircraft Powerplant Installation Hazard Mitigation
F3117F3117/F3117M Specification for Crew Interface in Aircraft
3
2.2 Code of Federal Regulations (CFR):
14 CFR part 3323 Airworthiness Standards: Aircraft EnginesNormal Category Airplanes
14 CFR part 3533 Airworthiness Standards: PropellersAircraft Engines
14 CFR part 34 Fuel Venting and Exhaust Emission Requirements for Turbine Engine Powered Airplanes
14 CFR part 35 Airworthiness Standards: Propellers
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, 2019. Published February 2018March 2019. Originally approved in 2015. Last previous edition approved in 20162018 as
F3062/F3062M – 16.F3062/F3062M–18. DOI: 10.1520/F3062_F3062M-18.10.1520/F3062_F3062M–19.
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’sstandard’s Document Summary page on the ASTM website.
3
Available from U.S. Government Printing Office Superintendent of Documents, Publishing Office, 732 N. Capitol St., NW, Mail Stop: SDE, Washington, DC 20401,
www.access.gpo.gov.https://www.gpo.gov.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
---------------------- Page: 1 ----------------------
F3062/F3062M − 19
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2.3 Federal Aviation Administration (FAA) Publications:
AC 2
...
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