ASTM F3062/F3062M-20
(Specification)Standard Specification for Aircraft Powerplant Installation
Standard Specification for Aircraft Powerplant Installation
ABSTRACT
This specification provides minimum requirements for the installation and integration of powerplant system units and is applicable to small aeroplanes as defined in the F44 terminology standard. 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.
This specification covers: air induction system for each engine and auxiliary power unit and their accessories, powerplant exhaust system, forced air induction and bleed air systems, oil system, liquid cooling, turbojet and turbofan reversing systems, and powerplant accessories and components. Also specified are tank tests for pressure, vibration, and tank sloshing.
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 shall 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 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.
1.6 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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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:F3062/F3062M −20
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 mendations issued by the World Trade Organization Technical
Barriers to Trade (TBT) Committee.
1.1 This specification covers minimum requirements for the
installation and integration of powerplant system units.
2. Referenced Documents
1.2 This specification is applicable to small aeroplanes as 2
2.1 ASTM Standards:
defined in the F44 terminology standard. Use of the term
F2339 Practice for Design and Manufacture of Reciprocat-
airplane is used throughout this specification and will mean
ing Spark Ignition Engines for Light Sport Aircraft
“small airplane.”
F2506 Specification for Design and Testing of Light Sport
1.3 The applicant for a design approval shall seek the Aircraft Propellers
F2538 Practice for Design and Manufacture of Reciprocat-
individual guidance to their respective CAA body concerning
the use of this standard as part of a certification plan. For ing Compression Ignition Engines for Light SportAircraft
F2840 Practice for Design and Manufacture of Electric
information on which CAA regulatory bodies have accepted
this standard (in whole or in part) as a means of compliance to Propulsion Units for Light Sport Aircraft
F3060 Terminology for Aircraft
their Small Aircraft Airworthiness regulations (Hereinafter
referred to as “the Rules”), refer to the ASTM F44 webpage F3063/F3063M Specification for Aircraft Fuel Storage and
Delivery
(www.ASTM.org/COMITTEE/F44.htm) which includes CAA
website links. F3066/F3066M Specification forAircraft Powerplant Instal-
lation Hazard Mitigation
1.4 References within this standard normally refer to docu-
F3117/F3117M Specification for Crew Interface in Aircraft
ments in United States legal system. Appendix X1 cross
3
2.2 Code of Federal Regulations (CFR):
references documents in the legal system of other countries of
14 CFR part 23 Airworthiness Standards: Normal Category
corresponding content.
Airplanes
1.5 Units—The values stated are SI units followed by
14 CFR part 33 Airworthiness Standards: Aircraft Engines
imperial units in brackets.The values stated in each system are
14CFRpart34 FuelVentingandExhaustEmissionRequire-
not necessarily exact equivalents; therefore, to ensure confor-
ments for Turbine Engine Powered Airplanes
mance with the standard, each system shall be used indepen-
14 CFR part 35 Airworthiness Standards: Propellers
4
dently of the other, and values from the two systems shall not
2.3 Federal Aviation Administration (FAA) Publications:
be combined.
AC 23-8C Flight Test Guide for Certification of Part 23
Airplanes
1.6 This standard does not purport to address all of the
safety concerns, if any, associated with its use. It is the CAR 13 Aircraft Engine Airworthiness
responsibility of the user of this standard to establish appro- TSO-C77 Technical Standard Order – Gas Turbine Auxil-
priate safety, health, and environmental practices and deter- liary Power Units
5
mine the applicability of regulatory limitations prior to use. 2.4 JAA Documents:
1.7 This international standard was developed in accor- JAR-E Engines
dance with internationally recognized principles on standard- JAR-P Propellers
ization established in the Decision on Principles for the
Development of International Standards, Guides and Recom-
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.
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 June 1, 2020. Published June 2020. Originally Ave., SW, Washington, DC 20591, https://www.faa.gov.
5
approved in 2015. Last previous edition approved in 2019 as F3062/F3062M–19. Available from IHS Markit, 15 Inverness Way East, Englewood, CO 80112,
DOI: 10.1520/F3062_F3062M-20. http://www.global.ihs.com.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19
...
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 − 19 F3062/F3062M − 20
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 mustshall 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 mayare not
benecessarily exact equivalents; therefore, to ensure conformance with the standard, each system shall be used independently of
the other. Combiningother, and values from the two systems may result in non-conformance with the standard.shall not be
combined.
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 Storage and Delivery
F3066/F3066M Specification for Aircraft Powerplant Installation Hazard Mitigation
F3117/F3117M Specification for Crew Interface in Aircraft
3
2.2 Code of Federal Regulations (CFR):
14 CFR part 23 Airworthiness Standards: Normal Category Airplanes
14 CFR part 33 Airworthiness Standards: Aircraft 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 Feb. 1, 2019June 1, 2020. Published March 2019June 2020. Originally approved in 2015. Last previous edition approved in 20182019 as
F3062/F3062M–18.–19. DOI: 10.1520/F3062_F3062M–19.10.1520/F3062_F3062M-20.
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.
3
Available from U.S. Government Publishing Office, 732 N. Capitol St., NW, Washington, DC 20401, https://www.gpo.gov.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
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F3062/F3062M − 20
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2.3 Federal Aviation Administration (FAA) Publications:
AC 23-8C Flight Test Guide for Certification of Part 23 Airplanes
C
...
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