ASTM F3062/F3062M-15

Standard Specification for Installation of Powerplant Systems

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 (http://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 and health practices and determine the applicability of regulatory limitations prior to use.

General Information

• Status: Historical
• Publication Date: 31-May-2015
• ICS: 49.050 - Aerospace engines and propulsion systems
• Technical Committee: F44 - General Aviation Aircraft
• Drafting Committee: F44.40 - Powerplant

Relations

• Replaced By: ASTM F3062/F3062M-16 - Standard Specification for Installation of Powerplant Systems
• Effective Date: 01-Sep-2016
• Referred By: ASTM F3239-22a - Standard Specification for Aircraft Electric Propulsion Systems
• Effective Date: 01-Jun-2015
• Referred By: ASTM F3060-20 - Standard Terminology for Aircraft
• Effective Date: 01-Jun-2015
• Referred By: ASTM F3066/F3066M-23 - Standard Specification for Aircraft Powerplant Installation Hazard Mitigation
• Effective Date: 01-Jun-2015
• Referred By: ASTM F3563-22 - Standard Specification for Design and Construction of Large Fixed Wing Unmanned Aircraft Systems
• Effective Date: 01-Jun-2015
• Referred By: ASTM F3064/F3064M-21 - Standard Specification for Aircraft Powerplant Control, Operation, and Indication
• Effective Date: 01-Jun-2015
• Referred By: ASTM F3432-20a - Standard Practice for Powerplant Instruments
• Effective Date: 01-Jun-2015
• Referred By: ASTM F3264-23 - Standard Specification for Normal Category Aeroplanes Certification
• Effective Date: 01-Jun-2015

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:F3062/F3062M −15
StandardSpecification for
1
Installation of Powerplant Systems
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 F2339 Practice for Design and Manufacture of Reciprocat-
ing Spark Ignition Engines for Light Sport Aircraft
1.1 This specification covers minimum requirements for the
F2506 Specification for Design and Testing of Light Sport
installation and integration of powerplant system units.
Aircraft Propellers
1.2 This specification is applicable to small aeroplanes as
F2538 Practice for Design and Manufacture of Reciprocat-
defined in the F44 terminology standard. Use of the term
ing Compression Ignition Engines for Light SportAircraft
airplane is used throughout this specification and will mean
F2840 Practice for Design and Manufacture of Electric
“small airplane.”
Propulsion Units for Light Sport Aircraft
1.3 The applicant for a design approval must seek the
F3060 Terminology for Aircraft
individual guidance to their respective CAA body concerning F3066/F3066M Specification for Powerplant Systems Spe-
the use of this standard as part of a certification plan. For
cific Hazard Mitigation
information on which CAA regulatory bodies have accepted 3
2.2 Code of Federal Regulations (CFR):
this standard (in whole or in part) as a means of compliance to
14 CFR part 33 Airworthiness Standards: Aircraft Engines
their Small Aircraft Airworthiness regulations (Hereinafter
14 CFR part 35 Airworthiness Standards: Propellers
referred to as “the Rules”), refer to the ASTM F44 webpage
14CFRpart34 FuelVentingandExhaustEmissionRequire-
(www.ASTM.org/COMITTEE/F44.htm) which includes CAA
ments for Turbine Powered Airplanes
website links.
4
2.3 Federal Aviation Administration (FAA) Publications:
1.4 References within this standard normally refer to docu-
AC 23-8C Flight Test Guide for certification of part 23
ments in United States legal system. Appendix X1 cross
airplanes
references documents in the legal system of other countries of
CAR 13 Aircraft Engines Airworthiness
corresponding content.
TSO C77 Technical Standard Order – Gas Turbine Auxil-
1.5 Units—The values stated are SI units followed by
liary Power Units
imperial units in brackets. The values stated in each system
5
2.4 JAA Documents:
may not be exact equivalents; therefore, each system shall be
JAR-E Engines
used independently of the other. Combining values from the
JAR-P Propellers
two systems may result in non-conformance with the standard.
JAR-22 Gliders and Powered Gliders
1.6 This standard does not purport to address all of the
6
2.5 EASA Documents:
safety concerns, if any, associated with its use. It is the
CS-22 Certification Specifications for Gliders and Powered
responsibility of the user of this standard to establish appro-
Gliders
priate safety and health practices and determine the applica-
CS-E Certification Specifications for Engines
bility of regulatory limitations prior to use.
CS-P Certification Specifications for Propellers
CS-APU Certification Specifications for Auxiliary Power
2. Referenced Documents
Units
2
2.1 ASTM Standards:
1 3
ThisspecificationisunderthejurisdictionofASTMCommitteeF44onGeneral AvailablefromU.S.GovernmentPrintingOfficeSuperintendentofDocuments,
Aviation Aircraft and is the direct responsibility of Subcommittee F44.40 on 732 N. Capitol St., NW, Mail Stop: SDE, Washington, DC 20401, www.access-
Powerplant. .gpo.gov.
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Current edition approved June 1, 2015. Published August 2015. DOI: 10.1520/ Available from Federal Aviation Administration (FAA), 800 Independence
F3062_F3062M-15. Ave., SW, Washington, DC 20591, www.faa.gov.
2 5
For referenced ASTM standards, visit the ASTM website, www.astm.org, or Available from Global Engineering Documents, 15 Inverness Way, East
contact ASTM Customer Service at [e-mail]. For Annual Book of ASTM Englewood, CO 80112-5704, global.ihs.com.
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Standards volume information, refer to the standard’s Document Summary page on Available from EASA European Aviation Safety Agency, Postfach 10 12 53.
the ASTM website. D-50452 Koeln, Germany, easa.europa.eu.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
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F3062/F3062M−15
3. Terminology 5. Air Induction System
3.1 The following are a selection of relevant terms. See
5.1 General:
Terminology F3060 for more definitions and abbreviations.
5.1.1 The air induction system for each engine and auxiliary
power unit and their accessories must supply the air r
...