ASTM F3062/F3062M-16
(Specification)Standard Specification for Installation of Powerplant Systems
Standard Specification for Installation of Powerplant Systems
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 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 and health practices and determine the applicability of regulatory limitations prior to use.
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Designation:F3062/F3062M −16
Standard Specification 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 2. Referenced Documents
2
2.1 ASTM Standards:
1.1 This specification covers minimum requirements for the
F2339 Practice for Design and Manufacture of Reciprocat-
installation and integration of powerplant system units.
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
F2840 Practice for Design and Manufacture of Electric
1.3 The applicant for a design approval must seek the
Propulsion Units for Light Sport Aircraft
individual guidance to their respective CAA body concerning
F3060 Terminology for Aircraft
the use of this standard as part of a certification plan. For
F3066/F3066M Specification for Powerplant Systems Spe-
information on which CAA regulatory bodies have accepted
cific Hazard Mitigation
this standard (in whole or in part) as a means of compliance to 3
2.2 Code of Federal Regulations (CFR):
their Small Aircraft Airworthiness regulations (Hereinafter
14 CFR part 33 Airworthiness Standards: Aircraft Engines
referred to as “the Rules”), refer to the ASTM F44 webpage
14 CFR part 35 Airworthiness Standards: Propellers
(www.ASTM.org/COMITTEE/F44.htm) which includes CAA
14CFRpart34 FuelVentingandExhaustEmissionRequire-
website links.
ments for Turbine Powered Airplanes
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
5
imperial units in brackets. The values stated in each system
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
6
2.5 EASA Documents:
1.6 This standard does not purport to address all of the
CS-22 Certification Specifications for Gliders and Powered
safety concerns, if any, associated with its use. It is the
Gliders
responsibility of the user of this standard to establish appro-
CS-E Certification Specifications for Engines
priate safety and health practices and determine the applica-
bility of regulatory limitations prior to use.
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
AvailablefromU.S.GovernmentPrintingOfficeSuperintendentofDocuments,
732 N. Capitol St., NW, Mail Stop: SDE, Washington, DC 20401, www.access-
.gpo.gov.
1 4
ThisspecificationisunderthejurisdictionofASTMCommitteeF44onGeneral Available from Federal Aviation Administration (FAA), 800 Independence
Aviation Aircraft and is the direct responsibility of Subcommittee F44.40 on Ave., SW, Washington, DC 20591, www.faa.gov.
5
Powerplant. Available from Global Engineering Documents, 15 Inverness Way, East
Current edition approved Sept. 1, 2016. Published September 2016. Originally Englewood, CO 80112-5704, global.ihs.com.
6
approved in 2015. Last previous edition approved in 2015 as F3062/F3062M – 15. Available from EASA European Aviation Safety Agency, Postfach 10 12 53.
DOI: 10.1520/F3062_F3062M-16. D-50452 Koeln, Germany, easa.europa.eu.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
---------------------- Page: 1 ----------------------
F3062/F3062M−16
CS-P Certification Specifications for Propellers 4.2.4 Each powerplant installation must be constructed and
CS-APU Certification Specifications for Auxiliary Power arranged to be accessible for necessary inspections and main-
Units tenance.
4.2.4.1 Engine cowls and nacelles must be easily removabl
...
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 − 15 F3062/F3062M − 16
Standard Specification for
1
Installation of Powerplant Systems
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 and health practices and determine the applicability of regulatory
limitations prior to use.
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
F3066/F3066M Specification for Powerplant Systems Specific Hazard Mitigation
3
2.2 Code of Federal Regulations (CFR):
14 CFR part 33 Airworthiness Standards: Aircraft Engines
14 CFR part 35 Airworthiness Standards: Propellers
14 CFR part 34 Fuel Venting and Exhaust Emission Requirements for Turbine Powered Airplanes
4
2.3 Federal Aviation Administration (FAA) Publications:
AC 23-8C Flight Test Guide for certification of part 23 airplanes
CAR 13 Aircraft Engines Airworthiness
TSO C77 Technical Standard Order – Gas Turbine Auxilliary Power Units
5
2.4 JAA Documents:
JAR-E Engines
JAR-P 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 June 1, 2015Sept. 1, 2016. Published August 2015September 2016. Originally approved in 2015. Last previous edition approved in 2015 as
F3062/F3062M – 15. DOI: 10.1520/F3062_F3062M-15.10.1520/F3062_F3062M-16.
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 Printing Office Superintendent of Documents, 732 N. Capitol St., NW, Mail Stop: SDE, Washington, DC 20401, www.access.gpo.gov.
4
Available from Federal Aviation Administration (FAA), 800 Independence Ave., SW, Washington, DC 20591, www.faa.gov.
5
Available from Global Engineering Documents, 15 Inverness Way, East Englewood, CO 80112-5704, global.ihs.com.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
---------------------- Page: 1 ----------------------
F3062/F3062M − 16
JAR-22 Gliders and Powered Gliders
6
2.5 EASA Documents:
CS-22 Certification Specifications for Gliders and Powered Gliders
CS-E Certification Specifications for Engines
CS-P Certification Specifications f
...
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