1、Designation:F3062/F3062M15Standard Specification forInstallation of Powerplant Systems1This standard is issued under the fixed designation F3062/F3062M;the number immediately following the designation indicates the yearof original adoption or,in the case of revision,the year of last revision.A numbe
2、r in parentheses indicates the year of last reapproval.A superscript epsilon()indicates an editorial change since the last revision or reapproval.1.Scope1.1 This specification covers minimum requirements for theinstallation and integration of powerplant system units.1.2 This specification is applica
3、ble to small aeroplanes asdefined in the F44 terminology standard.Use of the termairplane is used throughout this specification and will mean“small airplane.”1.3 The applicant for a design approval must seek theindividual guidance to their respective CAA body concerningthe use of this standard as pa
4、rt of a certification plan.Forinformation on which CAA regulatory bodies have acceptedthis standard(in whole or in part)as a means of compliance totheir Small Aircraft Airworthiness regulations(Hereinafterreferred to as“the Rules”),refer to the ASTM F44 webpage(www.ASTM.org/COMITTEE/F44.htm)which in
5、cludes CAAwebsite links.1.4 References within this standard normally refer to docu-ments in United States legal system.Appendix X1 crossreferences documents in the legal system of other countries ofcorresponding content.1.5 UnitsThe values stated are SI units followed byimperial units in brackets.Th
6、e values stated in each systemmay not be exact equivalents;therefore,each system shall beused independently of the other.Combining values from thetwo systems may result in non-conformance with the standard.1.6 This standard does not purport to address all of thesafety concerns,if any,associated with
7、 its use.It is theresponsibility of the user of this standard to establish appro-priate safety and health practices and determine the applica-bility of regulatory limitations prior to use.2.Referenced Documents2.1 ASTM Standards:2F2339 Practice for Design and Manufacture of Reciprocat-ing Spark Igni
8、tion Engines for Light Sport AircraftF2506 Specification for Design and Testing of Light SportAircraft PropellersF2538 Practice for Design and Manufacture of Reciprocat-ing Compression Ignition Engines for Light SportAircraftF2840 Practice for Design and Manufacture of ElectricPropulsion Units for L
9、ight Sport AircraftF3060 Terminology for AircraftF3066/F3066M Specification for Powerplant Systems Spe-cific Hazard Mitigation2.2 Code of Federal Regulations(CFR):314 CFR part 33 Airworthiness Standards:Aircraft Engines14 CFR part 35 Airworthiness Standards:Propellers14 CFR part 34 Fuel Venting and
10、Exhaust Emission Require-ments for Turbine Powered Airplanes2.3 Federal Aviation Administration(FAA)Publications:4AC 23-8C Flight Test Guide for certification of part 23airplanesCAR 13 Aircraft Engines AirworthinessTSO C77 Technical Standard Order Gas Turbine Auxil-liary Power Units2.4 JAA Documents
11、:5JAR-E EnginesJAR-P PropellersJAR-22 Gliders and Powered Gliders2.5 EASA Documents:6CS-22 Certification Specifications for Gliders and PoweredGlidersCS-E Certification Specifications for EnginesCS-P Certification Specifications for PropellersCS-APU Certification Specifications for Auxiliary PowerUn
12、its1This specification is under the jurisdiction ofASTM Committee F44 on GeneralAviation Aircraft and is the direct responsibility of Subcommittee F44.40 onPowerplant.Current edition approved June 1,2015.Published August 2015.DOI:10.1520/F3062_F3062M-15.2For referenced ASTM standards,visit the ASTM
13、website,www.astm.org,orcontact ASTM Customer Service at serviceastm.org.For Annual Book of ASTMStandards volume information,refer to the standards Document Summary page onthe ASTM website.3Available from U.S.Government Printing Office Superintendent of Documents,732 N.Capitol St.,NW,Mail Stop:SDE,Wa
14、shington,DC 20401,www.access-.gpo.gov.4Available from Federal Aviation Administration(FAA),800 IndependenceAve.,SW,Washington,DC 20591,www.faa.gov.5Available from Global Engineering Documents,15 Inverness Way,EastEnglewood,CO 80112-5704,.6Available from EASA European Aviation Safety Agency,Postfach
15、10 12 53.D-50452 Koeln,Germany,easa.europa.eu.Copyright ASTM International,100 Barr Harbor Drive,PO Box C700,West Conshohocken,PA 19428-2959.United States1 3.Terminology3.1 The following are a selection of relevant terms.SeeTerminology F3060 for more definitions and abbreviations.3.2 Definitions:3.2
16、.1 powerplant,nall units and components necessaryfor propelling the aircraft or for providing auxiliary power forthe aircraft(APU).3.2.2 powerplant installation,nthe installation of an en-gine or auxiliary power unit including all components that arenecessary for propulsion or for providing auxiliary power(APU)and affects the safety of the major propulsive units.3.2.3 reciprocating engine,nengines with the characteris-tics of a non-continuous flow piston engines.3.2.3.1 DiscussionFor the purpose