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    ASTM F3062 / F3062M - 20

    Standard Specification for Aircraft Powerplant Installation

    Active Standard ASTM F3062 / F3062M | Developed by Subcommittee: F44.40

    Book of Standards Volume: 15.09


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    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 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.


    2. Referenced Documents (purchase separately) The documents listed below are referenced within the subject standard but are not provided as part of the standard.

    Federal Aviation Administration (FAA) Publications

    AC 23-8C Flight Test Guide for Certification of Part 23 Airplanes

    CAR 13

    TSO-C77

    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

    14 CFR part 35 Airworthiness Standards: Propellers

    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

    JAA Documents

    JAR-22 Sailplanes and Powered Sailplanes

    JAR-E Engines

    JAR-P


    ICS Code

    ICS Number Code 49.050 (Aerospace engines and propulsion systems)

    UNSPSC Code

    UNSPSC Code 25202000(Aircraft power systems)


    Referencing This Standard
    Link Here
    Link to Active (This link will always route to the current Active version of the standard.)

    DOI: 10.1520/F3062_F3062M-20

    Citation Format

    ASTM F3062 / F3062M-20, Standard Specification for Aircraft Powerplant Installation, ASTM International, West Conshohocken, PA, 2020, www.astm.org

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