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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. 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) PublicationsAC 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
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 DocumentsJAR-22 Sailplanes and Powered Sailplanes JAR-E Engines JAR-P
ICS Number Code 49.050 (Aerospace engines and propulsion systems)
UNSPSC Code 25202000(Aircraft power systems)
|Link to Active (This link will always route to the current Active version of the standard.)|
ASTM F3062 / F3062M-20, Standard Specification for Aircraft Powerplant Installation, ASTM International, West Conshohocken, PA, 2020, www.astm.orgBack to Top