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1.1 This specification covers minimum requirements for the control, indication, and operational characteristics of propulsion systems. It was developed based on propulsion system installed on aeroplanes, but may be applicable to other applications as well.
1.2 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 Aeroplane Airworthiness regulations (Hereinafter referred to as “the Rules”), refer to ASTM F44 webpage (www.ASTM.org/COMITTEE/F44.htm) which includes CAA website links.
1.3 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.
1.4 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.
1.5 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.
Other StandardsUS 14 CFR (Code of Federal Regulations) Part 23 Amendment 62
F3060 Terminology for Aircraft
F3062/F3062M Specification for Installation of Powerplant Systems
F3063/F3063M Specification for Aircraft Fuel and Energy Storage and Delivery
F3066/F3066M Specification for Aircraft Powerplant Installation Hazard Mitigation
F3116/F3116M Specification for Design Loads and Conditions
F3117 Specification for Crew Interface in Aircraft
ICS Number Code 49.140 (Space systems and operations)
UNSPSC Code 26100000(Power sources)
|Link to Active (This link will always route to the current Active version of the standard.)|
ASTM F3064 / F3064M-18a, Standard Specification for Aircraft Powerplant Control, Operation, and Indication, ASTM International, West Conshohocken, PA, 2018, www.astm.orgBack to Top