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1.1 This specification covers minimum requirements for the design and integration of Fuel/Energy Storage and Delivery system installations for aeroplanes.
1.2 This specification is applicable to aeroplanes as defined in the F44 terminology standard.
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 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.
1.4 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.
1.5 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 (purchase separately) The documents listed below are referenced within the subject standard but are not provided as part of the standard.
F3060 Terminology for Aircraft
F3116/F3116M Specification for Design Loads and Conditions
ICS Number Code 49.050 (Aerospace engines and propulsion systems)
UNSPSC Code 25202400(Aircraft fuel tanks and systems)
|Link to Active (This link will always route to the current Active version of the standard.)|
ASTM F3063 / F3063M-16a, Standard Specification for Design and Integration of Fuel/Energy Storage and Delivery System Installations for Aeroplanes, ASTM International, West Conshohocken, PA, 2016, www.astm.orgBack to Top