ASTM International - ASTM F3231/F3231M-17

Standard Specification for Electrical Systems in Small Aircraft

historical
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Organization: ASTM International
Publication Date: 15 February 2017
Status: historical
Page Count: 6
ICS Code (Aircraft and space vehicles in general): 49.020
scope:

1.1 This specification covers international standards for the electrical systems aspects of airworthiness and design for "small" aircraft.

1.2 The applicant for a design approval must seek the individual guidance of their respective CAA body concerning the use of this specification as part of a certification plan. For information on which CAA regulatory bodies have accepted this specification (in whole or in part) as a means of compliance to their Small Aircraft Airworthiness regulations (hereinafter referred to as "the Rules"), refer to ASTM F44 webpage (www.ASTM.org/COMMITTEE/F44.htm) which includes CAA website links.

1.3 The values stated in either SI units or inch-pound units are to be regarded separately as standard. 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 and health practices and determine the applicability of regulatory limitations prior to use.

Document History

June 1, 2019
Standard Specification for Electrical Systems for Aircraft with Combustion Engine Electrical Power Generation
1.1 This specification covers electrical systems, electrical equipment, and electrical power distribution aspects of airworthiness and design for aeroplanes with combustion engine generation of...
ASTM F3231/F3231M-17
February 15, 2017
Standard Specification for Electrical Systems in Small Aircraft
1.1 This specification covers international standards for the electrical systems aspects of airworthiness and design for “small” aircraft. 1.2 The applicant for a design approval must seek the...
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