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1.1 This specification covers international standards for the flight control 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 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.
1.4 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.
F3060 Terminology for Aircraft
F3061/F3061M Specification for Systems and Equipment in Small Aircraft
F3116/F3116M Specification for Design Loads and Conditions
F3117/F3117M Specification for Crew Interface in Aircraft
F3173/F3173M Specification for Aircraft Handling Characteristics
F3180/F3180M Specification for Low-Speed Flight Characteristics of Aircraft
Other StandardsFAA-S-ACS RTCA/DO-335 Guidance for Installation of Automatic Flight Guidance and Control Systems (AFGCS) for Part 23 Airplanes Available from RTCA, Inc., 1150 18th St., NW, Suite 910, Washington, DC 20036, http://www.rtca.org.
ICS Number Code 49.020 (Aircraft and space vehicles in general)
UNSPSC Code 25201800(Aircraft master control systems)
|Link to Active (This link will always route to the current Active version of the standard.)|
ASTM F3232 / F3232M-20, Standard Specification for Flight Controls in Small Aircraft, ASTM International, West Conshohocken, PA, 2020, www.astm.orgBack to Top