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ASTM F3232/F3232M-17

Historical Revision

Standard Specification for Flight Controls in Small Aircraft

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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 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.


SDO ASTM: ASTM International
Document Number F3232
Publication Date Feb. 15, 2017
Language en - English
Page Count 6
Revision Level 17
Supercedes
Committee F44.50
Publish Date Document Id Type View
Nov. 15, 2024 F3232_F3232M-24 Revision
Oct. 1, 2023 F3232_F3232M-23A Revision
May 1, 2023 F3232_F3232M-23 Revision
Nov. 1, 2020 F3232_F3232M-20 Revision
Nov. 1, 2019 F3232_F3232M-19AE01 Revision
Nov. 1, 2019 F3232_F3232M-19A Revision
May 1, 2019 F3232_F3232M-19 Revision
Feb. 15, 2017 F3232_F3232M-17 Revision