Standard Active Last Updated: May 21, 2024 Track Document
ASTM F3229/F3229M-23a

Standard Practice for Static Pressure System Tests in Small Aircraft

Standard Practice for Static Pressure System Tests in Small Aircraft F3229_F3229M-23A ASTM|F3229_F3229M-23A|en-US Standard Practice for Static Pressure System Tests in Small Aircraft Standard new BOS Vol. 15.09 Committee F44 2024-05-21 00:00:00
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1.1 This practice covers internationally accepted methods for the conducting static pressure system tests 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 practice as part of a certification plan. For information on which CAA regulatory bodies have accepted this practice (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 ( 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, 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.

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Book of Standards Volume: 15.09
Developed by Subcommittee: F44.50
Pages: 2
DOI: 10.1520/F3229_F3229M-23A
ICS Code: 49.020