ASTM F3229/F3229M-17 PDF

Scope: 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 (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.

ASTM F3229/F3229M-17 Referenced Document

ASTM F3060 Standard Terminology for Aircraft*， 2020-01-01 Update
ASTM F3061/F3061M Standard Specification for Systems and Equipment in Aircraft*， 2023-10-01 Update

2023 ASTM F3229/F3229M-23 Standard Practice for Static Pressure System Tests in Small Aircraft
2023 ASTM F3229/F3229M-17(2023) Standard Practice for Static Pressure System Tests in Small Aircraft
2017 ASTM F3229/F3229M-17 Standard Practice for Static Pressure System Tests in Small Aircraft