ASTM F3229/F3229M-23
(Practice)Standard Practice for Static Pressure System Tests in Small Aircraft
Standard Practice for Static Pressure System Tests in Small Aircraft
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, 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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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.
Designation: F3229/F3229M − 23
Standard Practice for
1
Static Pressure System Tests in Small Aircraft
This standard is issued under the fixed designation F3229/F3229M; the number immediately following the designation indicates the year
of original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval.
A superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
1. Scope otherwise formally accepted by the governing civil aviation
authority; earlier revisions are not acceptable.
1.1 This practice covers internationally accepted methods
2
for the conducting static pressure system tests for “small” 2.2 ASTM Standards:
aircraft. F3060 Terminology for Aircraft
F3061/F3061M Specification for Systems and Equipment in
1.2 The applicant for a design approval must seek the
Aircraft
individual guidance of their respective CAA body concerning
F3230 Practice for Safety Assessment of Systems and
the use of this practice as part of a certification plan. For
Equipment in Small Aircraft
information on which CAA regulatory bodies have accepted
F3233/F3233M Specification for Flight and Navigation In-
this practice (in whole or in part) as a means of compliance to
strumentation in Aircraft
their Small Aircraft Airworthiness regulations (hereinafter
referred to as “the Rules”), refer to ASTM F44 webpage
3. Terminology
(www.ASTM.org/COMMITTEE/F44.htm) which includes
CAA website links. 3.1 Terminology specific to this practice is provided below.
For general terminology, refer to Terminology F3060.
1.3 The values stated in either SI units or inch-pound units
are to be regarded separately as standard. The values stated in 3.2 Definitions of Terms Specific to This Standard:
each system may not be exact equivalents; therefore, each 3.2.1 aircraft type code, n—an Aircraft Type Code (ATC) is
system shall be used independently of the other. Combining defined by considering both the technical considerations re-
values from the two systems may result in non-conformance garding the design of the aircraft and the airworthiness level
with the standard. established based upon risk-based criteria; the method of
defining an ATC applicable to this practice is defined in
1.4 This standard does not purport to address all of the
Practice F3230.
safety concerns, if any, associated with its use. It is the
responsibility of the user of this standard to establish appro-
4. Static Pressure System Tests
priate safety, health, and environmental practices and deter-
NOTE 1—Table 1 provides correlation between various Aircraft Type
mine the applicability of regulatory limitations prior to use.
Codes and the individual requirements contained within this section; refer
1.5 This international standard was developed in accor-
to 3.2.1. For each subsection, an indicator can be found under each ATC
dance with internationally recognized principles on standard-
character field; three indicators are used:
ization established in the Decision on Principles for the An empty cell ( ) in all applicable ATC character field columns
indicates that an aircraft must meet the requirements of that subsection.
Development of International Standards, Guides and Recom-
A white circle (○) in multiple columns indicates that the requirements
mendations issued by the World Trade Organization Technical
of that subsection are not applicable to an aircraft only if all such ATC
Barriers to Trade (TBT) Committee.
character fields are applicable.
A mark-out (×) in any of the applicable ATC character field columns
2. Referenced Documents
indicates that the requirements of that subsection are not applicable to an
aircraft if that ATC character field is applicable.
2.1 Following is a list of external standards referenced
Example—An aircraft with an ATC of 1SRLLDLN is being considered.
throughout this practice; the earliest revision acceptable for use
Since all applicable columns are empty for 4.2.1, that subsection is
is indicated. In all cases later document revisions are accept- applicable to the aircraft. 4.1.1 would not be applicable, since it contains
an × in the “D” meteorological condition column.
able if shown to be equivalent to the listed revision, or if
4.1 Proof Test for Unpressurized Aircraft:
1
This practice is under the jurisdiction of ASTM Committee F44 on General
Aviation Aircraft and is the direct responsibility of Subcommittee F44.50 on
2
Systems and Equipment. For referenced ASTM standards, visit the ASTM website, www.astm.org, or
Current edition approved Nov. 1, 2023. Published December 2023. Originally contact ASTM Customer Service at service@astm.org. For Annual Book
...
This document is not an ASTM standard and is intended only to provide the user of an ASTM standard an indication of what changes have been made to the previous version. Because
it may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current version
of the standard as published by ASTM is to be considered the official document.
Designation: F3229/F3229M − 17 (Reapproved 2023) F3229/F3229M − 23
Standard Practice for
1
Static Pressure System Tests in Small Aircraft
This standard is issued under the fixed designation F3229/F3229M; the number immediately following the designation indicates the year
of original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval.
A superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
1. 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, 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
2.1 Following is a list of external standards referenced throughout this practice; the earliest revision acceptable for use is indicated.
In all cases later document revisions are acceptable if shown to be equivalent to the listed revision, or if otherwise formally
accepted by the governing civil aviation authority; earlier revisions are not acceptable.
2
2.2 ASTM Standards:
F3060 Terminology for Aircraft
F3061/F3061M Specification for Systems and Equipment in Aircraft
F3230 Practice for Safety Assessment of Systems and Equipment in Small Aircraft
F3233/F3233M Specification for Flight and Navigation Instrumentation in Aircraft
1
This practice is under the jurisdiction of ASTM Committee F44 on General Aviation Aircraft and is the direct responsibility of Subcommittee F44.50 on Systems and
Equipment.
Current edition approved May 1, 2023Nov. 1, 2023. Published May 2023December 2023. Originally approved in 2017. Last previous edition approved in 20172023 as
F3229/F3229M – 17.F3229/F3229M – 17 (2023). DOI: 10.1520/F3229_F3229M-17R23.10.1520/F3229_F3229M-23.
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM Standards
volume information, refer to the standard’s Document Summary page on the ASTM website.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
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F3229/F3229M − 23
3. Terminology
3.1 Terminology specific to this practice is provided below. For general terminology, refer to Terminology F3060.
3.2 Definitions of Terms Specific to This Standard:
3.2.1 aircraft type code, n—an Aircraft Type Code (ATC) is defined by considering both the technical considerations regarding
the design of the aircraft and the airworthiness level established based upon risk-based criteria; the method of defining an ATC
applicable to this practice is defined in SpecificationPractice F3061/F3061MF3230.
4. Static Pressure System Tests
NOTE 1—Table 1 provides correlation between various Aircraft Type Codes and the individual requirements contained within this section; refer to 3.2.1.
For each subsection, an indicator can be found under each ATC character field; three indicators are used:
An empty cell ( ) in all applicable ATC character field columns indicates that an aircraft must meet the requirements of that subsection.
A white circle (○) in mul
...
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