ASTM F3060-16a
(Terminology)Standard Terminology for Aircraft
Standard Terminology for Aircraft
SCOPE
1.1 This terminology contains a listing of terms, abbreviations, acronyms, and symbols related to aircraft covered by ASTM Committees F37 and F44 airworthiness design standards. It is intended to ensure the consistent use of terminology throughout all ASTM light aircraft standards.
1.2 Units—The definitions of units will be as defined in NIST SP 330 and will not be duplicated in this document. NIST SP 330 is available on the internet. 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 nonconformance with the standard.
1.3 Source References—The listed document(s) was/were the original source for the definition. However, the definition may have been edited for use in this document and the F37 and F44 standards and may not completely match the original in every respect.
1.4 A definition adapted from a particular standard within the ASTM aircraft collection of standards is not limited to use within only those standards.
1.5 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.
General Information
Relations
Standards Content (Sample)
NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.
Contact ASTM International (www.astm.org) for the latest information
Designation: F3060 − 16a
Standard Terminology for
1
Aircraft
This standard is issued under the fixed designation F3060; 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.
2
1. Scope 2.1 ASTM Standards:
F2241 SpecificationforContinuedAirworthinessSystemfor
1.1 This terminology contains a listing of terms,
Powered Parachute Aircraft
abbreviations, acronyms, and symbols related to aircraft cov-
F2242 Specification for ProductionAcceptance Testing Sys-
ered by ASTM Committees F37 and F44 airworthiness design
tem for Powered Parachute Aircraft
standards. It is intended to ensure the consistent use of
F2243 Specification for Required Product Information to be
terminology throughout all ASTM light aircraft standards.
Provided with Powered Parachute Aircraft
1.2 Units—The definitions of units will be as defined in
F2244 Specification for Design and Performance Require-
NIST SP 330 and will not be duplicated in this document.
ments for Powered Parachute Aircraft
NIST SP 330 is available on the internet. The values stated in
F2245 Specification for Design and Performance of a Light
eitherSIunitsorinch-poundunitsaretoberegardedseparately
Sport Airplane
as standard. The values stated in each system may not be exact
F2249 Specification for In-ServiceTest Methods forTempo-
equivalents;therefore,eachsystemshallbeusedindependently
rary Grounding Jumper Assemblies Used on De-
of the other. Combining values from the two systems may
Energized Electric Power Lines and Equipment
result in nonconformance with the standard.
F2279 Practice for QualityAssurance in the Manufacture of
3
Fixed Wing Light Sport Aircraft (Withdrawn 2014)
1.3 Source References—The listed document(s) was/were
the original source for the definition. However, the definition F2295 Practice for Continued Operational Safety Monitor-
ing of a Light Sport Aircraft
may have been edited for use in this document and the F37 and
F44 standards and may not completely match the original in F2317/F2317M Specification for Design of Weight-Shift-
Control Aircraft
every respect.
F2352 Specification for Design and Performance of Light
1.4 A definition adapted from a particular standard within
Sport Gyroplane Aircraft
theASTM aircraft collection of standards is not limited to use
F2354 SpecificationforContinuedAirworthinessSystemfor
within only those standards.
Lighter-Than-Air Light Sport Aircraft
1.5 This standard does not purport to address all of the
F2355 Specification for Design and Performance Require-
safety concerns, if any, associated with its use. It is the
ments for Lighter-Than-Air Light Sport Aircraft
responsibility of the user of this standard to establish appro-
F2356 Specification for ProductionAcceptance Testing Sys-
priate safety, health, and environmental practices and deter-
tem for Lighter-Than-Air Light Sport Aircraft
mine the applicability of regulatory limitations prior to use.
F2411 Specification for Design and Performance of an
1.6 This international standard was developed in accor- 3
Airborne Sense-and-Avoid System (Withdrawn 2014)
dance with internationally recognized principles on standard-
F2415 Practice for Continued Airworthiness System for
ization established in the Decision on Principles for the
Light Sport Gyroplane Aircraft
Development of International Standards, Guides and Recom-
F2425 SpecificationforContinuedAirworthinessSystemfor
mendations issued by the World Trade Organization Technical
Weight-Shift-Control Aircraft
Barriers to Trade (TBT) Committee.
F2426 Guide onWing Interface Documentation for Powered
Parachute Aircraft
2. Referenced Documents
F2427 Specification for Required Product Information to be
NOTE 1—All terms will reference the source of the definition. Any
Provided with Lighter-Than-Air Light Sport Aircraft
terms not referencing their source will be considered for deletion.
1 2
ThisterminologyisunderthejurisdictionofASTMCommitteeF44onGeneral For referenced ASTM standards, visit the ASTM website, www.astm.org, or
Aviation Aircraft and is the direct responsibility of Subcommittee F44.91 on contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
Terminology. Standards volume information, refer to the standard’s Document Summary page on
Current edition approved Nov. 1, 2016. Published November 2016. Originally the ASTM website.
3
approved in 2014. Last previous edition approved in 2016 as F3060 – 16. DOI: The last approved version of this historical standard is referenced on
10.1520/F3060-16A. www.astm.org.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United Stat
...
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: F3060 − 16 F3060 − 16a
Standard Terminology for
1
Aircraft
This standard is issued under the fixed designation F3060; 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 terminology contains a listing of terms, abbreviations, acronyms, and symbols related to aircraft covered by ASTM
Committees F37 and F44 airworthiness design standards. It is intended to ensure the consistent use of terminology throughout all
ASTM light aircraft standards.
1.2 Units—The definitions of units will be as defined in NIST SP 330 and will not be duplicated in this document. NIST SP
330 is available on the internet. 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 nonconformance with the standard.
1.3 Source References—The listed document(s) was/were the original source for the definition. However, the definition may
have been edited for use in this document and the F37 and F44 standards and may not completely match the original in every
respect.
1.4 A definition adapted from a particular standard within the ASTM aircraft collection of standards is not limited to use within
only those standards.
1.5 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.
2. Referenced Documents
NOTE 1—All terms will reference the source of the definition. Any terms not referencing their source will be considered for deletion.
2
2.1 ASTM Standards:
F2241 Specification for Continued Airworthiness System for Powered Parachute Aircraft
F2242 Specification for Production Acceptance Testing System for Powered Parachute Aircraft
F2243 Specification for Required Product Information to be Provided with Powered Parachute Aircraft
F2244 Specification for Design and Performance Requirements for Powered Parachute Aircraft
F2245 Specification for Design and Performance of a Light Sport Airplane
F2249 Specification for In-Service Test Methods for Temporary Grounding Jumper Assemblies Used on De-Energized Electric
Power Lines and Equipment
3
F2279 Practice for Quality Assurance in the Manufacture of Fixed Wing Light Sport Aircraft (Withdrawn 2014)
F2295 Practice for Continued Operational Safety Monitoring of a Light Sport Aircraft
F2317/F2317M Specification for Design of Weight-Shift-Control Aircraft
F2352 Specification for Design and Performance of Light Sport Gyroplane Aircraft
F2354 Specification for Continued Airworthiness System for Lighter-Than-Air Light Sport Aircraft
F2355 Specification for Design and Performance Requirements for Lighter-Than-Air Light Sport Aircraft
F2356 Specification for Production Acceptance Testing System for Lighter-Than-Air Light Sport Aircraft
3
F2411 Specification for Design and Performance of an Airborne Sense-and-Avoid System (Withdrawn 2014)
F2415 Practice for Continued Airworthiness System for Light Sport Gyroplane Aircraft
F2425 Specification for Continued Airworthiness System for Weight-Shift-Control Aircraft
1
This terminology is under the jurisdiction of ASTM Committee F44 on General Aviation Aircraft and is the direct responsibility of Subcommittee F44.91 on Terminology.
Current edition approved April 1, 2016Nov. 1, 2016. Published April 2016November 2016. Originally approved in 2014. Last previous edition approved in 20152016 as
F3060 – 15b.F3060 – 16. DOI: 10.1520/F3060-16.10.1520/F3060-16A.
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.
3
The last approved version of this historical standard is referenced on www.astm.org.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
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F3060 − 16a
F2426 Guide on Wing Interface Documentation for Powered Parachute Aircraft
F242
...
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