ASTM F3061/F3061M-19
(Specification)Standard Specification for Systems and Equipment in Small Aircraft
Standard Specification for Systems and Equipment in Small Aircraft
SCOPE
1.1 This specification covers international standards for the systems and equipment 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 standard as part of a certification plan. For information on which CAA regulatory bodies have accepted this standard (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 are not necessarily exact equivalents; therefore, to ensure conformance with the standard, each system shall be used independently of the other, and values from the two systems shall not be combined.
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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Designation:F3061/F3061M −19
Standard Specification for
1
Systems and Equipment in Small Aircraft
ThisstandardisissuedunderthefixeddesignationF3061/F3061M;thenumberimmediatelyfollowingthedesignationindicatestheyear
of original adoption or, in the case of revision, the year of last revision.Anumber 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 specification covers international standards for the
2
systems and equipment aspects of airworthiness and design for
2.2 ASTM Standards:
“small” aircraft.
F3060Terminology for Aircraft
F3082/F3082MSpecification for Weights and Centers of
1.2 The applicant for a design approval must seek the
Gravity of Aircraft
individual guidance of their respective CAA body concerning
F3083/F3083M Specification for Emergency Conditions,
the use of this standard as part of a certification plan. For
Occupant Safety and Accommodations
information on which CAA regulatory bodies have accepted
F3116/F3116MSpecification for Design Loads and Condi-
this standard (in whole or in part) as a means of compliance to
tions
their Small Aircraft Airworthiness regulations (hereinafter
F3117/F3117MSpecification for Crew Interface in Aircraft
referred to as “the Rules”), refer to ASTM F44 webpage
F3179/F3179MSpecification for Performance of Aircraft
(www.astm.org/COMMITTEE/F44.htm) which includes CAA
F3227/F3227MSpecification for Environmental Systems in
website links.
Small Aircraft
1.3 The values stated in either SI units or inch-pound units
F3228Specification for Flight Data and Voice Recording in
are to be regarded separately as standard. The values stated in
Small Aircraft
each system are not necessarily exact equivalents; therefore, to
F3230 Practice for Safety Assessment of Systems and
ensure conformance with the standard, each system shall be
Equipment in Small Aircraft
used independently of the other, and values from the two
F3231/F3231MSpecification for Electrical Systems forAir-
systems shall not be combined.
craft with Combustion Engine Electrical Power Genera-
1.4 This standard does not purport to address all of the
tion
safety concerns, if any, associated with its use. It is the
F3232/F3232MSpecification for Flight Controls in Small
responsibility of the user of this standard to establish appro-
Aircraft
priate safety, health, and environmental practices and deter-
F3233/F3233MSpecification for Instrumentation in Small
mine the applicability of regulatory limitations prior to use.
Aircraft
1.5 This international standard was developed in accor-
F3234/F3234MSpecification for Exterior Lighting in Small
dance with internationally recognized principles on standard-
Aircraft
ization established in the Decision on Principles for the
F3236 Specification for High Intensity Radiated Field
Development of International Standards, Guides and Recom-
(HIRF) Protection in Small Aircraft
mendations issued by the World Trade Organization Technical
F3309/F3309MPracticeforSimplifiedSafetyAssessmentof
Barriers to Trade (TBT) Committee.
Systems and Equipment in Small Aircraft
F3316/F3316MSpecification for Electrical Systems forAir-
2. Referenced Documents
craft with Electric or Hybrid-Electric Propulsion
2.1 Following is a list of external standards referenced
3
2.3 SAE Standard:
throughout this specification; the earliest revision acceptable
SAEARP4754, RevAGuidelines for Development of Civil
for use is indicated. In all cases later document revisions are
Aircraft Systems
acceptable if shown to be equivalent to the listed revision, or if
1 2
ThisspecificationisunderthejurisdictionofASTMCommitteeF44onGeneral For referenced ASTM standards, visit the ASTM website, www.astm.org, or
Aviation Aircraft and is the direct responsibility of Subcommittee F44.50 on contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
Systems and Equipment. Standards volume information, refer to the standard’s Document Summary page on
Current edition approved June 1, 2019. Published June 2019. Originally the ASTM website.
3
approved in 2015. Last previous edition approved in 2017 as F3061/F3061M–17. AvailablefromSAEInternational(SAE),400CommonwealthDr.,Warrendale,
DOI: 10.1520/F3061_F3061M–19. PA 15096, http://www.sae.org.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
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F3061/F3061M−19
2.4 Other Standards: (1)An “S” indicates a single-engine aircraft.
FAA-S-8081-14B, Change 5Private Pilot Practical Test (2)An “M” indicates a multiengine aircraft.
4
Standards for Airplane 3.2.1.3 Discussion—The third character in theAircraftTy
...
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: F3061/F3061M − 17 F3061/F3061M − 19
Standard Specification for
1
Systems and Equipment in Small Aircraft
This standard is issued under the fixed designation F3061/F3061M; 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 specification covers international standards for the systems and equipment 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 standard as part of a certification plan. For information on which CAA regulatory bodies have accepted this standard (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)(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 mayare not benecessarily exact equivalents; therefore, to ensure conformance with the standard, each system shall be used
independently of the other. Combiningother, and values from the two systems may result in non-conformance with the
standard.shall not be combined.
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 safety, health, and healthenvironmental 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 specification; 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
F3082/F3082M Specification for Weights and Centers of Gravity of Aircraft
F3083/F3083M Specification for Emergency Conditions, Occupant Safety and Accommodations
F3116/F3116M Specification for Design Loads and Conditions
F3117F3117/F3117M Specification for Crew Interface in Aircraft
F3179/F3179M Specification for Performance of Aircraft
F3227/F3227M Specification for Environmental Systems in Small Aircraft
F3228 Specification for Flight Data and Voice Recording in Small Aircraft
F3230 Practice for Safety AssessmentsAssessment of Systems and Equipment in Small Aircraft
F3231/F3231M Specification for Electrical Systems in Small Aircraftfor Aircraft with Combustion Engine Electrical Power
Generation
F3232/F3232M Specification for Flight Controls in Small Aircraft
F3233/F3233M Specification for Instrumentation in Small Aircraft
1
This specification 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 Feb. 15, 2017June 1, 2019. Published March 2017June 2019. Originally approved in 2015. Last previous edition approved in 20162017 as
F3061/F3061M – 16b.F3061/F3061M–17. DOI: 10.1520/F3061_F3061M-17.10.1520/F3061_F3061M–19.
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’sstandard’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
1
---------------------- Page: 1 ----------------------
F3061/F3061M − 19
F3234/F3234M Specification for Exterior Lighting in Small Aircraft
F3236 Specification for High Intensity Radiated Field (HIRF) Protection in Small Aircraft
F3309/F3309M Practice for Simplified Safety Assessment of Systems and Equip
...
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