ASTM F3061/F3061M-19a
(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 −19a
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 for use is indicated. In all cases later document revisions are
acceptable if shown to be equivalent to the listed revision, or if
1.1 This specification covers international standards for the
otherwise formally accepted by the governing civil aviation
systems and equipment aspects of airworthiness and design for
authority; earlier revisions are not acceptable.
“small” aircraft.
2
2.2 ASTM Standards:
1.2 The applicant for a design approval must seek the
F3060Terminology for Aircraft
individual guidance of their respective CAA body concerning
F3082/F3082MSpecification for Weights and Centers of
the use of this standard as part of a certification plan. For
Gravity of Aircraft
information on which CAA regulatory bodies have accepted
F3083/F3083M Specification for Emergency Conditions,
this standard (in whole or in part) as a means of compliance to
Occupant Safety and Accommodations
their Small Aircraft Airworthiness regulations (hereinafter
F3116/F3116MSpecification for Design Loads and Condi-
referred to as “the Rules”), refer to ASTM F44 webpage
tions
(www.astm.org/COMMITTEE/F44.htm) which includes CAA
F3117/F3117MSpecification for Crew Interface in Aircraft
website links.
F3179/F3179MSpecification for Performance of Aircraft
1.3 The values stated in either SI units or inch-pound units
F3227/F3227MSpecification for Environmental Systems in
are to be regarded separately as standard. The values stated in
Small Aircraft
each system are not necessarily exact equivalents; therefore, to
F3228Specification for Flight Data and Voice Recording in
ensure conformance with the standard, each system shall be
Small Aircraft
used independently of the other, and values from the two
F3230 Practice for Safety Assessment of Systems and
systems shall not be combined.
Equipment in Small Aircraft
1.4 This standard does not purport to address all of the F3231/F3231MSpecification for Electrical Systems forAir-
safety concerns, if any, associated with its use. It is the
craft with Combustion Engine Electrical Power Genera-
responsibility of the user of this standard to establish appro- tion
priate safety, health, and environmental practices and deter-
F3232/F3232MSpecification for Flight Controls in Small
mine the applicability of regulatory limitations prior to use. Aircraft
1.5 This international standard was developed in accor-
F3233/F3233MSpecification for Instrumentation in Small
dance with internationally recognized principles on standard- Aircraft
ization established in the Decision on Principles for the
F3234/F3234MSpecification for Exterior Lighting in Small
Development of International Standards, Guides and Recom- Aircraft
mendations issued by the World Trade Organization Technical
F3236 Specification for High Intensity Radiated Field
Barriers to Trade (TBT) Committee. (HIRF) Protection in Small Aircraft
F3309/F3309MPracticeforSimplifiedSafetyAssessmentof
2. Referenced Documents
Systems and Equipment in Small Aircraft
2.1 Following is a list of external standards referenced F3316/F3316MSpecification for Electrical Systems forAir-
craft with Electric or Hybrid-Electric Propulsion
throughout this specification; the earliest revision acceptable
F3367PracticeforSimplifiedMethodsforAddressingHigh-
Intensity Radiated Fields (HIRF) and Indirect Effects of
1
ThisspecificationisunderthejurisdictionofASTMCommitteeF44onGeneral
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, 2019. Published December 2019. Originally contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
approved in 2015. Last previous edition approved in 2019 as F3061/F3061M–19.
Standards volume information, refer to the standard’s Document Summary page on
DOI: 10.1520/F3061_F3061M–19A. the ASTM website.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
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F3061/F3061M−19a
Lightning on Aircraft (3)A “3” indicates an aeroplane certification level corre-
3
sponding to Level 3; this corresponds to seating for seven or
2.3 SAE Standard:
more passengers but no more than nine (excluding crew).
SAEARP4754, RevAGuidelines for Development of Civil
(4)A “4” indicates an aeroplane certification l
...
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 − 19 F3061/F3061M − 19a
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) 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.
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
F3117/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 Assessment of Systems and Equipment in Small Aircraft
F3231/F3231M Specification for Electrical Systems for Aircraft with Combustion Engine Electrical Power Generation
F3232/F3232M Specification for Flight Controls in Small Aircraft
F3233/F3233M Specification for Instrumentation in Small Aircraft
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 Equipment 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 June 1, 2019Nov. 1, 2019. Published June 2019November 2019. Originally approved in 2015. Last previous edition approved in 20172019 as
F3061/F3061M–17.–19. DOI: 10.1520/F3061_F3061M–19.10.1520/F3061_F3061M–19A.
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
1
---------------------- Page: 1 ----------------------
F3061/F3061M − 19a
F3316/F3316M Specification for Electrical Systems for Aircraft with Electric or Hybrid-Electric Propulsion
F3367 Practice for Simplified Methods f
...
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