ASTM F3061/F3061M-16b
(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 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.
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Designation:F3061/F3061M −16b
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 F3066/F3066MSpecification for Powerplant Systems Spe-
cific Hazard Mitigation
1.1 This specification covers international standards for the
F3083/F3083MSpecification for Emergency Conditions,
systemsandequipmentaspectsofairworthinessanddesignfor
Occupant Safety and Accommodations
“small” aircraft.
F3116/F3116MSpecification for Design Loads and Condi-
1.2 The applicant for a design approval must seek the
tions
individual guidance of their respective CAA body concerning
2.3 Other Standards:
the use of this standard as part of a certification plan. For
14 CFR Part 23 Amendment 62Airworthiness Standards:
information on which CAA regulatory bodies have accepted
Normal, Utility, Acrobatic, and Commuter Category Air-
this standard (in whole or in part) as a means of compliance to
planes
their Small Aircraft Airworthiness regulations (hereinafter
EUROCAE ED-107, Rev AGuide to Certification of Air-
referred to as “the Rules”), refer to ASTM F44 webpage
craft in a High-Intensity Radiated Field (HIRF) Environ-
(www.ASTM.org/COMMITTEE/F44.htm) which includes
ment
CAA website links.
FAA-S-8081-14B, Change 5Private Pilot Practical Test
1.3 The values stated in either SI units or inch-pound units
Standards for Airplane
are to be regarded separately as standard. The values stated in
RTCA/DO-178, Rev BSoftware Considerations inAirborne
each system may not be exact equivalents; therefore, each
Systems and Equipment Certification
system shall be used independently of the other. Combining
RTCA/DO-254Design Assurance Guidance for Airborne
values from the two systems may result in non-conformance
Electronic Hardware
with the standard.
RTCA/DO-335 Guidance for Installation of Automatic
Flight Guidance and Control Systems (AFGCS) for Part
1.4 This standard does not purport to address all of the
23 Airplanes
safety concerns, if any, associated with its use. It is the
3
responsibility of the user of this standard to establish appro-
2.4 SAE Standards:
priate safety and health practices and determine the applica-
SAE AIR825/4, Rev AChemical Oxygen Systems
bility of regulatory limitations prior to use.
SAEARP4754, RevAGuidelines for Development of Civil
Aircraft Systems
2. Referenced Documents
SAE ARP4761Guidelines and Methods for Conducting the
2.1 Following is a list of external standards referenced SafetyAssessmentProcessonCivilAirborneSystemsand
throughout this document; the earliest revision acceptable for Equipment
use is indicated. In all cases later document revisions are SAEARP5583, RevAGuide to Certification ofAircraft in a
acceptableifshowntobeequivalenttothelistedrevision,orif High-Intensity Radiated Field (HIRF) Environment
otherwise formally accepted by the governing civil aviation SAE AS8017, Rev AMinimum Performance Standard for
authority; earlier revisions are not acceptable. Anticollision Light Systems
2 SAE AS8037, Rev –Minimum Performance Standard for
2.2 ASTM Standards:
Aircraft Position Lights
1
ThisspecificationisunderthejurisdictionofASTMCommitteeF44onGeneral 3. Terminology
Aviation Aircraft and is the direct responsibility of Subcommittee F44.50 on
3.1 Terminology specific to this standard is provided below.
Systems and Equipment.
Current edition approved Dec. 1, 2016. Published January 2017. Originally For general terminology, refer to the Terminology standard
approved in 2015. Last previous edition approved in 2016 as F3061/F3061M–16a.
referenced in Section 2.
DOI: 10.1520/F3061_F3061M-16B.
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
3
Standards volume information, refer to the standard’s Document Summary page on AvailablefromSAEInternational(SAE),400CommonwealthDr.,Warrendale,
the ASTM website. PA 15096, http://www.sae.org.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
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F3061/F3061M−16b
3.2 Definitions of Terms Specific to This Standard: 3.2.1.5 Discussion—The fifth character in theAircraft Type
3.2.1 aircraft type code, n—anAircraftType Code (ATC) is Code indicates the cruise speed of the aircraft.
defined by considering both the technical considerations re-
(1)An “L” indicates a cruise speed less than or equal to
garding the design of the aircraft and the airworthiness level 463 km/h
...
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 − 16a F3061/F3061M − 16b
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 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.
2. Referenced Documents
2.1 Following is a list of external standards referenced throughout this document; 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:
F3066/F3066M Specification for Powerplant Systems Specific Hazard Mitigation
F3083/F3083M Specification for Emergency Conditions, Occupant Safety and Accommodations
F3116/F3116M Specification for Design Loads and Conditions
2.3 Other Standards:
14 CFR Part 23 Amendment 62 Airworthiness Standards: Normal, Utility, Acrobatic, and Commuter Category Airplanes
EUROCAE ED-107, Rev A Guide to Certification of Aircraft in a High-Intensity Radiated Field (HIRF) Environment
FAA-S-8081-14B, Change 5 Private Pilot Practical Test Standards for Airplane
RTCA/DO-178, Rev B Software Considerations in Airborne Systems and Equipment Certification
RTCA/DO-254 Design Assurance Guidance for Airborne Electronic Hardware
RTCA/DO-335 Guidance for Installation of Automatic Flight Guidance and Control Systems (AFGCS) for Part 23 Airplanes
3
2.4 SAE Standards:
SAE AIR825/4, Rev A Chemical Oxygen Systems
SAE ARP4754, Rev A Guidelines for Development of Civil Aircraft Systems
SAE ARP4761 Guidelines and Methods for Conducting the Safety Assessment Process on Civil Airborne Systems and
Equipment
SAE ARP5583, Rev A Guide to Certification of Aircraft in a High-Intensity Radiated Field (HIRF) Environment
SAE AS8017, Rev A Minimum Performance Standard for Anticollision Light Systems
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 Aug. 1, 2016Dec. 1, 2016. Published September 2016January 2017. Originally approved in 2015. Last previous edition approved in 2016 as
F3061/F3061M – 16.F3061/F3061M – 16a. DOI: 10.1520/F3061_F3061M-16A.10.1520/F3061_F3061M-16B.
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
Available from SAE International (SAE), 400 Commonwealth Dr., Warrendale, PA 15096, http://www.sae.org.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
---------------------- Page: 1 ----------------------
F3061/F3061M − 16b
SAE AS8037, Rev – Minimum Performance Standard for Aircraft Position Lights
3. Terminology
3.1 Terminology specific to this standard is provided below. For general terminology, refer to the Termi
...
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