ASTM F3117/F3117M-18c
(Specification)Standard Specification for Crew Interface in Aircraft
Standard Specification for Crew Interface in Aircraft
SCOPE
1.1 This specification covers international standards for the crew interface aspects of airworthiness and design for aircraft. “Crew” includes flight crew and maintenance crew. The material was developed through open consensus of international experts in general aviation. This information was created by focusing on Normal Category aeroplanes. The content may be more broadly applicable; it is the responsibility of the applicant to substantiate broader applicability as a specific means of compliance.
1.2 An applicant intending to propose this information as Means of Compliance for a design approval must seek guidance from their respective oversight authority (for example, published guidance from applicable CAAs) concerning the acceptable use and application thereof. For information on which oversight authorities have accepted this specification (in whole or in part) as an acceptable Means of Compliance to their regulatory requirements (hereinafter “the Rules”), refer to ASTM Committee F44 web page (https://www.astm.org/COMMITTEE/F44.htm).
1.3 Units—This document may present information in either SI units, English Engineering units, or both. 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.
1.4 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:F3117/F3117M −18c
Standard Specification for
1
Crew Interface in Aircraft
ThisstandardisissuedunderthefixeddesignationF3117/F3117M;thenumberimmediatelyfollowingthedesignationindicatestheyear
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 mendations issued by the World Trade Organization Technical
Barriers to Trade (TBT) Committee.
1.1 This specification covers international standards for the
crew interface aspects of airworthiness and design for aircraft.
2. Referenced Documents
“Crew” includes flight crew and maintenance crew. The
2
2.1 ASTM Standards:
material was developed through open consensus of interna-
F3060 Terminology for Aircraft
tional experts in general aviation.This information was created
F3061/F3061M Specification for Systems and Equipment in
by focusing on Normal Category aeroplanes. The content may
Small Aircraft
be more broadly applicable; it is the responsibility of the
F3064/F3064M Specification for Aircraft Powerplant
applicant to substantiate broader applicability as a specific
Control, Operation, and Indication
means of compliance.
F3116/F3116M Specification for Design Loads and Condi-
1.2 An applicant intending to propose this information as
tions
Means of Compliance for a design approval must seek guid-
F3173/F3173M Specification for Aircraft Handling Charac-
ance from their respective oversight authority (for example,
teristics
published guidance from applicable CAAs) concerning the
F3174/F3174M Specification for Establishing Operating
acceptable use and application thereof. For information on
Limitations and Information for Aeroplanes
which oversight authorities have accepted this specification (in
F3179/F3179M Specification for Performance of Aircraft
whole or in part) as an acceptable Means of Compliance to
F3233/F3233M Specification for Instrumentation in Small
their regulatory requirements (hereinafter “the Rules”), refer to
Aircraft
ASTM Committee F44 web page (https://www.astm.org/
F3235 Specification for Aircraft Storage Batteries
COMMITTEE/F44.htm). 3
2.2 Code of Federal Regulations (CFR):
1.3 Units—Thisdocumentmaypresentinformationineither
14 CFR Part 23 Amendment 62
SI units, English Engineering units, or both. The values stated
3. Terminology
in each system may not be exact equivalents; therefore, each
system shall be used independently of the other. Combining
3.1 Refer to Terminology F3060.
values from the two systems may result in nonconformance
4. Pilot/Occupant Compartment
with the standard.
4.1 Pilot Compartment:
1.4 This standard does not purport to address all of the
4.1.1 For each pilot compartment, the compartment and its
safety concerns, if any, associated with its use. It is the
equipment must allow each pilot to perform flight crew duties
responsibility of the user of this standard to establish appro-
without unreasonable concentration or fatigue.
priate safety, health, and environmental practices and deter-
4.1.2 For each pilot compartment, where the flight crew are
mine the applicability of regulatory limitations prior to use.
separated from the passengers by a partition, there must be a
1.5 This international standard was developed in accor-
means to facilitate two-way communication between flight
dance with internationally recognized principles on standard-
crew and cabin occupants, such as an opening or openable
ization established in the Decision on Principles for the
window or door or other means.
Development of International Standards, Guides and Recom-
1 2
ThisspecificationisunderthejurisdictionofASTMCommitteeF44onGeneral For referenced ASTM standards, visit the ASTM website, www.astm.org, or
Aviation Aircraft and is the direct responsibility of Subcommittee F44.10 on contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
General. Standards volume information, refer to the standard’s Document Summary page on
Current edition approved Nov. 1, 2018. Published December 2018. Originally the ASTM website.
3
approved in 2015. Last previous edition approved in 2018 as F3117–18b. DOI: Available from U.S. Government Publishing Office (GPO), 732 N. Capitol St.,
10.1520/F3117_F3117M–18C. NW, Washington, DC 20401, http://www.gpo.gov.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
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F3117/F3117M−18c
NOTE 1—A single intercom port from passenger compartment to crew
4.2.4.6 When the vision system is not in operation, it may
may suffice as other means. If an opening is not provided to allow visual
not restrict the pilot from performing the maneuvers specified
verification of o
...
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: F3117 − 18b F3117/F3117M − 18c
Standard Specification for
1
Crew Interface in Aircraft
This standard is issued under the fixed designation F3117;F3117/F3117M; 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 crew interface aspects of airworthiness and design for aircraft.
“Crew” includes flight crew and maintenance crew. The material was developed through open consensus of international experts
in general aviation. This information was created by focusing on Normal Category aeroplanes. The content may be more broadly
applicable; it is the responsibility of the applicant to substantiate broader applicability as a specific means of compliance.
1.2 The applicant An applicant intending to propose this information as Means of Compliance for a design approval must seek
the individual guidance of their respective Civil Aviation Authority (CAA) body concerning the use of this standard as part of a
certification plan. from their respective oversight authority (for example, published guidance from applicable CAAs) concerning
the acceptable use and application thereof. For information on which CAA regulatory bodies oversight authorities have accepted
this standardspecification (in whole or in part) as a means of compliancean acceptable Means of Compliance to their airworthiness
regulations (hereinafter referred to as regulatory requirements (hereinafter “the Rules”), refer to ASTM F44 webpage
(www.ASTM.org/COMMITTEE/F44.htm) which includes CAA website links.Committee F44 web page (https://www.astm.org/
COMMITTEE/F44.htm).
1.3 Units—This document may present information in either SI units, English Engineering units, or both. 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.
1.4 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
2.1 ASTM Standards:
F3060 Terminology for Aircraft
F3061/F3061M Specification for Systems and Equipment in Small Aircraft
F3064/F3064M Specification for Aircraft Powerplant Control, Operation, and Indication
F3116/F3116M Specification for Design Loads and Conditions
F3173/F3173M Specification for Aircraft Handling Characteristics
F3174/F3174M Specification for Establishing Operating Limitations and Information for Aeroplanes
F3179/F3179M Specification for Performance of Aircraft
F3233/F3233M Specification for Instrumentation in Small Aircraft
F3235 Specification for Aircraft Storage Batteries
3
2.2 Code of Federal Regulations (CFR):
14 CFR Part 23 Amendment 62
1
This specification is under the jurisdiction of ASTM Committee F44 on General Aviation Aircraft and is the direct responsibility of Subcommittee F44.10 on General.
Current edition approved May 1, 2018Nov. 1, 2018. Published July 2018December 2018. Originally approved in 2015. Last previous edition approved in 2018 as
F3117 – 18a.F3117–18b. DOI: 10.1520/F3117-18B.10.1520/F3117_F3117M–18C.
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.
3
Available from U.S. Government Printing Office, Superintendent of Documents, Publishing Office (GPO), 732 N. Capitol St., NW, Washington, DC 20401-0001,
http://www.access.gpo.gov.20401, http://www.gpo.gov.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
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F3117/F3117M − 18c
3. Termin
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