ASTM F3117-18b
(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.
1.2 The applicant 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. For information on which CAA regulatory bodies have accepted this standard (in whole or in part) as a means of compliance to their 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 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.
1.4 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 −18b
Standard Specification for
1
Crew Interface in Aircraft
This standard is issued under the fixed designation F3117; 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 F3174/F3174M Specification for Establishing Operating
Limitations and Information for Aeroplanes
1.1 This specification covers international standards for the
F3179/F3179M Specification for Performance of Aircraft
crew interface aspects of airworthiness and design for aircraft.
3
2.2 Code of Federal Regulations (CFR):
“Crew” includes flight crew and maintenance crew.
14 CFR Part 23 Amendment 62
1.2 The applicant for a design approval must seek the
individualguidanceoftheirrespectiveCivilAviationAuthority
3. Terminology
(CAA) body concerning the use of this standard as part of a
3.1 Refer to Terminology F3060.
certification plan. For information on which CAA regulatory
bodies have accepted this standard (in whole or in part) as a
4. Pilot / Occupant Compartment
means of compliance to their airworthiness regulations (here-
4.1 Pilot Compartment:
inafterreferredtoas“theRules”),refertoASTMF44webpage
4.1.1 For each pilot compartment, the compartment and its
(www.ASTM.org/COMMITTEE/F44.htm) which includes
equipment must allow each pilot to perform flight crew duties
CAA website links.
without unreasonable concentration or fatigue.
1.3 This standard does not purport to address all of the
4.1.2 For each pilot compartment, where the flight crew are
safety concerns, if any, associated with its use. It is the
separated from the passengers by a partition, there must be a
responsibility of the user of this standard to establish appro-
means to facilitate two-way communication between flight
priate safety, health, and environmental practices and deter-
crew and cabin occupants, such as an opening or openable
mine the applicability of regulatory limitations prior to use.
window or door or other means.
1.4 This international standard was developed in accor-
dance with internationally recognized principles on standard-
NOTE 1—A single intercom port from passenger compartment to crew
may suffice as other means. If an opening is not provided to allow visual
ization established in the Decision on Principles for the
verification of occupant compartment conditions, such as Oxygen System
Development of International Standards, Guides and Recom-
status in Specification F3061/F3061M, other indication means may be
mendations issued by the World Trade Organization Technical
required for other systems.
Barriers to Trade (TBT) Committee.
4.1.3 If communication between flight crew and cabin
occupants relies on electrical power, the one-way communica-
2. Referenced Documents
2 tion from the flight crew to the cabin occupants must be
2.1 ASTM Standards:
considered an essential electrical load.
F3060 Terminology for Aircraft
4.2 Pilot Compartment View:
F3061/F3061M Specification for Systems and Equipment in
4.2.1 Each pilot compartment must be arranged with suffi-
Small Aircraft
ciently clear and undistorted view to enable the pilot to safely
F3064/F3064M Specification for Aircraft Powerplant
taxi, takeoff, approach, land, and perform any maneuvers
Control, Operation, and Indication
within the operating limitations of the aircraft.
F3173/F3173M Specification for Aircraft Handling Charac-
4.2.2 Each pilot compartment must be free from glare and
teristics
reflections that could interfere with the pilot’s vision. Compli-
ance must be shown in all operations for which certification is
1
ThisspecificationisunderthejurisdictionofASTMCommitteeF44onGeneral
requested.
Aviation Aircraft and is the direct responsibility of Subcommittee F44.10 on
General.
4.2.3 Each pilot compartment must be designed so that each
CurrenteditionapprovedMay1,2018.PublishedJuly2018.Originallyapproved
pilot is protected from the elements so that moderate rain
in 2015. Last previous edition approved in 2018 as F3117 – 18a. DOI: 10.1520/
F3117-18B.
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
3
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM Available from U.S. Government Printing Office, Superintendent of
Standards volume information, refer to the standard’s Document Summary page on Documents, 732 N. Capitol St., NW, Washington, DC 20401-0001, http://
the ASTM website. www.access.gpo.gov.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
---------------------- Page: 1 ----------------------
F3117−18b
conditions do not unduly impair the pilot’s view of the flight
(1)
...
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 − 18a F3117 − 18b
Standard Specification for
1
Crew Interface in Aircraft
This standard is issued under the fixed designation F3117; 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.
1.2 The applicant 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. For information on which CAA regulatory bodies have
accepted this standard (in whole or in part) as a means of compliance to their 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 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.
1.4 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
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
3
2.2 Code of Federal Regulations (CFR):
14 CFR Part 23 Amendment 62
3. Terminology
3.1 Refer to Terminology F3060.
4. Pilot / Occupant Compartment
4.1 Pilot Compartment:
4.1.1 For each pilot compartment, the compartment and its equipment must allow each pilot to perform flight crew duties
without unreasonable concentration or fatigue.
4.1.2 For each pilot compartment, where the flight crew are separated from the passengers by a partition, there must be a means
to facilitate two-way communication between flight crew and cabin occupants, such as an opening or openable window or door
or other means.
NOTE 1—A single intercom port from passenger compartment to crew may suffice as other means. If an opening is not provided to allow visual
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 Feb. 1, 2018May 1, 2018. Published March 2018July 2018. Originally approved in 2015. Last previous edition approved in 2018 as
F3117 – 18.F3117 – 18a. DOI: 10.1520/F3117-18A.10.1520/F3117-18B.
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 U.S. Government Printing Office, Superintendent of Documents, 732 N. Capitol St., NW, Washington, DC 20401-0001, http://www.access.gpo.gov.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1
---------------------- Page: 1 ----------------------
F3117 − 18b
verification of occupant compartment conditions, such as Oxygen System status in Specification F3061/F3061M, other indication means may be required
for other systems.
4.1.3 If communication between flight crew and cabin occupants relies on electrical power, the one-way communication from
the flight crew to the cabin occupants must be considered an essential electrical load.
4.2 Pilot Compartment View:
4.2.1 Each pilot compartment must be arranged with sufficiently clear and undistorted view to enable the pilot to safely taxi,
takeoff, approach, land, and perform any maneuvers within the operating limitations of the aircraft.
4.2.2 Each pilot
...
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