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.

General Information

Status
Historical
Publication Date
31-Jan-2018
Drafting Committee
Current Stage
Ref Project

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NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.
Contact ASTM International (www.astm.org) for the latest information
Designation:F3117 −18a
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.
3
1. Scope 2.2 Code of Federal Regulations (CFR):
14 CFR Part 23 Amendment 62
1.1 This specification covers international standards for the
crew interface aspects of airworthiness and design for aircraft.
3. Terminology
“Crew” includes flight crew and maintenance crew.
3.1 Refer to Terminology F3060.
1.2 The applicant for a design approval must seek the
4. Pilot / Occupant Compartment
individualguidanceoftheirrespectiveCivilAviationAuthority
(CAA) body concerning the use of this standard as part of a
4.1 Pilot Compartment:
certification plan. For information on which CAA regulatory
4.1.1 For each pilot compartment, the compartment and its
bodies have accepted this standard (in whole or in part) as a
equipment must allow each pilot to perform flight crew duties
means of compliance to their airworthiness regulations (here-
without unreasonable concentration or fatigue.
inafterreferredtoas“theRules”),refertoASTMF44webpage
4.1.2 For each pilot compartment, where the flight crew are
(www.ASTM.org/COMMITTEE/F44.htm) which includes
separated from the passengers by a partition, there must be a
CAA website links.
means to facilitate two-way communication between flight
crew and cabin occupants, such as an opening or openable
1.3 This standard does not purport to address all of the
window or door or other means.
safety concerns, if any, associated with its use. It is the
responsibility of the user of this standard to establish appro-
NOTE 1—A single intercom port from passenger compartment to crew
priate safety, health, and environmental practices and deter-
may suffice as other means. If an opening is not provided to allow visual
verification of occupant compartment conditions, such as Oxygen System
mine the applicability of regulatory limitations prior to use.
status in Specification F3061/F3061M, other indication means may be
1.4 This international standard was developed in accor-
required for other systems.
dance with internationally recognized principles on standard-
4.1.3 If communication between flight crew and cabin
ization established in the Decision on Principles for the
occupants relies on electrical power, the one-way communica-
Development of International Standards, Guides and Recom-
tion from the flight crew to the cabin occupants must be
mendations issued by the World Trade Organization Technical
considered an essential electrical load.
Barriers to Trade (TBT) Committee.
4.2 Pilot Compartment View:
2. Referenced Documents 4.2.1 Each pilot compartment must be arranged with suffi-
ciently clear and undistorted view to enable the pilot to safely
2
2.1 ASTM Standards:
taxi, takeoff, approach, land, and perform any maneuvers
F3060 Terminology for Aircraft
within the operating limitations of the aircraft.
F3061/F3061M Specification for Systems and Equipment in
4.2.2 Each pilot compartment must be free from glare and
Small Aircraft
reflections that could interfere with the pilot’s vision. Compli-
F3064/F3064M Specification for Aircraft Powerplant
ance must be shown in all operations for which certification is
Control, Operation, and Indication
requested.
4.2.3 Each pilot compartment must be designed so that each
pilot is protected from the elements so that moderate rain
1
ThisspecificationisunderthejurisdictionofASTMCommitteeF44onGeneral
conditions do not unduly impair the pilot’s view of the flight
Aviation Aircraft and is the direct responsibility of Subcommittee F44.10 on
path in normal flight and while landing.
General.
4.2.4 A vision system with a transparent display surface
Current edition approved Feb. 1, 2018. Published March 2018. Originally
approved in 2015. Last previous edition approved in 2018 as F3117 – 18. DOI:
located in the pilot’s outside field of view, such as a head
10.1520/F3117-18A.
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 ----------------------
F3117−18a
up-display, head mounted display, or other equivalent
...

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 − 18 F3117 − 18a
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
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
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.
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 Jan. 1, 2018Feb. 1, 2018. Published March 2018. Originally approved in 2015. Last previous edition approved in 20152018 as
F3117 – 15.F3117 – 18. DOI: 10.1520/F3117-18.10.1520/F3117-18A.
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 − 18a
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 compartment must be free from glare and reflections that could interfere with the pilot’s vision. Compliance
must be shown in all operations for which certification is requested.
4.2.3 Each pilot compartment must be design
...

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