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SAE ARP 4107 : 2008

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

AEROSPACE GLOSSARY OF HUMAN FACTORS ENGINEERS
Available format(s)

Hardcopy , PDF

Superseded date

11-06-2020

Language(s)

English

Published date

02-16-2008

Provides design to serve persons who need to know the accepted meanings, within specific contexts, of the terminology used in reports, articles, regulations, and other materials dealing with aviation safety - with particular reference to terms specific to human factors in aviation safety.

Committee
G-10
DocumentType
Standard
Pages
114
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

SAE ARP 5677 : 2012 HUMAN ENGINEERING CONSIDERATIONS FOR AIRBORNE IMPLEMENTATION OF ENHANCED SYNTHETIC VISION SYSTEMS
SAE ARP 5898 : 2013 HUMAN INTERFACE CRITERIA FOR FLIGHT DECK SURFACE OPERATIONS DISPLAYS
SAE ARP 5364 : 2003 HUMAN FACTOR CONSIDERATIONS IN THE DESIGN OF MULTIFUNCTION DISPLAY SYSTEMS FOR CIVIL AIRCRAFT
SAE ARD 50083 : 1999 HUMAN FACTORS ISSUES ASSOCIATED WITH COCKPIT DISPLAY OF TRAFFIC INFORMATION (CDTI)
SAE ARP 5589 : 2005 HUMAN ENGINEERING CONSIDERATIONS FOR DESIGN AND IMPLEMENTATION OF PERSPECTIVE FLIGHT GUIDANCE DISPLAYS
SAE ARP 5056 : 2013 FLIGHT CREW INTERFACE CONSIDERATIONS IN THE FLIGHT DECK DESIGN PROCESS FOR PART 25 AIRCRAFT
SAE ARP 5119 : 2013 LOCATION OF AND DISPLAY SYMBOLOGY REQUIREMENTS FOR HEAD-DOWN ELECTRONIC FLIGHT DISPLAYS FOR STEEP IMC APPROACHES
SAE ARP 5430 : 2013 HUMAN INTERFACE CRITERIA FOR VERTICAL SITUATION AWARENESS DISPLAYS
SAE ARP 4155 : 2008 HUMAN INTERFACE DESIGN METHODOLOGY FOR INTEGRATED DISPLAY SYMBOLOGY
RG.AERO 000721 : 2016 GENERAL RECOMMENDATIONS FOR THE BIT ARCHITECTURE IN AN INTEGRATED SYSTEM
SAE ARP 6023 : 2013 HUMAN ENGINEERING CONSIDERATIONS FOR IMPLEMENTING ENHANCED SYNTHETIC VISION SYSTEMS IN VERTICAL FLIGHT CAPABLE PLATFORMS

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