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SAE ARP 1782 : 2012

Current
Current

The latest, up-to-date edition.

PHOTOMETRIC AND COLORMETRIC MEASUREMENT PROCEDURES FOR AIRBORNE DIRECT VIEW CRT DISPLAYS
Published date

12-09-2012

Specifies methods to be used in measuring those performance characteristics important for color and luminance use in direct view airborne electronic display systems.

Committee
A-20A
DocumentType
Standard
ProductNote
THIS VERSION IS NOW STABILIZED
PublisherName
SAE International
Status
Current
Supersedes

AFGS-87213 Revision B:1993 DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED
FAA AC 23.1311-1 : 2011 INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES
SAE AS 8055A : 2015 MINIMUM PERFORMANCE STANDARD FOR AIRBORNE HEAD UP DISPLAY (HUD)
SAE J 1757-1 : 2015 STANDARD METROLOGY FOR VEHICULAR DISPLAYS
SAE ARP 5677 : 2012 HUMAN ENGINEERING CONSIDERATIONS FOR AIRBORNE IMPLEMENTATION OF ENHANCED SYNTHETIC VISION SYSTEMS
FAA AC 25-11 : 2014 ELECTRONIC FLIGHT DISPLAYS
SAE ARP 4032 : 2013 HUMAN ENGINEERING CONSIDERATIONS IN THE APPLICATION OF COLOR TO ELECTRONIC AIRCRAFT DISPLAYS
A-A-58055 Base Document:1996 Indicator, Attitude, Three Inch, Solid State Self-Contained
SAE ARD 50083 : 1999 HUMAN FACTORS ISSUES ASSOCIATED WITH COCKPIT DISPLAY OF TRAFFIC INFORMATION (CDTI)
SAE ARP 4260 : 2014 PHOTOMETRIC AND COLORIMETRIC MEASUREMENT PROCEDURES FOR AIRBORNE ELECTRONIC FLAT PANEL DISPLAYS
SAE ARP 5589 : 2005 HUMAN ENGINEERING CONSIDERATIONS FOR DESIGN AND IMPLEMENTATION OF PERSPECTIVE FLIGHT GUIDANCE DISPLAYS
SAE ARP 5287 : 2008 OPTICAL MEASUREMENT PROCEDURES FOR AIRBORNE HEAD UP DISPLAY (HUD)
SAE ARP 5898 : 2013 HUMAN INTERFACE CRITERIA FOR FLIGHT DECK SURFACE OPERATIONS DISPLAYS
MIL-HDBK-87213 Revision A:2005 ELECTRONICALLY/OPTICALLY GENERATED AIRBORNE DISPLAYS
SAE ARP 5430 : 2013 HUMAN INTERFACE CRITERIA FOR VERTICAL SITUATION AWARENESS DISPLAYS
SAE ARP 4103A : 2014(R2019) FLIGHT DECK LIGHTING FOR COMMERCIAL TRANSPORT AIRCRAFT
SAE ARP 4103 : 2014 FLIGHT DECK LIGHTING FOR COMMERCIAL TRANSPORT AIRCRAFT
SAE ARP 6023 : 2013 HUMAN ENGINEERING CONSIDERATIONS FOR IMPLEMENTING ENHANCED SYNTHETIC VISION SYSTEMS IN VERTICAL FLIGHT CAPABLE PLATFORMS

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