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SAE AS8055A

Current

Current

The latest, up-to-date edition.

Minimum Performance Standard for Airborne Head Up Display (HUD)

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

28-07-2015

€147.52
Excluding VAT

1. SCOPE
2. REFERENCES
3. GENERAL REQUIREMENTS
4. MINIMUM PERFORMANCE STANDARDS UNDER
   STANDARD CONDITIONS
5. MINIMUM PERFORMANCE STANDARDS UNDER
   ENVIRONMENTAL CONDITIONS
6. TEST PROCEDURES
7. GLOSSARY OF TERMS
8. NOTES
APPENDIX A - HEAD UP DISPLAYS

This SAE Aerospace Standard (AS) specifies minimum performance standards for airborne binocular Head-Up Displays (HUDs) in fixed wing (14 CFR part 23, 25) aircraft; while this document is also applicable to rotorcraft (14 CFR part 27, 29) additional performance standards may be required for rotorcraft.

DocumentType
Standard
Pages
36
PublisherName
SAE International
Status
Current
Supersedes

This SAE Aerospace Standard (AS) specifies minimum performance standards for airborne binocular Head-Up Displays (HUDs) in fixed wing (14 CFR part 23, 25) aircraft; while this document is also applicable to rotorcraft (14 CFR part 27, 29) additional performance standards may be required for rotorcraft. This aerospace standard covers basic display standards, but does not include specific application requirements. Specific applications can include flight instrumentation, navigation, engine and system status, alerting, surveillance, communication, terrain awareness, weather, enhanced vision, synthetic vision and other displays.This document covers criteria for conformal and non-conformal HUD systems that are intended for use in the flight deck by the pilot or copilot. Display minimum performance characteristics are specified for standard and other environmental conditions for the purpose of product qualification.This document does not address sensor imaging systems, displays worn by the pilot (goggles, helmet mounted displays) or specific symbology to be displayed.This document is intended to be used in combination with other guidance material contained in current system specific, Technical Standard Orders (TSOs), Advisory Circulars (ACs), and other Federal Aviation Administration (FAA)-approved guidance material. This SAE Aerospace Standard can be applicable to HUDs used across multiple aircraft types.

FAA AC 23.1311-1 : 2011 INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES
SAE ARP5677 Human Engineering Considerations for Airborne Implementation of Enhanced Synthetic Vision Systems
FAA AC 25-11 : 2014 ELECTRONIC FLIGHT DISPLAYS
FAA AC 90-106 : 2017 ENHANCED FLIGHT VISION SYSTEMS
FAA AC 20-167 : 2016 AIRWORTHINESS APPROVAL OF ENHANCED VISION SYSTEM, SYNTHETIC VISION SYSTEM, COMBINED VISION SYSTEM, AND ENHANCED FLIGHT VISION SYSTEM EQUIPMENT
SAE ARP5364 Human Factor Considerations in the Design of Multifunction Display Systems for Civil Aircraft
SAE ARP5287 Optical Measurement Procedures for Airborne Head Up Display (HUD)
ARINC 764 : 2005 HEAD-UP DISPLAY (HUD) SYSTEM
SAE ARP4103A Flight Deck Lighting for Commercial Transport Aircraft
FAA AC 25.1329-1 : 2016 APPROVAL OF FLIGHT GUIDANCE SYSTEMS
FAA AC 20-185 : 2015 AIRWORTHINESS APPROVAL OF SYNTHETIC VISION GUIDANCE SYSTEM
SAE ARP 4103 : 2014 FLIGHT DECK LIGHTING FOR COMMERCIAL TRANSPORT AIRCRAFT
SAE ARP6023 Human Engineering Considerations for Implementing Enhanced Synthetic Vision Systems in Vertical Flight Capable Platforms

SAE ARP1161A Crew Station Lighting - Commercial Aircraft
SAE ARP 4260 : 2014 PHOTOMETRIC AND COLORIMETRIC MEASUREMENT PROCEDURES FOR AIRBORNE ELECTRONIC FLAT PANEL DISPLAYS
FAA AC 23.1311-1 : 2011 INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES
RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
FAA AC 25-11 : 2014 ELECTRONIC FLIGHT DISPLAYS
FAA AC 20-136 : 2011 AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
MIL-STD-1787 Revision B:1996 AIRCRAFT DISPLAY SYMBOLOGY
FAA AC 20-158 : 2014 THE CERTIFICATION OF AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEMS FOR OPERATION IN THE HIGH-INTENSITY RADIATED FIELDS (HIRF) ENVIRONMENT
SAE ARP4032B Human Engineering Considerations in the Application of Color to Electronic Aircraft Displays
FAA AC 120-28 : 0 CRITERIA FOR APPROVAL OF CATEGORY 3 WEATHER MINIMA FOR TAKEOFF, LANDING, AND ROLLOUT
FAA AC 25.773-1 : 0 PILOT COMPARTMENT VIEW DESIGN CONSIDERATIONS
SAE ARP 4101 : 1988 FLIGHT DECK LAYOUT AND FACILITIES
SAE ARP 4105 : 2012 ABBREVIATIONS, ACRONYMS, AND TERMS FOR USE ON THE FLIGHT DECK
SAE ARP 4155 : 1997 HUMAN INTERFACE DESIGN METHODOLOGY FOR INTEGRATED DISPLAY SYMBOLOGY
SAE ARP 5287 : 1999 OPTICAL MEASUREMENT PROCEDURES FOR AIRBORNE HEAD UP DISPLAY (HUD)
MIL-HDBK-87213 Revision A:2005 Electronically / Optically Generated Airborne Displays
FAA AC 23.1309-1 : 2011 SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
MIL-STD-1295 Revision A:1984 HUMAN FACTORS ENGINEERING DESIGN CRITERIA FOR HELICOPTER COCKPIT ELECTRO-OPTICAL DISPLAY SYMBOLOGY
SAE AIR4742A Display Characteristics of FDI Head-Up Guidance System as Approved for the B-727 Airplane
FAA AC 120-29 : 0 CRITERIA FOR APPROVAL OF CATEGORY 1 AND CATEGORY 2 WEATHER MINIMA FOR APPROACH
SAE ARP5583A Guide to Certification of Aircraft in a High-Intensity Radiated Field (HIRF) Environment
SAE ARP4102/8A Flight Deck Head-Up Displays
FAA AC 25.1309-1 : 0 SYSTEM DESIGN AND ANALYSIS
SAE ARP 1874 : 1988 DESIGN OBJECTIVES FOR CRT DISPLAYS FOR PART 25 (TRANSPORT) AIRCRAFT
SAE ARP 4102/7 : 1988 ELECTRONIC DISPLAYS
SAE AS8034B Minimum Performance Standard for Airborne Multipurpose Electronic Displays
SAE ARP 4256 : 2001 DESIGN OBJECTIVES FOR LIQUID CRYSTAL DISPLAYS FOR PART 25 (TRANSPORT) AIRCRAFT
SAE ARP 4102 : 1988 FLIGHT DECK PANELS, CONTROLS, AND DISPLAYS
SAE ARP1782B Photometric and Colorimetric Measurement Procedures for Airborne Direct View CRT Displays
SAE ARP 4103 : 2014 FLIGHT DECK LIGHTING FOR COMMERCIAL TRANSPORT AIRCRAFT

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