SAE AS8055A
Current
The latest, up-to-date edition.
Minimum Performance Standard for Airborne Head Up Display (HUD)
Hardcopy , PDF
English
28-07-2015
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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