SAE ARP5364
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Human Factor Considerations in the Design of Multifunction Display Systems for Civil Aircraft
14-12-2020
27-03-2003
1 Scope
1.1 Purpose
2 References
2.1 SAE publications
2.2 U.S. Government publications
2.3 Other publications
2.4 Definitions
2.5 Abbreviations and acronyms
3 System function
3.1 Primary flight information
3.2 Primary flight display
3.3 Primary engine information
3.4 Secondary engine information
3.5 Visual crew alerting system (CAS) information
3.6 Navigation information
3.7 Weather information
3.8 Terrain and obstacles
3.9 Airport mapping
3.10 Traffic information
3.11 Aircraft systems functions
3.12 Data link functions
3.13 The radio management system function
3.14 Electronic data management system
3.15 Electronic checklist
3.16 Imaging systems
4 Design objectives
4.1 Crew interface
4.2 Information characteristics
4.3 Reliability
4.4 Mode and data source awareness
4.5 Display design considerations
5 Implementation and integration
5.1 User input controls
5.2 Layering
5.3 Clutter control
5.4 Automatic switching and Pop-Ups
5.5 Visual crew alerting and display prioritization
5.6 Sensor and information fusion
5.7 Windowing and data block
5.8 Reconfiguration modes
5.9 Synoptic, system displays and maintenance pages
5.10 Data link
5.11 Menu structures and architecture
5.12 Default settings
5.13 Overlays
5.14 Self-test
5.15 Data storage and retrieval
5.16 Retrofit integration
6 Training
7 Glossary
Appendix A Related literature
Appendix B Examples of existing display combinations of
MFD functions
Specifies the crew access to a variety of data, or combinations of data, used to fly the aircraft, to navigate, to communicate, and to manage aircraft systems.
DocumentType |
Standard
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PublisherName |
SAE International
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Status |
Superseded
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SupersededBy |
The function of a multifunctional display (MFD) system is to provide the crew access to a variety of data, or combinations of data, used to fly the aircraft, to navigate, to communicate, and to manage aircraft systems. MFDs may also display primary flight information (PFI) as needed to insure continuity of operations. This document sets forth design and operational recommendations concerning the human factors considerations for MFD systems.The MFD system may contain one or more electronic display devices capable of presenting data in several possible formats. MFDs are designed to depict PFI, navigation, communication, aircraft state, aircraft system management, weather, traffic, and/or other information used by the flight crew for command and control of the aircraft. The information displayed may be combined to make an integrated display or one set of data may simply replace another.The information contained in this document can be applied to the design of all MFDs, including electronic flight bags (EFB), regardless of aircraft type. This document makes extensive use of “lessons learned” and information developed and currently in use by systems and airframe manufacturers through the evolutionary development of today’s advanced systems.Some assumptions used in developing this document include:MFDs will incorporate a human-centered design using knowledge gained from previous work and research.This document is intended to apply to new systems or modifications to existing systems.Each function of a MFD is capable of providing accurate and timely information appropriate to the tasks of the flight crew for certain aircraft operations throughout all phases of flight.MFD systems will be based on the aeronautical English language, but other languages may have to be considered.MFD systems will meet international harmonized certification requirements.Use of the information in this document is subject to the certification requirements for a given airplane.The design process should include operator training considerations throughout its development.PFI will be available on the flight deck at all times.
FAA AC 23.1311-1 : 2011 | INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES |
SAE ARP5621 | Electronic Display of Aeronautical Information (Charts) |
FAA AC 25-11 : 2014 | ELECTRONIC FLIGHT DISPLAYS |
SAE ARP4032B | Human Engineering Considerations in the Application of Color to Electronic Aircraft Displays |
SAE ARP5898 | Human Interface Criteria for Flight Deck Surface Operations Displays |
SAE ARP 4102/15 : 2000 | ELECTRONIC DATA MANAGEMENT SYSTEM (EDMS) |
RTCA DO 200B : 2015 | STANDARDS FOR PROCESSING AERONAUTICAL DATA |
SAE ARP4107 | AEROSPACE GLOSSARY FOR HUMAN FACTORS ENGINEERS |
RTCA DO-201A : 2000 | STANDARDS FOR AERONAUTICAL INFORMATION |
SAE ARP 5365 : 1999 | HUMAN INTERFACE CRITERIA FOR COCKPIT DISPLAY OF TRAFFIC INFORMATION |
FAA AC 25-11 : 2014 | ELECTRONIC FLIGHT DISPLAYS |
SAE ARP 1068 : 1994 | FLIGHT DECK INSTRUMENTATION, DISPLAY CRITERIA AND ASSOCIATED CONTROLS FOR TRANSPORT AIRCRAFT |
SAE ARP 4102/13 : 1993 | DATA LINK |
SAE ARP4032B | Human Engineering Considerations in the Application of Color to Electronic Aircraft Displays |
SAE ARP5108A | Human Interface Criteria for Terrain Separation Assurance Display Technology |
FAA AC 25-23 : 0 | AIRWORTHINESS CRITERIA FOR THE INSTALLATION APPROVAL OF A TERRAIN AWARENESS AND WARNING SYSTEM (TAWS) FOR PART 25 AIRPLANES |
SAE ARP 4791 : 1996 | HUMAN ENGINEERING RECOMMENDATIONS FOR DATA LINK SYSTEMS |
RTCA DO 243 : 1998 | GUIDANCE FOR INITIAL IMPLEMENTATION OF COCKPIT DISPLAY OF TRAFFIC INFORMATION |
SAE ARP 4102/4 : 1988 | FLIGHT DECK ALERTING SYSTEM (FAS) |
SAE ARP 4102/1 : 1988 | ON BOARD WEIGHT AND BALANCE SYSTEM |
SAE ARP4102/2A | Automatic Braking System (ABS) |
SAE ARP 571 : 1994 | FLIGHT DECK CONTROLS AND DISPLAYS FOR COMMUNICATION AND NAVIGATION EQUIPMENT FOR TRANSPORT AIRCRAFT |
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) |
SAE AS8055A | Minimum Performance Standard for Airborne Head Up Display (HUD) |
SAE ARP 4033 : 1995 | PILOT-SYSTEM INTEGRATION |
SAE ARP4102/8A | Flight Deck Head-Up Displays |
SAE ARP 1874 : 1988 | DESIGN OBJECTIVES FOR CRT DISPLAYS FOR PART 25 (TRANSPORT) AIRCRAFT |
SAE ARP 5288 : 2001 | TRANSPORT CATEGORY AIRPLANE HEAD UP DISPLAY (HUD) SYSTEMS |
SAE ARP5289A | Electronic Aeronautical Symbols |
SAE ARP 4102/7 : 1988 | ELECTRONIC DISPLAYS |
SAE ARP 4101/2 : 1989 | PILOT VISIBILITY FROM THE FLIGHT DECK |
SAE AS8034B | Minimum Performance Standard for Airborne Multipurpose Electronic Displays |
SAE AS 425 : 1985 | NOMENCLATURE AND ABBREVIATIONS FOR USE ON THE FLIGHT DECK |
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 ARP 4102/3 : 1988 | FLIGHT DECK TIRE PRESSURE MONITORING SYSTEM (TPMS) |
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