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MIL-HDBK-87213 Revision A:2005

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

Electronically / Optically Generated Airborne Displays

Available format(s)

PDF

Superseded date

02-03-2020

Language(s)

English

Published date

08-02-2005

€17.95
Excluding VAT

FORWARD
1 SCOPE
  1.1 Scope
  1.2 Use
  1.3 Structure
  1.4 Deviation
  1.5 Responsible engineering office
2 APPLICABLE DOCUMENTS
  2.1 Government documents
      2.1.1 Specifications, standards, and handbooks
      2.1.2 Other Government documents, drawings, and
             publications
  2.2 Non-Government standards and other publications
3 REQUIREMENTS
  3.1 Controls and displays segment
      3.1.1 Primary flight displays (PFD)
      3.1.2 Situation displays
      3.1.3 Head up or helmet mounted displays (HUD/HMD)
      3.1.4 Vehicle management subsystem (VMS) displays
      3.1.5 Warning, caution, and advisory (WCA) displays
      3.1.6 Avionic subsystem control and data entry
      3.1.7 Video recording
  3.2 Characteristics of subordinate elements
      3.2.1 Performance environments
      3.2.2 System interface
      3.2.3 Reliability
      3.2.4 Maintainability
      3.2.5 Weight
      3.2.6 Volume
  3.3 Design and construction
      3.3.1 Environmental integrity
      3.3.2 Safety
      3.3.3 Human engineering
4 VERIFICATIONS
  4.1 Verification of controls and displays segment
      4.1.1 Verification of primary flight displays
      4.1.2 Verification of situation displays
      4.1.3 Verification of HUD/HMD
      4.1.4 Verification of vehicle management subsystem (VMS)
             displays
      4.1.5 Verification of warning, caution, and advisory (WCA)
             displays
      4.1.6 Verification of avionic subsystem control and data
             entry
      4.1.7 Verification of video recording
  4.2 Verification of characteristics of subordinate elements
      4.2.1 Verification of performance environments
      4.2.2 Verification of system interface
      4.2.3 Verification of reliability
      4.2.4 Maintainability verification
      4.2.5 Verification of weight
      4.2.6 Verification of volume
  4.3 Verification of design and construction
      4.3.1 Verification of environmental integrity
      4.3.2 Verification of safety
      4.3.3 Human engineering verification
5 DEFINITIONS AND ACRONYMS
  5.1 Definitions
      5.1.1 Average luminance
      5.1.2 Built-in tests (BIT)
      5.1.3 Conformal
      5.1.4 Contrast definitions
      5.1.5 Diffuse reflection
      5.1.6 Display element
      5.1.7 Fill factor
      5.1.8 Gray shade
      5.1.9 Gray level
      5.1.10 Line pair
      5.1.11 Line rate
      5.1.12 Lines (of resolution)
      5.1.13 Malfunctions
      5.1.14 Minutes and milliradians
      5.1.15 Occlude
      5.1.16 Out-of-tolerance condition
      5.1.17 Pixel
      5.1.18 Self-tests
      5.1.19 Specular reflection
      5.1.20 Quantities of light
  5.2 Acronyms
6 NOTES
  6.1 Intended use
  6.2 Subject term (key word) listing
  6.3 International Standardization Agreements
  6.4 Changes from previous issue
APPENDIX
A.1. Acceleration display
A.2. Attitude display
A.3. Attitude director indicator (ADI)
A.4. Clock/timer
A.5. Engine pressure ratio system (EPR)
A.6. Engine temperature display
A.7. Flight director system (FDS)
A.8. Rate of fuel flow system
A.9. Fuel savings advisory system (FSAS)
A.10. Fuel quantity system
A.11. Horizontal situation indicator (HSI)
A.12. Hydraulic pressure indicator and sensor
A.13. Magnetic compass
A.14. Engine oil quantity indicating system
A.15. Oil pressure indicating system
A.16. Position indicating system
A.17. Tachometer indicator system
A.18. Thrust computing system (TCS)
A.19. Turn and slip display
A.20. Warning system
FIGURES
TABLES

Describes the sample specification paragraphs, rationale, guidance, and lessons learned that are useful in the development of the primary flight displays and mission avionics controls and displays subsystem for an aircraft.

DevelopmentNote
Supersedes AFGS 87213 (04/2003)
DocumentType
Standard
Pages
196
PublisherName
US Military Specs/Standards/Handbooks
Status
Superseded
SupersededBy
Supersedes

This handbook provides sample specification paragraphs, rationale, guidance, and lessons learned that are useful in the development of the primary flight displays and mission avionics controls and displays subsystem for an aircraft. This includes head-up Displays (HUDs), helmet-mounted displays (HMDs), and multi-function displays (MFDs), used for presentation of graphics as well as display of television (TV), forward looking infrared (FLIR), radar video, and the associated electronic display generation equipment. Rationale paragraphs explain the reason for specifying each parameter. Guidance paragraphs explain what values are normally used and why. Lessons learned paragraphs serve as a historical information repository for this technical area.

SAE AS8055A Minimum Performance Standard for Airborne Head Up Display (HUD)
SAE J1757/1_201505 Standard Metrology for Vehicular Displays
DEFSTAN 00-970(PT0)/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/17(2016) : 2016 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/14(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/15(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/13(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/16(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
SAE ARP5287 Optical Measurement Procedures for Airborne Head Up Display (HUD)
SAE ARP 4260 : 2014 PHOTOMETRIC AND COLORIMETRIC MEASUREMENT PROCEDURES FOR AIRBORNE ELECTRONIC FLAT PANEL DISPLAYS
ADS-65-HDBK : 2004 AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIRWORTHINESS QUALIFICATION AND VERIFICATION GUIDANCE FOR ELECTRO-OPTICAL AND SENSOR SYSTEMS

MIL-PRF-1 Revision N:2011 ELECTRON TUBES - GENERAL SPECIFICATION FOR
MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
MIL-HDBK-87244 Base Document:1995 AVIONICS/ELECTRONICS INTEGRITY
MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
MIL-STD-1787 Revision B:1996 AIRCRAFT DISPLAY SYMBOLOGY
JSSG-2010 Base Document:1998 Crew Systems
MIL-STD-411 Revision F:1997 AIRCREW STATION ALERTING SYSTEMS
MIL-HDBK-1553 Revision A:1988 Multiplex Application Handbook
MIL-L-85762 Revision A:1988 LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION
MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
JSSG-2010-11 Base Document:1998 Crew Systems Emergency Egress Handbook
MIL-STD-3009 Base Document:2001 LIGHTING, AIRCRAFT, NIGHT VISION IMAGING SYSTEM (NVIS) COMPATIBLE
MIL-STD-1472 Revision G:2012 HUMAN ENGINEERING
FAA AC 25.1309-1 : 0 SYSTEM DESIGN AND ANALYSIS
SMPTE ST 170 : 2004 TELEVISION - COMPOSITE ANALOG VIDEO SIGNAL - NTSC FOR STUDIO APPLICATIONS
MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
SAE ARP 4256 : 2001 DESIGN OBJECTIVES FOR LIQUID CRYSTAL DISPLAYS FOR PART 25 (TRANSPORT) AIRCRAFT
SAE ARP1782B Photometric and Colorimetric Measurement Procedures for Airborne Direct View CRT Displays
JSSG-2010-5 Base Document:1998 Crew Systems Aircraft Lighting Handbook
STANAG 3350 : 0 ANALOGUE VIDEO STANDARD FOR AIRCRAFT SYSTEM APPLICATIONS
MIL-STD-1553 Revision B:1978 DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA

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