AFGS-87213 Revision B:1993
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED
27-02-1997
1 SCOPE
1.1 Scope
1.2 Use
1.2.1 Structure
1.2.2 Instructional handbook
1.3 Deviation
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
3.1 Item definition
3.1.1 Item diagrams
3.1.2 Interface definition
3.2 Characteristics
3.2.1 Performance
3.2.2 Physical characteristics
3.2.3 Reliability
3.2.4 Maintainability
3.2.5 Product integrity
3.3 Design and construction
3.3.1 (Reserved)
3.3.2 Electromagnetic compatibility
3.3.3 Nameplates and product marking
3.3.4 Explosive decompression
3.3.5 Interchangeability
3.3.6 Safety
3.3.7 Human engineering
4 VERIFICATIONS
4.1 General
4.1.1 Verification of diagrams
4.1.2 Verification of system interface
4.2 Verification of characteristics
4.2.1 Verification of performance
4.2.2 Verification of weight
4.2.3 Reliability verification
4.2.4 Maintainability verification
4.2.5 Verification of product integrity
4.3 Verification of design and construction
4.3.1 (Reserved)
4.3.2 (Reserved)
4.3.3 Verification of nameplates and product marking
4.3.4 Verification of explosive decompression
4.3.5 Verification of interchangeability
4.3.6 Verification of safety
4.3.7 Human engineering verification
5 PACKAGING
5.1 Packaging
6 NOTES
6.1 Intended use
6.2 Definitions
6.3 Quantities of light
6.3.1 Candela per square meter (cd/m[2])
6.3.2 Lumens per square meter (1m/m[2])
6.3.3 Candelas (cd)
6.3.4 Lumens (lm)
6.4 Responsible engineering office
6.5 International standardization agreements
6.6 Subject term (key word) listing
6.7 Changes from previous issue
APPENDIX
Establishes development requirements for electronically generated displays for airborne use including head-up displays (HUDs), helmet-mounted displays (HMDs), and multi-function displays (MFDs), including displays for TV, FLIR, and radar video, and the associated electronic display generation equipment.
Committee |
FSC 6610
|
DevelopmentNote |
B NOTICE 1 - Notice of Change B NOTICE 2 - Notice of Cancellation/Superseded by MIL HDBK 87213 (04/2003)
|
DocumentType |
Standard
|
Pages |
142
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
Superseded
|
SupersededBy |
A-A-58055 Base Document:1996 | Indicator, Attitude, Three Inch, Solid State Self-Contained |
MIL-E-87235 Base Document:1985 | EMERGENCY ESCAPE, AIRCRAFT (REQUEST FOR ISSUE MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
MIL L 7808 : K (1) | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
MIL-STD-883 Revision K:2016 | TEST METHOD STANDARD - MICROCIRCUITS |
MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
MIL-STD-1787 Revision B:1996 | AIRCRAFT DISPLAY SYMBOLOGY |
MIL T 5624 : R | TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5 |
MIL P 7788 : F | PANEL, INFORMATION INTEGRALLY ILLUMINATED |
MIL-M-38510 Revision J:1991 | MICROCIRCUITS, SPECIFICATION FOR |
MIL E 5400 : T | ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
MIL-C-6781 Revision B:1960 | CONTROL PANEL, AIRCRAFT EQUIPMENT, RACK OR CONSOLE MOUNTED |
MIL C 83723 : E | CONNECTORS, ELECTRICAL (CIRCULAR, ENVIRONMENT RESISTING) RECEPTACLES AND PLUGS GENERAL SPECIFICATION FOR |
MIL-STD-1515 Revision A:1978 | FASTENER SYSTEMS FOR AEROSPACE APPLICATION |
MIL-L-85762 Revision A:1988 | LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
MIL H 83282 : C | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, AIRCRAFT, METRIC, NATO CODE NUMBER H 537 |
MIL STD 1800 : A NOTICE 1 | HUMAN ENGINEERING PERFORMANCE REQUIREMENTS FOR SYSTEMS |
MIL A 87244 : A NOTICE 1 | AVIONICS ELECTRONICS INTEGRITY PROGRAM REQUIREMENTS |
AFGS 87240 : A NOTICE 1 | LIGHTING EQUIPMENT, AIRBORNE, INTERIOR AND EXTERIOR |
MIL-STD-882 Revision E:2012 | System Safety |
MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
MIL-STD-471 Revision A:1973 | MAINTAINABILITY DEMONSTRATION |
MIL-STD-1295 Revision A:1984 | HUMAN FACTORS ENGINEERING DESIGN CRITERIA FOR HELICOPTER COCKPIT ELECTRO-OPTICAL DISPLAY SYMBOLOGY |
MIL S 19500 : J | SEMICONDUCTOR DEVICES, GENERAL SPECIFICATION FOR |
MIL STD 1799 : NOTICE 1 | |
MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
MIL T 83133 : D | TURBINE FUELS, AVIATION, KEROSENE TYPES, NATO F-34 (JP-8) AND NATO F-35 |
ARINC 725 : 1979 SUPP 2 | ELECTRONIC FLIGHT INSTRUMENTS (EFI) |
MIL-A-8243 Revision D:1985 | ANTI-ICING AND DEICING-DEFROSTING FLUIDS |
AFGS-87266 Base Document:1992 | AIRCRAFT COCKPIT TRANSPARENCY SYSTEM |
MIL-P-15024-5 Base Document:1971 | PLATE, IDENTIFICATION |
MIL STD 1801 : NOTICE 1 | |
MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
MIL-STD-462 Revision D:1993 | MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS |
SAE AS 8034 : 2011 | MINIMUM PERFORMANCE STANDARD FOR AIRBORNE MULTIPURPOSE ELECTRONIC DISPLAYS |
MIL-B-5087 Revision B:1964 | BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
SAE ARP 4256 : 2001 | DESIGN OBJECTIVES FOR LIQUID CRYSTAL DISPLAYS FOR PART 25 (TRANSPORT) AIRCRAFT |
MIL-N-7513 Revision F:1980 | NOMENCLATURE ASSIGNMENT, CONTRACTORS METHOD FOR OBTAINING |
SAE ARP 1782 : 2012 | PHOTOMETRIC AND COLORMETRIC MEASUREMENT PROCEDURES FOR AIRBORNE DIRECT VIEW CRT DISPLAYS |
MIL-STD-781 Revision D:1986 | RELIABILITY TESTING FOR ENGINEERING DEVELOPMENT, QUALIFICATION AND PRODUCTION |
MIL-STD-1553 Revision B:1978 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |
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