MIL D 87213 : 0
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
DISPLAYS/OPTICALLY GENERATED REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503
Withdrawn date
27-07-2023
Publisher
Describes electronically generated displays for airborne use, including Head Up Displays and Multi-Function Displays and displays for FLIR, TV, and Radar video, and the related electronic display generation equipment.
| DocumentType |
Standard
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
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| DEFSTAN 00-970(PT1)SEC6/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/14(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| 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)/7(2011) : 2011 | 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)/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(PT1)SEC6/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT7)SEC2/SUPP6/5(2015) : INTERIM | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
| DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
| DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| DEFSTAN 00-970(PT1)SEC6/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| 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 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-STD-884 Revision C:1975 | ELECTRONICALLY OR OPTICALLY GENERATED DISPLAYS FOR AIRCRAFT CONTROL AND COMBAT CUE INFORMATION |
| 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 H 83282 : C | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, AIRCRAFT, METRIC, NATO CODE NUMBER H 537 |
| 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-1472 Revision G:2012 | HUMAN ENGINEERING |
| MIL T 83133 : D | TURBINE FUELS, AVIATION, KEROSENE TYPES, NATO F-34 (JP-8) AND NATO F-35 |
| MIL-A-8243 Revision D:1985 | ANTI-ICING AND DEICING-DEFROSTING FLUIDS |
| MIL-P-15024-5 Base Document:1971 | PLATE, IDENTIFICATION |
| MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
| MIL-STD-462 Revision D:1993 | MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS |
| MIL-B-5087 Revision B:1964 | BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
| MIL-N-7513 Revision F:1980 | NOMENCLATURE ASSIGNMENT, CONTRACTORS METHOD FOR OBTAINING |
| 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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