MIL-E-6051 Revision D:1967
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
Available format(s)
PDF
Superseded date
08-04-1997
Superseded by
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Outlines requirements for systems electromagnetic compatibility, including control of the system electromagnetic environment, lightning protection, bonding and grounding. Coverage includes: system electromagnetic compatibility program; electromagnetic compatibility board; wiring and cabling; bonding and grounding; external grounds for aircraft; grounding jack installation.
| Committee |
AREA EMCS
|
| DocumentType |
Standard
|
| Pages |
23
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| MIL-HDBK-253 Base Document:1978 | GUIDANCE FOR THE DESIGN AND TEST OF SYSTEMS PROTECTED AGAINST THE EFFECTS OF ELECTROMAGNETIC ENERGY |
| MIL-STD-2156 Base Document:1983 | LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| MIL-STD-1553 Revision B:1978 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |
| JSGS-87231 Revision A:1995 | ENGINES, AIRCRAFT, TURBINE |
| MIL-M-8555 Revision C:1984 | MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
| MIL-L-6503 Revision H:1975 | LIGHTING EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATION FOR INSTALLATION OF |
| MIL-A-85055 Base Document:1979 | Avionics System Performance Specification for A-4M/AV-8 Bombing Set, Angle Rate AN/ASB-19(V) |
| MIL-STD-7080 Base Document:1994 | SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
| MIL-HDBK-11991 Base Document:1996 | DESIGN OF ELECTRICAL, ELECTRONIC, AND ELECTRO-MECHANICAL EQUIPMENT, GUIDED MISSILE AND ASSOCIATED WEAPONS SYSTEMS |
| MIL-P-85833 Base Document:1989 | PROTECTIVE ASSEMBLY, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL |
| MIL-STD-1522 Revision A:1984 | STANDARD GENERAL REQUIREMENTS FOR SAFE DESIGN AND OPERATION OF PRESSURIZED MISSILE AND SPACE SYSTEMS |
| MIL-A-23595 Revision D:1995 | AMPLIFIER, AUDIO FREQUENCY |
| MIL-D-70789 Revision A:1992 | DYNAMIC REFERENCE UNIT (DRU) |
| MIL F 85406 : 0 | FUSE SYSTEM, JOINT SERVICE ELECTRONIC BOMB FMU-139/B |
| 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)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| 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)/11(2013) : 2013 | 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 |
| MIL-HDBK-508 Base Document:1998 | WIRING AND WIRING DEVICES FOR COMBAT AND TACTICAL VEHICLES, SELECTION AND INSTALLATION OF |
| MIL-STD-339 Base Document:1987 | WIRING AND WIRING DEVICES FOR COMBAT AND TACTICAL VEHICLES, SELECTION AND INSTALLATION OF |
| 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 |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-HDBK-272 Revision A:1993 | NUCLEAR WEAPONS SYSTEMS, SAFETY DESIGN AND EVALUATION CRITERIA FOR |
| MIL-E-4158 Revision E:1973 | ELECTRONIC EQUIPMENT, GROUND GENERAL REQUIREMENTS FOR |
| MIL-HDBK-244 Revision A:1990 | GUIDE TO AIRCRAFT - STORES COMPATIBILITY |
| MIL-W-8160 Revision D:1961 | WIRING, GUIDED MISSILE, INSTALLATION OF, GENERAL SPECIFICATION FOR |
| MIL STD 1763 : A | AIRCRAFT STORES CERTIFICATION PROCEDURES |
| MIL-STD-877 Base Document:1968 | ANTENNA SUBSYSTEMS, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF |
| MIL-B-81365 Base Document:1966 | BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
| MIL-E-7080 Revision B:1962 | ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
| MIL-HDBK-2097 Revision A:1997 | ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
| KKK-T-2893 Base Document:1997 | TRUCK, AMMUNITION HANDLING: STAKE AND PLATFORM BODY, 24,000 POUNDS GVW, 4 BY 2 OR 4 BY 4 |
| AAEP-03 : 2016 | BIBLIOGRAPHY ON ELECTROMAGNETIC COMPATIBILITY (EMC) |
| MIL-D-8685 Revision B:1967 | DATA AND TESTS, ENGINEERING, CONTRACT REQUIREMENTS FOR GUIDED MISSILE TARGET SYSTEMS |
| SAE AS8700 | Installation and Test of Electronic Equipment in Aircraft, General Specification for |
| BWB TL 6130-0032 : 2ED 2006 | |
| MIL-HDBK-1760 Revision A:2004 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| MIL-R-87245 Base Document:1986 | RADIO COMMUNICATION SYSTEM, AIRBORNE (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA: ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
| SAE AS4764A | Validation Methods for MIL-STD-1760 Aircraft Station Interfaces |
| MIL-D-8804 Revision B:1993 | DE-ICING SYSTEM, PNEUMATIC BOOT, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-I-8700 Revision A:1970 | INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-P-5238 Revision C:1974 | PUMP, CENTRIFUGAL, FUEL BOOSTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| NASA KSC STD E 0012 : 2013 | FACILITY GROUNDING AND LIGHTNING PROTECTION, STANDARD FOR |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| MIL-A-5999 Revision B:1973 | ANTENNA SUBSYSTEM FOR AIRCRAFT MARKER BEACON EQUIPMENT GENERAL SPECIFICATION FOR |
| NASA MSFC HDBK 670 : 1991 | GENERAL ENVIRONMENTAL TEST GUIDELINES (GETG) FOR PROTOFLIGHT INSTRUMENTS AND EXPERIMENTS |
| MIL-I-8671 Revision D:1994 | INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
| MIL-STD-188-124 Revision B:1992 | GROUNDING BONDING AND SHIELDING FOR COMMON LONG HAUL TACTICAL COMMUNICATION SYSTEMS INCLUDING GROUND BASED COMMUNICATIONS ELECTRONICS FACILITIES & EQUIPMENTS |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| MIL-HDBK-1763 Base Document:1998 | AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
| MIL-T-18232 Revision B:1968 | TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
| JSSG-2010-12 Base Document:1998 | Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
| MIL-STD-188-310 Revision A:1980 | SUBSYSTEM DESIGN AND ENGINEERING STANDARDS FOR TECHNICAL CONTROL FACILITIES |
| SAE AS4270A | Validation Methods for MIL-STD-1760 Mission Stores |
| DEFSTAN 00-69(PT2)/1(1998) : 1998 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM - PART 2: DESIGN PRINCIPLES AND PRACTICES FOR, AND GUIDE TO, THE IMPLEMENTATION OF THE AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| MIL-STD-1512 Base Document:1972 | ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS |
| DOD STD 1788 : LATEST | AVIONICS INTERFACE DESIGN STANDARD (METRIC) |
| MIL-F-8615 Revision D:1976 | FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
| SAE ARP4729A | Document for 270 Voltage Direct Current (270 V DC) System |
| MIL-G-58103 Base Document:1979 | GRIP ASSEMBLY, CYCLIC CONTROLLER, HELICOPTER |
| MIL-R-29583 Base Document:1992 | RADIO SET |
| MIL-L-85762 Revision A:1988 | LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
| MIL-D-18300 Revision H:1993 | DESIGN EXAMINATIONS, ENGINEERING AVIONIC SYSTEMS/EQUIPMENT GENERAL REQUIREMENTS FOR |
| MIL-D-8708 Revision C:1991 | DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
| SAE AS47641A | Validation Methods for MIL-STD-1760B Aircraft Station Interfaces |
| MIL-I-8672 Revision B:1969 | INSTALLATION AND TEST OF AIRCRAFT PYROTECHNIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR [ASG] |
| MIL-T-7743 Revision F:1993 | TESTING, STORE SUSPENSION AND RELEASE EQUIPMENT, GENERAL SPECIFICATION FOR |
| ANEP-45 : 0 | |
| EIA EMCB1-1 : 1993 | HISTORICAL RATIONALE FOR MILITARY EMI LIMITS |
| EIA IS 647 : 1996 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE EMISSIONS AND SUSCEPTIBILITY CHARACTERISTICS OF EQUIPMENT INTENDED TO OPERATE IN SEVERE ELECTROMAGNETIC ENVIRONMENTS |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| MIL-C-12889 Revision A:1957 | CAPACITORS, BY-PASS, RADIO-INTERFERENCE REDUCTION, PAPER DIELECTRIC, AC AND DC, (HERMETICALLY SEALED IN METALLIC CASES) GENERAL SPECIFICATION FOR |
| MIL-STD-831 Base Document:1963 | TEST REPORTS, PREPARATION OF |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| MIL C 5 : G | CAPACITOR, FIXED, MICA DIELECTRIC, GENERAL SPECIFICATION FOR |
| MS33645 Revision C:1977 | RECEPTACLE, GROUNDING, INSTALLATION OF |
| MS25384 Revision C:1973 | ELECTROSTATIC DISCHARGER JUMPER, FUEL NOZZLE TO AIRCRAFT |
| MIL-STD-462 Revision D:1993 | MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS |
| MIL C 11693 : C | CAPACITOR, FEED THROUGH, RADIO INTERFERENCE REDUCTION, DC (HERMETICALLY SEALED IN METALLIC CASE), STYLE CZ20 |
| MIL-B-5087 Revision B:1964 | BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
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