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MIL-E-6051 Revision D:1967
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
08-04-1997
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Superseded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 AS 8700 : 1999 | 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 AS 4764 : 2017 | 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 AS 4270 : 2017 | 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 ARP 4729 : 2017 | 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 AS 47641 : 2017 | 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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