MIL-DTL-83413 Revision C:2012
Current
Current
The latest, up-to-date edition.
CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING, GENERAL SPECIFICATION FOR
Amended by
Available format(s)
PDF
Publisher
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
Describes the electrical aircraft grounding connectors and grounding assemblies, including plugs, receptacles, grounding clamp, connectors, jumper cable assemblies, and other accessories.
| Committee |
FSC 5935
|
| DevelopmentNote |
Supersedes MIL C 83413 (A). (10/2005)
|
| DocumentType |
Standard
|
| Pages |
40
|
| ProductNote |
New child AMD 2 2019 now added
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
| MIL-DTL-83413-5 Revision C:2013 | CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING: RECEPTACLES, ONE PIECE |
| MIL-DTL-83413-12 Revision A:2015 | Connectors and Assemblies, Electrical, Aircraft Grounding: Grounding Clamp Connector for Types I and III Grounding Assemblies, Stainless Steel Clip, Electrical |
| 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)/14(2014) : 2014 | 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)/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)/11(2013) : 2013 | 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)/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-PRF-32020 Revision B:2011 | PROVER, LIQUID VOLUMETRIC POSITIVE DISPLACEMENT METER |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| MIL-PRF-27720 Revision G:2009 | TANK, STORAGE, LIQUID OXYGEN/LIQUID NITROGEN, TMU-24/E |
| MIL-DTL-83413-3 Revision D:2014 | Connectors and Assemblies, Electrical, Aircraft Grounding, Type III Grounding Assembly, Discharger, Electrostatic |
| MIL-HDBK-274 Revision A:2011 | ELECTRICAL GROUNDING FOR AIRCRAFT SAFETY |
| SAE AIR 4004 : 2015 | GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR |
| MIL-DTL-83413-7 Revision F:2015 | Connectors and Assemblies, Electrical, Aircraft Grounding: Grounding Clamp Connector for Types I and III Grounding Assemblies, Aluminum Clip, Electrical |
| MIL-DTL-83413-4 Revision E:2014 | CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING: PLUGS, FOR TYPES 1 AND 2 GROUNDING ASSEMBLIES |
| MIL-DTL-83413-1 Revision D:2010 | Connectors and Assemblies, Electrical, Aircraft Grounding: Type I Grounding Assembly, Discharger, Electrostatic |
| MIL-DTL-83413-2 Revision C:2010 | Connectors and Assemblies, Electrical, Aircraft Grounding: Type II Grounding Assembly, Discharger, Electrostatic |
| MIL-DTL-83413-10 Revision C:2010 | Connectors and Assemblies, Electrical, Aircraft Grounding: Jumper Cable Assembly, Aircraft to Fuel Nozzle, Discharger, Electrostatic |
| MIL-DTL-83413-6 Revision C:2008 | CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING: RECEPTACLES, TWO PIECE, WITH INSERTS AND HOUSINGS |
| MIL-DTL-83413-8 Revision E:2015 | CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING: TYPE 4 JUMPER CABLE ASSEMBLY, LEAD, ELECTRICAL |
| MIL-STD-202-211 Base Document:2015 | METHOD 211, TERMINAL STRENGTH |
| ASTM B 733 : 2015 : REDLINE | Standard Specification for Autocatalytic (Electroless) Nickel-Phosphorus Coatings on Metal |
| ISO 46:1973 | Aircraft — Fuel nozzle grounding plugs and sockets |
| NASM171401-171900:2014 | PIN, SPRING, CORROSION RESISTANT STEEL |
| MIL-DTL-83420 Revision P:2017 | WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| SAE AMS 5032 : 2013 | WIRE, STEEL, 0.18-0.23C (SAE 1020), ANNEALED |
| SAE AS 7928 : 2011 | TERMINALS, LUG: SPLICES, CONDUCTOR: CRIMP STYLE, COPPER, GENERAL SPECIFICATION FOR |
| FF-S-200 Revision B:2004 | SETSCREWS: HEXAGON SOCKET AND SPLINE SOCKET, HEADLESS |
| NASM51021:2017 | SETSCREW, HEXAGON SOCKET, CUP POINT, CORROSION-RESISTING STEEL, PASSIVATED, UNC-3A, PLAIN AND SELF-LOCKING |
| NASM 20615 : 2003 | RIVET, SOLID, UNIVERSAL HEAD, BRASS, COPPER, NICKEL-COPPER ALLOY |
| STANAG 3632 : 0 | AIRCRAFT AND GROUND SUPPORT EQUIPMENT ELECTRICAL CONNECTIONS FOR STATIC GROUNDING |
| MIL-STD-202-110 Base Document:2015 | METHOD 110, SAND AND DUST |
| SAE AMS 6274 : 2016 | STEEL BARS, FORGINGS AND TUBING, 0.50CR - 0.55NI - 0.20MO (0.18 - 0.23C) (SAE 8620) |
| MIL-STD-1285 Revision D:2004 | MARKING OF ELECTRICAL AND ELECTRONIC PARTS |
| FED-STD-H28 Revision A:1994 | Screw-Thread Standards for Federal Services |
| ASTM A 304 : 2016 : REDLINE | Standard Specification for Carbon and Alloy Steel Bars Subject to End-Quench Hardenability Requirements |
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