MIL C 83413 : A
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING, GENERAL SPECIFICATION FOR
Available format(s)
PDF
Publisher
Superseded date
22-09-2005
Superseded by
$34.82
Including GST where applicable
Requirements for aircraft grounding connectors/assemblies, electrical.
| Committee |
FSC 5935
|
| DocumentType |
Standard
|
| Pages |
22
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| MIL-STD-7080 Base Document:1994 | Selection and Installation of Aircraft Electric 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)/14(2014) : 2014 | 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)/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-T-62032 Revision H:1991 | TRUCKS, TANK: FUEL SERVICING AND AIRCRAFT FUEL SERVICING, 1,000 TO 4,000 GALLON, DIESEL AND GASOLINE ENGINE DRIVEN, 16,000 TO 50,000 POUNDS GVW, 4X2, 4X4, 6X4, AND 6X6, MODIFIED COMMERCIAL |
| MIL-PRF-38170 Revision H:2000 | Tank, Mobile Storage, Liquid Oxygen TMU-27/M |
| DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| MIL-STD-188-124 Revision B:1992 | Grounding, Bonding and Shielding for Common Long Haul/TacticalCommunication Systems Including Ground Based Communications-Electronics Facilities and Equipments |
| MIL-D-8708 Revision C:1991 | Demonstration: Aircraft Weapon Systems, General Specification for |
| ISO 46:1973 | Aircraft — Fuel nozzle grounding plugs and sockets |
| MIL C 55330 : B | CONNECTORS, PREPARATION FOR DELIVERY OF |
| MIL-STD-45662 Revision A:1988 | Calibration Systems Requirements (Refer to ISO-10012-1 and ANSI-Z540-1 or Comparable Standards as Alternatives to MIL-STD-45662) |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| SAE AMS5032G | Wire, Steel 0.18 - 0.23C (SAE 1020) Annealed |
| MIL W 83420 : E | WIRE, ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL |
| FF-S-200 Revision B:2004 | Setscrews: Hexagon Socket and Spline Socket, Headless |
| MIL-STD-1344 Revision A:1977 | Test Methods for Electrical Connectors (S/S by EIA364, See Notice 6 for Individual Test Method Replacement) |
| MIL-T-7928 Revision G:1976 | Terminals, Lug: Splices, Conductor: Crimp Style, Copper, General Specification for (S/S BY SAE-AS7928) |
| MS51963 Revision C:1972 | SETSCREW-HEXAGON SOCKET, CUP POINT, ALLOY STEEL, CADMIUM PLATED, UNC-3A, PLAIN AND SELF-LOCKING (S/S BY NASM51963) |
| MS20615 Revision G:1995 | RIVET, SOLID-UNIVERSAL HEAD, BRASS, COPPER, NICKEL-COPPER ALLOY (S/S BY NASM20615) |
| QQ-W-470 Revision B:1965 | Wire, Steel, Carbon, Spring, Music (See Notice of Cancellation for Replacement Information) |
| MIL-STD-202 Revision H:2015 | ELECTRONIC AND ELECTRICAL COMPONENT PARTS |
| SAE AMS6274R | 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 |
| MIL-STD-105 Revision E:1989 | Sampling Procedures and Tables for Inspection by Attributes (See Notice 3 for Replacement Information) |
| ASTM A 304 : 2016 : REDLINE | Standard Specification for Carbon and Alloy Steel Bars Subject to End-Quench Hardenability Requirements |
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