SAE AS50881F
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Wiring Aerospace Vehicle
Available format(s)
Hardcopy , PDF
Superseded date
08-08-2019
Superseded by
Language(s)
English
Published date
29-05-2015
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.
FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE AND DESIGN
CONFORMANCE PROVISIONS
5. PACKAGING
6. NOTES
7. NOTES
APPENDIX A - OPEN OR PROTECTED HARNESSES
APPENDIX B - SIGNIFICANT WIRE IDENTIFICATION
APPENDIX C - NON-SIGNIFICANT WIRE IDENTIFICATION
INDEX
REFERENCED DOCUMENTS INDEX
Specifies all aspects in electrical wire interconnection systems (EWIS) from the selection through installation of wiring and wiring devices and optical cabling and termination devices used in aerospace vehicles.
| DevelopmentNote |
Supersedes MIL W 5088. (06/2000)
|
| DocumentType |
Standard
|
| Pages |
91
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
This specification covers all aspects in electrical wire interconnection systems (EWIS) from the selection through installation of wiring and wiring devices and optical cabling and termination devices used in aerospace vehicles. Aerospace vehicles include manned and unmanned airplanes, helicopters, lighter-than-air vehicles, missiles and external pods.
| SAE AS 4372 : 2014 | PERFORMANCE REQUIREMENTS FOR WIRE, ELECTRIC, INSULATED COPPER OR COPPER ALLOY |
| SAE AS60491 | Sleeve, Protection, For Cable and Harness Protection |
| SAE AIR 6127 : 2017 | MANAGING HIGHER VOLTAGES IN AEROSPACE ELECTRICAL SYSTEMS |
| SAE AIR 5451 : 2017 | A GUIDE TO LANDING GEAR SYSTEM INTEGRATION |
| SAE AS6129 | AS6129: Interface Standard, Airborne EO/IR Systems, Electrical |
| SAE AIR5558 | Ultraviolet (UV) Laser Marking Performance of Aerospace Wire Constructions |
| MIL-HDBK-863 Revision A:2015 | WIRING DATA AND SYSTEM SCHEMATIC DIAGRAMS PREPARATION OF |
| MIL-DTL-85052-14 Base Document:2017 | Clamp, Loop, Stainless Steel, 500 Degrees F, Silicone Rubber, Fabric Reinforced |
| FAA AC 25.1701-1 : 2007 | CERTIFICATION OF ELECTRICAL WIRING INTERCONNECTION SYSTEMS ON TRANSPORT CATEGORY AIRPLANES |
| MIL-STD-3001-1 Revision A:2014 | PREPARATION OF DIGITAL TECHNICAL INFORMATION FOR MULTI-OUTPUT PRESENTATION OF TECHNICAL MANUALS (PART 1 OF 8 PARTS) |
| SAE AS7768A | Light, Desk, Aircraft |
| SAE ARP94910 | Aerospace - Vehicle Management Systems - Flight Control Design, Installation and Test of, Military Unmanned Aircraft, Specification Guide For |
| SAE AS23190C | Wiring, Positioning, and Support Accessories |
| ARINC 791-1 : 2014 | MARK 1 AVIATION KU-BAND AND KA-BAND SATELLITE COMMUNICATION SYSTEM - PART 1: PHYSICAL INSTALLATION AND AIRCRAFT INTERFACES |
| SAE AIR4165A | General Requirements for Powered Drive Units (PDUs) in Aircraft Cargo Systems |
| SAE AS95234A | Connectors, Electrical, Reverse Bayonet, General Specification for |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-STD-2088 Revision B:2007 | BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT |
| 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)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 61-12(PT0)/3(2011) : 2011 | WIRES, CORDS AND CABLES ELECTRICAL METRIC UNITS - PART 0: GENERAL REQUIREMENTS AND TEST METHODS GENERIC SPECIFICATION |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-STD-1678-1 Revision D:2016 | FIBER OPTIC CABLING SYSTEMS REQUIREMENTS AND MEASUREMENTS - PART 1: DESIGN, INSTALLATION AND MAINTENANCE REQUIREMENTS (PART 1 OF 6 PARTS) |
| 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)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-DTL-9419 Revision H:2016 | Switch, Toggle, Momentary, Four-Position on, Center off, General Specification for |
| 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 |
| MIL-STD-1353 Revision C:2014 | ELECTRICAL CONNECTORS, PLUG-IN SOCKETS AND ASSOCIATED HARDWARE, SELECTION AND USE OF |
| MIL-PRF-7115 Revision G:2012 | CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR |
| 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)/16(2015) : 2015 | 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 STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
| MIL-DTL-24317 Revision B:2010 | SWITCHES, MULTISTATION, PUSHBUTTON, ILLUMINATED AND NON-ILLUMINATED), GENERAL SPECIFICATION FOR |
| SAE AIR5575A | Hot Stamp Wire Marking Concerns for Aerospace Vehicle Applications |
| AFGS-87219 Revision B:2012 | ELECTRICAL POWER SYSTEMS, AIRCRAFT |
| SAE ARP5369B | Guidelines for Wire Identification Marking Using the Hot Stamp Process |
| MIL-PRF-8805-8 Revision H:2012 | Switches, Sensitive, SPDT, Leaf Actuator, Low Level to 4 Amperes, Hermetic Seal |
| SAE ARP5614 | Guidelines for Harness Critical Clamp Locator Marker Installation on Electrical Cable Assemblies |
| MIL-STD-1587 Revision D:2017 | MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
| MIL-DTL-85052-5 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 275 DEGREES F, ETHYLENE PROPYLENE |
| SAE AS 5942 : 2014 | MARKING OF ELECTRICAL INSULATING MATERIALS |
| SAE AIR38B | Guide for the Design of Threaded Screw or Stud Type Electrical Equipment Terminations |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| MIL-DTL-85052-10 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 275 DEGREES F, NITRILE BUTADIENE RUBBER FUEL AND PETROLEUM BASED HYDRAULIC FLUID RESISTANT |
| MIL-DTL-85052-6 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 400 DEGREES F, FLUOROSILICONE |
| MIL-DTL-85052-12 Base Document:2017 | Clamp, Loop, Stainless Steel, 400 Degrees F, Fluorosilicone |
| MIL-DTL-85052-11 Base Document:2017 | Clamp, Loop, Stainless Steel, 275 Degrees F, Side Lock, Ethylene Propylene |
| SAE AS22759C | Wire, Electrical, Fluoropolymer-Insulated, Copper or Copper Alloy |
| MIL-DTL-85052-8 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 500 DEGREES F, SILICONE RUBBER, FABRIC REINFORCED |
| SAE ARP4404C | Aircraft Electrical Installations |
| SAE ARP 4404 : 2013 | AIRCRAFT ELECTRICAL INSTALLATIONS |
| SAE AS95234 | Connectors, Electrical, Reverse Bayonet, General Specification For |
| GEIA STD 0008 : 2011 | DERATING OF ELECTRONIC COMPONENTS |
| IPC HDBK 630 : 0 | GUIDELINES FOR DESIGN, MANUFACTURE, INSPECTION AND TESTING OF ELECTRONIC ENCLOSURES ASSEMBLY |
| ARINC 791P2-1 : 2014 | MARK I AVIATION KU-BAND AND KA-BAND SATELLITE COMMUNICATION SYSTEM - PART 2: ELECTRICAL INTERFACES AND FUNCTIONAL EQUIPMENT DESCRIPTION |
| MIL-DTL-9490 Revision E:2008 | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE AS5649 | Wire and Cable Marking Process, UV Laser |
| MIL-DTL-85052-9 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 550 DEGREES F, POLY-TETRAFLUOROETHYLENE (PTFE) |
| MIL-HDBK-522 Revision A:2016 | GUIDELINES FOR INSPECTION OF AIRCRAFT ELECTRICAL WIRING INTERCONNECT SYSTEMS |
| MIL-PRF-7032 Revision H:2010 | INVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-STD-1289 Revision D:2003 | AIRBORNE STORES GROUND FIT AND COMPATIBILITY, REQUIREMENTS |
| MIL-HDBK-1646 Base Document:2016 | Selectionof Electrical Contacts, Connectors and Associated Servicing Tools |
| MIL-DTL-85052-15 Base Document:2017 | Clamp, Loop, Stainless Steel, 550 Degrees F, Poly-Tetrafluoroethylene (PTFE) |
| SAE AS85485B | Cable, Electric, Filter Line, Radio Frequency Absorptive |
| SAE AS12500 | Corrosion Prevention and Deterioration Control in Electronic Components and Assemblies |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| MIL-DTL-6852 Revision C:2014 | SPLICE, CONDUCTOR, ELECTRIC, DISCONNECT, GENERAL SPECIFICATION FOR |
| MIL-DTL-85052-13 Base Document:2017 | Clamp, Loop, Stainless Steel, 212 Degrees F, Chloroprene |
| MIL-DTL-7627 Revision G:2010 | INDICATOR, TURN AND SLIP, 28 V DC |
| DEFSTAN 61-5(PT6)/6(2009) : 2009 | NOMINAL 12 V AND 24 V DC ELECTRICAL SYSTEMS IN MILITARY PLATFORMS |
| MIL-DTL-85052-16 Base Document:2017 | Clamp, Loop, Stainless Steel, 275 Degrees Fahrenheit, Nitrile Butadiene Rubber Fuel and Petroleum Based Hydraulic Fluid Resistant |
| SAE AS94900 | Aerospace - Flight Control Systems - Design, Installation and Test of Piloted Military Aircraft, General Specification For |
| STANAG 3347 : 2014 | IDENTIFICATION OF AIRCRAFT ELECTRICAL CIRCUITS |
| MIL-DTL-85052-7 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 212 DEGREES F, CHLOROPRENE |
| SAE ARP5794 | Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard |
| SAE AIR 4004 : 2015 | GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR |
| SAE AS81703A | Connectors, Electric, Circular, Miniature, Rack and Panel or Push-Pull Coupling, Environment Resisting |
| SAE AIR 1329C : 2014 | ELECTRICAL CONNECTORS AND WIRING, COMPATIBILITY OF |
| SAE AS81714B | Terminal Junction System (TJS), Environment Resistant General Specification For |
| MIL-STD-1568 Revision D:2015 | Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
| SAE AMSDTL23053/5A | Insulation Sleeving, Electrical, Heat Shrinkable, Polyolefin, Flexible, Crosslinked |
| SAE AS4373E | Test Methods for Insulated Electric Wire |
| MIL-I-3190 Revision F:1991 | INSULATION SLEEVING, ELECTRICAL, FLEXIBLE, COATED, GENERAL SPECIFICATION FOR |
| SAE AS83519C | Shield Termination, Solder Style, Insulated, Heat-Shrinkable, Environment Resistant General Specification For |
| SAE AIR5558 | Ultraviolet (UV) Laser Marking Performance of Aerospace Wire Constructions |
| MIL-M-24041 Revision C:1981 | MOLDING AND POTTING COMPOUND |
| SAE AS81824D | Splice, Electric, Crimp, Copper, Environment Resistant |
| MIL-DTL-25516 Revision F:2004 | CONNECTORS, ELECTRICAL, MINIATURE, COAXIAL, ENVIRONMENT RESISTANT TYPE, GENERAL SPECIFICATION FOR |
| SAE AS4536C | Safety Cable Kit Procurement Specification and Requirement for Use |
| SAE AS33731 | STRIP, MOUNTING, NUT INSULATING, FOR MS27212 TERMINAL BOARD |
| SAE AMSS8802D | Sealing Compound, Fuel Resistant, Integral Fuel Tanks and Fuel Cell Cavities |
| A-A-52082 Revision D:2009 | TAPE, LACING AND TYING, TFE-FLUOROCARBON |
| SAE AS8700 | Installation and Test of Electronic Equipment in Aircraft, General Specification for |
| SAE AS85485A | Cable, Electric, Filter Line, Radio Frequency Absorptive |
| SAE AS 25435 : 2015 | TERMINAL-LUG, CRIMP STYLE, STRAIGHT TYPE, FOR ALUMINUM AIRCRAFT WIRE, CLASS 1 |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| SAE AS25439B | SPLICE-PERMANENT CRIMP STYLE, 2 WAY TYPE FOR ALUMINUM AIRCRAFT WIRE, CLASS 1 |
| SAE AS7351A | CLAMP, LOOP TYPE BONDING |
| SAE AS 85049/138 : 2017 | CONNECTOR ACCESSORIES, ELECTRICAL, CAP, DUST, PLASTIC, CATEGORY 9 |
| NASM 22529:2014 | GROMMET, EDGING |
| MIL-PRF-39012 Revision F:2014 | CONNECTORS, COAXIAL, RADIO FREQUENCY, GENERAL SPECIFICATION FOR |
| NASM21266:2016 | GROMMET, PLASTIC, EDGING |
| SAE AS 5768 : 2013 | TOOL, STRIPPER, ELECTRICAL INSULATION, GENERAL SPECIFICATION FOR |
| MIL-PRF-46846 Revision D:2013 | Rubber, Synthetic, Heat - Shrinkable |
| SAE AIR 1329C : 2014 | ELECTRICAL CONNECTORS AND WIRING, COMPATIBILITY OF |
| A-A-52084 Revision C:2015 | Tape, Lacing and Tying, Aramid |
| MIL-PRF-29504 Revision B:2002 | TERMINI, FIBER OPTIC CONNECTOR, REMOVABLE, GENERAL SPECIFICATION FOR |
| MIL-PRF-55339 Revision C:2005 | Adapters, Connectors, Coaxial, Radio Frequency, (Between Series and within Series), General Specification for |
| SAE AS81824/13 | SPLICE, STUB, ELECTRIC, PERMANENT, CRIMP STYLE, NICKEL/COPPER, INSULATED, ENVIRONMENT RESISTANT, 175 °C MAX |
| SAE AIR6151B | Torque, Threaded Application, Electrical Connector, Accessory and Terminal Board Installation |
| MIL-DTL-5846 Revision D:2008 | Chromel and Alumel Thermocouple Electrical Wire |
| SAE AS4461C | Assembly and Soldering Criteria for High Quality/High Reliability Soldering Wire and Cable Termination in Aerospace Vehicles |
| MIL-HDBK-502 Revision A:2013 | Product Support Analysis |
| MIL-PRF-23586 Revision F:1996 | Sealing Compound (With Accelerator), Silicone Rubber, Electrical |
| SAE AS 85049/104 : 2016 | CONNECTORS, ACCESSORIES, COMPOSITE, RFI/EMI, ELECTRICAL, STRAIN RELIEF, 45 DEGREES, SELF-LOCKING, CATEGORY 3C (FOR MIL-DTL-38999 SERIES 3 AND 4 CONNECTORS) |
| SAE AS33681B | STRAP, TIEDOWN, ELECTRICAL COMPONENTS, IDENTIFICATION, ADJUSTABLE, SELF-CLINCHING, PLASTIC, TYPE II, CLASS 1 |
| SAE AS6136 | Conduit, Electrical, Flexible, Shielded, Aluminum Alloy for Aircraft Installations |
| A-A-52083 Revision D:2015 | Tape, Lacing and Tying, Glass |
| MIL-DTL-3607 Revision C:2009 | Connectors, Coaxial, Radiofrequency, Series for Pulse, General Specification for |
| A-A-59178 Revision B:2016 | NIPPLE, ELECTRICAL TERMINAL |
| MIL-DTL-3655 Revision D:2004 | Connector, Plug and Receptacle, Electrical (Coaxial, Series Twin), and Associated Fittings, General Specification for |
| SAE AS81714/12A | TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, WIRE IN-LINE JUNCTIONS, DOUBLE, SERIES I |
| SAE AS25438B | TERMINAL-LUG, CRIMP STYLE, RIGHT ANGLE TYPE, FOR ALUMINUM AIRCRAFT WIRE, CLASS 1 |
| SAE AS85485/8A | CABLE, ELECTRIC, FILTER LINE, SHIELDED, JACKETED, RADIO FREQUENCY ABSORPTIVE, 150 °C, 600-VOLT |
| MIL-STD-196 Revision F:2013 | JOINT ELECTRONICS TYPE DESIGNATION AUTOMATED SYSTEM |
| MIL-DTL-81381 Revision C:2005 | WIRE, ELECTRIC, POLYIMIDE-INSULATED, COPPER OR COPPER ALLOY |
| NAS831:2013 | CAP, PROTECTIVE, ELECTRICAL CONNECTOR |
| SAE ARP 6400 : 2016 | RECOMMENDED PRACTICE FOR PROCESSING AND HANDLING WIRE AND CABLE WITH SILVER PLATED CONDUCTORS AND SHIELDS |
| MIL-T-81490 Revision A:1991 | TRANSMISSION LINES, TRANSVERSE ELECTROMAGNETIC MODE |
| SAE AS23190C | Wiring, Positioning, and Support Accessories |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| SAE AMSDTL23053/11A | Insulation Sleeving, Electrical, Heat Shrinkable, Fluorinated Ethylene Propylene, Non-Crosslinked |
| SAE AS5419 | Cable, Thermocouple Extension, Shielded and Unshielded |
| SAE AS85485/12A | CABLE, ELECTRIC, FILTER LINE, SMALL DIAMETER WIRE, SHIELDED, JACKETED, RADIO FREQUENCY ABSORPTIVE, 150 °C, 600-VOLT |
| MIL-STD-7080 Base Document:1994 | SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
| SAE AS 85049/105 : 2016 | CONNECTORS, ACCESSORIES, COMPOSITE, RFI/EMI, ELECTRICAL, STRAIN RELIEF, 90 DEGREES, SELF-LOCKING, CATEGORY 3C (FOR MIL-DTL-38999 SERIES 3 AND 4 CONNECTORS) |
| SAE AMSDTL23053/12A | Insulation Sleeving, Electrical, Heat Shrinkable, Polytetrafluoroethylene |
| NASM33540:2003 | SAFETY WIRING, SAFETY CABLING, COTTER PINNING, GENERAL PRACTICES FOR |
| NAS837:2013 | PLUG, PROTECTIVE, ELECTRICAL CONNECTOR |
| ASME Y14.24 : 2012 | TYPES AND APPLICATIONS OF ENGINEERING DRAWINGS - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES |
| MIL-DTL-5541 Revision F:2006 | Chemical Conversion Coatings on Aluminum and Aluminum Alloys |
| SAE AIR4465 | Design and Handling Guide Radio Frequency Absorptive Type Wire and Cables (Filter Line, MIL-C-85485) |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| NEMA WC 27500 : 2015 | STANDARD FOR AEROSPACE AND INDUSTRIAL ELECTRICAL CABLE |
| MIL-HDBK-863 Revision A:2015 | WIRING DATA AND SYSTEM SCHEMATIC DIAGRAMS PREPARATION OF |
| SAE AS22759C | Wire, Electrical, Fluoropolymer-Insulated, Copper or Copper Alloy |
| IEEE 315 : 1975 | GRAPHIC SYMBOLS FOR ELECTRICAL AND ELECTRONICS DIAGRAMS (INCLUDING REFERENCE DESIGNATION LETTERS) |
| A-A-59474 Revision C:2013 | INSULATION TAPE, ELECTRICAL; HIGH TEMPERATURE, POLYTETRAFLUOROETHYLENE, PRESSURE-SENSITIVE |
| SAE ARP1870A | Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety |
| MIL-DTL-83517 Revision B:2015 | Connector, Coaxial, Radio Frequency for Coaxial, Strip or Microstrip Transmission Line General Specification for |
| SAE AS85049D | Connector Accessories, Electrical General Specification For |
| SAE AS 4372 : 2014 | PERFORMANCE REQUIREMENTS FOR WIRE, ELECTRIC, INSULATED COPPER OR COPPER ALLOY |
| SAE AS 25274 : 2016 | CAP, ELECTRICAL (WIRE END, CRIMP STYLE, TYPE 2, CLASS 1) FOR 105 DEGREES C TOTAL CONDUCTOR TEMPERATURE |
| NASM20995:2012 | WIRE, SAFETY OR LOCK |
| MIL-DTL-25038 Revision J:2012 | WIRE, ELECTRICAL, HIGH TEMPERATURE, FIRE RESISTANT, AND FLIGHT CRITICAL |
| MIL-DTL-3650 Revision B:2003 | Connectors, Coaxial, Radio Frequency, Series LC |
| SAE AS81714B | Terminal Junction System (TJS), Environment Resistant General Specification For |
| SAE AS70991B | Terminals: Lug and Splice, Crimp Style, Aluminum, For Aluminum Aircraft Wire |
| SAE AMSDTL23053/18A | Insulation Sleeving, Electrical, Heat Shrinkable, Modified Fluoropolymer, Crosslinked |
| SAE AS7928B | Terminals, Lug: Splices, Conductor: Crimp Style, Copper, General Specification For |
| SAE ARP5614 | Guidelines for Harness Critical Clamp Locator Marker Installation on Electrical Cable Assemblies |
| SAE AS 85049/80 : 2017 | CONNECTOR ACCESSORIES, ELECTRICAL, DUMMY CONTACT, SIZES 16, 12 AND 8, CATEGORY 7 (FOR MIL-DTL-38999 CONNECTORS) |
| MS35489 Revision K:2012 | Grommets, Synthetic and Silicone Rubber, Hot-Oil and Coolant Resistant |
| MIL DTL 17 : J | CABLES, RADIO FREQUENCY, FLEXIBLE AND SEMIRIGID, GENERAL SPECIFICATION FOR |
| SAE AS81044A | Wire, Electrical, Crosslinked Polyalkene, Crosslinked Alkane-Imide Polymer, or Polyarlyene Insulated, Copper or Copper Alloy |
| NASM3036:2014 | GROMMETS, RUBBER, HOT-OIL AND COOLANT RESISTANT |
| SAE AMSDTL23053 | Insulation Sleeving, Electrical, Heat Shrinkable, General Specification For |
| MIL-STD-7179 Revision A:2009 | Finishes, Coatings, and Sealants, for the Protection of Aerospace Weapons Systems and Support Equipment |
| SAE AS27212A | TERMINAL BOARD ASSEMBLY, MOLDED-IN-STUD, ELECTRIC |
| SAE AS10380 | COUPLING INSTALLATIONS, STANDARD CONDUIT, ELECTRICAL |
| NASM25440:2012 | WASHERS, FOR USE WITH AIRCRAFT ALUMINUM TERMINALS |
| SAE AS 39029/112 : 2014 | CONTACT BUSHING, ELECTRICAL CONNECTOR CONTACT, WIRE BARREL |
| MIL-PRF-8516 Revision G:1997 | SEALING COMPOUND, SYNTHETIC RUBBER, ELECTRIC CONNECTORS AND ELECTRIC SYSTEMS, CHEMICALLY CURED |
| SAE AS7928/14A | TERMINAL, ELECTRIC, PERMANENT, CRIMP STYLE, TIN-COATED COPPER, INSULATED, ENVIRNOMENT RESISTANT, CLASS 1 150 °C, HEATLESS SEALING |
| SAE AS3509B | CABLE, SAFETY, KIT, NICKEL ALLOY, UNS N0660 |
| SAE AS39029D | Contacts, Electrical Connector, General Specification For |
| MIL-PRF-49142 Revision B:2004 | CONNECTOR, TRIAXIAL, RADIO FREQUENCY, GENERAL SPECIFICATION FOR |
| SAE AS 5942 : 2014 | MARKING OF ELECTRICAL INSULATING MATERIALS |
| SAE AS7974A | Cable Assemblies and Attachable Plugs, External Electrical Power, Aircraft, General Specification For |
| MIL-I-631 Revision D:1961 | INSULATION, ELECTRICAL, SYNTHETIC - RESIN COMPOSITION, NONRIGID |
| ASME Y14.100 : 2017 | ENGINEERING DRAWING PRACTICES - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES |
| A-A-59163 Revision A:2010 | INSULATION TAPE, ELECTRICAL, SELF-ADHERING UNSUPPORTED SILICONE RUBBER |
| SAE AS81790A | Connectors, Receptacle, External Electric Power, Aircraft General Specification for |
| MIL-STD-681 Revision F:2012 | IDENTIFICATION CODING AND APPLICATION OF HOOKUP AND LEAD WIRE |
| SAE AS81824/1A | SPLICE, IN-LINE, ELECTRIC, CRIMP, SN/CU, ENVIRONMENTAL, HEAT-SHRINKABLE SLEEVE (150 °C), 1 × 1 SEALANT OPENING |
| FED-STD-595 Revision C:2008 | COLORS USED IN GOVERNMENT PROCUREMENT |
| MIL C 83413/8 : A | CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING, TYPE 4 JUMPER CABLE ASSEMBLY, LEAD, ELECTRICAL |
| SAE AMSDTL23053/8A | Insulation Sleeving, Electrical, Heat Shrinkable, Polyvinylidene Fluoride, Semi-Rigid, Crosslinked |
| SAE AS21919 | CLAMP, LOOP TYPE, CUSHIONED SUPPORT |
| SAE AS85049/103C | CONNECTORS, ACCESSORIES, COMPOSITE, RFI/EMI, ELECTRICAL, STRAIN RELIEF, STRAIGHT, SELF-LOCKING, CATEGORY 3C (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORS) |
| MS27488 Revision N:2008 | PLUG, END SEAL, ELECTRICAL CONNECTOR |
| MIL-STD-1553 Revision B:1978 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |
| SAE AS 90387 : 2016 | WIRING INSTALLATION TOOLS FOR PLASTIC AND METAL TIEDOWN STRAPS |
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