MIL-W-5088 Revision L:1991
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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 (Future Design Should Refer to SAE-AS50881)
Available format(s)
PDF
Published date
10-05-1991
Publisher
Superseded date
01-04-1998
Superseded by
€16.67
Excluding VAT
Covers aspects from selection to the installation of wiring and wiring devices used in aerospace vehicles, including helicopters, airplanes, lighter-than-air vehicles, and missiles. Coverage includes application, applicable documents, terminology interpretation, deviations, materials, metals, nonmetals, sealing materials, maintenance considerations, ambient temperature, and missile wiring application.
| DevelopmentNote |
INACTIVE FOR NEW DESIGN
|
| DocumentType |
Standard
|
| Pages |
88
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
This specification covers all aspects from the selection through installation of wiring and wiring devices used in aerospace vehicles.
| MIL-R-85895 Base Document:1988 | RACK, BOMB EJECTOR, AIRCRAFT BRU-32/A |
| MIL-C-6781 Revision B:1960 | Control Panel: Aircraft Equipment, Rack or Console Mounted |
| DEFSTAN 00-970(PT1)SEC6/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
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| MIL-L-85762 Revision A:1988 | LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
| MIL-R-83372 Base Document:1972 | RELAYS, ELECTROMAGNETIC, HYBRID, EMI SUPPRESSED, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT) |
| MIL-I-83294 Base Document:1971 | Installation Requirement, Aircraft Propulsion Systems, General Specification for (No S/S Document) |
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| MIL-R-29583 Base Document:1992 | Radio Set, AN/ARC-210(V) (No S/S Document) |
| MIL S 24317 : 0 | SWITCH, MULTI-STATION, PUSHBUTTON (ILLUMINATED AND NON-ILLUMINATED), GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT1)SEC6/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL-E-23001 Revision B:1976 | Electric Generating System, Variable Speed Constant Frequency, Aircraft, General Specification for (S/S by MIL-E-85583) |
| DEFSTAN 00-970(PT1)SEC6/14(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL I 7627 : F | INDICATOR, TURN AND SLIP 28V DC |
| MIL-L-6503 Revision H:1975 | Lighting Equipment, Aircraft, General Specification for Installation of |
| DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| MIL-A-22145 Revision C:1992 | Accelerometer Group, Counting,(MS25447 and MS25448) (S/S by SAE-AS22145) |
| DEFSTAN 00-970(PT1)SEC6/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL-I-85071 Revision A:1992 | Inverters, Aircraft, DC to AC, General Specification for (S/S by MIL-PRF-7032) |
| MIL-STD-7080 Base Document:1994 | Selection and Installation of Aircraft Electric Equipment |
| MIL-HDBK-83575 Base Document:1998 | General Handbook for Space Vehicle Wiring Harness Design and Testing |
| MIL-T-81714 Revision E:1988 | Terminal Junction System (TJS), Environment Resistant General Specification for (S/S by SAE-AS81714) |
| MIL-C-7135 Revision F:1967 | Compressor, Pneumatic, 3,000 PSI -- 2 SCFM Aero 2A (*), Aero 2A-1 (*), Aero 2B (*), and Aero 2B-1 (*) |
| MIL-R-81046 Base Document:1964 | RECORDER-REPRODUCER SET, SOUND AN/AQH-1 (V) (NO S/S DOCUMENT) |
| MIL-C-23697 Base Document:1963 | Computer Set, Navigational AN/ASN-42(*) |
| DEFSTAN 00-970(PT7)SEC2/SUPP6/6(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-HDBK-1587 Base Document:1996 | Materials and Process Requirements for Air Force Weapons Systems (S/S by MIL-STD-1587) |
| 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 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-A-81973 Base Document:1974 | Aircrew Automated Escape Systems, Test Vehicles for Ground Track Performance Testing, Rocket and/or Jet Engine Propelled, General Specification for (No S/S Document) |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| 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 |
| MIL T 28800 : E | TEST EQUIPMENT FOR USE WITH ELECTRICAL AND ELECTRONIC EQUIPMENT GENERAL SPECIFICATION FOR |
| 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)/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 |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-R-81876 Revision B:1988 | Receiver-Transmitter Radio Set AN/APX-100(V) (No S/S Document) |
| MIL W 8777 : C | WIRE, ELECTRICAL, SILICONE-INSULATED COPPER 600-VOLT, 200 DEGREE C |
| DEFSTAN 00-970(PT1)SEC6/4(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| 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-H-8891 Revision A:1978 | Hydraulic Systems, Manned Flight Vehicles, Type III Design, Installation and Data Requirements for, General Specification for |
| MIL R 23016 : A | RADIO SET AN/ARC-94 |
| MIL-STD-2156 Base Document:1983 | Launcher, Rail, Guided Missile, Aircraft, General Design Criteria for |
| MIL-J-23013 Base Document:1961 | Junction Box JEU-25 (*)/A (No S/S Document) |
| DEFSTAN 00-970(PT7)SEC2/SUPP6/5(2015) : INTERIM | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
| MIL-H-5440 Revision H:1993 | Hydraulic Systems, Aircraft, Design and Installation Requirements for (S/S by SAE-AS5440) |
| MIL-E-45782 Revision C:1993 | Electrical Wiring, Procedures for |
| MIL-A-81621 Base Document:1969 | Accelerometer, Electrical, Linear ABU-13/A |
| MIL-DTL-8777 Revision F:2011 | Wire, Electrical, Silicone-Insulated, Copper, 600-Volt, 200 Degrees C |
| MIL-A-26624 Revision B:1981 | Air Conditioner, A/M32C-5, Trailer Mounted, Vapor Cycle, Electric Motor Driven (No S/S Document) |
| MIL-M-25047 Revision C:1968 | Markings and Exterior Finish Colors for Airplanes, Airplane Parts, and Missiles (Ballistic Missiles Excluded) (No S/S Document) |
| MIL-I-85671 Base Document:1987 | INDICATOR, FREQUENCY CHANNEL ID-2121A/ARC, ID-2229A/ARC AND ID-2303/ARC |
| MIL-D-81358 Revision B:1970 | Display Group, Tactical Data AN/ASA-66 |
| MIL-T-23733 Revision A:1968 | Transmitter, Rate Gyroscope T-751( )/AJB-3 (No S/S Document) |
| MIL-A-23670 Revision A:1965 | Attitude Heading Reference System HEADING AN/ASN-50(*) |
| MIL M 87158 : A | MANUALS, TECHNICAL, AIRCRAFT BATTLE DAMAGE ASSESSMENT AND REPAIR |
| MIL-B-81365 Base Document:1966 | Bleed Air Systems, General Specification for |
| MIL-C-22764 Revision C:1964 | Coder Receiver Transmitter KY-532A/ASQ |
| MIL-S-8512 Revision D:1974 | Support Equipment, Aeronautical, Special, General Specification for the Design of |
| MIL-E-7080 Revision B:1962 | Electric Equipment, Aircraft, Selection and Installation of (S/S by MIL-STD-7080) |
| MIL-STD-2131 Revision A:1991 | Launcher, Ejection, Guided Missile, Aircraft, General Design Criteria for |
| MIL-S-5594 Revision B:1971 | Switch, Toggle, Electrically Held Sealed, General Specification For (S/S by SAE-AS55941) |
| DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| MIL B 8075 : D | BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
| MIL-S-83129 Revision A:1972 | SPECTROMETER, FLUID ANALYSIS A/E35U-3 (NO S/S DOCUMENT) |
| DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
| SAE AS8700 | Installation and Test of Electronic Equipment in Aircraft, General Specification for |
| MIL-HDBK-516 Revision C:2014 | Airworthiness Certification Criteria |
| MIL-M-9397 Revision E:1979 | Frequency Converter, Mobile, Type MC-1A |
| MIL-S-8812 Revision D:1975 | Steering System, Aircraft General Requirements for |
| MIL-S-8710 Revision B:1969 | Strainer, Airframe Fuel System, General Specification for |
| DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| MIL S 8805/48 : F | SWITCH, SENSITIVE, ROLLER LEVER, SELF RETURN, RESILIENT SEAL, FLUID RESISTANT |
| SAE AIR5271 | A Guideline for Application of High-Density Fiber Optic Interconnects to Aerospace Platforms |
| MIL-E-7016 Revision F:1976 | Electric Load and Power Source Capacity, Aircraft, Analysis of |
| MIL-R-21073 Revision A:1960 | Recorder, Magnetic Distortion, RO-32/ASQ |
| DEFSTAN 00-970(PT1)SEC6/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL F 26685 : B NOTICE 1 | FLIGHT DIRECTOR SYSTEM, DESIGN AND INSTALLATION OF |
| MIL-DTL-26126 Revision C:2002 | Relays, Electrical, Overvoltage, DC, General Specification for (No S/S Document) |
| MIL-A-23887 Revision A:1965 | Altimeter Set, Electronic AN/APN-141(V) |
| MIL-C-85518 Base Document:1984 | COMPUTER SET, STANDARD AIRBORNE AN/AYK-14(V) GENERAL SPECIFICATION FOR |
| MIL-D-23222 Revision A:1971 | Demonstration Requirements for Helicopters |
| MIL-I-8673 Base Document:1955 | Installation and Test of Aircraft Flexible Weapons Systems (No S/S Document) |
| MIL-D-81641 Base Document:1972 | Display, Head-up, General Specification for |
| MIL-I-81454 Base Document:1967 | Indicator, Gyroscope, Vertical Reference ID-1481(*)/A |
| MIL-A-81359 Base Document:1970 | Aircraft Weapons Release Set AN/AWE-1 |
| MIL-C-19941 Revision A:1966 | Controller, S-2 Compass, Type (No S/S Document) |
| MIL T 25920 : C | TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION |
| MIL-D-8804 Revision B:1993 | Deicing System, Pneumatic Boot, Aircraft, General Specification for (S/S by SAE-AS8804) |
| MIL C 5898 : D | CORD, ELECTRICAL [WF 5/U, WF 14/U,WD 34/U, WM 53/U, WM 85/U] |
| MIL R 26895 : 0 | RELAY, FIELD CONTROL, GENERATOR 28 VOLT DC, TYPE MD AND 1 |
| MIL I 18373 : B | INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF |
| MIL-C-85248 Revision A:1984 | Camera, Still Picture, Panoramic, KA-99A |
| MIL-R-24011 Revision A:1965 | Radar Altimeter Warning Set AN/APQ-107(*) |
| MIL-R-6463 Revision A:1952 | RELAY, GENERATOR EQUALIZER BUS, TYPE A-1 (NO S/S DOCUMENT) |
| MIL-C-18277 Revision B:1961 | Coupler, Antenna CU-351/AR and Coupler, Antenna CU-509/AR |
| MIL-C-85642 Base Document:1985 | COMMUNICATIONS CENTRAL AN/ASC-26 |
| MIL C 81125 : NOTICE 1 | COUPLER, ANTENNA CU-1304 (*)/ARC AND MOUNTING MT-3261 (*)/ARC |
| MIL-A-22424 Revision A:1967 | Adapters, Compensating, MS28107, MA-1 Compass System (No S/S Document) |
| DOD-STD-863 Revision B:1979 | WIRING DATA AND SYSTEM SCHEMATIC DIAGRAMS PREPARATION OF |
| MIL-I-8700 Revision A:1970 | Installation and Test of Electronic Equipment in Aircraft, General Specification for (S/S by SAE-AS8700) |
| MIL-P-5238 Revision C:1974 | Pump, Centrifugal, Fuel Booster, Aircraft, General Specification For |
| SAE ARP1897 | Clamp Selection and Installation Guide |
| SAE AIR5575A | Hot Stamp Wire Marking Concerns for Aerospace Vehicle Applications |
| MIL-G-81665 Base Document:1971 | Generator Transmitter Group AN/ASA-76 (U) (No S/S Document) |
| MIL-A-23622 Base Document:1963 | Actuator, Aircraft, Electro-Mechanical, Linear, Direct Current |
| MIL-STD-681 Revision F:2012 | Identification Coding and Application of Hookup and Lead Wire |
| MIL-R-28894 Base Document:1986 | RELAYS, HYBRID OR SOLID STATE, SENSORS, ESTABLISHED RELIABILITY GENERAL SPECIFICATION FOR (NO S/S DOCUMENT) |
| MIL S 8805/43 : G | SWITCH, SENSITIVE, PLUNGER, 7 AMPERES RESILIENT SEAL, FLUID RESISTANT |
| MIL-A-19939 Revision A:1966 | Amplifier, Two Channel, Integral, S-2 Compass (No S/S Document) |
| MIL-W-22759 Revision E:1990 | WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED, COPPER OR COPPER ALLOY (S/S BY SAE-AS22759) |
| MIL-C-81991 Base Document:1975 | Converter, Aircraft DC to DC, Boost General Specification for (No S/S Document) |
| MIL R 26126 : B | RELAY, ELECTRICAL, OVERVOLTAGE DC, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL-I-23366 Revision B:1987 | Indicator, Horizontal Situation ID-1013(*)/A |
| DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT |
| MIL-DTL-25561 Revision B:1995 | Grip Assembly, Controller, Aircraft Type MC-2 (See Notice 2 for Replacement Information) |
| MIL-R-9221 Base Document:1953 | RELAY, FIELD CONTROL, GENERATOR 24 VOLT DC, TYPE M-2 (NO S/S DOCUMENT) |
| MIL-E-85583 Revision A:1987 | ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-G-83380 Base Document:1979 | Generator Set, Gas Turbine Engine Driven, 60KW, 400 HZ (No S/S Document) |
| MIL-E-25499 Revision C:1970 | Electrical System, Aircraft, Design and Installation of, General Requirements for (No S/S Document) |
| MIL-I-8671 Revision D:1994 | Installation of Droppable Stores and Associated Release Systems |
| MIL-F-23447 Base Document:1962 | Fire Warning Systems, Aircraft, Radiation Sensing Type, Test and Installation of |
| DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL-W-26217 Revision B:1985 | Winch, Drum, Power Operated AF/E24H-1, Cargo Loading, 4,000 Pound Capacity, Variable Speed, 28V DC Portable |
| MIL-N-81207 Revision A:1973 | Navigational Set, TACAN AN/ARN-84 (V) |
| SAE AS55941A | Switches, Toggle, Electrically Held, Sealed, General Specification For |
| SAE ARP1070D | Design and Testing of Antiskid Brake Control Systems for Total Aircraft Compatibility |
| MIL-G-23081 Revision C:1972 | Gyroscope Indicator System, Vertical |
| MIL-D-19326 Revision H:1990 | Design and Installation of Liquid Oxygen Systems in Aircraft, General Specification for |
| MIL-R-81498 Revision C:1979 | Receiving-Decoding Group AN/ARA-63 |
| MIL-G-23083 Revision C:1972 | Gyroscope, Rate Switching MS 17399 |
| MIL-B-23431 Revision B:1993 | Beacon, Radar AN/APN-154(V) |
| MIL-F-8615 Revision D:1976 | Fuel System Components, General Specification for (S/S by SAE-ARP8615) |
| MIL-I-85112 Base Document:1978 | Indicator Set, Vertical Scale |
| MIL-A-85505 Base Document:1983 | ALTIMETER, STANDBY, TYPES 1 AND 2 |
| MIL-A-85672 Base Document:1987 | AMPLIFIER, RADIO FREQUENCY AM-7177A/ARC |
| MIL-W-18326 Revision A:1956 | WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR (S/S BY MIL-STD-2219) |
| MIL-A-81605 Revision D:1984 | Altimeter Set, Electronic AN/APN194(V) |
| SAE AS22145A | Accelerometer Group, Counting (MS25447 and MS25448) |
| MIL-D-8708 Revision C:1991 | Demonstration: Aircraft Weapon Systems, General Specification for |
| MIL-I-81453 Revision A:1977 | Interrogator Set AN/APX-76B(V) (No S/S Document) |
| MIL-T-85678 Base Document:1974 | TRANSPONDER, RADAR TRACKING |
| MIL-A-81296 Revision D:1985 | Altimeter Set, Electronic, AN/APN-171(V) |
| MIL M 4803 : D | MOTOR-GENERATOR, 400 HZ PRECISE OUTPUT, GENERAL REQUIREMENTS FOR |
| MIL-L-85314 Revision A:1983 | LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
| MIL-A-81423 Base Document:1966 | Attitude Heading Reference System AN/ASN-73 (No S/S Document) |
| MIL D 83753 : NOTICE 2 | DISPENSER, BOMB, TYPE SUU-21/A |
| MIL-I-8672 Revision B:1969 | Installation and Test of Aircraft Pyrotechnic Equipment in Aircraft, General Specification for (No S/S Document) |
| MIL-C-85392 Base Document:1987 | CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW-7D, GENERAL SPECIFICATION FOR |
| MIL C 7115 : F | CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-C-81883 Base Document:1976 | Control Group, Electric Power OK-XXX (V)/A, General Specification for (No S/S Document) |
| MIL-I-7802 Revision A:1967 | Indicator, MS28088, Turn and Slip (Three Phase) |
| MIL-C-85283 Revision B:1994 | Control-Monitor Set, Guided Weapon, AN/AWW-9B, P/N 1064AS4100 |
| MIL-L-5667 Revision B:1964 | Lighting Equipment, Aircraft Instrument Panel, General Specification for Installation of (No S/S Document) |
| MIL M 23888 : NOTICE 1 | MONITOR, RADIO FREQUENCY ID AND 9O2A/AR |
| MIL S 9419 : E | SWITCH, TOGGLE, MOMENTARY, FOUR-POSITION ON, CENTER OFF, GENERAL SPECIFICATION FOR |
| MIL-C-85373 Revision A:1987 | CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW 12A |
| MIL-T-81821 Base Document:1969 | Trainers, Maintenance, Equipment and Services General Specification For (No S/S Document) |
| MIL-D-5025 Revision C:1961 | Direction Finder Group AN/APA-69A and AN/APA-69C |
| MIL-C-18244 Revision A:1962 | Control and Stabilization Systems: Automatic, Piloted Aircraft, General Specification for |
| MIL-P-18987 Revision A:1962 | PLOTTING BOARD, TACTICAL DISPLAY PT-396/AS |
| MIL-P-19461 Revision A:1959 | Plotting Board, Tactical Display, PT-429/A |
| MIL-I-3190 Revision F:1991 | Insulation Sleeving, Electrical, Flexible, Coated, General Specification for |
| MIL-M-24041 Revision C:1981 | Molding and Potting Compound, Chemically Cured, Polyurethane |
| ASME Y32.2 : LATEST | DRAW AND TERM - GRAPHICS SYMBOLS STANDARDS - FOR ELECTRICAL AND ELECTRONIC DIAGRAMS |
| MS33540 Revision J:1986 | SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR (S/S BY NASM33540) |
| MIL-S-23190 Revision E:1986 | STRAPS, CLAMPS, AND MOUNTING HARDWARE, PLASTIC AND METAL FOR CABLE HARNESS TYING AND SUPPORT (S/S BY SAE-AS23190) |
| MIL-W-22759 Revision E:1990 | WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED, COPPER OR COPPER ALLOY (S/S BY SAE-AS22759) |
| MIL C 22520 : F | CRIMPING TOOLS, TERMINAL HAND OR POWER ACTUATED, WIRE TERMINATION AND TOOL KITS - GENERAL SPECIFICATION FOR |
| MS27212 Revision P:1994 | TERMINAL BOARD ASSEMBLY, MOLDED-IN-STUD, ELECTRIC (S/S BY SAE-AS27212) |
| MS25281 Revision K:1978 | CLAMP, LOOP, PLASTIC, WIRE SUPPORT (S/S BY SAE-AS25281) |
| MS90387 Revision H:2007 | Tool, Hand, Adjustable for Plastic and Metal Tiedown Straps (S/S by SAE-AS90387) |
| MIL-STD-704 Revision F:2004 | Aircraft Electric Power Characteristics |
| MIL-STD-970 Base Document:1987 | STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF (NO S/S DOCUMENT) |
| MIL-C-7762 Revision A:1967 | Compass, Installation of (No S/S Document) |
| MIL C 83517 : 0 | CONNECTOR, COAXIAL, RADIO FREQUENCY FOR COAXIAL, STRIP OR MICROSTRIP TRANSMISSION LINE, GENERAL SPECIFICATION FOR |
| MIL A 55339 : A | ADAPTER, CONNECTOR, COAXIAL, RADIO FREQUENCY, (BETWEEN SERIES & WITHIN SERIES) GENERAL SPECIFICATION FOR |
| DOD STD 100 : C NOTICE 6 | ENGINEERING DRAWING PRACTICES |
| MS25439 Revision A:1964 | Splice-Permanent Crimp Style, 2 Way Type for Aluminum Aircraft Wire, Class 1 (S/S By SAE-AS25439) |
| MIL-E-6051 Revision D:1967 | Electromagnetic Compatibility Requirements, Systems (S/S by MIL-STD-464) |
| MS25440 Revision C:1974 | WASHERS, FOR USE WITH AIRCRAFT ALUMINUM TERMINALS (S/S BY NASM25440) |
| MIL-STD-1353 Revision C:2014 | Electrical Connectors, Plug-in Sockets and Associated Hardware, Selection and Use of |
| DOD-STD-863 Revision B:1979 | WIRING DATA AND SYSTEM SCHEMATIC DIAGRAMS PREPARATION OF |
| MS25436 Revision A:1964 | Terminal, Lug, Crimp Style 90 Degrees Upright Type, for Aluminum Aircraft Wire, Class 1 (S/S by SAE-AS25436) |
| MS25274 Revision G:1982 | CAP, ELECTRICAL (WIRE END, CRIMP STYLE, TYPE II, CLASS 1) FOR 105 DEG. C TOTAL CONDUCTOR TEMPERATURE (S/S/ BY SAE-AS25274) |
| MIL-T-81490 Revision A:1991 | TRANSMISSION LINES, TRANSVERSE ELECTROMAGNETIC MODE |
| MIL-T-7099 Revision E:1979 | TERMINAL, LUG AND SPLICE, CRIMP STYLE ALUMINUM, FOR ALUMINUM AIRCRAFT WIRE (S/S BY SAE-AS70991) |
| MIL-C-26637 Revision A:1987 | Connectors, Coaxial, Radio Frequency, Series LT, General Specification for (No S/S Document) |
| MIL C 3650 : A | CONNECTOR, COAXIAL, RADIO FREQUENCY, SERIES LC |
| MIL-T-81714 Revision E:1988 | Terminal Junction System (TJS), Environment Resistant General Specification for (S/S by SAE-AS81714) |
| MIL-STD-889 Revision C:2016 | Galvanic Compatibility of Electrically Conductive Materials |
| MS21919 Revision E:1981 | Clamp, Loop Type, Cushioned, Support |
| MIL-C-85049 Revision A:1990 | Connector Accessories, Electrical General Specification for (S/S by SAE-AS85049) |
| MIL-T-43435 Revision B:1974 | TAPE, LACING AND TYING (S/S BY A-A-52080 THRU A-A-52084) |
| MIL-M-81260 Revision A:1971 | Manual, Technical, Aircraft/System/Equipment Maintenance |
| MIL-C-85485 Revision A:1983 | CABLE, ELECTRIC, FILTER LINE, RADIO FREQUENCY ABSORPTIVE |
| MIL C 39012 : C | GENERAL SPECIFICATION FOR RADIO FREQUENCY COAXIAL CONNECTORS |
| MIL-HDBK-216 Base Document:1962 | R.F. Transmission Lines and Fittings (Future Acquisitions may refer to EIA-979) |
| MS21266 Revision E:1981 | GROMMET, PLASTIC, EDGING (S/S BY NASM21266) |
| MIL-STD-1388-1 Revision A:1983 | Logistic Support Analysis (S/S by MIL-HDBK-502) |
| MIL S 8516 : F | SEALING COMPOUND, POLYSULFIDE RUBBER, ELECTRIC CONNECTORS AND ELECTRICAL SYSTEMS CHEMICALLY CURED |
| MIL C 25516 : D | CONNECTOR, ELECTRICAL, MINIATURE, COAXIAL, ENVIRONMENT RESISTANT TYPE, GENERAL SPECIFICATION FOR |
| MIL-I-23594 Revision C:1988 | Insulation Tape, Electrical, High Temperature, High Temperature, Polytetrafluoroethylene, Pressure-Sensitive (S/S by A-A-59474) |
| MIL-T-81714-12 Revision C:1988 | Terminal Junction System Terminal Junction Blocks, Sectional, Wire In-Line Junctions, Double Series I (S/S by SAE-AS81714/12) |
| MIL I 23053 : D | INSULATION SLEEVING, ELECTRICAL, HEAT SHRINKABLE MODIFIED FLUOROPOLYMER, CROSSLINKED |
| MIL-B-7883 Revision B:1968 | Brazing of Steels, Copper, Copper Alloys, Nickel Alloys, Aluminum and Aluminum Alloys (Future Acquisition should specify one AWS-C3.4, AWS-C3.5, AWS-C3.6 and AWS-C3.7) |
| MIL C 3643 : A | CONNECTOR, COAXIAL RADIO FREQUENCY, SERIES HN ASSOCIATED FITTINGS GENERAL SPECIFICATION FOR |
| MIL-C-39029 Revision D:1988 | Contacts, Electrical Connector, General Specification for (S/S by SAE-AS39029) |
| MIL S 23586 : E | SEALING COMPOUND, ELECTRICAL, SILICONE RUBBER, ACCELERATOR REQUIRED |
| MS90376 Revision E:1993 | Cap, Dust, Plastic, Electric Connector (See Notice 2 for Replacement Information) |
| MS35489 Revision K:2012 | Grommets, Synthetic and Silicone Rubber, Hot-Oil and Coolant Resistant |
| MS25438 Revision A:1964 | Terminal, Lug, Crimp Style, Right Angle Type, for Aluminum Aircraft Wire, Class 1 (S/S by SAE-AS25438) |
| MIL-I-7444 Revision D:1984 | Insulation Sleeving, Electrical, Flexible (See Notice 3 for Replacement Information) |
| MIL-S-83519 Revision A:1984 | SHIELD TERMINATION, SOLDER STYLE, INSULATED, HEAT-SHRINKABLE, ENVIRONMENT RESISTANT GENERAL SPECIFICATION FOR (S/S BY SAE-AS83519) |
| MIL-T-7928 Revision G:1976 | Terminals, Lug: Splices, Conductor: Crimp Style, Copper, General Specification for (S/S BY SAE-AS7928) |
| MIL C 3655 : C | CONNECTOR, PLUG AND RECEPTACLE, ELECTRICAL [COAXIAL SERIES TWIN] AND ASSOCIATED FITTINGS, GENERAL SPECIFICATION FOR |
| MIL C 3607 : A | CONNECTOR, COAXIAL, RADIO FREQUENCY, SERIES PULSE GENERAL SPECIFICATION FOR |
| MIL-T-81714-11 Revision F:1988 | Terminal Junction System Terminal Junction Blocks, Sectional, Wire In- Line Junctions, Single Series I (S/S by SAE-AS81714/11) |
| MIL C 49142 : 0 | CONNECTOR, PLUGS & RECEPTACLES, ELECTRICAL, TRIAXIAL,RADIO FREQUENCY, GENERAL SPECIFICATION FOR |
| MS3373 Revision C:1972 | STRIP, MOUNTING, NUT INSULATING, FOR MS 27212 TERMINAL BOARD (S/S BY SAE-AS33731) |
| MIL-C-6136 Revision A:1965 | Conduit: Electrical, Flexible, Shielded, Aluminum Alloy for Aircraft Installations (Use SAE-AS6136) |
| MIL-I-631 Revision D:1961 | Insulation, Electrical, Synthetic - Resin Composition, Nonrigid |
| MIL-B-5087 Revision B:1964 | Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464) |
| MS25171 Revision C:1959 | NIPPLE, ELECTRICAL TERMINAL (ASG) (S/S BY A-A-59178) |
| MIL-I-8700 Revision A:1970 | Installation and Test of Electronic Equipment in Aircraft, General Specification for (S/S by SAE-AS8700) |
| MIL-STD-681 Revision F:2012 | Identification Coding and Application of Hookup and Lead Wire |
| FED-STD-595 Revision C:2008 | Colors Used in Government Procurement (S/S By SAE-AMS-STD-595) |
| MS18029 Revision E:1971 | Cover Assembly, Electrical, for MS27212 Terminal Board Assembly (S/S by SAE-AS18029) |
| MIL-E-7080 Revision B:1962 | Electric Equipment, Aircraft, Selection and Installation of (S/S by MIL-STD-7080) |
| MS25435 Revision A:1964 | Terminal, Lug, Crimp Style, for Aluminum Aircraft Wire Class 1 (S/S by SAE-AS25435) |
| MIL-F-7179 Revision G:1993 | Finishes, Coatings, and Sealants for the Protection of Aerospace Weapons Systems (S/S by MIL-STD-7179) |
| MS27488 Revision N:2008 | Plug, End Seal, Electrical Connector |
| MIL-STD-1553 Revision B:1978 | Digital Time Division Command/Response Multiplex Data Bus |
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