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  • MIL-W-5088 Revision L:1991

    View superseded by
    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
    View superseded by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

    Superseded date:  01-04-1998

    Language(s): 

    Published date:  10-05-1991

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    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.

    Scope - (Show below) - (Hide below)

    This specification covers all aspects from the selection through installation of wiring and wiring devices used in aerospace vehicles.

    General Product Information - (Show below) - (Hide below)

    Development Note INACTIVE FOR NEW DESIGN
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Superseded
    Superseded By

    Standards Referenced By This Book - (Show below) - (Hide below)

    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
    DEFSTAN 00-970(PT1)SEC6/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT
    MIL-L-85762 Revision A:1988 LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION
    MIL-R-83372 Base Document:1972 RELAY, ELECTROMAGNETIC, HYBRID, EMI SUPPRESSED, GENERAL SPECIFICATION FOR
    MIL-I-83294 Base Document:1971 INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR
    DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    MIL-R-29583 Base Document:1992 RADIO SET
    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
    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)
    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
    MIL-STD-7080 Base Document:1994 SELECTION & 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
    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)
    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 WEAPON SYSTEM
    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
    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)
    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 111 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
    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, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR
    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
    MIL-M-25047 Revision C:1968 MARKINGS AND EXTERIOR FINISH COLORS FOR AIRPLANES, AIRPLANE PARTS, AND MISSILES (BALLISTIC MISSILES EXCLUDED)
    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)
    MIL-A-23670 Revision A:1965 ATTITUDE HEADING REFERENCE SYSTEM 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 SPECIFICATIONS FOR
    MIL-C-22764 Revision C:1964 CODER RECEIVER TRANSMITTER K & Y532A 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
    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
    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
    DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT
    SAE AS 8700 : 1999 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 AIR 5271 : 2009 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
    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
    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
    MIL T 25920 : C TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION
    MIL-D-8804 Revision B:1993 DE-ICING SYSTEM, PNEUMATIC BOOT, AIRCRAFT, GENERAL SPECIFICATION FOR
    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 A1
    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, MS281O7, MA-1 COMPASS SYSTEM
    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
    MIL-P-5238 Revision C:1974 PUMP, CENTRIFUGAL, FUEL BOOSTER, AIRCRAFT, GENERAL SPECIFICATION FOR
    SAE ARP 1897 : 2013 CLAMP SELECTION AND INSTALLATION GUIDE
    SAE AIR 5575 : 2017 HOT STAMP WIRE MARKING CONCERNS FOR AEROSPACE VEHICLE APPLICATIONS
    MIL-G-81665 Base Document:1971 GENERATOR TRANSMITTER GROUP AN/ASA-76 (U)
    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 RELAY, HYBRID OR SOLID STATE, SENSORS, ESTABLISHED RELIABILITY GENERAL SPECIFICATION FOR
    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
    MIL-W-22759 Revision E:1990 WIRE, ELECTRIC, FLUOROPOLYMER-INSULATED, COPPER OR COPPER ALLOY
    MIL-C-81991 Base Document:1975 CONVERTER, AIRCRAFT DC TO DC, BOOST GENERAL SPECIFICATION FOR
    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-1O13(*)/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
    MIL-R-9221 Base Document:1953 RELAY, FIELD CONTROL, GENERATOR 24 VOLT DC TYPE M AND 2
    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, 30 AND 60 KW, 400 HZ
    MIL-E-25499 Revision C:1970 ELECTRICAL SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION OF, GENERAL REQUIREMENTS FOR
    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, 4OOO POUND CAPACITY, VARIABLE SPEED, 28V DC PORTABLE
    MIL-N-81207 Revision A:1973 NAVIGATIONAL SET, TACAN AN/ARN-84 (V)
    SAE AS 55941 : 2013 SWITCHES, TOGGLE, ELECTRICALLY HELD, SEALED, GENERAL SPECIFICATION FOR
    SAE ARP 1070E : 2019 DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY
    SAE ARP 1070 : 2014 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 [ASG]
    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
    MIL-A-81605 Revision D:1984 ALTIMETER SET, ELECTRONIC AN/APN-194(V)
    SAE AS 22145 : 2012 ACCELEROMETER GROUP, COUNTING (MS25447 AND MS25448)
    MIL-D-8708 Revision C:1991 DEMONSTRATION REQUIREMENTS FOR AIRPLANES
    MIL-I-81453 Revision A:1977 INTERROGATOR SET AN APX 76B(V)
    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
    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 [ASG]
    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
    MIL-I-7802 Revision A:1967 INDICATOR, MS 28088, TURN AND SLIP [THREE PHASE]
    MIL-C-85283 Revision B:1994 CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW-9
    MIL-L-5667 Revision B:1964 LIGHTING EQUIPMENT, AIRCRAFT INSTRUMENT PANEL, GENERAL SPECIFICATION FOR INSTALLATION OF [ASG]
    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
    MIL-D-5025 Revision C:1961 DIRECTION FINDER GROUPS 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

    Standards Referencing This Book - (Show below) - (Hide below)

    MIL-I-3190 Revision F:1991 INSULATION SLEEVING, ELECTRICAL, FLEXIBLE, COATED, GENERAL SPECIFICATION FOR
    MIL-M-24041 Revision C:1981 MOLDING AND POTTING COMPOUND
    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
    MIL-S-23190 Revision E:1986 STRAPS, CLAMPS AND MOUNTING HARDWARE, PLASTIC FOR CABLE HARNESS TYING AND SUPPORT
    MIL-W-22759 Revision E:1990 WIRE, ELECTRIC, FLUOROPOLYMER-INSULATED, COPPER OR COPPER ALLOY
    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
    MS25281 Revision K:1978 CLAMP, LOOP PLASTIC, WIRE SUPPORT
    MS90387 Revision H:2007 TOOL, HAND, ADJUSTABLE FOR PLASTIC AND METAL TIEDOWN STRAPS
    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
    MIL-C-7762 Revision A:1967 COMPASS, INSTALLATION OF
    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,
    MIL-E-6051 Revision D:1967 ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
    MS25440 Revision C:1974 WASHER FOR USE WITH AIRCRAFT ALUMINUM TERMINALS
    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
    MS25274 Revision G:1982 CAP, ELECTRICAL, (WIRE END, CRIMP STYLE, TYPE 2, CLASS 1) FOR 105 DEGREE C TOTAL CONDUCTOR TEMPERATURE
    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
    MIL-C-26637 Revision A:1987 CONNECTORS, COAXIAL, RADIO FREQUENCY, SERIES LT
    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
    MIL-STD-889 Revision C:2016 DISSIMILAR METALS
    MS21919 Revision E:1981 CLAMP, LOOP TYPE, CUSHIONED, SUPPORT
    MIL-C-85049 Revision A:1990 CONNECTOR ACCESSORIES, ELECTRICAL GENERAL SPECIFICATION FOR
    MIL-T-43435 Revision B:1974 TAPE, LACING, AND TYING
    MIL-M-81260 Revision A:1971 MANUALS, 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
    MIL-STD-1388-1 Revision A:1983 LOGISTIC SUPPORT ANALYSIS
    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, POLYTETRAFLUOROETHYLENE, PRESSURE SENSITIVE
    MIL-T-81714-12 Revision C:1988 TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, WIRE IN-LINE JUNCTIONS, DOUBLE, SERIES 1
    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
    MIL C 3643 : A CONNECTOR, COAXIAL RADIO FREQUENCY, SERIES HN ASSOCIATED FITTINGS GENERAL SPECIFICATION FOR
    MIL-C-39029 Revision D:1988 CONTACT, ELECTRICAL CONNECTOR, GENERAL SPECIFICATION FOR
    MIL S 23586 : E SEALING COMPOUND, ELECTRICAL, SILICONE RUBBER, ACCELERATOR REQUIRED
    MS90376 Revision E:1993 CAP, DUST, PLASTIC, ELECTRIC CONNECTOR
    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
    MIL-I-7444 Revision D:1984 INSULATION SLEEVING, ELECTRICAL FLEXIBLE
    MIL-S-83519 Revision A:1984 SPLICE, SHIELD TERMINATION, SOLDER STYLE, INSULATION, HEAT SHRINKABLE, ENVIRONMENT RESISTANT, GENERAL SPECIFICATION FOR
    MIL-T-7928 Revision G:1976 TERMINAL, LUG SPLICES, CONDUCTOR, CRIMP STYLE, COPPER, GENERAL SPECIFICATION FOR
    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 1
    NAS813:2012 CAP, PROTECTIVE, ELECTRICAL CONNECTOR
    NAS820:2012 PLUG - PROTECTIVE, ELECTRICAL CONNECTOR
    MIL C 49142 : 0 CONNECTOR, PLUGS & RECEPTACLES, ELECTRICAL, TRIAXIAL,RADIO FREQUENCY, GENERAL SPECIFICATION FOR
    MS3373 Revision C:1972 STRIP, MOUNTING, NUT INSULATING, FOR MS27212 TERMINAL BOARD
    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 LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
    MS25171 Revision C:1959 NIPPLE, ELECTRICAL TERMINAL (ASG)
    MIL-I-8700 Revision A:1970 INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR
    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
    MS18029 Revision E:1971 COVER ASSEMBLY ELECTRICAL FOR MS27212 TERMINAL BOARD ASSEMBLY
    MIL-E-7080 Revision B:1962 ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF
    MS25435 Revision A:1964 TERMINAL, LUG, CRIMP STYLE, STRAIGHT TYPE, FOR ALUMINUM AIRCRAFT WIRE CLASS 1
    MIL-F-7179 Revision G:1993 FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM
    MS27488 Revision N:2008 PLUG, END SEAL, ELECTRICAL CONNECTOR
    MIL-STD-1553 Revision B:1978 DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA
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