MIL-W-5088 Revision L:1991
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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)
04-01-1998
05-10-1991
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
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DocumentType |
Standard
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Pages |
88
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PublisherName |
US Military Specs/Standards/Handbooks
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Status |
Superseded
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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 |
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 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 SPECIFICATIONS 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 |
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-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 |
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, 4,000 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 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 |
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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