MIL-STD-143 Revision B:1969
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
Available format(s)
PDF
Superseded date
23-07-2013
Publisher
This standard is suitable for use in specifications when it is necessary to control the design selection of items, materials, and processes not definitely specified.
| DevelopmentNote |
Supersedes MIL STD 1471 (B). (09/2010)
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| DocumentType |
Standard
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| Pages |
11
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| SupersededBy |
| MIL-R-85895 Base Document:1988 | RACK, BOMB EJECTOR, AIRCRAFT BRU-32/A |
| MIL-A-85802 Base Document:1986 | ACTUATOR, ELECTROMECHANICAL, LINEAR |
| MIL-W-17316 Revision A:1980 | WIND MEASURING SET AN/PMQ-30 (COMPONENTS OF) |
| SAE AS 8568 : 2012 | BINOCULARS, PRISMATIC, HAND-HELD (FOR AERONAUTICAL USE) (7 X 50 AND 6 X 42 (WIDE FIELD)) |
| MIL C 83166 : LATEST | CONVERTER MULTIPLEXER, SIGNAL DATA, GENERAL SPECIFICATION FOR |
| MIL C 38240 : C | COMPUTER, ALTITUDE, ALTITUDE ENCODING CPU 66, GENERAL SPECIFICATION FOR AND MTU 39/A MOUNTING TRAY |
| MIL-I-8580 Revision B:1965 | INDICATOR, TACHOMETER, HELICOPTER, 0-4000 RPM TYPE MA 1 |
| MIL-I-18856 Revision B:1969 | INDICATOR, ANGLE OF ATTACK, 28V DC MS28062 AND MS28067 |
| MIL-A-38307 Revision A:1981 | ACCELEROMETER, AIRCRAFT, MX-6663/AJB-7 |
| MIL-T-38034 Revision E:1970 | TIMER, FIRE CONTROL, BOMBING, DUAL |
| MIL-I-83294 Base Document:1971 | INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-P-81655 Base Document:1970 | PITOT STATIC TUBE, L-SHAPED, COMPENSATED, ELECTRICALLY HEATED, GENERAL SPECIFICATION FOR |
| MIL T 5578 : C | TANK, FUEL, AIRCRAFT, SELF-SEALING |
| MIL L 24554 : 0 | LAMPS MK III INTERFACE SIGNAL SWITCHING SET |
| MIL H 26385 : E | HOSE, OXYGEN AND PRESSURIZATION, OZONE RESISTANT |
| SAE AS 5604 : 2012 | COMPASS: MAGNETIC, PILOT'S STANDBY |
| MIL-A-26846 Revision B:1984 | AIR CONDITIONER, A/M32C-4, TRAILER MOUNTED, VAPOR CYCLE, ELECTRIC, MOTOR DRIVEN |
| MIL-I-7062 Revision C:1975 | INDICATOR, POSITION, CONTROL SURFACES, 28 VOLT DC, GENERAL SPECIFICATION FOR |
| MIL-C-5809 Revision G:1987 | CIRCUIT BREAKERS, TRIP-FREE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL T 6396 : E | TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
| DOD STD 100 : C NOTICE 6 | ENGINEERING DRAWING PRACTICES |
| MIL T 27252 : A | TEST SET, SYNCHRO, TTU-73/E DC SELSYN, AIRCRAFT INSTRUMENTS |
| MIL-P-26292 Revision C:1969 | PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF |
| MIL-T-83460 Base Document:1975 | TRANSDUCER, MOTIONAL PICKUP TRU-164/A |
| MIL-R-81202 Revision D:1981 | RECEIVER ASSEMBLY, NITROGEN, FOR LAU-7 SERIES LAUNCHERS |
| MIL-I-83152 Revision B:1974 | INDICATOR, INDICATED-AIRSPEED AVU-22/A (INDICATOR-TRANSDUCER) |
| MIL-L-6503 Revision H:1975 | LIGHTING EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATION FOR INSTALLATION OF |
| MIL-T-26561 Revision C:1984 | TESTER, TYPE MA-2 RECEPTION COUPLING BREAK-AWAY FORCE, PORTABLE |
| MIL-O-23678 Revision B:1982 | Oxygen Systems, Portable, High Pressure, Aircraft |
| MIL I 25688 : A | INDICATOR, ELECTRICAL TACHOMETER ERU-3/A. CRANKSHAFT SPEED 500-4,000 RPM, 3 1/4 INCH SIZE |
| MIL D 83320 : 0 | DETECTOR, MAGNETIC AZIMUTH DSU-14/A |
| MIL C 38214 : B | COMPASS, MAGNETIC,MOUNTED |
| MIL-P-9388 Revision B:1986 | PUMP, PRESSURE, OIL FREE AIR TYPE MA-2 |
| MIL-T-5483 Revision D:1964 | TRANSMITTER, PRESSURE, SYNCHRO AIRCRAFT 165 DEGREE MOVEMENT |
| MIL-C-27298 Revision B:1980 | CLOCK, AIRCRAFT, MECHANICAL ABU AND 9-A |
| MIL-B-49436 Revision B:1993 | BATTERIES, RECHARGEABLE, NICKEL CADMIUM, SEALED |
| MIL-T-38473 Revision A:1972 | TIMER, PRECISION, BOMBING, 0 - 30 MINUTES |
| MIL-F-85421 Revision B:1986 | FITTINGS, TUBE, FLUID SYSTEMS, SEPARABLE, BEAM SEAM, 3000/4000 PSI - GENERAL SPECIFICATION FOR |
| MIL-C-8605 Revision B:1990 | CAP, PRESSURE FUEL SERVICING |
| MIL-P-85833 Base Document:1989 | PROTECTIVE ASSEMBLY, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL |
| MIL-A-38140 Revision B:1977 | ALTIMETER, PRESSURE AAU-16/A |
| MIL B 81757 : C | BATTERIES & CELLS STORAGE, NICKEL CADMIUM, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL C 27536 : B | COUPLING, CLAMP, GROOVED, V-BAND |
| MIL-C-27505 Revision B:1967 | Cartridge, Engine Starter MXU-4A/A |
| MIL-G-25597 Revision D:1973 | GYROSCOPE, DISPLACEMENT, ROLL AND PITCH, TYPE MD-1 |
| MIL-STD-838 Revision C:1983 | LUBRICATION OF MILITARY EQUIPMENT |
| MIL-STD-482 Revision A:1974 | CONFIGURATION STATUS ACCOUNTING DATA ELEMENTS AND RELATED FEATURES |
| MIL-L-50794 Base Document:1973 | LINEAR SHAPED CHARGE ASSEMBLY |
| SAE AS 8181 : 1997 | DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-B-8568 Revision B:1967 | BINOCULAR, PRISMATIC, HAND-HELD [FOR AERONAUTICAL USE] 7 X 50 AND 6 X 42 WIDE FIELD [ASG] |
| MIL-I-6726 Revision B:1966 | Inclinometer, Aircraft |
| MIL-T-27305 Revision C:1987 | TRANSFORMER AND INDUCTORS [AUDIO, POWER AND HIGH POWER PULSE] INDUCTOR, POWER TF5S04ZZ |
| MIL H 27267 : B | HOSE TETRAFLUOROETHYLENE, HIGH TEMPERATURE, MEDIUM PRESSURE |
| 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 C 38359 : A | CABLE, POWER, ELECTRICAL, AIRPORT LIGHTING, CROSS-LINKED, POLYETHYLENE XLP |
| MIL T 27535 : A | TRANSFORMER, POWER, ISOLATION, SERIES CIRCUIT, AIRPORT LIGHTING, GENERAL SPECIFICATION FOR |
| MIL-M-7255 Revision B:1969 | MANOMETER, PRESSURE, DIFFERENTIAL AND ABSOLUTE TYPE E 1 |
| MIL-A-85072 Revision A:1987 | ACTUATOR, ELECTROMECHANICAL, LINEAR |
| MIL-I-27709 Revision A:1962 | INDICATOR, ATTITUDE ARU-14/A, REMOTE |
| MIL-E-5627 Revision B:1965 | EXTINGUISHERS, FIRE, CARBON DIOXIDE, PORTABLE |
| MIL P 83207 : B | PITOT STATIC TUBE, NOSE BOOM, COMPENSATED, GENERAL SPECIFICATION FOR |
| MIL-T-26922 Revision D:1977 | TEST SET, ELECTRICAL POWER A/M24T-8() |
| MIL-A-55503 Base Document:1966 | ATTITUDE HEADING REFERENCE SET AN/ASN-76 |
| MIL-P-6457 Revision E:1974 | POWER SUPPLY, METALLIC RECTIFIER TYPE, GENERAL SPECIFICATION FOR |
| MIL-I-38338 Revision D:1991 | INDICATOR, OIL QUANTITY, CONTINUOUS TRANSMISSION, NUCLEONIC |
| MIL-D-82687 Base Document:1980 | DEVICE, ARMING FIRING, ROCKET MOTOR MARK 298 MOD O |
| MIL F 85406 : 0 | FUSE SYSTEM, JOINT SERVICE ELECTRONIC BOMB FMU-139/B |
| MIL V 85855 : 0 | VALVE, QUICK DISCONNECT, FOR THE PROTECTIVE ASSEMBLY, CHEMICAL, RADIOLOGICAL |
| MIL-I-27196 Revision C:1988 | INDICATOR, VERTICAL VELOCITY AAU-9/A, INTEGRALLY LIGHTED |
| MIL V 27166 : D | VALVE, PRESSURE EQUALIZING, GASEOUS PRODUCTS |
| MIL T 25620 : C | TESTER, OXYGEN MASK, HEADSET AND MICROPHONE, TYPE MQ-1A |
| MIL I 27279 : B | INDICATOR, MACH NUMBER AVU-11/A, INTEGRAL LIGHTING |
| MIL-C-5499 Revision B:1984 | CORE, AIRCRAFT, HIGH PRESSURE AIR VALVE |
| MIL-I-27202 Revision A:1980 | INDICATOR, ELECTRICAL TACHOMETER, 0-110 PERCENT RPM 2-INCH SIZE, INTEGRALLY LIGHTED |
| MIL B 83424 : 0 | BATTERY SYSTEMS, SEALED CELL, NICKEL CADMIUM, INTEGRAL CHARGE CONTROL, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-81724 Base Document:1969 | ADAPTER, LAUNCHER, AIRCRAFT, ADU-299/E |
| MIL M 7584 : A | METER, FUEL FLOW SYNCHRO STYLE TYPE B 3A |
| MIL-C-23367 Base Document:1963 | COMPUTER, FLIGHT DIRECTOR, AIRCRAFT |
| SAE AS 7997:1999 | MOTORS, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT - GENERAL SPECIFICATION FOR |
| MIL-A-23121 Revision C:1970 | AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR |
| MIL-B-5087 Revision B:1964 | BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
| MIL-C-6985 Revision B:1966 | CLAMP, HOSE |
| MIL-C-19179 Revision B:1963 | COUPLING ASSEMBLY, QUICK-DISCONNECT, FUEL |
| 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 |
| MIL-S-6451 Revision E:1977 | SHIELD, PROTECTIVE, AIRCRAFT AND MISSILES |
| MIL-H-8775 Revision D:1976 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
| MIL-A-83477 Revision A:1976 | AIR CONDITIONER, A/M32C-18 TRAILER MOUNTED, DIESEL ENGINE DRIVEN |
| MIL-HDBK-508 Base Document:1998 | WIRING AND WIRING DEVICES FOR COMBAT AND TACTICAL VEHICLES, SELECTION AND INSTALLATION OF |
| MIL-S-503 Revision B:1988 | SIREN, ELECTRIC, 2 AND 5 HORSEPOWER |
| MIL-STD-339 Base Document:1987 | WIRING AND WIRING DEVICES FOR COMBAT AND TACTICAL VEHICLES, SELECTION AND INSTALLATION OF |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-C-85521 Base Document:1983 | CONCENTRATOR, OXYGEN, GGU-7/A |
| MIL-C-85829 Base Document:1989 | COUPLING ASSEMBLY, HOSE, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE |
| MIL-S-26547 Revision C:1985 | STARTER-GENERATOR ENGINE STU-6A |
| MIL-L-7806 Revision A:1956 | LIGHT, PANEL, PLASTIC PLATE, LIGHTING |
| MIL-STD-2097 Revision A:1989 | ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
| MIL-M-8609 Revision B:1965 | MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-E-4158 Revision E:1973 | ELECTRONIC EQUIPMENT, GROUND GENERAL REQUIREMENTS FOR |
| MIL-STD-2156 Base Document:1983 | LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| MIL C 87104 : 0 | COAXIAL ASSEMBLIES, GENERAL SPECIFICATION FOR |
| MIL-G-83872 Revision A:1977 | GYROSCOPE, DISPLACEMENT, TYPE SBU-23/A |
| MIL-T-38049 Revision A:1972 | TRANSMITTER, PRESSURE TRU 60A |
| MIL E 27005 : A | EXPLOSIVE KIT, PARACHUTE RELEASE MLU-5/B AND EXPLOSIVE KIT, PARACHUTE RELEASE MLU-7/B |
| MIL I 38120 : A (3) | INDICATOR, RATE OF FLOW AND TRANSFER EFU 20/A |
| MIL-S-25392 Revision B:1968 | SANDWICH CONSTRUCTION, PLASTIC RESIN, GLASS FABRIC BASE, LAMINATED FACINGS AND POLYURETHANE FOAMED-IN-PLACE CORE, FOR AIRCRAFT STRUCTURAL APPLICATIONS |
| MIL-C-7413 Revision B:1970 | COUPLING, QUICK DISCONNECT, AUTOMATIC SHUTOFF, GENERAL SPECIFICATION FOR |
| SAE AS 6451 : 2013 | SHIELDS, PROTECTIVE, AIRCRAFT AND MISSILES |
| MIL H 83796 : 0 | HOSE ASSEMBLY, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
| MIL-C-81093 Revision B:1984 | CARTRIDGES, EXPLOSIVE BOLT, (FOR TORPEDOES MARK 46 ALL MODS) |
| MIL-C-83124 Base Document:1969 | CARTRIDGE ACTUATED DEVICES PROPELLANT ACTUATED DEVICES GENERAL DESIGN SPECIFICATION FOR |
| MIL-E-50796 Base Document:1973 | EXPANDING SHIELDED MILD DETONATING CORD ASSEMBLY |
| MIL T 38170 : F | TANK, MOBILE STORAGE, LIQUID OXYGEN TMU 27/M |
| MIL C 7958 : A | CONTROL, PUSH PULL, FLEXIBLE AND RIGID |
| MIL-A-81918 Base Document:1976 | ADAPTER, LAUNCHER, AIRCRAFT, ADU-299A/A |
| MIL P 81716 : 0 | PACKING, PREFORMED, STRAIGHT THREAD TUBE FITTING BOSS, TYPE II HYDRAULIC (MINUS 65 DEG F TO PLUS 275 DEG F) |
| MIL-C-29025 Revision A:1978 | COMMUNICATIONS SYSTEMS FOR TRAINING DEVICES, GENERAL SPECIFICATION FOR |
| MIL-T-52497 Revision A:1972 | TRANSFORMER, POWER ISOLATION, SERIES CIRCUIT AIRPORT LIGHTING 6.6/6.6 AMPERES. |
| 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 B 38608 : A | BOMB, FIRE, BLU-23/B |
| MIL-I-25091 Revision B:1985 | INDICATOR, CABIN AIR PRESSURE, PRESSURIZED AIRCRAFT, 1-7/8 INCH DIAL, TYPE MA-2 |
| MIL R 83178 : A | REGULATOR, OXYGEN, DILUTER DEMAND, AUTOMATIC PRESSURE BREATHING, GENERAL SPECIFICATION FOR |
| MIL C 6458 : C | CHAIN ASSEMBLY, SINGLE LEG, AIRCRAFT CARGO TIE DOWN |
| MIL V 7899 : C | VALVE, CHECK, AIRCRAFT FUEL SYSTEM |
| MIL-G-23337 Base Document:1962 | GAGE - PRESSURE, DIAL INDICATING |
| MIL G 26611 : D | GENERATOR, TACHOMETER GEU-7/A, MINIATURE |
| MIL-A-6589 Revision A:1968 | AMPLIFIER, ELECTRONIC CONTROL, SINGLE CHANNEL, TYPE A-2 |
| MIL-H-4495 Revision D:1985 | HOSE ASSEMBLY, RUBBER, AERIAL REFUELING |
| MIL-A-83469 Base Document:1976 | ADJUSTER, LAP BELT, 1-3/4 INCH WEBBING |
| MIL-A-85481 Base Document:1981 | ARMING WIRE ASSEMBLIES |
| MIL P 26517 : A | POWER SUPPLY, TRANSFORMER-RECTIFIER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-M-87977 Base Document:1987 | MAINTENANCE PLATFORM, AIRCRAFT |
| MIL-A-23670 Revision A:1965 | ATTITUDE HEADING REFERENCE SYSTEM AN/ASN-50(*) |
| MIL-B-26220 Revision D:1974 | BATTERIES, STORAGE, AIRCRAFT, NICKEL-CADMIUM GENERAL SPECIFICATION FOR |
| MIL T 25446 : D | TRANSMITTER, TEMPERATURE, ELECTRICAL RESISTANCE |
| MIL S 25057 : B | SCREEN SYSTEM, AIR INLET, AIRCRAFT TURBINE ENGINE, GENERAL SPECIFICATION FOR |
| MIL-I-5133 Revision C:1953 | INDICATOR, ATTITUDE TYPE J 8 |
| MIL-B-83769 Revision D:1983 | BATTERY, STORAGE, LEAD ACID, GENERAL SPECIFICATION FOR |
| MIL-C-47267 Base Document:1974 | CLEANING & SURFACE PREPARATION, VAPOR BLAST |
| MIL-S-8512 Revision D:1974 | SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
| MIL-C-5604 Revision B:1962 | COMPASS, MAGNETIC, PILOTS STANDBY |
| MIL-T-26017 Revision C:1972 | TEST STAND, HYDRAULIC SYSTEM COMPONENTS, TYPE MK-3A (STAND, TEST, AIRCRAFT HYDRAULIC SYSTEM, ELECTRIC MOTOR DRIVEN, TYPE MK-3A) |
| MIL-S-85377 Revision A:1983 | SWITCH, STEPPING, DIRECT CURRENT AIRCRAFT DISPENSER |
| MIL-E-7080 Revision B:1962 | ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
| MIL-C-85019 Base Document:1976 | COMPUTER, AIR NAVIGATION, TRUE AIRSPEED, MACH NUMBER, WIND COMPONENTS SUPERSONIC, TYPE MB-9 |
| MIL-C-9082 Revision H:1986 | CONVERTER, OXYGEN, AIRCRAFT, LIQUID TO GASEOUS, GENERAL SPECIFICATION FOR |
| MIL-S-6150 Revision D:1987 | STARTER, ENGINE, ELECTRICAL, DIRECT CRANKING, AIRCRAFT 28 VOLT DC |
| MIL-S-83427 Base Document:1974 | SURVIVAL KIT CONTAINERS, CNU-129(V)/P AND CNU-130/P |
| MIL L 58085 : A | LIGHT, BEACON, ANTI COLLISION AIRCRAFT |
| MIL B 38672 : A | BOMB, FRAGMENTATION, PARTS KIT FOR: BLU-24 OR BLU-66 |
| MIL-H-8890 Base Document:1961 | HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG] |
| MIL-P-8564 Revision D:1970 | PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
| MIL B 8075 : D | BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
| MIL-M-85831 Base Document:1989 | MASK, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE, NON-OXYGEN |
| SAE AS 17852 : 2012 | REDUCERS, OXYGEN PRESSURE |
| MIL-E-11991 Revision E:1983 | ELECTRONIC, ELECTRICAL, AND ELECTRO-MECHANICAL EQUIPMENT, GUIDED MISSILE AND ASSOCIATED WEAPON SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL I 38715 : B | INDICATOR, COMBUSTIBLE GAS AND TOXIC GAS |
| MIL-S-83129 Revision A:1972 | SPECTROMETER, FLUID ANALYSIS A/E35U-3 |
| MIL-C-38373 Revision B:1975 | CAP, FLUID TANK FILLER |
| MIL S 83352 : B | SIGNAL KIT, PERSONNEL, DISTRESS, A/P25S-5A |
| MIL C 4928 : A | CHARGER, BATTERY, SILICON DIODE, TYPE A-1 |
| MIL-M-82433 Revision A:1972 | MOTOR, DIRECT CURRENT)(FOR TORPEDO MK 46 MOD 1) |
| MIL-T-9720 Revision F:1984 | Truck, Lift, Aerial Stores, 3000 Pounds Capacity MJ-1A and MJ-1B |
| MIL H 38390 : C | HOSE ASSEMBLY, TETRAFLUOROETHYLENE PNEUMATIC, HIGH PRESSURE |
| MIL-L-38200 Revision B:1966 | LIFE PRESERVER, UNDERARM, ADULT LPU 5/P |
| MIL-R-85880 Base Document:1988 | ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL-S-6330 Revision H:1965 | SURVIVAL KIT, LIFE RAFT |
| MIL-M-9397 Revision E:1979 | FREQUENCY CONVERTER, MOBILE, TYPE MC-1A |
| MIL-I-6447 Revision C:1974 | INDICATOR, TRUE AIRSPEED TYPE M 1A |
| MIL-I-5418 Revision B:1963 | INDICATOR: AIRSPEED, PITOT STATIC, SENSITIVE, 50-650 KNOTS |
| 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 |
| MIL T 5421 : B | TUBE, PITOT, ELECTRICALLY HEATED, AIRCRAFT |
| MIL-M-7997 Revision C:1981 | MOTOR, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT GENERAL SPECIFICATION FOR |
| MIL-I-18802 Revision A:1962 | INSTALLATION OF FUEL AND OIL LINES, AIRCRAFT |
| MIL-I-85506 Base Document:1983 | INDICATOR, INDICATED AIRSPEED, STANDBY TYPES I, II, AND III |
| MIL-S-83576 Base Document:1974 | SOLAR CELL ARRAYS, SPACE VEHICLE, DESIGN AND TESTING, GENERAL SPECIFICATION FOR |
| MIL-I-83751 Base Document:1967 | INDICATOR, SAFETY LEVEL, RF |
| MIL-S-85510 Base Document:1981 | |
| MIL-S-7852 Revision B:1968 | SEAT, AIRCREW, ADJUSTABLE SWIVEL TYPE E-1 |
| MIL-B-26793 Revision B:1958 | BLOWER, GASOLINE ENGINE DRIVEN, TYPE A-1 |
| MIL-A-26107 Revision D:1960 | AIR CONDITIONER, TRAILER-MOUNTED, FREON CYCLE, 11-1/2 TON REFRIGERATING CAPACITY, TYPE MA-3 |
| SAE ARP 4729 : 2017 | DOCUMENT FOR 270 VOLTAGE DIRECT CURRENT (270 V DC) SYSTEM |
| MIL-A-38331 Base Document:1964 | AMPLIFIER-POWER SUPPLY AM-4080/ASN-55, LEVELLING |
| MIL-T-81272 Base Document:1966 | THERMOCOUPLE, ENGINE, CYLINDER, BAYONET TYPE, MS90324 |
| MIL-V-8610 Revision B:1984 | VALVE, FUEL SHUTOFF SOLENOID OPERATED, 28 VOLT, DC |
| MIL-HDBK-838 Base Document:1997 | LUBRICATION OF MILITARY EQUIPMENT |
| MIL-I-27273 Revision A:1965 | INVERTER, POWER, STATIC, GENERAL SPECIFICATION FOR |
| MIL V 8057 : F | VALVE, OXYGEN, PRESSURE BUILDUP AND VENT |
| MIL-B-87983 Base Document:1988 | BAR, PRY, WHEELED TYPE, HAND OPERATED, MA-1, COMMERCIAL |
| MIL F 26685 : B NOTICE 1 | FLIGHT DIRECTOR SYSTEM, DESIGN AND INSTALLATION OF |
| MIL F 83296 : 0 | FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, HIGH PRESSURE (3,000 PSI HYDRAULIC AND PNEUMATIC) |
| MIL-A-7237 Revision B:1975 | AIR INDUCTION SYSTEM, RECIPROCATING ENGINE, GENERAL SPECIFICATION FOR |
| MIL-S-9487 Revision C:1985 | SWITCH, TRIGGER, SINGLE POLE, TWO STAGE, MOMENTARY |
| MIL V 87223 : 0 | VALVE, PRESSURE, ANTI-G SUIT, MXU-804/A AND MXU-805/A |
| SAE AS 18802 : 2013 | FUEL AND OIL LINES, AIRCRAFT, INSTALLATION OF |
| MIL-A-83216 Revision B:1976 | AIR CONDITIONER A/E32C-39 |
| MIL-V-5461 Revision C:1977 | VALVE, VACUUM BREAKING |
| MIL-T-7771 Revision B:1980 | TUBE, EXTENSION, GYRO STABILIZED DRIFT METER |
| MIL I 82356 : NOTICE 1 | INSTRUMENTS, SIMULATED, FOR AIRCRAFT TRAINING DEVICES; GENERAL SPECIFICATION FOR |
| MIL I 85581 : 0 | INTERVALOMETER, ROCKET LAUNCHER, REUSABLE |
| MIL-C-7474 Revision E:1978 | CASTER, INDUSTRIAL |
| MIL-A-81852 Revision A:1986 | ALTIMETER-ENCODER AAU-32/A |
| MIL-I-22075 Revision C:1984 | Indicator, Bearing-Distance-Heading ID-663D/U |
| MIL-V-8712 Revision A:1965 | VALVE, AIR RELIEF, LOW PRESSURE |
| MIL-I-85832 Base Document:1989 | INTERCOM, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE SET |
| MIL-R-47321 Base Document:1987 | REGULATOR, PRESSURE |
| MIL-M-4871 Revision C:1984 | MAINTENANCE PLATFORM |
| MIL-C-4952 Revision E:1988 | CARTRIDGES, DESICCANT, DEHYDRATOR |
| MIL-H-7365 Revision D:1986 | HOSE, AIR DUCT, FOR GROUND HEATERS |
| MIL-R-38162 Revision B:1971 | RADIOSONDE SET AN/AMT 13 |
| MIL C 22263 : B | COUPLING FUEL LINE, FLEXIBLE, 125 PSI, GENERAL SPECIFICATION FOR |
| MIL-A-38202 Revision C:1972 | AIRCRAFT ARRESTING SYSTEM BAK-12A/E32A; PORTABLE, ROTARY FRICTION |
| MIL W 5846 : C | WIRE, ELECTRICAL, CHROMEL AND ALUMEL, THERMOCOUPLE |
| MIL S 25073 : 0 | |
| MIL-H-85042 Revision A:1983 | HOOKS, BOMB RACK, GENERAL SPECIFICATION FOR |
| MIL-V-85033 Revision A:1981 | VALVE CHARGING |
| MIL-C-7460 Revision A:1971 | CHROMIUM PLATING, POROUS CHANNEL TYPE, AIRCRAFT ENGINE CYLINDERS, GENERAL SPECIFICATIONS FOR |
| MIL-T-21578 Revision A:1966 | TEST EQUIPMENT, HAZARDOUS LOCATION, INSTALLED, BASIC REQUIREMENTS FOR |
| MIL-C-87987 Base Document:1989 | CRANE, HYDRAULIC, WHEEL MOUNTED, 7.5 & 15 TON CAPACITIES |
| MIL-R-5520 Revision C:1964 | RESERVOIRS, AIRCRAFT, HYDRAULIC, NON-SEPARATED TYPE |
| MIL T 25439 : A (1) | TRANSMITTER, RATE OF FLOW, IN-FLIGHT REFUELLING, 0-10,000 PPM, TYPE MB-3 |
| MIL B 8598 : A (1) | BULB, ELECTRICAL RESISTANCE, THERMOMETER, FREE AIR |
| MIL-A-81851 Revision B:1986 | ALTIMETER AAU-31/A |
| MIL-C-83864 Revision A:1982 | CONTAINER, INNER, SURVIVAL KIT |
| MIL-T-27200 Revision C:1975 | TRANSMITTER, RATE GYROSCOPE TRU-2A/A |
| MIL-P-27965 Base Document:1967 | PLOTTING SET, THEODOLITE ML-625/GM |
| MIL-G-85468 Base Document:1981 | GENERATOR CONTROL INDICATOR SG-118/AST-4(V) |
| MIL C 19328 : E | CONVERTER, LIQUID OXYGEN, 5 LITER, MBA-5A |
| SAE AS 1297 : 2008(S2014) | REDUCERS, PNEUMATIC PRESSURE, MISSILE |
| NASA STD 3000 VOL 2 : 1995 | MAN-SYSTEMS INTEGRATION STANDARDS - VOLUME 2 |
| MIL-F-8615 Revision D:1976 | FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
| MIL-L-25798 Revision D:1984 | LIFE PRESERVER, UNDERARM, CASUALTY, TYPE MB-1 |
| MIL G 6162 : B | GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION |
| MIL C 4710 : D | CASE SET, TRANSPORT AND STORAGE |
| MIL-A-23622 Base Document:1963 | ACTUATOR, AIRCRAFT, ELECTRO-MECHANICAL, LINEAR, DIRECT CURRENT |
| MIL H 26633 : C | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, OXYGEN |
| MIL I 5099 : B | INDICATOR CABIN AIR PRESSURE, 1-7/8 INCH DIAL, TYPE MA-1 |
| MIL I 25725 : A | INDICATOR, TORQUE PRESSURE, MAGNESYN STYLE, SINGLE CLAMP MOUNTED, 2 IN SIZE, 50-400 PSI TYPE A-8 |
| MIL-I-18804 Revision B:1964 | INDICATOR, VERTICAL SPEED, 0 - 6000 FPM, 2 INCH |
| MIL C 83438 : 1986 | CLOTHING OUTFITS, EXTREME COLD WEATHER SURVIVAL |
| MIL L 27639 : C (2) | LIFE PRESERVER INFLATING ASSEMBLY FLU-1A/P |
| NASA MSFC SPEC 250 : 1963 | PROTECTIVE FINISHES FOR SPACE VEHICLE STRUCTURES AND ASSOCIATED FLIGHT EQUIPMENT GENERAL SPECIFICATION FOR |
| MIL-M-6404 Revision A:1965 | METER, VOLUMETRIC, POSITIVE DISPLACEMENT LIQUID, TYPE F 1 AIRCRAFT FUEL 300 GALLONS PER MINUTE |
| SAE AS 85352 : 2011 | INFLATOR ASSEMBLY AND GAGE ELEMENTS, PNEUMATIC PRESSURE, REMOTE CONTROL, DIRECT READING |
| MIL I 38135 : B (3) | INDICATOR, INDICATED AIRSPEED AVU 19/A STANDBY |
| MIL G 8360 : A | GAGE, PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE, 10-75 IN MERCURY TYPE MB 1 |
| MIL-D-38386 Revision E:1989 | DUCT ASSEMBLY, GROUND, CONDITIONED AIR, INSULATED, FLEXIBLE |
| MIL C 27019 : B | CARTRIDGE KIT, BOMB EJECTION MLU-9/B |
| MIL-G-82455 Base Document:1966 | Generator, Gas |
| MIL-B-19906 Revision A:1961 | BOMB RACK AND ROCKET LAUNCHER, COMBINATION, AERO 15 SERIES |
| MIL-L-21652 Revision A:1964 | LIGHT, BEACON, ANTI COLLISION AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL-H-21722 Revision B:1992 | HOOK, THRUST STABILIZING, JATO-45OO POUNDS NOMINAL THRUST |
| MIL-I-26689 Revision C:1981 | INDICATOR, HORIZONTAL SITUATION, AQU-2/A |
| MIL-I-58067 Revision A:1977 | INDICATOR, VERTICAL VELOCITY, RAPID RESPONSE ACCELERATION SENSITIVE, GENERAL SPECIFICATION FOR |
| MIL-R-28894 Base Document:1986 | RELAY, HYBRID OR SOLID STATE, SENSORS, ESTABLISHED RELIABILITY GENERAL SPECIFICATION FOR |
| MIL-N-3336 Revision A:1964 | NUT, SHEET SPRING, INSTRUMENT MOUNTING |
| MIL-W-5845 Revision C:1973 | WIRE, ELECTRICAL, IRON AND CONSTANTAN, THERMOCOUPLE |
| MIL-S-6551 Revision A:1981 | |
| MIL-A-5034 Revision B:1979 | ADAPTER, BOMB RACK, 30-INCH, AERO 1A |
| MIL-I-25931 Revision B:1964 | INDICATOR, POSITION, LANDING GEAR, SYMBOL-INDICATING, INTEGRALLY LIGHTED |
| MIL M 7793 : F | METER, TIME TOTALIZING |
| MIL-A-25915 Revision A:1980 | ACCELEROMETER, AIRCRAFT, PILOTS WARNING, TYPE MA-2 |
| MIL C 27889 : D | COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING, CPU-46/A, GENERAL SPECIFICATION FOR AND MTU-38/A MOUNTING TRAY |
| MIL-P-82459 Base Document:1966 | PRESSURE TRANSDUCER (FOR TORPEDO MK 46 MOD 0 AND MOD 1) |
| MIL-I-85352 Base Document:1980 | INFLATOR ASSEMBLY AND GAGE ELEMENTS, PNEUMATIC PRESSURE REMOTE CONTROL, DIRECT READING |
| MIL-G-81168 Base Document:1964 | GYROSCOPE, RATE INTEGRATING |
| MIL-C-81991 Base Document:1975 | CONVERTER, AIRCRAFT DC TO DC, BOOST GENERAL SPECIFICATION FOR |
| MIL E 83425 : 0 | EARCUP, SOUND PROTECTIVE MX-8376/AR GENERAL SPECIFICATION FOR |
| MIL-S-58095 Revision A:1986 | SEAT SYSTEM: CRASH RESISTANCE, NON-EJECTION, AIRCREW, GENERAL SPECIFICATION FOR |
| MIL-A-83462 Base Document:1975 | ARCTIC CUSHIONS - CLOTHING, CHU-10/P AND CHU-11/P |
| MIL I 25137 : A | INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED, TYPE ME-4 |
| MIL-C-26485 Revision D:1968 | CONTROL ASSEMBLY, ATTITUDE, GYROSCOPIC AF/A24G-1A |
| MIL-R-23761 Revision B:1975 | Regulators, Voltage, and Control Panels Aircraft, Direct Current Generator, General Specification for |
| MIL-I-22126 Revision B:1972 | INDICATOR, TORQUEMETER, ENGINE, TURBOPROP |
| MIL I 83452 : LATEST | INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
| MIL R 83725 : B | RELAY, VACUUM, GENERAL SPECIFICATION FOR |
| MIL-B-81949 Base Document:1974 | BRUSHES, FLAP, ROTARY, ABRASIVE, GENERAL SPECIFICATION FOR |
| MIL-T-26639 Revision C:1969 | TESTER, TORQUE WRENCH |
| MIL A 25088 : C | |
| MIL-B-87167 Base Document:1985 | BELT, AIRCRAFT SAFETY, HBU-12/A |
| MIL-I-25861 Revision D:1967 | INDICATOR, PRESSURE, HYDRAULIC, 0-4000 PSI INTEGRALLY LIGHTED |
| MIL-S-5804 Revision C:1967 | SEAT, AIRCRAFT, TROOP, WALL STYLE |
| MIL C 25478 : B | COOLER, LUBRICATING OIL, AIRCRAFT ENGINE, SYNTHETIC OIL, GENERAL SPECIFICATION FOR |
| MIL-B-3402 Revision C:1984 | BLOWER, GASOLINE-DRIVEN, AIRCRAFT VENTILATION, PORTABLE 2,900 CFM TYPE A-2 |
| MIL C 27715 : 0 | CIRCUIT BREAKER, TRIP-FREE, HIGH TEMPERATURE, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL-P-38027 Revision A:1973 | PRESSURE INDICATING SYSTEM, HYDRAULIC A/A27 J-1 |
| MIL-S-26716 Revision A:1982 | STAND, TEST, AIRCRAFT HYDRAULIC SYSTEMS, NON-PORTABLE |
| MIL G 8348 : H | GAGE, ASSEMBLIES, AIR PRESSURE, DIAL INDICATING CHUCK TYPE SELF CONTAINED |
| MIL-C-87150 Base Document:1980 | CLOTHING OUTFIT, EXTREME COLD WEATHER SURVIVAL A/P22S-18 |
| MIL-F-27656 Revision C:1987 | FILTER UNIT, FLUID, PRESSURE MXU-4O8/M, ABSOLUTE 5 MICRON, HYDRAULIC |
| MIL-C-27718 Revision D:1984 | CRANE, HYDRAULIC, TRUCK MOUNTED, A/S32A-16 16,5OO POUND CRANE CAPACITY, 6X4, DED |
| MIL-C-5026 Revision F:1984 | CUTOUT RELAY, ENGINE GENERATOR |
| MIL-A-25896 Revision E:1983 | ADAPTER, PRESSURE FUEL SERVICING, NOMINAL 2.5 INCH DIAMETER |
| MIL O 38338 : C (1) | OIL QUANTITY GAGING SYSTEM, CONTINUOUS TRANSISTORIZED NUCLEONIC, GENERAL SPECIFICATION FOR |
| MIL-H-27269 Revision A:1977 | HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
| MIL-A-83136 Revision A:1990 | ARRESTING HOOK INSTALLATION, RUNWAY ARRESTING SYSTEM, AIRCRAFT, EMERGENCY |
| MIL C 7989 : B | COVER, LIGHT TRANSMITTING, FOR AERONAUTICAL LIGHTS, GENERAL SPECIFICATION FOR |
| MIL-B-55130 Revision A:1984 | BATTERIES, RECHARGEABLE, NICKEL CADMIUM SEALED |
| MIL C 38618 : A | COUPLER, DRIVE ASSEMBLY GOVERNOR, FUZE BOMB MAU 87A B |
| MIL-C-6499 Revision E:1970 | CLOCK, AIRCRAFT MECHANICAL TYPE A 13A |
| MIL D 38613 : A | DRIVE, ASSEMBLY, ARMING, BOMB FUZE, ATU-35B/B |
| MIL-G-23723 Base Document:1964 | GYROSCOPE, RATE SWITCHING CN-495/AJB-3 |
| MIL-I-23252 Revision B:1981 | INDICATOR, PRESSURE |
| DOD-HDBK-791 Base Document:1988 | MAINTAINABILITY DESIGN TECHNIQUES |
| MIL-S-81771 Revision A:1975 | Seat System; Aircrew, Crash Resistant; General Specification for |
| MIL G 23701 : 0 | MILITARY SPECIFICATION GYROSCOPE, RATE SWITCHING AN/ASN-52 |
| MIL S 38039 : B | SYSTEM, ILLUMINATED, WARNING, CAUTION, AND ADVISORY, GENERAL SPECIFICATION FOR |
| MIL-S-25093 Revision B:1963 | SEA RESCUE KITS, DROPPABLE |
| MIL-C-8412 Revision B:1969 | COMPASS, MAGNETIC, SLAVED GYRO, TYPE J-4 |
| MIL R 83055 : 0 | RAIN REPELLENT DISPENSING SYSTEMS, AIRCRAFT WINDSHIELD, GENERAL SPECIFICATION FOR |
| MIL-W-5908 Revision D:1973 | WIRE, ELECTRICAL, COPPER AND CONSTANTAN, THERMOCOUPLE |
| MIL-C-7488 Revision A:1974 | COOLERS, OIL, PLATE, AIRCRAFT |
| MIL-A-81327 Revision A:1985 | ACOUSTIC LOCATING DEVICE (FOR TORPEDO MK 46 MOD O) |
| MIL-R-7051 Revision A:1966 | RELAY BANK, BOMB SALVO CIRCUIT 3 UNIT, 28 VOLT DC TYPE A 1 |
| MIL-D-8181 Revision B:1965 | DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR |
| MIL-I-81023 Revision D:1985 | INDUCTOR, 28V, D.C. LABORATORY TEST GENERAL SPECIFICATION FOR |
| MIL-B-5046 Revision D:1968 | BOARD, CHART PLOTTING MARK 7 [ASG] |
| MIL I 26359 : B | INDICATOR, ATTITUDE, REMOTE ARU-4/A |
| MIL-P-9389 Revision A:1987 | PUMP PRESSURE, OIL AND FREE AIR, TYPE MA AND 3 |
| MIL-G-83380 Base Document:1979 | GENERATOR SET, GAS TURBINE ENGINE DRIVEN, 30 AND 60 KW, 400 HZ |
| MIL-P-83126 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
| MIL-C-28661 Revision A:1981 | CABLE, POWER, ELECTRICAL, HIGH VOLTAGE |
| MIL P 81305 : A | POWER, DISTRIBUTION PANEL, ALTERNATING CURRENT, F-4 AIRCRAFT, SPECIFICATION FOR |
| MIL-P-85034 Base Document:1976 | POWER PACKAGE, EMERGENCY AC/DC GENERATOR, RAM AIR TURBINE DRIVEN |
| MIL-D-21625 Revision G:1993 | DESIGN AND EVALUATION OF CARTRIDGES FOR CARTRIDGE ACTUATED DEVICES |
| MIL-T-38306 Base Document:1964 | TRANSMITTER, RATE GYROSCOPE T 970/AJB - 7 |
| MIL-B-26026 Revision B:1967 | BATTERY, STORAGE, AIRCRAFT, TYPE MA-2-1 |
| MIL-STD-1174 Revision B:1979 | ASSOCIATED LISTS FOR ARRADCOM ENGINEERING DRAWINGS |
| MIL R 83726 : B | RELAY, HYBRID, TIME DELAY (ON RELEASE), CLASS B, TYPE LIA, HERMETICALLY SEALED, DPDT, 10 AMPERES, ADJUSTABLE TIME DELAY (EXTERNAL RESISTOR)O.1 TO 500 SECONDS |
| MIL V 9050 : E (1) | VALVE, OXYGEN, PRESSURE RELIEF, AIRCRAFT |
| MIL-S-48405 Base Document:1973 | Shielded and Confined Mild Detonating Cord Assemblies |
| MIL-S-38399 Revision A:1975 | STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR |
| MIL-T-38760 Base Document:1966 | TENSIOMETER DIAL INDICATING |
| MIL B 49450 : 0 | BATTERY, RECHARGEABLE, NICKEL CADMIUM, VENTED, AIRCRAFT,BB-716/A |
| MIL C 25369 : C | CYLINDER, CARBON DIOXIDE, FOR INFLATION OF PNEUMATIC LIFE PRESERVERS |
| MIL D 22706 : F | DUCT AND SCUFF COVER, PNEUMATIC, FLEXIBLE |
| MIL-A-27198 Revision B:1987 | ALTIMETER, PRESSURE AAU-7/A |
| MIL-C-9075 Revision A:1968 | COMPUTER AND TRANSMITTER, TRUE AIRSPEED, PITOT STATIC, 150-900 KNOTS, TYPE MA 1 |
| MIL-D-7106 Revision C:1987 | DRIFTMETER, ELECTRICALLY DRIVEN GYRO STABILIZED |
| MIL A 85046 : 0 | ACTUATOR, LINEAR ELECTROMECHANICAL |
| MIL P 83206 : B | PITOT STATIC TUBE, L SHAPED, COMPENSATED, GENERAL SPECIFICATION FOR |
| MIL-F-18870 Revision E:1975 | FIRE CONTROL EQUIPMENT, NAVAL SHIP AND SHORE, GENERAL SPECIFICATION |
| MIL-V-23255 Revision B:1976 | VALVE, PRESSURE RELIEF |
| MIL D 81544 : A | DISPENSER, PARACHUTE FLARE, SUU-44/A |
| MIL I 7491 : B | INDICATOR RATE OF FLOW, FUEL TOTALIZING, SERVO STYLE, TYPE F 1 |
| MIL A 25676 : D | ADAPTOR, PRESSURE LUBRICATING OIL SERVICING, AIRCRAFT |
| MIL F 38363 : B (3) | FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-C-81774 Revision A:1973 | CONTROL PANEL, AIRCRAFT, GENERAL REQUIREMENTS FOR |
| DOD STD 1476 : A | METRIC SYSTEM, APPLICATION IN NEW DESIGN |
| MIL-A-27261 Revision A:1966 | ACCELEROMETER, AIRCRAFT |
| MIL-E-18927 Revision E:1983 | ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
| SAE AIR 4728 : 2013 | REFERENCES, SPACECRAFT AND SPACECRAFT SERVICING, FLUID SYSTEM COMPONENTS (ABBREVIATIONS, ACRONYMS, DEFINITIONS, APPLICABLE DOCUMENTS AND ENVIRONMENTAL CONDITIONS) |
| SAE AS 8712 : 2013 | VALVE; AIR RELIEF, LOW PRESSURE |
| MIL-W-81752 Revision A:1987 | WINDSHIELDED SYSTEM, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR |
| MIL-V-25023 Revision B:1967 | VALVE, FUEL DRAIN, SELF-LOCKING |
| MIL-I-85112 Base Document:1978 | INDICATOR SET, VERTICAL SCALE |
| MIL-T-27-233 Base Document:1978 | TRANSFORMERS AND INDUCTORS (AUDIO POWER AND HIGH POWER PULSE) INDUCTOR CHARGING TF5S37ZZ |
| MIL-A-25933 Revision B:1985 | ALTIMETER, PRESSURIZED COMPARTMENT, INTEGRALLY LIGHTED 0-50,000 FEET, 1-7/8 INCH DIAL |
| MIL C 87148 : 0 | CLOTHING OUTFIT, EXTREME COLD WEATHER SURVIVAL A/P22S-14 |
| MIL-I-25479 Revision A:1987 | INDICATOR, MACH NUMBER, SENSITIVE, SERVOED, RANGE .5 TO 1.O, TYPE ME-5 |
| MIL-A-26360 Revision B:1982 | AMPLIFIER, ELECTRONIC CONTROL ASU-3/A |
| MIL-A-27330 Revision B:1987 | ACCELEROMETER, ELECTRICAL, LINEAR TRU-3/A |
| MIL-B-4173 Revision B:1969 | BENCH, WORK, GENERAL PURPOSE |
| MIL-B-49041 Base Document:1974 | BATTERY, DRY BA-1579/U |
| MIL-T-26609 Revision C:1994 | TRANSMITTER, POSITION |
| MIL-H-23799 Base Document:1963 | HOSE ASSEMBLY, METAL, TRANSFER, LIQUID OXYGEN |
| MIL-G-58103 Base Document:1979 | GRIP ASSEMBLY, CYCLIC CONTROLLER, HELICOPTER |
| MIL-T-27730 Revision A:1964 | TAPE, ANTISEIZE, POLYTETRAFLUOROETHYLENE, WITH DISPENSER |
| MIL-I-27552 Revision C:1995 | INDICATOR, TEMPERATURE, THERMOCOUPLE EHU-15A/A, POTENTIOMETER TYPE, WHITE LIGHTED |
| MIL F 38642 : A | FIN ASSEMBLY, BOMB, MXU-469/B AND MXU-467/B |
| MIL-F-85720 Base Document:1985 | FITTING, TUBE, FLUID SYSTEMS, SEPARABLE, HIGH PRESSURE, DYNAMIC BEAM, SEAL, GENERAL SPECIFICATION FOR |
| MIL-S-21277 Revision A:1958 | SWITCH, LIQUID LEVEL, GENERAL SPECIFICATION FOR |
| MIL A 83366 : 0 | ANTENNA ASSEMBLIES, AIRBORNE, GENERAL SPECIFICATION FOR |
| MIL-S-7470 Revision A:1975 | SHAFT, POWER TRANSMISSION, AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR |
| MIL-T-81838 Base Document:1971 | TANK, FUEL, AIRCRAFT, AUXILIARY EXTERNAL 300 GALLON, TYPE AERO 1D |
| MIL T 83174 : B (3) | TRANSMITTER, ACCELEROMETER, AXIAL |
| MIL H 83298 : A | HOSE, TETRAFLUOROETHYLENE, HIGH TEMPERATURE, HIGH PRESSURE (3000 PSI) HYDRAULIC AND PNEUMATIC |
| MIL S 8932 : A | SWITCH, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-85505 Base Document:1983 | ALTIMETER, STANDBY, TYPES 1 AND 2 |
| MIL C 87149 : 1986 | CLOTHING OUTFIT, EXTREME COLD WEATHER SURVIVAL A/P22S-15 |
| MIL-E-83304 Revision B:1975 | EXTINGUISHER UNIT, FIRE BROMOCHLORODIFLUOROMETHANE, FEU-2/S32P, 40 GALLON CAPACITY, TRUCK MOUNTING |
| MIL-L-85762 Revision A:1988 | LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
| MIL-N-25161 Revision C:1969 | NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
| MIL-G-26988 Revision C:1971 | GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
| MIL-I-83262 Revision B:1977 | INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
| MIL D 26503 : A | DETECTOR, MAGNETIC AZIMUTH AND COMPENSATOR, DETECTOR, MAGNETIC AZIMUTH |
| MIL-I-27680 Revision C:1973 | INDICATOR, ATTITUDE, ARU-12/A, REMOTE |
| SAE AS 85075 : 2000 | TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR |
| MIL-T-49388 Revision A:1983 | TRAY ASSEMBLY, BATTERY CHARGING MX-10154 |
| MIL-P-11268 Revision L:1983 | PART, MATERIALS, AND PROCESSES USED IN ELECTRONIC EQUIPMENT |
| MIL G 38195 : G | GENERATOR SET, GAS TURBINE ENGINE 60 KW 400 HERTZ, GENERAL PURPOSE |
| MIL-I-27623 Revision C:1972 | INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
| MIL-I-7087 Revision A:1968 | INDICATOR, PRESSURE OIL, 0-200 PSI |
| MIL-I-25950 Revision B:1967 | INDICATOR, PRESSURE, OIL, 0-100 PSI |
| MIL-I-7071 Revision B:1972 | INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
| MIL-I-83117 Revision B:1975 | INDICATOR, ANGLE OF ATTACK |
| MIL-P-85315 Base Document:1979 | Pump, Ejector, Air Vehicle Fuel, General Specification For |
| MIL S 9320 : C | SIGNAL, WARNING, AUDIBLE, FOR HEADSET |
| MIL-C-6235 Revision D:1970 | COMPASS, MAGNETIC, UNMOUNTED POCKET SURVIVAL |
| MIL-V-18318 Revision B:1966 | VALVE, PRESSURE REGULATING, OXYGEN SYSTEM |
| MIL F 47299 : A | FAIRING, FRANGIBLE, AIRBORNE ROCKET LAUNCHER FOR 2.75 INCH ROCKET SYSTEM |
| MIL-A-9094 Revision D:1969 | ARRESTER, LIGHTNING, GENERAL SPECIFICATION FOR |
| MIL-G-81065 Revision A:1967 | GYRO-PENDULUM ASSEMBLY (FOR TORPEDO MK 46 MOD O AND MK 46 MOD 1) |
| MIL-I-25941 Revision D:1986 | INDICATOR, TURN AND SLIP, 2-INCH SIZE, INTEGRALLY LIGHTED |
| MIL-T-60530 Revision A:1971 | TECHNICAL DATA PACKAGE FOR AMC MATERIAL |
| MIL-G-27693 Revision A:1962 | GYROSCOPE, DISPLACEMENT SBU-6/A, ROLL AND PITCH |
| MIL M 4803 : D | MOTOR-GENERATOR, 400 HZ PRECISE OUTPUT, GENERAL REQUIREMENTS FOR |
| MIL-I-25645 Revision D:1970 | INDICATOR, LIQUID OXYGEN QUANTITY, CAPACITANCE TYPE, GENERAL SPECIFICATION FOR |
| MIL-G-5678 Revision C:1964 | GAGE PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE |
| MIL-I-7084 Revision A:1988 | INDICATOR, PRESSURE, HYDRAULIC 0-4,000 PSI |
| MIL-P-9400 Revision C:1991 | PLASTIC LAMINATE AND SANDWICH CONSTRUCTION PARTS, AIRCRAFT STRUCTURAL PROCESS SPECIFICATION REQUIREMENTS |
| MIL G 5413 : D NOTICE 1 | GENERATOR, TACHOMETER, FOUR POLE |
| MIL-D-26124 Revision B:1977 | DUCT AND DUCT ASSEMBLY, PNEUMATIC, FLEXIBLE |
| MIL-G-25591 Revision E:1981 | GYROSCOPE, RATE, SWITCHING, TYPE MC-1 |
| MIL-T-7258 Revision B:1985 | TRANSMITTER, TEMPERATURE ELECTRICAL RESISTANCE TYPE B-4 |
| MIL T 25435 : B | TRANSMITTER, PRESSURE, AIRCRAFT, VARIABLE RELUCTANCE TYPE, GENERAL SPECIFICATION FOR |
| MIL-L-6273 Revision D:1983 | LIGHT, NAVIGATIONAL, BEACON, OBSTACLE OR CODE, TYPE G 1 |
| MIL-I-5415 Revision C:1987 | INDICATOR, AIR SPEED, PITOT STATIC PRESSURE GENERAL SPECIFICATION FOR |
| MIL-A-27671 Revision B:1965 | AMPLIFIER-INDICATOR GROUP, ALTITUDE VERTICAL SPEED A/A24G-11 |
| MIL-L-6723 Revision C:1987 | LIGHT, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL G 6019 : C | GAGE, PRESSURE, DIAL INDICATING, LOW-PRESSURE OXYGEN |
| MIL-B-4330 Revision C:1984 | BOOT, EXTREME COLD WEATHER |
| MIL-I-38258 Base Document:1965 | INDICATOR, ATTITUDE ARU 18/A DIRECTOR |
| MIL-C-87975 Base Document:1985 | CLOCK, AIRCRAFT, MECHANICAL ABU-32/A |
| MIL-T-594 Revision B:1974 | TEST SET, ARMATURE AND STATOR |
| MIL-E-81512 Base Document:1968 | ENCODER, SHAFT POSITION TO DIGITAL, CONTACT TYPE, ALTITUDE REPORTING, GENERAL SPECIFICATION FOR |
| MIL M 62361 : C | MOTOR, DRIVE, DIRECT CURRENT 2 RPM/8RPM |
| MIL H 26666 : D (1) | HOSE ASSEMBLY, PNEUMATIC, HIGH PRESSURE |
| MIL-I-27619 Revision G:1974 | INDICATORS, ATTITUDE DIRECTOR |
| MIL-C-23157 Revision D:1979 | CLIPBOARD, PILOTS, MXU-163/P AND MARK 2A |
| MIL-B-4792 Revision E:1994 | BUMPER, RUBBER, DUPLEX ROUND |
| MIL H 87961 : NOTICE 2 | HOSE AND HOSE ASSEMBLIES, AIR DUCT, AIR BREATHING, OXYGEN SYSTEM GENERAL SPECIFICATION FOR |
| MIL-T-58082 Revision A:1974 | TESTER, PYROMETER & THERMOCOUPLE, FIELD, TYPE N-3A |
| MIL W 6496 : B NOTICE 1 | WINCH, DRUM, ENGINE OF TURRET HOIST, TYPE A-1 |
| MIL-M-7969 Revision C:1965 | Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for |
| MIL-I-8672 Revision B:1969 | INSTALLATION AND TEST OF AIRCRAFT PYROTECHNIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR [ASG] |
| MIL-C-38207 Revision A:1965 | CLOCK, AIRCRAFT, MECHANICAL ABU 11/A |
| MIL-C-83435 Base Document:1974 | CLOTHING OUTFIT, EXTREME COLD WEATHER SURVIVAL A/P22S-10 |
| MIL G 21480 : A | GENERATOR SYSTEM, 400 HERTZ ALTERNATING CURRENT, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL I 27851 : B | INDICATOR, INDICATED AIRSPEED AVU-17/A |
| MIL-T-25307 Revision D:1985 | TRANSMITTER, PRESSURE, HYDRAULIC, TYPE MJ-1 |
| MIL-C-38418 Revision E:1981 | CONTROL ASSEMBLY, GYROSCOPE, ATTITUDE A/A24G-39 |
| MIL A 25949 : E (2) | ACCELEROMETER, AIRCRAFT RANGE -5 TO PLUS 1OG UNITS, INTEGRALLY LIGHTED |
| MIL-I-25437 Revision B:1984 | INDICATORS, AIRCRAFT, PRESSURE, VOLTAGE RATIO TYPE, GENERAL SPECIFICATION FOR |
| MIL-I-8974 Revision A:1981 | INDICATOR, EVENT COUNTING, GENERAL SPECIFICATION FOR |
| MIL M 62368 : A | MOTOR, GEARHEAD, 18-30 VOLTS, DIRECT CURRENT |
| MIL I 87108 : A | INFLATION ASSEMBLY, FLU-2A/P |
| MIL-B-55118 Revision A:1971 | BATTERIES, STORAGE, (CELLS) VENTED, NICKEL CADMIUM |
| MIL T 26898 : B | TEST SET, AIRFIELD LIGHTING SYSTEMS, TYPE MM-1 |
| MIL L 25866 : B | LIGHT, EMERGENCY EXIT, AIRCRAFT LEU AND 1-A |
| MIL-B-83183 Revision B:1987 | BARRIER, AIRCRAFT ARRESTING |
| MIL-P-25062 Revision B:1964 | PARACHUTE RECOVERY SYSTEM, MISSILE AND DRONE, GENERAL REQUIREMENT FOR DEVELOPMENT OF |
| MIL B 38634 : LATEST | BOMB, FIRE, BLU 32A B |
| MIL-I-23524 Revision A:1986 | INDICATOR, ATTITUDE DIRECTOR, REMOTE, ID 1329A (V) |
| MIL-A-19273 Revision B:1976 | ANTENNA AS-515A/SPG AND MX-7232/SPG-53B (RADAR ANTENNA SCANNER) |
| NASA MSFC STD 506 : 1988 | MATERIALS AND PROCESSES CONTROL |
| MIL-F-38762 Base Document:1966 | FLUORESCENT PENETRANT INSPECTION UNITS |
| MIL-V-85830 Base Document:1989 | VENTILATOR, TACTICAL, HELICOPTER AIRCREWMEN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE |
| MIL C 25666 : E (1) | CONVERTER, LIQUID OXYGEN, CAPACITANCE TYPE GAGING, GENERAL SPECIFICATION FOR |
| DOD-C-85050 Base Document:1982 | CHARGERS, BATTERY, NICKEL-CADMIUM, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-I-23832 Revision A:1980 | INDICATOR, TACHOMETER, TRIPLE POINTER, HELICOPTER |
| MIL G 9398 : C | GENERATOR, TACHOMETER, TWO POLE HIGH TEMPERATURE AIRCRAFT |
| MIL I 27190 : B | INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI |
| MIL-D-38134 Revision A:1971 | DETECTOR, MAGNETIC AZIMUTH DSU-4/A, HIGH TEMPERATURE |
| MIL-I-81049 Revision A:1972 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
| MIL-T-5420 Revision B:1970 | TUBE, PITOT STATIC, ELECTRICALLY HEATED, AIRCRAFT |
| MIL C 38333 : 0 | CONTROLLER, COMPASS SYSTEM C-6448/ASN-55 |
| MIL-S-5733 Revision B:1952 | SOLENOID, FUSE ARMING, TYPE F AND 1 |
| MIL L 6484 : C | LIGHT, COCKPIT UTILITY, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL R 6466 : B NOTICE 1 | RELAY, ARMATURE, EXCITER PROTECTION, TYPE A-1 |
| MIL L 7830 : D | LIGHT ASSEMBLY, MARKER, AIRCRAFT OBSTRUCTION |
| MIL-I-7906 Revision A:1961 | INDICATOR, GYRO HORIZON, MANUALLY CAGED, ELECTRIC, TYPE MB 1 |
| MIL C 25531 : D | COUPLING HALF, QUICK DISCONNECT, PNEUMATIC STARTER, EXTERNAL, LOW PRESSURE, DIRECT RELEASE |
| MIL C 87147 : 0 | OUTLINES VACUUM PACKAGED ACCESSORIES FOR THE SRU-6/P overcoat. |
| MIL-L-5667 Revision B:1964 | LIGHTING EQUIPMENT, AIRCRAFT INSTRUMENT PANEL, GENERAL SPECIFICATION FOR INSTALLATION OF [ASG] |
| MIL L 38169 : NOTICE 2 | LENSES, GOGGLE AND VISOR, HELMET, OPTICAL CHARACTERISTICS |
| MIL I 83361 : (4) | INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
| MIL-B-8621 Revision A:1964 | BOARD, CHART, MARK 6A MARK 6B AND MARK 6C |
| MIL-P-38136 Revision A:1969 | PITOT STATIC TUBE COMPENSATED TRU 62/A |
| MIL-E-38453 Revision A:1971 | ENVIRONMENTAL CONTROL, ENVIRONMENTAL PROTECTION, AND ENGINE BLEED AIR SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL M 5388 : B | MACHMETER; PITOT STATIC OPERATED, RANGE 0.5 TO 1.5, TYPE A-2B |
| MIL-P-8945 Revision A:1967 | PANEL, RELAY, PILOT, ENCLOSED, AIRPORT LIGHTING |
| DOD-STD-2140 Base Document:1982 | MACHINERY ALTERATION (MACHALT) INSTRUCTIONS, PREPARATION OF (METRIC) |
| MIL-T-81821 Base Document:1969 | TRAINERS, MAINTENANCE, EQUIPMENT AND SERVICES GENERAL SPECIFICATION FOR |
| MIL-C-7079 Revision A:1965 | CIRCUIT BREAKERS, NON TRIP-FREE GENERAL SPECIFICATION FOR |
| MIL T 25627 : C | TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |
| MIL-A-27391 Revision B:1963 | ALTIMETER, PRESSURE AAU-2A |
| MIL-HDBK-188 Base Document:1983 | GUIDE FOR DEVELOPERS AND USERS OF COMMUNICATIONS SYSTEMS STANDARDS IN THE MIL-STD-188 SERIES - VOLUME 1 OF 2 VOLUMES: STANDARDS DEVELOPMENT AND USE/ORGANIZATIONAL RELATIONSHIPS - VOLUME 2 OF 2 VOLUMES: DETAILS CONCERNING STANDARDIZATION ORGANIZATIONS |
| MIL-A-83039 Revision B:1971 | AIR CONDITIONER A/M32C-10A AIR CYCLE FOR AIRCRAFT GROUND SUPPORT |
| MIL-B-55679 Base Document:1969 | BATTERY, DRY (SPECIAL PURPOSE) |
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