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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
Available format(s)
PDF
Superseded date
23-07-2013
Superseded by
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.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
|
| Pages |
11
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| 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Superseded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 HEADING 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 | Seats, Helicopter Cabin, Crashworthy, General Specification for |
| 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, Anticollision, 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-408/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 Requirements 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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