|
MIL R 85895 : 0
|
RACK, BOMB EJECTOR, AIRCRAFT BRU-32/A |
|
MIL A 85802 : 0
|
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 : B
|
INDICATOR, TACHOMETER, HELICOPTER, 0-4000 RPM TYPE MA 1 |
|
MIL I 18856 : B
|
INDICATOR, ANGLE OF ATTACK, 28V DC MS28062 AND MS28067 |
|
MIL A 38307 : A
|
ACCELEROMETER, AIRCRAFT, MX-6663/AJB-7 |
|
MIL T 38034 : E
|
TIMER, FIRE CONTROL, BOMBING, DUAL |
|
MIL I 83294 : 0
|
INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR |
|
MIL P 81655 : 0
|
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 : B
|
AIR CONDITIONER, A/M32C-4, TRAILER MOUNTED, VAPOR CYCLE, ELECTRIC, MOTOR DRIVEN |
|
MIL I 7062 : C
|
INDICATOR, POSITION, CONTROL SURFACES, 28 VOLT DC, GENERAL SPECIFICATION FOR |
|
MIL C 5809 : G
|
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 : C
|
PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF |
|
MIL T 83460 : 0
|
TRANSDUCER, MOTIONAL PICKUP TRU-164/A |
|
MIL R 81202 : D
|
RECEIVER ASSEMBLY, NITROGEN, FOR LAU-7 SERIES LAUNCHERS |
|
MIL I 83152 : B
|
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 : C
|
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 : B
|
PUMP, PRESSURE, OIL FREE AIR TYPE MA-2 |
|
MIL T 5483 : D
|
TRANSMITTER, PRESSURE, SYNCHRO AIRCRAFT 165 DEGREE MOVEMENT |
|
MIL C 27298 : B
|
CLOCK, AIRCRAFT, MECHANICAL ABU AND 9-A |
|
MIL B 49436 : B
|
BATTERIES, RECHARGEABLE, NICKEL CADMIUM, SEALED |
|
MIL T 38473 : A
|
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 : B
|
CAP, PRESSURE FUEL SERVICING |
|
MIL P 85833 : 0
|
PROTECTIVE ASSEMBLY, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL |
|
MIL A 38140 : B
|
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 : B
|
CARTRIDGE, ENGINE STARTER MXU-4A/A |
|
MIL G 25597 : D
|
GYROSCOPE, DISPLACEMENT, ROLL AND PITCH, TYPE MD-1 |
|
MIL STD 838 : C
|
LUBRICATION OF MILITARY EQUIPMENT |
|
MIL-STD-482 Revision A:1974
|
CONFIGURATION STATUS ACCOUNTING DATA ELEMENTS AND RELATED FEATURES |
|
MIL L 50794 : 0
|
LINEAR SHAPED CHARGE ASSEMBLY |
|
SAE AS 8181 : 1997
|
DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS, GENERAL SPECIFICATION FOR |
|
MIL B 8568 : B
|
BINOCULAR, PRISMATIC, HAND-HELD [FOR AERONAUTICAL USE] 7 X 50 AND 6 X 42 WIDE FIELD [ASG] |
|
MIL I 6726 : B
|
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 : F
|
COMPRESSOR, PNEUMATIC, 3000 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 : B
|
MANOMETER, PRESSURE, DIFFERENTIAL AND ABSOLUTE TYPE E 1 |
|
MIL A 85072 : A
|
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 : D
|
TEST SET, ELECTRICAL POWER A/M24T-8() |
|
MIL A 55503 : 0
|
ATTITUDE HEADING REFERENCE SET AN/ASN-76 |
|
MIL-P-6457 Revision E:1974
|
POWER SUPPLY, METALLIC RECTIFIER TYPE, GENERAL SPECIFICATION FOR |
|
MIL I 38338 : D
|
INDICATOR, OIL QUANTITY, CONTINUOUS TRANSMISSION, NUCLEONIC |
|
MIL D 82687 : 0
|
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 : C
|
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 : B
|
CORE, AIRCRAFT, HIGH PRESSURE AIR VALVE |
|
MIL I 27202 : A
|
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 : 0
|
ADAPTER, LAUNCHER, AIRCRAFT, ADU-299/E |
|
MIL M 7584 : A
|
METER, FUEL FLOW SYNCHRO STYLE TYPE B 3A |
|
MIL C 23367 : 0
|
COMPUTER, FLIGHT DIRECTOR, AIRCRAFT |
|
SAE AS 7997A : 1999(S2018)
|
MOTORS, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT - GENERAL SPECIFICATION FOR |
|
MIL-H-8775 Revision D:1976
|
HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
|
MIL C 85521 : 0
|
CONCENTRATOR, OXYGEN, GGU-7/A |
|
MIL C 85829 : 0
|
COUPLING ASSEMBLY, HOSE, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE |
|
MIL S 26547 : C
|
STARTER-GENERATOR ENGINE STU-6A |
|
MIL L 7806 : A
|
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 : E
|
ELECTRONIC EQUIPMENT, GROUND GENERAL REQUIREMENTS FOR |
|
MIL STD 2156 : 0
|
LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
|
MIL C 87104 : 0
|
COAXIAL ASSEMBLIES, GENERAL SPECIFICATION FOR |
|
MIL G 83872 : A
|
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 : B
|
SANDWICH CONSTRUCTION, PLASTIC RESIN, GLASS FABRIC BASE, LAMINATED FACINGS AND POLYURETHANE FOAMED-IN-PLACE CORE, FOR AIRCRAFT STRUCTURAL APPLICATIONS |
|
MIL C 7413 : B
|
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 : B
|
CARTRIDGES, EXPLOSIVE BOLT, (FOR TORPEDOES MARK 46 ALL MODS) |
|
MIL C 83124 : 0
|
CARTRIDGE ACTUATED DEVICES PROPELLANT ACTUATED DEVICES GENERAL DESIGN SPECIFICATION FOR |
|
MIL E 50796 : 0
|
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 : 0
|
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 : A
|
COMMUNICATIONS SYSTEMS FOR TRAINING DEVICES, GENERAL SPECIFICATION FOR |
|
MIL T 52497 : A
|
TRANSFORMER, POWER ISOLATION, SERIES CIRCUIT AIRPORT LIGHTING 6.6/6.6 AMPERES. |
|
MIL A 26624 : B
|
AIR CONDITIONER, A/M32C-5, TRAILER MOUNTED, VAPOR CYCLE, ELECTRIC MOTOR DRIVEN |
|
MIL M 25047 : C
|
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 : B
|
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 : 0
|
GAGE - PRESSURE, DIAL INDICATING |
|
MIL G 26611 : D
|
GENERATOR, TACHOMETER GEU-7/A, MINIATURE |
|
MIL A 6589 : A
|
AMPLIFIER, ELECTRONIC CONTROL, SINGLE CHANNEL, TYPE A-2 |
|
MIL H 4495 : D
|
HOSE ASSEMBLY, RUBBER, AERIAL REFUELING |
|
MIL A 83469 : 0
|
ADJUSTER, LAP BELT, 1-3/4 INCH WEBBING |
|
MIL A 85481 : 0
|
ARMING WIRE ASSEMBLIES |
|
MIL P 26517 : A
|
POWER SUPPLY, TRANSFORMER-RECTIFIER, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL M 87977 : 0
|
MAINTENANCE PLATFORM, AIRCRAFT |
|
MIL A 23670 : A
|
ATTITUDE HEADING REFERENCE SYSTEM AN/ASN-50(*) |
|
MIL B 26220 : D
|
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 : C
|
INDICATOR, ATTITUDE TYPE J 8 |
|
MIL B 83769 : D
|
BATTERY, STORAGE, LEAD ACID, GENERAL SPECIFICATION FOR |
|
MIL C 47267 : 0
|
CLEANING & SURFACE PREPARATION, VAPOR BLAST |
|
MIL S 8512 : D
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
|
MIL C 5604 : B
|
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 : A
|
SWITCH, STEPPING, DIRECT CURRENT AIRCRAFT DISPENSER |
|
MIL E 7080 : B
|
ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
|
MIL C 85019 : 0
|
COMPUTER, AIR NAVIGATION, TRUE AIRSPEED, MACH NUMBER, WIND COMPONENTS SUPERSONIC, TYPE MB-9 |
|
MIL C 9082 : H
|
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 : 0
|
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 : 0
|
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 : 0
|
MASK, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE, NON-OXYGEN |
|
SAE AS 17852 : 2012
|
REDUCERS, OXYGEN PRESSURE |
|
MIL E 11991 : E
|
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 : A
|
SPECTROMETER, FLUID ANALYSIS A/E35U-3 |
|
MIL C 38373 : B
|
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 : A
|
MOTOR, DIRECT CURRENT)(FOR TORPEDO MK 46 MOD 1) |
|
MIL T 9720 : F
|
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 : 0
|
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 : C
|
INDICATOR, TRUE AIRSPEED TYPE M 1A |
|
MIL I 5418 : B
|
INDICATOR: AIRSPEED, PITOT STATIC, SENSITIVE, 50-650 KNOTS |
|
MIL S 8812 : D
|
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 : C
|
MOTOR, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT GENERAL SPECIFICATION FOR |
|
MIL I 18802 : A
|
INSTALLATION OF FUEL AND OIL LINES, AIRCRAFT |
|
MIL I 85506 : 0
|
INDICATOR, INDICATED AIRSPEED, STANDBY TYPES I, II, AND III |
|
MIL S 83576 : 0
|
SOLAR CELL ARRAYS, SPACE VEHICLE, DESIGN AND TESTING, GENERAL SPECIFICATION FOR |
|
MIL I 83751 : 0
|
INDICATOR, SAFETY LEVEL, RF |
|
MIL S 85510 : 0
|
|
|
MIL S 7852 : B
|
SEAT, AIRCREW, ADJUSTABLE SWIVEL TYPE E-1 |
|
MIL B 26793 : B
|
BLOWER, GASOLINE ENGINE DRIVEN, TYPE A-1 |
|
MIL A 26107 : D
|
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 : 0
|
AMPLIFIER-POWER SUPPLY AM-4080/ASN-55, LEVELLING |
|
MIL T 81272 : 0
|
THERMOCOUPLE, ENGINE, CYLINDER, BAYONET TYPE, MS90324 |
|
MIL V 8610 : B
|
VALVE, FUEL SHUTOFF SOLENOID OPERATED, 28 VOLT, DC |
|
MIL HDBK 838 : 0
|
LUBRICATION OF MILITARY EQUIPMENT |
|
MIL I 27273 : A
|
INVERTER, POWER, STATIC, GENERAL SPECIFICATION FOR |
|
MIL V 8057 : F
|
VALVE, OXYGEN, PRESSURE BUILDUP AND VENT |
|
MIL B 87983 : 0
|
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 : B
|
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 : B
|
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 A 38726 : 0
|
ADAPTER ASSEMBLY, REUSABLE, FLEXIBLE HOSE, LOW PRESSURE |
|
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 : E
|
CASTER, INDUSTRIAL |
|
MIL A 81852 : A
|
ALTIMETER-ENCODER AAU-32/A |
|
MIL I 22075 : C
|
INDICATOR, BEARING DISTANCE-HEADING; ID - 663D/U |
|
MIL V 8712 : A
|
VALVE, AIR RELIEF, LOW PRESSURE |
|
MIL I 85832 : 0
|
INTERCOM, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE SET |
|
MIL R 47321 : 0
|
REGULATOR, PRESSURE |
|
MIL M 4871 : C
|
MAINTENANCE PLATFORM |
|
MIL C 4952 : E
|
CARTRIDGES, DESICCANT, DEHYDRATOR |
|
MIL H 7365 : D
|
HOSE, AIR DUCT, FOR GROUND HEATERS |
|
MIL R 38162 : B
|
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 : A
|
HOOKS, BOMB RACK, GENERAL SPECIFICATION FOR |
|
MIL V 85033 : A
|
VALVE CHARGING |
|
MIL C 7460 : A
|
CHROMIUM PLATING, POROUS CHANNEL TYPE, AIRCRAFT ENGINE CYLINDERS, GENERAL SPECIFICATIONS FOR |
|
MIL T 21578 : A
|
TEST EQUIPMENT, HAZARDOUS LOCATION, INSTALLED, BASIC REQUIREMENTS FOR |
|
MIL C 87987 : 0
|
CRANE, HYDRAULIC, WHEEL MOUNTED, 7.5 & 15 TON CAPACITIES |
|
MIL R 5520 : C
|
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 : B
|
ALTIMETER AAU-31/A |
|
MIL-C-83864 Revision A:1982
|
CONTAINER, INNER, SURVIVAL KIT |
|
MIL T 27200 : C
|
TRANSMITTER, RATE GYROSCOPE TRU-2A/A |
|
MIL P 27965 : 0
|
PLOTTING SET, THEODOLITE ML-625/GM |
|
MIL G 85468 : 0
|
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 : D
|
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 : 0
|
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 : B
|
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 : A
|
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 : 1966
|
Generator, Gas |
|
MIL B 19906 : A
|
BOMB RACK AND ROCKET LAUNCHER, COMBINATION, AERO 15 SERIES |
|
MIL L 21652 : A
|
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 : C
|
INDICATOR, HORIZONTAL SITUATION, AQU-2/A |
|
MIL I 58067 : A
|
INDICATOR, VERTICAL VELOCITY, RAPID RESPONSE ACCELERATION SENSITIVE, GENERAL SPECIFICATION FOR |
|
MIL R 28894 : 0
|
RELAY, HYBRID OR SOLID STATE, SENSORS, ESTABLISHED RELIABILITY GENERAL SPECIFICATION FOR |
|
MIL N 3336 : A
|
NUT, SHEET SPRING, INSTRUMENT MOUNTING |
|
MIL W 5845 : C
|
WIRE, ELECTRICAL, IRON AND CONSTANTAN, THERMOCOUPLE |
|
MIL S 6551 : A
|
|
|
MIL A 5034 : B
|
ADAPTER, BOMB RACK, 30-INCH, AERO 1A |
|
MIL I 25931 : B
|
INDICATOR, POSITION, LANDING GEAR, SYMBOL-INDICATING, INTEGRALLY LIGHTED |
|
MIL M 7793 : F
|
METER, TIME TOTALIZING |
|
MIL A 25915 : A
|
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 : 0
|
PRESSURE TRANSDUCER (FOR TORPEDO MK 46 MOD 0 AND MOD 1) |
|
MIL I 85352 : 0
|
INFLATOR ASSEMBLY AND GAGE ELEMENTS, PNEUMATIC PRESSURE REMOTE CONTROL, DIRECT READING |
|
MIL G 81168 : 0
|
GYROSCOPE, RATE INTEGRATING |
|
MIL C 81991 : 0
|
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 : A
|
SEAT SYSTEM: CRASH RESISTANCE, NON-EJECTION, AIRCREW, GENERAL SPECIFICATION FOR |
|
MIL A 83462 : 0
|
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 : D
|
CONTROL ASSEMBLY, ATTITUDE, GYROSCOPIC AF/A24G-1A |
|
MIL R 23761 : B
|
REGULATORS, VOLTAGE, AND CONTROL PANELS AIRCRAFT DIRECT CURRENT GENERATOR, GENERAL SPECIFICATION FOR |
|
MIL I 22126 : B
|
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 : 0
|
BRUSHES, FLAP, ROTARY, ABRASIVE, GENERAL SPECIFICATION FOR |
|
MIL T 26639 : C
|
TESTER, TORQUE WRENCH |
|
MIL A 25088 : C
|
|
|
MIL B 87167 : 0
|
BELT, AIRCRAFT SAFETY, HBU-12/A |
|
MIL I 25861 : D
|
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 : C
|
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 : A
|
PRESSURE INDICATING SYSTEM, HYDRAULIC A/A27 J-1 |
|
MIL S 26716 : A
|
STAND, TEST, AIRCRAFT HYDRAULIC SYSTEMS, NON-PORTABLE |
|
MIL G 8348 : H
|
GAGE, ASSEMBLIES, AIR PRESSURE, DIAL INDICATING CHUCK TYPE SELF CONTAINED |
|
MIL C 87150 : 1986
|
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 : D
|
CRANE, HYDRAULIC, TRUCK MOUNTED, A/S32A-16 16,5OO POUND CRANE CAPACITY, 6X4, DED |
|
MIL C 5026 : F
|
CUTOUT RELAY, ENGINE GENERATOR |
|
MIL A 25896 : E
|
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 : A
|
HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
|
MIL A 83136 : A
|
ARRESTING HOOK INSTALLATION, RUNWAY ARRESTING SYSTEM, AIRCRAFT, EMERGENCY |
|
MIL C 7989 : B
|
COVER, LIGHT TRANSMITTING, FOR AERONAUTICAL LIGHTS, GENERAL SPECIFICATION FOR |
|
MIL B 55130 : A
|
BATTERIES, RECHARGEABLE, NICKEL CADMIUM SEALED |
|
MIL C 38618 : A
|
COUPLER, DRIVE ASSEMBLY GOVERNOR, FUZE BOMB MAU 87A B |
|
MIL C 6499 : E
|
CLOCK, AIRCRAFT MECHANICAL TYPE A 13A |
|
MIL D 38613 : A
|
DRIVE, ASSEMBLY, ARMING, BOMB FUZE, ATU-35B/B |
|
MIL G 23723 : 0
|
GYROSCOPE, RATE SWITCHING CN-495/AJB-3 |
|
MIL I 23252 : B
|
INDICATOR, PRESSURE |
|
DOD HDBK 791 : 0
|
MAINTAINABILITY DESIGN TECHNIQUES |
|
MIL S 81771 : A
|
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 : B
|
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 : A
|
COOLERS, OIL, PLATE, AIRCRAFT |
|
MIL A 81327 : A
|
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 : B
|
DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR |
|
MIL I 81023 : D
|
INDUCTOR, 28V, D.C. LABORATORY TEST GENERAL SPECIFICATION FOR |
|
MIL B 5046 : D
|
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 : 0
|
GENERATOR SET, GAS TURBINE ENGINE DRIVEN, 30 AND 60 KW, 400 HZ |
|
MIL P 83126 : A
|
PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
|
MIL C 28661 : A
|
CABLE, POWER, ELECTRICAL, HIGH VOLTAGE |
|
MIL P 81305 : A
|
POWER, DISTRIBUTION PANEL, ALTERNATING CURRENT, F-4 AIRCRAFT, SPECIFICATION FOR |
|
MIL P 85034 : 0
|
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 : 0
|
TRANSMITTER, RATE GYROSCOPE T 970/AJB - 7 |
|
MIL B 26026 : B
|
BATTERY, STORAGE, AIRCRAFT, TYPE MA-2-1 |
|
MIL STD 1174 : B
|
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 : 0
|
SHIELDED AND CONFINED MILD DETONATING CORD ASSEMBLIES |
|
MIL S 38399 : A
|
STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR |
|
MIL T 38760 : 0
|
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 : B
|
ALTIMETER, PRESSURE AAU-7/A |
|
MIL C 9075 : A
|
COMPUTER AND TRANSMITTER, TRUE AIRSPEED, PITOT STATIC, 150-900 KNOTS, TYPE MA 1 |
|
MIL D 7106 : C
|
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 : E
|
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-81774A:1973
|
CONTROL PANEL, AIRCRAFT, GENERAL REQUIREMENTS FOR |
|
DOD STD 1476 : A
|
METRIC SYSTEM, APPLICATION IN NEW DESIGN |
|
MIL A 27261 : A
|
ACCELEROMETER, AIRCRAFT |
|
MIL E 18927 : E
|
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 : A
|
WINDSHIELDED SYSTEM, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR |
|
MIL-V-25023 Revision B:1967
|
VALVE, FUEL DRAIN, SELF-LOCKING |
|
DOD B 24673 : 0
|
BELLS, SHIPS AND SMALL CRAFT |
|
MIL I 85112 : 0
|
INDICATOR SET, VERTICAL SCALE |
|
MIL T 27-233 : 0
|
TRANSFORMERS AND INDUCTORS (AUDIO POWER AND HIGH POWER PULSE) INDUCTOR CHARGING TF5S37ZZ |
|
MIL A 25933 : B
|
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 : A
|
INDICATOR, MACH NUMBER, SENSITIVE, SERVOED, RANGE .5 TO 1.O, TYPE ME-5 |
|
MIL A 26360 : B
|
AMPLIFIER, ELECTRONIC CONTROL ASU-3/A |
|
MIL A 27330 : B
|
ACCELEROMETER, ELECTRICAL, LINEAR TRU-3/A |
|
MIL B 4173 : B
|
BENCH, WORK, GENERAL PURPOSE |
|
MIL B 49041 : 0
|
BATTERY, DRY BA-1579/U |
|
MIL T 26609 : C
|
TRANSMITTER, POSITION |
|
MIL H 23799 : 0
|
HOSE ASSEMBLY, METAL, TRANSFER, LIQUID OXYGEN |
|
MIL G 58103 : 0
|
GRIP ASSEMBLY, CYCLIC CONTROLLER, HELICOPTER |
|
MIL T 27730 : A
|
TAPE, ANTISEIZE, POLYTETRAFLUOROETHYLENE, WITH DISPENSER |
|
MIL I 27552 : C
|
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 : 0
|
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 : A
|
SHAFT, POWER TRANSMISSION, AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR |
|
MIL T 81838 : 0
|
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 : 0
|
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 : A
|
LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
|
MIL N 25161 : C
|
NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
|
MIL G 26988 : C
|
GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
|
MIL I 83262 : B
|
INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
|
MIL D 26503 : A
|
DETECTOR, MAGNETIC AZIMUTH AND COMPENSATOR, DETECTOR, MAGNETIC AZIMUTH |
|
MIL I 27680 : C
|
INDICATOR, ATTITUDE, ARU-12/A, REMOTE |
|
SAE AS 85075 : 2000
|
TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR |
|
MIL T 49388 : A
|
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 : A
|
INDICATOR, PRESSURE OIL, 0-200 PSI |
|
MIL I 25950 : B
|
INDICATOR, PRESSURE, OIL, 0-100 PSI |
|
MIL I 7071 : B
|
INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
|
MIL I 83117 : B
|
INDICATOR, ANGLE OF ATTACK |
|
MIL P 85315 : 0
|
PUMP, EJECTOR, AIR VEHICLE FUEL, GENERAL SPECIFICATION FOR |
|
MIL S 9320 : C
|
SIGNAL, WARNING, AUDIBLE, FOR HEADSET |
|
MIL C 6235 : D
|
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 : D
|
ARRESTER, LIGHTNING, GENERAL SPECIFICATION FOR |
|
MIL G 81065 : A
|
GYRO-PENDULUM ASSEMBLY (FOR TORPEDO MK 46 MOD O AND MK 46 MOD 1) |
|
MIL I 25941 : D
|
INDICATOR, TURN AND SLIP, 2-INCH SIZE, INTEGRALLY LIGHTED |
|
MIL T 60530 : A
|
TECHNICAL DATA PACKAGE FOR AMC MATERIAL |
|
MIL G 27693 : A
|
GYROSCOPE, DISPLACEMENT SBU-6/A, ROLL AND PITCH |
|
MIL M 4803 : D
|
MOTOR-GENERATOR, 400 HZ PRECISE OUTPUT, GENERAL REQUIREMENTS FOR |
|
MIL I 25645 : D
|
INDICATOR, LIQUID OXYGEN QUANTITY, CAPACITANCE TYPE, GENERAL SPECIFICATION FOR |
|
MIL G 5678 : C
|
GAGE PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE |
|
MIL I 7084 : A
|
INDICATOR, PRESSURE, HYDRAULIC 0-4,000 PSI |
|
MIL P 9400 : C
|
PLASTIC LAMINATE AND SANDWICH CONSTRUCTION PARTS, AIRCRAFT STRUCTURAL PROCESS SPECIFICATION REQUIREMENTS |
|
MIL G 5413 : D NOTICE 1
|
GENERATOR, TACHOMETER, FOUR POLE |
|
MIL D 26124 : B
|
DUCT AND DUCT ASSEMBLY, PNEUMATIC, FLEXIBLE |
|
MIL G 25591 : E
|
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 : B
|
AMPLIFIER-INDICATOR GROUP, ALTITUDE VERTICAL SPEED A/A24G-11 |
|
MIL L 6723 : C
|
LIGHT, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL G 6019 : C
|
GAGE, PRESSURE, DIAL INDICATING, LOW-PRESSURE OXYGEN |
|
MIL B 4330 : C
|
BOOT, EXTREME COLD WEATHER |
|
MIL I 38258 : 0
|
INDICATOR, ATTITUDE ARU 18/A DIRECTOR |
|
MIL C 87975 : 0
|
CLOCK, AIRCRAFT, MECHANICAL ABU-32/A |
|
MIL T 594 : B
|
TEST SET, ARMATURE AND STATOR |
|
MIL E 81512 : 0
|
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 : G
|
INDICATORS, ATTITUDE DIRECTOR |
|
MIL C 23157 : D
|
CLIPBOARD, PILOTS, MXU-163/P AND MARK 2A |
|
MIL B 4792 : E
|
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 : C
|
MOTOR, 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 : A
|
CLOCK, AIRCRAFT, MECHANICAL ABU 11/A |
|
MIL C 83435 : 0
|
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 : D
|
TRANSMITTER, PRESSURE, HYDRAULIC, TYPE MJ-1 |
|
MIL C 38418 : E
|
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 : B
|
INDICATORS, AIRCRAFT, PRESSURE, VOLTAGE RATIO TYPE, GENERAL SPECIFICATION FOR |
|
MIL I 8974 : A
|
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 : A
|
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 : B
|
BARRIER, AIRCRAFT ARRESTING |
|
MIL P 25062 : B
|
PARACHUTE RECOVERY SYSTEM, MISSILE AND DRONE, GENERAL REQUIREMENT FOR DEVELOPMENT OF |
|
MIL B 38634 : LATEST
|
BOMB, FIRE, BLU 32A B |
|
MIL I 23524 : A
|
INDICATOR, ATTITUDE DIRECTOR, REMOTE, ID 1329A (V) |
|
MIL A 19273 : B
|
ANTENNA AS-515A/SPG AND MX-7232/SPG-53B (RADAR ANTENNA SCANNER) |
|
NASA MSFC STD 506 : 1988
|
MATERIALS AND PROCESSES CONTROL |
|
MIL F 38762 : 0
|
FLUORESCENT PENETRANT INSPECTION UNITS |
|
MIL V 85830 : 0
|
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 : 0
|
CHARGERS, BATTERY, NICKEL-CADMIUM, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL I 23832 : A
|
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 : A
|
DETECTOR, MAGNETIC AZIMUTH DSU-4/A, HIGH TEMPERATURE |
|
MIL I 81049 : A
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
|
MIL T 5420 : B
|
TUBE, PITOT STATIC, ELECTRICALLY HEATED, AIRCRAFT |
|
MIL C 38333 : 0
|
CONTROLLER, COMPASS SYSTEM C-6448/ASN-55 |
|
MIL S 5733 : B
|
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 : A
|
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 : A
|
PANEL, RELAY, PILOT, ENCLOSED, AIRPORT LIGHTING |
|
DOD STD 2140 : 0
|
MACHINERY ALTERATION (MACHALT) INSTRUCTIONS, PREPARATION OF (METRIC) |
|
MIL T 81821 : 0
|
TRAINERS, MAINTENANCE, EQUIPMENT AND SERVICES GENERAL SPECIFICATION FOR |
|
MIL C 7079 : A
|
CIRCUIT BREAKERS, NON TRIP-FREE GENERAL SPECIFICATION FOR |
|
MIL T 25627 : C
|
TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |
|
MIL A 27391 : B
|
ALTIMETER, PRESSURE AAU-2A |
|
MIL HDBK 188 : 0
|
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 : B
|
AIR CONDITIONER A/M32C-10A AIR CYCLE FOR AIRCRAFT GROUND SUPPORT |
|
MIL B 55679 : 0
|
BATTERY, DRY (SPECIAL PURPOSE) |