MIL-A-85802 Base Document:1986
|
ACTUATOR, ELECTROMECHANICAL, LINEAR |
MIL C 83166 : LATEST
|
CONVERTER MULTIPLEXER, SIGNAL DATA, GENERAL SPECIFICATION FOR |
MIL-A-83783 Base Document:1972
|
Adapter, Test, MX-9042/G |
MIL-A-6271 Revision C:1976
|
ANTENNA, SUBSYSTEM FOR VHF AIRBORNE COMMUNICATION EQUIPMENT GENERAL SPECIFICATION FOR |
MIL-R-38370 Revision B:1972
|
RECORDING SET, FLIGHT DATA A/A24U-10 |
MIL-A-38307 Revision A:1981
|
ACCELEROMETER, AIRCRAFT, MX-6663/AJB-7 |
MIL-I-83294 Base Document:1971
|
INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR |
MIL-C-87979 Base Document:1987
|
CLOCK, AIRCRAFT, ELECTRONIC |
SAE MA 4098 : 2015
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, HEAVY DUTY, METALLIC REINFORCED, 204 DEGREE C, 35000 KPA, HYDRAULIC AND PNEUMATIC, METRIC |
MIL-B-8914 Revision B:1966
|
BEARING, ROLLER, SELF-ALIGNING, AIRFRAME, ANTIFRICTION |
MIL P 5516 : C
|
PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, 160 DEGREES F |
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-R-38435 Revision B:1968
|
RECORDING SET, SIGNAL DATA A/A 24U-6 |
MIL-E-23001 Revision B:1976
|
ELECTRIC GENERATING SYSTEM, VARIABLE SPEED CONSTANT FREQUENCY, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL T 6396 : E
|
TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
MIL-G-83872 Revision A:1977
|
GYROSCOPE, DISPLACEMENT, TYPE SBU-23/A |
MIL F 27272 : B
|
FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
MIL A 87136 : NOTICE 1
|
ANTENNAS, AIRBORNE GENERAL SPECIFICATION FOR |
MIL-I-83152 Revision B:1974
|
INDICATOR, INDICATED-AIRSPEED AVU-22/A (INDICATOR-TRANSDUCER) |
MIL-T-83460 Base Document:1975
|
TRANSDUCER, MOTIONAL PICKUP TRU-164/A |
SAE AS 4388 : 2013
|
HOSE ASSEMBLY PTFE HEAVY DUTY, -65 TO 400 DEGREES F (-55 TO 204 DEGREES C) 8000 PSI (56000 KPA) HYDRAULIC AND PNEUMATIC |
MIL D 9129 : D
|
DISCHARGERS, ELECTROSTATIC - GENERAL SPECIFICATION FOR |
MIL H 26385 : E
|
HOSE, OXYGEN AND PRESSURIZATION, OZONE RESISTANT |
MIL-R-81202 Revision D:1981
|
RECEIVER ASSEMBLY, NITROGEN, FOR LAU-7 SERIES LAUNCHERS |
MIL I 7627 : F
|
INDICATOR, TURN AND SLIP 28V DC |
MIL-P-25621 Revision B:1974
|
PRESERVATION, PACKAGING AND PACKING OF RUBBER AND NYLON FUEL, OIL AND WATER PLUS ALCOHOL CELLS |
MIL-R-8236 Revision F:1995
|
REEL, SHOULDER HARNESS, INERTIA LOCK |
MIL-A-85055 Base Document:1979
|
AVIONICS SYSTEM PERFORMANCE SPECIFICATION FOR A-4M/AV-8 BOMBING SET, ANGLE RATE AN/ASB-19(V) |
MIL-STD-1556 Revision B:1986
|
GOVERNMENT/INDUSTRY DATA EXCHANGE PROGRAM CONTRACTOR PARTICIPATION REQUIREMENTS |
MIL S 5765 : F
|
STRAND, WIRE ROPE, ARMORED STEEL |
MIL C 38214 : B
|
COMPASS, MAGNETIC,MOUNTED |
MIL-M-49199 Revision A:1985
|
MICROPHONE, LINEAR M-162/AIC GENERAL SPECIFICATIONS FOR |
MIL D 83320 : 0
|
DETECTOR, MAGNETIC AZIMUTH DSU-14/A |
MIL-P-9388 Revision B:1986
|
PUMP, PRESSURE, OIL FREE AIR TYPE MA-2 |
MIL-I-85071 Revision A:1992
|
INVERTERS, AIRCRAFT, DC TO AC, GENERAL SPECIFICATION FOR |
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-S-27447 Revision A:1976
|
SURVIVAL KIT, PARACHUTE PACK SRU-16/P |
MIL F 5373 : D
|
FUSEHOLDER, BLOCK TYPE, AIRCRAFT |
MIL-A-38140 Revision B:1977
|
ALTIMETER, PRESSURE AAU-16/A |
MIL C 27536 : B
|
COUPLING, CLAMP, GROOVED, V-BAND |
MIL H 81014 : A NOTICE 1
|
HOOK, HELICOPTER, EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C |
MIL-A-27471 Revision C:1993
|
ADAPTER, PRESSURE-REDUCER, IN-LINE CRU-43A/A |
MIL-G-25597 Revision D:1973
|
GYROSCOPE, DISPLACEMENT, ROLL AND PITCH, TYPE MD-1 |
SAE AS 8181 : 1997
|
DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS, GENERAL SPECIFICATION FOR |
MIL B 8954 : B
|
BASE AND ACCESSORIES, AIRPORT MARKER LIGHTS, GENERAL SPECIFICATION FOR |
MIL-C-87972 Revision A:1987
|
CASTERS, RIGID AND SWIVEL, GENERAL SPECIFICATION FOR |
MIL H 27516 : D
|
HOSE AND HOSE ASSEMBLY, NON-METALLIC, SUCTION AND DISCHARGE |
MIL H 27267 : B
|
HOSE TETRAFLUOROETHYLENE, HIGH TEMPERATURE, MEDIUM PRESSURE |
SAE AS 8905 : 2012
|
FITTINGS AND CARGO RINGS, TIE-DOWN, AIRCRAFT FLOOR |
MIL S 9395 : F
|
SWITCHES, PRESSURE, [ABSOLUTE, GAGE AND DIFFERENTIAL] GENERAL SPECIFICATION FOR |
MIL-S-38160 Revision B:1968
|
Selector, Antenna C-4808/ARC |
MIL C 38359 : A
|
CABLE, POWER, ELECTRICAL, AIRPORT LIGHTING, CROSS-LINKED, POLYETHYLENE XLP |
MIL I 27220 : B
|
INDICATOR SET, LIQUID OXYGEN QUANTITY A/A24J-8 |
MIL-I-83449 Base Document:1974
|
INDICATOR SET, LIQUID OXYGEN QUANTITY, A/A24J-21 |
MIL T 27535 : A
|
TRANSFORMER, POWER, ISOLATION, SERIES CIRCUIT, AIRPORT LIGHTING, GENERAL SPECIFICATION FOR |
MIL-A-85072 Revision A:1987
|
ACTUATOR, ELECTROMECHANICAL, LINEAR |
MIL B 5806 : F
|
BOX, SHIPPING, AND STORAGE, HELICOPTER BLADE |
MIL-P-9024 Revision G:1972
|
PACKAGING, MATERIALS HANDLING AND TRANSPORTABILITY, SYSTEM AND SYSTEM SEGMENTS GENERAL SPECIFICATION FOR |
MIL P 83207 : B
|
PITOT STATIC TUBE, NOSE BOOM, COMPENSATED, GENERAL SPECIFICATION FOR |
MIL-T-83823 Base Document:1991
|
TRUCK, FIRE FIGHTING (STRUCTURAL OR BRUSH STRUCTURAL) |
MIL-I-38338 Revision D:1991
|
INDICATOR, OIL QUANTITY, CONTINUOUS TRANSMISSION, NUCLEONIC |
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 R 87978 : LATEST
|
REMOVER, PAINT, EPOXY AND POLYURETHANE SYSTEMS, TANK TYPE: AMBIENT TEMPERATURE, FOR AIRCRAFT WHEELS AND LANDING GEAR COMPONENTS |
MIL V 27166 : D
|
VALVE, PRESSURE EQUALIZING, GASEOUS PRODUCTS |
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 T 25620 : C
|
TESTER, OXYGEN MASK, HEADSET AND MICROPHONE, TYPE MQ-1A |
MIL-I-27202 Revision A:1980
|
INDICATOR, ELECTRICAL TACHOMETER, 0-110 PERCENT RPM 2-INCH SIZE, INTEGRALLY LIGHTED |
MIL-P-5431 Revision A:1967
|
Plastic, Phenolic, Graphited Sheets, Rods, Tubes and Shapes |
MIL M 7584 : A
|
METER, FUEL FLOW SYNCHRO STYLE TYPE B 3A |
SAE AMS R 25988 : 2017
|
RUBBER, FLUOROSILICONE ELASTOMER, OIL-AND-FUEL-RESISTANT, SHEETS, STRIPS, MOLDED PARTS AND EXTRUDED SHAPES |
SAE AS 8796 : 2013
|
HOSE, AIR DUCT, FLEXIBLE, AIRCRAFT |
SAE AS 38404 : 2013
|
COUPLINGS, HOSE, REATTACHABLE SCREW-ON |
MIL H 25579 : E
|
HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
MIL-C-6985 Revision B:1966
|
CLAMP, HOSE |
MIL-T-83303 Revision C:1988
|
TRUCK, FIREFIGHTING, AIRFIELD RAMP, 4X4, A/S32P-20, TWIN AGENT, SKID MOUNTED |
MIL-C-4751 Revision D:1983
|
CASTERS, RIGID AND SWIVEL, PRECISION HEAVY DUTY, AND SHOCK ABSORBING |
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 C 38159 : B
|
CONNECTOR, ELECTRIC, RAMP POWER, 480/277 VOLTS, GENERAL SPECIFICATION FOR |
MIL-A-83477 Revision A:1976
|
AIR CONDITIONER, A/M32C-18 TRAILER MOUNTED, DIESEL ENGINE DRIVEN |
MIL-STD-2097 Revision A:1989
|
ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
MIL-R-38522 Revision B:1972
|
RADOME CW-860/GPS |
MIL-M-87113 Revision A:1993
|
MASK, OXYGEN, MBU-10/P |
MIL-R-85111 Revision A:1980
|
RECOVERY ASSIST SECURING AND TRAVERSING SYSTEM FOR LAMPS MK 111 HELICOPTER |
MIL-P-85710 Base Document:1986
|
PARACHUTES, PERSONNEL, EMERGENCY ESCAPE GENERAL DESIGN SPECIFICATION FOR |
MIL F 83870 : A
|
FILTER ELEMENT, FLUID PRESSURE, TRANSMISSION, AIRCRAFT DISPOSABLE, 20 MICRON ABSOLUTE |
MIL C 87104 : 0
|
COAXIAL ASSEMBLIES, GENERAL SPECIFICATION FOR |
MIL-T-38049 Revision A:1972
|
TRANSMITTER, PRESSURE TRU 60A |
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-I-87965 Base Document:1979
|
INDICATOR, THRUST, ENGINE TESTING, TEST STAND AIRCRAFT ENGINE, A/M37 SERIES |
MIL STD 1763 : A
|
AIRCRAFT STORES CERTIFICATION PROCEDURES |
MIL-A-81918 Base Document:1976
|
ADAPTER, LAUNCHER, AIRCRAFT, ADU-299A/A |
MIL W 5521 : B
|
WASHER, AIRCRAFT HYDRAULIC PACKING BACK UP |
MIL-C-38392 Revision A:1969
|
COMPRESSOR, HERMETIC, AIR CONDITIONING, GENERAL SPECIFICATION FOR |
MIL-A-26624 Revision B:1981
|
AIR CONDITIONER, A/M32C-5, TRAILER MOUNTED, VAPOR CYCLE, ELECTRIC MOTOR DRIVEN |
MIL-G-52732 Revision B:1985
|
GENERATORS SETS, GASOLINE ENGINE DRIVEN 0.5KW THRU 10KW 60 HERTZ 400 HERTZ & 28V DIRECT CURRENT TYPE 1 (TACTICAL) CLASS 2 (UTILITY) GENERAL SPECIFICATION FOR |
MIL H 81529 : 0
|
HOOK, HELICOPTER EXTERNAL CARGO, 6,000 POUND CAPACITY TYPE A |
MIL-C-5778 Revision D:1992
|
COVER, AIRCRAFT COMPONENTS, GENERAL REQUIREMENTS FOR |
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-T-25363 Revision D:1973
|
TANK, PNEUMATIC PRESSURE, AIRCRAFT, GLASS FIBER |
MIL-A-27195 Revision A:1989
|
ACCELEROMETER, AIRCRAFT, MECHANICAL ABU-6/A |
MIL B 38608 : A
|
BOMB, FIRE, BLU-23/B |
MIL-H-4495 Revision D:1985
|
HOSE ASSEMBLY, RUBBER, AERIAL REFUELING |
MIL-C-85636 Base Document:1984
|
CLOTH, KNIT, JERSEY, ARAMID |
SAE AS 1960 : 2013
|
COUPLING ASSEMBLY, V-BAND, SHEET METAL FLANGE, PNEUMATIC TUBE |
MIL H 6615 : E
|
HOSE ASSEMBLIES, RUBBER, FUEL AND WATER, WITH DETACHABLE COUPLINGS, LOW TEMPERATURE |
MIL-F-25381 Revision A:1972
|
FLIGHT TESTING, ELECTRICAL SYSTEM, PILOTED AIRCRAFT AND GUIDED MISSILE, GENERAL REQUIREMENTS FOR |
MIL-C-38972 Base Document:1970
|
CARTRIDGE, BOMB EJECTION CCU-9/B |
MIL-B-26220 Revision D:1974
|
BATTERIES, STORAGE, AIRCRAFT, NICKEL-CADMIUM GENERAL SPECIFICATION FOR |
MIL S 25057 : B
|
SCREEN SYSTEM, AIR INLET, AIRCRAFT TURBINE ENGINE, GENERAL SPECIFICATION FOR |
MIL-R-85895 Base Document:1988
|
RACK, BOMB EJECTOR, AIRCRAFT BRU-32/A |
MIL E 8971 : B
|
ELECTRODES, GRAPHITE, SPECTROSCOPIC GRADE |
MIL-S-8512 Revision D:1974
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
MIL-A-49273 Base Document:1988
|
AMPLIFIER, POWER SUPPLY AM-7152/GRC-213 & ADAPTER KIT, VEHICLE MK-2154/GRC-213 |
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-C-85019 Base Document:1976
|
COMPUTER, AIR NAVIGATION, TRUE AIRSPEED, MACH NUMBER, WIND COMPONENTS SUPERSONIC, TYPE MB-9 |
SAE MA 620 : 2015
|
HOSE ASSEMBLIES, CONVOLUTED POLYTETRAFLUOROETHYLENE METALLIC REINFORCED, HIGH TEMPERATURE, MEDIUM PRESSURE, AIRCRAFT METRIC |
MIL-P-58102 Base Document:1978
|
PLASTIC SHEET AND LAMINATES, FLEXIBLE FOR ENVIRONMENTAL PROTECTIVE STORAGE AND SHIPPING SYSTEMS |
MIL-A-85652 Base Document:1984
|
AMPLIFIER-MIXER AM-7157/DKT-59 |
MIL-HDBK-2097 Revision A:1997
|
ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
MIL-S-83427 Base Document:1974
|
SURVIVAL KIT CONTAINERS, CNU-129(V)/P AND CNU-130/P |
MIL-A-85648 Base Document:1983
|
AMPLIFIER, TRAVELING WAVE TUBE |
MIL B 8075 : D
|
BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
MIL-H-13109 Revision A:1966
|
HEADSET, ELECTRICAL, GENERAL SPECIFICATION FOR |
MIL-S-83129 Revision A:1972
|
SPECTROMETER, FLUID ANALYSIS A/E35U-3 |
MIL-C-25973 Revision B:1971
|
CONVERTER, LIQUID OXYGEN, GCU-12A/A |
MIL-C-38373 Revision B:1975
|
CAP, FLUID TANK FILLER |
SAE AS 38390 : 2013
|
Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 4000 psi, 160 °F, Covered Pneumatic |
SAE AS 4897 : 1994
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE (PTFE), LOW PRESSURE, 450 DEGREES F AND FIREPROOF, PROCUREMENT SPECIFICATION FOR |
MIL-T-9720 Revision F:1984
|
Truck, Lift, Aerial Stores, 3000 Pounds Capacity MJ-1A and MJ-1B |
MIL-S-6330 Revision H:1965
|
SURVIVAL KIT, LIFE RAFT |
MIL-H-38360 Revision B:1966
|
HOSE, ASSEMBLIES, TETRAFLUOROETHYLENE, HIGH-TEMPERATURE, HIGH PRESSURE, 3000 PSI HYDRAULIC AND PNEUMATIC |
MIL-M-9397 Revision E:1979
|
FREQUENCY CONVERTER, MOBILE, TYPE MC-1A |
MIL-A-85116 Base Document:1980
|
ACTUATOR, PISTON, MINIATURE |
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-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-C-38404 Revision E:1992
|
COUPLING, HOSE, REATTACHABLE SCREW-ON |
MIL-A-38331 Base Document:1964
|
AMPLIFIER-POWER SUPPLY AM-4080/ASN-55, LEVELLING |
MIL-A-85317 Base Document:1980
|
ACTUATOR, ELECTRO-PYROTECHNIC, LINEAR, ATU-89/B |
MIL-V-8610 Revision B:1984
|
VALVE, FUEL SHUTOFF SOLENOID OPERATED, 28 VOLT, DC |
MIL-I-27273 Revision A:1965
|
INVERTER, POWER, STATIC, GENERAL SPECIFICATION FOR |
MIL-M-27274 Revision E:1993
|
MASK, OXYGEN MBU-5/P |
MIL V 8057 : F
|
VALVE, OXYGEN, PRESSURE BUILDUP AND VENT |
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-W-87105 Base Document:1977
|
WAVEGUIDE ASSEMBLIES, GENERAL SPECIFICATION FOR |
MIL-S-9487 Revision C:1985
|
SWITCH, TRIGGER, SINGLE POLE, TWO STAGE, MOMENTARY |
MIL STD 1550 : 0
|
QUALITY ASSURANCE TESTING AND INSPECTION OF AIRCRAFT CREW EMERGENCY ESCAPE PROPELLANT EQUIPMENT |
MIL-A-83216 Revision B:1976
|
AIR CONDITIONER A/E32C-39 |
MIL-V-5461 Revision C:1977
|
VALVE, VACUUM BREAKING |
MIL-S-18471 Revision G:1983
|
|
MIL-C-83821 Base Document:1990
|
CRANE, WHEEL MOUNTED, CRASH, ROUGH TERRAIN, HYDRAULIC FULL REVOLVING, 4X4, DED, FIGHTER TYPE AIRCRAFT |
MIL-I-26382 Revision C:1994
|
INDICATOR SET, LIQUID OXYGEN QUANTITY A/A24J-4 AND A/A24J-8 |
MIL I 85581 : 0
|
INTERVALOMETER, ROCKET LAUNCHER, REUSABLE |
MIL T 25920 : C
|
TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION |
MIL-DTL-27536 Revision C:1995
|
COUPLING, CLAMP, GROOVED, V-BAND |
MIL-A-28988 Revision B:1982
|
AMPLIFIER, RADIO FREQUENCY, AM-6545/GRC-193 |
MIL-C-7474 Revision E:1978
|
CASTER, INDUSTRIAL |
MIL H 8794 : D
|
HOSE, RUBBER, HYDRAULIC, FUEL AND OIL RESISTANT |
MIL-C-85637 Revision A:1987
|
CLOTH, LAMINATED, FIRE RESISTANT, WATERPROOF AND MOISTURE VAPOR PERMEABLE |
MIL-F-25562 Revision B:1964
|
FILTER, RADIO INTERFERENCE F AND 245-APX AND 25 |
MIL-I-6533 Revision B:1970
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, MULTIFUNCTION TYPE G 10 |
MIL-C-85300 Base Document:1982
|
COOLER, CRYOGENIC DETECTOR |
MIL-M-4871 Revision C:1984
|
MAINTENANCE PLATFORM |
MIL-C-4952 Revision E:1988
|
CARTRIDGES, DESICCANT, DEHYDRATOR |
MIL C 5898 : D
|
CORD, ELECTRICAL [WF 5/U, WF 14/U,WD 34/U, WM 53/U, WM 85/U] |
MIL-H-7365 Revision D:1986
|
HOSE, AIR DUCT, FOR GROUND HEATERS |
MIL-I-27882 Revision A:1963
|
INDICATOR, LIQUID OXYGEN, QUANTITY GMU-37/A |
MIL-A-38202 Revision C:1972
|
AIRCRAFT ARRESTING SYSTEM BAK-12A/E32A; PORTABLE, ROTARY FRICTION |
MIL-F-27630 Revision D:1970
|
FILTER-SEPARATOR, LIQUID FUEL FFU-2/E |
MIL W 5846 : C
|
WIRE, ELECTRICAL, CHROMEL AND ALUMEL, THERMOCOUPLE |
MIL S 25073 : 0
|
|
MIL-P-83763 Base Document:1969
|
POWER SUPPLY, TRANSISTORIZED |
MIL-H-85042 Revision A:1983
|
HOOKS, BOMB RACK, GENERAL SPECIFICATION FOR |
MIL-V-85033 Revision A:1981
|
VALVE CHARGING |
MIL-S-29413 Revision B:1988
|
SHELTER, JOINING CORRIDOR FOR |
MIL-A-6224 Revision E:1976
|
ANTENNA SUBSYSTEM FOR UHF AIRBORNE COMMUNICATIONS EQUIPMENT, GENERAL SPECIFICATION FOR |
MIL-C-87987 Base Document:1989
|
CRANE, HYDRAULIC, WHEEL MOUNTED, 7.5 & 15 TON CAPACITIES |
MIL H 49198 : A
|
HEADSET-MICROPHONE KIT, MK-1564( )/AIC |
MIL-R-5520 Revision C:1964
|
RESERVOIRS, AIRCRAFT, HYDRAULIC, NON-SEPARATED TYPE |
MIL-G-52884 Revision A:1981
|
GENERATOR SETS, DIESEL ENGINE DRIVEN, 15 THRU 200 KILOWATTS 50/60 & 400 HERTZ, (TACTICAL) |
MIL-D-21625 Revision G:1993
|
DESIGN AND EVALUATION OF CARTRIDGES FOR CARTRIDGE ACTUATED DEVICES |
MIL-B-38401 Revision A:1973
|
BEACON SET, RADIO AN/URT-33 |
MIL J 83010 : B NOTICE 1
|
JACK, AIRCRAFT LANDING GEAR MMU-87/E, 35-TON CAPACITY |
MIL-C-5136 Revision C:1968
|
CABLE, POWER, ELECTRICAL POLYCHLOROPRENE SHEATHED, BUNA COMPOUND INSULATED |
MIL-C-83864 Revision A:1982
|
CONTAINER, INNER, SURVIVAL KIT |
MIL-T-27200 Revision C:1975
|
TRANSMITTER, RATE GYROSCOPE TRU-2A/A |
MIL-L-38217 Revision D:1975
|
LIGHT, MARKER DISTRESS |
MIL-G-85468 Base Document:1981
|
GENERATOR CONTROL INDICATOR SG-118/AST-4(V) |
MIL-I-5417 Revision D:1968
|
INDICATOR, INDICATED AIRSPEED 40-400 KNOTS |
MIL-I-5721 Revision C:1970
|
INDICATOR, INDICATED AIRSPEED 20-250 KNOTS |
MIL-A-25487 Revision B:1987
|
ANTENNA AT-172()/ARN-14 |
SAE AS 5944 : 1999
|
SLINGS, AIRCRAFT, GENERAL SPECIFICATION FOR |
SAE MA 1975 : 2015
|
HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID REINFORCED, 135 DEGREE C, STANDARD DUTY, 28000/21000 KPA, HYDRAULIC, AIRCRAFT SYSTEMS |
SAE MA 1339 : 2015
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 21,000 KPA, 204 DEGREE C, LIGHTWEIGHT, HYDRAULIC AND PNEUMATIC, METRIC |
SAE AS 38386 : 2013
|
DUCT ASSEMBLY, GROUND, CONDITIONED AIR, INSULATED, FLEXIBLE |
SAE MA 2150 : 2015
|
CLAMPS, LOOP OR P STYLE, SINGLE POINT MOUNT, MULTIPLE SHAPES, METRIC |
SAE AS 4098 : 2013
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, HEAVY DUTY, METALLIC REINFORCED, 400 DEGREE F, 5000 PSI HYDRAULIC AND PNEUMATIC |
SAE MA 2126 : 2015
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE (PTFE), UP TO 232 DEGREES C AND 10 500 KPA PROCUREMENT SPECIFICATION, METRIC |
SAE MA 2250 : 2015
|
COUPLING FUEL, FLEXIBLE VARIABLE CAVITY, THREADED TYPE WITH FERRULES, METRIC |
MIL H 38390 : C
|
HOSE ASSEMBLY, TETRAFLUOROETHYLENE PNEUMATIC, HIGH PRESSURE |
MIL G 6162 : B
|
GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION |
MIL-DTL-26894 Revision D:1998
|
Hose and Hose Assembly, Rubber, Gasoline, Refueling, Low Temperature |
MIL-S-29410 Revision B:1988
|
SHELTER ASSEMBLY, RIGID GENERAL PURPOSE |
MIL F 87260 : 0
|
FOAM MATERIAL, EXPLOSION SUPPRESSION, INHERENTLY ELECTRICALLY CONDUCTIVE, FOR AIRCRAFT FUEL TANK & DRY BAY AREAS |
MIL-C-38226 Revision B:1987
|
CONTAINER, POLYURETHANE, RIGID OR ELASTIC FOR PACKAGING SMALL ENGINES |
MIL R 83397 : A
|
RUBBER, POLYURETHANE, CASTABLE, HUMIDITY RESISTANT |
MIL H 26633 : C
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, OXYGEN |
MIL I 25725 : A
|
INDICATOR, TORQUE PRESSURE, MAGNESYN STYLE, SINGLE CLAMP MOUNTED, 2 IN SIZE, 50-400 PSI TYPE A-8 |
MIL-B-87986 Base Document:1989
|
BEAD BREAKER, PNEUMATIC TIRE |
MIL C 83438 : 1986
|
CLOTHING OUTFITS, EXTREME COLD WEATHER SURVIVAL |
MIL-S-26547 Revision C:1985
|
STARTER-GENERATOR ENGINE STU-6A |
MIL-M-6404 Revision A:1965
|
METER, VOLUMETRIC, POSITIVE DISPLACEMENT LIQUID, TYPE F 1 AIRCRAFT FUEL 300 GALLONS PER MINUTE |
MIL I 38135 : B (3)
|
INDICATOR, INDICATED AIRSPEED AVU 19/A STANDBY |
MIL-STD-449 Revision D:1973
|
MEASUREMENT OF RADIO FREQUENCY SPECTRUM CHARACTERISTICS |
MIL-A-5999 Revision B:1973
|
ANTENNA SUBSYSTEM FOR AIRCRAFT MARKER BEACON EQUIPMENT GENERAL SPECIFICATION FOR |
MIL-F-21346 Revision B:1976
|
FUSEHOLDERS, BLOCK, AND SHROUD TYPE, AND ASSOCIATED FUSE CLIPS; GENERAL SPECIFICATION FOR |
MIL-A-7292 Revision A:1952
|
ANTENNA AT-190B/AP |
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-S-29412 Revision C:1994
|
SHELTER, COMPLEXING KIT FOR |
MIL W 006729 : B (1)
|
WATERTIGHTNESS OF AIRCRAFT, TESTING |
MIL-I-58067 Revision A:1977
|
INDICATOR, VERTICAL VELOCITY, RAPID RESPONSE ACCELERATION SENSITIVE, GENERAL SPECIFICATION FOR |
MIL-B-38951 Revision A:1964
|
BOMB, LOADING PRACTICE BDU-32/E |
MIL-T-81587 Revision A:1971
|
TIMER ASSEMBLY RAIN REPELLENT |
MIL-R-38987 Base Document:1972
|
RADIAC SET AN/PDR-69 |
MIL-F-8905 Revision B:1967
|
FITTINGS AND CARGO RINGS, TIEDOWN, AIRCRAFT FLOOR |
MIL-S-6551 Revision A:1981
|
|
MIL-W-5845 Revision C:1973
|
WIRE, ELECTRICAL, IRON AND CONSTANTAN, THERMOCOUPLE |
MIL-A-5034 Revision B:1979
|
ADAPTER, BOMB RACK, 30-INCH, AERO 1A |
MIL-A-25367 Revision B:1988
|
ANTENNA AT-536/ARN |
MIL C 27889 : D
|
COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING, CPU-46/A, GENERAL SPECIFICATION FOR AND MTU-38/A MOUNTING TRAY |
MIL-V-27296 Revision C:1993
|
VALVE, OXYGEN MASK, COMBINATION INHALATION AND EXHALATION |
MIL-I-85352 Base Document:1980
|
INFLATOR ASSEMBLY AND GAGE ELEMENTS, PNEUMATIC PRESSURE REMOTE CONTROL, DIRECT READING |
MIL H 26894 : C
|
HOSE ASSEMBLY, RUBBER, GASOLINE, REFUELING, LOW TEMPERATURE |
SAE AS 53731 : 2014
|
FUSE HOLDER, BLOCK TYPE, AIRCRAFT |
MIL-C-81991 Base Document:1975
|
CONVERTER, AIRCRAFT DC TO DC, BOOST GENERAL SPECIFICATION FOR |
MIL-DTL-85537 Revision A:1997
|
TRAILER, MUNITIONS, AERO 51C |
MIL-A-83462 Base Document:1975
|
ARCTIC CUSHIONS - CLOTHING, CHU-10/P AND CHU-11/P |
MIL-T-24448 Revision A:1971
|
TORSIONMETER (FOR MEASUREMENT OF TORQUE DEFLECTION OF PROPELLER PROPULSION SHAFTS OF NAVAL SHIPS) |
MIL-C-26485 Revision D:1968
|
CONTROL ASSEMBLY, ATTITUDE, GYROSCOPIC AF/A24G-1A |
MIL-S-5944 Revision C:1990
|
SLING, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL R 83725 : B
|
RELAY, VACUUM, GENERAL SPECIFICATION FOR |
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-T-26639 Revision C:1969
|
TESTER, TORQUE WRENCH |
MIL-S-5804 Revision C:1967
|
SEAT, AIRCRAFT, TROOP, WALL STYLE |
MIL H 87174 : 0
|
HELMET, FLYERS' HGU-55/P |
MIL-B-3402 Revision C:1984
|
BLOWER, GASOLINE-DRIVEN, AIRCRAFT VENTILATION, PORTABLE 2,900 CFM TYPE A-2 |
SAE AS 6302 : 2016
|
TRANSMITTER, PRESSURE, FUEL, 0-600 PSI |
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 G 8348 : H
|
GAGE, ASSEMBLIES, AIR PRESSURE, DIAL INDICATING CHUCK TYPE SELF CONTAINED |
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 R 83936 : B
|
REMOVER, PAINT, TANK TYPE, FOR AIRCRAFT WHEELS, LANDING GEAR COMPONENTS, AND OTHER AIRCRAFT AND AGE COMPONENTS |
MIL H 26521 : J
|
HOSE ASSEMBLY, NONMETALLIC, FUEL, COLLAPSIBLE, LOW TEMPERATURE WITH NON-REUSABLE COUPLINGS |
MIL-C-8956 Revision A:1970
|
CLAMP, LOOP TUBE SUPPORT |
MIL C 38618 : A
|
COUPLER, DRIVE ASSEMBLY GOVERNOR, FUZE BOMB MAU 87A B |
MIL-C-38979 Revision A:1978
|
Cartridge, Bomb Ejection CCU-1/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 |
SAE AS 85352 : 2011
|
INFLATOR ASSEMBLY AND GAGE ELEMENTS, PNEUMATIC PRESSURE, REMOTE CONTROL, DIRECT READING |
MIL-I-23252 Revision B:1981
|
INDICATOR, PRESSURE |
MIL-G-5678 Revision C:1964
|
GAGE PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE |
MIL S 38039 : B
|
SYSTEM, ILLUMINATED, WARNING, CAUTION, AND ADVISORY, GENERAL SPECIFICATION FOR |
MIL L 10911 : D
|
LOUDSPEAKER, PERMANENT MAGNET (UNENCASED, 2.5-, 3-, 4-, 5-, 6-, 8-, 10-, AND 12-, INCH DIAMETER CONE) |
MIL-W-5908 Revision D:1973
|
WIRE, ELECTRICAL, COPPER AND CONSTANTAN, THERMOCOUPLE |
MIL-D-8181 Revision B:1965
|
DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR |
MIL-A-25730 Revision C:1976
|
ANTENNA SUBSYSTEMS FOR AIRBORNE IDENTIFICATION AND NAVIGATION EQUIPMENT, GENERAL SPECIFICATION FOR |
MIL-I-81023 Revision D:1985
|
INDUCTOR, 28V, D.C. LABORATORY TEST GENERAL SPECIFICATION FOR |
MIL-B-38977 Base Document:1968
|
Bomb, Practice BDU-38/B |
MIL-I-27665 Revision B:1984
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE ABU-1O/A, -50 DEGREES TO +50 DEGREES C |
MIL E 83425 : 0
|
EARCUP, SOUND PROTECTIVE MX-8376/AR GENERAL SPECIFICATION FOR |
MIL H 83797 : 0
|
HOSE, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
MIL-T-38306 Base Document:1964
|
TRANSMITTER, RATE GYROSCOPE T 970/AJB - 7 |
MIL-S-29411 Revision B:1988
|
SHELTER ASSEMBLIES, 10 FOOT AND 20 FOOT ELECTROMAGNETIC INTERFERENCE |
MIL-B-26026 Revision B:1967
|
BATTERY, STORAGE, AIRCRAFT, TYPE MA-2-1 |
MIL-HDBK-1763 Base Document:1998
|
AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
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 H 7061 : B
|
HOSE, RUBBER, AIRCRAFT, SELF SEALING, AROMATIC FUEL |
MIL-A-38187 Revision A:1972
|
ANTENNA AT-983/ARN AND ANTENNA AT-983A/ARN |
MIL-C-29567 Base Document:1989
|
CLOTH, LAMINATED, STRETCHABLE, WATERPROOF AND MOISTURE VAPOR PERMEABLE |
MIL-I-27247 Revision C:1985
|
INDICATOR, TEMPERATURE, SYNCHRO |
MIL B 83054 : B
|
BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK |
MIL-I-52172 Revision C:1983
|
INSULATION BATT, NYLON THERMAL |
MIL-C-19787 Revision C:1969
|
CABLE, ELECTRIC, TORPEDO, 65 CONDUCTOR (FOR TORPEDO CONTROL,) SHOW 172 |
MIL A 85046 : 0
|
ACTUATOR, LINEAR ELECTROMECHANICAL |
MIL P 83206 : B
|
PITOT STATIC TUBE, L SHAPED, COMPENSATED, GENERAL SPECIFICATION FOR |
MIL G 83163 : 0
|
GYRO, DIRECTIONAL CN-1251/ASN-89(V) |
SAE AS 4604 : 2003
|
HOSE ASSEMBLY, 3000 PSI, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 400 DEGREES F, HEAVY DUTY, AIRCRAFT HYDRAULIC SYSTEMS |
MIL-V-23255 Revision B:1976
|
VALVE, PRESSURE RELIEF |
MIL D 81544 : A
|
DISPENSER, PARACHUTE FLARE, SUU-44/A |
MIL A 25676 : D
|
ADAPTOR, PRESSURE LUBRICATING OIL SERVICING, AIRCRAFT |
MIL-A-9597 Revision B:1963
|
ANTENNA AT-309()/GPX |
MIL-A-27261 Revision A:1966
|
ACCELEROMETER, AIRCRAFT |
MIL-B-23306 Revision B:1985
|
BINOCULAR, SHIP, 20-POWER AND ACCESSORIES |
SAE MA 2007A : 2015
|
HOSE ASSEMBLY, TETRAFLUOROETHYLENE, LIGHTWEIGHT, 204 DEGREE C, 21000 KPA HYDRAULIC, METRIC |
SAE MA 2241 : 2015
|
COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, FIXED CAVITY, SELF-BONDING, METRIC |
SAE AS 6054 : 2006
|
DRUM, METAL-SHIPPING AND STORAGE |
SAE MA 2151 : 2015
|
CLAMP ASSEMBLIES, SADDLE OR OMEGA STYLE, TWO POINT MOUNT, MULTIPLE SHAPES, METRIC |
MIL C 38240 : C
|
COMPUTER, ALTITUDE, ALTITUDE ENCODING CPU 66, GENERAL SPECIFICATION FOR AND MTU 39/A MOUNTING TRAY |
MIL H 85800 : 0
|
HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID FIBER REINFORCED, 5000 & 8000 PSI, GENERAL SPECIFICATION FOR |
MIL-A-25933 Revision B:1985
|
ALTIMETER, PRESSURIZED COMPARTMENT, INTEGRALLY LIGHTED 0-50,000 FEET, 1-7/8 INCH DIAL |
MIL-F-8615 Revision D:1976
|
FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
PPP-C-1337 Revision B:1976
|
CONTAINERS, COMPOSITE (STEEL DRUM WITH POLYETHYLENE INSERT) |
MIL-D-28963 Revision A:1975
|
|
MIL-T-27-233 Base Document:1978
|
TRANSFORMERS AND INDUCTORS (AUDIO POWER AND HIGH POWER PULSE) INDUCTOR CHARGING TF5S37ZZ |
MIL C 87148 : 0
|
CLOTHING OUTFIT, EXTREME COLD WEATHER SURVIVAL A/P22S-14 |
MIL D 26392 : C
|
DUMMY CONVERTERS, LIQUID OXYGEN INDICATOR SYSTEM 10 LITER CRU-23/A AND 25 LITER CRU-24/A |
MIL-G-58103 Base Document:1979
|
GRIP ASSEMBLY, CYCLIC CONTROLLER, HELICOPTER |
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-B-7949 Revision E:1981
|
BEARING, BALL, AIRFRAME, ANTIFRICTION |
MIL T 83174 : B (3)
|
TRANSMITTER, ACCELEROMETER, AXIAL |
MIL A 83366 : 0
|
ANTENNA ASSEMBLIES, AIRBORNE, GENERAL SPECIFICATION FOR |
MIL S 8932 : A
|
SWITCH, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-B-85099 Base Document:1978
|
BATTERY, WET PRIMARY FOR AN/DKT-37(V) TELEMETRY PACKAGE |
MIL H 83298 : A
|
HOSE, TETRAFLUOROETHYLENE, HIGH TEMPERATURE, HIGH PRESSURE (3000 PSI) HYDRAULIC AND PNEUMATIC |
MIL-H-58108 Base Document:1986
|
HEADSET-MICROPHONE KIT MK-2193/AIC |
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-G-52889 Revision C:1981
|
GENERATOR SET, DIESEL ENGINE DRIVEN 5 KW, 60 HERTZ & 10 KW, 60 & 400 HERTZ TACTICAL, UTILITY, GENERAL SPECIFICATION FOR |
MIL D 26503 : A
|
DETECTOR, MAGNETIC AZIMUTH AND COMPENSATOR, DETECTOR, MAGNETIC AZIMUTH |
SAE AS 85075 : 2000
|
TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR |
MIL F 81836 : A SUPP 1
|
FILTER AND DISPOSABLE ELEMENT, FLUID PRESSURE, HYDRAULIC, 3 MICRON ABSOLUTE |
MIL-L-85297 Base Document:1980
|
LEAD, EXPLOSIVE MARK 24 MOD O MARK 25 MOD O |
MIL-D-18300 Revision H:1993
|
DESIGN EXAMINATIONS, ENGINEERING AVIONIC SYSTEMS/EQUIPMENT GENERAL REQUIREMENTS FOR |
MIL-C-25601 Revision C:1969
|
COUPLER, ANTENNA CU-308D/U |
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 L 25567 : D
|
LEAK DETECTION COMPOUND, OXYGEN SYSTEMS (METRIC) |
MIL-I-83117 Revision B:1975
|
INDICATOR, ANGLE OF ATTACK |
MIL-C-6235 Revision D:1970
|
COMPASS, MAGNETIC, UNMOUNTED POCKET SURVIVAL |
MIL-T-26963 Revision D:1992
|
TESTER, PRESSURE GAGE, HYDRAULIC, PORTABLE TYPE MP-1 |
MIL-I-25941 Revision D:1986
|
INDICATOR, TURN AND SLIP, 2-INCH SIZE, INTEGRALLY LIGHTED |
MIL M 4803 : D
|
MOTOR-GENERATOR, 400 HZ PRECISE OUTPUT, GENERAL REQUIREMENTS FOR |
MIL-L-85314 Revision A:1983
|
LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
MIL-I-7084 Revision A:1988
|
INDICATOR, PRESSURE, HYDRAULIC 0-4,000 PSI |
MIL-G-25591 Revision E:1981
|
GYROSCOPE, RATE, SWITCHING, TYPE MC-1 |
MIL-L-6273 Revision D:1983
|
LIGHT, NAVIGATIONAL, BEACON, OBSTACLE OR CODE, TYPE G 1 |
MIL-S-6904 Revision B:1965
|
Signal, Emergency Warning, General Specification For |
MIL-C-87975 Base Document:1985
|
CLOCK, AIRCRAFT, MECHANICAL ABU-32/A |
MIL-E-6051 Revision D:1967
|
ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM |
MIL-P-5315 Revision B:1964
|
PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT |
MIL-I-24772 Base Document:1992
|
INDICATOR, OXYGEN, COMBUSTIBLE GAS, CARBON MONOXIDE, AND HYDROGEN SULFIDE, PORTABLE (METRIC) |
MIL H 26666 : D (1)
|
HOSE ASSEMBLY, PNEUMATIC, HIGH PRESSURE |
MIL-C-27505 Revision B:1967
|
Cartridge, Engine Starter MXU-4A/A |
MIL-I-27619 Revision G:1974
|
INDICATORS, ATTITUDE DIRECTOR |
MIL-R-5049 Revision D:1989
|
RING, WIPER, PISTON ROD |
MIL H 87961 : NOTICE 2
|
HOSE AND HOSE ASSEMBLIES, AIR DUCT, AIR BREATHING, OXYGEN SYSTEM GENERAL SPECIFICATION FOR |
MIL A 25949 : E (2)
|
ACCELEROMETER, AIRCRAFT RANGE -5 TO PLUS 1OG UNITS, INTEGRALLY LIGHTED |
MIL-C-83435 Base Document:1974
|
CLOTHING OUTFIT, EXTREME COLD WEATHER SURVIVAL A/P22S-10 |
MIL-C-38207 Revision A:1965
|
CLOCK, AIRCRAFT, MECHANICAL ABU 11/A |
MIL I 27851 : B
|
INDICATOR, INDICATED AIRSPEED AVU-17/A |
MIL G 21480 : A
|
GENERATOR SYSTEM, 400 HERTZ ALTERNATING CURRENT, AIRCRAFT GENERAL SPECIFICATION FOR |
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-I-7075 Revision A:1965
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, MULTIFUNCTION -50 DEGREES TO +50 DEGREES C 2 INCH SIZE |
MIL T 26898 : B
|
TEST SET, AIRFIELD LIGHTING SYSTEMS, TYPE MM-1 |
MIL-B-27044 Revision C:1968
|
BOMB, PRACTICE BDU-12/B |
MIL-P-85511 Revision A:1987
|
PANEL ASSEMBLY, TARGET, BANNER, AERIAL TDU-32 SERIES |
MIL-B-83183 Revision B:1987
|
BARRIER, AIRCRAFT ARRESTING |
MIL B 38634 : LATEST
|
BOMB, FIRE, BLU 32A B |
MIL C 7115 : F
|
CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL V 25961 : F
|
VALVE, FILL-BUILDUP-VENT, LIQUID OXYGEN CONVERTER, CRU-5O/A |
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-A-38329 Base Document:1964
|
ATTITUDE HEADING REFERENCE SET AN/ASN-55 |
MIL-P-38268 Revision C:1988
|
AURAL PROTECTORS, SOUND |
MIL-T-5420 Revision B:1970
|
TUBE, PITOT STATIC, ELECTRICALLY HEATED, AIRCRAFT |
MIL C 38333 : 0
|
CONTROLLER, COMPASS SYSTEM C-6448/ASN-55 |
MIL B 83771 : A
|
BATTERY, REMOTELY ACTIVATED SUBMINIATURE RESERVE PRIMARY |
MIL L 7830 : D
|
LIGHT ASSEMBLY, MARKER, AIRCRAFT OBSTRUCTION |
MIL L 24560 : 0
|
LIGHTS AND GLASSWARE FOR NAVIGATION, SIGNAL AND WARNING, NAVAL SHIPBOARD USE, GENERAL SPECIFICATION FOR |
MIL C 87147 : 0
|
OUTLINES VACUUM PACKAGED ACCESSORIES FOR THE SRU-6/P overcoat. |
MIL-C-27212 Revision B:1970
|
CABLE, POWER, ELECTRICAL, AIRPORT LIGHTING CONTROL |
MIL I 83361 : (4)
|
INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
MIL-B-25820 Revision B:1967
|
BOMB, LOADING PRACTICE BDU-6/E AND BDU-35/E |
MIL-B-22227 Revision A:1976
|
BEARING, BALL, ANNULAR, GENERATOR AND MOTOR-GENERATOR |
MIL C 38257 : 0
|
CONTROL, TRANSPONDER SET C-6280( )(P)/APX |
MIL-P-38136 Revision A:1969
|
PITOT STATIC TUBE COMPENSATED TRU 62/A |
MIL-C-7942 Revision B:1966
|
CONNECTORS, HOSE, QUICK-DISCONNECT, ANTI "G" SUIT |
MIL R 25988 : B
|
RUBBER, FLUOROSILICONE ELASTOMER, OIL AND FUEL RESISTANT, SHEETS, STRIPS, MOLDED PARTS AND EXTRUDED SHAPES |
MIL S 9419 : E
|
SWITCH, TOGGLE, MOMENTARY, FOUR-POSITION ON, CENTER OFF, GENERAL SPECIFICATION FOR |
MIL-DTL-81944 Revision C:1997
|
TRAILER, MUNITIONS, SMALL (MHU-126 A/M) |
MIL-P-8945 Revision A:1967
|
PANEL, RELAY, PILOT, ENCLOSED, AIRPORT LIGHTING |
MIL-I-26380 Revision B:1964
|
INDICATOR, LIQUID OXYGEN QUANTITY GMU-5/A |
MIL-F-25880 Revision B:1972
|
FILTER, BAND PASS, BAND SUPPRESSION F -339/A |
MIL P 83825 : 0
|
PANEL ASSY, AUTOMATIC POWER TRANSFER FOR MB-TEEN AND EMU SERIES DIESEL ENGINE GENERATOR SETS |
MIL-A-85434 Revision A:1983
|
AMPLIFIER, TRAVELING WAVE TUBE AM-6937/DLQ-3B |
SAE AS 5778 : 1997
|
COVERS, AIRCRAFT COMPONENTS, GENERAL REQUIREMENTS FOR |
MIL T 25627 : C
|
TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |
MIL-A-27391 Revision B:1963
|
ALTIMETER, PRESSURE AAU-2A |
MIL D 6054 : F
|
DRUM, METAL - SHIPPING AND STORAGE |
MIL-C-38973 Base Document:1970
|
CARTRIDGE, BOMB EJECTION CCU-10/B |
MIL-M-25500 Revision B:1969
|
MOCKUP TESTING, ELECTRICAL SYSTEM, PILOTED AIRCRAFT AND GUIDED MISSILE, GENERAL REQUIREMENTS FOR |
MIL-A-83039 Revision B:1971
|
AIR CONDITIONER A/M32C-10A AIR CYCLE FOR AIRCRAFT GROUND SUPPORT |
MIL-C-58104 Revision A:1983
|
COVER, PROTECTIVE FOR PARTS AND EQUIPMENT |
SAE AS 6399 : 1999
|
HOSE, RUBBER, WIRE-WOUND, SYNTHETIC, ICE ELIMINATING SYSTEM |
SAE AS 6451 : 2013
|
SHIELDS, PROTECTIVE, AIRCRAFT AND MISSILES |
SAE AIR 4728 : 2013
|
REFERENCES, SPACECRAFT AND SPACECRAFT SERVICING, FLUID SYSTEM COMPONENTS (ABBREVIATIONS, ACRONYMS, DEFINITIONS, APPLICABLE DOCUMENTS AND ENVIRONMENTAL CONDITIONS) |
NAS1599:1980
|
CONNECTORS, GENERAL PURPOSE, ELECTRICAL, MINIATURE CIRCULAR, ENVIRONMENT RESISTING, 200 DEG. C. MAXIMUM TEMPERATURE |
SAE MA 614 : 2015
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE (PTFE), METALLIC REINFORCED, 28,000 KPA, 204 DEGREES C, HYDRAULIC, METRIC |
SAE MA 4623 : 2015
|
Hose Assembly, Polytetrafluoroethylene, Para Aramid Reinforced Heavy-Duty, 21 000 kPa, 135 °C, Aircraft Hydraulic Systems, Metric |