MIL-STD-831 Base Document:1963
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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TEST REPORTS, PREPARATION OF
Available format(s)
PDF
Superseded date
23-04-1999
Superseded by
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Provides format and contact criteria for preparation of test reports covering tests on systems, subsystems, components, equipments and parts. Coverage includes applicable documents, definitions, page size, format, margins, abbreviations, corrected pages, color differentiation, and illustrations. Also gives detailed diagrams.
| DocumentType |
Standard
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| Pages |
18
|
| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| 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 MA4098 | Hose Assembly, Polytetrafluoroethylene, Heavy Duty, Metallic Reinforced, 204 °C, 35 000 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 AS4388 | Hose Assembly PTFE Heavy Duty, -65 To 400 °F (-55 To 204 °C) 8000 psi (56 000 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 Specification 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 AS8181A | 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 AS8905A | 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 AMSR25988A | Rubber, Fluorosilicone Elastomer, Oil-and-Fuel-Resistant, Sheets, Strips, Molded Parts, and Extruded Shapes |
| SAE AS8796 | Hose, Air Duct, Flexible, Aircraft |
| SAE AS38404 | 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 AS1960 | 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 MA620 | 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 AS38390 | Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 4000 psi, 160 °F, Covered Pneumatic |
| SAE AS4897 | Hose Assembly, Polytetrafluoroethylene (PTFE), Low Pressure, 450 °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 | 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-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 | System, Aircrew Automated Escape, Ejection Seat Type, General Specification For |
| 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/A241-8 |
| 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 AS5944 | Slings, Aircraft, General Specification For |
| SAE MA1975 | Hose Assemblies, Polytetrafluoroethylene, Aramid Reinforced, 135 °C, Standard Duty, 28 000/21 000 kPa, Hydraulic, Aircraft Systems |
| SAE MA1339 | Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 21,000 kPa, 204 °C, Lightweight, Hydraulic and Pneumatic, Metric |
| SAE AS38386 | Duct Assembly, Ground, Conditioned Air, Insulated, Flexible |
| SAE MA2150 | Clamps, Loop or P Style, Single Point Mount, Multiple Shapes, Metric |
| SAE AS4098A | Hose Assembly, Polytetrafluoroethylene, Heavy Duty, Metallic Reinforced, 400 °F, 5000 psi Hydraulic and Pneumatic |
| SAE MA2126B | Hose Assembly, Polytetrafluoroethylene (PTFE), up to 232 °C and 10 500 kPa Procurement Specification, Metric (ISO/DIS 10502) |
| SAE MA2250 | 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 AS53731A | 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 AS6302A | 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-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 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 AS85352 | 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 AS4604B | Hose Assembly, 3000 psi, Polytetrafluoroethylene, Metallic Reinforced, 400 °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 MA2007A | Hose Assembly, Tetrafluoroethylene, Lightweight, 204 °C, 21 000 kPa Hydraulic, Metric |
| SAE MA2241 | Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Metric |
| SAE AS6054 | Drum, Metal-Shipping and Storage |
| SAE MA2151 | 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 AS6451A | Shields, Protective, Aircraft and Missiles |
| SAE AIR4728 | 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 MA614A | Hose Assembly, Polytetrafluoroethylene (PTFE), Metallic Reinforced, 28,000 kPa, 204 °C, Hydraulic, Metric |
| SAE MA4623 | Hose Assembly, Polytetrafluoroethylene, Para Aramid Reinforced Heavy-Duty, 21 000 kPa, 135 °C, Aircraft Hydraulic Systems, Metric |
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