MIL-STD-794 Revision E:1982
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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PART AND EQUIPMENT, PROCEDURES FOR PACKAGING AND PACKING OF
Available format(s)
PDF
Superseded date
23-07-2013
Publisher
Measures for packaging parts and equipment based on their composition, surface finish, weight, size, configuration and required level of protection. Coverage includes referenced documents, definitions, packaging design drawings, reusable containers, unpacking instructions, packing, marking, hazardous material shipment, security assistance material, and packaging design validation. Also gives tables and appendices.
| DocumentType |
Standard
|
| Pages |
124
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| MIL-W-17316 Revision A:1980 | WIND MEASURING SET AN/PMQ-30 (COMPONENTS OF) |
| MIL A 85670 : 0 | ANTENNA, BROADBAND AS-3191/A, AS-3792/A, AND AS -3793/A |
| MIL C 38240 : C | COMPUTER, ALTITUDE, ALTITUDE ENCODING CPU 66, GENERAL SPECIFICATION FOR AND MTU 39/A MOUNTING TRAY |
| MIL-V-25023 Revision B:1967 | VALVE, FUEL DRAIN, SELF-LOCKING |
| DOD-S-87956 Base Document:1979 | SHELTER, S-80A AND S-82A |
| MIL-I-18856 Revision B:1969 | INDICATOR, ANGLE OF ATTACK, 28V DC MS28062 AND MS28067 |
| MIL-T-38034 Revision E:1970 | TIMER, FIRE CONTROL, BOMBING, DUAL |
| MIL-A-38307 Revision A:1981 | ACCELEROMETER, AIRCRAFT, MX-6663/AJB-7 |
| MIL-R-38370 Revision B:1972 | RECORDING SET, FLIGHT DATA A/A24U-10 |
| MIL-P-81655 Base Document:1970 | PITOT STATIC TUBE, L-SHAPED, COMPENSATED, ELECTRICALLY HEATED, GENERAL SPECIFICATION FOR |
| MIL-C-87979 Base Document:1987 | CLOCK, AIRCRAFT, ELECTRONIC |
| GGG-M-125-7 Revision B:1985 | RESPIRATOR ASSEMBLY: HALF MASK, AIR-PURIFYING, COMBINATION CHEMICAL CARTRIDGE AND FILTER (FOR PESTICIDES AND ORGANIC VAPORS) |
| MIL-T-81998 Base Document:1975 | TEST SET, RADIO SET AN/ARM-165 |
| MIL-S-85018 Revision A:1978 | Second Order Attitude Reference System (Soars) AN/ASN-116 |
| MIL-G-17713 Revision D:1988 | GAGES, LIQUID LEVEL MEASURING, TANK |
| SAE AMS 3731 : 2016 | POTTING COMPOUND, EPOXY, BISPHENOL A-TYPE |
| MIL-I-7062 Revision C:1975 | INDICATOR, POSITION, CONTROL SURFACES, 28 VOLT DC, GENERAL SPECIFICATION FOR |
| SAE AMS 3650 : 2012 | RODS, SHEETS, AND MOLDED SHAPES, POLYCHLOROTRIFLURORETHYNEN (PCTFE) UNPLASTICIZED |
| MIL-I-7065 Revision A:1976 | INDICATOR, POSITION, AILERON TRIM TAB |
| MIL-P-25518 Revision B:1981 | Plastic Materials, Silicone Resin, Glass Fiber Base, Low Pressure Laminated |
| MIL-E-23001 Revision B:1976 | ELECTRIC GENERATING SYSTEM, VARIABLE SPEED CONSTANT FREQUENCY, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL F 8815 : D | FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC LINE, 15 MICRON ABSOLUTE AND 5 MICRON ABSOLUTE, TYPE 11 SYSTEMS; GENERAL SPECIFICATION FOR |
| MIL T 27252 : A | TEST SET, SYNCHRO, TTU-73/E DC SELSYN, AIRCRAFT INSTRUMENTS |
| SAE AMS 3695 : 2014 | ADHESIVE FILM, EPOXY-BASE, FOR HIGH DURABILITY STRUCTURAL ADHESIVE BONDING |
| MIL-T-83460 Base Document:1975 | TRANSDUCER, MOTIONAL PICKUP TRU-164/A |
| MIL D 9129 : D | DISCHARGERS, ELECTROSTATIC - GENERAL SPECIFICATION FOR |
| MIL I 7627 : F | INDICATOR, TURN AND SLIP 28V DC |
| MIL-R-81202 Revision D:1981 | Receiver Assembly, Nitrogen, for LAU-7 Series Launchers |
| MIL-I-83152 Revision B:1974 | INDICATOR, INDICATED-AIRSPEED AVU-22/A (INDICATOR-TRANSDUCER) |
| MIL-A-85055 Base Document:1979 | Avionics System Performance Specification for A-4M/AV-8 Bombing Set, Angle Rate AN/ASB-19(V) |
| MIL-B-36558 Revision B:1992 | BEDS, ADJUSTABLE |
| 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 C 38214 : B | COMPASS, MAGNETIC,MOUNTED |
| MIL-C-27298 Revision B:1980 | CLOCK, AIRCRAFT, MECHANICAL ABU AND 9-A |
| MIL F 83861 : B | FILTER ELEMENTS, NONCLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE, TYPE 1I, SYSTEMS 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 H 11996 : B | HANDSET H-60/PT, HANDSET H-156/U, AND HANDSET H-165/U |
| MIL-C-8605 Revision B:1990 | CAP, PRESSURE FUEL SERVICING |
| MIL-P-85833 Base Document:1989 | PROTECTIVE ASSEMBLY, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL |
| MIL E 85726 : A | ENCLOSURE, STANDARD AVIONICS, FORCED AIR COOLED, GENERAL SPECIFICATION FOR |
| MIL-A-38140 Revision B:1977 | ALTIMETER, PRESSURE AAU-16/A |
| MIL C 27536 : B | COUPLING, CLAMP, GROOVED, V-BAND |
| GG-C-2736 Revision A:1987 | CATHETER, CARDIOVASCULAR (FLOW DIRECTED, THERMODILUTION) |
| MIL-G-25597 Revision D:1973 | GYROSCOPE, DISPLACEMENT, ROLL AND PITCH, TYPE MD-1 |
| MIL-L-50794 Base Document:1973 | LINEAR SHAPED CHARGE ASSEMBLY |
| MIL-I-6726 Revision B:1966 | Inclinometer, Aircraft |
| MIL-C-87972 Revision A:1987 | CASTERS, RIGID AND SWIVEL, GENERAL SPECIFICATION FOR |
| MIL P 28809 : A | PRINTED WIRING ASSEMBLIES |
| MIL-E-17555 Revision H:1984 | ELECTRONIC AND ELECTRICAL EQUIPMENT, ACCESSORIES, AND PROVISIONED ITEMS (REPAIR PARTS); PACKAGING OF |
| SAE AS 8905 : 2012 | FITTINGS AND CARGO RINGS, TIE-DOWN, AIRCRAFT FLOOR |
| MIL-C-7135 Revision F:1967 | Compressor, Pneumatic, 3,000 PSI -- 2 SCFM Aero 2A (*), Aero 2A-1 (*), Aero 2B (*), and Aero 2B-1 (*) |
| MIL I 7231 : B | INDICATOR, TRUE AIRSPEED, SYNCHRO REPEATER TYPE N 1 |
| MIL-STD-1546 Revision B:1992 | PARTS, MATERIALS, AND PROCESSES CONTROL PROGRAM FOR SPACE AND LAUNCH VEHICLES |
| MIL-P-9024 Revision G:1972 | PACKAGING, MATERIALS HANDLING AND TRANSPORTABILITY, SYSTEM AND SYSTEM SEGMENTS GENERAL SPECIFICATION FOR |
| MIL-M-38706 Revision A:1984 | MULTIMETER |
| MIL P 83207 : B | PITOT STATIC TUBE, NOSE BOOM, COMPENSATED, GENERAL SPECIFICATION FOR |
| MIL W 87893 : A | WORKSTATION, ELECTROSTATIC DISCHARGE (ESD) CONTROL |
| SAE AMS 3636 : 2012 | TUBING, PLASTIC, ELECTRICAL INSULATION, IRRADIATED POLYOLEFIN, PIGMENTED, FLEXIBLE, HEAT-SHRINKABLE, 2 TO 1 SHRINK RATIO |
| MIL-P-6457 Revision E:1974 | POWER SUPPLY, METALLIC RECTIFIER TYPE, GENERAL SPECIFICATION FOR |
| 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 T 25620 : C | TESTER, OXYGEN MASK, HEADSET AND MICROPHONE, TYPE MQ-1A |
| MIL-R-85669 Base Document:1988 | REPEATER SET, RADIO, POD AN/ARQ-49 |
| MIL I 27279 : B | INDICATOR, MACH NUMBER AVU-11/A, INTEGRAL LIGHTING |
| MIL-C-5499 Revision B:1984 | CORE, AIRCRAFT, HIGH PRESSURE AIR VALVE |
| MIL-I-27202 Revision A:1980 | INDICATOR, ELECTRICAL TACHOMETER, 0-110 PERCENT RPM 2-INCH SIZE, INTEGRALLY LIGHTED |
| MIL-A-81724 Base Document:1969 | ADAPTER, LAUNCHER, AIRCRAFT, ADU-299/E |
| MIL M 7584 : A | METER, FUEL FLOW SYNCHRO STYLE TYPE B 3A |
| SAE AMS 1640 : 2011 | CORROSION REMOVING COMPOUND, FOR AIRCRAFT SURFACES |
| SAE AMS 4750 : 2017 | SOLDER, TIN-LEAD, 45SN - 55PB |
| SAE AS 8796 : 2013 | HOSE, AIR DUCT, FLEXIBLE, AIRCRAFT |
| SAE AMS 5316E : 1987(S2017) | Ductile (Nodular) Iron Castings, Sand 80,000 psi (550 MPa) Tensile Strength As Cast |
| SAE AMS 3572 : 2016 | RESIN POLYURETHANE, FOAM-IN-PLACE, RIGID |
| SAE AMS 3676 : 2015 | INSULATION, SOUND AND THERMAL, RESIN-BONDED GLASS FIBER, MEDIUM FILAMENT |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-C-28809 Revision B:1988 | CIRCUIT CARD ASSEMBLIES, RIGID, FLEXIBLE & RIGID FLEX |
| MIL-N-85353 Base Document:1981 | NUTS (FASTENERS) INTERNALLY THREADED, PRELOAD LOCKING 450 DEG F 800 DEG F,1200 DEG F, GENERAL SPECIFICATION FOR |
| MIL-C-63550 Revision E:1985 | CABLE ASSEMBLIES, ELECTRICAL, FABRICATION SPECIFICATION FOR |
| F-F-2790 Base Document:1991 | FILTER, AIR EXTENDED AREA, INITIAL INSTALLATION |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL-T-81364 Base Document:1966 | T-BOLT, 180,000 PSI TYPE 431 STAINLESS STEEL, MANUFACTURING PROCESS REQUIREMENTS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL M 29212 : B NOTICE 1 | MIXING PLANT, ASPHALT, DRUM TYPE, PORTABLE, ELECTRIC MOTOR DRIVEN, 120 TONS PER HOUR CAPACITY |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-G-81559 Revision C:1984 | Gyroscope Assemblies and Attitude and Directional Reference Instruments for Aircraft, Packaging of |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-C-85521 Base Document:1983 | Concentrator, Oxygen, GGU-7/A |
| MIL I 7067 : B | INDICATOR, POSITION, FLAPS, 0 - 60 DEGREE MARKING, 2 INCH SIZE |
| MIL-C-85829 Base Document:1989 | COUPLING ASSEMBLY, HOSE, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE |
| MIL-S-26547 Revision C:1985 | STARTER-GENERATOR ENGINE STU-6A |
| MIL-I-6447 Revision C:1974 | INDICATOR, TRUE AIRSPEED TYPE M 1A |
| MIL-STD-2097 Revision A:1989 | ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
| MIL-R-85111 Revision A:1980 | RECOVERY ASSIST SECURING AND TRAVERSING SYSTEM FOR LAMPS MK 111 HELICOPTER |
| SAE AMS 5384 : 2017 | ALLOY CASTINGS, INVESTMENT, CORROSION AND HEAT RESISTANT, 53NI - 18CR - 18CO - 4.0MO - 2.9TI - 2.9AL - 0.006B, VACUUM-MELTED, VACUUM-CAST, SOLUTION AND PRECIPITATION HEAT TREATED |
| MIL A 28875 : 0 | AMPLIFIER, RADIO FREQUENCY AND MICROWAVE, SOLID STATE, GENERAL SPECIFICATION FOR |
| MIL-F-29419 Base Document:1985 | FRAME, SHIPPING [SIXCON] |
| MIL F 83870 : A | FILTER ELEMENT, FLUID PRESSURE, TRANSMISSION, AIRCRAFT DISPOSABLE, 20 MICRON ABSOLUTE |
| MIL-I-85506 Base Document:1983 | INDICATOR, INDICATED AIRSPEED, STANDBY TYPES I, II, AND III |
| SAE AMS 3733 : 2015 | POTTING COMPOUND, EPOXY, TWO PART, HIGHLY FILLED, HEAT CURE, HIGH COMPRESSIVE STRENGTH |
| GGG-M-125-3 Revision A:1982 | RESPIRATOR ASSEMBLIES: AIR LINE, WITH DISPOSABLE HOOD (SUPPLIED AIR) |
| GGG-M-125 Revision G:1985 | RESPIRATOR AND RESPIRATOR ASSEMBLIES: AIR LINE; NON-POWERED AIR-PURIFYING AND POWERED AIR-PURIFYING |
| MIL-G-83872 Revision A:1977 | GYROSCOPE, DISPLACEMENT, TYPE SBU-23/A |
| MIL-T-38049 Revision A:1972 | TRANSMITTER, PRESSURE TRU 60A |
| GGG-M-125-2 Revision A:1982 | RESPIRATOR ASSEMBLIES: AIR LINE, WITH HELMET (SUPPLIED AIR) |
| MIL-STD-726 Revision H:1985 | PACKAGING REQUIREMENTS CODE |
| GGG-M-125-4 Revision C:1985 | RESPIRATOR ASSEMBLY: HALF MASK, AIR-PURIFYING, CHEMICAL CARTRIDGE (FOR ORGANIC VAPORS) |
| MIL C 7958 : A | CONTROL, PUSH PULL, FLEXIBLE AND RIGID |
| MIL-C-4109 Revision F:1986 | COUPLING ASSEMBLY, LOW PRESSURE, AIR HOSE, QUICK-DISCONNECT |
| MIL-E-50796 Base Document:1973 | EXPANDING SHIELDED MILD DETONATING CORD ASSEMBLY |
| SAE AS 5604 : 2012 | COMPASS: MAGNETIC, PILOT'S STANDBY |
| MIL-A-81621 Base Document:1969 | ACCELEROMETER, ELECTRICAL, LINEAR ABU-13/A |
| MIL-A-81918 Base Document:1976 | ADAPTER, LAUNCHER, AIRCRAFT, ADU-299A/A |
| SAE AS 6302 : 2016 | TRANSMITTER, PRESSURE, FUEL, 0-600 PSI |
| MIL F 28861 : B | FILTER AND CAPACITOR, RADIO FREQUENCY/ELECTROMAGNETIC INTERFERENCE SUPPRESSION, GENERAL SPECIFICATION FOR |
| GGG-M-125-11 Revision A:1982 | RESPIRATOR ASSEMBLY: HELMET WITH POWERED AIR-PURIFYING UNIT (PORTABLE BACK-PACK) |
| MIL H 81529 : 0 | HOOK, HELICOPTER EXTERNAL CARGO, 6,000 POUND CAPACITY TYPE A |
| MIL-D-81358 Revision B:1970 | Display Group, Tactical Data AN/ASA-66 |
| MIL-T-23733 Revision A:1968 | TRANSMITTER, RATE GYROSCOPE T-751 (/AJB-3) |
| MIL R 83178 : A | REGULATOR, OXYGEN, DILUTER DEMAND, AUTOMATIC PRESSURE BREATHING, GENERAL SPECIFICATION FOR |
| MIL-I-25091 Revision B:1985 | INDICATOR, CABIN AIR PRESSURE, PRESSURIZED AIRCRAFT, 1-7/8 INCH DIAL, TYPE MA-2 |
| MIL V 7899 : C | VALVE, CHECK, AIRCRAFT FUEL SYSTEM |
| MIL-T-25363 Revision D:1973 | TANK, PNEUMATIC PRESSURE, AIRCRAFT, GLASS FIBER |
| MIL-C-42061 Base Document:1988 | CAP, SCREW, BOTTLE AND JAR |
| MIL-R-42043 Base Document:1987 | REGULATOR, OXYGEN |
| GG-W-239 Revision C:1985 | WHEELS, ABRASIVE, (SILICON CARBIDE, MOUNTED, DENTAL) |
| GG-B-735 Revision B:1985 | BRUSH, BRISTLE, DENTAL HANDPIECE (MANDREL MOUNTED) |
| MIL-Y-87125 Revision A:1979 | YARN, GRAPHITE, 1000/3000 FILAMENTS |
| ZZ-H-461 Revision E:1986 | HOSE AND HOSE ASSEMBLY, RUBBER, GAS (ACETYLENE HYDROGEN, AIR AND OXYGEN |
| MIL-T-85230 Revision A:1992 | TARGET, TOW, AERIAL, TDU-34/A |
| MIL-B-37965 Base Document:1986 | BURS, BONE SURGERY (CORROSION-RESISTING STEEL) |
| MIL-E-83510 Revision A:1980 | EARPHONE ELEMENT |
| MIL W 3662 : B | WIRE, PLATINUM ALLOY [PLATINUM RUTHENIUM, PLATINUM IRIDIUM |
| MIL-A-36188 Revision B:1989 | APRON, DENTAL, PLASTIC |
| MIL M 26542 : D (1) SUPP 1 | MICROPHONE, DYNAMIC, GENERAL SPECIFICATION FOR |
| SAE AMS 3713 : 2013 | CORE, FLEXIBLE HONEYCOMB, POLYAMIDE PAPER BASE, PHENOLIC COATED |
| GG-S-1616 Revision A:1987 | SCISSORS, COLLAR AND CROWN |
| GGG-M-125-1 Revision B:1982 | RESPIRATOR ASSEMBLIES, AIR LINE, WITH FACE PIECE (SUPPLIED AIR) |
| SAE AMS 7245 : F1993 | INSERTS, THREAD FORM, CORROSION RESISTANT STEEL - 18CR 9.2NI |
| MIL-A-81258 Base Document:1965 | AMPLIFIER, RESOLVER, GENERAL SPECIFICATION FOR |
| WW-U-531 Revision F:1984 | UNION, PIPE, STEEL OR MALLEABLE IRON, THREADED CONNECTION, 150 LB, 250 LB & 300 LB WSP |
| MIL-F-63051 Revision A:1985 | FUZE, M934 SERIES ACTUATORS FOR |
| MIL T 25446 : D | TRANSMITTER, TEMPERATURE, ELECTRICAL RESISTANCE |
| MIL H 81581/8 : 0 | HOSE ASSEMBLIES, CABLE ASSEMBLIES, COMMUNICATION, ASSOCIATED |
| MIL-R-85895 Base Document:1988 | RACK, BOMB EJECTOR, AIRCRAFT BRU-32/A |
| MIL-I-5133 Revision C:1953 | INDICATOR, ATTITUDE TYPE J 8 |
| MIL-T-21578 Revision A:1966 | TEST EQUIPMENT, HAZARDOUS LOCATION, INSTALLED, BASIC REQUIREMENTS FOR |
| MIL-C-85019 Base Document:1976 | COMPUTER, AIR NAVIGATION, TRUE AIRSPEED, MACH NUMBER, WIND COMPONENTS SUPERSONIC, TYPE MB-9 |
| MIL-C-9082 Revision H:1986 | CONVERTER, OXYGEN, AIRCRAFT, LIQUID TO GASEOUS, GENERAL SPECIFICATION FOR |
| SAE AMS 3625 : 2016 | ELASTOMERIC TUBING, ELECTRICAL INSULATION, CROSSLINKED SILICONE, PIGMENTED, FLEXIBLE, HEAT-SHRINKABLE, 1.750 TO 1 SHRINK RATIO |
| MIL-A-85652 Base Document:1984 | AMPLIFIER-MIXER AM-7157/DKT-59 |
| MIL-P-83927 Revision B:1981 | Power Supplies, Guided Missile Launchers, Single Types PP-2401B/A PP-2401C/A PP-2401D/A, PP-4285/A, PP-4286/A, and Composite Type PP-4506/A and PS-1037 |
| MIL-S-83427 Base Document:1974 | SURVIVAL KIT CONTAINERS, CNU-129(V)/P AND CNU-130/P |
| MIL R 19648 : C | RELAY, TIME DELAY, THERMAL GENERAL SPECIFICATION FOR |
| MIL-B-1107 Revision G:1986 | BELT, INDIVIDUAL EQUIPMENT, M-1936 |
| MIL-A-85648 Base Document:1983 | Amplifier, Traveling Wave Tube |
| MIL-C-81790 Revision A:1990 | CONNECTORS, RECEPTACLE, EXTERNAL ELECTRIC POWER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL B 8075 : D | BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
| MIL-M-85831 Base Document:1989 | MASK, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE, NON-OXYGEN |
| MIL-B-42017 Base Document:1986 | BUR, BONE SURGERY (TUNGSTEN CARBIDE), GENERAL REQUIREMENTS FOR |
| MIL-C-38373 Revision B:1975 | CAP, FLUID TANK FILLER |
| SAE AMS 3593 : 2017 | TUBING, PLASTIC, ELECTRICAL INSULATION, IRRADIATED POLYVINYLIDENE FLUORIDE, SEMI-RIGID, HEAT-SHRINKABLE, MARKER SLEEVING GRADE, LOW OUTGASSING |
| MIL I 5356 : A | INDICATOR AIRSPEED, PITOT STATIC TYPE L 7 |
| SAE ARP 899 : 2013 | TUBE FITTINGS, FLUID SYSTEMS, PERMANENT TYPE, GENERAL REQUIREMENTS FOR |
| SAE AMS 1775 : 2015 | FABRIC, NYLON UPHOLSTERY, FIRE RETARDANT |
| SAE AMS 3894 : 2016 | Carbon Fiber Tape and Sheet Epoxy Resin Impregnated |
| SAE AMS 7440 : 2016 | BALLS, STEEL, LOW-CHROMIUM, HIGH CARBON HARDENED AND TEMPERED |
| SAE AMS 4824 : 2015 | BEARINGS, BABBITT-COATED LEADED-BRONZE STEEL BACK |
| MIL-L-9131 Revision H:1983 | LIFE RAFTS, INFLATABLE, TWENTY MAN |
| SAE AMS 3903 : 2013 | CLOTH, ORGANIC FIBER (PARA-ARAMID), HIGH MODULUS, EPOXY RESIN IMPREGNATED |
| MIL-T-17286 Revision D:1989 | TURBINES AND GEARS, SHIPBOARD PROPULSION AND AUXILIARY STEAM, PACKAGING OF |
| SAE AMS 5358 : 2017 | STEEL CASTINGS, INVESTMENT, CORROSION RESISTANT, 18CR - 9NI, SOLUTION HEAT TREATED |
| MIL-E-87236 Base Document:1985 | |
| MIL-I-5170 Revision C:1987 | INDICATOR, POSITION, HORIZONTAL STABILIZER |
| MIL-S-8812 Revision D:1975 | STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
| SAE AMS 3816 : 2016 | BRAID, FLAT, NYLON, ELECTRICAL TYING - WAX COATED |
| MIL-E-87235 Base Document:1985 | EMERGENCY ESCAPE, AIRCRAFT (REQUEST FOR ISSUE MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
| MIL-HDBK-772 Base Document:1981 | MILITARY PACKAGING ENGINEERING |
| MIL-S-8710 Revision B:1969 | STRAINER, AIRFRAME FUEL SYSTEM, GENERAL SPECIFICATION FOR |
| GGG-M-125-5 Revision B:1985 | RESPIRATOR ASSEMBLY: HALF MASK, AIR-PURIFYING PARTICULATE-FILTER (FOR DUSTS, FUMES, AND MISTS) |
| MIL-F-48863 Revision C:1985 | FUZE, GUIDED MISSILE, M934E6 PARTS ASSEMBLY, LOADING & PACKING FOR |
| MIL-P-82579 Base Document:1973 | POWER SUPPLY, MULTIVOLTAGE, DIRECT CURRENT (FOR TORPEDO TEST SET MARK 281 MOD 1) |
| MIL-T-81272 Base Document:1966 | THERMOCOUPLE, ENGINE, CYLINDER, BAYONET TYPE, MS90324 |
| MIL E 6058 : B NOTICE 1 | ENGINE, AIRCRAFT, RECIPROCATING, PREPARATION FOR SHIPMENT AND STORAGE OF |
| MIL-V-8610 Revision B:1984 | VALVE, FUEL SHUTOFF SOLENOID OPERATED, 28 VOLT, DC |
| MIL-I-25852 Revision B:1981 | INDICATOR, TEMPERATURE, THERMO COUPLE EHU-4/A |
| MIL-I-9343 Revision C:1985 | INDICATOR, TEMPERATURE, THERMOCOUPLE, ENGINE EXHAUST, TYPE MJ 1 |
| MIL V 8057 : F | VALVE, OXYGEN, PRESSURE BUILDUP AND VENT |
| MIL D 39030 : B | DUMMY LOAD, ELECTRICAL, COAXIAL AND STRIPLINE |
| MIL D 22612 : C | DETECTOR, CONTAMINATED FUEL |
| MIL-T-85703 Base Document:1984 | TOOL, POWER DRIVE TLU 437/E |
| MIL-C-85518 Base Document:1984 | COMPUTER SET, STANDARD AIRBORNE AN/AYK-14(V) GENERAL SPECIFICATION FOR |
| MIL-F-85596 Base Document:1983 | FIN, RETARDER, AIR INFLATABLE BSU-85/B |
| MIL E 24021 : J NOTICE 1 | ELECTRIC POWER MONITORS, EXTERNAL, AIRCRAFT |
| MIL-S-18471 Revision G:1983 | System, Aircrew Automated Escape, Ejection Seat Type, General Specification For |
| MIL-I-87216 Base Document:1984 | INSTRUMENT SYSTEMS, AIRBORNE REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT PATTERSON AFB OH 45433-6503 |
| MIL-T-7771 Revision B:1980 | TUBE, EXTENSION, GYRO STABILIZED DRIFT METER |
| MIL-I-81454 Base Document:1967 | INDICATOR, GYROSCOPE, VERTICAL REFERENCE ID-1481 (*)/A |
| MIL W 3459 : D | WIPER, WINDOW, ELECTRIC, PENDULUM TYPE (MARINE SERVICE, HEAVY DUTY) |
| MIL-M-21734 Revision C:1971 | MICROPHONE, DYNAMIC, OXYGEN MASK M-94B/A |
| MIL-I-26382 Revision C:1994 | INDICATOR SET, LIQUID OXYGEN QUANTITY A/A24J-4 AND A/A24J-8 |
| SAE AMS 3897 : 2016 | CLOTH, CARBON FIBER, RESIN IMPREGNATED |
| MIL H 8795 : D | HOSE ASSEMBLY, RUBBER HYDRAULIC, FUEL AND OIL RESISTANT |
| MIL-R-7705 Revision B:1975 | RADOME, GENERAL SPECIFICATION FOR |
| GG-R-1549 Revision A:1986 | |
| MIL-I-49466 Base Document:1990 | INSULATOR; DISKS, PLATES & WASHERS GENERAL SPECIFICATION FOR |
| MIL-P-70343 Base Document:1990 | PACKING, FIBERGLASS, ROPE & WICK |
| MIL-A-81852 Revision A:1986 | ALTIMETER-ENCODER AAU-32/A |
| MIL-I-22075 Revision C:1984 | Indicator, Bearing-Distance-Heading ID-663D/U |
| MIL-I-7063 Revision B:1979 | INDICATOR, POSITION, RUBBER TRIM TAB |
| MIL-B-23071:C | Blowers, Miniature, for Cooling Electronic Equipment General Specification for<br> |
| MIL-I-85832 Base Document:1989 | INTERCOM, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE SET |
| GG-R-1638 Revision A:1985 | REMOVAL, DENTAL CROWN (SIMPLEX) |
| MIL-R-47321 Base Document:1987 | REGULATOR, PRESSURE |
| MIL-M-4871 Revision C:1984 | MAINTENANCE PLATFORM |
| MIL-R-38162 Revision B:1971 | RADIOSONDE SET AN/AMT 13 |
| SAE AMS 5363 : 2017 | STEEL CASTINGS, SAND AND CENTRIFUGAL, CORROSION AND HEAT RESISTANT, 18.5CR - 10.5NI - 0.90 (CB+TA), SOLUTION HEAT TREATED |
| 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 C 5033 : C | CLOCK, AIRCRAFT, CIVIL DATE 24 HOUR DIAL 2 3/4 IN DIAMETER |
| MIL-H-85042 Revision A:1983 | HOOKS, BOMB RACK, GENERAL SPECIFICATION FOR |
| MIL-V-85033 Revision A:1981 | Valve, Charging |
| MIL S 55041 : C | SWITCH, WAVEGUIDE GENERAL SPECIFICATION FOR |
| MIL-C-85642 Base Document:1985 | COMMUNICATIONS CENTRAL AN/ASC-26 |
| MIL-C-83864 Revision A:1982 | CONTAINER, INNER, SURVIVAL KIT |
| MIL-B-12841 Revision B:1970 | BASIC ISSUE ITEMS FOR MILITARY VEHICLES, CARRIAGES AND EQUIPMENT; PREPARATION FOR SHIPMENT AND STORAGE |
| MIL-T-27200 Revision C:1975 | TRANSMITTER, RATE GYROSCOPE TRU-2A/A |
| MIL-G-85468 Base Document:1981 | GENERATOR CONTROL INDICATOR SG-118/AST-4(V) |
| MIL-I-5721 Revision C:1970 | INDICATOR, INDICATED AIRSPEED 20-250 KNOTS |
| MIL I 9304 : B | INDICATOR, RATE OF FLOW, FUEL, SYNCHRO STYLE 0-12,000 PPH TYPE MA 6 |
| SAE AMS 3870 : 2016 | CERAMIC MOLDINGS AND EXTRUSIONS, DENSE, ULTRA-HIGH ALUMINA (99% AL[2]O[3]) |
| SAE AMS 7304 : 2015 | SPRINGS, STEEL, 0.85 - 1.05C, HARDENED AND TEMPERED AFTER FORMING |
| MIL-F-63412 Base Document:1981 | FUZE PROBE ASSEMBLY, PNEUMATIC ASSEMBLING & PACKING (TOW) |
| SAE AMS 2535 : 2015 | COATING, VAPOR DEPOSITED POLY-MONOCHLORO-PARA-XYLYLENE FOR MICROCIRCUITS |
| SAE AMS 3843 : 2014 | POLYTETRAFLUOROETHYLENE SHEET, ASBESTOS FIBER REINFORCED, HIGH COMPRESSIBILITY, LOW DENSITY |
| SAE AMS 3834 : 2016 | CLOTH, TYPE 'E' GLASS, 'B' STAGE POLYESTER-RESIN-IMPREGNATED, 7781 STYLE FABRIC, FLAME RESISTANT, IMPROVED STRENGTH |
| SAE AMS 3632 : 2011 | TUBING, PLASTIC, ELECTRICAL INSULATION, IRRADIATED POLYVINYLIDENE FLUORIDE, SEMI-RIGID, HEAT-SHRINKABLE, 2 TO 1 SHRINK RATIO |
| SAE AMS 5330 : 2015 | STEEL CASTINGS, INVESTMENT, 0.80CR - 1.8NI - 0.35MO (0.38 - 0.46C) (SAE 4340 MODIFIED), ANNEALED |
| SAE AMS 1725 : 1986 | SKIN PROTECTIVE COMPOUND, CHEMICAL BARRIER |
| SAE AMS 5409 : 1984 | ALLOY CASTING, INVESTMENT, CORROSION AND HEAT RESISTANT 61NI - 16CR - 8.5CO - 1.8MO - 2.6W - 0.8CB - 3.4TI - 1.8TA - 3.4A1- 0.010B - 0.06ZR (0.03 - 0.08C), VACUUM MELTED, VACUUM CAST, AS CAST |
| SAE AMS 2510 : 2017 | ENGINE GRAY FINISHING LOW BAKING |
| SAE AMS 3020 : 2013 | OIL, REFERENCE, FOR 'L' STOCK RUBBER TESTING |
| SAE AMS 5315 : 2017 | DUCTILE (NODULAR) IRON CASTINGS, SAND, 60,000 PSI (415 MPA) TENSILE STRENGTH, FERRITIZE ANNEALED |
| SAE AMS 7312 : 1983(S2016) | PISTON RINGS, CENTRIFUGALLY-CAST IRON |
| SAE AMS 1548 : 2017 | CLEANER, TURBINE ENGINE GAS PATH, SOLVENT EMULSION TYPE |
| SAE AS 1297 : 2008(S2014) | REDUCERS, PNEUMATIC PRESSURE, MISSILE |
| SAE AMS 5395 : 2018 | ALLOY IRON CASTINGS, DUCTILE, SAND, CORROSION RESISTANT, 22NI (2.5 - 3.0C), AS CAST |
| SAE AMS 3804 : 2016 | CLOTH, AIRPLANE, COTTON, MERCERIZED, 65 POUNDS (290 N) BREAKING STRENGTH |
| SAE AMS 3582 : 2017 | PLASTIC TUBING, ELECTRICAL INSULATION - CROSSLINKED POLYVINYL CHLORIDE, FLEXIBLE, HEAT SHRINKABLE, 2 TO 1 SHRINK RATIO |
| SAE ARP 618 : 2013 | BOSS FITTINGS, METAL SEAL, FLUID SYSTEMS: GENERAL REQUIREMENTS FOR |
| SAE AMS 3689 : 2014 | ADHESIVE, FOAMING, HONEYCOMB, CORE SPLICE, STRUCTURAL, -54 TO +177 DEGREES C (-65 TO +350 DEGREES F) |
| SAE AMS 2421 : 1979 | PLATING MAGNESIUM FOR SOLDERABILITY - ZINC IMMERSION PROCESS |
| SAE AMS 3821 : 2015 | CLOTH, TYPE 'E' GLASS, 'B' STAGE EPOXY-RESIN-IMPREGNATED 7781 STYLE FABRIC, FLAME RESISTANT |
| 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-G-81665 Base Document:1971 | GENERATOR TRANSMITTER GROUP AN/ASA-76 (U) |
| 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-B-37036 Revision A:1985 | BUR, DENTAL, FINISHING (TUNGSTEN CARBIDE) |
| SAE AMS 5389 : 1987(R2017) | ALLOY CASTINGS, SAND, CORROSION AND HEAT RESISTANT, 55NI - 16.5CR - 17MO - 4.5W - 5.8FE - 0.40V, SOLUTION HEAT TREATED |
| MIL-H-36364 Revision B:1990 | HOLDER, RADIAC DETECTING ELEMENT, FILM BADGE TYPE |
| MIL-C-6720 Revision C:1964 | CLOCK, AIRCRAFT, ELAPSED TIME, CIVIL DATE 24 HOUR 2 3/4 INCH DIAL |
| MIL G 8360 : A | GAGE, PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE, 10-75 IN MERCURY TYPE MB 1 |
| MIL-B-28599 Revision C:1988 | BAG, LINEMAN'S GLOVE |
| MIL-C-82576 Base Document:1973 | CABLE ASSEMBLY, TEST (FOR TORPEDO TEST SET MARK 281 MOD 1) |
| MIL-C-1258 Revision D:1983 | CUP, OIL, LUBRICATING AND OILERS, SELF-FEEDING |
| MIL T 6349 : C NOTICE 1 | TEST SET, SYNCHRO |
| MIL F 15733 : G | FILTERS & CAPACITORS, RADIO FREQUENCY INTERFERENCE |
| MIL-R-28894 Base Document:1986 | RELAY, HYBRID OR SOLID STATE, SENSORS, ESTABLISHED RELIABILITY GENERAL SPECIFICATION FOR |
| MIL-I-12718 Revision F:1985 | INSIGNIA, DISTINGUISHING, ARMY AND AIR FORCE, WOVEN |
| MIL-I-81508 Base Document:1966 | INDICATOR PLUG, FOR MISSILE PROPELLANTS |
| DOD-I-85390 Base Document:1980 | INDICATOR, TIME TEMPERATURE, CARD, CHEMICALLY ACTIVATED, METRIC |
| MIL-F-8905 Revision B:1967 | FITTINGS AND CARGO RINGS, TIEDOWN, AIRCRAFT FLOOR |
| MIL-A-5034 Revision B:1979 | ADAPTER, BOMB RACK, 30-INCH, AERO 1A |
| MIL M 7793 : F | METER, TIME TOTALIZING |
| MIL-C-49468 Base Document:1990 | CRYSTAL UNITS, QUARTZ, PRECISION, GENERAL SPECIFICATION FOR |
| MIL-A-25915 Revision A:1980 | ACCELEROMETER, AIRCRAFT, PILOTS WARNING, TYPE MA-2 |
| GG-T-585 Revision B:1986 | TONOMETER, OPHTHALMIC, SCHIOTZ |
| GG-T-621 Revision C:1985 | TRANSIT, ONE-MINUTE; AND TRANSIT TRIPODS |
| MIL-I-85352 Base Document:1980 | INFLATOR ASSEMBLY AND GAGE ELEMENTS, PNEUMATIC PRESSURE REMOTE CONTROL, DIRECT READING |
| MIL-C-81991 Base Document:1975 | CONVERTER, AIRCRAFT DC TO DC, BOOST GENERAL SPECIFICATION FOR |
| MIL-STD-1475 Base Document:1974 | CONTAMINATION CONTROL TECHNOLOGY PACKAGING PROTECTION OF PRECISION CLEANED MATERIAL |
| MIL-A-83462 Base Document:1975 | ARCTIC CUSHIONS - CLOTHING, CHU-10/P AND CHU-11/P |
| MIL-C-26485 Revision D:1968 | CONTROL ASSEMBLY, ATTITUDE, GYROSCOPIC AF/A24G-1A |
| MIL-R-23761 Revision B:1975 | Regulators, Voltage, and Control Panels Aircraft, Direct Current Generator, General Specification for |
| MIL-I-22126 Revision B:1972 | INDICATOR, TORQUEMETER, ENGINE, TURBOPROP |
| MIL-T-85026 Revision D:1988 | TEST SET AN/ASM-475 FOR THE AN/ASX-2 RECOGNITION SET |
| MIL I 83452 : LATEST | INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
| MIL C 25478 : B | COOLER, LUBRICATING OIL, AIRCRAFT ENGINE, SYNTHETIC OIL, GENERAL SPECIFICATION FOR |
| MIL-M-28519 Revision A:1984 | METER, VOLUMETRIC, POSITIVE DISPLACEMENT, LIQUID, AIRCRAFT FUEL, 6OO GPM |
| MIL A 25088 : C | |
| MIL-R-83520 Base Document:1983 | RELAYS, ELECTROMECHANICAL, GENERAL PURPOSE, NON-HERMETICALLY SEALED, PLASTIC ENCLOSURE (UST COVER) |
| MIL-B-36162 Revision C:1987 | BLADES, LARYNGOSCOPE, MILLER |
| MIL I 83287 : E | INDICATOR, FAULT LOCATING GENERAL SPECIFICATION FOR |
| MIL-A-18218 Revision B:1984 | ANALYZERS, FLUE-GAS, ORSAT-TYPE, PORTABLE |
| MIL-S-26716 Revision A:1982 | STAND, TEST, AIRCRAFT HYDRAULIC SYSTEMS, NON-PORTABLE |
| 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-G-7734 Revision C:1981 | GAGE, PRESSURE ENGINE AND UTILITY AIRCRAFT |
| MIL O 38338 : C (1) | OIL QUANTITY GAGING SYSTEM, CONTINUOUS TRANSISTORIZED NUCLEONIC, GENERAL SPECIFICATION FOR |
| MIL S 24251 : B | SHIELD, RETAINER (BASES), AND ADAPTERS, ELECTRON TUBE, HEAT DISSIPATING, GENERAL SPECIFICATION FOR |
| MIL-H-27269 Revision A:1977 | HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
| SAE AMS 3802 : 2016 | CLOTH, AIRPLANE, COTTON, MERCERIZED, 50 POUNDS (220 N) BREAKING STRENGTH |
| MIL C 38618 : A | COUPLER, DRIVE ASSEMBLY GOVERNOR, FUZE BOMB MAU 87A 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 I 8136 : A | INDICATOR, FUEL FLOW RATE, SYNCHRO STYLE, SINGLE CLAMP MOUNTED 2 INCH SIZE 300 TO 3,000 PPH TYPE A 12 |
| MIL-C-7488 Revision A:1974 | COOLERS, OIL, PLATE, AIRCRAFT |
| SAE AMS 3818 :1993(S2016) | BRAID, FLAT, POLYESTER, LACING AND TYING, SYNTHETIC RUBBER COATED, LOW OUTGASSING |
| MIL-I-27665 Revision B:1984 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE ABU-1O/A, -50 DEGREES TO +50 DEGREES C |
| GGG-M-125-6 Revision B:1985 | RESPIRATOR ASSEMBLY: HALF MASK, AIR-PURIFYING, COMBINATION CHEMICAL CARTRIDGE AND FILTER (FOR PAINT SPRAY AND ORGANIC VAPORS) |
| MIL-I-27203 Revision B:1987 | Indicator, Position, Wing Flap |
| MIL-E-85583 Revision A:1987 | ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-P-85034 Base Document:1976 | POWER PACKAGE, EMERGENCY AC/DC GENERATOR, RAM AIR TURBINE DRIVEN |
| MIL O 55310 : C | OSCILLATOR, CRYSTAL, GENERAL SPECIFICATION FOR |
| GGG-M-125-9 Revision A:1982 | RESPIRATOR ASSEMBLIES, AIR LINE, HOOD AND HELMET (FOR ABRASIVE BLASTING OPERATIONS) |
| MIL V 9050 : E (1) | VALVE, OXYGEN, PRESSURE RELIEF, AIRCRAFT |
| SAE AMS 1450 : 1998 | DISINFECTANT (INSECTICIDE), AIRCRAFT |
| SAE AMS 5375 : 1982 | ALLOY CASTINGS, INVESTMENT, CORROSION AND HEAT RESISTANT 65.5CO - 25CR - 1.8NI - 5.0W AS CAST |
| SAE AMS 5351 : 2017 | STEEL CASTINGS, SAND, CORROSION AND MODERATE HEAT RESISTANT, 13CR, NORMALIZED AND TEMPERED |
| MIL-S-48405 Base Document:1973 | Shielded and Confined Mild Detonating Cord Assemblies |
| SAE AMS 5348 : 2017 | STEEL CASTINGS, TUBULAR, CENTRIFUGAL, CORROSION RESISTANT, 15CR - 4.6NI - 0.22 (CB+TA) - 2.8CU, SOLUTION HEAT TREATED |
| MIL H 7061 : B | HOSE, RUBBER, AIRCRAFT, SELF SEALING, AROMATIC FUEL |
| MIL L 51167 : A | LABORATORY, CHEMICAL, BASE, M2A1 |
| MIL C 25369 : C | CYLINDER, CARBON DIOXIDE, FOR INFLATION OF PNEUMATIC LIFE PRESERVERS |
| MIL-M-55565 Revision C:1988 | MICROCIRCUITS, PACKAGING OF |
| MIL-A-27198 Revision B:1987 | ALTIMETER, PRESSURE AAU-7/A |
| MIL-C-9075 Revision A:1968 | COMPUTER AND TRANSMITTER, TRUE AIRSPEED, PITOT STATIC, 150-900 KNOTS, TYPE MA 1 |
| MIL-I-27247 Revision C:1985 | INDICATOR, TEMPERATURE, SYNCHRO |
| MIL B 83054 : B | BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK |
| MIL A 3933 : E | ATTENUATORS, FIXED GENERAL SPECIFICATION FOR |
| SAE AMS 2550 : 2017 | TREATMENT OF SHEET METAL PARTS, CORROSION-RESISTANT STEEL |
| MIL-A-23899 Revision B:1984 | AURAL PROTECTOR, SOUND |
| MIL-V-23255 Revision B:1976 | VALVE, PRESSURE RELIEF |
| MIL-I-8404 Revision A:1953 | INDICATOR, PRESSURE, SINGLE 0 TO 35 PSI FUEL PRESSURE TYPE C 33 |
| 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-I-82577 Base Document:1973 | INDICATOR, DIGITAL (FOR TORPEDO TEST SET MARK 281 MOD 1) |
| MIL-N-81207 Revision A:1973 | Navigational Set, TACAN AN/ARN-84 (V) |
| MIL-A-27261 Revision A:1966 | ACCELEROMETER, AIRCRAFT |
| MIL-STD-758 Revision C:1990 | PACKAGING PROCEDURES FOR SUBMARINE REPAIR PARTS |
| MIL-I-81400 Base Document:1966 | INSTRUMENT, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-22424 Revision A:1967 | ADAPTERS, COMPENSATING, MS281O7, MA-1 COMPASS SYSTEM |
| SAE AIR 4728 : 2013 | REFERENCES, SPACECRAFT AND SPACECRAFT SERVICING, FLUID SYSTEM COMPONENTS (ABBREVIATIONS, ACRONYMS, DEFINITIONS, APPLICABLE DOCUMENTS AND ENVIRONMENTAL CONDITIONS) |
| SAE AMS 5373 : 2017 | ALLOY CASTINGS, SAND, CORROSION AND HEAT RESISTANT, 16CO - 29CR - 4.5W, AS CAST, UNS R30006 |
| SAE AMS 4176 : 2001 | HONEYCOMB CORE - FOR SANDWICH CONSTRUCTION 5056, 350-DEG F (175-DEG C) |
| SAE AMS 7878 : 1987 | TUNGSTEN CARBIDE POWDER, COBALT COATED |
| SAE AMS 7464 : 2017 | BOLTS AND SCREWS, STEEL, LOW-ALLOY HEAT RESISTANT, 222,000 PSI (1517 MPA) TENSILE STRENGTH, HARDENED AND TEMPERED, ROLL THREADED |
| SAE AMS 3815 : 2016 | BRAID, FLAT, NYLON, ELECTRICAL TYING SYNTHETIC RUBBER COATED |
| SAE AMS 2690 : 2017 | PARALLEL GAP, WELDING, MICROELECTRONIC INTERCONNECTIONS TO THIN FILM SUBSTRATES |
| SAE AMS5341:2012(S2017) | STEEL CASTINGS, INVESTMENT, CORROSION RESISTANT, 19.5CR - 10.5NI - 0.25S (TYPE 303), SOLUTION HEAT TREATED |
| SAE AMS 7466 : 1993 | BOLTS AND SCREWS - NICKEL ALLOY, CORROSION AND HEAT RESISTANT, UPSET HEADED, ROLL THREADED, FATIGUE RESISTANT |
| SAE AMS 3688 : 2014 | ADHESIVE, FOAMING, HONEYCOMB CORE SPLICE, STRUCTURAL, -55 DEGREES C TO +82 DEGREES C (-65 DEGREES F TO +180 DEGREES F) |
| SAE AMS 2399 : 2011 | ELECTROLESS NICKEL-BORON PLATING |
| SAE AMS 3813 : 2016 | ROPE, ARAMID FIBER, JACKETED FOR ANTENNA-SUPPORT SYSTEMS |
| MIL-R-81498 Revision C:1979 | RECEIVING-DECODING GROUP AN/ARA-63 |
| MIL-T-81187 Base Document:1966 | Transmitter, Rate of Fuel Flow, Synchro Type MS90361 |
| MIL-G-23083 Revision C:1972 | Gyroscope, Rate Switching MS 17399 |
| MIL-STD-1367 Revision A:1989 | PACKAGING, HANDLING, STORAGE, AND TRANSPORTABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS) |
| 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] |
| MIL-I-85112 Base Document:1978 | INDICATOR SET, VERTICAL SCALE |
| MIL-T-27-233 Base Document:1978 | TRANSFORMERS AND INDUCTORS (AUDIO POWER AND HIGH POWER PULSE) INDUCTOR CHARGING TF5S37ZZ |
| MIL-I-25130 Revision B:1974 | INDICATOR, PRESSURE, OIL, 0-300PSI, TYPE MO-1 |
| MIL T 21038 : D | TRANSFORMERS, PULSE, LOW POWER, GENERAL SPECIFICATION FOR |
| MIL C 55330 : B | CONNECTORS, PREPARATION FOR DELIVERY OF |
| MIL-A-26360 Revision B:1982 | AMPLIFIER, ELECTRONIC CONTROL ASU-3/A |
| MIL-A-27330 Revision B:1987 | ACCELEROMETER, ELECTRICAL, LINEAR TRU-3/A |
| MIL-B-23459 Revision D:1988 | BUOY, HOSE SUPPORT, INFLATABLE |
| MIL V 9439 : D | VALVE, OXYGEN, CYLINDER, HIGH PRESSURE |
| SAE AMS 4805 : 2012(S2018) | BEARINGS, SINTERED METAL POWDER, 89CU - 10SN, OIL IMPREGNATED |
| MIL-W-6940 Revision D:1985 | WIRE STRAND, STEEL, NONFLEXIBLE (PREFORMED) |
| 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 T 83174 : B (3) | TRANSMITTER, ACCELEROMETER, AXIAL |
| MIL-S-7470 Revision A:1975 | SHAFT, POWER TRANSMISSION, AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR |
| MIL-T-81838 Base Document:1971 | Tank, Fuel, Aircraft, Auxiliary External 300 Gallon, Type AERO-1D |
| SAE AMS 2689 : 2016 | FUSION WELDING TITANIUM AND TITANIUM ALLOYS |
| SAE AMS 3732 : 2015 | POTTING COMPOUND, EPOXY ONE PART, FILLED, HEAT CURE, LOW CTE |
| SAE AMS 3912 : 2014 | RADOMES, FOAM SANDWICH, POLYIMIDE/QUARTZ CLOTH CONSTRUCTION |
| MIL-I-25482 Revision D:1993 | INDICATOR, ENGINE TESTING |
| MIL-A-85505 Base Document:1983 | ALTIMETER, STANDBY, TYPES 1 AND 2 |
| MIL-H-58108 Base Document:1986 | HEADSET-MICROPHONE KIT MK-2193/AIC |
| MIL-I-7112 Revision B:1985 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, CYLINDER HEAD 0 DEGREES C TO 300 DEGREES C |
| MIL-M-29417 Base Document:1984 | MODULE, FUEL PUMP [SIXCON] |
| MIL-N-25161 Revision C:1969 | NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
| MIL-G-26988 Revision C:1971 | GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
| MIL-A-81605 Revision D:1984 | ALTIMETER SET, ELECTRONIC AN/APN-194(V) |
| MIL-I-83245 Revision A:1994 | INDICATOR SET, OIL PRESSURE A/A24J-17 |
| SAE AMS 3579 : 2017 | PLASTIC TUBING, ELECTRICAL INSULATION, NON-CROSSLINKED POLYVINYL CHLORIDE, FLEXIBLE, HEAT SHRINKABLE, 1.6 TO 1 SHRINK RATIO |
| MIL-I-27680 Revision C:1973 | INDICATOR, ATTITUDE, ARU-12/A, REMOTE |
| SAE AS 85075 : 2000 | TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR |
| SAE AMS 5115 : 2017 | Wire, Carbon Steel 0.60 - 0.75C Hardened and Tempered |
| SAE AMS 3684 : 2016 | RESIN, POLYIMIDE, SEALING HIGH-TEMPERATURE RESISTANT, 315 DEGREES C (600 DEGREES F) UNFILLED |
| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF |
| MIL-A-29505 Base Document:1966 | Antenna Group, Tacan, OE-273(V)/Urn |
| MIL-P-85585 Base Document:1982 | Probes, Eddy Current, Unshielded, Single Coil, Absolute |
| MIL T 25502 : C | TRUE HEADING COMPUTER GROUP AN/AJA-I |
| MIL W 3970 : C | WAVEGUIDE ASSEMBLIES, RIGID, GENERAL SPECIFICATION FOR |
| MIL-W-45562 Revision C:1992 | WELDING AND SOLDERING EQUIPMENT, SUPPLIES AND ACCESSORIES, PACKAGING OF |
| MIL-I-81453 Revision A:1977 | INTERROGATOR SET AN APX 76B(V) |
| MIL-I-27623 Revision C:1972 | INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
| MIL-T-85678 Base Document:1974 | TRANSPONDER, RADAR TRACKING |
| MIL-I-25950 Revision B:1967 | INDICATOR, PRESSURE, OIL, 0-100 PSI |
| MIL-I-7087 Revision A:1968 | INDICATOR, PRESSURE OIL, 0-200 PSI |
| MIL-A-81296 Revision D:1985 | ALTIMETER SET, ELECTRONIC AN/APN-171(V) |
| MIL-I-83117 Revision B:1975 | INDICATOR, ANGLE OF ATTACK |
| MIL-H-21594 Revision C:1986 | Hookpoint, Aircraft Arresting |
| MIL-T-25485 Revision C:1974 | TRANSMITTER, THRUST, SINGLE SYNCHRO STYLE, PRESSURE RATIO, TYPE MK-2 |
| GG-E-916 Revision F:1987 | EXPLORERS, DENTAL; EXPLORER-PROBE, DENTAL |
| MIL-C-26237 Revision C:1983 | CRADLE, AIRCRAFT-MISSILE COMPONENTS MMU-1/E |
| MIL L 12606 : D | LOUDSPEAKER, PERMANENT MAGNET (UNENCASED, 3 INCH AND 4 INCH DIAMETER CONE, 2 WATT, FUNGUS, GUNBLAST, AND IMMERSION RESISTANT), TYPE LL-445/U, M12606-01, AND M12606-02 |
| MIL-B-42027 Base Document:1986 | BROACH, PULP CANAL, BARBED, STERILE |
| MIL-C-87970 Base Document:1982 | CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
| MIL L 10911 : D | LOUDSPEAKER, PERMANENT MAGNET (UNENCASED, 2.5-, 3-, 4-, 5-, 6-, 8-, 10-, AND 12-, INCH DIAMETER CONE) |
| MIL-S-81977 Base Document:1974 | Simulater, Radar Signal SM-697/UPQ-5 |
| 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-B-4330 Revision C:1984 | BOOT, EXTREME COLD WEATHER |
| GG-B-101 Revision G:1986 | BANDAGE, CAST, PLASTER OF PARIS IMPREGNATED (HARD COATED) |
| 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-C-87975 Base Document:1985 | CLOCK, AIRCRAFT, MECHANICAL ABU-32/A |
| GG-F-599 Revision B:1988 | FORCEPS, DRESSING, DENTAL |
| MIL-E-22437 Revision E:1981 | EQUIPMENT, DEGAUSSING FOR MCM SHIPS |
| MIL-A-25175 Revision C:1976 | AIR TRANSPORT, NONTACTICAL, PACKING FOR |
| MIL-I-27619 Revision G:1974 | INDICATORS, ATTITUDE DIRECTOR |
| MIL H 87961 : NOTICE 2 | HOSE AND HOSE ASSEMBLIES, AIR DUCT, AIR BREATHING, OXYGEN SYSTEM GENERAL SPECIFICATION FOR |
| MIL-B-4792 Revision E:1994 | BUMPER, RUBBER, DUPLEX ROUND |
| MIL I 27851 : B | INDICATOR, INDICATED AIRSPEED AVU-17/A |
| MIL-C-38418 Revision E:1981 | Control Assembly, Gyroscope, Attitude A/A24G-39 |
| MIL-T-8249 Revision B:1979 | TRANSMITTER, RATE OF FLOW, FUEL, TYPE MB-2 |
| MIL-I-8974 Revision A:1981 | INDICATOR, EVENT COUNTING, GENERAL SPECIFICATION FOR |
| MIL-A-28624 Revision B:1984 | AUGER, EARTH, PORTABLE; HAND-HELD, TWO-MAN, GASOLINE-ENGINE DRIVEN |
| GG-R-1472 Revision B:1987 | RETAINER, MATRIX, DENTAL (TOFFLEMIRE) |
| MIL T 26898 : B | TEST SET, AIRFIELD LIGHTING SYSTEMS, TYPE MM-1 |
| AA-S-130 Revision B:1991 | SCREENS, BEDSIDE, ALUMINUM |
| MIL-B-27044 Revision C:1968 | BOMB, PRACTICE BDU-12/B |
| MIL-C-22585 Revision A:1984 | COMPUTER, PRESSURE REDUCTION, METEOROLOGICAL CP-402/UM() |
| MIL-P-85511 Revision A:1987 | PANEL ASSEMBLY, TARGET, BANNER, AERIAL TDU-32 SERIES |
| MIL B 38634 : LATEST | BOMB, FIRE, BLU 32A B |
| SAE AMS 3823 : 2015 | CLOTH, GLASS, STYLE 7781, CHROME-SILANE FINISH |
| MIL-V-85830 Base Document:1989 | VENTILATOR, TACTICAL, HELICOPTER AIRCREWMEN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE |
| MIL C 25666 : E (1) | CONVERTER, LIQUID OXYGEN, CAPACITANCE TYPE GAGING, GENERAL SPECIFICATION FOR |
| DOD-C-85050 Base Document:1982 | CHARGERS, BATTERY, NICKEL-CADMIUM, AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE MA 1568 : 2018 | NUT, SELF LOCKING - UNS S66286, 425 DEGREE C AND 650 DEGREE C, 1100 MPA, MJ THREAD, PROCUREMENT SPECIFICATION FOR, METRIC |
| MIL-C-81883 Base Document:1976 | CONTROL GROUP, ELECTRIC POWER OK-XXX (V) A GENERAL SPECIFICATION FOR |
| MIL-I-7802 Revision A:1967 | INDICATOR, MS 28088, TURN AND SLIP [THREE PHASE] |
| MIL-I-23832 Revision A:1980 | Indicator, Tachometer, Triple Pointer, Helicopter |
| MIL-D-38134 Revision A:1971 | DETECTOR, MAGNETIC AZIMUTH DSU-4/A, HIGH TEMPERATURE |
| MIL-I-81049 Revision A:1972 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
| GG-C-1320 Revision B:1985 | CUP, POLISHING, DENTAL HANDPIECE (SCREW STEM) |
| MIL-T-5420 Revision B:1970 | TUBE, PITOT STATIC, ELECTRICALLY HEATED, AIRCRAFT |
| MIL-R-17772 Revision C:1982 | RADIATOR, HEATING, BASEBOARD PANEL, STEAM AND HOT WATER |
| GG-B-140 Revision D:1986 | BATH, WATER, DENTAL IMPRESSION COMPOUND |
| GG-C-1282 Revision C:1985 | CURETTES, ALVEOLAR (MOLT AND MILLER) |
| MIL-P-87133 Base Document:1978 | PLOTTER, COMBAT MISSION PLU-6/C (AIR NAVIGATION) |
| MIL-I-42044 Revision A:1991 | SEXUAL ASSAULT DETERMINATION KIT |
| MIL-T-4638 Revision B:1985 | TESTERS, MATERIAL HARDNESS (ROCKWELL TYPE) |
| MIL I 83361 : (4) | INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
| MIL-P-38136 Revision A:1969 | PITOT STATIC TUBE COMPENSATED TRU 62/A |
| MIL M 5388 : B | MACHMETER; PITOT STATIC OPERATED, RANGE 0.5 TO 1.5, TYPE A-2B |
| MIL R 85725 : 0 | RACK, INTEGRATED AVIONICS, FORCED AIR COOLED, GENERAL SPECIFICATION FOR |
| MIL-L-5567 Revision F:1983 | LIFE RAFTS, INFLATABLE 4 AND 7 MAN FOR AIRCRAFT USE |
| GGG-M-125-10 Revision A:1982 | RESPIRATOR ASSEMBLY: HELMET WITH POWERED AIR-PURIFYING UNIT |
| GGG-M-125-8 Revision B:1985 | RESPIRATOR ASSEMBLY: HALF MASK, AIR-PURIFYING PARTICULATE-FILTER (FOR DUSTS AND MISTS) |
| MIL-G-8170 Revision D:1987 | GAGE, OIL PRESSURE, DIRECT INDICATING, SINGLE CLAMP MOUNTED 0 -200 PSI 320 DEGREE SCALE 2 INCH SIZE, TYPE AGU 12/A AND AGU 13/A |
| MIL-STD-834 Revision C:1974 | PACKAGING DATA FORMS, INSTRUCTIONS FOR PREPARATION AND USE OF |
| MIL-A-85434 Revision A:1983 | AMPLIFIER, TRAVELING WAVE TUBE AM-6937/DLQ-3B |
| MIL T 25627 : C | TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |
| MIL-E-82578 Base Document:1973 | ENCODER, SHAFT ANGLE POSITION, CYCLIC DECIMAL CODED (FOR TORPEDO TEST SET MARK 281 MOD 1) |
| MIL H 83776 : A | HELMET, FLYER'S, WINTER |
| SAE AMS 7311 : 2017 | PISTON RINGS, CENTRIFUGALLY-CASE ALLOYED IRON, 0.50MO - 0.50CU |
| SAE AMS 3081 : 1978 | ANTI SCUFFING TREATMENT, GRAPHITE VARNISH |
| SAE AMS 1451 : 1998 | DISINFECTANT, AIRCRAFT FOR USE IN CARGO COMPARTMENTS |
| SAE AS 23899 : 2012 | AURAL PROTECTOR, SOUND |
| SAE AMS5328E:1987(S2017) | STEEL CASTINGS, INVESTMENT, 0.80CR - 1.8NI - 0.35MO (0.28 - 0.36C) (SAE 4330 MODIFIED), ANNEALED |
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