QQ-P-416 Revision F:1991
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
PLATING, CADMIUM (ELECTRODEPOSITED)
Available format(s)
PDF
Superseded date
28-03-2002
Publisher
Important note : All end users must be registered with an Account prior to user licenses being assigned.Requirements for electrodeposited cadmium plating of various degrees of thickness.
| Committee |
AREA MFFP
|
| DevelopmentNote |
F Notice 1 - Notice of Cancellation/Superseded by SAE AMS QQ P 416. (05/2002)
|
| DocumentType |
Standard
|
| Pages |
33
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| Standards | Relationship |
| SAE AMS 2400 : 2013 | Similar to |
| SAE AMS QQ P 416 : 2016 | Similar to |
| MIL-C-24938 Revision A:1993 | COATS, FIREMEN'S, STRUCTURAL/ALUMINIZED PROXIMITY |
| DOD-C-24529 Base Document:1976 | CHARGERS, BATTERY, LIFT TRUCK AND PALLET TRANSPORTER BATTERY SERVICE (METRIC) |
| SAE AS 8568 : 2012 | BINOCULARS, PRISMATIC, HAND-HELD (FOR AERONAUTICAL USE) (7 X 50 AND 6 X 42 (WIDE FIELD)) |
| MIL-C-53052 Base Document:1985 | Connector, Electrical, Power |
| MIL-S-26547 Revision C:1985 | STARTER-GENERATOR ENGINE STU-6A |
| MIL-H-7195 Revision G:1991 | HARDWARE, PARACHUTE, GENERAL SPECIFICATION FOR |
| MIL C 38240 : C | COMPUTER, ALTITUDE, ALTITUDE ENCODING CPU 66, GENERAL SPECIFICATION FOR AND MTU 39/A MOUNTING TRAY |
| MIL-I-8580 Revision B:1965 | INDICATOR, TACHOMETER, HELICOPTER, 0-4000 RPM TYPE MA 1 |
| MIL-S-23665 Revision B:1968 | SONOBUOY, DETECTION DEVICES, PRESERVATION, PACKAGING AND PACKING, PROCEDURES FOR |
| MIL-T-5842 Revision B:1985 | TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR |
| MIL-T-38034 Revision E:1970 | TIMER, FIRE CONTROL, BOMBING, DUAL |
| MIL-F-63428 Base Document:1981 | FEED ASSEMBLY, AMMO FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2 |
| MIL R 27426 : A | RING, RETAINING, SPIRAL (UNIFORM CROSS SECTION) |
| MIL C 27599 : B | CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT, ENVIRONMENTAL RESISTANT, SOLDER CONTACTS GENERAL SPECIFICATION FOR |
| GG-G-91 Revision D:1972 | GAGE, TIRE PRESSURE, SELF CONTAINED AND INFLATOR GAGE, PNEUMATIC TIRE |
| MIL-B-8914 Revision B:1966 | BEARING, ROLLER, SELF-ALIGNING, AIRFRAME, ANTIFRICTION |
| MIL T 5578 : C | TANK, FUEL, AIRCRAFT, SELF-SEALING |
| FF-R-556 Revision D:1981 | RIVET, SOLID, SMALL, RIVET, SPLIT, SMALL, RIVET TUBULAR SMALL, FLAT WASHER (BURR) AND CAP RIVET, GENERAL PURPOSE |
| MIL C 83513 : C | CONNECTORS, ELECTRICAL, RECTANGULAR, MICROMINIATURE, POLARIZED SHELL, GENERAL SPECIFICATION FOR |
| MIL-R-10761 Revision A:1962 | ROTARY CONVERTER (MOTOR GENERATOR) PU 134 ()/U, PU 140 ()/U, PU 141()/U & PU 143 ()/U |
| MIL-T-13420 Revision A:1959 | TELEPHONE SET TA 264() PT |
| MIL-I-7062 Revision C:1975 | INDICATOR, POSITION, CONTROL SURFACES, 28 VOLT DC, GENERAL SPECIFICATION FOR |
| MIL-C-19853 Revision D:1994 | CARBON REMOVING COMPOUND (FOR USE IN AGITATED TANK) |
| MIL C 53072 : B | CHEMICAL AGENT RESISTANT COATING (CARC) SYSTEM APPLICATION PROCEDURES AND QUALITY CONTROL INSPECTION |
| SAE AS 7997:1999 | MOTORS, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT - GENERAL SPECIFICATION FOR |
| MIL T 6396 : E | TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
| MIL-T-83460 Base Document:1975 | TRANSDUCER, MOTIONAL PICKUP TRU-164/A |
| MIL C 12520/9 : A | CONNECTORS, RECEPTACLE, ELECTRICAL WATERPROOF (SHELL SIZE 20, FEMALE INSERTS) |
| MIL I 7627 : F | INDICATOR, TURN AND SLIP 28V DC |
| MIL-I-83152 Revision B:1974 | INDICATOR, INDICATED-AIRSPEED AVU-22/A (INDICATOR-TRANSDUCER) |
| MIL-C-81703 Base Document:1971 | CONNECTOR, ELECTRIC, CIRCULAR, MINIATURE, RACK AND PANEL OR PUSH-PULL COUPLING, ENVIRONMENT RESISTING |
| MIL-S-29574 Base Document:1989 | SEALING COMPOUND, POLYTHIOETHER, FOR AIRCRAFT STRUCTURES, FUEL AND HIGH TEMPERATURE RESISTANT, FAST CURING AT AMBIENT AND LOW TEMPERATURE |
| MIL M 5794 : B | MICROPHONE, UNIT M 6A/UR AND MICROPHONE CARBON M 51/UR |
| MIL-R-10985 Revision A:1956 | REEL, AUTOMATIC TAKE-UP, EXTENSION CABLE, 24-VOLT, D.C |
| MIL-A-8243 Revision D:1985 | ANTI-ICING AND DEICING-DEFROSTING FLUIDS |
| MIL D 83320 : 0 | DETECTOR, MAGNETIC AZIMUTH DSU-14/A |
| MIL C 38214 : B | COMPASS, MAGNETIC,MOUNTED |
| MIL-I-983 Revision E:1966 | INTERIOR COMMUNICATION EQUIPMENT, NAVAL SHIPBOARD, BASIC DESIGN REQUIREMENTS FOR |
| MIL C 21097 : E | CONNECTORS, ELECTRICAL, PRINTED WIRING BOARD, GENERAL PURPOSE GENERAL SPECIFICATION FOR |
| MIL P 45952 : 0 | PIN,QUICK RELEASE, DETENT GENERAL SPECIFICATION FOR |
| MIL-C-27298 Revision B:1980 | CLOCK, AIRCRAFT, MECHANICAL ABU AND 9-A |
| MIL-T-38473 Revision A:1972 | TIMER, PRECISION, BOMBING, 0 - 30 MINUTES |
| MIL C 21567 : A | COMPOUND, SILICONE, SOFT FILM |
| MIL A 18357 : 0 | ANTENNA AT-145B/A |
| MIL H 52471 : D | HOSE AND HOSE ASSEMBLIES, RUBBER, HYDRAULIC PRESSURE TYPE, GENERAL SPECIFICATION FOR |
| SAE AIR 5479 : 2017 | ENVIRONMENTALLY COMPLIANT PROCESSES FOR LANDING GEAR |
| MIL-A-38140 Revision B:1977 | ALTIMETER, PRESSURE AAU-16/A |
| MIL C 27536 : B | COUPLING, CLAMP, GROOVED, V-BAND |
| MIL F 0051068 : E | FILTER, PARTICULATE, HIGH-EFFICIENCY, FIRE RESISTANT |
| MIL H 81014 : A NOTICE 1 | HOOK, HELICOPTER, EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C |
| MIL-STD-193 Revision L:1991 | PAINTING PROCEDURES AND MARKING FOR VEHICLES, CONSTRUCTION EQUIPMENT, MATERIAL HANDLING EQUIPMENT, AND SPARE PARTS |
| MIL-G-25597 Revision D:1973 | Gyroscope, Displacement, Roll and Pitch, Type MD-1 |
| MIL C 3607 : A | CONNECTOR, COAXIAL, RADIO FREQUENCY, SERIES PULSE GENERAL SPECIFICATION FOR |
| MIL-B-53102 Base Document:1990 | BERM LINER ASSEMBLIES, ARCTIC SERVICE |
| MIL-B-8568 Revision B:1967 | BINOCULAR, PRISMATIC, HAND-HELD [FOR AERONAUTICAL USE] 7 X 50 AND 6 X 42 WIDE FIELD [ASG] |
| MIL C 28840 : A | CONNECTOR ELECTRICAL, CIRCULAR THREADED, HIGH DENSITY, HIGH SHOCK SHIPBOARD, CLASS D - GENERAL SPECIFICATION FOR |
| FF-B-584 Revision F:1989 | BOLTS, FINNED NECK, KEY HEAD, MACHINE, RIBBED NECK, SQUARE NECK, TEE HEAD |
| MIL-C-10750 Revision J:1988 | COAT, FIREMEN'S |
| MIL-A-23595 Revision D:1995 | AMPLIFIER, AUDIO FREQUENCY |
| MIL-S-45933 Base Document:1971 | STUD, KEYRING LOCKED, 125 AND 160 KSI FTU, GENERAL SPECIFICATION FOR |
| GGG-W-686 Revision C:1969 | WRENCH TORQUE |
| MIL-C-7135 Revision F:1967 | Compressor, Pneumatic, 3,000 PSI -- 2 SCFM Aero 2A (*), Aero 2A-1 (*), Aero 2B (*), and Aero 2B-1 (*) |
| MIL-C-601 Revision G:1971 | CYLINDER, CARBON DIOXIDE FILLED, TECHNICAL |
| AA-O-00235 Base Document:1962 | OFFICE FURNITURE, STEEL, SECTIONAL |
| MIL-I-81186 Base Document:1966 | INDICATOR, RATE OF FUEL FLOW SYNCHRO TYPE, M590360 |
| MIL-S-6715 Base Document:1950 | SPRING, HELICAL, AIRCRAFT |
| MIL-M-7255 Revision B:1969 | MANOMETER, PRESSURE, DIFFERENTIAL AND ABSOLUTE TYPE E 1 |
| MIL B 5806 : F | BOX, SHIPPING, AND STORAGE, HELICOPTER BLADE |
| MIL-I-21206 Revision B:1960 | Indicator, Rate of Flow, Fuel; EFU-7/A (300-5000-15000 PPH) |
| MIL-I-27709 Revision A:1962 | INDICATOR, ATTITUDE ARU-14/A, REMOTE |
| MIL-G-7818 Base Document:1951 | GAGE, FUEL QUANTITY, CAPACITOR TYPE, COMPENSATED, 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 S 81733 : C | SEALING AND COATING COMPOUND CORROSION INHIBITIVE |
| TT-R-2918 Revision A:2001 | REMOVAL, PAINT, NO HAZARDOUS AIR POLLUTANTS (HAPS) |
| MIL-A-55503 Base Document:1966 | ATTITUDE HEADING REFERENCE SET AN/ASN-76 |
| MIL-C-8603 Revision B:1984 | CLAMPS, LOOP TYPE, AND STRAPS, SUPPORT |
| MIL T 8878 : D | TURNBUCKLE, POSITIVE SAFETYING |
| MIL-W-50258 Revision A:1971 | WARHEAD SECTION, 762MM ROCKET, PRACTICE: M38 METAL PARTS FOR |
| MIL C 21617 : 0 | CONNECTOR, PLUG AND RECEPTACLE ELECTRICAL RECTANGULAR, POLARIZED SHELL, MINIATURE TYPE |
| MIL R 007885 : C SUPP 1 | RIVETS; BLIND, STRUCTURAL, LOCKED AND FRICTION RETAINED SPINDLE, GENERAL SPECIFICATION FOR |
| MIL-P-43116 Revision A:1964 | PIKE,WIRE AND PIKES, POLE |
| DOD N 70329 : 0 | NUT, PLAIN, ROUND, BALL AND ROLLER BEARINGS, METRIC, GENERAL SPECIFICATION FOR |
| MIL B 5423 : C | BOOT, DUST AND WATER SEAL 1 [FOR TOGGLE AND PUSHBUTTON SWITCHES, CIRCUIT BREAKERS, AND ROTARY ACTUATED PARTS] GENERAL SPECIFICATION FOR |
| A-A-1037 Revision B:1990 | WIRE FABRIC (INDUSTRIAL) |
| MIL-C-23367 Base Document:1963 | Computer, Flight Director, Aircraft |
| MIL I 45932 : 0 | INSERT, SCREW THREAD, THIN WALL, LOCK IN |
| SAE AS 13572 : 2014 | SPRINGS, HELICAL, COMPRESSION AND EXTENSION |
| PREN 6068 : 200P2 | AEROSPACE SERIES - PIN, QUICK RELEASE, SELF-RETAINING, POSITIVE LOCKING, SINGLE ACTING, BUTTON HANDLE |
| NASM 21045:2004 | NUT, SELF-LOCKING, HEXAGON, REGULAR HEIGHT, 450 DEGREES F, 125 KSIFTU |
| SAE AS 39631 : 1999 | UNIVERSAL JOINT, ANTIFRICTION BEARINGS |
| ASTM F 844 : 2007 : REV A : R2013 | Standard Specification for Washers, Steel, Plain (Flat), Unhardened for General Use |
| SAE AS 1501 : 1994 | HOSE, AIR DUCT, FLEXIBLE, NONMETALLIC, AIRCRAFT |
| ASTM F 1387 : 1999 | Standard Specification for Performance of Piping and Tubing Mechanically Attached Fittings |
| AA-D-2757 Base Document:1990 | DOOR, VAULT, SECURITY |
| MIL-A-23121 Revision C:1970 | AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR |
| MIL-P-5673 Revision D:1983 | PIN, STRAIGHT HEADED |
| MIL-DTL-7885-16 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, UNIVERSAL PROTRUDING HEAD, NICKEL-COPPER ALLOY SLEEVE (ALUM COAT), MECHANICALLY LOCKED CRES SPINDLE, OVERSIZE DIAMETER (TYPE I, STYLE B, CLASS 4) |
| MIL-N-45938 Revision A:1995 | NUT, PLAIN, CLINCH AND NUT, SEL-LOCKING, CLINCH GENERAL SPECIFICATION FOR |
| MIL-P-23460 Revision E:1991 | PIN, QUICK-RELEASE, SELF-RETAINING POSITIVE-LOCKING |
| MIL-DTL-7885-12 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, 100 DEG. FLUSH HEAD, 5056 AL ALLOY SLEEVE, MECHANICALLY LOCKED CRES SPINDLE |
| MIL-U-3963 Revision A:1958 | UNIVERSAL JOINT, ANTIFRICTION BEARINGS |
| MS21077 Revision H:1994 | NUT, SELF-LOCKING, PLATE, TWO LUG, FLOATING, NON-METALLIC INSERT, STEEL 125 KSI FTU, 250 DEG F |
| MIL-F-5591 Revision C:1986 | FASTENERS, PANEL, NONSTRUCTURAL |
| MIL-C-6985 Revision B:1966 | CLAMP, HOSE |
| MIL-DTL-7885-14 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, UNIVERSAL PROTRUDING HEAD, 5056 AL ALLOY SLEEVE, MECHANICALLY LOCKED CRES SPINDLE, OVERSIZE DIAMETER (TYPE I, STYLE B, CLASS 1) |
| AA-C-2859 Base Document:1994 | CABINET, SECURITY, WEAPONS STORAGE |
| MIL-DTL-7885-11 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, UNIVERSAL PROTRUDING HEAD, 5056 AL ALLOY SLEEVE, MECHANICALLY LOCKED CRES SPINDLE (TYPE I, STYLE A, CLASS 1) |
| 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-DTL-7885-28 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, FLANGED DOME HEAD, 5056 AL ALLOY SLEEVE, MECHANICALLY LOCKED 8740 ALLOY STEEL SPINDLE, OVERSIZE DIAMETER (TYPE I, STYLE B, CLASS 4) |
| MIL-S-21472 Revision C:1988 | SCREW, SHOULDER, HEXAGON SOCKET-HEAD AND SLOTTED-HEAD GENERAL SPECIFICATION FOR |
| MIL-DTL-7885-15 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, 100 DEG.FLUSH HEAD, 5056 AL ALLOY SLEEVE, MECHANICALLY LOCKED CRES SPINDLE, OVERSIZE DIAMETER (TYPE I, STYLE B, CLASS 2) |
| MIL-S-45909 Revision C:1989 | STUD, LOCKED IN - RING LOCKED SERRATED |
| MIL-F-81177 Revision E:1984 | FASTENERS, BLIND, HIGH STRENGTH, INSTALLATION FORMED ALLOY STEEL, GENERAL SPECIFICATION FOR |
| MIL-DTL-7885-20 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, 100 DEG. FLUSH SHEAR HEAD, NICKEL-COPPER ALLOY SLEEVE (ALUM COAT), MECHANICALLY LOCKED CRES SPINDLE, (TYPE 1, STYLE A, CLASS 3) |
| MIL PRF 83513 : D | CONNECTORS, ELECTRICAL, RECTANGULAR, MICROMINIATURE, POLARIZED SHELL, GENERAL SPECIFICATION FOR |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MS17987 Revision G:1994 | PIN, QUICK RELEASE, SELF-RETAINING, POSITIVE LOCKING, SINGLE ACTING, RING HANDLE |
| MIL-P-10971 Revision E:1969 | PIN, SPRING, TUBULAR (COILED AND SLOTTED) |
| MIL N 25027 : G | NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F |
| MIL-PRF-25134 Revision C:1996 | REMOVER, PAINT AND LACQUER, SOLVENT TYPE |
| MIL-G-16491 Revision F:1989 | GROMMET, METALLIC |
| MIL-F-22978 Revision A:1963 | FASTENER, ROTARY, QUICK-OPERATING, HIGH STRENGTH (ASG) |
| MIL-A-81973 Base Document:1974 | AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR |
| MIL-B-83050 Revision D:1985 | BOLT, SELF RETAINING, IMPEDANCE TYPE |
| MIL-S-7839 Revision B:1973 | SCREW, STRUCTURAL, AIRCRAFT |
| MIL F 83798 : B | FITTING, RUBBER HOSE, LIGHTWEIGHT MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
| MIL-C-24066 Revision C:1992 | CLIP, COMPONENT, NON-ELECTRICAL, GENERAL SPECIFICATION FOR |
| AA-F-363 Revision C:1990 | FILING CABINET, SECURITY, MAPS AND PLANS, GENERAL FILING AND STORAGE |
| MIL-P-16610 Revision B:1975 | PIN, TAPERED, PLAIN |
| MIL-DTL-7885-27 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, 100 DEG. FLUSH SHEAR HEAD, 5056 AL ALLOY SLEEVE, MECHANICALLY LOCKED 8740 ALLOY STEEL SPINDLE (TYPE I, STYLE A, CLASS 3) |
| MIL-T-53101 Base Document:1990 | TANKS, FABRIC, COLLAPSIBLE, 3000, 10,000 & 20,000 GALLON, PETROLEUM, LOW TEMPERATURE |
| MIL I 45910 : C | INSERT, SCREW THREAD LOCKED IN & RING LOCKED 1 SERRATED GENERAL SPECIFICATION FOR |
| AA-F-357 Revision F:1970 | FILING CABINET, STEEL, LEGAL AND LETTER SIZE, INSULATED, SECURITY |
| MIL-H-8775 Revision D:1976 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
| MIL-DTL-7885-13 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, 100 DEG. FLUSH SHEAR HEAD, 5056 AL ALLOY SLEEVE, MECHANICALLY LOCKED CRES SPINDLE |
| MIL-DTL-25027 Revision H:1997 | NUT, SELF-LOCKING, 250 DEG F, 450 DEG F, AND 850 DEG F |
| MIL-F-8975 Revision B:1982 | FASTENER, BLIND, HIGH STRENGTH, INSTALLATION FORMED CORROSION RESISTANT STEEL, HEAT RESISTANT STEEL AND TITANIUM, GENERAL SPECIFICATION FOR |
| MIL-N-45938-6 Revision C:1995 | NUT, SELF LOCKING, CLINCH (SWAGE-CLINCHING, KNURLED SHANK, MINIATURE 450 DEG.F) |
| MIL-N-52110 Revision F:1982 | NOZZLE, FUEL & OIL SERVICING, NONAUTOMATIC SHUTOFF & NOZZLES, FUEL SERVICING AUTOMATIC SHUTOFF |
| MIL PRF 24308 : D | CONNECTORS, ELECTRIC, RECTANGULAR, NONENVIRONMENTAL, MINIATURE, POLARIZED SHELL, RACK AND PANEL, GENERAL SPECIFICATION FOR |
| AA-V-2737 Base Document:1990 | MODULAR VAULT SYSTEMS |
| MIL-B-8831 Revision B:1982 | BOLT, 180 KSI FTU AND 180 KSI FSU 450 DEG F PROTRUDING AND FLUSH HEAD, GENERAL SPECIFICATION FOR |
| MIL-T-83965 Revision B:1990 | TRUCK, FIRE FIGHTING, A/S32P-10, FORCIBLE ENTRY |
| MIL-P-21143 Revision B:1984 | PIN, STRAIGHT, HEADLESS (DOWEL) |
| MIL-B-7838 Revision C:1989 | BOLT, INTERNAL WRENCHING 160 KSI FTU |
| MIL-W-45595 Revision D:1985 | WASHER, RECESSED, SADDLE AND SHOULDERED METAL |
| MIL-N-8984 Base Document:1972 | NUT, SELF-LOCKING, STEEL, 260 KS1 FTU 450 DEGREES F |
| MS20604 Revision K:1995 | RIVET, BLIND, NONSTRUCTURAL, UNIVERSAL HEAD, CLASS 1 |
| MS17984 Revision F:1994 | PIN QUICK RELEASE, SELF RETAINING POSITIVE LOCKING SINGLE ACTING BUTTON HANDLE |
| MIL-N-8985 Base Document:1972 | NUT, SELF-LOCKING STEEL, 180 KS1 FTU 450 DEGREES F |
| MS21025 Revision F:1996 | NUT, CASTELLATED, HEXAGON |
| AA-S-1518 Revision A:1970 | SAFE, TOOL RESISTANT, UNINSULATED, SECURITY |
| MIL-B-45908 Revision B:1985 | BOLT, EYE, GENERAL SPECIFICATION FOR |
| MIL-R-27384 Revision B:1970 | RIVET, BLIND, DRIVE TYPE |
| AA-D-600 Revision D:2000 | DOOR, VAULT, SECURITY |
| MIL-S-45915 Revision A:1967 | STUD, LOCKED IN - KEY LOCKED - GENERAL SPECIFICATION FOR |
| AA-V-2940 Base Document:2008 | VAULT SYSTEM, ARMORY, ASSEMBLED |
| MIL-B-8952 Revision B:1995 | BEARING, ROLLER, ROD END, ANTIFRICTION, SELF-ALIGNING |
| MIL-DTL-6162 Revision C:2000 | GENERATORS AND STARTER-GENERATORS, ELECTRICAL DIRECT CURRENT, NOMINAL 30 VOLTS, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL-F-8961 Revision A:1992 | Fastener Element, Self-Locking, Externally Threaded, 450 Degrees Fahrenheit and 1,200 Degrees Fahrenheit |
| MIL F 5508 : B | FUSE, AIRCRAFT AUTOMATIC QUANTITY MEASURING HYDRAULIC |
| MIL-R-81876 Revision B:1988 | RECEIVER, TRANSMITTER RADIO SET AN/APX-100(V) |
| MIL-I-6447 Revision C:1974 | INDICATOR, TRUE AIRSPEED TYPE M 1A |
| DOD-I-63274 Revision A:1983 | Insert, Screw Thread-Thin Wall, Locked in, Metric, General Specification for |
| MIL F 18240 : E | FASTENER ELEMENT, SELF-LOCKING, THREADED FASTENER, 250 DEG F MAXIMUM |
| MIL-L-7806 Revision A:1956 | LIGHT, PANEL, PLASTIC PLATE, LIGHTING |
| MIL-A-28737 Revision A:1977 | ANTENNA, IFF, AS-2188(),(3 METERS) (1O FEET)), AS-2189 (1.8 METERS (6 FEET)) |
| MIL A 24775 : 0 | AIR CONDITIONING FAN COIL UNITS, HORIZONTAL AND VERTICAL TYPES, NAVAL SHIPBOARD |
| MIL S 5002 : D | SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
| MIL-M-8609 Revision B:1965 | MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE AMS C 19853 : 1998 | CARBON REMOVING COMPOUND (FOR USE IN AGITATED TANK) |
| MIL-S-8660 Revision C:1983 | SILICONE COMPOUND, NATO CODE NUMBER S 736 |
| MIL-B-25084 Base Document:1955 | BEACON, RADIO AN-APN 69 |
| MIL-C-81511 Revision F:1992 | CONNECTOR, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT ENVIRONMENT RESISTING, AND ACCESSORIES GENERAL SPECIFICATION FOR |
| MIL B 45912 : A | BOLT, SELF-LOCKING, HEXAGON HEAD, STEEL |
| MIL-S-43770 Base Document:1972 | SNAP HOOKS GENERAL SPECIFICATION FOR |
| MIL-S-24298 Revision A:1969 | SAFETY BELT AND HARNESS, SUBMARINE PERSONNEL |
| MIL-H-62217 Revision A:1981 | HOSE AND HOSE ASSEMBLIES, NON METALLIC, SILICONE, POLYESTER AND WIRE REINFORCED (FOR COOLANT AND HEATING SYSTEMS OF DIESEL & GASOLINE POWERED ENGINES) |
| MIL R 23016 : A | RADIO SET AN/ARC-94 |
| SAE AS 4444 : 2013 | FITTINGS, 24 DEGREE CONE FLARELESS, FLUID CONNECTION, 5000 PSI |
| MIL L 60427 : B | LOCKWIRE, FOR 2.75 INCH ROCKET MOTOR ALL MARKS AND MODS |
| MIL-STD-2156 Base Document:1983 | LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| MIL-F-46579 Revision D:1976 | FUSE, POINT DETONATING, M505A3, PARTS FOR |
| MIL-I-45934 Base Document:1971 | INSERT, SCREW THREAD, KEYRING LOCKED, SELF LOCKING AND NON SELF LOCKING, 125, 180, AND 220 KSI FTU: GENERAL SPECIFICATION FOR |
| MIL S 8516 : F | SEALING COMPOUND, POLYSULFIDE RUBBER, ELECTRIC CONNECTORS AND ELECTRICAL SYSTEMS CHEMICALLY CURED |
| AA-C-001402 Base Document:1986 | CABINET, PROTECTIVE STORAGE AND FILING, UNINSULATED, WITH COMBINATION PADLOCK |
| MIL-C-85049 Revision A:1990 | CONNECTOR ACCESSORIES, ELECTRICAL GENERAL SPECIFICATION FOR |
| MIL-P-21415 Revision C:1973 | PROTECTIVE FINISH AND PAINTING FOR POLARIS FLEET BALLISTIC MISSILE |
| MIL-F-45060 Revision D:1975 | FUZE, MINE, COMBINATION M605, PARTS FOR |
| MIL-A-19736 Revision A:1960 | AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-C-40084 Revision C:1990 | CORROSION PREVENTIVE COMPOUND, WATER EMULSIFIABLE, OIL TYPE |
| MIL S 13623 : C | SWITCH, ROTARY, 28 VOLT DC |
| MIL-STD-1250 Revision A:1992 | CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
| MIL C 7958 : A | CONTROL, PUSH PULL, FLEXIBLE AND RIGID |
| MIL P 81716 : 0 | PACKING, PREFORMED, STRAIGHT THREAD TUBE FITTING BOSS, TYPE II HYDRAULIC (MINUS 65 DEG F TO PLUS 275 DEG F) |
| FF-B-575 Revision C:1970 | BOLTS, HEXAGON AND SQUARE |
| MIL C 7907 : A | CLEANING COMPOUND, DECONTAMINATING [FOR SOILED AND RADIOACTIVE CONTAMINATED SURFACES] |
| MIL-C-1161 Revision E:1988 | COLLAR, DOG, LEATHER |
| MIL-D-83029 Revision A:1968 | DRIVE ASSEMBLY, CONSTANT SPEED, GENERAL SPECIFICATION FOR |
| MIL H 81529 : 0 | HOOK, HELICOPTER EXTERNAL CARGO, 6,000 POUND CAPACITY TYPE A |
| MIL-I-85671 Base Document:1987 | INDICATOR, FREQUENCY CHANNEL ID-2121A/ARC, ID-2229A/ARC AND ID-2303/ARC |
| MIL R 11767 : F | RELAY ASSEMBLY, GUN & FIRING, WATERPROOF, 24 VOLT DIRECT CURRENT |
| MIL-G-23337 Base Document:1962 | GAGE - PRESSURE, DIAL INDICATING |
| MIL G 26611 : D | GENERATOR, TACHOMETER GEU-7/A, MINIATURE |
| DOD-B-63545 Base Document:1982 | BOLTS, RIBBED SHOULDER, WHEEL MOUNTING, METRIC GENERAL SPECIFICATION FOR |
| MIL F 45968 : A | FITTINGS, AUTOMOTIVE TUBE, BRASS INVERTED FLARE (WITH STEEL NUT) |
| MIL P 26517 : A | POWER SUPPLY, TRANSFORMER-RECTIFIER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-C-82594 Base Document:1971 | CORROSION PREVENTIVE COMPOUND AND SURFACE SEALER FOR NONFERROUS METALS |
| MIL-F-50454 Revision A:1969 | FUZE, GRENADE, M219E1 LOADING, ASSEMBLING AND PACKING |
| MIL-I-82437 Base Document:1966 | |
| MIL-B-51492 Revision A:1987 | BELT, SAFETY BOAT |
| MIL-T-19576 Revision A:1961 | TRANSMITTER, REMOTE COMPASS, THIN WING TYPE ML-1 (UNSTABILIZED) |
| MIL C 55302/38 : B | CONNECTORS, PRINTED CIRCUIT SUBASSEMBLY AND ACCESSORIES: PLUG, ELECTRICAL, POLARIZED SHELL, MALE, 0.100 INCH CONTACT SPACING, PIN TERMINAL |
| MIL-D-9063 Revision B:1965 | DESEALANT, INTEGRAL FUEL AND OIL TANKS |
| MIL-F-8839 Revision A:1988 | Fittings, Lubrication Drive Type |
| DOD-P-63477 Base Document:1981 | PIN, SPRING, TUBULAR, (COILED AND SLOTTED), GENERAL SPECIFICATION FOR, METRIC |
| MIL-T-13513 Revision B:1989 | TERMINAL, LUG, SPLICE, CONDUCTOR (ELECTRICAL, SOLDERLESS, FOR AUTOMOTIVE USE) |
| MIL C 45918 : 0 | CLEVISES AND CONNECTORS (ROD END) |
| MIL-I-5133 Revision C:1953 | INDICATOR, ATTITUDE TYPE J 8 |
| MIL-P-60009 Revision B:1990 | PROPELLANT CHARGE ASSEMBLY ROCKET, HIGH EXPLOSIVE, 66MM, M72A1, WITH COUPLER |
| MIL C 38999 : J | CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET THREADED & BREECH COUPLING) ENVIRONMENT RESISTANT, REMOVABLE CRIMP & HERMETIC SOLDER CONTACTS |
| MIL-C-5604 Revision B:1962 | COMPASS, MAGNETIC, PILOTS STANDBY |
| MIL-C-29145 Revision B:1984 | COAT, FIREMANS, ALUMINIZED PROXIMITY |
| MIL-H-87111 Revision A:1984 | HEAT SINKS, SEMICONDUCTOR DEVICES, GENERAL SPECIFICATION FOR |
| MIL-F-60323 Revision A:1971 | FUZE, PD, M525, M526 & M527B1 LESS HEAD ASSEMBLY METAL PARTS FOR |
| MIL-R-52255 Revision D:1988 | REPAIR KIT AND REPAIR KIT COMPONENTS, FOR COLLAPSIBLE FABRIC TANKS, DRUMS, AND BOATS |
| MIL-HDBK-1250 Revision A:1995 | CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
| MIL-B-13136 Revision B:1968 | BATTERIES DRY |
| MIL-A-21071 Revision B:1973 | ANTIFOGGING COMPOUND, TRANSPARENT AIRCRAFT ENCLOSURES |
| NAS159:2002 | BOLT - INTERNAL WRENCHING - AIRCRAFT |
| MIL-C-43616 Revision C:1981 | CLEANING COMPOUND, AIRCRAFT SURFACE |
| MIL-I-23870 Base Document:1963 | INDICATOR, FUEL RATE OF FLOW, 0 TO 15 GPM |
| MIL-STD-1516 Revision B:1990 | UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIAL |
| MIL P 7034 : D | PULLEY, GROOVE, ANTIFRICTION BEARING, GREASE LUBRICATED, AIRCRAFT |
| MIL U 18182 : E | UNION, PIPE, FORGED STEEL, THREADED, WATER OIL GAS (2,000, 3,000 AND 6,000 LB/IN2) |
| MIL-S-6150 Revision D:1987 | STARTER, ENGINE, ELECTRICAL, DIRECT CRANKING, AIRCRAFT 28 VOLT DC |
| DOD-B-63475 Base Document:1981 | BOLTS, SHOULDER, HEXAGON HEAD, GENERAL SPECIFICATION FOR, METRIC |
| MIL-STD-2131 Revision A:1991 | LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| MIL L 58085 : A | LIGHT, BEACON, ANTI COLLISION AIRCRAFT |
| DOD-P-70330 Base Document:1982 | PLUG, EXPANSION METRIC, GENERAL SPECIFICATION FOR |
| MIL-T-704 Revision K:1992 | Treatment and Painting of Material |
| MIL-P-8564 Revision D:1970 | PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
| MIL B 8075 : D | BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
| MIL-R-48233 Revision A:1980 | Rod, Stabilizing, Coated for 2.75 Inch Rocket Motor MK4/MK40and Mods |
| MIL-C-4150 Revision J:1989 | CASE, TRANSIT AND STORAGE, WATERPROOF AND WATER-VAPORPROOF |
| MIL I 38715 : B | INDICATOR, COMBUSTIBLE GAS AND TOXIC GAS |
| MIL R 46963 : A | ROCKET MOTOR, M42A1, BOOSTER |
| MIL-A-62019 Revision B:1969 | ARMORED RECONNAISSANCE/AIRBORNE ASSAULT VEHICLE: FULL-TRACKED, 152 MM, M551; PROCESSING FOR STORAGE AND SHIPMENT OF |
| MIL S 12109 : C | SOLENOID, ELECTRICAL, CLASS 2 (MACHINE GUN) |
| MIL C 4928 : A | CHARGER, BATTERY, SILICON DIODE, TYPE A-1 |
| MIL C 83723 : E | CONNECTORS, ELECTRICAL (CIRCULAR, ENVIRONMENT RESISTING) RECEPTACLES AND PLUGS GENERAL SPECIFICATION FOR |
| MIL-DTL-85110 Revision B:1997 | BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR |
| NASM 7838 : 2004 | BOLT, INTERNAL WRENCHING, 160 KSI FTU |
| NASM20392:2011 | PIN, STRAIGHT, HEADED DRILLED SHANK |
| SAE AS 85731 : 2015 | FASTENER, POSITIVE LOCKING, ELECTRONIC EQUIPMENT, GENERAL SPECIFICATION FOR |
| NASM35338:2013 | WASHER, LOCK-SPRING, HELICAL, REGULAR (MEDIUM) SERIES |
| NASM35338:2014 | WASHER, LOCK-SPRING, HELICAL, REGULAR (MEDIUM) SERIES |
| ASTM B 766 : 1986 : R1998 | Standard Specification for Electrodeposited Coatings of Cadmium |
| MIL-DTL-5015 Revision H:2000 | CONNECTORS, ELECTRICAL, CIRCULAR THREADED, AN TYPE - GENERAL SPECIFICATION FOR |
| MIL F 3922 : B | FLANGE, WAVEGUIDE, GENERAL PURPOSE GENERAL SPECIFICATION FOR |
| MIL-P-17802 Revision E:1987 | PADLOCK AND PADLOCK SETS, LOW SECURITY, KEY OPERATED, REGULAR (OPEN) SHACKLE |
| MIL-V-5527 Revision A:1951 | VALVE, AIRCRAFT, HYDRAULIC THERMAL EXPANSION RELIEF |
| MIL-S-45005 Revision C:0198 | SEAL, PLAIN, AND SEAL, PLAIN, ENCASED, FLUID, RADIAL, SINGLE AND MULTIPLE LIP SEAL |
| MIL-M-9397 Revision E:1979 | FREQUENCY CONVERTER, MOBILE, TYPE MC-1A |
| MIL S 6807 : D | SWITCHES, ROTARY, SELECTOR POWER - GENERAL SPECIFICATION FOR |
| MIL-P-46416 Revision A:1964 | PROJECTILE, 25 MILLIMETER M379 FOR TRAINER MORTAR M32, ASSEMBLY |
| SAE AS 8181 : 1997 | DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-C-6122 Base Document:1950 | COLLIMATOR, SEXTANT, AIRCRAFT |
| MIL-I-5418 Revision B:1963 | INDICATOR: AIRSPEED, PITOT STATIC, SENSITIVE, 50-650 KNOTS |
| MIL-S-8812 Revision D:1975 | STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
| FF-W-100 Revision C:1969 | WASHER, LOCK, TOOTH |
| MIL-S-8710 Revision B:1969 | STRAINER, AIRFRAME FUEL SYSTEM, GENERAL SPECIFICATION FOR |
| MIL-F-3541 Revision C:1989 | FITTING, LUBRICATION, GENERAL SPECIFICATION FOR |
| MIL-M-7997 Revision C:1981 | Motor, Aircraft Hydraulic, Constant Displacement General Specification for |
| TT-R-248 Revision B:1981 | REMOVER, PAINT AND LACQUER, SOLVENT TYPE |
| MIL A 24045 : 69 NOTICE 1 | ALIDADE, BINOCULAR MARINE |
| NASM 23460 : 2004 | PIN, QUICK-RELEASE, SELF-RETAINING, POSITIVE-LOCKING |
| NASM21042:1998 | NUT, SELF-LOCKING, 450 DEGREES F, REDUCED HEXAGON, REDUCED HEIGHT, RING BASE, NON-CORROSION RESISTANT STEEL |
| MIL-S-85510 Base Document:1981 | Seats, Helicopter Cabin, Crashworthy, General Specification for |
| MIL-S-7852 Revision B:1968 | SEAT, AIRCREW, ADJUSTABLE SWIVEL TYPE E-1 |
| MIL-B-26793 Revision B:1958 | BLOWER, GASOLINE ENGINE DRIVEN, TYPE A-1 |
| MIL-A-26107 Revision D:1960 | AIR CONDITIONER, TRAILER-MOUNTED, FREON CYCLE, 11-1/2 TON REFRIGERATING CAPACITY, TYPE MA-3 |
| MIL-A-6425 Revision B:1959 | ADAPTOR, PRESSURE FUEL SERVICING, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-38331 Base Document:1964 | AMPLIFIER-POWER SUPPLY AM-4080/ASN-55, LEVELLING |
| MIL-C-81582 Revision B:1975 | CONNECTOR, ELECTRICAL, BAYONET COUPLING, ENVIRONMENTAL RESISTING, UMBILICAL, GENERAL SPECIFICATION FOR |
| DOD-P-63542 Base Document:1981 | PIN, GROOVE, HEADED LONGITUDINAL GROOVE, METRIC, GENERAL SPECIFICATION FOR |
| MIL-W-70342 Base Document:1988 | WASHER, FLAT, METRIC |
| MIL-V-8610 Revision B:1984 | VALVE, FUEL SHUTOFF SOLENOID OPERATED, 28 VOLT, DC |
| FF-T-305 Revision C:1974 | THUMBSCREW |
| NASM16562:2010 | PIN, SPRING, TUBULAR, SLOTTED |
| MIL-M-70780 Base Document:1988 | MINE, ANTI-PERSONNEL: M86 ARMING ASSEMBLY FOR |
| MIL-I-27273 Revision A:1965 | Inverter, Power, Static, General Specification for |
| MIL-G-8798 Base Document:1956 | GAGE SYSTEM, FUEL QUANTITY, CAPACITOR TYPE NONVACUUM TUBE, INTEGRALLY LIGHTED GENERAL SPECIFICATION FOR |
| MIL-I-21203 Revision A:1962 | Indicator, Attitude, Spherical, Direct Reading, Fast Erecting, Electric Gyro |
| MIL-A-19940 Base Document:1957 | AMPLIFIER, CONTROL SINGLE CHANNEL, S-2 COMPASS |
| MIL-G-22169 Base Document:1959 | GYRO, VERTICAL AND MOUNT |
| MIL-C-18053 Revision A:1958 | CONTROL AMPLIFIER, ALTITUDE (P-1 AUTOMATIC PILOT RADAR SET, AN/APN-22) |
| MIL-F-85731 Base Document:1986 | FASTENER, POSITIVE LOCKING, ELECTRONIC EQUIPMENT GENERAL SPECIFICATION FOR |
| MIL T 21014/1 : 0 | TUNGSTEN BASE PARTS, HIGH DENSITY METAL (SINTERED OR HOT PRESSED), COATED, ELECTRODEPOSITED CADMIUM |
| MIL-S-9487 Revision C:1985 | SWITCH, TRIGGER, SINGLE POLE, TWO STAGE, MOMENTARY |
| MIL-R-19750 Revision A:1958 | REGULATOR; VOLTAGE, 28 V, 120 DEGREE C, FOR 30 V DIRECT-CURRENT GENERATOR, GENERAL SPECIFICATION FOR |
| DOD-N-70333 Base Document:1985 | NUT, PLAIN AND SELF-LOCKING, CLINCH, METRIC (SELF-CLINCHING, KNURLED COLLAR) FIXED AND FLOATING, GENERAL SPECIFICATION FOR |
| MIL-N-85615-8 Base Document:1989 | Nut, Self-Sealing, Self-Locking, Alloy Steel, 125 KSI FTU, 250 Deg. F and 450 Deg. F |
| MIL-P-48188 Revision A:1992 | PROJECTILE, 155MM, HE: M692 AND M692 AND M731, METALLIC HARDWARE FOR |
| FF-P-386 Revision D:1971 | PIN, COTTER (SPLIT) |
| FF-P-101 Revision F:1984 | PADLOCK |
| MIL-PRF-8516 Revision G:1997 | SEALING COMPOUND, SYNTHETIC RUBBER, ELECTRIC CONNECTORS AND ELECTRIC SYSTEMS, CHEMICALLY CURED |
| FF-N-845 Revision D:1981 | NUT, PLAIN, WING, INCH AND METRIC |
| MIL-S-18471 Revision G:1983 | System, Aircrew Automated Escape, Ejection Seat Type, General Specification For |
| MIL-V-5461 Revision C:1977 | VALVE, VACUUM BREAKING |
| MIL-B-81820 Revision F:1994 | BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, LOW SPEED OSCILLATION, 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 82356 : NOTICE 1 | INSTRUMENTS, SIMULATED, FOR AIRCRAFT TRAINING DEVICES; GENERAL SPECIFICATION FOR |
| MIL-P-19692 Revision E:1994 | PUMPS, HYDRAULIC, VARIABLE FLOW, GENERAL SPECIFICATION FOR |
| MIL-F-5509 Revision D:1978 | FITTING, FLARED TUBE, FLUID CONNECTION |
| MIL C 24308 : C | CONNECTORS, ELECTRIC, RECTANGULAR, NON-ENVIRONMENTAL, MINIATURE, POLARIZED SHELL, RACK AND PANEL, GENERAL SPECIFICATION FOR |
| MIL-I-45914 Revision A:1991 | INSERT, SCREW THREAD - LOCKED IN, KEY LOCKED |
| MIL-I-22075 Revision C:1984 | Indicator, Bearing-Distance-Heading ID-663D/U |
| MIL C 55422 : 0 | CLIP, ELECTRICAL, GRID AND ANODE, GENERAL SPECIFICATIONS FOR |
| MIL-R-47321 Base Document:1987 | REGULATOR, PRESSURE |
| AA-F-2815 Base Document:1992 | FILING CABINET, UNINSULATED, SECURITY (SECRET AND CONFIDENTIAL STORAGE) |
| MIL-W-50930 Base Document:1971 | WARHEAD SECTION 762MM ROCKET TRAINING M42' |
| DOD-S-70328 Base Document:1982 | SPACER, RING, METRIC GENERAL SPECIFICATION FOR |
| DOD-B-70331 Base Document:1983 | Bolt, Self Locking, Hexagon Head, Steel, Metric, General Specification for |
| MIL C 22263 : B | COUPLING FUEL LINE, FLEXIBLE, 125 PSI, GENERAL SPECIFICATION FOR |
| ASTM F 844 : 2007 : REV A | Standard Specification for Washers, Steel, Plain (Flat), Unhardened for General Use |
| MIL-STD-808 Revision A:1983 | FINISH, MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN SUPPORT EQUIPMENT |
| MIL-W-50932 Base Document:1971 | WARHEAD SECTION, 762MM ROCKET, TRAINING: M42, OGIVE FOR |
| MIL-B-25870 Revision A:1972 | BEARINGS SINTERED METAL, PROCESSING OF |
| MIL-A-47309 Revision A:1991 | AMPLIFIER, PNEUMATIC |
| A-A-55628 Revision A:1998 | NUT, PLAIN, CAP, HIGH CROWN UNC-2B AND UNF-2B |
| MIL S 25073 : 0 | |
| MIL C 12520/11 : A | CONNECTORS, RECEPTACLE, ELECTRICAL WATERPROOF (SHELL SIZE 26, FEMALE INSERTS) |
| MIL-D-7713 Base Document:1951 | Drift Meter, Type B-5 |
| MIL-B-81819 Revision B:1987 | BEARING, PLAIN, (SLIDING SPHERICAL, SLEEVE & THRUST) SELF LUBRICATING, HIGH SPEED OSCILLATION, GENERAL SPECIFICATION FOR |
| MIL-N-85615-3 Base Document:1989 | Nut Assembly, Self-Sealing, Floating, Self-Locking, 125 KSI FTU, 225 Deg. F, Variable Nut Height 1/64 In. Oversize (For Repair) |
| MIL T 5579 : 0 | TANK, SELF-SEALING OIL, AIRCRAFT |
| MIL-T-21578 Revision A:1966 | TEST EQUIPMENT, HAZARDOUS LOCATION, INSTALLED, BASIC REQUIREMENTS FOR |
| MIL-C-6629 Base Document:1951 | CARBON MICROPHONE M-15 ( )/UR |
| DOD-S-63543 Base Document:1982 | STUD & ROD, THREADED, METRIC, GENERAL SPECIFICATION FOR |
| MIL-C-5584 Revision D:1988 | CONTAINER, SHIPPING AND STORAGE, METAL REUSABLE |
| MIL T 25439 : A (1) | TRANSMITTER, RATE OF FLOW, IN-FLIGHT REFUELLING, 0-10,000 PPM, TYPE MB-3 |
| MIL-T-23643 Base Document:1963 | TEST SET, TARGET CONTROL SYSTEM AN/SRM SERIES (AN/SRM-2, AN/SRM-3, AN/SRM-4, AN/SRM-5 AND AN/SRM-6) |
| FF-W-84 Revision A:1967 | WASHER, LOCK (SPRING) |
| MIL-PRF-85704 Revision C:1998 | CLEANING COMPOUND, TURBINE ENGINE GAS PATH |
| MIL T 83454 : 0 | TERMINAL, STUD, BLIND PLATE, FOR ELECTRICAL BONDING AND GROUNDING (NONINSULATED) |
| MIL-S-58112 Base Document:1989 | SLING, MULTI LEG, HELICOPTER, EXTERNAL CARGO |
| MIL-A-27328 Base Document:1960 | AMPLIFIER-INDICATOR GROUP, ALTITUDE VERTICAL SPEED A/A24G-7 |
| MIL I 7304 : B | INDICATOR, PRESSURE TORQUE SENSITIVE TYPE A 9 |
| MIL-I-5488 Revision A:1957 | INDICATOR TURN AND SLIP 28V DC 2 3/4 SIX, TYPE MD 10 |
| MIL-I-5482 Revision C:1960 | INDICATOR, PRESSURE, SYNCHRO, AIRCRAFT 165 DEGREE SCALE |
| PREN 6067 : 200P2 | AEROSPACE SERIES - PIN, QUICK RELEASE, SELF-RETAINING, POSITIVE LOCKING, DOUBLE ACTING, BUTTON HANDLE |
| MIL-P-5238 Revision C:1974 | PUMP, CENTRIFUGAL, FUEL BOOSTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| FF-N-836 Revision E:1994 | Nut: Square, Hexagon, Cap, Slotted, Castle, Knurled, Welding and Single Ball Seat |
| ASTM F 1387 : 1999 : R2012 | Standard Specification for Performance of Piping and Tubing Mechanically Attached Fittings |
| ASTM B 766 : 1986 : R2003 | Standard Specification for Electrodeposited Coatings of Cadmium |
| MS24693 Revision K:1995 | SCREW, MACHINE, FLAT COUNTERSUNK HEAD, 100 DEG, CROSS RECESSED, UNC-2A AND UNF-2A (IN./MM) |
| NASA MSFC STD 486 : 1992 | STANDARD, THREADED FASTENERS, TORQUE LIMITS FOR |
| MS35338 Revision L:1994 | WASHER, LOCK SPRING, HELICAL, REGULAR (MEDIUM) SERIES |
| MIL-N-85615-4 Base Document:1989 | Nut Assembly, Self-Sealing, Low Profile, Floating, Self-Locking, 125KSI FTU, 225 Deg. F |
| MIL G 6162 : B | GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION |
| MIL-A-22212 Base Document:1959 | ANTENNAS, AT-500(*)/AP AND AT-929(*)/AP; AND ANTENNA BASE AB-117(*)/AP |
| MIL-DTL-26894 Revision D:1998 | Hose and Hose Assembly, Rubber, Gasoline, Refueling, Low Temperature |
| FF-B-561 Revision D:1989 | BOLT, (SCREW), LAG |
| FF-S-210 Revision B:1981 | SETSCREWS, SQUARE HEAD (INCH) AND SLOTTED HEADLESS (INCH AND METRIC) |
| MIL-F-18280 Revision F:1995 | FITTING, FLARELESS TUBE, FLUID CONNECTION |
| MIL I 5099 : B | INDICATOR CABIN AIR PRESSURE, 1-7/8 INCH DIAL, TYPE MA-1 |
| MIL-I-18804 Revision B:1964 | INDICATOR, VERTICAL SPEED, 0 - 6000 FPM, 2 INCH |
| NASA MSFC SPEC 250 : 1963 | PROTECTIVE FINISHES FOR SPACE VEHICLE STRUCTURES AND ASSOCIATED FLIGHT EQUIPMENT GENERAL SPECIFICATION FOR |
| MIL C 12520/10 : A | CONNECTORS, RECEPTACLE, ELECTRICAL WATERPROOF (SHELL SIZE 26, MALE INSERTS) |
| MIL P 17842 : NOTICE 1 | POWER PLANT VIBRATION ISOLATOR, DESIGN AND INSTALLATION REQUIREMENTS |
| MIL I 38135 : B (3) | INDICATOR, INDICATED AIRSPEED AVU 19/A STANDBY |
| MIL-R-24358 Base Document:1968 | RESTORATION SHIPBOARD ELECTRONIC EQUIPMENT F, 1N AND 2N COGNIZANCE |
| MIL F 0040048 : B INT (1) | FLAGSTAFFS AND INSIGNIA, FLAGSTAFF HEADS, GENERAL SPECIFICATION FOR |
| MIL-N-85615 Base Document:1986 | Nut, Sealing, Self-Locking, 250 Degrees F, 450 Degrees F General Specification For |
| MIL S 8834 : F | SWITCH, TOGGLE, POSITIVE BREAK, GENERAL SPECIFICATION FOR |
| MIL G 8360 : A | GAGE, PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE, 10-75 IN MERCURY TYPE MB 1 |
| MIL-T-5684 Revision B:1981 | TIE RODS; ROUND AND SQUARE, AIRCRAFT |
| MIL-G-16408 Revision B:1953 | GAGE, LIQUID LEVEL, TAPE AND FLOAT, DIRECT READING (FOR SHIPBOARD USE) |
| DOD-S-63275 Revision A:1982 | STUD, SCREW THREAD, LOCKED IN, RING LOCKED, SERRATED, METRIC AND RING LOCK SERRATED METRIC, GENERAL SPECIFICATION FOR |
| NNN-T-580 Base Document:1963 | TONG LABORATORY |
| MIL C 12520/8 : A | CONNECTORS, RECEPTACLE, ELECTRICAL WATERPROOF (SHELL SIZE 20, MALE INSERTS) |
| MIL-L-21652 Revision A:1964 | Light, Beacon, Anticollision, Aircraft, General Specification for |
| MIL S 9479 : C | |
| MIL T 6349 : C NOTICE 1 | TEST SET, SYNCHRO |
| MIL-I-58067 Revision A:1977 | INDICATOR, VERTICAL VELOCITY, RAPID RESPONSE ACCELERATION SENSITIVE, GENERAL SPECIFICATION FOR |
| MIL C 12520 : C | CONNECTOR, PLUG AND RECEPTACLE (ELECTRICAL, WATERPROOF), AND ACCESSORIES: GENERAL SPECIFICATION FOR |
| MIL C 8783 : A | CLAMP, HOSE, FLAT BAND 500 DEG. F |
| GGG-S-001333 Revision A Interim Revision:1975 | SCRAPER AND SQUEEGEE, VEHICLE WINDOW |
| AA-B-00540 Revision D Interim Revision:1978 | BOOKCASE SECTIONS, BASE AND TOP, STEEL, CONTEMPORARY STYLE |
| MIL-S-10522 Revision K:1975 | SIMULATOR, BOOBY TRAP WHISTLING M 119 PARTS FOR AND LOADING ASSEMBLING AND PACKING |
| MIL-I-81508 Base Document:1966 | INDICATOR PLUG, FOR MISSILE PROPELLANTS |
| MIL-N-3336 Revision A:1964 | Nut, Sheet Spring, Instrument Mounting |
| MIL-V-5622 Revision A:1963 | Volt-Ammeter, Dual Pointer Direct Current |
| MIL-F-60988 Revision B:1973 | FUZE, PD, M551 LESS BOOSTER |
| MIL-C-11569 Revision D:1979 | CLAMPS, HOSE, WATER, UNIVERSAL 3/8- TO 1-INCH AND 1- TO 3-INCH |
| MIL T 55069 : C NOTICE 1 | TRAINING AID, MODEL BRIDGE, FLOATING ALUMINUM, HIGHWAY TYPE, DECK BALK SUPERSTRUCTURE ON PNEUMATIC FLOATS |
| MIL-B-6038 Revision A:1961 | BEARING, BALL BELLCRANK, ANTI FRICTION, AIRFRAME |
| MIL-M-21365 Revision A:1961 | MICROPHONE, CARBON, NOISE CANCELLING, TYPE M-58/U |
| MIL-B-8948 Revision A:1972 | Bearing, Plain, Rod End, TFE Lined, Self-Aligning |
| MIL-S-6551 Revision A:1981 | |
| DOD-T-63549 Base Document:1982 | THUMBSCREW, WING HEAD, METRIC, GENERAL SPECIFICATION FOR (METRIC) |
| MIL C 27889 : D | COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING, CPU-46/A, GENERAL SPECIFICATION FOR AND MTU-38/A MOUNTING TRAY |
| FF-S-107 Revision C:1969 | SCREW, TAPPING AND DRIVE |
| MIL-C-11760 Revision D:1979 | CLAMPS, HOSE, PNEUMATIC, FOR UNIVERSAL COUPLINGS |
| MIL W 3903 : D | WIRE ROPE ASSEMBLY, SINGLE LEG |
| MIL-I-23264 Revision A:1968 | Insulators, Ceramic, Electrical and Electronic, General Specification for |
| MIL-I-85352 Base Document:1980 | INFLATOR ASSEMBLY AND GAGE ELEMENTS, PNEUMATIC PRESSURE REMOTE CONTROL, DIRECT READING |
| MIL-R-50858 Revision C:1979 | ROCKET, PRACTICE, 35MM SUBCALIBER, M73 PARTS FOR LOADING & ASSEMBLING |
| MIL P 27235 : A | PIN, STRAIGHT, HEADED (CLEVIS PINS) |
| ASTM B 766 : 1986 : R2015 | Standard Specification for Electrodeposited Coatings of Cadmium |
| MIL-C-27251 Revision A:1971 | CLEANING COMPOUND, AIRCRAFT SURFACE, LOW TEMPERATURE |
| DOD-P-63479 Base Document:1981 | PIN, STRAIGHT, HEADED (CLEVIS PIN) GENERAL SPECIFICATION FOR, METRIC |
| MIL H 26894 : C | HOSE ASSEMBLY, RUBBER, GASOLINE, REFUELING, LOW TEMPERATURE |
| MIL-W-10698 Revision C:1969 | WRENCH, OPEN END, AND WRENCH ASSEMBLY, STAMPED STEEL |
| MIL-G-81168 Base Document:1964 | GYROSCOPE, RATE INTEGRATING |
| MIL-P-83037 Revision A:1968 | PLATFORM, CARGO, AERIAL DELIVERY A/E29H-1 |
| MIL-C-81991 Base Document:1975 | CONVERTER, AIRCRAFT DC TO DC, BOOST GENERAL SPECIFICATION FOR |
| MIL C 85704 : B | CLEANING COMPOUND, TURBINE ENGINE GAS PATH |
| 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 |
| SAE MA 2005 : 2015 | TUBE FITTINGS, AEROSPACE FLUID SYSTEMS, SEPARABLE, FOR 24 DEGREE CONE, GENERAL SPECIFICATION, METRIC |
| MIL-I-22126 Revision B:1972 | INDICATOR, TORQUEMETER, ENGINE, TURBOPROP |
| MIL-I-23366 Revision B:1987 | Indicator, Horizontal Situation ID-1013(*)/A |
| MIL I 83452 : LATEST | INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
| MIL-B-81949 Base Document:1974 | BRUSHES, FLAP, ROTARY, ABRASIVE, GENERAL SPECIFICATION FOR |
| MIL-A-17204 Revision D:1982 | ADAPTERS, STRAIGHT OR REDUCING, PIPE THREAD TO HOSE THREAD |
| MIL-N-58106 Base Document:1982 | NET, HELICOPTER CARGO CARRYING EXTERNAL 5,000 AND 10,000 POUND CAPACITIES |
| MIL I 23145 : B | INFLATION ASSEMBLIES, LIFE PRESERVER |
| MIL-S-5804 Revision C:1967 | SEAT, AIRCRAFT, TROOP, WALL STYLE |
| MIL C 25478 : B | COOLER, LUBRICATING OIL, AIRCRAFT ENGINE, SYNTHETIC OIL, GENERAL SPECIFICATION FOR |
| RR-G-700 Revision B:1963 | GRIP, WIRE, STRAND, WIRE ROPE AND CABLE |
| MIL-S-70334 Base Document:1987 | SHIM, SOLID GENERAL SPECIFICATION FOR |
| MIL-I-83751 Base Document:1967 | INDICATOR, SAFETY LEVEL, RF |
| MIL F 6001 : A | FITTING, AIRCRAFT, SOLDER TYPE TUBE |
| MIL-C-10464 Revision F:1990 | CANS, HERMETIC SEALING, METAL, LIGHT CAGE, TEAR-STRIP TYPE |
| MIL-A-25896 Revision E:1983 | ADAPTER, PRESSURE FUEL SERVICING, NOMINAL 2.5 INCH DIAMETER |
| 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 |
| MIL-S-3644 Revision B:1985 | SHAFT ASSEMBLY, FLEXIBLE |
| MIL R 83936 : B | REMOVER, PAINT, TANK TYPE, FOR AIRCRAFT WHEELS, LANDING GEAR COMPONENTS, AND OTHER AIRCRAFT AND AGE COMPONENTS |
| MIL-R-23057 Base Document:1961 | Regulator, Compressed Air, High Pressure (3500 PSI) |
| MIL-R-60897 Base Document:1968 | REMOVER, AIRCRAFT CANOPY, M8A1 METAL PARTS ASSEMBLY (CONVERSION) |
| MIL-G-23723 Base Document:1964 | Gyroscope, Rate Switching CN-495/AJB-3 |
| MIL-S-81771 Revision A:1975 | Seat System; Aircrew, Crash Resistant; General Specification for |
| MIL G 23701 : 0 | MILITARY SPECIFICATION GYROSCOPE, RATE SWITCHING AN/ASN-52 |
| MIL-C-8412 Revision B:1969 | COMPASS, MAGNETIC, SLAVED GYRO, TYPE J-4 |
| MIL-S-63302 Base Document:1979 | SAFETY AND ARMING ASSEMBLIES FOR MINES: M74 AND M75 |
| MIL-S-63326 Base Document:1981 | SAFETY AND ARMING ASSEMBLIES FOR MINES: BLU-91/B AND BLU-92/B |
| MIL-D-8181 Revision B:1965 | DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR |
| MIL I 6424 : A NOTICE 1 | INDICATOR, INDUCTION COMPASS, TYPE V 8 |
| MIL-B-5046 Revision D:1968 | BOARD, CHART PLOTTING MARK 7 [ASG] |
| P-C-444 Revision B:1983 | CLEANING COMPOUND, SOLVENT SOLUBLE, GREASE EMULSIFYING |
| MIL C 5015 : G | CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR |
| BS ISO 9758:2000 | Fork-ends, in corrosion-resistant steel, threaded, for rolling bearings, for aircraft control wire rope. Dimensions and loads |
| MIL-G-83380 Base Document:1979 | GENERATOR SET, GAS TURBINE ENGINE DRIVEN, 30 AND 60 KW, 400 HZ |
| MIL-E-85583 Revision A:1987 | ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR |
| BS ISO 9738:2000 | Turnbarrels, for aircraft control wire rope. Dimensions and loads |
| MIL-C-22542 Revision B:1987 | CLEANING COMPOUND, HIGH PRESSURE CLEANER, LIQUID |
| DOD C 83527 : 0 | CONNECTORS, PLUG AND RECEPTACLE, ELECTRICAL, RECTANGULAR MULTIPLE INSERT TYPE, RACK TO PANEL, ENVIRONMENT RESISTING, 150 DEGREES C - TOTAL CONTINUOUS OPERATING TEMPERATURE, GENERAL SPECIFICATION FOR |
| MIL-P-85034 Base Document:1976 | POWER PACKAGE, EMERGENCY AC/DC GENERATOR, RAM AIR TURBINE DRIVEN |
| NASA MSFC SPEC 384 : 1964 | LEAK TEST COMPOUND, LOX COMPATIBLE |
| MIL C 28748 : B | CONNECTOR, ELECTRICAL, RECTANGULAR, RACK AND PANEL, SOLDER TYPE AND CRIMP TYPE CONTACTS, GENERAL SPECIFICATION FOR |
| MIL-T-38306 Base Document:1964 | TRANSMITTER, RATE GYROSCOPE T 970/AJB - 7 |
| MIL-G-7817 Base Document:1951 | GAGE, FUEL QUANTITY, CAPACITOR TYPE, UNCOMPENSATED, GENERAL SPECIFICATION FOR |
| MIL F 22606 : C | FLASK COMPRESSED GAS AND END PLUGS FOR AIR, OXYGEN AND NITROGEN |
| MIL-DTL-81014 Revision B:2001 | HOOK, HELICOPTER EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C |
| MIL-PRF-29607 Base Document:1996 | CLEANING COMPOUND, AVIONICS COMPONENTS, NON-OZONE DEPLETING |
| MIL-D-83411 Revision A:1973 | DEICER/ANTI-ICER FLUID (FOR RUNWAYS AND TAXIWAYS) |
| MIL STD 194 : A NOTICE 2 | SYSTEM FOR PAINTING AND FINISHING FIRE-CONTROL MATERIEL |
| MIL-T-38760 Base Document:1966 | TENSIOMETER DIAL INDICATING |
| MIL C 25369 : C | CYLINDER, CARBON DIOXIDE, FOR INFLATION OF PNEUMATIC LIFE PRESERVERS |
| MIL-B-23072 Base Document:1961 | BLOWER, ANTI-EXPOSURE SUIT VENTILATION, GENERAL SPECIFICATION FOR |
| MIL-D-81227 Revision B:1976 | DETECTOR KIT, WATER, AUTOMOTIVE, AVIATION FUEL |
| MIL C 87937 : B | CLEANING COMPOUND, AEROSPACE EQUIPMENT |
| MIL-C-9075 Revision A:1968 | COMPUTER AND TRANSMITTER, TRUE AIRSPEED, PITOT STATIC, 150-900 KNOTS, TYPE MA 1 |
| MIL-F-51477 Base Document:1982 | FILTER, PARTICULATE, HIGH EFFICIENCY, FIRE RESISTANT, BIOLOGICAL USE, GENERAL SPECIFICATION FOR |
| MIL P 18722 : 0 | PYROMETERS, PORTABLE, HANDHELD. |
| MIL-R-7885 Revision D:1988 | RIVET, BLIND, STRUCTURAL, MECHANICALLY LOCKED SPINDLE AND FRICTION LOCKED SPINDLE, GENERAL SPECIFICATION FOR |
| MIL-C-52705 Revision B:1994 | COUPLING, HOSE STEAM |
| FF-S-88 Revision B:1977 | SCREW, EYE |
| GGG-S-00825 Revision A Interim Revision:1971 | SWAGING TOOL, FLEXIBLE CABLE TERMINAL |
| MIL-C-11218 Revision E:1988 | CONVEYORS, ROLLER AND WHEEL, GRAVITY AND CONVEYER SUPPORTS |
| MIL-S-24240 Base Document:1966 | SCREW, COLLAR, 12-POINT, EXTERNAL WRENCHING GENERAL SPECIFICATION FOR |
| MIL P 83206 : B | PITOT STATIC TUBE, L SHAPED, COMPENSATED, GENERAL SPECIFICATION FOR |
| MIL L 24047 : A | LIFE PRESERVER, YOKE TYPE, SCUBA, U.S. NAVY MARK 3 |
| MIL-A-22165 Base Document:1959 | Amplifier, Compass, Servo (Type MF-1 Compass) |
| MIL-T-8652 Revision A:1959 | TIEDOWN, CARGO, AIRCRAFT, 5,000 LB CAPACITY, TYPE MC 1 |
| MIL C 29602 : 0 | CLEANING COMPOUNDS, FOR PARTS WASHERS AND SPRAY CABINETS |
| MIL-I-21685 Base Document:1958 | INDICATOR, COMPASS REPEATER, ROTATING DIAL, TYPE MW-2 |
| MIL A 25676 : D | ADAPTOR, PRESSURE LUBRICATING OIL SERVICING, AIRCRAFT |
| MIL F 38363 : B (3) | FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-27261 Revision A:1966 | Accelerometer, Aircraft |
| NASM25027:2012 | NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F |
| DOD-W-63474 Revision B:1994 | WASHERS, SPRING TENSION, METRIC, GENERAL SPECIFICATION FOR |
| NASM 20615 : 2003 | RIVET, SOLID, UNIVERSAL HEAD, BRASS, COPPER, NICKEL-COPPER ALLOY |
| ISO 9758:2000 | Aerospace — Fork-ends, in steel, threaded, for rolling bearings, for aircraft control wire rope — Dimensions and loads |
| NASM20995:2012 | WIRE, SAFETY OR LOCK |
| ASTM F 1387 : 1999 : R2005 | Standard Specification for Performance of Piping and Tubing Mechanically Attached Fittings |
| MS75009 Revision J:2005 | Bracket Assembly, Resistor (Power Type) |
| MIL-DTL-18240 Revision F:1997 | FASTENER ELEMENT, SELF-LOCKING, THREADED FASTENER, 250 DEGREES F MAXIMUM |
| MIL-DTL-85097 Revision E:2000 | USN/USMC PROPELLANT ACTUATED DEVICES (PADS) - GENERAL SPECIFICATION FOR |
| MIL-PRF-81733 Revision D:1998 | SEALING AND COATING COMPOUND, CORROSION INHIBITIVE |
| MIL-B-81934 Revision B:1991 | BEARING, SLEEVE, PLAIN AND FLANGED, SELF LUBRICATING |
| MIL-R-81294 Revision D:1990 | REMOVER, PAINT, EPOXY, POLYSULPHIDE AND POLYURETHANE SYSTEMS |
| DOD-I-63276 Revision A:1983 | INSERT, SCREW THREAD, LOCKED IN, RING LOCKED, SERRATED, METRIC AND RING LOCK SERRATED METRIC |
| MIL C 83383 : C | CIRCUIT BREAKER, REMOTE CONTROL THERMAL, TRIP FREE, GENERAL SPECIFICATION FOR |
| AA-C-001770 Revision A Interim Revision:1978 | CABINET, WARDROBE AND STORAGE, CONTEMPORARY STYLE, STEEL, GENERAL OFFICE |
| MIL S 4510 : E | SPOTLIGHT, INCANDESCENT, ROOF MOUNTED, AUTOMOTIVE |
| MIL-F-8378 Revision B:1975 | FREQUENCY METERS, AIRCRAFT 380 TO 420 HERTZ AND 350 TO 450 HERTZ |
| AA-D-001923 Base Document:1975 | DESK ATTACHMENTS, L, RETURN PLATFORM, CONTEMPORARY STYLE |
| MIL-F-8615 Revision D:1976 | FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
| MIL-S-21433 Revision A:1959 | SOCKETS, TURNBUCKLES, AND TURNBUCKLE ASSEMBLIES - WIRE ROPE, WEDGE AND THREADED LOCK SLEEVE |
| MIL C 17850 : A | COMPASS MAGNETIC, CARD, POCKET, TYPE MC-1 |
| MIL-W-48271 Revision A:1984 | WARHEAD METAL PARTS ASSEMBLY M251 PARTS AND ASSEMBLING |
| BS ISO 9757:2000 | Fork-ends, in corrosion-resistant steel, threaded, for aircraft control wire rope turnbarrels. Dimensions and loads |
| MIL-I-21718 Base Document:1958 | Indicator, Airspeed, Pitot Static, Maximum Allowable Speed, 40-400 Knots |
| MIL-DTL-27426 Revision C:1998 | RINGS, RETAINING, SPIRAL (UNIFORM CROSS SECTION) |
| MIL-S-21277 Revision A:1958 | SWITCH, LIQUID LEVEL, GENERAL SPECIFICATION FOR |
| MIL-B-7949 Revision E:1981 | BEARING, BALL, AIRFRAME, ANTIFRICTION |
| MIL-S-29398 Revision C:1984 | SLING SYSTEM, HELICOPTER EXTERNAL CARGO 40,000 POUND CAPACITY |
| MIL-R-29583 Base Document:1992 | RADIO SET |
| MIL T 83174 : B (3) | TRANSMITTER, ACCELEROMETER, AXIAL |
| RR-S-001301 Base Document:1967 | SAFETY EQUIPMENT, CLIMBING |
| NASM 21209 : 2003 | INSERT, SCREW THREAD, COARSE AND FINE, SCREW LOCKING, HELICAL COIL, CRES |
| MIL W 12133 : D | WASHER, SPRING TENSION GENERAL SPECIFICATION FOR |
| MIL H 13444 : E | HOSE & HOSE ASSEMBLIES, RUBBER: FUEL AND OIL |
| MIL-A-85672 Base Document:1987 | AMPLIFIER, RADIO FREQUENCY AM-7177A/ARC |
| MIL-G-26988 Revision C:1971 | GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
| MIL-C-22249 Revision B:1989 | CONNECTOR SET, ELECTRICAL, HERMETICALLY SEALED, SUBMARINE |
| MIL-W-18326 Revision A:1956 | WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR |
| MIL N 45913 : B | NUTS, SELF LOCKING, HEXAGON, PREVAILING-TORQUE |
| SAE AS 5604 : 2012 | COMPASS: MAGNETIC, PILOT'S STANDBY |
| MIL-R-81903 Revision A:1977 | REMOVER, ACID ACTIVATED, FOR AMINE CURED EPOXY COATING SYSTEMS |
| AA-D-001918 Base Document:1975 | DESK, FLAT TOP, STEEL, CONTEMPORARY STYLE |
| MIL-I-27680 Revision C:1973 | INDICATOR, ATTITUDE, ARU-12/A, REMOTE |
| SAE AS 85075 : 2000 | TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR |
| MIL-S-22783 Revision C:1972 | SEALING MACHINES, ELECTRICAL IMPULSE (JAW TYPE) |
| MIL C 83527 : A | |
| MIL C 23216 : C | CONTACTS, ELECTRIC CONNECTOR, GENERAL SPECIFICATION FOR |
| MIL-R-81835 Base Document:1971 | REMOVER, ORGANIC COATING, HOT TANK TYPE |
| MIL-S-7877 Revision B:1956 | Seat, Passenger, Cabin Folding |
| MIL C 22992 : E | CONNECTOR, PLUGS AND RECEPTACLES, ELECTRICAL, WATERPROOF, QUICK DISCONNECT, HEAVY DUTY TYPE GENERAL SPECIFICATION FOR |
| MIL-P-11268 Revision L:1983 | PART, MATERIALS, AND PROCESSES USED IN ELECTRONIC EQUIPMENT |
| MIL-I-27623 Revision C:1972 | INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
| MIL C 52404 : B | CONNECTIONS: HOSE, FIRE AND WATER |
| MIL L 25567 : D | LEAK DETECTION COMPOUND, OXYGEN SYSTEMS (METRIC) |
| MIL-I-83117 Revision B:1975 | INDICATOR, ANGLE OF ATTACK |
| MIL-P-85315 Base Document:1979 | Pump, Ejector, Air Vehicle Fuel, General Specification For |
| MIL-C-14039 Revision C:1981 | COMPASS, SUN, UNIVERSAL TYPE 0 TO 90 DEGREES, NORTH AND SOUTH LATITUDES, WITH CARRYING CASE |
| MIL I 45916 : B | INSERT,SCREW THREAD - THREAD CUTTING AND THREAD FORMING |
| MIL-F-40048 Revision C:1984 | FLAGSTAFFS AND INSIGNIA, FLAGSTAFF HEADS, GENERAL SPECIFICATION FOR |
| MIL-R-14368 Revision C:1974 | REGULATOR ASSEMBLY, RELAY ASSEMBLY, AND VOLTAGE REGULATOR ASSEMBLY: 24-VOLT (NOMINAL RATING), 100 TO 400 AMPERE, DIRECT CURRENT |
| FF-S-111 Revision D:1974 | SCREW, WOOD |
| MIL-B-55252 Revision B:1992 | BATTERIES, NON-RECHARGEABLE, MAGNESIUM |
| MIL-G-27693 Revision A:1962 | GYROSCOPE, DISPLACEMENT SBU-6/A, ROLL AND PITCH |
| MIL-I-25645 Revision D:1970 | INDICATOR, LIQUID OXYGEN QUANTITY, CAPACITANCE TYPE, GENERAL SPECIFICATION FOR |
| MIL-N-25161 Revision C:1969 | NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
| MIL-G-5678 Revision C:1964 | GAGE PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE |
| MIL G 5413 : D NOTICE 1 | GENERATOR, TACHOMETER, FOUR POLE |
| MIL-F-5504 Revision B:1958 | Filters and Filter Elements, Fluid Pressure, Hydraulic Micronic Type |
| MIL-I-38258 Base Document:1965 | INDICATOR, ATTITUDE ARU 18/A DIRECTOR |
| MIL-A-27671 Revision B:1965 | AMPLIFIER-INDICATOR GROUP, ALTITUDE VERTICAL SPEED A/A24G-11 |
| MIL G 24211 : 0 | GASKET, WAVEGUIDE FLANGE, GENERAL SPECIFICATION FOR |
| MIL-H-9859 Revision A:1968 | HANDWHEEL, ORDNANCE |
| MIL-B-8976 Base Document:1969 | BEARINGS, PLAIN, SELF-ALIGNING, ALL METAL |
| MIL M 62361 : C | MOTOR, DRIVE, DIRECT CURRENT 2 RPM/8RPM |
| DOD-N-63548 Base Document:1982 | NUT, PLAIN, HEXAGON, WHEEL MOUNTING, METRIC, GENERAL SPECIFICATION FOR |
| MIL-I-27619 Revision G:1974 | INDICATORS, ATTITUDE DIRECTOR |
| MIL-M-7969 Revision C:1965 | Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for |
| MIL I 27851 : B | INDICATOR, INDICATED AIRSPEED AVU-17/A |
| MIL A 25949 : E (2) | ACCELEROMETER, AIRCRAFT RANGE -5 TO PLUS 1OG UNITS, INTEGRALLY LIGHTED |
| DOD-P-63478 Base Document:1981 | PIN, STRAIGHT, HEADLESS (DOWEL), GENERAL SPECIFICATION FOR, METRIC |
| MIL-A-58066 Revision A:1966 | ALTIMETER, PRESSURE, PARACHUTIST'S |
| MIL R 70337 : 0 | RING, RETAINING, ROUND SECTION GENERAL SPECIFICATION FOR |
| MIL M 62368 : A | MOTOR, GEARHEAD, 18-30 VOLTS, DIRECT CURRENT |
| MIL-F-51068 Revision F:1986 | FILTERS, PARTICULATE (HIGH-EFFICIENCY FIRE RESISTANT) |
| SAE AS6011 : 1999 | CYLINDERS, CARBON DIOXIDE FILLED, TECHNICAL |
| MIL L 25866 : B | LIGHT, EMERGENCY EXIT, AIRCRAFT LEU AND 1-A |
| MIL-B-3990 Revision D:1980 | BEARINGS, ROLLER, NEEDLE, AIRFRAME, ANTIFRICTION, INCH |
| MIL-I-23524 Revision A:1986 | INDICATOR, ATTITUDE DIRECTOR, REMOTE, ID 1329A (V) |
| MIL-S-10521 Revision K:1983 | SIMULATOR, BOOBY TRAP, FLASH, M117 PARTS FOR AND LOADING ASSEMBLING AND PACKING |
| MIL C 22442/32 : A | CABLE ASSEMBLY, RADIO FREQUENCY (AIRCRAFT AUDIO), ASSOCIATED PARTS |
| ISO 9736:2000 | Aerospace — Eye-ends, in steel, threaded, for aircraft control wire rope — Dimensions and loads |
| MS24466 Revision K:1998 | BEARING, ROLLER, NEEDLE DOUBLE ROW, HEAVY DUTY, TRACK ROLLER, TYPE 6, ANTIFRICTION, INCH |
| DOD-C-85050 Base Document:1982 | CHARGERS, BATTERY, NICKEL-CADMIUM, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-I-81049 Revision A:1972 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
| MIL G 9398 : C | GENERATOR, TACHOMETER, TWO POLE HIGH TEMPERATURE AIRCRAFT |
| MIL-D-38134 Revision A:1971 | DETECTOR, MAGNETIC AZIMUTH DSU-4/A, HIGH TEMPERATURE |
| DOD-P-63464 Revision A:1982 | PIN, GROOVED, HEADLESS-LONGITUDINAL GROOVE, METRIC, GENERAL SPECIFICATION FOR |
| MIL-H-29144 Revision B:1985 | HOOD, FIREMANS,ALUMINIZED, PROXIMITY |
| MIL-S-5733 Revision B:1952 | SOLENOID, FUSE ARMING, TYPE F AND 1 |
| MIL C 38333 : 0 | CONTROLLER, COMPASS SYSTEM C-6448/ASN-55 |
| MIL-E-6719 Revision A:1972 | ELBOW; ELECTRICAL CONDUIT |
| MIL-I-7906 Revision A:1961 | INDICATOR, GYRO HORIZON, MANUALLY CAGED, ELECTRIC, TYPE MB 1 |
| MIL-H-81324 Base Document:1966 | HONING MACHINE, DRY PORTABLE |
| MIL C 25955 : 0 | CONNECTOR, ELECTRICAL, ENVIRONMENT RESISTING MINIATURE, WITH SNAP-IN CONTACTS |
| MIL-B-8621 Revision A:1964 | Board, Chart, Mark 6A, Mark 6B and Mark 6C |
| KKK-T-728 Revision A:1973 | TRUCK, HAND, TWO-WHEELED (LIGHT DUTY) 300 POUND CAPACITY |
| MIL C 85570 : B (1) | CLEANING COMPOUND, AIRCRAFT, EXTERIOR |
| MIL-N-3337 Revision C:1985 | NUT, SHEET SPRING |
| MIL-DTL-26517 Revision B:2000 | Power Supply, Transformer-Rectifier, Aircraft, General Specification for |
| MIL-C-5191 Revision B:1953 | COMPUTER AND TRANSMITTER, TRUE AIRSPEED PITOT STATIC, TYPE A-2 |
| MIL M 5388 : B | MACHMETER; PITOT STATIC OPERATED, RANGE 0.5 TO 1.5, TYPE A-2B |
| MIL-F-25173 Revision A:1956 | FASTENER, CONTROL PANEL, AIRCRAFT EQUIPMENT |
| MIL-R-24243 Revision C:1987 | RIVET, BLIND, NON-STRUCTURAL, RETAINED MANDREL, GENERAL SPECIFICATION FOR |
| MIL-S-10555 Revision H:1975 | SIMULATOR, BOOBY TRAP ILLUMINATING M 118 PARTS FOR, AND LOADING ASSEMBLING AND PACKING |
| MIL-R-11050 Revision B:1969 | RECTIFIER, METALLIC, SELENIUM |
| MIL-W-5013 Revision L:1991 | WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL F 14072 : D | FINISHES FOR GROUND BASED ELECTRONIC EQUIPMENT |
| SAE AS 8660 : 1999 | SILICONE COMPOUND NATO CODE NUMBER S-736 |
| MIL R 3390 : F | RINGS, DEE |
| MIL T 25627 : C | TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |
| ASTM D 5363 : 2016 : REDLINE | Standard Specification for Anaerobic Single-Component Adhesives (AN) |
| MIL-A-27391 Revision B:1963 | ALTIMETER, PRESSURE AAU-2A |
| ASTM B 766 : 1986 : R2008 | Standard Specification for Electrodeposited Coatings of Cadmium |
| MIL-B-55679 Base Document:1969 | BATTERY, DRY (SPECIAL PURPOSE) |
| NASM21250:2013 | BOLT, TENSION, STEEL, EXTERNAL WRENCHING, FLANGED, 12-POINT, 180 KSI FTU, 450 DEGREES F |
| SAE AMS R 81835 : 2008 | REMOVER, ORGANIC COATING, HOT TANK TYPE |
| MIL-C-81562 Revision B:1983 | COATING, CADMIUM, TIN CADMIUM AND ZINC (MECHANICALLY DEPOSITED) |
| MIL S 5002 : D | SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
| MIL-STD-1312-1 Base Document:1984 | FASTENER TEST METHODS - METHOD 1, SALT SPRAY |
| ASTM B 567 : 1998 | Standard Test Method for Measurement of Coating Thickness by the Beta Backscatter Method |
| MIL-STD-1312-5 Revision A:1984 | FASTENER TEST METHODS, METHOD 5, STRESS DURABILITY |
| MIL-S-5000 Revision E:1982 | STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS AND REFORGING STOCK |
| MIL-STD-1312-12 Base Document:1985 | FASTENER TEST METHODS, METHOD 12, THICKNESS OF METALLIC COATINGS |
| ASTM E 8 : 2004 | Standard Test Methods for Tension Testing of Metallic Materials |
| MIL-S-8844 Revision D:1987 | STEEL BAR, REFORGING STOCK AND MECHANICAL TUBING LOW ALLOY PREMIUM QUALITY |
| MIL-STD-105 Revision E:1989 | SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES |
| TT-C-490 Revision F:2013 | CHEMICAL CONVERSION COATINGS AND PRETREATMENTS FOR METALLIC SUBSTRATES (BASE FOR ORGANIC COATINGS) |
| MIL-STD-1312-14 Base Document:1987 | FASTENER TEST METHODS, METHOD 14, STRESS DUPABILITY INTERNALLY THREADED FASTENERS |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.