MIL A 8625 : F
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
Available format(s)
PDF
Superseded date
13-03-2021
Published date
10-09-1993
Publisher
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES
Describes the requirements for six types and two classes of electrolytically formed anodic coatings on aluminum and aluminum alloys for non-architectural applications.
| Committee |
AREA MFFP
|
| DevelopmentNote |
Supersedes SAE AMS A 8625 (10/2003)
|
| DocumentType |
Standard
|
| Pages |
23
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| SAE AMS 2471 : 2014 | Similar to |
| SAE AMS 2472 : 2014 | Similar to |
| SAE AMS 2469 : 2014 | Similar to |
| SAE AMS 2470 : 2013 | Similar to |
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| MIL T 27252 : A | TEST SET, SYNCHRO, TTU-73/E DC SELSYN, AIRCRAFT INSTRUMENTS |
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| MIL-DTL-5815-1 Revision B:2013 | Antenna, Blade, UHF, AT-256A/ARC (Series N Connector) |
| MIL-I-7721 Revision D:1992 | INDICATOR, VERTICAL SPEED, 3-INCH |
| MIL-I-38121 Revision C:1989 | INDICATOR, PRESSURE, EGU-9/A |
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| MIL-A-8243 Revision D:1985 | ANTI-ICING AND DEICING-DEFROSTING FLUIDS |
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| MIL C 38214 : B | COMPASS, MAGNETIC,MOUNTED |
| MIL-I-81969 Revision B:1982 | INSTALLING AND REMOVAL TOOLS, CONNECTOR ELECTRICAL CONTACT, GENERAL SPECIFICATION FOR |
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| AN815 Revision 10:2015 | UNION - FLARED TUBE |
| MIL-T-38473 Revision A:1972 | TIMER, PRECISION, BOMBING, 0 - 30 MINUTES |
| MIL-C-8605 Revision B:1990 | CAP, PRESSURE FUEL SERVICING |
| MIL-A-38140 Revision B:1977 | ALTIMETER, PRESSURE AAU-16/A |
| MIL-DTL-52525-40 Revision B:2008 | FITTINGS, HOSE, CRIMP TYPE, SPLIT-FLANGE, STRAIGHT |
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| 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 |
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| MIL-V-82466 Base Document:1967 | VACUUM-AIR-NITROGEN DISTRIBUTION SYSTEM |
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| MIL-F-22735 Revision C:1980 | FILM, ELASTOMERIC, FLUORESCENT, FOR WEAPONS SYSTEMS |
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| MIL-A-55503 Base Document:1966 | ATTITUDE HEADING REFERENCE SET AN/ASN-76 |
| MIL T 8878 : D | TURNBUCKLE, POSITIVE SAFETYING |
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| MIL-DTL-52525-36 Revision B:2008 | FITTINGS, HOSE, CRIMP TYPE, SPLIT-FLANGE, 90 DEGREES BENT TUBE |
| MIL-A-38267 Revision A:1971 | APPLICATION OF POLYURETHANE FUEL TANK COATINGS |
| MIL V 85855 : 0 | VALVE, QUICK DISCONNECT, FOR THE PROTECTIVE ASSEMBLY, CHEMICAL, RADIOLOGICAL |
| MS9095 Revision B:2010 | NIPPLE, TUBE - ALUMINUM, BOSS |
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| MIL R 87978 : LATEST | REMOVER, PAINT, EPOXY AND POLYURETHANE SYSTEMS, TANK TYPE: AMBIENT TEMPERATURE, FOR AIRCRAFT WHEELS AND LANDING GEAR COMPONENTS |
| GG D 475 : A | DIVIDER, SPACING, EQUAL |
| MIL-I-27196 Revision C:1988 | INDICATOR, VERTICAL VELOCITY AAU-9/A, INTEGRALLY LIGHTED |
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| MIL-L-19537 Revision C:1965 | LACQUER, ACRYLIC NITROCELLULOSE GLOSS (FOR AIRCRAFT USE) |
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| MIL-STD-2088 Revision B:2007 | BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT |
| MIL-A-23121 Revision C:1970 | AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR |
| 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-U-3963 Revision A:1958 | UNIVERSAL JOINT, ANTIFRICTION BEARINGS |
| MIL-DTL-29563 Revision B:2014 | Antenna System, Aims Shipboard, Electronically Steered OE-120/UPX |
| MIL H 25579 : E | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL-DTL-27272 Revision D:2015 | Fittings, Polytetrafluoroethylene Hose, High-Temperature, Medium-Pressure, General Specification for |
| MIL-F-5591 Revision C:1986 | FASTENERS, PANEL, NONSTRUCTURAL |
| MS27291 Revision H:2015 | SUPPORT, CABLE, ELECTRICAL CONNECTOR, FOR MIL-DTL-26500 |
| MS3186 Revision G:2011 | CONNECTOR, MOUNTING TO CONNECTORS, MOUNTING NUTS, PLAIN HEXAGON |
| MIL-S-45909 Revision C:1989 | STUD, LOCKED IN - RING LOCKED SERRATED |
| MS27559 Revision E:2009 | SUPPORT, CABLE, RIGHT ANGLE |
| MIL-DTL-14072 Revision F:2013 | FINISHES FOR GROUND BASED ELECTRONIC EQUIPMENT |
| 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-G-16491 Revision F:1989 | GROMMET, METALLIC |
| MIL-DTL-25531 Revision F:2013 | Coupling Half, Quick Disconnect, Pneumatic Starter, External, Low Pressure |
| MIL-HDBK-2193 Base Document:1994 | HYDRAULIC SYSTEM COMPONENTS, SHIP |
| 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 |
| MS27558 Revision E:2009 | SUPPORT, CABLE, RIGHT ANGLE, CLOSED |
| MIL-S-7839 Revision B:1973 | SCREW, STRUCTURAL, AIRCRAFT |
| MIL F 83798 : B | FITTING, RUBBER HOSE, LIGHTWEIGHT MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
| MIL S 22885 : E | SWITCH, PUSH BUTTON, ILLUMINATED, GENERAL SPECIFICATION FOR |
| 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 |
| MIL-DTL-28754-62 Revision A:2016 | CONNECTORS, ELECTRICAL, MODULAR, TYPE 4, CONNECTOR, 100 PIN, CENTER, CROSSOVER, CONTACT TAILS ON .050 CENTERS |
| MIL-DTL-28748 Revision D:2001 | CONNECTOR, PLUG AND RECEPTACLE, RECTANGULAR, RACK AND PANEL SOLDER TYPE AND CRIMP TYPE CONTACTS - GENERAL SPECIFICATION FOR |
| MIL-H-8775 Revision D:1976 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
| MIL-STD-1353 Revision C:2014 | ELECTRICAL CONNECTORS, PLUG-IN SOCKETS AND ASSOCIATED HARDWARE, SELECTION AND USE OF |
| MIL-DTL-917 Revision F:2014 | ELECTRIC POWER EQUIPMENT, BASIC REQUIREMENTS FOR |
| MIL-DTL-5523 Revision E:2011 | VALVE; RELIEF, HYDRAULIC PRESSURE |
| MIL T 28800 : E | TEST EQUIPMENT FOR USE WITH ELECTRICAL AND ELECTRONIC EQUIPMENT GENERAL SPECIFICATION FOR |
| MIL-C-5501 Revision G:1989 | CAP AND PLUG, PROTECTIVE, DUST AND MOISTURE SEAL |
| MIL-A-82175 Base Document:1968 | ARMOR, BODY, FRAGMENTATION, PROTECTIVE: FOOTWEAR |
| MIL-C-6818 Revision D:1973 | CLAMP, INSTRUMENT MOUNTING AIRCRAFT |
| MIL-DTL-25027 Revision H:1997 | NUT, SELF-LOCKING, 250 DEG F, 450 DEG F, AND 850 DEG F |
| MIL-DTL-28827 Revision C:2011 | SWITCHES, THERMOSTATIC, (VOLATILE LIQUID), HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
| MIL-DTL-45913 Revision D:2011 | NUTS, SELF-LOCKING, HEXAGON, PREVAILING TORQUE |
| FF-S-85 Revision D:2005 | Screw, Cap, Slotted and Hexagon Head |
| MIL-N-52110 Revision F:1982 | NOZZLE, FUEL & OIL SERVICING, NONAUTOMATIC SHUTOFF & NOZZLES, FUEL SERVICING AUTOMATIC SHUTOFF |
| MIL S 3786 : F | SWITCH, ROTARY, CLOSED CONSTRUCTION, 2 AMPERES, LOW LEVEL, POSITIVE SHAFT GROUNDING STYLE SR04 |
| MIL-T-83965 Revision B:1990 | TRUCK, FIRE FIGHTING, A/S32P-10, FORCIBLE ENTRY |
| MIL-DTL-5099 Revision C:2011 | INDICATOR, CABIN AIR PRESSURE, 1-7/8 INCH DIAL, TYPE MA-1 |
| MIL-DTL-28754-6 Revision D:2014 | CONNECTORS, ELECTRICAL, MODULAR, TYPE 4, 40 PIN, STRAIGHT THROUGH |
| 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 |
| MIL-DTL-22263 Revision C:2009 | Coupling Fuel Line, Flexible, 125 PSI General Specification for |
| MIL-G-81559 Revision C:1984 | Gyroscope Assemblies and Attitude and Directional Reference Instruments for Aircraft, Packaging of |
| MIL-DTL-28754-97 Revision A:2015 | CONNECTORS, ELECTRICAL, MODULAR, TYPE 4, CONNECTOR, 150 CONTACT, RIGHT ANGLE, CONTACT TAILS ON 0.100 CENTERS |
| MIL-R-27384 Revision B:1970 | RIVET, BLIND, DRIVE TYPE |
| MIL-DTL-9395 Revision K:2016 | Switches, Pressure (Absolute, Gage and Differential) General Specification for |
| MIL-DTL-25579 Revision H:2014 | Hose Assembly, Polytetrafluoroethylene, High Temperature, Medium Pressure, General Specification for |
| MIL V 5523 : D | VALVE, RELIEF, HYDRAULIC PRESSURE |
| MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
| A-A-59590 Revision D:2014 | HOLDER, ELECTRICAL CARD, WEDGE RETAINERS, 3 PIECE, FOR COLD PLATE APPLICATIONS, GENERAL REQUIREMENTS FOR |
| MIL-DTL-28748-17 Revision B:2016 | CONNECTORS, ELECTRICAL, RECTANGULAR, RACK AND PANEL, HARDWARE FOR |
| MIL DTL 28754/60 : A | CONNECTORS, ELECTRICAL, MODULAR, TYPE 4, CONNECTOR, 100 PIN, CENTER CONTACT TAILS ON .100 CENTERS |
| MIL-R-5674 Revision F:1994 | RIVETS, STRUCTURAL, ALUMINIUM ALLOY, TITANIUM COLUMBIUM ALLOY GENERAL SPECIFICATION FOR |
| MIL-D-23615 Revision C:1993 | DESIGN AND EVALUATION OF CARTRIDGE ACTUATED DEVICES |
| MIL-DTL-28754-11 Revision F:2014 | Connectors, Electrical, Modular, Type IV, 40 Contact, Right Angle (for Solid or Dip Frame) |
| MIL-DTL-6162 Revision C:2000 | GENERATORS AND STARTER-GENERATORS, ELECTRICAL DIRECT CURRENT, NOMINAL 30 VOLTS, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL-DTL-28754-59 Revision A:2016 | CONNECTORS, ELECTRICAL, MODULAR, TYPE 4, CONNECTOR, 100 PIN, CENTER CONTACT TAILS ON .100 CENTERS (CERAMIC COMPATIBLE) |
| MIL-DTL-25707-1 Revision C:2011 | ANTENNA, FLUSH MOUNT TYPE AT-740/A |
| SAE AS 4468 G : 2017 | HOSE ASSEMBLY, 125 PSI, LINED SILICONE, POTABLE WATER, PROCUREMENT SPECIFICATION |
| A-A-59789 Revision B:2014 | HOLDER, ELECTRICAL CARD, WEDGE RETAINERS, 5 PIECE, FOR COLD PLATE APPLICATIONS, GENERAL REQUIREMENTS FOR |
| MIL-R-85880 Base Document:1988 | ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL-DTL-24317 Revision B:2010 | SWITCHES, MULTISTATION, PUSHBUTTON, ILLUMINATED AND NON-ILLUMINATED), GENERAL SPECIFICATION FOR |
| SAE AS 4841 : 2017 | FITTINGS, 37 DEGREES INTERNAL FLARE, FLUID CONNECTION, PROCUREMENT SPECIFICATION |
| MIL-C-85829 Base Document:1989 | COUPLING ASSEMBLY, HOSE, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE |
| MIL V 7891 : E | VALVE, OXYGEN FILLER, LOW AND PRESSURE |
| SAE AMS C 19853 : 1998 | CARBON REMOVING COMPOUND (FOR USE IN AGITATED TANK) |
| MS27082 Revision E:2014 | ELBOW, NIPPLE END, SWIVEL FLANGE TO HOSE - 90 DEGREES |
| MIL-S-8802 Revision F:1990 | SEALING COMPOUND, TEMPERATURE-RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES, HIGH ADHESION |
| 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 |
| A-A-2653 Base Document:1992 | BINDER, NOTE PAD, SPRING-BACK |
| DEFSTAN 00-77(PT1)/1(2005) : INTERIM | ASAAC STANDARDS - PART 1: PROPOSED STANDARDS FOR PACKAGING |
| MIL-G-19053 Revision C:1957 | GAGE - AIRCRAFT, CAPACITANCE, LIQUID OXYGEN CONVERTER, GENERAL SPECIFICATION FOR |
| MIL C 60982 : B | CASE, CARTRIDGE, 40MM, M169 PART FOR |
| AN841 Revision 7:2013 | ADAPTER - HOSE TO FLARED TUBE |
| MIL-DTL-24800 Base Document:1996 | CLEANING COMPOUND - AQUEOUS - OXYGEN SYSTEMS COMPONENTS |
| 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 |
| MIL-C-81945 Revision B:1989 | COATING COMPOUND, WEAPON INSULATION, INTUMESCENT |
| MIL L 46147 : B | LUBRICANT, SOLID FILM, AIR CURED (CORROSION INHIBITING) |
| MIL-C-83231 Revision A:1981 | COATING, POLYURETHANE, RAIN EROSION RESISTANT FOR EXTERIOR AIRCRAFT AND MISSILE PLASTIC PARTS |
| MIL-P-21600 Revision A:1962 | PAINT SYSTEM, FLUORESCENT, REMOVABLE, FOR AIRCRAFT APPLICATION |
| MIL R 23016 : A | RADIO SET AN/ARC-94 |
| SAE AS 4444 : 2013 | FITTINGS, 24 DEGREE CONE FLARELESS, FLUID CONNECTION, 5000 PSI |
| MIL-DTL-83796-6 Revision D:2014 | HOSE ASSEMBLY, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, FIELD ATTACHABLE END FITTINGS, FLARE TO FLANGE, WITH LOCKWIRE HOLE |
| MIL-STD-2156 Base Document:1983 | LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| MIL F 83870 : A | FILTER ELEMENT, FLUID PRESSURE, TRANSMISSION, AIRCRAFT DISPOSABLE, 20 MICRON ABSOLUTE |
| SAE AS 81934 : 2016 | BEARINGS, SLEEVE, PLAIN AND FLANGED, SELF-LUBRICATING |
| MIL-T-38049 Revision A:1972 | TRANSMITTER, PRESSURE TRU 60A |
| MIL-C-60872 Revision A:1992 | CARTRIDGE, DELAY, XM271, ASSEMBLY |
| MIL-DTL-83796-14 Revision A:2010 | Hose Assembly, Rubber, Lightweight, Medium Pressure, Internal Support Coil, Field Attachable End Fittings, Flare to Flange |
| MIL-DTL-25427 Revision B:2009 | COUPLING ASSEMBLY, HYDRAULIC, SELF SEALING, QUICK DISCONNECT, GENERAL SPECIFICATION FOR |
| A-A-59432 Revision B:2015 | PLUGS, PIPE, MAGNETIC, HEADLESS: IRON, STEEL OR ALUMINUM ALLOY |
| MS27061 Revision D:2013 | Nipple Subassembly, Flared, Straight - with Swivel Nut |
| MIL-C-7413 Revision B:1970 | COUPLING, QUICK DISCONNECT, AUTOMATIC SHUTOFF, GENERAL SPECIFICATION FOR |
| MIL-C-60643 Revision A:1992 | CARTRIDGE, IMPULSE, M127 ASSEMBLY |
| 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-DTL-26518 Revision C:2000 | CONNECTORS, ELECTRICAL, MINIATURE, RACK AND PANEL, ENVIRONMENT RESISTANT, 200 DEGREES C AMBIENT TEMPERATURE - GENERAL SPECIFICATION FOR |
| MIL-DTL-28754-22 Revision H:2014 | Connectors, Electrical, Modular, Frame, Casting, Type IV, Single Span |
| A-A-59950 Base Document:2014 | HOLDER, ELECTRICAL CARD, WEDGE RETAINERS, 7 BODY, FOR COLD PLATE APPLICATIONS, GENERAL REQUIREMENTS FOR |
| MIL-T-22913 Revision C:1971 | TIMER (FOR TORPEDO MARK 37 MOD 2) |
| MIL-T-62032 Revision H:1991 | TRUCK, TANK, FUEL SERVICING, AND AIRCRAFT FUEL SERVICING, 1,000 - 4,000 GALLON, DIESEL & GASOLINE ENGINE DRIVEN, 16,000 GVW, 4X2, 4X4. 6 X 4 & 6X6 COMMERCIAL |
| MIL-C-85049 Revision A:1990 | CONNECTOR ACCESSORIES, ELECTRICAL GENERAL SPECIFICATION FOR |
| MIL C 60945 : B | CARTRIDGE, 40MM, PRACTICE, M385A1 DUMMY CARTRIDGE, 40MM HIGH VELOCITY, M922 PROJECTILE PARTS FOR |
| MIL-DTL-83798-5 Revision E:2017 | Fittings, Rubber Hose, Lightweight, Medium Pressure, Flareless, Swivel Nut, 45 Degrees |
| MIL-P-21415 Revision C:1973 | PROTECTIVE FINISH AND PAINTING FOR POLARIS FLEET BALLISTIC MISSILE |
| MIL C 46241 : F | CARTRIDGE, AIRCRAFT EJECTION SEAT, CATAPULT, M36 |
| MIL-HDBK-510 Revision A:2014 | AEROSPACE FUELS CERTIFICATION |
| MIL-C-83124 Base Document:1969 | CARTRIDGE ACTUATED DEVICES PROPELLANT ACTUATED DEVICES GENERAL DESIGN SPECIFICATION FOR |
| MIL-A-19736 Revision A:1960 | AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-E-50796 Base Document:1973 | EXPANDING SHIELDED MILD DETONATING CORD ASSEMBLY |
| MIL-T-52983 Revision G:1994 | TANK, FABRIC, COLLAPSIBLE, 3,000 10,000 20,000 AND 50,000 GALLON, FUEL |
| MIL-C-83445 Revision A:1980 | COATING SYSTEM, POLYURETHANE, NON-YELLOWING WHITE, RAIN EROSION RESISTANT, THERMALLY REFLECTIVE |
| MIL-STD-1250 Revision A:1992 | CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
| SAE AS 1969 : 2013 | COUPLING ASSEMBLY, SELF-HEALING, QUICK DISCONNECT FUEL AND OIL SYSTEM COMPONENTS |
| AN842 Revision 13:2013 | ELBOW - PIPE TO HOSE, 90 DEGREES |
| MIL C 7958 : A | CONTROL, PUSH PULL, FLEXIBLE AND RIGID |
| BS ISO 7169:2014 | Aerospace. Separable tube fittings for fluid systems, for 24° cones, for pressures up to 3 000 psi or 21 000 kPa. Procurement specification, inch/metric |
| FF-B-575 Revision C:1970 | BOLTS, HEXAGON AND SQUARE |
| MIL-B-42079 Base Document:1994 | BRACE ASSEMBLY ADJUSTABLE BED |
| MIL-C-87936 Revision A:1985 | CLEANING COMPOUNDS, AIRCRAFT EXTERIOR SURFACES, WATER DILUTABLE |
| GG-S-161 Revision D:1985 | SCALES, DRAFTING, AND SCALES, PLOTTING (GENERAL SPECIFICATION) |
| 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-25091 Revision B:1985 | INDICATOR, CABIN AIR PRESSURE, PRESSURIZED AIRCRAFT, 1-7/8 INCH DIAL, TYPE MA-2 |
| MIL-P-5994 Revision D:1972 | PUMP, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY, GENERAL SPECIFICATION FOR |
| MIL R 83178 : A | REGULATOR, OXYGEN, DILUTER DEMAND, AUTOMATIC PRESSURE BREATHING, GENERAL SPECIFICATION FOR |
| MIL P 23470 : C | PIN-RIVET, THREADED AND COLLAR, PIN-RIVET, THREADED, TORQUE CONTROLLED, PRE-STRESS, SELF-LOCKING, GENERAL SPECIFICATION FOR |
| MIL V 7899 : C | VALVE, CHECK, AIRCRAFT FUEL SYSTEM |
| MIL-G-23337 Base Document:1962 | GAGE - PRESSURE, DIAL INDICATING |
| MIL-A-27195 Revision A:1989 | ACCELEROMETER, AIRCRAFT, MECHANICAL ABU-6/A |
| MIL G 26611 : D | GENERATOR, TACHOMETER GEU-7/A, MINIATURE |
| MIL-A-6589 Revision A:1968 | AMPLIFIER, ELECTRONIC CONTROL, SINGLE CHANNEL, TYPE A-2 |
| MIL-R-43040 Revision B:1972 | REMOVAL TOOLS, CONNECTOR, ELECTRICAL, CONTACT |
| MIL-DTL-60944 Revision B Interim Revision:2004 | CARTRIDGE, 40 MM - PRACTICE, M385A1 |
| MIL-P-514 Revision D:1966 | PLATE, IDENTIFICATION, INSTRUCTION AND MARKING BLANK |
| MIL J 2829 : E | JOINT SEALING PACKING |
| MS27389 Revision D:2014 | ELBOW SUB ASSEMBLY, FLARELESS, 45 DEGREES FORGED, SWIVEL NUT |
| MIL-R-81553 Revision B:1992 | REGULATOR, CHEST MOUNTED, OXYGEN, POSITIVE PRESSURE, CRU-79/P |
| 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 |
| AN844 Revision 13:2013 | ELBOW - PIPE TO HOSE, 45 DEGREES |
| MS3180 Revision G:2012 | Connectors, Electrical Circular, Cover, Protective Plug, MIL-DTL-26482 Series 1 and 2, Bayonet Coupling |
| MIL-DTL-39030-11 Revision A:2003 | DUMMY LOAD, ELECTRICAL, COAXIAL, TYPE 5 (N), HIGH POWER |
| MIL-DTL-28754-9 Revision E:2014 | CONNECTORS, ELECTRICAL, MODULAR, TYPE 4, DOUBLE SPAN, CONNECTOR ASSEMBLY, (DIP FRAME) |
| MIL-DTL-24251-3 Revision D:2013 | Shield, Electron Tube, Heat Dissipating 7 and 9 Pin, Miniature (Split Shell) |
| MIL-PRF-22885-114 Base Document:2009 | SWITCHES, PUSHBUTTON, WHITE LIGHT EMITTING DIODE (LED) OR 4 LAMP REPLACEABLE INCANDESCENT ILLUMINATED, STANDARD, NIGHT VISION IMAGING SYSTEM (NVIS) AND SUNLIGHT READABLE DISPLAYS, DIMMABLE, SPDT, DPDT AND 4PDT, LOW LEVEL TO 7 AMPERES, SEALED AND UNSEALED, SOLDER AND COMMON TERMINATION SYSTEM (CTS) TERMINATIONS |
| MIL-T-19576 Revision A:1961 | TRANSMITTER, REMOTE COMPASS, THIN WING TYPE ML-1 (UNSTABILIZED) |
| MIL C 28748/5 : D | CONNECTOR, ELECTRICAL, RECTANGULAR, RACK AND PANEL, SOLDER TYPE PIN CONTACTS, SIZE 2O |
| MIL-D-9063 Revision B:1965 | DESEALANT, INTEGRAL FUEL AND OIL TANKS |
| MS24132 Revision G:2013 | Shield, Electrical, Connector, for 7, 9, 14, 20, and 26 Rack and Panel Contact Connectors |
| MIL C 55302/26 : E | CONNECTORS, PRINTED CIRCUIT SUBASSEMBLY AND ACCESSORIES, PLUG 30 THRU 140- CONTACT POSITIONS, FOR PRINTED WIRING BOARDS (.100SQ. GRID) |
| MIL S 25057 : B | SCREEN SYSTEM, AIR INLET, AIRCRAFT TURBINE ENGINE, GENERAL SPECIFICATION FOR |
| MS18192 Revision G:2011 | Shield, Electrical Connectors for 7, 9, 14, 20, 26, 34, 42, 50 and 75 Contact Connectors |
| MIL-I-5133 Revision C:1953 | INDICATOR, ATTITUDE TYPE J 8 |
| MIL-G-22077 Revision C:1993 | GENERATOR SETS, GAS TURBINE, DIRECT AND ALTERNATING CURRENT NAVAL SHIPBOARD USE |
| MIL C 38999 : J | CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET THREADED & BREECH COUPLING) ENVIRONMENT RESISTANT, REMOVABLE CRIMP & HERMETIC SOLDER CONTACTS |
| MIL-DTL-83526-21 Revision C:2014 | Connector, Fiber Optic, Circular Hermaphroditic, Bulkhead, Low Profile without Strain Relief, Jam-Nut Mount, 2 and 4 Positions, Expanded Beam |
| MS3181 Revision G:2012 | CONNECTORS, ELECTRICAL CIRCULAR, COVER, PROTECTIVE, RECEPTACLE, MIL-DTL-26482 SERIES 1 AND 2, BAYONET COUPLING |
| MIL-C-5604 Revision B:1962 | COMPASS, MAGNETIC, PILOTS STANDBY |
| MIL-S-85377 Revision A:1983 | SWITCH, STEPPING, DIRECT CURRENT AIRCRAFT DISPENSER |
| AN807 Revision 7:2007 | Adapter, Straight, Tube to Hose |
| MS27067 Revision D:2013 | Elbow Subassembly, Flared, 45 Degrees Forged, Swivel Nut |
| MIL-C-46941 Revision A:1993 | CARTRIDGE, IMPULSE, M146 ASSEMBLY |
| MIL-PRF-23377 Revision K:2012 | PRIMER COATINGS: EPOXY, HIGH-SOLIDS |
| MIL-H-87111 Revision A:1984 | HEAT SINKS, SEMICONDUCTOR DEVICES, GENERAL SPECIFICATION FOR |
| MIL-HDBK-1250 Revision A:1995 | CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
| 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-DTL-52525-13 Revision C:2008 | FITTINGS, HOSE, CRIMP TYPE, SPLIT-FLANGE STRAIGHT |
| MIL-DTL-38999 Revision M:2015 | Connectors, Electrical, Circular, Miniature, High Density, Quick Disconnect (Bayonet, Threaded or Breech Coupling), Environment Resistant with Crimp Removable Contacts or Hermetically Sealed with Fixed, Solderable Contacts, General Specification for |
| MIL-S-6150 Revision D:1987 | STARTER, ENGINE, ELECTRICAL, DIRECT CRANKING, AIRCRAFT 28 VOLT DC |
| MIL-STD-2198 Base Document:1990 | DESIGN REQUIREMENTS FOR METAL ELECTRICAL BACKPLANE ASSEMBLIES |
| MIL-DTL-32464 Revision A:2017 | FITTINGS, ADAPTER, HYDRAULIC AND PNEUMATIC, 37 DEGREES SPHERICAL TO ANPT CONNECTORS, 1500 TO 3000 PSI, GENERAL SPECIFICATION FOR |
| MIL-S-83427 Base Document:1974 | SURVIVAL KIT CONTAINERS, CNU-129(V)/P AND CNU-130/P |
| MIL-C-60604 Revision A:1992 | CARTRIDGE, THRUSTER, M119 |
| MIL C 38271 : B | CONNECTOR, OXYGEN MASK TO REGULATOR CRU-60/P |
| MIL-F-24666 Base Document:1986 | FILTER ELEMENT, SHIP FUEL SYSTEM PREFILTER, NONCLEANABLE, HIGH EFFICIENCY |
| MIL C 6864 : C | CLEANING COMPOUND, SOLVENT, OIL COOLER |
| MIL-DTL-24127 Revision A:2016 | EDUCTORS, GASOLINE, OIL, OR WATER |
| TT-P-2756 Revision A:1996 | POLYURETHANE COATING - SELF-PRIMING TOPCOAT, LOW VOLATILE ORGANIC COMPOUND (VOC) CONTENT |
| ASTM F 901 : 2001 : R2012 | Standard Specification for Aluminum Transmission Tower Bolts and Nuts |
| MIL L 58085 : A | LIGHT, BEACON, ANTI COLLISION AIRCRAFT |
| MIL-STD-2131 Revision A:1991 | LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| MIL-T-704 Revision K:1992 | Treatment and Painting of Material |
| MS20760 Revision D:2013 | ADAPTER, STRAIGHT, FLANGE TO TUBE |
| MIL-DTL-32371 Base Document:2012 | Fittings, Adapter, Hydraulic and Pneumatic, Spherical to ORFS Connectors, 1500 to 3000 PSI, General Specification for |
| MIL-P-8564 Revision D:1970 | PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
| MIL B 8075 : D | BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
| MIL-M-85831 Base Document:1989 | MASK, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE, NON-OXYGEN |
| SAE AS 17852 : 2012 | REDUCERS, OXYGEN PRESSURE |
| MIL-DTL-28754 Revision E:2016 | Connectors, Electrical, Modular, and Component Parts General Specification for |
| MIL-DTL-83526-20 Revision C:2014 | Connector, Fiber Optic Plug, Circular Hermaphroditic, In-Line Mount, 2 and 4 Positions, Expanded Beam |
| MIL I 38715 : B | INDICATOR, COMBUSTIBLE GAS AND TOXIC GAS |
| MIL-L-8937 Revision D:1982 | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING, [NATO CODE NUMBER S 1738] |
| MIL-T-53055 Revision C:1991 | TANK, 3,000 GALLON & 4600 GALLON FABRIC, COLLAPSIBLE, DRINKING WATER, SEMI-TRAILER MOUNTED |
| MIL-F-7179 Revision G:1993 | FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM |
| MIL S 83352 : B | SIGNAL KIT, PERSONNEL, DISTRESS, A/P25S-5A |
| MIL C 4928 : A | CHARGER, BATTERY, SILICON DIODE, TYPE A-1 |
| MIL-A-63576 Revision A:1985 | ALUMINUM OXIDE COATINGS, LUBRICATIVE, FOR ALUMINUM AND ALUMINUM ALLOYS |
| 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 |
| SAE AS 85731 : 2015 | FASTENER, POSITIVE LOCKING, ELECTRONIC EQUIPMENT, GENERAL SPECIFICATION FOR |
| SAE AS 18280 : 2017 | FITTINGS, 24 DEGREES CONE FLARELESS, FLUID CONNECTION, 3000 PSI |
| NASM24694:2012 | SCREW, MACHINE, FLAT COUNTERSUNK HEAD, 100 DEGREES, STRUCTURAL, CROSS RECESSED, UNC-3A AND UNF-3A |
| SAE AS 85028 : 2017 | CONNECTOR, ELECTRICAL, RECTANGULAR, INDIVIDUAL CONTACT SEALING, POLARIZED CENTER JACKSCREW, GENERAL SPECIFICATION FOR |
| SAE AS 1701 : 2017 | LUBRICANT, SOLID FILM |
| SAE AS 5994A:2000(S2013) | PUMP UNITS, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY |
| MIL-G-18997 Revision E:1991 | GAUGE, PRESSURE, DIAL INDICATING |
| DSCC 84103 : J | HOLDER, ELECTRICAL CARD, WEDGE RETAINER, 3-PIECE, SCREW ACTUATED |
| MIL-DTL-5421 Revision D:2011 | TUBES, PITOT, ELECTRICALLY HEATED, AIRCRAFT |
| MIL-DTL-85061 Revision C:2009 | COUPLING, FUEL LINE, FLEXIBLE, 125 PSI |
| MIL-DTL-83796-18 Revision A:2010 | Hose Assembly, Rubber, Lightweight, Medium Pressure, Internal Support Coil, Field Attachable End Fittings, Flange to Flange |
| MIL-PRF-81975 Revision C:2008 | COUPLINGS, REGULATED, AERIAL PRESSURE REFUELING TYPE MA-2, TYPE MA-3 AND TYPE MA-4 |
| MIL-DTL-26633 Revision F:2014 | Hose Assembly, Nonconductive, Polytetrafluoroethylene, Oxygen |
| MIL-C-83982 Base Document:1974 | COMPOUND, SEALING, FLUID RESISTANT |
| MS18199 Revision C:2013 | Plate, Retaining, Receptacle Electrical Connector, for 34, 42, 50 and 75 Contact Connectors |
| MIL-DTL-52525-5 Revision D:2011 | Fittings, Hose, Screw-on to 37 Degree Flare Female Swivel, Straight |
| MIL-DTL-52525-34 Revision B:2008 | FITTINGS, HOSE, SCREW-ON TO 4-BOLT SPLIT-FLANGE, STRAIGHT |
| MIL-DTL-52525-2 Revision C:2008 | Fittings, Hose, Screw-on to 37 Degree Flare Female Swivel, 45 Degree Bent Tube |
| MIL-M-9397 Revision E:1979 | FREQUENCY CONVERTER, MOBILE, TYPE MC-1A |
| MS27064 Revision E:2014 | ELBOW SUBASSEMBLY, SWIVEL FLANGE, 45 DEGREES |
| MIL S 6807 : D | SWITCHES, ROTARY, SELECTOR POWER - GENERAL SPECIFICATION FOR |
| MIL S 28827 : A | SWITCH, THERMOSTATIC, (VOLATILE LIQUID) HERMETICALLY SEALED GENERAL SPECIFICATION FOR |
| A-A-59812 Revision A:2015 | HOLDER, ELECTRICAL CARD, METAL CARD GUIDE, MULTIPLE PIECE, GENERAL REQUIREMENTS FOR |
| SAE AS 8181 : 1997 | DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS, GENERAL SPECIFICATION FOR |
| FAA AC 150/5345-45 : 2007 | LOW-IMPACT RESISTANT (LIR) STRUCTURES |
| MIL C 24356 : A | COUPLING, SEGMENTED AND SPLIT CLAMPS REATTACHABLE, 2-1/2-, 4-, 6- AND 7- INCH, FOR REFUELING-AT-SEA HOSE |
| MIL-B-36492 Base Document:1966 | BED, ORTHOPEDIC |
| MIL-T-25193 Revision B:1961 | Transmitter, Remote Compass, Type C-2 (Unstabilized) |
| MIL-I-8474 Revision C:1983 | INSPECTION OF ALUMINUM ALLOY PARTS, ANODIZING PROCESS FOR |
| 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 |
| MIL-C-46946 Revision B:1994 | CARTRIDGE, IMPULSE, M43 ASSEMBLY |
| ASTM F 901 : 2001 | Standard Specification for Aluminum Transmission Tower Bolts and Nuts |
| MIL T 5421 : B | TUBE, PITOT, ELECTRICALLY HEATED, AIRCRAFT |
| MIL-DTL-83796-15 Revision A:2010 | Hose Assembly, Rubber, Lightweight, Medium Pressure, Internal Support Coil, Field Attachable End Fittings, Flare to Flange, with Lockwire Hole |
| MS27075 Revision D:2013 | NIPPLE, FLARED, TUBE TO HOSE - SWIVEL NUT |
| MIL-I-70756 Base Document:1988 | INERT PROJECTILE ASSEMBLY LESS ESCAPEMENT ASSEMBLY METAL PARTS AND ASSEMBLING AND PACKAGING |
| MIL-C-27725 Revision B:1969 | COATING, CORROSION PREVENTIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS |
| MS27071 Revision D:2013 | UNION, NIPPLE |
| MIL-W-8604 Revision A:1982 | WELDING, FUSION, ALUMINUM ALLOYS, PROCESSING AND PERFORMANCE OF |
| MIL-M-7997 Revision C:1981 | Motor, Aircraft Hydraulic, Constant Displacement General Specification for |
| MIL-C-83873 Revision A:1993 | CLEANING COMPOUND, PRECOATING SURFACE, AIRCRAFT & AEROSPACE GROUND EQUIPMENT (AGE) |
| MIL-DTL-26482 Revision H:2007 | Connectors, Electrical, Circular, Miniature, Quick Disconnect, Environment Resisting, Receptacles and Plugs, General Specification for |
| MIL C 81904 : B | COATING COMPOUND, THERMAL INSULATION, ABLATIVE |
| MIL-K-8662 Revision E:1974 | KNIFE, HUNTING, SHEATHED, SURVIVAL PILOT S |
| TT-R-248 Revision B:1981 | REMOVER, PAINT AND LACQUER, SOLVENT TYPE |
| MIL-PRF-46010 Revision H:2013 | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING NATO CODE S-1738 |
| MIL-DTL-28754-25 Revision B:2014 | Connectors, Electrical, Modular, Guide, Retaining |
| MIL A 24533 : B | ACTUATORS, ROTARY HYDRAULIC RACK AND PINION |
| MIL-HDBK-510-1 Revision A:2010 | AEROSPACE FUELS CERTIFICATION |
| MIL-DTL-3928 Revision H:2016 | SWITCHES, RADIO-FREQUENCY TRANSMISSION LINE, (COAXIAL AND MICROSTRIP), GENERAL SPECIFICATION FOR |
| MIL-DTL-19068 Revision B:2006 | VALVES, SHUTTLE, HYDRAULIC, AIRCRAFT, TYPE 2 SYSTEMS |
| MS20762 Revision D:2016 | ELBOW, FLARED TUBE, FLANGED, SWIVEL, 90 DEGREES |
| MIL-DTL-50647 Revision B:2005 | Cartridge, Delay, M293 Assembly |
| MS27068 Revision D:2013 | Elbow Subassembly, Flared, 90 Degrees Forged, Swivel Nut |
| MIL F 18264 : D | FINISHES: ORGANIC, WEAPONS SYSTEM, APPLICATION AND CONTROL OF |
| MS27390 Revision C:2013 | Elbow Subassembly, Flareless, 90 Degrees, Forged, Swivel Nut |
| MIL-P-21563 Revision B:1962 | POINT SYSTEM, FLUORESCENT, FOR AIRCRAFT APPLICATION (ASA) |
| MIL-DTL-3954 Revision D:2015 | DUMMY LOADS, ELECTRICAL, WAVEGUIDE, GENERAL SPECIFICATION FOR |
| NASM 23460 : 2004 | PIN, QUICK-RELEASE, SELF-RETAINING, POSITIVE-LOCKING |
| NASA MSFC STD 156 : 1962 | RIVETING, FABRICATING AND INSPECTION, STANDARD FOR |
| DSCC 85122 : G | INDICATOR ASSEMBLIES: RED, YELLOW, GREEN; PLAIN AND FILTERED LENSES; PANEL-SEALED, AND PANEL AND REAR SEALED |
| MIL-DTL-7034 Revision F:2005 | PULLEYS, GROOVE, ANTIFRICTION BEARING, GREASE LUBRICATED, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-PRF-6864 Revision F:2010 | CLEANING COMPOUND, SOLVENT, OIL COOLER |
| MIL-S-85510 Base Document:1981 | Seats, Helicopter Cabin, Crashworthy, General Specification for |
| MIL-DTL-7899 Revision D:2014 | VALVES, CHECK, AIRCRAFT FUEL SYSTEM |
| NASA PRC 5006 : 2003 | PROCESS SPECIFICATION FOR THE ANODIZING OF ALUMINUM ALLOYS |
| MIL E 917 : E | ELECTRIC POWER EQUIPMENT, BASIC REQUIREMENTS (NAVAL SHIPBOARD USE) |
| 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-C-38404 Revision E:1992 | COUPLING, HOSE, REATTACHABLE SCREW-ON |
| MIL-A-38331 Base Document:1964 | AMPLIFIER-POWER SUPPLY AM-4080/ASN-55, LEVELLING |
| MIL-F-50994 Base Document:1972 | FUZE, ROCKET M423 MODIFIED (BUNKER) LESS BOOSTER AND LEAD |
| MIL-V-8610 Revision B:1984 | VALVE, FUEL SHUTOFF SOLENOID OPERATED, 28 VOLT, DC |
| MIL-S-49036 Base Document:1974 | Suppressor, Electrical Transient (No S/S Document) |
| MIL-F-50905 Base Document:1971 | FUZE, ROCKET, M427, MOD 5 LOADING ASSEMBLING AND PACKING |
| MIL-B-48600 Revision A:1979 | BASE PLUG ASSEMBLY |
| SAE AS 22520 : 2011 | CRIMPING TOOLS, WIRE TERMINATION, GENERAL SPECIFICATION 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 V 8057 : F | VALVE, OXYGEN, PRESSURE BUILDUP AND VENT |
| MIL-DTL-8348 Revision K:2008 | Gage Assemblies, Air Pressure, Dial Indicating Chuck Type, Self-Contained |
| MIL-A-19940 Base Document:1957 | AMPLIFIER, CONTROL SINGLE CHANNEL, S-2 COMPASS |
| MIL-G-22169 Base Document:1959 | GYRO, VERTICAL AND MOUNT |
| MIL-DTL-32373 Base Document:2011 | Plug, Machine Thread, Magnetic: Drain |
| 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-D-60873 Revision A:1992 | DELAY ELEMENT, CARTRIDGE, XM69, ASSEMBLY |
| MIL L 13629 : C NOTICE 1 | LACQUER, AIR DRYING FOR CRIMPED PARTS |
| MS28760 Revision E:2007 | Fitting End, Straight, Attachable, Hydraulic and Pneumatic, High Pressure Hose 3000 PSI, Flared Tube |
| MIL-H-9890 Revision E:1988 | HARDWARE, INDIVIDUAL LOAD CARRYING EQUIPMENT: AND HARDWARE, MISCELLANEOUS |
| MIL T 0053055 : B | TANK, 3000 GALLON & 4600 GALLON FABRIC, COLLAPSIBLE, DRINKING WATER, SEMI-TRAILER MOUNTED |
| MIL-A-7237 Revision B:1975 | AIR INDUCTION SYSTEM, RECIPROCATING ENGINE, GENERAL SPECIFICATION FOR |
| MIL L 0046010 : D | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING |
| MIL T 5350 : E | TRANSMITTER, SYNCHRO OPERATED, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-DTL-6807 Revision F:2012 | Switches, Rotary, Selector Power, General Specification for |
| MIL-PRF-64266 Revision B:2016 | CONNECTORS, FIBER OPTIC, CIRCULAR AND RECTANGULAR, PLUG AND RECEPTACLE STYLE, MULTIPLE REMOVABLE GENDERLESS TERMINI, ENVIRONMENT RESISTING GENERAL SPECIFICATION FOR |
| MIL-PRF-46147 Revision D:2008 | LUBRICANT, SOLID FILM, AIR CURED, CORROSION INHIBITING |
| MIL-R-19750 Revision A:1958 | REGULATOR; VOLTAGE, 28 V, 120 DEGREE C, FOR 30 V DIRECT-CURRENT GENERATOR, GENERAL SPECIFICATION FOR |
| MIL P 19834 : B | PLATE, IDENTIFICATION, METAL FOIL, ADHESIVE BACKED |
| MIL-R-50781 Base Document:1972 | RESOLVER, ELECTRICAL LINEAR GENERAL SPECIFICATION FOR |
| SAE AS 4060 : 2013 | TUBE FITTINGS SWAGED JOINT, ROLLER EXPANDER, MANUAL PROCESS, REQUIREMENTS FOR |
| MIL-DTL-32460 Revision A:2017 | ADAPTER, HYDRAULIC AND PNEUMATIC, 37 DEGREES FLARE TUBE FITTING TO ORFS CONNECTORS, 1500 TO 3000 PSI AND -65 DEGREES F TO 250 DEGREES F, GENERAL SPECIFICATION FOR |
| MIL-DTL-83796-1 Revision C:2014 | HOSE ASSEMBLY, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, FIELD ATTACHABLE END FITTINGS, FLARE TO FLARE |
| MIL-DTL-83796-5 Revision D:2014 | HOSE ASSEMBLY, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, FIELD ATTACHABLE END FITTINGS, FLARE TO FLANGE |
| MIL-DTL-83798 Revision D:2008 | FITTING, RUBBER HOSE, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
| MIL-DTL-15291 Revision G:2013 | SWITCHES, ROTARY, SNAP ACTION AND DETENT/SPRING RETURN ACTION, GENERAL SPECIFICATION FOR |
| MIL-P-63514 Revision A:1986 | PROJECTILE, 105MM, TP-T, M489A1, METAL PARTS ASSEMBLY |
| MIL-DTL-52525-38 Revision B:2008 | FITTINGS, HOSE, SCREW-ON TO 37 DEGREES FLARE FEMALE SWIVEL, 45 DEGREES BENT TUBE |
| MIL-B-29186 Base Document:1978 | BARRIER SYSTEM: FLOATING, OIL AND DEBRIS CONTAINMENT (FOR PERMANENT INSTALLATION) |
| FF-N-845 Revision D:1981 | NUT, PLAIN, WING, INCH AND METRIC |
| MIL-DTL-83796-13 Base Document:2008 | Hose Assembly, Rubber, Lightweight, Medium Pressure, Internal Support Coil, Field Attachable End Fittings, Flareless to Flareless, with Lockwire Hole |
| MIL-DTL-52525-3 Revision D:2011 | Fittings, Hose, Screw-on to 37 Degree Flare Female Swivel, 90 Degree Bent Tube, Short Drop |
| MIL L 81329 : C | LUBRICANT, SOLID FILM, EXTREME ENVIRONMENT, NATO CODE NUMBER S-1737, METRIC |
| MIL-V-5461 Revision C:1977 | VALVE, VACUUM BREAKING |
| MIL-T-7771 Revision B:1980 | TUBE, EXTENSION, GYRO STABILIZED DRIFT METER |
| MIL-PRF-85285 Revision E:2012 | COATING: POLYURETHANE, AIRCRAFT AND SUPPORT EQUIPMENT |
| MIL-C-83821 Base Document:1990 | CRANE, WHEEL MOUNTED, CRASH, ROUGH TERRAIN, HYDRAULIC FULL REVOLVING, 4X4, DED, FIGHTER TYPE AIRCRAFT |
| MIL-PRF-22885-115 Base Document:2012 | SWITCHES, PUSHBUTTON, ULTRA-COMPACT, LED ILLUMINATION, NVIS, SEALED |
| 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 C 28748/6 : D | CONNECTOR, ELECTRICAL, RECTANGULAR, RACK AND PANEL, SOLDER TYPE SOCKET CONTACTS, SIZE 2O |
| MIL-D-43699 Revision C:1987 | DRUMS, FABRIC, COLLAPSIBLE, (DRINKING WATER, 55-,250- & 500 GALLON CAPACITIES) |
| MIL-C-63063 Base Document:1976 | CASE, CARTRIDGE, 40MM, M169; PLUG, BASE FOR |
| MIL-C-18438 Revision B:1962 | CHARGER, BATTERY, GENERATOR TYPE |
| MIL-HDBK-349 Base Document:1994 | MANUFACTURE AND INSPECTION OF ADHESIVE BONDED, ALUMINUM HONEYCOMB SANDWICH ASSEMBLIES FOR AIRCRAFT |
| MIL S 22710 : E | SWITCHES, ROTARY (PRINTED CIRCUIT), (THUMBWHEEL, INLINE, AND PUSHBUTTON), GENERAL SPECIFICATION FOR |
| MIL-F-5509 Revision D:1978 | FITTING, FLARED TUBE, FLUID CONNECTION |
| MS27062 Revision D:2013 | Nipple Subassembly, Straight, Swivel Flange |
| MIL-P-81985 Base Document:1974 | PEENING OF METALS |
| MIL-DTL-60247 Revision B:1995 | CARTRIDGE, DELAY, M155 ASSEMBLY |
| MIL-A-81852 Revision A:1986 | ALTIMETER-ENCODER AAU-32/A |
| MIL-PRF-83936 Revision C:1996 | REMOVER, PAINT, TANK TYPE - FOR AIRCRAFT WHEELS, LANDING GEAR COMPONENTS AND OTHER AIRCRAFT AND SUPPORT EQUIPMENT |
| MIL-I-22075 Revision C:1984 | Indicator, Bearing-Distance-Heading ID-663D/U |
| MIL-I-85832 Base Document:1989 | INTERCOM, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE SET |
| SAE AMS P 21600 : 2013 | PAINT SYSTEM, FLUORESCENT, REMOVABLE, FOR AIRCRAFT APPLICATION |
| MS20757 Revision C:2013 | Connector, Fixed Flange, to Hose |
| DOD-M-24672 Base Document:1986 | MOLDS, AND MOLD HEATING PLATEN FOR MOLDING ELECTRICAL CONNECTORS AND CABLES (METRIC) |
| MIL-R-47321 Base Document:1987 | REGULATOR, PRESSURE |
| MIL D 28803 : A | DISPLAY, OPTOELECTRONIC, READOUTS, BACK LIGHTED SEGMENTED, GENERAL SPECIFICATION FOR |
| MIL S 45310 : H NOTICE 1 | SEMITRAILER, TANK, GASOLINE AND FUEL OIL, COMMERCIAL |
| MIL C 22263 : B | COUPLING FUEL LINE, FLEXIBLE, 125 PSI, GENERAL SPECIFICATION FOR |
| MS18204 Revision F:2013 | SHELL, ELECTRICAL, CONNECTOR, RECEPTACLE, RECTANGULAR, POLARIZING |
| MIL-STD-808 Revision A:1983 | FINISH, MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN SUPPORT EQUIPMENT |
| MIL C 5033 : C | CLOCK, AIRCRAFT, CIVIL DATE 24 HOUR DIAL 2 3/4 IN DIAMETER |
| MIL-B-233 Revision D:1987 | BOXES, SUPPLY SUPPORT ITEMS, STOWAGE AND STORAGE |
| 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 | |
| MS20756 Revision F:2011 | FLANGE, SWIVEL, RETAINING |
| MIL-DTL-28754-7 Revision D:2014 | Connectors, Electrical, Modular, Type IV, Single Span, Connector Assembly |
| MIL-A-23547 Revision E:1977 | ANTENNA COUPLER, CU-9370/UR |
| MIL-DTL-52525-9 Revision C:2008 | FITTINGS, HOSE, SCREW-ON TO 37 DEGREES FLARE FEMALE SWIVEL, STRAIGHT |
| MIL T 25439 : A (1) | TRANSMITTER, RATE OF FLOW, IN-FLIGHT REFUELLING, 0-10,000 PPM, TYPE MB-3 |
| MIL-DTL-83796-3 Revision C:2014 | HOSE ASSEMBLY, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, FIELD ATTACHABLE END FITTINGS, FLARELESS TO FLARELESS |
| MIL-C-85642 Base Document:1985 | COMMUNICATIONS CENTRAL AN/ASC-26 |
| MIL-B-38401 Revision A:1973 | BEACON SET, RADIO AN/URT-33 |
| MIL I 6839 : C | INDICATOR, POSITION, LANDING GEAR |
| MIL-H-53062 Base Document:1986 | HOSE ASSEMBLY, RUBBER LIGHTWEIGHT, COLLAPSIBLE 6 INCH; FOR POL SERVICE |
| FF-W-84 Revision A:1967 | WASHER, LOCK (SPRING) |
| MIL-C-50446 Revision A:1981 | CASE, CARTRIDGE, 40MM, M118 PARTS FOR |
| MIL-A-81851 Revision B:1986 | ALTIMETER AAU-31/A |
| MIL-T-27200 Revision C:1975 | TRANSMITTER, RATE GYROSCOPE TRU-2A/A |
| MIL-T-48295 Base Document:1974 | TEST SET, ELECTRICAL CIRCUIT, BOMB DISPENSER A/E 24T-79 |
| AN914 Revision 11:2012 | ELBOW, PIPE, INTERNAL AND EXTERNAL THREAD, 90 DEGREES |
| MIL-S-58112 Base Document:1989 | SLING, MULTI LEG, HELICOPTER, EXTERNAL CARGO |
| MIL-DTL-25308 Revision C:2010 | GAGE, PRESSURE, DIAL INDICATING, HYDRAULIC, TYPE ME-1 |
| MIL-DTL-83796-9 Revision C:2010 | Hose Assembly, Rubber, Lightweight, Medium Pressure, Field Attachable End Fittings, Flange to Flange |
| MIL C 22520 : F | CRIMPING TOOLS, TERMINAL HAND OR POWER ACTUATED, WIRE TERMINATION AND TOOL KITS - GENERAL SPECIFICATION FOR |
| SAE AS 19692 : 2016 | Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump |
| ASTM D 2651 : 2001 | Standard Guide for Preparation of Metal Surfaces for Adhesive Bonding |
| MIL-A-27328 Base Document:1960 | AMPLIFIER-INDICATOR GROUP, ALTITUDE VERTICAL SPEED A/A24G-7 |
| SAE ARP 1281 : 2002 | ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
| MIL S 8805/95 : F | SWITCH, PUSH 2 PDT MOMENTARY 1 AMPERE, SEALED AND UNSEALED, EMI AND NON EMI SHIELDED |
| MIL-DTL-28754-94 Revision A:2015 | CONNECTORS, ELECTRICAL, MODULAR, CONNECTOR FRAME, TYPE 4, DIP, 0.4 PITCH, FORMAT C, D AND E |
| 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 |
| FF-N-836 Revision E:1994 | Nut: Square, Hexagon, Cap, Slotted, Castle, Knurled, Welding and Single Ball Seat |
| MIL A 29563 : 0 | ANTENNA SYSTEM, AIMS SHIPBOARD, ELECTRONICALLY STEERED OE-120/UPX |
| MIL-DTL-50714 Revision C:2004 | INITIATOR, PROPELLANT ACTUATED, DELAY, M113 ASSEMBLY |
| MS20761 Revision C:2016 | ELBOW, FLARED TUBE, FLANGED, SWIVEL, 45 DEGREES |
| MIL-DTL-55302-26 Revision G:2008 | CONNECTORS, PRINTED CIRCUIT SUBASSEMBLY AND ACCESSORIES: PLUG, 30 THRU 140 CONTACT POSITIONS, FOR PRINTED WIRING BOARDS (.100 SQ. GRID) |
| MIL-C-81790 Revision A:1990 | CONNECTORS, RECEPTACLE, EXTERNAL ELECTRIC POWER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE AMS P 81985 : 2001 | PEENING OF METALS |
| SAE AS 27194C : 2014(S2018) | SEAL, BONDED, ALUMINUM ALLOY 6061-T6, AMS4027, MOLD IN GROOVE, NBR RUBBER, AMS-P-5315 |
| SAE AS 6449 : 2017 | SOLID FILM LUBRICANT |
| SAE AS 6026 : 2013 | CONTROL UNIT, PRESSURE GENERATING, MANUALLY OPERATED, AIRCRAFT HYDRAULIC BRAKE SYSTEM |
| SAE ARP 4058 : 2017 | GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS |
| SAE AMS T 22085 : 1999 | TAPES, PRESSURE-SENSITIVE, ADHESIVE, PRESERVATION & SEALING |
| SAE AS 6450 : 2012(S2019) | LUBRICANT APPLICATION, SOLID FILM, HEAT CURED, POTABLE WATER, HYDRAULIC, AND OTHER FLUID SYSTEMS |
| SAE AS 4842 : 2016 | FITTINGS AND BOSSES, PIPE THREADED, FLUID CONNECTION |
| SAE AS 1297 : 2008(S2014) | REDUCERS, PNEUMATIC PRESSURE, MISSILE |
| BS EN 4660-004:2011 | Aerospace series. Modular and open avionics architectures Packaging |
| ASTM F 1110 : 2009 : R2014 | Standard Test Method for Sandwich Corrosion Test |
| MS24693 Revision K:1995 | SCREW, MACHINE, FLAT COUNTERSUNK HEAD, 100 DEG, CROSS RECESSED, UNC-2A AND UNF-2A (IN./MM) |
| MIL-DTL-28754-47 Revision C:2015 | CONNECTORS, ELECTRICAL MODULAR, TYPE 4, CONNECTOR, 100 PIN, RIGHT ANGLE CONTACT TAILS ON .100 CENTERS |
| MIL-DTL-52525-17 Revision C:2008 | FITTINGS, CLAMP-HALVES, FLANGE TO PORT, FOR 4-BOLT SPLIT-FLANGE |
| MIL-DTL-45910 Revision D:2015 | INSERT, SCREW THREAD-LOCKED IN AND RING LOCKED, SERRATED GENERAL SPECIFICATION FOR |
| MIL-DTL-83361 Revision B:2007 | INDICATOR, PRESSURE, OIL, DUAL, 0-100 PSI, EGU-18/A |
| UNI EN 4473 : 2010 | AEROSPACE SERIES - ALUMINIUM PIGMENTED COATINGS FOR FASTENERS - TECHNICAL SPECIFICATION |
| MIL-PRF-57267 Base Document:2017 | COUPLING, AERIAL PRESSURE REFUELING TYPE MA-5 |
| MIL-STD-186 Revision F:2002 | PROTECTIVE FINISHING SYSTEMS FOR ROCKETS, GUIDED MISSILES, SUPPORT EQUIPMENT AND RELATED MATERIALS |
| MIL-DTL-28754-10 Revision D:2014 | Connectors, Electrical, Modular, Connector, Type IV, 40 Pin, Contact Tails on 0.050 Centers |
| MIL-DTL-28754-101 Revision A:2015 | CONNECTORS, ELECTRICAL, MODULAR, TYPE 4, CONNECTOR, 0.6 PITCH, 250 CONTACT, CENTER |
| STANAG 4626 : 2013 | MODULAR AND OPEN AVIONICS ARCHITECTURE |
| MIL-DTL-52525-31 Revision B:2008 | FITTINGS, HOSE, SCREW-ON TO 37 DEGREES FLARE FEMALE SWIVEL |
| A-A-59832 Revision B:2016 | EXTRACTOR, ELECTRICAL CARD, METAL, GENERAL REQUIREMENTS FOR |
| MIL-R-19309 Revision D:2003 | RELAY, SENSITIVE (FOR TORPEDO MARK 37 MOD 2) |
| DOD C 63976 : 0 | CASE, CARTRIDGE, 30MM, AMMUNITION FOR M788 M789 AND M799 SERIES OF 30 MM, AMMUNITION |
| MIL G 6162 : B | GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION |
| MIL-L-23398 Revision D:1985 | LUBRICANT, SOLID FILM, AIR DRYING, CORROSION INHIBITING, NATO CODE NUMBER S 749 |
| MIL-DTL-26894 Revision D:1998 | Hose and Hose Assembly, Rubber, Gasoline, Refueling, Low Temperature |
| MIL-DTL-52525 Revision F:2008 | FITTINGS, HOSE, HYDRAULIC, REUSABLE, FIELD-ATTACHABLE AND CLAMP-HALVES, TO MATE WITH SAE-J517 TYPE HOSES, GENERAL SPECIFICATION FOR |
| MIL-DTL-28803 Revision C:2013 | DISPLAY, OPTOELECTRONIC, SEGMENTED READOUTS, BACKLIGHTED, GENERAL SPECIFICATION FOR |
| I.S. EN 6101:2016 | AEROSPACE SERIES - RIVET, 100 DEGREES MEDIUM FLUSH HEAD, CLOSE TOLERANCE - INCH SERIES |
| 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 25725 : A | INDICATOR, TORQUE PRESSURE, MAGNESYN STYLE, SINGLE CLAMP MOUNTED, 2 IN SIZE, 50-400 PSI TYPE A-8 |
| 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 |
| MS18200 Revision B:2013 | Plate, Retaining, Receptacle Electrical Connector, for Size 66 and 104 Contact Connectors |
| MIL-D-6055 Revision D:1987 | DRUM, METAL REUSABLE, SHIPPING AND STORAGE [CAP FROM 88 TO 510 CUBIC INCHES] |
| MIL-I-85889 Base Document:1988 | IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| 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-DTL-32434 Base Document:2013 | Hose Assembly, Polytetrafluoroethylene, Convoluted, High Temperature, Medium Pressure, General Specification for |
| MS27391 Revision F:2013 | Nipple, Flareless, Tube to Hose - Swivel Nut |
| MIL-C-6720 Revision C:1964 | CLOCK, AIRCRAFT, ELAPSED TIME, CIVIL DATE 24 HOUR 2 3/4 INCH DIAL |
| MIL-DTL-83723 Revision H:2016 | CONNECTORS, ELECTRICAL, CIRCULAR, ENVIRONMENT RESISTING AND HERMETICALLY SEALED, RECEPTACLES AND PLUGS, GENERAL SPECIFICATION FOR |
| MIL-DTL-28754-13 Revision D:2014 | Connectors, Electrical, Modular, Connector Assembly, Type IV, Single Span (without Guide Ribs) |
| MIL-DTL-38394 Revision E:2009 | Transmitter, Pressure TRU-81/A, Oil, 0-500 PSI |
| MIL G 8360 : A | GAGE, PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE, 10-75 IN MERCURY TYPE MB 1 |
| MIL-PRF-22885-79 Revision E:2006 | SWITCHES, PUSH BUTTON, ILLUMINATED, MOMENTARY, SPDT AND DPDT, ONE LAMP, 7 AMPERE SILVER CONTACTS, 1 AMPERE GOLD CONTACT |
| MIL-B-85667-13 Base Document:1991 | BOLT, 100 DEGREES TENSION FLUSH HEAD, STRAIGHT SHANK, ALUMINUM ALLOY SLEEVE, TITANIUM ALLOY PIN, 95 KSI FSU, 160 KSI FTU |
| MIL C 83867 : B | CONNECTOR, OXYGEN MASK HOSE NON-EJECTION TYPE |
| NASA KSC SPEC F 0009 : 1988 | DESIGN, FABRICATION, AND ERECTION OF SIGNS AT JOHN F. KENNEDY SPACE CENTER, SPECIFICATION FOR |
| MIL-DTL-28748-8 Revision F:2009 | CONNECTORS, ELECTRICAL, RECTANGULAR, RACK AND PANEL, SOLDER TYPE SOCKET CONTACTS, SIZE 22 |
| DOD-S-63275 Revision A:1982 | STUD, SCREW THREAD, LOCKED IN, RING LOCKED, SERRATED, METRIC AND RING LOCK SERRATED METRIC, GENERAL SPECIFICATION FOR |
| MIL-A-23282 Revision B:1965 | ACTUATOR |
| MIL-L-21652 Revision A:1964 | Light, Beacon, Anticollision, Aircraft, General Specification for |
| MIL S 9479 : C | |
| MIL-DTL-7961 Revision D:2007 | LIGHTS, INDICATORS, PRESS TO TEST |
| MIL-H-18911 Revision A:1974 | HEAD AND MOTOR, ROCKET, INERT PARTS, PAINTING AND MARKING |
| MIL T 6349 : C NOTICE 1 | TEST SET, SYNCHRO |
| MIL-I-26689 Revision C:1981 | INDICATOR, HORIZONTAL SITUATION, AQU-2/A |
| MIL-I-58067 Revision A:1977 | INDICATOR, VERTICAL VELOCITY, RAPID RESPONSE ACCELERATION SENSITIVE, GENERAL SPECIFICATION FOR |
| MS16051 Revision G:2014 | COUPLING, GROUND COOLING, COMBAT TYPE AIRCRAFT |
| MIL-B-23401 Revision E:1989 | BURNER, CARBON MONOXIDE AND HYDROGEN, CATALYTIC TYPE (MARK 4 E) NAVAL SUBMARINE USE |
| MIL-N-3336 Revision A:1964 | Nut, Sheet Spring, Instrument Mounting |
| MIL-V-5622 Revision A:1963 | Volt-Ammeter, Dual Pointer Direct Current |
| MIL L 3661 : B | LAMPHOLDER, INDICATOR LIGHTS, INDICATOR LIGHT HOUSINGS AND INDICATOR LIGHT LENSES GENERAL SPECIFICATION FOR |
| MIL-DTL-50869 Revision F Interim Revision:2004 | Fuze, Point Initiating, Base Detonating (PIBD) - M550, Less Spitback Assembly Loading, Assembling, and Packing |
| MIL-DTL-52618 Revision F:2012 | FITTINGS, PIPE, ALUMINUM-ALLOY THREADED, 150-POUND, GENERAL SPECIFICATION FOR |
| MIL-S-6551 Revision A:1981 | |
| NASA KSC F 124 : 1994 | SPECIFICATION FOR FITTINGS, FLARED TUBE |
| NASA HDBK 6003 : 2008 | APPLICATION OF DATA MATRIX IDENTIFICATION SYMBOLS TO AEROSPACE PARTS USING DIRECT PART MARKING METHODS/TECHNIQUES |
| MIL-DTL-28754-23 Revision G:2014 | CONNECTORS, ELECTRICAL, MODULAR, CONNECTOR ASSEMBLY, TYPE 4, SINGLE SPAN |
| MIL-DTL-83796-8 Revision D:2014 | HOSE ASSEMBLY, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, FIELD ATTACHABLE END FITTINGS, FLARELESS TO FLANGE, WITH LOCKWIRE HOLE |
| MIL-DTL-28754-12 Revision G:2014 | Connectors, Electrical, Modular, Connector Assembly, Type IV, Single Span (for Solid State or Dip Frame) |
| MS28761 Revision C:2007 | Fitting End, Straight, Attachable, Hydraulic, High Pressure Hose 3000 PSI, Flareless Tube |
| MIL-DTL-50648 Revision B:2005 | Delay Element, Cartridge, M75 Assembly |
| NASA PRC 5008 : 2002 | PROCESS SPECIFICATION FOR SPECIALTY ANODIZING OF ALUMINUM ALLOYS TO CONTROL OPTICAL PROPERTIES |
| MIL-P-7962 Revision D:1980 | PRIMER COATING, CELLULOSE NITRATE MODIFIED ALKYD TYPE, CORROSION INHIBITING, FAST DRYING [FOR SPRAY APPLICATION OVER PRETREATMENT COATING |
| MIL M 7793 : F | METER, TIME TOTALIZING |
| MIL-A-25915 Revision A:1980 | ACCELEROMETER, AIRCRAFT, PILOTS WARNING, TYPE MA-2 |
| MIL C 27889 : D | COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING, CPU-46/A, GENERAL SPECIFICATION FOR AND MTU-38/A MOUNTING TRAY |
| MIL-L-19538 Revision C:1970 | LACQUER, ACRYLIC NITROCELLULOSE, CAMOUFLAGE (FOR AIRCRAFT USE) |
| MIL-DTL-83798-9 Revision D:2017 | Fittings, Rubber Hose, Lightweight, Medium Pressure, Swivel Flange, 90 Degrees |
| MIL-I-85352 Base Document:1980 | INFLATOR ASSEMBLY AND GAGE ELEMENTS, PNEUMATIC PRESSURE REMOTE CONTROL, DIRECT READING |
| AA-C-112 Revision D:1976 | CARTS, SURGICAL DRESSING |
| MIL-V-27296 Revision C:1993 | VALVE, OXYGEN MASK, COMBINATION INHALATION AND EXHALATION |
| MIL H 26894 : C | HOSE ASSEMBLY, RUBBER, GASOLINE, REFUELING, LOW TEMPERATURE |
| MIL-G-81168 Base Document:1964 | GYROSCOPE, RATE INTEGRATING |
| MIL-DTL-22520 Revision G:1997 | CRIMPING TOOLS, WIRE TERMINATION, GENERAL SPECIFICATION FOR |
| MIL-C-81003 Base Document:1964 | Clinometer, Elevation ML-591/U |
| SAE AMS 3116 A : 2005 | PRIMER COATING; EPOXY, CHEMICAL AND SOLVENT RESISTANT NON-CHROMATED, CORROSION PREVENTIVE |
| MIL-S-24317-9 Revision B:2006 | Switches, Multistation, Push Button, Matrix Arrangement Plug-In Module, 2 Amperes, Unsealed, Type SM09L1 |
| MIL-S-8805-36 Revision B:1990 | SWITCHES, PUSH, 2PDT, ALTERNATE ACTION, 1 AMPERE, DUST-TIGHT |
| MIL-C-81991 Base Document:1975 | CONVERTER, AIRCRAFT DC TO DC, BOOST GENERAL SPECIFICATION FOR |
| MIL-PRF-22885-111 Revision B:2010 | SWITCHES, PUSHBUTTON, LIGHT EMITTING DIODE (LED) ILLUMINATED, STANDARD, NIGHT VISION IMAGING SYSTEM (NVIS) AND SUNLIGHT READABLE DISPLAYS, SPDT AND DPDT, LOW LEVEL TO 7 AMPERES, SEALED AND UNSEALED, SOLDER AND COMMON TERMINATION SYSTEM (CTS) TERMINATIONS |
| MIL-DTL-46618 Revision C:2011 | CARTRIDGE IMPULSE, M73 ASSEMBLY |
| MIL-P-63357 Revision A:1980 | Projectile, Training, 155MM, 823 |
| MIL-HDBK-83377 Base Document:1997 | Adhesive Bonding (Structural) for Aerospace and Other Systems, Requirements for |
| MIL-DTL-83796-17 Revision A:2010 | Hose Assembly, Rubber, Lightweight, Medium Pressure, Internal Support Coil, Field Attachable End Fittings, Flareless to Flange, with Lockwire Hole |
| MIL-STD-7179 Revision A:2009 | Finishes, Coatings, and Sealants, for the Protection of Aerospace Weapons Systems and Support Equipment |
| MIL C 85704 : B | CLEANING COMPOUND, TURBINE ENGINE GAS PATH |
| MIL H 24565 : 0 | HOSE AND FITTINGS, OIL AND TURBINE FUEL, SMOOTH BORE, CORRUGATED COVER, 7 INCH |
| MIL-DTL-46200 Revision C:2005 | CARTRIDGE, IMPULSE, M42A1 ASSEMBLY |
| MIL-C-81740 Base Document:1969 | COATING, ALUMINUM AND ALUMINUM ALLOYS (METALLIC COMPOUND DECOMPOSITION) |
| 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-I-23366 Revision B:1987 | Indicator, Horizontal Situation ID-1013(*)/A |
| MIL I 83452 : LATEST | INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
| SAE MA 2005 : 2015 | TUBE FITTINGS, AEROSPACE FLUID SYSTEMS, SEPARABLE, FOR 24 DEGREE CONE, GENERAL SPECIFICATION, METRIC |
| MIL-G-45811 Revision D:1992 | GAGE, AIR, LOW PRESSURE, PNEUMATIC FLOATING EQUIPMENT |
| MIL A 25088 : C | |
| MIL-A-17204 Revision D:1982 | ADAPTERS, STRAIGHT OR REDUCING, PIPE THREAD TO HOSE THREAD |
| MIL-I-25861 Revision D:1967 | INDICATOR, PRESSURE, HYDRAULIC, 0-4000 PSI INTEGRALLY LIGHTED |
| MIL I 23145 : B | INFLATION ASSEMBLIES, LIFE PRESERVER |
| MIL-S-5804 Revision C:1967 | SEAT, AIRCRAFT, TROOP, WALL STYLE |
| MIL-C-81946 Base Document:1973 | COATING SYSTEM, THERMAL INSULATION, INTUMESCENT |
| MIL C 25478 : B | COOLER, LUBRICATING OIL, AIRCRAFT ENGINE, SYNTHETIC OIL, GENERAL SPECIFICATION FOR |
| MIL-S-70334 Base Document:1987 | SHIM, SOLID GENERAL SPECIFICATION FOR |
| MIL-C-82493 Base Document:1967 | CABLE ASSEMBLY MARK 10 MOD O |
| WW-C-621 Revision G:1990 | COUPLING ASSEMBLY, HOSE (FIRE, WOVEN-JACKETED, RUBBER OR FABRIC-LINED AND UNLINED) |
| MIL-DTL-28754-17 Revision E:2014 | Connectors, Electrical, Modular, Connector Assembly, Type V, Style I, Contact Tails on .100 Centers |
| MIL-DTL-7627 Revision G:2010 | INDICATOR, TURN AND SLIP, 28 V DC |
| MIL-I-83751 Base Document:1967 | INDICATOR, SAFETY LEVEL, RF |
| MIL-G-7734 Revision C:1981 | GAGE, PRESSURE ENGINE AND UTILITY AIRCRAFT |
| MIL-F-27656 Revision C:1987 | Filter Unit, Fluid, Pressure, MXU-408/M, Absolute, 5 Micron, Hydraulic |
| MIL G 8348 : H | GAGE, ASSEMBLIES, AIR PRESSURE, DIAL INDICATING CHUCK TYPE SELF CONTAINED |
| MIL-C-172 Revision C:1958 | CASES: BASES, MOUNTING & MOUNTS, VIBRATION (FOR USE WITH ELECTRONIC EQUIPMENT) |
| MIL-A-10957 Revision G:1986 | ADAPTER KIT, GRAVITY FEED, FOR 5 GALLON MILITARY GASOLINE CAN AND 55 GALLON DRUM |
| 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-T-48291 Base Document:1974 | TEST SET, ELECTRICAL CIRCUIT, BOMB DISPENSER A/E 24T-80 |
| MIL-R-23057 Base Document:1961 | Regulator, Compressed Air, High Pressure (3500 PSI) |
| MIL-C-6499 Revision E:1970 | CLOCK, AIRCRAFT MECHANICAL TYPE A 13A |
| MIL-G-23723 Base Document:1964 | Gyroscope, Rate Switching CN-495/AJB-3 |
| MIL-PRF-83323 Revision D:2016 | TESTER, UNIVERSAL RECEPTACLE, AERIAL REFUELING |
| 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-DTL-6508 Revision C:2011 | THERMOMETER, SELF-INDICATING, BIMETALLIC, GENERAL SPECIFICATION FOR |
| MIL-C-8412 Revision B:1969 | COMPASS, MAGNETIC, SLAVED GYRO, TYPE J-4 |
| MIL-DTL-60553 Revision D:2005 | CARTRIDGE, DELAY, M90 ASSEMBLY |
| MIL-PRF-22885-112 Revision A:2013 | Switches, Pushbutton, White Light Emitting Diode (LED) Illuminated, Standard, Night Vision Imaging System (NVIS) and Sunlight Readable Displays, Dimmable, SPDT and DPDT, Low Level to 7 Amperes, Sealed and Unsealed, Solder and Common Termination System (CTS) Terminations |
| MIL DTL 25627 : D | TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |
| MIL I 7069 : A NOTICE 1 | INDICATORS, TACHOMETER, ELECTRIC, PERCENT SPEED TYPE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-L-24560-26 Base Document:1990 | LIGHT, TASK AND SHIELD ASSEMBLY, FOR USE WITH SYMBOL 190.1 AND 192.1 BRASS LIGHT FIXTURES |
| MS28754 Revision E:2012 | FITTING END, SELF-SEALING FUEL HOSE, SWIVEL, DETACHABLE, FLANGED, 45 DEGREES |
| MIL C 28754/21 : E | CONNECTOR, ELECTRICAL, MODULAR, FRAME, CASTING, TYPE 4, DOUBLE SPAN |
| MIL C 28754/12 : F | CONNECTOR, ELECTRICAL, MODULAR, CONNECTOR ASSEMBLY, TYPE 4, SINGLE SPAN (FOR SOLID OR DIP FRAME) |
| SAE AS 4073 : 2013(R2018) | AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES |
| DOD-E-8983 Revision C:1977 | ELECTRONIC EQUIPMENT, AEROSPACE, EXTENDED SPACE ENVIRONMENT, GENERAL SPECIFICATION FOR |
| 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 |
| MS27756 Revision A:1993 | SNAP HOOK, PARACHUTE LANYARD |
| MIL-DTL-26500 Revision G:2011 | CONNECTORS, GENERAL PURPOSE, ELECTRICAL, MINIATURE, CIRCULAR, ENVIRONMENT RESISTING OR HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
| MIL-B-5046 Revision D:1968 | BOARD, CHART PLOTTING MARK 7 [ASG] |
| MIL L 46010 : D | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING |
| MIL I 26359 : B | INDICATOR, ATTITUDE, REMOTE ARU-4/A |
| MIL-P-9389 Revision A:1987 | PUMP PRESSURE, OIL AND FREE AIR, TYPE MA AND 3 |
| MIL-DTL-58085 Revision C:2012 | Light, Beacon, Anti-Collision, Aircraft |
| P-C-444 Revision B:1983 | CLEANING COMPOUND, SOLVENT SOLUBLE, GREASE EMULSIFYING |
| MIL-STD-171 Revision F:2011 | FINISHING OF METAL AND WOOD SURFACES |
| MIL-PRF-29602 Revision A:2005 | CLEANING COMPOUNDS, PARTS WASHER AND SPRAY CABINET |
| MIL P 23971 : B | POWER DIVIDERS, POWER COMBINERS AND POWER DIVIDER/COMBINERS, GENERAL SPECIFICATION FOR |
| MIL-P-83126 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
| MIL-DTL-5070 Revision F:2006 | ADAPTER, HOSE TO TUBE, PIPE AND FLANGE, REUSABLE - HYDRAULIC, FUEL, AND OIL LINES, GENERAL SPECIFICATION FOR |
| BS ISO 9738:2000 | Turnbarrels, for aircraft control wire rope. Dimensions and loads |
| MIL C 46200 : B | CARTRIDGE, IMPULSE, M42A1 ASSEMBLY |
| MIL-C-85528 Base Document:1983 | CONNECTOR, ELECTRICAL, MOUNTING DEVICE, FLANGE TYPE, GENERAL SPECIFICATION FOR |
| MIL-C-22542 Revision B:1987 | CLEANING COMPOUND, HIGH PRESSURE CLEANER, LIQUID |
| MIL-T-19646 Revision A:1990 | THERMOMETER, REMOTE READING, SELF-INDICATING DIAL, GAS ACTUATED |
| NASA MSFC SPEC 384 : 1964 | LEAK TEST COMPOUND, LOX COMPATIBLE |
| MIL-D-21625 Revision G:1993 | DESIGN AND EVALUATION OF CARTRIDGES FOR CARTRIDGE ACTUATED DEVICES |
| 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-DTL-28754-49 Revision A:2015 | CONNECTORS, ELECTRICAL, MODULAR, HOUSING |
| MIL-L-24560-9 Revision B:1990 | LIGHTS, NAVIGATION, SIDE, RED AND GREEN, 120 VOLTS, 50 WATTS, ONE LAMP, SYMBOLS 182.2 AND 183.2 |
| MIL C 28754/9 : D | CONNECTOR, ELECTRICAL, MODULAR, TYPE 4 DOUBLE SPAN, CONNECTOR ASSEMBLY, (DIP FRAME) |
| MS28753 Revision E:2012 | FITTING END, SELF-SEALING FUEL HOSE, SWIVEL, DETACHABLE, FLANGED, STRAIGHT |
| MIL-DTL-52471-8 Revision B:2008 | Hose Assemblies, Rubber: Hydraulic Pressure-Type; Type 100RE |
| SAE AS 5528 : 2016 | LUBRICANT APPLICATION, SOLID FILM, HEAT CURED, CORROSION INHIBITING |
| MS24133 Revision K:2013 | SHIELD, ELECTRICAL, CONNECTOR, FOR 34, 42, 50, AND 75 CONTACT RACK AND PANEL CONNECTOR |
| MIL-DTL-8789 Revision G:2015 | FITTING END, ATTACHABLE, HYDRAULIC, HIGH PRESSURE (3,000 PSI), GENERAL SPECIFICATION FOR |
| MIL-T-53066 Revision B:1994 | TANK, FABRIC, COLLAPSIBLE, 5000 BARREL, FUEL |
| MIL C 28754 : D | CONNECTOR, ELECTRICAL, MODULAR AND COMPONENT PARTS, GENERAL SPECIFICATION FOR |
| MIL-DTL-38449 Revision D:2010 | SIGNAL AND SIGNAL/INTERCOMMUNICATION AMPLIFIERS, UNIVERSAL, AERIAL REFUELING |
| MIL-DTL-81014 Revision B:2001 | HOOK, HELICOPTER EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C |
| MIL-DTL-19834 Revision C:2006 | PLATES, IDENTIFICATION OR INSTRUCTION, METAL FOIL, ADHESIVE BACKED, GENERAL SPECIFICATION FOR |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| MIL C 28754/23 : F | CONNECTOR, ELECTRICAL, MODULAR, CONNECTOR ASSEMBLY, TYPE 4, SINGLE SPAN |
| MIL L 7961 : C | LIGHT, INDICATOR, PRESS TO TEST |
| JSSG-2010-12 Base Document:1998 | Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
| AN848 Revision 13:2015 | Elbow, Hose, 90 Degree |
| SAE ARP 5812 : 2017 | ACTUATORS, LINEAR MECHANICAL, GENERAL SPECIFICATION GUIDE |
| MIL-S-48405 Base Document:1973 | Shielded and Confined Mild Detonating Cord Assemblies |
| MIL-S-38399 Revision A:1975 | STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR |
| MS18198 Revision C:2013 | Plate, Retaining, Receptacle Electrical Connector, for 9, 14, 20, and 26 Contact Connectors |
| MIL-T-53029 Revision C:1994 | TANKS, FABRIC, COLLAPSIBLE, 10,000 20,000 AND 50,000 GALLON, DRINKING WATER |
| AN 840 : 0011 | ADAPTER, STRAIGHT, PIPE TO HOSE |
| DOD-L-85645 Revision A:1988 | LUBRICANT, DRY THIN FILM, MOLECULAR BONDED (METRIC) |
| MIL STD 194 : A NOTICE 2 | SYSTEM FOR PAINTING AND FINISHING FIRE-CONTROL MATERIEL |
| MIL-T-38760 Base Document:1966 | TENSIOMETER DIAL INDICATING |
| MS18193 Revision F:2011 | Shield, Electrical Connectors for 66 and 104 Contact Connectors |
| MS18203 Revision G:2013 | SHELL, ELECTRICAL, CONNECTOR, PLUG, RECTANGULAR, POLARIZING |
| MIL-DTL-24788 Revision B:2017 | Coupling Assembly, Semi-Dry-Break, Quick-Disconnect Fuel, with or without Continuity Switch |
| 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-A-27198 Revision B:1987 | ALTIMETER, PRESSURE AAU-7/A |
| 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-46851 Revision C:1993 | FAN, GUIDED MISSILE, GROUND SUPPORT EQUIPMENT, GENERAL SPECIFICATION FOR |
| MIL-T-52943 Base Document:1978 | TANK, FABRIC, COLLAPSIBLE, PILLOW TYPE (FOR POTABLE WATER) |
| 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 A 83419 : C | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
| AN 839 : 0009 | ELBOW, TUBE TO HOSE, 45 DEGREES |
| MIL-D-7106 Revision C:1987 | DRIFTMETER, ELECTRICALLY DRIVEN GYRO STABILIZED |
| MIL H 22199 : E | HELMET, SAILOR S, REINFORCED PLASTIC, MK 3 MOD O |
| DSCC 87019 : G | INDICATOR ASSEMBLIES, IR SECURE LIGHTING; RED, YELLOW, GREEN; PANEL SEALING |
| MIL-T-24388 Revision C:1990 | THERMOCOUPLE AND RESISTANCE TEMPERATURE ELEMENT ASSEMBLIES, GENERAL SPECIFICATION FOR (NAVAL SHIPBOARD) |
| MIL-DTL-7793 Revision H:2016 | METER, TIME TOTALIZING |
| 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-R-83726-27 Revision M:2016 | Relays, Hybrid, Time Delay, Voltage Sensitive, Delay on Drop-Out, Class A, Type V, Hermetically Sealed (Potted), SPDT, 2 Ampere, Track Mounted (No S/S Document) |
| MIL C 29602 : 0 | CLEANING COMPOUNDS, FOR PARTS WASHERS AND SPRAY CABINETS |
| MIL I 7491 : B | INDICATOR RATE OF FLOW, FUEL TOTALIZING, SERVO STYLE, TYPE F 1 |
| 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-DTL-52525-16 Revision D:2008 | FITTINGS, CLAMP-HALVES, FOR 4-BOLT SPLIT-FLANGE, SAE-J518, TYPE SPLIT-FLANGE CLAMP (SFC) |
| MS27394 Revision C:2014 | ELBOW, FLARELESS, TUBE TO HOSE - 90 DEGREE SWIVEL NUT |
| MIL-DTL-52471-2 Revision C:2008 | HOSE ASSEMBLIES, RUBBER: HYDRAULIC PRESSURE-TYPE; TYPE 100R2, DOUBLE-WIRE BRAIDED REINFORCEMENT HOSE |
| MIL-DTL-52525-37 Revision B:2008 | FITTINGS, HOSE, SCREW-ON TO 37 DEGREES FLARE FEMALE SWIVEL, STRAIGHT |
| MIL-DTL-52471-3 Revision C:2008 | HOSE ASSEMBLIES, RUBBER, HYDRAULIC PRESSURE-TYPE, TYPE 100RE, FOUR-WIRE BRAIDED REINFORCEMENT OR MULTIPLE WIRE BRAIDED STEEL WIRE REINFORCED HOSE |
| MIL-A-27261 Revision A:1966 | ACCELEROMETER, AIRCRAFT |
| NASM25027:2012 | NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F |
| MIL-A-81403 Base Document:1967 | ALTIMETER-ENCODER, AAU-21/A |
| MIL-E-18927 Revision E:1983 | ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
| SAE AS 4843 : 2016 | FITTINGS, BEADED, FLUID CONNECTION |
| SAE AS 27195 : 2014 | SEAL, BONDED, ALUMINUM ALLOY 6061-T6, AMS4027, MOLD IN GROOVE, NBR RUBBER, AMS-R-7362 |
| SAE AIR 4012 : 2012 | USAF AIRCRAFT WHEELS |
| SAE AS 1227 : 2013 | HOSE ASSEMBLY, CONVOLUTED POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, LOW PRESSURE, UP TO 400 DEGREES F, AIRCRAFT |
| SAE AS 81969 : 2016 | INSTALLING AND REMOVAL TOOLS, CONNECTOR ELECTRICAL CONTACT, GENERAL SPECIFICATION FOR |
| SAE AMS T 23397 : 1998 | TAPES, PRESSURE SENSITIVE ADHESIVE, FOR MASKING DURING PAINT STRIPPING OPERATIONS |
| SAE AMS 3603 : 2002 | PROTECTIVE FILM, HIGH PERFORMANCE, POLYMERIC PRESSURE SENSITIVE ADHESIVE, FOR AIRCRAFT EXTERIOR APPLICATIONS |
| NASM20995:2012 | WIRE, SAFETY OR LOCK |
| I.S. EN 4660-004:2011 | AEROSPACE SERIES - MODULAR AND OPEN AVIONICS ARCHITECTURES - PART 004: PACKAGING |
| SAE AS 5420 : 2017 | HOSE ASSEMBLY, HEATED, 125 PSIG, LINED SILICONE, POTABLE WATER, PROCUREMENT SPECIFICATION |
| ASTM F 901 : 2001 : R2017 | Standard Specification for Aluminum Transmission Tower Bolts and Nuts |
| I.S. EN 6069:2009 | AEROSPACE SERIES - RIVET, 100 DEGREE REDUCED FLUSH HEAD, CLOSE TOLERANCE - INCH SERIES |
| ISO 7169:2014 | Aerospace Separable tube fittings for fluid systems, for 24 degree cones, for pressures up to 3 000 psi or 21 000 kPa Procurement specification, inch/metric |
| BS EN 4473:2010 | Aerospace series. Aluminium pigmented coatings for fasteners. Technical specification |
| PREN 6101 : 200P2 | AEROSPACE SERIES - RIVET, 100 DEGREES MEDIUM FLUSH HEAD, CLOSE TOLERANCE - INCH SERIES |
| BS EN 6101:2016 | Aerospace series. Rivet, 100° medium flush head, close tolerance. Inch series |
| BS EN 6080:2016 | Aerospace series. Rivet, 100° normal flush head, close tolerance. Inch series |
| PREN 6069 : 200P3 | AEROSPACE SERIES - RIVET, 100 DEGREES REDUCED FLUSH HEAD, CLOSE TOLERANCE - INCH SERIES |
| 08/30192115 DC : 0 | BS EN 4473 ED.P2 - AEROSPACE SERIES - ALUMINIUM PIGMENTED COATINGS FOR FASTENERS - TECHNICAL SPECIFICATION |
| EN 6069:2009 | Aerospace series - Rivet, 100° reduced flush head, close tolerance - Inch series |
| EN 6080:2016 | Aerospace series - Rivet, 100° normal flush head, close tolerance - Inch series |
| MIL-DTL-9398 Revision D:2007 | GENERATOR, TACHOMETER, TWO-POLE, HIGH TEMPERATURE, AIRCRAFT |
| EN 6101:2016 | Aerospace series - Rivet, 100° medium flush head, close tolerance - Inch series |
| EN 4660-004:2011 | Aerospace series - Modular and Open Avionics Architectures - Part 004: Packaging |
| EN 4473:2010 | Aerospace series - Aluminium pigmented coatings for fasteners - Technical specification |
| MIL-DTL-28754-100 Revision A:2015 | CONNECTORS, ELECTRICAL, MODULAR, TYPE 4, CONNECTOR, 200 CONTACT, CENTER |
| MIL-DTL-28754-61 Revision A:2016 | Connectors, Electrical, Modular, Type IV, Connector, 100 Pin, Center, Crossover, Contact Tails on .100 Centers (Ceramic Compatible) |
| MIL-F-26301 Revision H:2014 | FLASHER, SOLID STATE, AIRCRAFT NAVIGATIONAL LIGHT, GENERAL SPECIFICATION FOR |
| MIL-DTL-55302-23 Revision H:2003 | CONNECTORS, PRINTED CIRCUIT SUBASSEMBLY AND ACCESSORIES: PLUG, DECADE INCREMENT 10 THRU 120, 150, 160 AND 180 CONTACT POSITIONS, FOR PRINTED WIRING BOARDS (.075 SPACING) |
| 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 C 85285 : C | |
| MIL-DTL-28748-16 Base Document:2004 | Connectors, Electrical, Hexagonal, Rack and Panel, Miniature, Plug-Receptacle, Female Solder Cup Pin Contacts, Size 20 |
| MIL F 50864 : B | FUZE, PIBD, M549, LESS SPITBACK METAL PARTS AND LOADING, ASSEMBLING AND PACKAGING |
| MIL-C-81947 Revision A:1975 | COATING COMPOUND, THERMAL INSULATION, THREE-COMPONENT, INTUMESCENT |
| 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 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 |
| MIL-A-25933 Revision B:1985 | ALTIMETER, PRESSURIZED COMPARTMENT, INTEGRALLY LIGHTED 0-50,000 FEET, 1-7/8 INCH DIAL |
| MIL-T-27-233 Base Document:1978 | TRANSFORMERS AND INDUCTORS (AUDIO POWER AND HIGH POWER PULSE) INDUCTOR CHARGING TF5S37ZZ |
| MIL-DTL-25867 Revision D:2006 | GAGE, PRESSURE, DIAL INDICATING, PNEUMATIC |
| 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-T-26609 Revision C:1994 | Transmitter, Position |
| MIL-T-70755 Base Document:1988 | TEST VEHICLE PROJECTILE METAL PARTS AND LOADING, ASSEMBLING AND PACKAGING |
| MIL C 17850 : A | COMPASS MAGNETIC, CARD, POCKET, TYPE MC-1 |
| MIL-I-21718 Base Document:1958 | Indicator, Airspeed, Pitot Static, Maximum Allowable Speed, 40-400 Knots |
| MIL-DTL-12216 Revision D:2007 | REFLECTOR, LIGHT: ALUMINUM, AND SHIELD, LIGHT: TELESCOPING, ALUMINUM |
| MIL-S-21277 Revision A:1958 | SWITCH, LIQUID LEVEL, GENERAL SPECIFICATION FOR |
| MIL L 81352 : A | LACQUER, ACRYLIC (FOR NAVAL WEAPONS SYSTEMS) |
| MIL-DTL-52525-45 Base Document:2008 | FITTINGS, HOSE, CRIMP TYPE, SPLIT-FLANGE, 90 DEGREES BENT TUBE |
| MIL-S-7470 Revision A:1975 | SHAFT, POWER TRANSMISSION, AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR |
| MIL-S-29398 Revision C:1984 | SLING SYSTEM, HELICOPTER EXTERNAL CARGO 40,000 POUND CAPACITY |
| MIL-DTL-52525-8 Revision C:2008 | Fittings, Hose, Screw-on to 37 Degree Flare Female Swivel, 90 DegreeBent Tube, Long Drop |
| MIL T 83174 : B (3) | TRANSMITTER, ACCELEROMETER, AXIAL |
| MIL-DTL-52525-39 Revision B:2008 | FITTINGS, HOSE, SCREW-ON TO 37DEGREES FLARE FEMALE SWIVEL, 90 DEGREES BENT TUBE |
| MIL S 8932 : A | SWITCH, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-85505 Base Document:1983 | ALTIMETER, STANDBY, TYPES 1 AND 2 |
| MIL-DTL-39030-8 Revision A:2003 | DUMMY LOAD, ELECTRICAL, COAXIAL, TYPE 4 (TNC), MEDIUM POWER |
| MIL-DTL-83798-8 Revision D:2017 | Fittings, Rubber Hose, Lightweight, Medium Pressure, Swivel Flange, 45 Degrees |
| MIL-A-27670 Revision D:1994 | AMPLIFIER-INDICATOR GROUP, INDICATED AIRSPEED A/A24G-10 |
| MIL S 3928 : D | SWITCH, (COAXIAL) RADIO FREQUENCY TRANSMISSION LINE, GENERAL SPECIFICATION FOR |
| MIL-A-83212 Revision A:1976 | ALTIMETER, PRESSURE AAU-27/A |
| 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 S 15291 : E | SWITCHES, ROTARY, SNAP ACTION AND DETENT/SPRING RETURN ACTION, GENERAL SPECIFICATION FOR |
| SAE AMS 2468 : 1999 | HARD ANODIC COATING TREATMENT OF ALUMINUM ALLOYS |
| 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 |
| MIL-R-81903 Revision A:1977 | REMOVER, ACID ACTIVATED, FOR AMINE CURED EPOXY COATING SYSTEMS |
| MIL-C-52978 Base Document:1980 | CHEST, COLLAPSIBLE TANK |
| MIL-DTL-52525-14 Revision C:2008 | FITTINGS, HOSE CRIMP TYPE, SPLIT-FLANGE 45 DEGREES BENT |
| MIL-DTL-83796-12 Base Document:2008 | HOSE ASSEMBLY, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, INTERNAL SUPPORT COIL, FIELD ATTACHABLE END FITTINGS, FLARELESS TO FLARELESS |
| MIL-I-83245 Revision A:1994 | INDICATOR SET, OIL PRESSURE A/A24J-17 |
| MIL D 26503 : A | DETECTOR, MAGNETIC AZIMUTH AND COMPENSATOR, DETECTOR, MAGNETIC AZIMUTH |
| 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-3443 Revision G:1993 | SHOTGUN, 12 GAGE, RIOT TYPE |
| MIL-P-6884 Revision F:1973 | PAINT, CAMOUFLAGE OR TEMPORARY IDENTIFICATION, SOLVENT REMOVABLE |
| MIL-STD-2193 Revision C:2012 | Ship Hydraulic System Components |
| MIL-R-81835 Base Document:1971 | REMOVER, ORGANIC COATING, HOT TANK TYPE |
| MIL-DTL-52525-42 Revision B:2008 | FITTINGS, HOSE, CRIMP TYPE, SPLIT-FLANGE 90 DEGREES BENT |
| MIL-DTL-52525-41 Revision A:2008 | FITTINGS, HOSE, CRIMP TYPE, SPLIT-FLANGE, 45 DEGREES BENT TUBE |
| MIL-D-60572 Revision B:1994 | DELAY ELEMENT, CARTRIDGE, M28 ASSEMBLY |
| MIL-R-25410 Revision G:1991 | REGULATORS, OXYGEN, DILUTER-DEMAND AUTOMATIC-PRESSURE BREATHING |
| TT-P-2760 Revision A:1994 | PRIMER COATING; POLYURETHANE, ELASTOMERIC |
| DOD-HDBK-343 Base Document:1986 | DESIGN, CONSTRUCTION, & TESTING REQUIREMENTS FOR ONE OF A KIND SPACE EQUIPMENT |
| SAE AS 4875 : 2016 | FITTINGS, STRAIGHT THREADED BOSS OR FLANGED, FLUID CONNECTION |
| MIL-S-7877 Revision B:1956 | Seat, Passenger, Cabin Folding |
| MIL-DTL-83798-2 Revision D:2017 | Fittings, Rubber Hose, Lightweight, Medium Pressure, Flared, Swivel Nut, 45 Degrees |
| MIL-DTL-13931 Revision J:1999 | Cannon: General Specification for |
| MIL-DTL-52525-12 Revision D:2011 | Fittings, Hose, Screw on to Split-Flange 90 Degree Bent |
| MIL-HDBK-1568 Base Document:1996 | MATERIAL AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS |
| MS27066 Revision F:2013 | Elbow Subassembly, Swivel Flange, 90 Degrees |
| MS27388 Revision D:2014 | ELBOW SUBASSEMBLY, FLARELESS, 90 DEGREES, SWIVEL NUT |
| 15/30327754 DC : 0 | BS EN 4660-004 - AEROSPACE SERIES - MODULAR AND OPEN AVIONICS ARCHITECTURES - PART 004: PACKAGING |
| SAE AS 6055 : 2006 | DRUM, METAL REUSABLE, SHIPPING AND STORAGE (CAP. FROM 88 TO 510 CUBIC INCHES) |
| MIL-I-27623 Revision C:1972 | INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
| 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-DTL-52525-33 Revision A:2008 | FITTINGS, WIRE REINFORCED HYDRAULIC HOSE AND CLAMP-HALVES: FIELD ATTACHABLE (REUSABLE), SCREW-ON TO 37 DEGREES FLARE FEMALE SWIVEL, 90 DEGREES BENT TUBE, FOR USE WITH TYPE 100RE FOUR-SPRIAL-WRAP REINFORCEMENT HOSE |
| MIL C 52404 : B | CONNECTIONS: HOSE, FIRE AND WATER |
| MIL L 25567 : D | LEAK DETECTION COMPOUND, OXYGEN SYSTEMS (METRIC) |
| MIL-M-24605 Revision A:1988 | MONITOR, HEAT STRESS |
| 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 26518 : B | CONNECTOR, ELECTRICAL, MINIATURE, RACK AND PANEL, ENVIRONMENT RESISTING, 2OO DEGREES C AMBIENT TEMPERATURE |
| A-A-2622 Revision A:1998 | ADAPTERS, PIPE TO HOSE, STRAIGHT OR REDUCING |
| MIL H 53027 : A | HOSE ASSEMBLY, RUBBER; LIGHTWEIGHT, COLLAPSIBLE, 6 INCH; FOR DRINKING (POTABLE) WATER |
| MIL-V-18318 Revision B:1966 | VALVE, PRESSURE REGULATING, OXYGEN SYSTEM |
| MIL T 53068 : 0 | TANKS, LIGHTWEIGHT, COLLAPSIBLE, PILLOW, 160 GALLON (NOMINAL), DRINKING WATER |
| MIL-T-26963 Revision D:1992 | TESTER, PRESSURE GAGE, HYDRAULIC, PORTABLE TYPE MP-1 |
| MIL I 45916 : B | INSERT,SCREW THREAD - THREAD CUTTING AND THREAD FORMING |
| MIL-G-81065 Revision A:1967 | GYRO-PENDULUM ASSEMBLY (FOR TORPEDO MK 46 MOD O AND MK 46 MOD 1) |
| MIL-I-25941 Revision D:1986 | INDICATOR, TURN AND SLIP, 2-INCH SIZE, INTEGRALLY LIGHTED |
| MIL S 8805/99 : F | SWITCHES, PUSH, 2 CIRCUIT AND DPDT, ALTERNATE AND MOMENTARY ACTION 2 AMPERES, WATERTIGHT, HIGH IMPACT SHOCK RESISTANT |
| MIL-DTL-28754-67 Revision A:2016 | CONNECTORS, ELECTRICAL, MODULAR, CONNECTOR FRAME, TYPE 4, DOUBLE SPAN, CENTER |
| MIL-C-87970 Base Document:1982 | CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
| 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-I-7084 Revision A:1988 | INDICATOR, PRESSURE, HYDRAULIC 0-4,000 PSI |
| MIL-I-27848 Revision B:1994 | INDICATOR, HORIZONTAL SITUATION AQU-4/A |
| MIL G 5413 : D NOTICE 1 | GENERATOR, TACHOMETER, FOUR POLE |
| MIL P 23377 : G | PRIMER COATING, EPOXY, HIGH SOLIDS |
| MIL-F-5504 Revision B:1958 | Filters and Filter Elements, Fluid Pressure, Hydraulic Micronic Type |
| MIL-G-25591 Revision E:1981 | Gyroscope, Rate, Switching, Type MC-1 |
| MIL-DTL-24251-5 Revision D:2013 | SHIELD, ELECTRON TUBE, HEAT DISSIPATING, 7 AND 9 PIN, MINIATURE (OPEN SIDES) |
| MIL T 25435 : B | TRANSMITTER, PRESSURE, AIRCRAFT, VARIABLE RELUCTANCE TYPE, GENERAL SPECIFICATION FOR |
| MIL-I-5415 Revision C:1987 | INDICATOR, AIR SPEED, PITOT STATIC PRESSURE GENERAL SPECIFICATION FOR |
| MIL-A-27671 Revision B:1965 | AMPLIFIER-INDICATOR GROUP, ALTITUDE VERTICAL SPEED A/A24G-11 |
| MIL-H-9859 Revision A:1968 | HANDWHEEL, ORDNANCE |
| MIL-B-21902 Revision A:1963 | |
| MIL-I-38258 Base Document:1965 | INDICATOR, ATTITUDE ARU 18/A DIRECTOR |
| MIL-DTL-32175 Base Document:2004 | FUZE, PIBD - M549A1, LESS SPITBACK ASSEMBLY |
| MIL-DTL-60982 Revision C Interim Revision:2004 | Case Cartridge, 40 Millimeter - M169 Loading, Assembling, Packing |
| MIL-C-87975 Base Document:1985 | CLOCK, AIRCRAFT, MECHANICAL ABU-32/A |
| MIL F 52618 : D | FITTING, PIPE, ALUMINUM ALLOY (THREADED) 150 POUND, GENERAL SPECIFICATION FOR |
| MIL M 62361 : C | MOTOR, DRIVE, DIRECT CURRENT 2 RPM/8RPM |
| NASA MSFC PROC 547 : 2014 | POLYURETHANE COATING, APPLICATION OF |
| MIL-A-82151 Revision B:1989 | ANTENNA: AS-2236, 30 TO 76 MEGAHERTZ |
| MIL-DTL-25708-1 Revision H:2012 | ANTENNA, BLADE, AT-741B/B (HN CONNECTOR) |
| MIL-DTL-25707-2 Revision C:2015 | ANTENNA, FLUSH MOUNT (RADIUS OF CURVATURE - 14.90 INCHES) |
| MIL S 21604 : D | SWITCHES, ROTARY, MULTIPOLE AND SELECTOR - GENERAL SPECIFICATION FOR |
| MS28755 Revision E:2012 | FITTING END, SELF-SEALING FUEL HOSE, SWIVEL, DETACHABLE, FLANGED, 90 DEGREES |
| MIL-C-23157 Revision D:1979 | CLIPBOARD, PILOTS, MXU-163/P AND MARK 2A |
| MIL-I-27619 Revision G:1974 | INDICATORS, ATTITUDE DIRECTOR |
| MIL-C-5414 Revision G:1993 | COMPUTER, AIR NAVIGATION DEAD RECKONING TYPE MB 4A AND TYPE CPU 26A/P |
| MIL-PRF-85582 Revision E:2012 | PRIMER COATINGS: EPOXY, WATERBORNE |
| MIL-DTL-52525-4 Revision D:2011 | Fittings, Hose, Screw-on to 37 Degree Flare Female Swivel, 90 Degree Bent Tube, Long Drop |
| MIL-T-5583 Revision C:1987 | Transmitter, Position, 28 Volts DC |
| MIL W 6496 : B NOTICE 1 | WINCH, DRUM, ENGINE OF TURRET HOIST, TYPE A-1 |
| MIL-M-7969 Revision C:1965 | Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for |
| MIL-DTL-83798-6 Revision D:2017 | Fittings, Rubber Hose, Lightweight, Medium Pressure, Flareless, Swivel Nut, 90 Degrees |
| MIL-C-38207 Revision A:1965 | CLOCK, AIRCRAFT, MECHANICAL ABU 11/A |
| MIL-DTL-6839 Revision E:2011 | INDICATOR, POSITION, LANDING GEAR |
| MS27386 Revision C:2013 | Nipple Subassembly, Flareless, Straight - with Swivel Nut |
| MIL I 27851 : B | INDICATOR, INDICATED AIRSPEED AVU-17/A |
| MIL-T-25307 Revision D:1985 | TRANSMITTER, PRESSURE, HYDRAULIC, TYPE MJ-1 |
| MIL A 25949 : E (2) | ACCELEROMETER, AIRCRAFT RANGE -5 TO PLUS 1OG UNITS, INTEGRALLY LIGHTED |
| MIL-C-45408 Revision C:1992 | CARTRIDGE, IMPULSE, M44A1 ASSEMBLY |
| MIL-I-25437 Revision B:1984 | INDICATORS, AIRCRAFT, PRESSURE, VOLTAGE RATIO TYPE, GENERAL SPECIFICATION FOR |
| MIL-P-6906 Revision B:1969 | PLATE, IDENTIFICATION AIRCRAFT |
| MIL-A-58066 Revision A:1966 | ALTIMETER, PRESSURE, PARACHUTIST'S |
| MIL-I-8974 Revision A:1981 | INDICATOR, EVENT COUNTING, GENERAL SPECIFICATION FOR |
| MIL M 62368 : A | MOTOR, GEARHEAD, 18-30 VOLTS, DIRECT CURRENT |
| MIL-A-43326 Revision A:1983 | ALTAR, PORTABLE |
| AA-S-271 Revision D:1967 | SHELVING, STORAGE AND DISPLAY, STEEL, INTERCHANGEABLE, NUT AND BOLT TYPE |
| MIL-DTL-28754-70 Revision A:2015 | CONNECTORS, ELECTRICAL, MODULAR, CONNECTOR FRAME, TYPE 4, SINGLE SPAN, CENTER |
| NASA KSC STD Z 0008 : 1996 | DESIGN OF GROUND LIFE SUPPORT SYSTEMS AND EQUIPMENT, STANDARD FOR |
| MIL-P-14250 Revision C:1981 | PIN, STRAIGHT, HEADED AND PIN, STRAIGHT, HEADLESS, SLOTTED TEMPLET STUD |
| MIL-DTL-28754-68 Revision A:2015 | CONNECTORS, ELECTRICAL, MODULAR, CONNECTOR FRAME, TYPE 4, DOUBLE SPAN, T-DIP |
| MIL L 25866 : B | LIGHT, EMERGENCY EXIT, AIRCRAFT LEU AND 1-A |
| MIL-I-23524 Revision A:1986 | INDICATOR, ATTITUDE DIRECTOR, REMOTE, ID 1329A (V) |
| MIL-A-53099 Base Document:1990 | ARCTIC FORWARD AREA REFUELLING EQUIPMENT (AFARE) |
| MIL-V-85830 Base Document:1989 | VENTILATOR, TACTICAL, HELICOPTER AIRCREWMEN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE |
| MIL-DTL-38999-46 Revision B:2008 | CONNECTORS, ELECTRICAL, CIRCULAR, PLUG, BREECH COUPLING, EMI GROUNDING, REMOVABLE CRIMP CONTACTS, SERIES 4 METRIC |
| MIL-PRF-32587 Base Document:2018 | Remover, Paint, Hap-Free, Neutral |
| DOD-C-85050 Base Document:1982 | CHARGERS, BATTERY, NICKEL-CADMIUM, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL C 7115 : F | CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-I-23832 Revision A:1980 | Indicator, Tachometer, Triple Pointer, Helicopter |
| NASA STD 6002 : 2008 | APPLYING DATA MATRIX IDENTIFICATION SYMBOLS ON AEROSPACE PARTS |
| 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-P-24764 Base Document:1991 | POWER SUPPLIES, SHIPBOARD, ELECTRONIC, GENERAL SPECIFICATION FOR |
| MIL-T-10629 Revision C:1978 | T-SQUARE [STEEL] |
| MIL C 28748/7 : E | CONNECTOR, ELECTRICAL, RECTANGULAR, RACK AND PANEL, SOLDER TYPE PIN CONTACTS, SIZE 22 |
| MIL-DTL-24251-6 Revision E:2013 | SHIELD, ELECTRON TUBE, HEAT DISSIPATING, 7 AND 9 PIN, MINIATURE (RETROFIT TYPE ONLY) |
| MIL I 27190 : B | INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI |
| MIL-D-38134 Revision A:1971 | DETECTOR, MAGNETIC AZIMUTH DSU-4/A, HIGH TEMPERATURE |
| MIL-I-26299 Revision G:1990 | INDICATORS, RATE OF FLOW, 0-5,000 PPH, INTEGRALLY LIGHTED |
| MIL-DTL-25707-3 Revision C:2011 | ANTENNA, FLUSH MOUNT (RADIUS OF CURVATURE - 66.50 INCHES) |
| MIL-T-5420 Revision B:1970 | TUBE, PITOT STATIC, ELECTRICALLY HEATED, AIRCRAFT |
| MIL C 38333 : 0 | CONTROLLER, COMPASS SYSTEM C-6448/ASN-55 |
| MIL-P-38268 Revision C:1988 | AURAL PROTECTORS, SOUND |
| MIL L 46138 : 0 | LACQUER, LUSTRELESS, ACRYLIC NITROCELLULOSE, SOLAR HEAT REFLECTING, OLIVE DRAB |
| MIL R 6466 : B NOTICE 1 | RELAY, ARMATURE, EXCITER PROTECTION, TYPE A-1 |
| MIL-I-7906 Revision A:1961 | INDICATOR, GYRO HORIZON, MANUALLY CAGED, ELECTRIC, TYPE MB 1 |
| MIL C 25531 : D | COUPLING HALF, QUICK DISCONNECT, PNEUMATIC STARTER, EXTERNAL, LOW PRESSURE, DIRECT RELEASE |
| MIL-T-23397 Revision B:1970 | TAPE, PRESSURE-SENSITIVE ADHESIVE, FOR MASKING DURING PAINT STRIPPING OPERATIONS |
| MIL-DTL-83798-7 Revision D:2017 | Fittings, Rubber Hose, Lightweight, Medium Pressure, Swivel Flange, Straight |
| MIL E 24127 : 0 | EDUCTORS; GASOLINE, OIL, OR WATER |
| MIL-DTL-85855 Revision A:1999 | VALVE, QUICK DISCONNECT, FOR THE PROTECTIVE ASSEMBLY, CHEMICAL, BIOLOGICAL, RADIOLOGICAL (CBR), A/P22P-9 (V) |
| MIL D 9555 : A NOTICE 1 | |
| MIL-DTL-25866 Revision C:2010 | LIGHT, EMERGENCY EXIT, AIRCRAFT LEU-1/A |
| MIL-DTL-28754-21 Revision F:2014 | Connectors, Electrical, Modular, Frame, Casting, Type IV, Double Span |
| MIL-C-47121 Base Document:1974 | COMPOUND, SEALING, POLYSULFIDE RUBBER |
| MIL-DTL-27190 Revision C:2006 | INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI |
| MIL I 83361 : (4) | INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
| MIL-B-8621 Revision A:1964 | Board, Chart, Mark 6A, Mark 6B and Mark 6C |
| MIL F 18953 : B | FAN, VANEAXIAL AND TUBEAXIAL, FIXED AND PORTABLE, VENTILATION, NAVAL SHIPBOARD |
| MIL-S-24317-12 Revision B:2006 | Switch, Multistation, Pushbutton, Illuminated Matrix Arrangement, Sunlight Readable, 4 Lamp, Plug-In Module, Style SM12L1 (No S/S Document) |
| MIL-L-24560-25 Base Document:1990 | LIGHT, TASK AND SHIELD ASSEMBLY FOR USE WITH SYMBOL 114.1 AND 115.1 PLASTIC LIGHT FIXTURES |
| MIL-DTL-26517 Revision B:2000 | Power Supply, Transformer-Rectifier, Aircraft, General Specification for |
| MIL-DTL-83796-2 Revision C:2014 | HOSE ASSEMBLY, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, FIELD ATTACHABLE END FITTINGS, FLARE TO FLARE, WITH LOCKWIRE HOLE |
| MIL M 5388 : B | MACHMETER; PITOT STATIC OPERATED, RANGE 0.5 TO 1.5, TYPE A-2B |
| MIL-R-24243 Revision C:1987 | RIVET, BLIND, NON-STRUCTURAL, RETAINED MANDREL, GENERAL SPECIFICATION FOR |
| MIL-PRF-87937 Revision D:2001 | CLEANING COMPOUND, AEROSPACE EQUIPMENT |
| MS27395 Revision D:2014 | ELBOW, FLARELESS, TUBE TO HOSE - 45 DEGREES SWIVEL NUT |
| MS27084 Revision D:2014 | ELBOW, NIPPLE END, SWIVEL FLANGE TO HOSE - 45 DEGREES |
| MIL-C-46274 Revision C:1992 | CARTRIDGE, IMPULSE, M94 ASSEMBLY |
| MIL-DTL-83798-1 Revision D:2017 | Fittings, Rubber Hose, Lightweight, Medium Pressure, Flared, Swivel Nut, Straight |
| MIL-C-60575 Revision A:1992 | CARTRIDGE, THRUSTER, M141 ASSEMBLY |
| MIL-W-5013 Revision L:1991 | WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-C-46221 Revision B:1992 | CARTRIDGE, IMPULSE, M37 ASSEMBLY |
| MIL F 14072 : D | FINISHES FOR GROUND BASED ELECTRONIC EQUIPMENT |
| MIL-P-85576 Revision B:1987 | POWER SUPPLY PP-2581C/A |
| MIL-DTL-83798-3 Revision D:2017 | Fittings, Rubber Hose, Lightweight, Medium Pressure, Flared, Swivel Nut, 90 Degrees |
| MIL-DTL-27193 Revision D:2017 | INDICATOR, ATTITUDE ARU-2B/A |
| MIL T 25627 : C | TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |
| MIL-DTL-28748-7 Revision F:2009 | CONNECTORS, ELECTRICAL, RECTANGULAR, RACK AND PANEL, SOLDER TYPE PIN CONTACTS, SIZE 22 |
| MIL-DTL-60567 Revision C:2005 | DELAY ELEMENT, CARTRIDGE, M14 ASSEMBLY |
| MIL-C-53071 Base Document:1987 | COUPLING ASSEMBLIES, QUICK-DISCONNECT, SEXLESS TYPE |
| MIL-A-27391 Revision B:1963 | ALTIMETER, PRESSURE AAU-2A |
| MIL C 28754/22 : G | CONNECTOR, ELECTRICAL, MODULAR, FRAME, CASTING, TYPE 4, SINGLE SPAN |
| NASA STD 6012 : 2012 | CORROSION PROTECTION FOR SPACE FLIGHT HARDWARE |
| MIL-P-8793 Revision A:1961 | PAINT, [GLOSS AND NONSPECULAR] FOR USE ON ELASTOMERIC PIGMENTED FILM [ASG] |
| MIL-DTL-24356 Revision B:2017 | Couplings and Split Clamps, 2½-, 4-, 6-, and 7-Inch Segmented, Reattachable, for Refueling-At-Sea Hose |
| SAE AS 5272 : 2016 | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING, PROCUREMENT SPECIFICATION |
| SAE AMS 3144 : 2012 | PRIMER, ANODIC ELECTRODEPOSITION FOR AIRCRAFT APPLICATIONS |
| SAE AS 38404 : 2013 | COUPLINGS, HOSE, REATTACHABLE SCREW-ON |
| NAS1599:1980 | CONNECTORS, GENERAL PURPOSE, ELECTRICAL, MINIATURE CIRCULAR, ENVIRONMENT RESISTING, 200 DEG. C. MAXIMUM TEMPERATURE |
| SAE AMS R 81835 : 2008 | REMOVER, ORGANIC COATING, HOT TANK TYPE |
| SAE ARP 4118 : 2013 | ISOLATION AND CORROSION PROTECTION OF DISSIMILAR MATERIALS, CARBON COMPOSITE STRUCTURE REPAIR |
| SAE AS 916 : 2016 | OXYGEN FLOW INDICATORS |
| SAE AS 95234 : 2014 | CONNECTORS, ELECTRICAL, REVERSE BAYONET, GENERAL SPECIFICATION FOR |
| SAE AS 1946 : 2015 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, UP TO 1500 PSI AND 450 DEGREES F, HYDRAULIC AND PNEUMATIC |
| ASTM D 2651 : 2001 : R2016 | Standard Guide for Preparation of Metal Surfaces for Adhesive Bonding |
| I.S. EN 4473:2010 | AEROSPACE SERIES - ALUMINIUM PIGMENTED COATINGS FOR FASTENERS - TECHNICAL SPECIFICATION |
| BS EN 6069:2009 | Aerospace series. Rivet, 100° reduced flush head, close tolerance. Inch series |
| PREN 6080 : 200P3 | AEROSPACE SERIES - RIVET, 100 DEGREES NORMAL FLUSH HEAD, CLOSE TOLERANCE - INCH SERIES |
| PREN 6081 : 200P2 | AEROSPACE SERIES - RIVET, UNIVERSAL HEAD, CLOSE TOLERANCE - INCH SERIES |
| DSCC 85033 : H | HOLDER, ELECTRICAL CARD, METAL CARD GUIDE, ZERO INSERTION FORCE |
| DSCC 89024 : E | HOLDER, ELECTRICAL CARD, WEDGE RETAINER, 5-PIECE, .250 INCH BY .260 INCH BODY SIZE |
| PREN 4473 : 200P2 | AEROSPACE SERIES - ALUMINIUM PIGMENTED COATINGS FOR FASTENERS - TECHNICAL SPECIFICATION |
| MIL P 85582 : B | PRIMER COATINGS: EPOXY, WATERBORNE |
| MIL P 23377 : G | PRIMER COATING, EPOXY, HIGH SOLIDS |
| ASTM D 2244 : 2016 : REDLINE | Standard Practice for Calculation of Color Tolerances and Color Differences from Instrumentally Measured Color Coordinates |
| ASTM G 26 : 1996 | Practice for Operating Light-Exposure Apparatus (Xenon-Arc Type) With and Without Water for Exposure of Nonmetallic Materials (Withdrawn 2000) |
| ASTM G 23 : 1996 | Practice for Operating Light-Exposure Apparatus (Carbon-Arc Type) With and Without Water for Exposure of Nonmetallic Materials (Withdrawn 2000) |
| FED-STD-141 Revision D:2001 | PAINT, VARNISH, LACQUER AND RELATED MATERIALS, METHODS OF INSPECTION, SAMPLING AND TESTING |
| MIL-STD-105 Revision E:1989 | SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES |
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