MIL-S-7742 Revision D:1991
Current
Current
The latest, up-to-date edition.
Screw Threads, Standard, Optimum Selected Series: General Specification for
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Published date
25-07-1991
Publisher
€16.67
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Covers requirements for selected series of Unified and Unified Miniature screw threads and gaging practice to determine conformance. Coverage includes applicable documents, miniature thread designation, basic thread data, pitch diameter, taper, incomplete threads, lead threads, runout, surface roughness, responsibility for inspection, lot quantities, and inspection methods.
| DocumentType |
Standard
|
| Pages |
20
|
| ProductNote |
NEW CHILD NOT 1 2019 IS NOW ADDED.
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification covers the requirements for a selected series of standard Unified and Unified Miniature screw threads, classes 3A and 3B of Fed-std-H28/2 and FED-STD-H28/5 for general aerospace and similar high-tech application.
| MIL-I-85889 Base Document:1988 | IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL C 38240 : C | COMPUTER, ALTITUDE, ALTITUDE ENCODING CPU 66, GENERAL SPECIFICATION FOR AND MTU 39/A MOUNTING TRAY |
| MIL-I-8580 Revision B:1965 | Indicator, Tachometer, Helicopter, 0-4000 RPM, Type MA-1 (No S/S Document) |
| MIL-T-5842 Revision B:1985 | Transparent Areas On Aircraft Surfaces (Windshields And Canopies), Rain Removing And Washing Systems For, De-Frosting, De-Icing, Defogging, General Specification For |
| MIL-T-38034 Revision E:1970 | TIMER, FIRE CONTROL, BOMBING, DUAL (NO S/S DOCUMENT) |
| MIL-A-38307 Revision A:1981 | Accelerometer, Aircraft MX-6663/AJB-7 (No S/S Document) |
| MIL-P-81655 Base Document:1970 | Pitot Static Tube, L-Shaped, Compensated, Electrically Heated, General Specification for |
| MIL C 27599 : B | CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT, ENVIRONMENTAL RESISTANT, SOLDER CONTACTS GENERAL SPECIFICATION FOR |
| SAE AS8181A | Detector, Ice, Air Intake Duct, Aircraft Engines and Airframe Systems, General Specification For |
| MIL T 5578 : C | TANK, FUEL, AIRCRAFT, SELF-SEALING |
| MIL-A-83577 Revision B:1988 | Assemblies, Moving Mechanical, for Space and Launch Vehicles, General Specification for (No S/S Document) |
| MIL-I-7062 Revision C:1975 | Indicator, Position, Control Surfaces, 28 Volt DC, General Specification for |
| MIL-C-5809 Revision G:1987 | Circuit Breakers, Trip-Free, Aircraft, General Specification for (S/S by SAE-AS58091) |
| MIL-E-23001 Revision B:1976 | Electric Generating System, Variable Speed Constant Frequency, Aircraft, General Specification for (S/S by MIL-E-85583) |
| MIL T 6396 : E | TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
| MIL F 27272 : B | FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL T 27252 : A | TEST SET, SYNCHRO, TTU-73/E DC SELSYN, AIRCRAFT INSTRUMENTS |
| MIL-M-8555 Revision C:1984 | Missile, Guided, Design and Construction, General Specification for (No S/S Document) |
| MIL-T-83460 Base Document:1975 | TRANSDUCER, MOTIONAL PICKUP TRU-164/A (NO S/S DOCUMENT) |
| MIL I 7627 : F | INDICATOR, TURN AND SLIP 28V DC |
| MIL-I-83152 Revision B:1974 | Indicator, Indicated-Airspeed AVU-22/A (Indicator-Transducer) |
| MIL-I-7721 Revision D:1992 | Indicator, Vertical Speed, 3-Inch |
| MIL-A-85055 Base Document:1979 | Avionics System Performance Specification for A-4M/AV-8 Bombing Set, Angle Rate AN/ASB-19(V) |
| MIL-R-8236 Revision F:1995 | Reel, Shoulder Harness, Inertia Lock |
| MIL I 25688 : A | INDICATOR, ELECTRICAL TACHOMETER ERU-3/A. CRANKSHAFT SPEED 500-4,000 RPM, 3 1/4 INCH SIZE |
| MIL I 27197 : C | INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
| MIL-C-81703 Base Document:1971 | Connectors, Electric, Circular, Miniature, Rack and Panel or Push-Pull Coupling, Environment Resisting (S/S by SAE-AS81703) |
| MIL-A-5885 Revision D:1987 | Accelerometer, Aircraft (No S/S Document) |
| MIL D 83320 : 0 | DETECTOR, MAGNETIC AZIMUTH DSU-14/A |
| MIL C 38214 : B | COMPASS, MAGNETIC,MOUNTED |
| MIL-P-9388 Revision B:1986 | Pump, Pressure, Oil Free Air Type MA-2 (No S/S Document) |
| MIL-T-5483 Revision D:1964 | Transmitter, Pressure, Synchro, Aircraft, 165 Degree Movement (No S/S Document) |
| MIL-I-85071 Revision A:1992 | Inverters, Aircraft, DC to AC, General Specification for (S/S by MIL-PRF-7032) |
| MIL-STD-7080 Base Document:1994 | Selection and Installation of Aircraft Electric Equipment |
| MIL-DTL-27188 Revision C:2006 | Indicator, Pressure EGU-2/A, Oil, 0-100 PSI |
| MS28052 Revision C:2011 | Valve, Check, Pressure Gage Lines Bleeder and Filler (No S/S Document) |
| MIL-DTL-32546 Base Document:2016 | Connectors, Electrical, Circular, for High-Speed Data Bus Transmission, Copper Conductor, General Specification for |
| MIL-C-27298 Revision B:1980 | Clock, Aircraft, Mechanical ABU-9-A |
| MIL-T-38473 Revision A:1972 | Timer, Precision, Bombing, 0 - 30 Minutes (No S/S Document) |
| MIL-C-8605 Revision B:1990 | Cap; Pressure Fuel Servicing |
| MIL-A-38140 Revision B:1977 | Altimeter, Pressure AAU-16/A (No S/S Document) |
| MIL H 81014 : A NOTICE 1 | HOOK, HELICOPTER, EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C |
| MIL-I-8691 Revision A:1955 | Indicator, Azimuth, ID-307/ARN (ASG) |
| MIL-G-25597 Revision D:1973 | Gyroscope, Displacement, Roll and Pitch, Type MD-1 |
| MS123142 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 2 3/8 Inch, Aluminum |
| MIL-L-50794 Base Document:1973 | Linear Shaped Charge Assembly |
| MIL-I-81186 Base Document:1966 | Indicator, Rate of Fuel Flow Synchro Type, M590360 |
| MS123122 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 3/8 Inch, Aluminum |
| MS123133 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 1 5/16 Inch, Aluminum |
| MS25048 Revision B:2005 | Mast, Antenna, Dead-End |
| MIL-M-7255 Revision B:1969 | Manometer, Pressure, Differential and Absolute, Type E-1 (No S/S Document) |
| MIL-I-27709 Revision A:1962 | Indicator, Altitude, ARU-14/A, Remote (No S/S Document) |
| MIL-G-7818 Base Document:1951 | Gage, Fuel Quantity, Capacitor Type, Compensated, General Specification for |
| MIL-E-5627 Revision B:1965 | Extinguishers, Fire, Carbon Dioxide, Portable (No S/S Document) |
| MIL-DTL-22992 Revision H:2015 | Connectors, Plugsand Receptacles, Electrical, Waterproof, Quick Disconnect, Heavy Duty Type, General Specification for |
| MIL P 83207 : B | PITOT STATIC TUBE, NOSE BOOM, COMPENSATED, GENERAL SPECIFICATION FOR |
| MIL-A-55503 Base Document:1966 | Attitude Heading Reference Set AN/ASN-76 (No S/S Document) |
| MIL-I-38338 Revision D:1991 | Indicator, Oil Quantity, Continuous Transmission, Nucleonic |
| MIL T 8878 : D | TURNBUCKLE, POSITIVE SAFETYING |
| MIL T 781 : D | TERMINAL, WIRE ROPE, SWAGING |
| MIL-W-48381 Base Document:1974 | Warhead Section, GM, Practice, Lightweight, M252E1 Parts And Assembling |
| MIL V 27166 : D | VALVE, PRESSURE EQUALIZING, GASEOUS PRODUCTS |
| MIL-I-27196 Revision C:1988 | Indicator, Vertical Velocity AAU-9/A, Integrally Lighted |
| MIL I 27279 : B | INDICATOR, MACH NUMBER AVU-11/A, INTEGRAL LIGHTING |
| MIL-I-27202 Revision A:1980 | Indicator, Electrical Tachometer, 0-110 Percent RPM 2-Inch Size, Integrally Lighted |
| DOD-E-83578 Revision A:1987 | EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) (NO S/S DOCUMENT) |
| MIL T 25627 : C | TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |
| MIL-A-24366 Base Document:1969 | Amplifier System, Audio, Low Noise, High Input Impedance (No S/S Document) |
| MIL-C-23367 Base Document:1963 | Computer, Flight Director, Aircraft |
| MIL-DTL-25949 Revision F:1995 | Accelerometer, Aircraft Range -5 to 10G Units, Integrally Lighted |
| MIL I 45932 : 0 | INSERT, SCREW THREAD, THIN WALL, LOCK IN |
| BS EN 6105:2016 | Aerospace series. Stud with shoulder |
| MS24357 Revision B:2016 | Flange, Drogue Cone - Type MA-2 Reception Coupling, Flight Pressure Refueling, Outline Dimensions for |
| MIL-N-45938 Revision A:1995 | NUT, PLAIN, CLINCH AND NUT, SELF-LOCKING, CLINCH, GENERAL SPECIFICATION FOR (S/S BY NASM45938) |
| MS 124691 124730 : E | INSERT, CRES HELICAL COIL FINE THREAD, 1-1/2 DIA NOMINAL LENGTH |
| MIL-DTL-27272 Revision D:2015 | Fittings, Polytetrafluoroethylene Hose, High-Temperature, Medium-Pressure, General Specification for |
| MIL-S-21472 Revision C:1988 | SCREW, SHOULDER, HEXAGON SOCKET-HEAD AND SLOTTED-HEAD GENERAL SPECIFICATION FOR (S/S BY NASM21472) |
| MIL-S-45909 Revision C:1989 | STUD, LOCKED IN, RING LOCKED, SERRATED, GENERAL SPECIFICATION FOR (S/S BY NASM45909) |
| MIL-C-19179 Revision B:1963 | Coupling Assembly, Quick-Disconnect, Fuel (S/S by MIL-C-24788) |
| MS27559 Revision E:2009 | Support, Cable, Right Angle |
| MIL-DTL-25531 Revision F:2013 | Coupling Half, Quick Disconnect, Pneumatic Starter, External, Low Pressure |
| MS27558 Revision E:2009 | Support, Cable, Right Angle, Closed |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL-S-7839 Revision B:1973 | SCREW, STRUCTURAL, AIRCRAFT (S/S BY NASM7839) |
| MS122116THRUMS122155 Revision D:1976 | INSERT CRES HELICAL COIL COARSE THREAD 1 1/2 DIA. NOMINAL LENGTH (S/S BY NASM122116THRU122155) |
| MIL T 28800 : E | TEST EQUIPMENT FOR USE WITH ELECTRICAL AND ELECTRONIC EQUIPMENT GENERAL SPECIFICATION FOR |
| MIL-DTL-25027 Revision H:1997 | Nut, Self-Locking 250 Degree F, 450 Degree F, and 800 Degree F (S/S by NASM-25027) |
| MIL-DTL-5099 Revision C:2011 | Indicator, Cabin Air Pressure, 1-7/8 Inch Dial, Type MA-1 |
| MIL-B-7838 Revision C:1989 | Bolt, Internal Wrenching, 160 KSI FTU (S/S by NASM7838) |
| MIL V 5523 : D | VALVE, RELIEF, HYDRAULIC PRESSURE |
| MS124731THRUMS124770 Revision D:1976 | INSERT, CRES HELICAL COIL FINE THREAD, 2 DIA NOMINAL LENGTH (S/S BY NASM124731THRU124770) |
| MIL-R-85880 Base Document:1988 | ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL-S-26547 Revision C:1985 | Starter-Generator Engine STU-6A |
| MIL-M-9397 Revision E:1979 | Frequency Converter, Mobile, Type MC-1A |
| MIL-I-6447 Revision C:1974 | Indicator, True Airspeed, Type M-1A (No S/S Document) |
| MIL-V-25023 Revision B:1967 | Valve, Fuel Drain, Self-Locking |
| MIL-G-19053 Revision C:1957 | GAGE - AIRCRAFT, CAPACITANCE, LIQUID OXYGEN CONVERTER, GENERAL SPECIFICATION FOR |
| SAE AS5590A | Connectors, Fiber Optic, Advanced, Circular or Rectangular, Plug and Receptacle, Environment Resistant, Removable Termini/Contacts, General Specification For |
| MS33786 Revision B:2013 | Fitting, Installation, Flared Tube and Hose, Swivel |
| MIL-M-8609 Revision B:1965 | Motor, DC, 28 Volt System, Aircraft, General Specification for |
| MIL-C-81511 Revision F:1992 | Connectors, Electrical, Circular, High Density, Quick Disconnect, Environment Resisting: and Accessories General Specification for (S/S by SAE-AS81511) |
| MIL R 23016 : A | RADIO SET AN/ARC-94 |
| MIL-A-6752 Revision A:1953 | Ammeters, Voltmeters, and Loadmeters; Direct Current |
| MIL-C-85049 Revision A:1990 | Connector Accessories, Electrical General Specification for (S/S by SAE-AS85049) |
| MIL-A-19736 Revision A:1960 | Air Refueling Systems, General Specification for |
| MIL-E-50796 Base Document:1973 | Expanding Shielded Mild Detonating Cord Assembly |
| MIL C 7958 : A | CONTROL, PUSH PULL, FLEXIBLE AND RIGID |
| MS123134 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 1 3/8 Inch, Aluminum |
| MIL H 81529 : 0 | HOOK, HELICOPTER EXTERNAL CARGO, 6,000 POUND CAPACITY TYPE A |
| MIL R 83178 : A | REGULATOR, OXYGEN, DILUTER DEMAND, AUTOMATIC PRESSURE BREATHING, GENERAL SPECIFICATION FOR |
| MIL-I-25091 Revision B:1985 | Indicator, Cabin Air Pressure, Pressurized Aircraft, 1-7/8 Inch Dial, Type MA-2 |
| MIL 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 26611 : D | GENERATOR, TACHOMETER GEU-7/A, MINIATURE |
| MIL-G-23337 Base Document:1962 | Gages, Pressure, Dial Indicating |
| MIL-A-6589 Revision A:1968 | Amplifier, Electronic Control, Single Channel, Type A-2 (No S/S Document) |
| MIL-C-6100 Revision A:1973 | Connector, Receptacle, Electrical, Aircraft (No S/S Document) |
| MIL P 26517 : A | POWER SUPPLY, TRANSFORMER-RECTIFIER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-T-19576 Revision A:1961 | TRANSMITTER, REMOTE COMPASS, THIN WING TYPE ML-1 (UNSTABILIZED) (NO S/S DOCUMENT) |
| MS24588 Revision C:2007 | Nipple, Adapter, Hose to Tube, Reusable, Hydraulic, Fuel and Oil Lines, 3/16 through 3/4 Inch Tubing Sizes |
| MIL-R-6518 Revision A:1953 | RELAY, ARMATURE, TYPE A-1 (NO S/S DOCUMENT) |
| MS123130 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 1 1/16 Inch, Aluminum |
| MS123138 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 1 7/8 Inch, Aluminum |
| MIL C 45918 : 0 | CLEVISES AND CONNECTORS (ROD END) |
| MIL-I-5133 Revision C:1953 | Indicator, Attitude, Type J-8 (No S/S Document) |
| MIL-B-81365 Base Document:1966 | Bleed Air Systems, General Specification for |
| MIL-B-83769 Revision D:1983 | Batteries, Storage, Lead-Acid, General Specification for (No S/S Document) |
| MIL C 38999 : J | CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET THREADED & BREECH COUPLING) ENVIRONMENT RESISTANT, REMOVABLE CRIMP & HERMETIC SOLDER CONTACTS |
| MIL-R-23761-2 Revision B:1991 | Regulators, Voltage, Aircraft Direct Current Generator, 28-Volt |
| MIL-C-5604 Revision B:1962 | Compass, Magnetic, Pilot\'s Standby (S/S by SAE-AS5604) |
| MIL L 38671 : A | LUG, SUSPENSION, BOMB MAU-129/A, "T" TYPE |
| MS25051 Revision B:2014 | Insert, Dead-End, Antenna |
| MIL-I-23870 Base Document:1963 | Indicator, Fuel Rate of Flow, 0 to 15 GPM (No S/S Document) |
| MIL-C-9082 Revision H:1986 | Converter, Oxygen, Aircraft, Liquid to Gaseous, General Specification for (No S/S Document) |
| MIL-C-24360 Revision A:1969 | Cable Assembly, Aircraft Autonavigator Alignment, Umbilical (No S/S Document) |
| 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 VOLTS DC (NO S/S DOCUMENT) |
| MIL-S-83427 Base Document:1974 | Survival Kit Containers, CNU-129(V)/P and CNU-130/P |
| MIL C 38271 : B | CONNECTOR, OXYGEN MASK TO REGULATOR CRU-60/P |
| MIL L 58085 : A | LIGHT, BEACON, ANTI COLLISION AIRCRAFT |
| MIL-H-8890 Base Document:1961 | Hydraulic Components, Type III (-65 Degrees to Plus 450 Degrees F) General Specification for (ASG) |
| MIL-P-8564 Revision D:1970 | Pneumatic System Components, Aeronautical, General Specification for |
| MIL I 38715 : B | INDICATOR, COMBUSTIBLE GAS AND TOXIC GAS |
| MIL-DTL-25469 Revision J:2014 | Valves, Filler, Liquid Oxygen, Aircraft Type |
| MIL C 4928 : A | CHARGER, BATTERY, SILICON DIODE, TYPE A-1 |
| MIL C 83723 : E | CONNECTORS, ELECTRICAL (CIRCULAR, ENVIRONMENT RESISTING) RECEPTACLES AND PLUGS GENERAL SPECIFICATION FOR |
| SAE AS7481C | Studs, Steel, UNS S66286 Aged After Roll Threaded Procurement Specification For |
| SAE AS81703A | Connectors, Electric, Circular, Miniature, Rack and Panel or Push-Pull Coupling, Environment Resisting |
| I.S. EN 6105:2016 | AEROSPACE SERIES - STUD WITH SHOULDER |
| SAE AS39901B | Bearings, Roller, Needle, Airframe, Antifriction, Inch |
| SAE AS50151C | Connectors, Electrical, Circular Threaded, AN Type, General Specification For |
| MIL-DTL-6129 Revision B:2014 | Valve, Check; Vacuum and Pressure System |
| MIL-DTL-5015 Revision H:2000 | Connectors, Electrical, Circular Threaded, AN Type, General Specification for (S/S by SAE-AS50151) |
| MIL-DTL-45932 Revision A:2015 | Insert, Screw Thread, Thin Wall, Locked in: General Specification for |
| MIL-DTL-5421 Revision D:2011 | Tubes, Pitot, Electrically Heated, Aircraft |
| MIL-T-9720 Revision F:1984 | Truck, Lift, Aerial Stores, 3000 Pounds Capacity MJ-1A and MJ-1B |
| SAE AS29600B | Connectors, Electrical, Circular, Miniature, Composite, High Density, Quick Coupling, Environment Resistant, Removable Crimp Contacts Associated Hardware, General Specification For |
| MIL-PRF-81975 Revision C:2008 | Couplings, Regulated, Aerial Pressure Refueling Type MA-2, Type MA-3 and Type MA-4 |
| MIL-DTL-87255 Revision A:2008 | Valves, Pressure, Anti-G Suit, High Flow |
| MIL-T-25193 Revision B:1961 | Transmitter, Remote Compass, Type C-2 (Unstabilized) |
| MIL-I-5418 Revision B:1963 | Indicator, Airspeed, Pitot Static, Sensitive, 50-650 Knots |
| MIL T 5421 : B | TUBE, PITOT, ELECTRICALLY HEATED, AIRCRAFT |
| MIL-S-81551 Base Document:1968 | SWITCH, TOGGLE, HERMETICALLY SEALED, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT) |
| MS27075 Revision D:2013 | Nipple, Flared, Tube to Hose - Swivel Nut |
| MS27071 Revision D:2013 | Union, Nipple |
| SAE AS18802 | Fuel and Oil Lines, Aircraft, Installation of |
| MIL-I-8505 Base Document:1948 | Indicator, Temperature, Electrical Resistance, -50 to +300 Degrees Celsius (No S/S Document) |
| MIL-DTL-19068 Revision B:2006 | VALVES, SHUTTLE, HYDRAULIC, AIRCRAFT, TYPE 2 SYSTEMS |
| MIL-I-18802 Revision A:1962 | Installation of Fuel and Oil Lines, Aircraft (S/S by SAE-AS18802) |
| MIL C 22992 : E | CONNECTOR, PLUGS AND RECEPTACLES, ELECTRICAL, WATERPROOF, QUICK DISCONNECT, HEAVY DUTY TYPE GENERAL SPECIFICATION FOR |
| MIL-DTL-7899 Revision D:2014 | Valve, Check, Aircraft Fuel System |
| MIL-A-6425 Revision B:1959 | Adapter, Pressure Fuel Servicing, Aircraft, General Specification for (S/S by MIL-A-25896) |
| MIL-A-38331 Base Document:1964 | Amplifier-Power Supply AM-4080/ASN-55, Leveling (No S/S Document) |
| MS172236THRUMS172270 Revision B:1974 | NUT, SPANNER, BEARING RETAINING, AERONAUTICAL (ASG) (S/S BY SAE-AS172236THRUAS172270) |
| MIL-I-27273 Revision A:1965 | Inverter, Power, Static, General Specification for |
| MIL-G-8798 Base Document:1956 | Gage System, Fuel-Quality, Capacitor-Type, Nonvacuum Tube, Integrally Lighted, General Specification for (S/S by MIL-G-26988) |
| 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 |
| SAE AS4073A | Air Cycle Air Conditioning Systems for Military Air Vehicles |
| MIL-G-22169 Base Document:1959 | Gyro, Vertical and Mount (No S/S Document) |
| MIL F 26685 : B NOTICE 1 | FLIGHT DIRECTOR SYSTEM, DESIGN AND INSTALLATION OF |
| MIL-A-19940 Base Document:1957 | Amplifier, Control, Single Channel, S-2 Compass (No S/S Document) |
| MIL-C-18053 Revision A:1958 | Control Amplifier, Altitude (P-1 Automatic Pilot Radar Set, AN/APN-22) (No S/S Document) |
| MIL T 5350 : E | TRANSMITTER, SYNCHRO OPERATED, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-S-9487 Revision C:1985 | SWITCH, TRIGGER, SINGLE POLE, TWO STAGE, MOMENTARY (S/S BY MIL-S-8805/111) |
| MIL-R-19750 Revision A:1958 | REGULATOR; VOLTAGE, 28V, 120 DEG. C, FOR 30V DIRECT-CURRENT GENERATOR, GENERAL SPECIFICATION FOR (S/S BY MIL-R-23761) |
| MIL-I-27304 Revision E:1977 | Indicator, Rate of Flow |
| MIL E 24021 : J NOTICE 1 | ELECTRIC POWER MONITORS, EXTERNAL, AIRCRAFT |
| MIL-V-5461 Revision C:1977 | VALVE, VACUUM BREAKING (NO S/S DOCUMENT) |
| MIL-T-7771 Revision B:1980 | TUBE, EXTENSION, GYRO STABILIZED DRIFT METER (NO S/S DOCUMENT) |
| MS21236 Base Document:1967 | RING, CARGO TIEDOWN (10,000 LB), TYPE III (S/S BY SAE-AS21236) |
| MIL-A-81852 Revision A:1986 | Altimeter-Encoder AAU-32/A |
| MIL-I-25863 Revision D:1990 | Indicator, Electrical Tachometer 0-110 Percent RPM, 2 Inch Size, Integrally Lighted |
| MIL-I-22075 Revision C:1984 | Indicator, Bearing-Distance-Heading ID-663D/U |
| MIL-V-8712 Revision A:1965 | VALVE, AIR RELIEF, LOW PRESSURE8(ASG) (S/S BY SAE-AS8712) |
| MIL-R-47321 Base Document:1987 | REGULATOR, PRESSURE, WATER PUMPED NITROGEN (NO S/S DOCUMENT) |
| MIL R 26895 : 0 | RELAY, FIELD CONTROL, GENERATOR 28 VOLT DC, TYPE MD AND 1 |
| MIL C 22263 : B | COUPLING FUEL LINE, FLEXIBLE, 125 PSI, GENERAL SPECIFICATION FOR |
| MIL I 18373 : B | INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF |
| MS123139 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 2 Inch, Aluminum |
| MS123136 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 1 5/8 Inch, Aluminum |
| MS123129 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 1 Inch, Aluminum |
| MIL C 5033 : C | CLOCK, AIRCRAFT, CIVIL DATE 24 HOUR DIAL 2 3/4 IN DIAMETER |
| MS123140 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 2 1/8 Inch, Aluminum |
| MIL-A-47309 Revision A:1991 | Amplifier, Pneumatic (S/S by SAE-ARP763) |
| MIL S 25073 : 0 | |
| MS27239 Revision E:2007 | Nipple, Straight, Adapter, Hose to Tube, Reusable, Hydraulic, Fuel and Oil Lines, 1/4 through 4 Inch Tube Sizes |
| AN116 Revision 3:2013 | Shackle, Anchor, Forger Carbon Steel Screw Pin |
| MIL T 25439 : A (1) | TRANSMITTER, RATE OF FLOW, IN-FLIGHT REFUELLING, 0-10,000 PPM, TYPE MB-3 |
| MIL B 8598 : A (1) | BULB, ELECTRICAL RESISTANCE, THERMOMETER, FREE AIR |
| MIL-C-85642 Base Document:1985 | COMMUNICATIONS CENTRAL AN/ASC-26 |
| MIL I 6839 : C | INDICATOR, POSITION, LANDING GEAR |
| MIL-A-81851 Revision B:1986 | Altimeter AAU-31/A |
| MIL-T-27200 Revision C:1975 | Transmitter, Rate Gyroscope TRU-2A/A |
| MIL-DTL-25308 Revision C:2010 | Gage, Pressure, Dial Indicating, Hydraulic, Type ME-1 |
| MS123132 Revision D:2010 | Plug - Straight Thread, O-Ring Seal , 1 1/4 Inch Aluminum |
| MIL-A-27328 Base Document:1960 | Amplifier-Indicator Group, Altitude-Vertical Speed A/A24G-7 (No S/S Document) |
| MIL I 7304 : B | INDICATOR, PRESSURE TORQUE SENSITIVE TYPE A 9 |
| MS25050 Revision B:2005 | Adapter, Antenna (No S/S Document) |
| MIL-I-5488 Revision A:1957 | Indicator, Turn and Slip, 28V, DC, 2-3/4 Size, Type MD-10 (No S/S Document) |
| MIL-P-5238 Revision C:1974 | Pump, Centrifugal, Fuel Booster, Aircraft, General Specification For |
| MIL-I-5482 Revision C:1960 | Indicator, Pressure, Synchro, Aircraft, 165 Degree Scale (No S/S Document) |
| MIL-C-81790 Revision A:1990 | Connectors, Receptacle, External Electric Power, Aircraft, General Specification for (S/S by SAE-AS81790) |
| SAE AS7250D | Nuts, Self-Locking, Steel, Corrosion and Heat Resistant High Strength, All Metal 1200 °F Use, UN Thread Form |
| SAE ARP1616B | Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel and Oil Systems |
| SAE AS58091A | Circuit Breakers, Trip-Free, Aircraft General Specification For |
| MIL-DTL-83361 Revision B:2007 | Indicator, Pressure, Oil, Dual, 0-100 PSI, EGU-18/A |
| MIL-PRF-57267 Base Document:2017 | Coupling, Aerial Pressure Refueling Type MA-5 |
| MIL-R-7649 Revision A:1953 | RELAY, ARMATURE, EXCITER-CONTROL, 115/200 VOLT, 3-PHASE 4-WIRE 400 CYCLE, TYPE H-1 (NO S/S DOCUMENT) |
| MIL-DTL-27599 Revision E:2016 | Connectors, Electrical, Circular, Miniature, High Density, Quick Disconnect, Environment Resistant, Solder Contacts, General Specification for |
| MIL-DTL-27715 Revision C:2014 | Circuit Breaker, Trip-Free, High Temperature, Aircraft General Specification for |
| MIL-DTL-19328 Revision F:1996 | Converter, Liquid Oxygen, 5 Liter, MB-5A |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MIL-A-23622 Base Document:1963 | Actuator, Aircraft, Electro-Mechanical, Linear, Direct Current |
| MS123135 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 1 1/2 Inch, Aluminum |
| MIL I 25689 : A NOTICE 1 | INDICATOR, ELECTRICAL TACHOMETER |
| 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 |
| AN805 Revision 8:2011 | Nut, Union |
| MIL I 38135 : B (3) | INDICATOR, INDICATED AIRSPEED AVU 19/A STANDBY |
| MS27391 Revision F:2013 | Nipple, Flareless, Tube to Hose - Swivel Nut |
| MIL-DTL-9320 Revision E:2010 | Signal, Warning, Audible, for Headset, Type MA-1 |
| MIL-C-6720 Revision C:1964 | Clock, Aircraft, Elapsed Time, Civil Date, 24-Hour, 2-3/4 Inch Dial (No S/S Document) |
| MIL-DTL-83723 Revision H:2016 | Connectors, Electrical, Circular, Environment Resisting and Hermetically Sealed, Receptacles and Plugs, General Specification for |
| MIL G 8360 : A | GAGE, PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE, 10-75 IN MERCURY TYPE MB 1 |
| MIL-T-5684 Revision B:1981 | Tie Rod: Round and Square, Aircraft (No S/S Document) |
| MIL R 7790 : 0 | RESISTOR, THERMOCOUPLE LEAD SPOOL |
| MIL-L-21652 Revision A:1964 | Light, Beacon, Anticollision, Aircraft, General Specification for |
| MIL T 6349 : C NOTICE 1 | TEST SET, SYNCHRO |
| MIL-I-26689 Revision C:1981 | Indicator, Horizontal Situation, AQU-2/A (No S/S Document) |
| MIL-I-58067 Revision A:1977 | Indicator, Vertical Velocity, Rapid Response Acceleration Sensitive, General Specification for (No S/S Document) |
| MIL C 8783 : A | CLAMP, HOSE, FLAT BAND 500 DEG. F |
| MIL-I-81508 Base Document:1966 | Indicator Plug, for Missile Propellants |
| MIL-P-25632 Revision B:1960 | PITOT STATIC TUBE, ELECTRICALLY HEATED, TEMPERATURE CONTROLLED, 115 VOLT, 400 HZ, TYPE MA-1 (NO S/S DOCUMENT) |
| MIL-I-25931 Revision B:1964 | Indicator, Position, Landing Gear, Symbol-Indicating, Integrally Lighted (No S/S Document) |
| MS123127 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 3/4 Inch, Aluminum, |
| MS123141 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 2 1/4 Inch, Aluminum |
| MS123143 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 2 1/2 Inch, Aluminum |
| MIL-DTL-25955 Revision A:2004 | Connectors, Electrical, Environment Resisting, Miniature, with Snap-in Contacts (No S/S Document) |
| MIL C 27889 : D | COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING, CPU-46/A, GENERAL SPECIFICATION FOR AND MTU-38/A MOUNTING TRAY |
| MIL F 83296 : 0 | FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, HIGH PRESSURE (3,000 PSI HYDRAULIC AND PNEUMATIC) |
| MS123120 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 1/4 Inch, Aluminum |
| MS123121 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 5/16 Inch, Aluminum |
| MIL-C-81991 Base Document:1975 | Converter, Aircraft DC to DC, Boost General Specification for (No S/S Document) |
| MIL-R-8573 Revision A:1957 | Reservoir, Air, Nonshatterable Steel |
| MIL I 83452 : LATEST | INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
| MIL-C-26485 Revision D:1968 | Control Assembly, Attitude Gyroscopic AF/A24G-1A (No S/S Document) |
| 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 A 25088 : C | |
| MIL-I-25861 Revision D:1967 | Indicator, Pressure, Hydraulic, 0-4,000 PSI, Integrally Lighted |
| MIL C 25478 : B | COOLER, LUBRICATING OIL, AIRCRAFT ENGINE, SYNTHETIC OIL, GENERAL SPECIFICATION FOR |
| MIL-I-83751 Base Document:1967 | Indicator, Safety Level, RF (No S/S Document) |
| MIL C 27715 : 0 | CIRCUIT BREAKER, TRIP-FREE, HIGH TEMPERATURE, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL-G-7734 Revision C:1981 | Gage, Pressure, Engine and Utility Aircraft |
| MS25057 Revision D:2013 | Takeup, Antenna |
| MIL-C-5026 Revision F:1984 | Cutout Relay, Engine Generator |
| MIL O 38338 : C (1) | OIL QUANTITY GAGING SYSTEM, CONTINUOUS TRANSISTORIZED NUCLEONIC, GENERAL SPECIFICATION FOR |
| MIL-H-27269 Revision A:1977 | Horizontal Situation Indicator Group AF/A24J-1 (No S/S Document) |
| MIL-R-23057 Base Document:1961 | Regulator, Compressed Air, High Pressure (3500 PSI) |
| MIL-G-23723 Base Document:1964 | Gyroscope, Rate Switching CN-495/AJB-3 |
| MIL-DTL-45918 Revision A:2009 | Clevises and Connectors (Rod End) |
| MIL G 23701 : 0 | MILITARY SPECIFICATION GYROSCOPE, RATE SWITCHING AN/ASN-52 |
| MIL-C-8412 Revision B:1969 | Compass, Magnetic, Slaved Gyro, Type J-4 (No S/S Document) |
| 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-DTL-25561 Revision B:1995 | Grip Assembly, Controller, Aircraft Type MC-2 (See Notice 2 for Replacement Information) |
| MIL-R-9221 Base Document:1953 | RELAY, FIELD CONTROL, GENERATOR 24 VOLT DC, TYPE M-2 (NO S/S DOCUMENT) |
| MIL-C-7488 Revision A:1974 | Cooler, Oil, Plate, Aircraft (S/S by MIL-PRF-25478) |
| 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 (S/S by SAE-AS8181) |
| MIL-DTL-7830 Revision E:2007 | Light Assembly, Marker, Aircraft Obstruction (No S/S Document) |
| MIL I 6424 : A NOTICE 1 | INDICATOR, INDUCTION COMPASS, TYPE V 8 |
| MIL-DTL-26500 Revision G:2011 | Connectors, General Purpose, Electrical, Miniature, Circular, Environment Resisting or Hermetically Sealed, General Specification for |
| MIL-STD-805 Revision B:1987 | TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR |
| MIL-R-7611 Base Document:1952 | RELAY, ARMATURE, TYPE MA-1 (NO S/S DOCUMENT) |
| MIL I 26359 : B | INDICATOR, ATTITUDE, REMOTE ARU-4/A |
| MIL-P-9389 Revision A:1987 | PUMP, PRESSURE, OIL FREE AIR TYPE MA-3 (NO S/S DOCUMENT) |
| MIL-DTL-58085 Revision C:2012 | Light, Beacon, Anti-Collision, Aircraft |
| MIL C 5015 : G | CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR |
| MIL-E-85583 Revision A:1987 | ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-P-83126 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
| MIL P 81305 : A | POWER, DISTRIBUTION PANEL, ALTERNATING CURRENT, F-4 AIRCRAFT, SPECIFICATION FOR |
| MIL-W-48274 Base Document:1974 | Warhead Section, GM, Training, XM201 Parts and Assembling (No S/S Document) |
| MIL-R-8373 Revision A:1954 | RELAY, CURRENT, TYPE D-1 (115 VOLTS, 400 CYCLE - SINGLE POLE) (NO S/S DOCUMENT) |
| MIL-T-38306 Base Document:1964 | Transmitter, Rate Gyroscope T-970/AJB-7 (No S/S Document) |
| MIL-B-26026 Revision B:1967 | Battery, Storage, Aircraft, Type MA-2-1 |
| MS25061 Revision C:2014 | Sleeve, Support, Antenna, Internal Thread |
| MIL-G-7817 Base Document:1951 | Gage, Fuel Quantity, Capacitor Type, Uncompensated, General Specification for (S/S BY MIL-G-26988) |
| MIL-DTL-81014 Revision B:2001 | Hook, Helicopter External Cargo, 20,000 Pound Capacity, Type C (No S/S Document) |
| MIL-T-18232 Revision B:1968 | Targets, Aerial, Powered, Design and Construction of General Specification for (No S/S Document) |
| MS24591 Revision D:2007 | Socket, Adapter, Hose to Tube, Reusable, Hydraulic, Fuel and Oil Lines, 1 through 2 Inches Tubing Sizes |
| MIL-S-48405 Base Document:1973 | Shielded and Confined Mild Detonating Cord Assemblies |
| MIL C 25369 : C | CYLINDER, CARBON DIOXIDE, FOR INFLATION OF PNEUMATIC LIFE PRESERVERS |
| MIL-B-23072 Base Document:1961 | Blower, Anti-Exposure Suit Ventilation, General Specification for(No S/S Document) |
| MIL-D-81227 Revision B:1976 | Detector Kit, Water, Automotive - Aviation Fuel (No S/S Document) |
| MIL-A-27198 Revision B:1987 | Altimeter, Pressure AAU-7/A |
| MIL-C-9075 Revision A:1968 | Computer and Transmitter, True Airspeed, Pitot-Static, 150-900 Knots, Type MA-1 (No S/S Document) |
| MIL-I-38391 Base Document:1965 | Indicator, Electrical Tachometer, ERU-12/A 0-350 RPM (Rotor), 0-7000 RPM (Engine) (No S/S Document) |
| MIL A 83419 : C | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
| MIL-D-7106 Revision C:1987 | Driftmeter, Electrically Driven Gyro Stabilized (No S/S Document) |
| MIL P 83206 : B | PITOT STATIC TUBE, L SHAPED, COMPENSATED, GENERAL SPECIFICATION FOR |
| MIL-A-22165 Base Document:1959 | Amplifier, Compass, Servo (Type MF-1 Compass) |
| MS25058 Revision C:2013 | Takeup, Tension, Antenna |
| 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-W-26217 Revision B:1985 | Winch, Drum, Power Operated AF/E24H-1, Cargo Loading, 4,000 Pound Capacity, Variable Speed, 28V DC Portable |
| MIL A 25676 : D | ADAPTOR, PRESSURE LUBRICATING OIL SERVICING, AIRCRAFT |
| MS33651 Revision C:2014 | Boss and Installations - Air Connection |
| MIL-A-81403 Base Document:1967 | Altimeter-Encoder, AAU-21/A (No S/S Document) |
| SAE ARP260D | Control Lever Connections (60° V Serrations) |
| SAE AS85049D | Connector Accessories, Electrical General Specification For |
| SAE ARP493B | Knobs, Control Aircraft, Recommended Design |
| MIL-DTL-9398 Revision D:2007 | Generator, Tachometer, Two-Pole, High Temperature, Aircraft |
| EN 6105:2016 | Aerospace series - Stud with shoulder |
| MIL-DTL-18240 Revision F:1997 | Fastener Element, Self-Locking, Threaded Fastener, 250 Degrees F Maximum |
| MIL-S-38399 Revision A:1975 | Starter, Pneumatic, Aircraft Engine General Specification For (No S/S Document) |
| MIL-C-29600 Base Document:1989 | Connectors, Electrical, Circular, Miniature, Composite, High Density, Quick Coupling, Environment Resistant, Removable Crimp Contacts, Associated Hardware, General Specification for (S/S by SAE-AS29600) |
| MIL-T-8598 Revision B:1990 | Transmitter, Temperature, Electrical Resistance, Flush-Mounted, Free Air |
| MIL-F-8378 Revision B:1975 | Frequency Meters, Aircraft 380 to 420 Hertz and 350 to 450 Hertz (No S/S Document) |
| MIL-A-25933 Revision B:1985 | Altimeter, Pressurized Compartment, Integrally Lighted 0-50,000 Feet, 1-7/8 Inch Dial |
| MIL-F-8615 Revision D:1976 | Fuel System Components, General Specification for (S/S by SAE-ARP8615) |
| MIL-T-27-233 Base Document:1978 | TRANSFORMERS AND INDUCTORS (AUDIO, POWER AND HIGH-POWER PULSE), INDUCTOR, CHARGING, TF5S37ZZ (NO S/S DOCUMENT) |
| MIL-I-25479 Revision A:1987 | Indicator, Mach Number, Sensitive, Servoed, Range .5 to 1.0, Type ME-5 (No S/S Document) |
| MIL-A-26360 Revision B:1982 | Amplifier, Electrical Control ASU-3/A (No S/S Document) |
| MIL-T-26609 Revision C:1994 | Transmitter, Position |
| MIL-G-58103 Base Document:1979 | Grip Assembly, Cyclic Controller, Helicopter |
| MIL-W-48271 Revision A:1984 | Warhead Metal Parts Assembly M251 Parts and Assembling |
| MIL-DTL-9395-10 Revision F:2006 | Switches, Pressure, (Gage), Type II |
| MIL-I-21718 Base Document:1958 | Indicator, Airspeed, Pitot Static, Maximum Allowable Speed, 40-400 Knots |
| MS27612 Revision M:2013 | Adapter, Hydraulic Bleeder Valve, Aircraft Wheel Brake |
| MS123123 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 7/16 Inch, Aluminum |
| MS123128 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 7/8 Inch, Aluminum |
| MIL-S-21277 Revision A:1958 | SWITCHES, LIQUID LEVEL, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT) |
| MS123137 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 1 3/4 Inch, Aluminum |
| MS123126 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 5/8 Inch, Aluminum |
| MIL-P-87210 Base Document:1984 | Pneumatic Power Systems, High Pressure (No S/S Document) |
| MIL-S-7470 Revision A:1975 | Shaft, Power Transmission, Aircraft Accessory, General Specification For |
| MIL-W-48866 Revision A:1980 | Warhead Section, GM, Practice Lightweight, M252 and Shipping and Storage Container, XM612, Spare Parts for |
| MIL-W-48369 Base Document:1974 | Warhead Section, GM, Practice, Lightweight, M252 Parts and Assembling |
| MIL T 83174 : B (3) | TRANSMITTER, ACCELEROMETER, AXIAL |
| MIL S 8932 : A | SWITCH, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-85505 Base Document:1983 | ALTIMETER, STANDBY, TYPES 1 AND 2 |
| MIL-A-27670 Revision D:1994 | Amplifier-Indicator Group Indicated Airspeed A/A24G-10 (No S/S Document) |
| MIL-A-83212 Revision A:1976 | Altimeter, Pressure AAU-27/A (No S/S Document) |
| MIL-G-26988 Revision C:1971 | Gage, Liquid Quantity, Capacitor Type Transistorized, General Specification for (No S/S Document) |
| MS123131 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 1 1/8 Inch, Aluminum |
| SAE AS5604A | Compass; Magnetic, Pilot\'s Standby |
| MIL-I-83262 Revision B:1977 | Indicator, Temperature, Thermocouple Hermetically Sealed, General Specification for (No S/S Document) |
| MIL-I-83245 Revision A:1994 | Indicator Set, Oil Pressure A/A24J-17 (No S/S Document) |
| MIL-V-23219 Base Document:1962 | Valve Manifolds, High Pressure Air Reducing (S/S by MIL-V-24272) |
| MIL D 26503 : A | DETECTOR, MAGNETIC AZIMUTH AND COMPENSATOR, DETECTOR, MAGNETIC AZIMUTH |
| MIL-I-27680 Revision C:1973 | Indicator, Altitude ARU-12/A, Remote (No S/S Document) |
| SAE AS8712 | Valve; Air Relief, Low Pressure |
| MS24590 Revision C:2007 | Socket, Adapter, Hose to Tube, Reusable, Hydraulic, Fuel and Oil Lines, 3/16 through 3/4 Inch Tubing Sizes |
| MIL-D-6728 Revision A:1956 | Damper, Engine Exhaust Flame and Glare (No S/S Document) |
| MIL-I-27623 Revision C:1972 | Indicator, Attitude, Remote Standby, 2 Inch (No S/S Document) |
| 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-I-7071 Revision B:1972 | Indicator, Temperature, Thermocouple Hermetically Sealed, General Specification for |
| MIL-P-85315 Base Document:1979 | Pump, Ejector, Air Vehicle Fuel, General Specification For |
| MIL-I-83117 Revision B:1975 | Indicator, Angle of Attack (No S/S Document) |
| MIL S 9320 : C | SIGNAL, WARNING, AUDIBLE, FOR HEADSET |
| MIL-V-18318 Revision B:1966 | VALVE, PRESSURE REGULATING, OXYGEN SYSTEM |
| MIL-T-26963 Revision D:1992 | Tester, Pressure Gage, Hydraulic, Portable, Type MP-1 (No S/S Document) |
| MIL-I-25941 Revision D:1986 | Indicator, Turn and Slip, 2- Inch Size, Integrally Lighted |
| MIL-G-27693 Revision A:1962 | Gyroscope, Displacement SBU-6/A, Roll and Pitch (No S/S Document) |
| MIL-I-25645 Revision D:1970 | Indicator, Liquid Oxygen Quantity, Capacitance Type, General Specification for |
| MIL-G-5678 Revision C:1964 | Gage, Pressure, Dial Indicating, Manifold Pressure (No S/S Document) |
| 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-L-85314 Revision A:1983 | LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
| MIL G 5413 : D NOTICE 1 | GENERATOR, TACHOMETER, FOUR POLE |
| MIL-DTL-6019 Revision E:2011 | Gages, Pressure, Dial Indicating, Low-Pressure Oxygen |
| 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 P 18148 : C | PLUG, ELECTRIC, AIRCRAFT STORAGE BATTERY |
| MIL-T-7258 Revision B:1985 | Transmitter, Temperature, Electrical Resistance, Type B-4 |
| MIL T 25435 : B | TRANSMITTER, PRESSURE, AIRCRAFT, VARIABLE RELUCTANCE TYPE, GENERAL SPECIFICATION FOR |
| MIL-I-38258 Base Document:1965 | Indicator, Attitude ARU-18/A, Director (No S/S Document) |
| MIL-C-87975 Base Document:1985 | Clock, Aircraft, Mechanical ABU-32/A (No S/S Document) |
| MIL-I-5415 Revision C:1987 | Indicator: Air Speed, Pitot-Static Pressure, General Specification for (No S/S Document) |
| MIL-A-27671 Revision B:1965 | Amplifier-Indicator Group, Altitude-Vertical Speed A/A24G-11 (No S/S Document) |
| MIL G 6019 : C | GAGE, PRESSURE, DIAL INDICATING, LOW-PRESSURE OXYGEN |
| MIL-E-81512 Base Document:1968 | Encoder, Shaft Position to Digital, Contact Type, Altitude Reporting; General Specification for (No S/S Document) |
| MIL-S-6904 Revision B:1965 | Signal, Emergency Warning, General Specification For |
| MIL-P-5315 Revision B:1964 | PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT (S/S BY SAE-AMS-P-5315) |
| MIL-T-58082 Revision A:1974 | TESTER, PYROMETER AND THERMOCOUPLE, FIELD, TYPE N-3A (NO S/S DOCUMENT) |
| MIL-T-5583 Revision C:1987 | Transmitter, Position, 28 Volts DC |
| MIL-M-7969 Revision C:1965 | Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for |
| MIL-L-19844 Revision A:1963 | Lead; Shielded, Detachable Ignition (No S/S Document) |
| MIL-C-38207 Revision A:1965 | Clock Aircraft, Mechanical ABU-11/A |
| MIL-DTL-6839 Revision E:2011 | Indicator, Position, Landing Gear |
| MIL G 21480 : A | GENERATOR SYSTEM, 400 HERTZ ALTERNATING CURRENT, AIRCRAFT GENERAL SPECIFICATION FOR |
| 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-I-25437 Revision B:1984 | Indicator, Aircraft, Pressure, Voltage Ratio Type, General Specification for |
| MIL-B-3990 Revision D:1980 | Bearings, Roller, Needle, Airframe, Antifriction, Inch (S/S by SAE-AS39901) |
| MS123125 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 9/16 Inch, Aluminum |
| MIL-I-23524 Revision A:1986 | Indicator, Attitude-Director, Remote, ID 1329A (V) |
| MIL C 25666 : E (1) | CONVERTER, LIQUID OXYGEN, CAPACITANCE TYPE GAGING, GENERAL SPECIFICATION FOR |
| MIL C 7115 : F | CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL R 5149 : B | ROCKET ENGINE, LIQUID PROPELLANT GENERAL SPECIFICATION FOR |
| DOD-C-85050 Base Document:1982 | Charger, Battery, Nickel-Cadmium, Aircraft General Specification for (No S/S Document) |
| MIL-O-19838 Base Document:1956 | Oil Systems: Aircraft, Installation and Test of |
| MIL G 9398 : C | GENERATOR, TACHOMETER, TWO POLE HIGH TEMPERATURE AIRCRAFT |
| MIL R 25532 : A | ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR |
| MIL I 27190 : B | INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI |
| MIL-I-26299 Revision G:1990 | Indicator, Rate of Flow, 0-5,000 PPH, Integrally Lighted (No S/S Document) |
| MIL V 25961 : F | VALVE, FILL-BUILDUP-VENT, LIQUID OXYGEN CONVERTER, CRU-5O/A |
| MIL-D-38134 Revision A:1971 | Detector, Magnetic Azimuth DSU-4/A, High Temperature (No S/S Document) |
| MIL-I-23832 Revision A:1980 | Indicator, Tachometer, Triple Pointer, Helicopter |
| MIL-I-81049 Revision A:1972 | Indicator, Temperature, Electrical Resistance, Voltage Compensated, Multifunction |
| MIL-T-5420 Revision B:1970 | Tubes, Pitot Static, Electrically Heated, Aircraft |
| MIL C 38333 : 0 | CONTROLLER, COMPASS SYSTEM C-6448/ASN-55 |
| MIL L 7830 : D | LIGHT ASSEMBLY, MARKER, AIRCRAFT OBSTRUCTION |
| MIL-E-6719 Revision A:1972 | Elbow, Electrical Conduit (No S/S Document) |
| 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 |
| MS27069 Revision H:2017 | Socket, Hose Coupling |
| MIL C 25955 : 0 | CONNECTOR, ELECTRICAL, ENVIRONMENT RESISTING MINIATURE, WITH SNAP-IN CONTACTS |
| MS24589 Revision C:2007 | Nipple, Adapter, Hose to Tube, Reusable, Hydraulic, Fuel and Oil Lines, 1 through 2 Inches Tubing Sizes |
| 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-DTL-26517 Revision B:2000 | Power Supply, Transformer-Rectifier, Aircraft, General Specification for |
| MIL-C-5191 Revision B:1953 | Computer and Transmitter, True Airspeed Pitot Static, Type A-2 (No S/S Document) |
| MIL-DTL-9395-30 Revision H:2012 | Switches, Pressure, (Gage), Type II 5 Amperes |
| MIL-P-38136 Revision A:1969 | PITOT STATIC TUBE, COMPENSATED TRU-62/A (NO S/S DOCUMENT) |
| MIL-DTL-25666 Revision F:1995 | Converter, Liquid Oxygen, Capacitance Type Gauging, General Specification for |
| MIL M 5388 : B | MACHMETER; PITOT STATIC OPERATED, RANGE 0.5 TO 1.5, TYPE A-2B |
| MS25049 Revision C:2014 | Mast, Antenna, Lead-Through (No S/S Document) |
| MIL-W-48757 Base Document:1975 | Warhead Section, GM, HE: M251 and M251A1 Spare Parts for |
| AND10050 Revision 21:2005 | Bosses, Standard Dimensions for Gasket Seal Straight Thread |
| MIL-C-7079 Revision A:1965 | Circuit Breakers, Non Trip-Free, General Specification for (No S/S Document) |
| MS123124 Revision D:2010 | Plug - Straight Thread, O-Ring Seal, 1/2 Inch, Aluminum |
| MS3345 Revision C:2013 | Flange, Split Mounting Meter, Time Totalizing |
| MIL-S-7886 Revision B:1962 | Spark Plug, Shielded, Aircraft Reciprocating Engine, General Specification For |
| MIL-A-27391 Revision B:1963 | Altimeter, Pressure AAU-2/A (No S/S Document) |
| SAE ARP5794 | Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard |
| SAE AS1371A | Nuts, Self-Locking, Corrosion Resistant Steel High Strength, Prevailing Torque, All Metal 800°F (427°C) Use, UNJ Thread Form |
| SAE AS838A | Aircraft Hydraulic Starter/Pumps |
| SAE MA2250 | Coupling Fuel, Flexible Variable Cavity, Threaded Type with Ferrules, Metric |
| MS27512 Revision H:2015 | Connectors, Electrical, Circular, Nut, Hexagon, Connector Mounting, for MIL-DTL-38999, Series II, and MIL-DTL-27599, Series II |
| PREN 6105 : 200P1 | AEROSPACE SERIES - STUD WITH SHOULDER |
| FED-STD-H28-1 Revision A:1985 | Screw-Thread Standards for Federal Services Section 1 Nomenclature, Definitions and Letter Symbols for Screw Threads |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| FED-STD-H28-5 Base Document:1978 | Screw Thread Standards for Federal Services, Section 5, Unified Miniature Screw Threads |
| FED-STD-H28-2 Revision B:1991 | Screw-Thread Standards for Federal Services Section 2 Unified Inch Screw Threads- UN and UNR Thread Forms |
| MIL-S-8879 Revision C:1991 | Screw Threads, Controlled Radius Root withIncreased Minor Diameter, General Specification for (S/S by SAE-AS8879) |
| FED-STD-H28-20 Revision B:1994 | Screw-Thread Standards for Federal Services Section 20 Inspection Methods for Acceptability of UN, UNR, UNJ, M, AND MJ Screw Threads |
| FED-STD-H28-6 Revision A:1978 | SCREW-THREAD STANDARDS FOR FEDERAL SERVICES SECTION 6 GAGES AND GAGING FOR UNIFIED SCREW THREADS-UN AND UNR THREAD FORMS |
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