MIL-W-17316 Revision A:1980
|
WIND MEASURING SET AN/PMQ-30 (COMPONENTS OF) |
MIL A 85670 : 0
|
ANTENNA, BROADBAND AS-3191/A, AS-3792/A, AND AS -3793/A |
MIL C 38240 : C
|
COMPUTER, ALTITUDE, ALTITUDE ENCODING CPU 66, GENERAL SPECIFICATION FOR AND MTU 39/A MOUNTING TRAY |
MIL-V-25023 Revision B:1967
|
VALVE, FUEL DRAIN, SELF-LOCKING |
DOD-S-87956 Base Document:1979
|
SHELTER, S-80A AND S-82A |
MIL-I-18856 Revision B:1969
|
INDICATOR, ANGLE OF ATTACK, 28V DC MS28062 AND MS28067 |
MIL-T-38034 Revision E:1970
|
TIMER, FIRE CONTROL, BOMBING, DUAL |
MIL-A-38307 Revision A:1981
|
ACCELEROMETER, AIRCRAFT, MX-6663/AJB-7 |
MIL-R-38370 Revision B:1972
|
RECORDING SET, FLIGHT DATA A/A24U-10 |
MIL-P-81655 Base Document:1970
|
PITOT STATIC TUBE, L-SHAPED, COMPENSATED, ELECTRICALLY HEATED, GENERAL SPECIFICATION FOR |
MIL-C-87979 Base Document:1987
|
CLOCK, AIRCRAFT, ELECTRONIC |
GGG-M-125-7 Revision B:1985
|
RESPIRATOR ASSEMBLY: HALF MASK, AIR-PURIFYING, COMBINATION CHEMICAL CARTRIDGE AND FILTER (FOR PESTICIDES AND ORGANIC VAPORS) |
MIL-T-81998 Base Document:1975
|
TEST SET, RADIO SET AN/ARM-165 |
MIL-S-85018 Revision A:1978
|
SECOND ORDER ATTITUDE REFERENCE SYSTEM (SOARS) AN/ASN-116 |
MIL-G-17713 Revision D:1988
|
GAGES, LIQUID LEVEL MEASURING, TANK |
SAE AMS 3731 : 2016
|
POTTING COMPOUND, EPOXY, BISPHENOL A-TYPE |
MIL-I-7062 Revision C:1975
|
INDICATOR, POSITION, CONTROL SURFACES, 28 VOLT DC, GENERAL SPECIFICATION FOR |
SAE AMS 3650 : 2012
|
RODS, SHEETS, AND MOLDED SHAPES, POLYCHLOROTRIFLURORETHYNEN (PCTFE) UNPLASTICIZED |
MIL-I-7065 Revision A:1976
|
INDICATOR, POSITION, AILERON TRIM TAB |
MIL-P-25518 Revision B:1981
|
Plastic Materials, Silicone Resin, Glass Fiber Base, Low Pressure Laminated |
MIL-E-23001 Revision B:1976
|
ELECTRIC GENERATING SYSTEM, VARIABLE SPEED CONSTANT FREQUENCY, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL F 8815 : D
|
FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC LINE, 15 MICRON ABSOLUTE AND 5 MICRON ABSOLUTE, TYPE 11 SYSTEMS; GENERAL SPECIFICATION FOR |
MIL T 27252 : A
|
TEST SET, SYNCHRO, TTU-73/E DC SELSYN, AIRCRAFT INSTRUMENTS |
SAE AMS 3695 : 2014
|
ADHESIVE FILM, EPOXY-BASE, FOR HIGH DURABILITY STRUCTURAL ADHESIVE BONDING |
MIL-T-83460 Base Document:1975
|
TRANSDUCER, MOTIONAL PICKUP TRU-164/A |
MIL D 9129 : D
|
DISCHARGERS, ELECTROSTATIC - GENERAL SPECIFICATION FOR |
MIL I 7627 : F
|
INDICATOR, TURN AND SLIP 28V DC |
MIL-R-81202 Revision D:1981
|
RECEIVER ASSEMBLY, NITROGEN, FOR LAU-7 SERIES LAUNCHERS |
MIL-I-83152 Revision B:1974
|
INDICATOR, INDICATED-AIRSPEED AVU-22/A (INDICATOR-TRANSDUCER) |
MIL-A-85055 Base Document:1979
|
AVIONICS SYSTEM PERFORMANCE SPECIFICATION FOR A-4M/AV-8 BOMBING SET, ANGLE RATE AN/ASB-19(V) |
MIL-B-36558 Revision B:1992
|
BEDS, ADJUSTABLE |
MIL-M-49199 Revision A:1985
|
MICROPHONE, LINEAR M-162/AIC GENERAL SPECIFICATIONS FOR |
MIL D 83320 : 0
|
DETECTOR, MAGNETIC AZIMUTH DSU-14/A |
MIL C 38214 : B
|
COMPASS, MAGNETIC,MOUNTED |
MIL-C-27298 Revision B:1980
|
CLOCK, AIRCRAFT, MECHANICAL ABU AND 9-A |
MIL F 83861 : B
|
FILTER ELEMENTS, NONCLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE, TYPE 1I, SYSTEMS GENERAL SPECIFICATION FOR |
MIL-T-38473 Revision A:1972
|
TIMER, PRECISION, BOMBING, 0 - 30 MINUTES |
MIL-F-85421 Revision B:1986
|
FITTINGS, TUBE, FLUID SYSTEMS, SEPARABLE, BEAM SEAM, 3000/4000 PSI - GENERAL SPECIFICATION FOR |
MIL H 11996 : B
|
HANDSET H-60/PT, HANDSET H-156/U, AND HANDSET H-165/U |
MIL-C-8605 Revision B:1990
|
CAP, PRESSURE FUEL SERVICING |
MIL-P-85833 Base Document:1989
|
PROTECTIVE ASSEMBLY, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL |
MIL E 85726 : A
|
ENCLOSURE, STANDARD AVIONICS, FORCED AIR COOLED, GENERAL SPECIFICATION FOR |
MIL-A-38140 Revision B:1977
|
ALTIMETER, PRESSURE AAU-16/A |
MIL C 27536 : B
|
COUPLING, CLAMP, GROOVED, V-BAND |
GG-C-2736 Revision A:1987
|
CATHETER, CARDIOVASCULAR (FLOW DIRECTED, THERMODILUTION) |
MIL-G-25597 Revision D:1973
|
GYROSCOPE, DISPLACEMENT, ROLL AND PITCH, TYPE MD-1 |
MIL-L-50794 Base Document:1973
|
LINEAR SHAPED CHARGE ASSEMBLY |
MIL-I-6726 Revision B:1966
|
Inclinometer, Aircraft |
MIL-C-87972 Revision A:1987
|
CASTERS, RIGID AND SWIVEL, GENERAL SPECIFICATION FOR |
MIL P 28809 : A
|
PRINTED WIRING ASSEMBLIES |
MIL-E-17555 Revision H:1984
|
ELECTRONIC AND ELECTRICAL EQUIPMENT, ACCESSORIES, AND PROVISIONED ITEMS (REPAIR PARTS); PACKAGING OF |
SAE AS 8905 : 2012
|
FITTINGS AND CARGO RINGS, TIE-DOWN, AIRCRAFT FLOOR |
MIL-C-7135 Revision F:1967
|
Compressor, Pneumatic, 3,000 PSI -- 2 SCFM Aero 2A (*), Aero 2A-1 (*), Aero 2B (*), and Aero 2B-1 (*) |
MIL I 7231 : B
|
INDICATOR, TRUE AIRSPEED, SYNCHRO REPEATER TYPE N 1 |
MIL-STD-1546 Revision B:1992
|
PARTS, MATERIALS, AND PROCESSES CONTROL PROGRAM FOR SPACE AND LAUNCH VEHICLES |
MIL-P-9024 Revision G:1972
|
PACKAGING, MATERIALS HANDLING AND TRANSPORTABILITY, SYSTEM AND SYSTEM SEGMENTS GENERAL SPECIFICATION FOR |
MIL-M-38706 Revision A:1984
|
MULTIMETER |
MIL P 83207 : B
|
PITOT STATIC TUBE, NOSE BOOM, COMPENSATED, GENERAL SPECIFICATION FOR |
MIL W 87893 : A
|
WORKSTATION, ELECTROSTATIC DISCHARGE (ESD) CONTROL |
SAE AMS 3636 : 2012
|
TUBING, PLASTIC, ELECTRICAL INSULATION, IRRADIATED POLYOLEFIN, PIGMENTED, FLEXIBLE, HEAT-SHRINKABLE, 2 TO 1 SHRINK RATIO |
MIL-P-6457 Revision E:1974
|
POWER SUPPLY, METALLIC RECTIFIER TYPE, GENERAL SPECIFICATION FOR |
MIL F 85406 : 0
|
FUSE SYSTEM, JOINT SERVICE ELECTRONIC BOMB FMU-139/B |
MIL V 85855 : 0
|
VALVE, QUICK DISCONNECT, FOR THE PROTECTIVE ASSEMBLY, CHEMICAL, RADIOLOGICAL |
MIL T 25620 : C
|
TESTER, OXYGEN MASK, HEADSET AND MICROPHONE, TYPE MQ-1A |
MIL-R-85669 Base Document:1988
|
REPEATER SET, RADIO, POD AN/ARQ-49 |
MIL I 27279 : B
|
INDICATOR, MACH NUMBER AVU-11/A, INTEGRAL LIGHTING |
MIL-C-5499 Revision B:1984
|
CORE, AIRCRAFT, HIGH PRESSURE AIR VALVE |
MIL-I-27202 Revision A:1980
|
INDICATOR, ELECTRICAL TACHOMETER, 0-110 PERCENT RPM 2-INCH SIZE, INTEGRALLY LIGHTED |
MIL-A-81724 Base Document:1969
|
ADAPTER, LAUNCHER, AIRCRAFT, ADU-299/E |
MIL M 7584 : A
|
METER, FUEL FLOW SYNCHRO STYLE TYPE B 3A |
SAE AMS 1640 : 2011
|
CORROSION REMOVING COMPOUND, FOR AIRCRAFT SURFACES |
SAE AMS 4750 : 2017
|
SOLDER, TIN-LEAD, 45SN - 55PB |
SAE AS 8796 : 2013
|
HOSE, AIR DUCT, FLEXIBLE, AIRCRAFT |
SAE AMS 5316E : 1987(S2017)
|
Ductile (Nodular) Iron Castings, Sand 80,000 psi (550 MPa) Tensile Strength As Cast |
SAE AMS 3572 : 2016
|
RESIN POLYURETHANE, FOAM-IN-PLACE, RIGID |
SAE AMS 3676 : 2015
|
INSULATION, SOUND AND THERMAL, RESIN-BONDED GLASS FIBER, MEDIUM FILAMENT |
DEFSTAN 00-970(PT0)/9(2012) : 2012
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-C-28809 Revision B:1988
|
CIRCUIT CARD ASSEMBLIES, RIGID, FLEXIBLE & RIGID FLEX |
MIL-N-85353 Base Document:1981
|
NUTS (FASTENERS) INTERNALLY THREADED, PRELOAD LOCKING 450 DEG F 800 DEG F,1200 DEG F, GENERAL SPECIFICATION FOR |
MIL-C-63550 Revision E:1985
|
CABLE ASSEMBLIES, ELECTRICAL, FABRICATION SPECIFICATION FOR |
F-F-2790 Base Document:1991
|
FILTER, AIR EXTENDED AREA, INITIAL INSTALLATION |
DEFSTAN 00-970(PT0)/14(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/7(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL BULL 343 : A
|
DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
MIL-T-81364 Base Document:1966
|
T-BOLT, 180,000 PSI TYPE 431 STAINLESS STEEL, MANUFACTURING PROCESS REQUIREMENTS |
DEFSTAN 00-970(PT0)/11(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/12(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/13(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL M 29212 : B NOTICE 1
|
MIXING PLANT, ASPHALT, DRUM TYPE, PORTABLE, ELECTRIC MOTOR DRIVEN, 120 TONS PER HOUR CAPACITY |
DEFSTAN 00-970(PT0)/8(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-G-81559 Revision C:1984
|
GYROSCOPE ASSEMBLIES ATTITUDE - DIRECTIONAL REFERENCE INSTRUMENTS FOR AIRCRAFT PACKAGING OF |
DEFSTAN 00-970(PT0)/10(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-C-85521 Base Document:1983
|
CONCENTRATOR, OXYGEN, GGU-7/A |
MIL I 7067 : B
|
INDICATOR, POSITION, FLAPS, 0 - 60 DEGREE MARKING, 2 INCH SIZE |
MIL-C-85829 Base Document:1989
|
COUPLING ASSEMBLY, HOSE, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE |
MIL-S-26547 Revision C:1985
|
STARTER-GENERATOR ENGINE STU-6A |
MIL-I-6447 Revision C:1974
|
INDICATOR, TRUE AIRSPEED TYPE M 1A |
MIL-STD-2097 Revision A:1989
|
ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
MIL-R-85111 Revision A:1980
|
RECOVERY ASSIST SECURING AND TRAVERSING SYSTEM FOR LAMPS MK 111 HELICOPTER |
SAE AMS 5384 : 2017
|
ALLOY CASTINGS, INVESTMENT, CORROSION AND HEAT RESISTANT, 53NI - 18CR - 18CO - 4.0MO - 2.9TI - 2.9AL - 0.006B, VACUUM-MELTED, VACUUM-CAST, SOLUTION AND PRECIPITATION HEAT TREATED |
MIL A 28875 : 0
|
AMPLIFIER, RADIO FREQUENCY AND MICROWAVE, SOLID STATE, GENERAL SPECIFICATION FOR |
MIL-F-29419 Base Document:1985
|
FRAME, SHIPPING [SIXCON] |
MIL F 83870 : A
|
FILTER ELEMENT, FLUID PRESSURE, TRANSMISSION, AIRCRAFT DISPOSABLE, 20 MICRON ABSOLUTE |
MIL-I-85506 Base Document:1983
|
INDICATOR, INDICATED AIRSPEED, STANDBY TYPES I, II, AND III |
SAE AMS 3733 : 2015
|
POTTING COMPOUND, EPOXY, TWO PART, HIGHLY FILLED, HEAT CURE, HIGH COMPRESSIVE STRENGTH |
GGG-M-125-3 Revision A:1982
|
RESPIRATOR ASSEMBLIES: AIR LINE, WITH DISPOSABLE HOOD (SUPPLIED AIR) |
GGG-M-125 Revision G:1985
|
RESPIRATOR AND RESPIRATOR ASSEMBLIES: AIR LINE; NON-POWERED AIR-PURIFYING AND POWERED AIR-PURIFYING |
MIL-G-83872 Revision A:1977
|
GYROSCOPE, DISPLACEMENT, TYPE SBU-23/A |
MIL-T-38049 Revision A:1972
|
TRANSMITTER, PRESSURE TRU 60A |
GGG-M-125-2 Revision A:1982
|
RESPIRATOR ASSEMBLIES: AIR LINE, WITH HELMET (SUPPLIED AIR) |
MIL-STD-726 Revision H:1985
|
PACKAGING REQUIREMENTS CODE |
GGG-M-125-4 Revision C:1985
|
RESPIRATOR ASSEMBLY: HALF MASK, AIR-PURIFYING, CHEMICAL CARTRIDGE (FOR ORGANIC VAPORS) |
MIL C 7958 : A
|
CONTROL, PUSH PULL, FLEXIBLE AND RIGID |
MIL-C-4109 Revision F:1986
|
COUPLING ASSEMBLY, LOW PRESSURE, AIR HOSE, QUICK-DISCONNECT |
MIL-E-50796 Base Document:1973
|
EXPANDING SHIELDED MILD DETONATING CORD ASSEMBLY |
SAE AS 5604 : 2012
|
COMPASS: MAGNETIC, PILOT'S STANDBY |
MIL-A-81621 Base Document:1969
|
ACCELEROMETER, ELECTRICAL, LINEAR ABU-13/A |
MIL-A-81918 Base Document:1976
|
ADAPTER, LAUNCHER, AIRCRAFT, ADU-299A/A |
SAE AS 6302 : 2016
|
TRANSMITTER, PRESSURE, FUEL, 0-600 PSI |
MIL F 28861 : B
|
FILTER AND CAPACITOR, RADIO FREQUENCY/ELECTROMAGNETIC INTERFERENCE SUPPRESSION, GENERAL SPECIFICATION FOR |
GGG-M-125-11 Revision A:1982
|
RESPIRATOR ASSEMBLY: HELMET WITH POWERED AIR-PURIFYING UNIT (PORTABLE BACK-PACK) |
MIL H 81529 : 0
|
HOOK, HELICOPTER EXTERNAL CARGO, 6,000 POUND CAPACITY TYPE A |
MIL-D-81358 Revision B:1970
|
DISPLAY GROUP, TACTICAL DATA AN/ASA-66 |
MIL-T-23733 Revision A:1968
|
TRANSMITTER, RATE GYROSCOPE T-751 (/AJB-3) |
MIL R 83178 : A
|
REGULATOR, OXYGEN, DILUTER DEMAND, AUTOMATIC PRESSURE BREATHING, GENERAL SPECIFICATION FOR |
MIL-I-25091 Revision B:1985
|
INDICATOR, CABIN AIR PRESSURE, PRESSURIZED AIRCRAFT, 1-7/8 INCH DIAL, TYPE MA-2 |
MIL V 7899 : C
|
VALVE, CHECK, AIRCRAFT FUEL SYSTEM |
MIL-T-25363 Revision D:1973
|
TANK, PNEUMATIC PRESSURE, AIRCRAFT, GLASS FIBER |
MIL-C-42061 Base Document:1988
|
CAP, SCREW, BOTTLE AND JAR |
MIL-R-42043 Base Document:1987
|
REGULATOR, OXYGEN |
GG-W-239 Revision C:1985
|
WHEELS, ABRASIVE, (SILICON CARBIDE, MOUNTED, DENTAL) |
GG-B-735 Revision B:1985
|
BRUSH, BRISTLE, DENTAL HANDPIECE (MANDREL MOUNTED) |
MIL-Y-87125 Revision A:1979
|
YARN, GRAPHITE, 1000/3000 FILAMENTS |
ZZ-H-461 Revision E:1986
|
HOSE AND HOSE ASSEMBLY, RUBBER, GAS (ACETYLENE HYDROGEN, AIR AND OXYGEN |
MIL-T-85230 Revision A:1992
|
TARGET, TOW, AERIAL, TDU-34/A |
MIL-B-37965 Base Document:1986
|
BURS, BONE SURGERY (CORROSION-RESISTING STEEL) |
MIL-E-83510 Revision A:1980
|
EARPHONE ELEMENT |
MIL W 3662 : B
|
WIRE, PLATINUM ALLOY [PLATINUM RUTHENIUM, PLATINUM IRIDIUM |
MIL-A-36188 Revision B:1989
|
APRON, DENTAL, PLASTIC |
MIL M 26542 : D (1) SUPP 1
|
MICROPHONE, DYNAMIC, GENERAL SPECIFICATION FOR |
SAE AMS 3713 : 2013
|
CORE, FLEXIBLE HONEYCOMB, POLYAMIDE PAPER BASE, PHENOLIC COATED |
GG-S-1616 Revision A:1987
|
SCISSORS, COLLAR AND CROWN |
GGG-M-125-1 Revision B:1982
|
RESPIRATOR ASSEMBLIES, AIR LINE, WITH FACE PIECE (SUPPLIED AIR) |
SAE AMS 7245 : F1993
|
INSERTS, THREAD FORM, CORROSION RESISTANT STEEL - 18CR 9.2NI |
MIL-A-81258 Base Document:1965
|
AMPLIFIER, RESOLVER, GENERAL SPECIFICATION FOR |
WW-U-531 Revision F:1984
|
UNION, PIPE, STEEL OR MALLEABLE IRON, THREADED CONNECTION, 150 LB, 250 LB & 300 LB WSP |
MIL-F-63051 Revision A:1985
|
FUZE, M934 SERIES ACTUATORS FOR |
MIL T 25446 : D
|
TRANSMITTER, TEMPERATURE, ELECTRICAL RESISTANCE |
MIL H 81581/8 : 0
|
HOSE ASSEMBLIES, CABLE ASSEMBLIES, COMMUNICATION, ASSOCIATED |
MIL-R-85895 Base Document:1988
|
RACK, BOMB EJECTOR, AIRCRAFT BRU-32/A |
MIL-I-5133 Revision C:1953
|
INDICATOR, ATTITUDE TYPE J 8 |
MIL-T-21578 Revision A:1966
|
TEST EQUIPMENT, HAZARDOUS LOCATION, INSTALLED, BASIC REQUIREMENTS FOR |
MIL-C-85019 Base Document:1976
|
COMPUTER, AIR NAVIGATION, TRUE AIRSPEED, MACH NUMBER, WIND COMPONENTS SUPERSONIC, TYPE MB-9 |
MIL-C-9082 Revision H:1986
|
CONVERTER, OXYGEN, AIRCRAFT, LIQUID TO GASEOUS, GENERAL SPECIFICATION FOR |
SAE AMS 3625 : 2016
|
ELASTOMERIC TUBING, ELECTRICAL INSULATION, CROSSLINKED SILICONE, PIGMENTED, FLEXIBLE, HEAT-SHRINKABLE, 1.750 TO 1 SHRINK RATIO |
MIL-A-85652 Base Document:1984
|
AMPLIFIER-MIXER AM-7157/DKT-59 |
MIL-P-83927 Revision B:1981
|
POWER SUPPLIES, GUIDED MISSILE LAUNCHERS, SINGLE TYPES PP-2401B/A PP-2401C/A PP-2401D/A, PP-4285/A, PP-4286/A, AND COMPOSITE TYPE PP-4506/A AND PS-1037 |
MIL-S-83427 Base Document:1974
|
SURVIVAL KIT CONTAINERS, CNU-129(V)/P AND CNU-130/P |
MIL R 19648 : C
|
RELAY, TIME DELAY, THERMAL GENERAL SPECIFICATION FOR |
MIL-B-1107 Revision G:1986
|
BELT, INDIVIDUAL EQUIPMENT, M-1936 |
MIL-A-85648 Base Document:1983
|
AMPLIFIER, TRAVELING WAVE TUBE |
MIL-C-81790 Revision A:1990
|
CONNECTORS, RECEPTACLE, EXTERNAL ELECTRIC POWER, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL B 8075 : D
|
BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
MIL-M-85831 Base Document:1989
|
MASK, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE, NON-OXYGEN |
MIL-B-42017 Base Document:1986
|
BUR, BONE SURGERY (TUNGSTEN CARBIDE), GENERAL REQUIREMENTS FOR |
MIL-C-38373 Revision B:1975
|
CAP, FLUID TANK FILLER |
SAE AMS 3593 : 2017
|
TUBING, PLASTIC, ELECTRICAL INSULATION, IRRADIATED POLYVINYLIDENE FLUORIDE, SEMI-RIGID, HEAT-SHRINKABLE, MARKER SLEEVING GRADE, LOW OUTGASSING |
MIL I 5356 : A
|
INDICATOR AIRSPEED, PITOT STATIC TYPE L 7 |
SAE ARP 899 : 2013
|
TUBE FITTINGS, FLUID SYSTEMS, PERMANENT TYPE, GENERAL REQUIREMENTS FOR |
SAE AMS 1775 : 2015
|
FABRIC, NYLON UPHOLSTERY, FIRE RETARDANT |
SAE AMS 3894 : 2016
|
Carbon Fiber Tape and Sheet Epoxy Resin Impregnated |
SAE AMS 7440 : 2016
|
BALLS, STEEL, LOW-CHROMIUM, HIGH CARBON HARDENED AND TEMPERED |
SAE AMS 4824 : 2015
|
BEARINGS, BABBITT-COATED LEADED-BRONZE STEEL BACK |
MIL-L-9131 Revision H:1983
|
LIFE RAFTS, INFLATABLE, TWENTY MAN |
SAE AMS 3903 : 2013
|
CLOTH, ORGANIC FIBER (PARA-ARAMID), HIGH MODULUS, EPOXY RESIN IMPREGNATED |
MIL-T-17286 Revision D:1989
|
TURBINES AND GEARS, SHIPBOARD PROPULSION AND AUXILIARY STEAM, PACKAGING OF |
SAE AMS 5358 : 2017
|
STEEL CASTINGS, INVESTMENT, CORROSION RESISTANT, 18CR - 9NI, SOLUTION HEAT TREATED |
MIL-E-87236 Base Document:1985
|
|
MIL-I-5170 Revision C:1987
|
INDICATOR, POSITION, HORIZONTAL STABILIZER |
MIL-S-8812 Revision D:1975
|
STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
SAE AMS 3816 : 2016
|
BRAID, FLAT, NYLON, ELECTRICAL TYING - WAX COATED |
MIL-E-87235 Base Document:1985
|
EMERGENCY ESCAPE, AIRCRAFT (REQUEST FOR ISSUE MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
MIL-HDBK-772 Base Document:1981
|
MILITARY PACKAGING ENGINEERING |
MIL-S-8710 Revision B:1969
|
STRAINER, AIRFRAME FUEL SYSTEM, GENERAL SPECIFICATION FOR |
GGG-M-125-5 Revision B:1985
|
RESPIRATOR ASSEMBLY: HALF MASK, AIR-PURIFYING PARTICULATE-FILTER (FOR DUSTS, FUMES, AND MISTS) |
MIL-F-48863 Revision C:1985
|
FUZE, GUIDED MISSILE, M934E6 PARTS ASSEMBLY, LOADING & PACKING FOR |
MIL-P-82579 Base Document:1973
|
POWER SUPPLY, MULTIVOLTAGE, DIRECT CURRENT (FOR TORPEDO TEST SET MARK 281 MOD 1) |
MIL-T-81272 Base Document:1966
|
THERMOCOUPLE, ENGINE, CYLINDER, BAYONET TYPE, MS90324 |
MIL E 6058 : B NOTICE 1
|
ENGINE, AIRCRAFT, RECIPROCATING, PREPARATION FOR SHIPMENT AND STORAGE OF |
MIL-V-8610 Revision B:1984
|
VALVE, FUEL SHUTOFF SOLENOID OPERATED, 28 VOLT, DC |
MIL-I-25852 Revision B:1981
|
INDICATOR, TEMPERATURE, THERMO COUPLE EHU-4/A |
MIL-I-9343 Revision C:1985
|
INDICATOR, TEMPERATURE, THERMOCOUPLE, ENGINE EXHAUST, TYPE MJ 1 |
MIL V 8057 : F
|
VALVE, OXYGEN, PRESSURE BUILDUP AND VENT |
MIL D 39030 : B
|
DUMMY LOAD, ELECTRICAL, COAXIAL AND STRIPLINE |
MIL D 22612 : C
|
DETECTOR, CONTAMINATED FUEL |
MIL-T-85703 Base Document:1984
|
TOOL, POWER DRIVE TLU 437/E |
MIL-C-85518 Base Document:1984
|
COMPUTER SET, STANDARD AIRBORNE AN/AYK-14(V) GENERAL SPECIFICATION FOR |
MIL-F-85596 Base Document:1983
|
FIN, RETARDER, AIR INFLATABLE BSU-85/B |
MIL E 24021 : J NOTICE 1
|
ELECTRIC POWER MONITORS, EXTERNAL, AIRCRAFT |
MIL-S-18471 Revision G:1983
|
|
MIL-I-87216 Base Document:1984
|
INSTRUMENT SYSTEMS, AIRBORNE REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT PATTERSON AFB OH 45433-6503 |
MIL-T-7771 Revision B:1980
|
TUBE, EXTENSION, GYRO STABILIZED DRIFT METER |
MIL-I-81454 Base Document:1967
|
INDICATOR, GYROSCOPE, VERTICAL REFERENCE ID-1481 (*)/A |
MIL W 3459 : D
|
WIPER, WINDOW, ELECTRIC, PENDULUM TYPE (MARINE SERVICE, HEAVY DUTY) |
MIL-M-21734 Revision C:1971
|
MICROPHONE, DYNAMIC, OXYGEN MASK M-94B/A |
MIL-I-26382 Revision C:1994
|
INDICATOR SET, LIQUID OXYGEN QUANTITY A/A24J-4 AND A/A24J-8 |
SAE AMS 3897 : 2016
|
CLOTH, CARBON FIBER, RESIN IMPREGNATED |
MIL H 8795 : D
|
HOSE ASSEMBLY, RUBBER HYDRAULIC, FUEL AND OIL RESISTANT |
MIL-R-7705 Revision B:1975
|
RADOME, GENERAL SPECIFICATION FOR |
GG-R-1549 Revision A:1986
|
|
MIL-I-49466 Base Document:1990
|
INSULATOR; DISKS, PLATES & WASHERS GENERAL SPECIFICATION FOR |
MIL-P-70343 Base Document:1990
|
PACKING, FIBERGLASS, ROPE & WICK |
MIL-A-81852 Revision A:1986
|
ALTIMETER-ENCODER AAU-32/A |
MIL-I-22075 Revision C:1984
|
Indicator, Bearing-Distance-Heading ID-663D/U |
MIL-I-7063 Revision B:1979
|
INDICATOR, POSITION, RUBBER TRIM TAB |
MIL-B-23071:C
|
Blowers, Miniature, for Cooling Electronic Equipment General Specification for
|
MIL-I-85832 Base Document:1989
|
INTERCOM, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE SET |
GG-R-1638 Revision A:1985
|
REMOVAL, DENTAL CROWN (SIMPLEX) |
MIL-R-47321 Base Document:1987
|
REGULATOR, PRESSURE |
MIL-M-4871 Revision C:1984
|
MAINTENANCE PLATFORM |
MIL-R-38162 Revision B:1971
|
RADIOSONDE SET AN/AMT 13 |
SAE AMS 5363 : 2017
|
STEEL CASTINGS, SAND AND CENTRIFUGAL, CORROSION AND HEAT RESISTANT, 18.5CR - 10.5NI - 0.90 (CB+TA), SOLUTION HEAT TREATED |
MIL C 22263 : B
|
COUPLING FUEL LINE, FLEXIBLE, 125 PSI, GENERAL SPECIFICATION FOR |
MIL-A-38202 Revision C:1972
|
AIRCRAFT ARRESTING SYSTEM BAK-12A/E32A; PORTABLE, ROTARY FRICTION |
MIL C 5033 : C
|
CLOCK, AIRCRAFT, CIVIL DATE 24 HOUR DIAL 2 3/4 IN DIAMETER |
MIL-H-85042 Revision A:1983
|
HOOKS, BOMB RACK, GENERAL SPECIFICATION FOR |
MIL-V-85033 Revision A:1981
|
VALVE CHARGING |
MIL S 55041 : C
|
SWITCH, WAVEGUIDE GENERAL SPECIFICATION FOR |
MIL-C-85642 Base Document:1985
|
COMMUNICATIONS CENTRAL AN/ASC-26 |
MIL-C-83864 Revision A:1982
|
CONTAINER, INNER, SURVIVAL KIT |
MIL-B-12841 Revision B:1970
|
BASIC ISSUE ITEMS FOR MILITARY VEHICLES, CARRIAGES AND EQUIPMENT; PREPARATION FOR SHIPMENT AND STORAGE |
MIL-T-27200 Revision C:1975
|
TRANSMITTER, RATE GYROSCOPE TRU-2A/A |
MIL-G-85468 Base Document:1981
|
GENERATOR CONTROL INDICATOR SG-118/AST-4(V) |
MIL-I-5721 Revision C:1970
|
INDICATOR, INDICATED AIRSPEED 20-250 KNOTS |
MIL I 9304 : B
|
INDICATOR, RATE OF FLOW, FUEL, SYNCHRO STYLE 0-12,000 PPH TYPE MA 6 |
SAE AMS 3870 : 2016
|
CERAMIC MOLDINGS AND EXTRUSIONS, DENSE, ULTRA-HIGH ALUMINA (99% AL[2]O[3]) |
SAE AMS 7304 : 2015
|
SPRINGS, STEEL, 0.85 - 1.05C, HARDENED AND TEMPERED AFTER FORMING |
MIL-F-63412 Base Document:1981
|
FUZE PROBE ASSEMBLY, PNEUMATIC ASSEMBLING & PACKING (TOW) |
SAE AMS 2535 : 2015
|
COATING, VAPOR DEPOSITED POLY-MONOCHLORO-PARA-XYLYLENE FOR MICROCIRCUITS |
SAE AMS 3843 : 2014
|
POLYTETRAFLUOROETHYLENE SHEET, ASBESTOS FIBER REINFORCED, HIGH COMPRESSIBILITY, LOW DENSITY |
SAE AMS 3834 : 2016
|
CLOTH, TYPE 'E' GLASS, 'B' STAGE POLYESTER-RESIN-IMPREGNATED, 7781 STYLE FABRIC, FLAME RESISTANT, IMPROVED STRENGTH |
SAE AMS 3632 : 2011
|
TUBING, PLASTIC, ELECTRICAL INSULATION, IRRADIATED POLYVINYLIDENE FLUORIDE, SEMI-RIGID, HEAT-SHRINKABLE, 2 TO 1 SHRINK RATIO |
SAE AMS 5330 : 2015
|
STEEL CASTINGS, INVESTMENT, 0.80CR - 1.8NI - 0.35MO (0.38 - 0.46C) (SAE 4340 MODIFIED), ANNEALED |
SAE AMS 1725 : 1986
|
SKIN PROTECTIVE COMPOUND, CHEMICAL BARRIER |
SAE AMS 5409 : 1984
|
ALLOY CASTING, INVESTMENT, CORROSION AND HEAT RESISTANT 61NI - 16CR - 8.5CO - 1.8MO - 2.6W - 0.8CB - 3.4TI - 1.8TA - 3.4A1- 0.010B - 0.06ZR (0.03 - 0.08C), VACUUM MELTED, VACUUM CAST, AS CAST |
SAE AMS 2510 : 2017
|
ENGINE GRAY FINISHING LOW BAKING |
SAE AMS 3020 : 2013
|
OIL, REFERENCE, FOR 'L' STOCK RUBBER TESTING |
SAE AMS 5315 : 2017
|
DUCTILE (NODULAR) IRON CASTINGS, SAND, 60,000 PSI (415 MPA) TENSILE STRENGTH, FERRITIZE ANNEALED |
SAE AMS 7312 : 1983(S2016)
|
PISTON RINGS, CENTRIFUGALLY-CAST IRON |
SAE AMS 1548 : 2017
|
CLEANER, TURBINE ENGINE GAS PATH, SOLVENT EMULSION TYPE |
SAE AS 1297 : 2008(S2014)
|
REDUCERS, PNEUMATIC PRESSURE, MISSILE |
SAE AMS 5395 : 2018
|
ALLOY IRON CASTINGS, DUCTILE, SAND, CORROSION RESISTANT, 22NI (2.5 - 3.0C), AS CAST |
SAE AMS 3804 : 2016
|
CLOTH, AIRPLANE, COTTON, MERCERIZED, 65 POUNDS (290 N) BREAKING STRENGTH |
SAE AMS 3582 : 2017
|
PLASTIC TUBING, ELECTRICAL INSULATION - CROSSLINKED POLYVINYL CHLORIDE, FLEXIBLE, HEAT SHRINKABLE, 2 TO 1 SHRINK RATIO |
SAE ARP 618 : 2013
|
BOSS FITTINGS, METAL SEAL, FLUID SYSTEMS: GENERAL REQUIREMENTS FOR |
SAE AMS 3689 : 2014
|
ADHESIVE, FOAMING, HONEYCOMB, CORE SPLICE, STRUCTURAL, -54 TO +177 DEGREES C (-65 TO +350 DEGREES F) |
SAE AMS 2421 : 1979
|
PLATING MAGNESIUM FOR SOLDERABILITY - ZINC IMMERSION PROCESS |
SAE AMS 3821 : 2015
|
CLOTH, TYPE 'E' GLASS, 'B' STAGE EPOXY-RESIN-IMPREGNATED 7781 STYLE FABRIC, FLAME RESISTANT |
MIL H 38390 : C
|
HOSE ASSEMBLY, TETRAFLUOROETHYLENE PNEUMATIC, HIGH PRESSURE |
MIL G 6162 : B
|
GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION |
MIL-G-81665 Base Document:1971
|
GENERATOR TRANSMITTER GROUP AN/ASA-76 (U) |
MIL H 26633 : C
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, OXYGEN |
MIL I 5099 : B
|
INDICATOR CABIN AIR PRESSURE, 1-7/8 INCH DIAL, TYPE MA-1 |
MIL I 25725 : A
|
INDICATOR, TORQUE PRESSURE, MAGNESYN STYLE, SINGLE CLAMP MOUNTED, 2 IN SIZE, 50-400 PSI TYPE A-8 |
MIL-B-37036 Revision A:1985
|
BUR, DENTAL, FINISHING (TUNGSTEN CARBIDE) |
SAE AMS 5389 : 1987(R2017)
|
ALLOY CASTINGS, SAND, CORROSION AND HEAT RESISTANT, 55NI - 16.5CR - 17MO - 4.5W - 5.8FE - 0.40V, SOLUTION HEAT TREATED |
MIL-H-36364 Revision B:1990
|
HOLDER, RADIAC DETECTING ELEMENT, FILM BADGE TYPE |
MIL-C-6720 Revision C:1964
|
CLOCK, AIRCRAFT, ELAPSED TIME, CIVIL DATE 24 HOUR 2 3/4 INCH DIAL |
MIL G 8360 : A
|
GAGE, PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE, 10-75 IN MERCURY TYPE MB 1 |
MIL-B-28599 Revision C:1988
|
BAG, LINEMAN'S GLOVE |
MIL-C-82576 Base Document:1973
|
CABLE ASSEMBLY, TEST (FOR TORPEDO TEST SET MARK 281 MOD 1) |
MIL-C-1258 Revision D:1983
|
CUP, OIL, LUBRICATING AND OILERS, SELF-FEEDING |
MIL T 6349 : C NOTICE 1
|
TEST SET, SYNCHRO |
MIL F 15733 : G
|
FILTERS & CAPACITORS, RADIO FREQUENCY INTERFERENCE |
MIL-R-28894 Base Document:1986
|
RELAY, HYBRID OR SOLID STATE, SENSORS, ESTABLISHED RELIABILITY GENERAL SPECIFICATION FOR |
MIL-I-12718 Revision F:1985
|
INSIGNIA, DISTINGUISHING, ARMY AND AIR FORCE, WOVEN |
MIL-I-81508 Base Document:1966
|
INDICATOR PLUG, FOR MISSILE PROPELLANTS |
DOD-I-85390 Base Document:1980
|
INDICATOR, TIME TEMPERATURE, CARD, CHEMICALLY ACTIVATED, METRIC |
MIL-F-8905 Revision B:1967
|
FITTINGS AND CARGO RINGS, TIEDOWN, AIRCRAFT FLOOR |
MIL-A-5034 Revision B:1979
|
ADAPTER, BOMB RACK, 30-INCH, AERO 1A |
MIL M 7793 : F
|
METER, TIME TOTALIZING |
MIL-C-49468 Base Document:1990
|
CRYSTAL UNITS, QUARTZ, PRECISION, GENERAL SPECIFICATION FOR |
MIL-A-25915 Revision A:1980
|
ACCELEROMETER, AIRCRAFT, PILOTS WARNING, TYPE MA-2 |
GG-T-585 Revision B:1986
|
TONOMETER, OPHTHALMIC, SCHIOTZ |
GG-T-621 Revision C:1985
|
TRANSIT, ONE-MINUTE; AND TRANSIT TRIPODS |
MIL-I-85352 Base Document:1980
|
INFLATOR ASSEMBLY AND GAGE ELEMENTS, PNEUMATIC PRESSURE REMOTE CONTROL, DIRECT READING |
MIL-C-81991 Base Document:1975
|
CONVERTER, AIRCRAFT DC TO DC, BOOST GENERAL SPECIFICATION FOR |
MIL-STD-1475 Base Document:1974
|
CONTAMINATION CONTROL TECHNOLOGY PACKAGING PROTECTION OF PRECISION CLEANED MATERIAL |
MIL-A-83462 Base Document:1975
|
ARCTIC CUSHIONS - CLOTHING, CHU-10/P AND CHU-11/P |
MIL-C-26485 Revision D:1968
|
CONTROL ASSEMBLY, ATTITUDE, GYROSCOPIC AF/A24G-1A |
MIL-R-23761 Revision B:1975
|
Regulators, Voltage, and Control Panels Aircraft, Direct Current Generator, General Specification for |
MIL-I-22126 Revision B:1972
|
INDICATOR, TORQUEMETER, ENGINE, TURBOPROP |
MIL-T-85026 Revision D:1988
|
TEST SET AN/ASM-475 FOR THE AN/ASX-2 RECOGNITION SET |
MIL I 83452 : LATEST
|
INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
MIL C 25478 : B
|
COOLER, LUBRICATING OIL, AIRCRAFT ENGINE, SYNTHETIC OIL, GENERAL SPECIFICATION FOR |
MIL-M-28519 Revision A:1984
|
METER, VOLUMETRIC, POSITIVE DISPLACEMENT, LIQUID, AIRCRAFT FUEL, 6OO GPM |
MIL A 25088 : C
|
|
MIL-R-83520 Base Document:1983
|
RELAYS, ELECTROMECHANICAL, GENERAL PURPOSE, NON-HERMETICALLY SEALED, PLASTIC ENCLOSURE (UST COVER) |
MIL-B-36162 Revision C:1987
|
BLADES, LARYNGOSCOPE, MILLER |
MIL I 83287 : E
|
INDICATOR, FAULT LOCATING GENERAL SPECIFICATION FOR |
MIL-A-18218 Revision B:1984
|
ANALYZERS, FLUE-GAS, ORSAT-TYPE, PORTABLE |
MIL-S-26716 Revision A:1982
|
STAND, TEST, AIRCRAFT HYDRAULIC SYSTEMS, NON-PORTABLE |
MIL-C-5026 Revision F:1984
|
CUTOUT RELAY, ENGINE GENERATOR |
MIL G 8348 : H
|
GAGE, ASSEMBLIES, AIR PRESSURE, DIAL INDICATING CHUCK TYPE SELF CONTAINED |
MIL-G-7734 Revision C:1981
|
GAGE, PRESSURE ENGINE AND UTILITY AIRCRAFT |
MIL O 38338 : C (1)
|
OIL QUANTITY GAGING SYSTEM, CONTINUOUS TRANSISTORIZED NUCLEONIC, GENERAL SPECIFICATION FOR |
MIL S 24251 : B
|
SHIELD, RETAINER (BASES), AND ADAPTERS, ELECTRON TUBE, HEAT DISSIPATING, GENERAL SPECIFICATION FOR |
MIL-H-27269 Revision A:1977
|
HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
SAE AMS 3802 : 2016
|
CLOTH, AIRPLANE, COTTON, MERCERIZED, 50 POUNDS (220 N) BREAKING STRENGTH |
MIL C 38618 : A
|
COUPLER, DRIVE ASSEMBLY GOVERNOR, FUZE BOMB MAU 87A B |
SAE AS 85352 : 2011
|
INFLATOR ASSEMBLY AND GAGE ELEMENTS, PNEUMATIC PRESSURE, REMOTE CONTROL, DIRECT READING |
MIL-I-23252 Revision B:1981
|
INDICATOR, PRESSURE |
MIL I 8136 : A
|
INDICATOR, FUEL FLOW RATE, SYNCHRO STYLE, SINGLE CLAMP MOUNTED 2 INCH SIZE 300 TO 3,000 PPH TYPE A 12 |
MIL-C-7488 Revision A:1974
|
COOLERS, OIL, PLATE, AIRCRAFT |
SAE AMS 3818 :1993(S2016)
|
BRAID, FLAT, POLYESTER, LACING AND TYING, SYNTHETIC RUBBER COATED, LOW OUTGASSING |
MIL-I-27665 Revision B:1984
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE ABU-1O/A, -50 DEGREES TO +50 DEGREES C |
GGG-M-125-6 Revision B:1985
|
RESPIRATOR ASSEMBLY: HALF MASK, AIR-PURIFYING, COMBINATION CHEMICAL CARTRIDGE AND FILTER (FOR PAINT SPRAY AND ORGANIC VAPORS) |
MIL-I-27203 Revision B:1987
|
INDICATOR, POSITION, WING FLAP |
MIL-E-85583 Revision A:1987
|
ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-P-85034 Base Document:1976
|
POWER PACKAGE, EMERGENCY AC/DC GENERATOR, RAM AIR TURBINE DRIVEN |
MIL O 55310 : C
|
OSCILLATOR, CRYSTAL, GENERAL SPECIFICATION FOR |
GGG-M-125-9 Revision A:1982
|
RESPIRATOR ASSEMBLIES, AIR LINE, HOOD AND HELMET (FOR ABRASIVE BLASTING OPERATIONS) |
MIL V 9050 : E (1)
|
VALVE, OXYGEN, PRESSURE RELIEF, AIRCRAFT |
SAE AMS 1450 : 1998
|
DISINFECTANT (INSECTICIDE), AIRCRAFT |
SAE AMS 5375 : 1982
|
ALLOY CASTINGS, INVESTMENT, CORROSION AND HEAT RESISTANT 65.5CO - 25CR - 1.8NI - 5.0W AS CAST |
SAE AMS 5351 : 2017
|
STEEL CASTINGS, SAND, CORROSION AND MODERATE HEAT RESISTANT, 13CR, NORMALIZED AND TEMPERED |
MIL-S-48405 Base Document:1973
|
Shielded and Confined Mild Detonating Cord Assemblies |
SAE AMS 5348 : 2017
|
STEEL CASTINGS, TUBULAR, CENTRIFUGAL, CORROSION RESISTANT, 15CR - 4.6NI - 0.22 (CB+TA) - 2.8CU, SOLUTION HEAT TREATED |
MIL H 7061 : B
|
HOSE, RUBBER, AIRCRAFT, SELF SEALING, AROMATIC FUEL |
MIL L 51167 : A
|
LABORATORY, CHEMICAL, BASE, M2A1 |
MIL C 25369 : C
|
CYLINDER, CARBON DIOXIDE, FOR INFLATION OF PNEUMATIC LIFE PRESERVERS |
MIL-M-55565 Revision C:1988
|
MICROCIRCUITS, PACKAGING OF |
MIL-A-27198 Revision B:1987
|
ALTIMETER, PRESSURE AAU-7/A |
MIL-C-9075 Revision A:1968
|
COMPUTER AND TRANSMITTER, TRUE AIRSPEED, PITOT STATIC, 150-900 KNOTS, TYPE MA 1 |
MIL-I-27247 Revision C:1985
|
INDICATOR, TEMPERATURE, SYNCHRO |
MIL B 83054 : B
|
BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK |
MIL A 3933 : E
|
ATTENUATORS, FIXED GENERAL SPECIFICATION FOR |
SAE AMS 2550 : 2017
|
TREATMENT OF SHEET METAL PARTS, CORROSION-RESISTANT STEEL |
MIL-A-23899 Revision B:1984
|
AURAL PROTECTOR, SOUND |
MIL-V-23255 Revision B:1976
|
VALVE, PRESSURE RELIEF |
MIL-I-8404 Revision A:1953
|
INDICATOR, PRESSURE, SINGLE 0 TO 35 PSI FUEL PRESSURE TYPE C 33 |
MIL D 81544 : A
|
DISPENSER, PARACHUTE FLARE, SUU-44/A |
MIL I 7491 : B
|
INDICATOR RATE OF FLOW, FUEL TOTALIZING, SERVO STYLE, TYPE F 1 |
MIL-I-82577 Base Document:1973
|
INDICATOR, DIGITAL (FOR TORPEDO TEST SET MARK 281 MOD 1) |
MIL-N-81207 Revision A:1973
|
NAVIGATIONAL SET, TACAN AN/ARN-84 (V) |
MIL-A-27261 Revision A:1966
|
ACCELEROMETER, AIRCRAFT |
MIL-STD-758 Revision C:1990
|
PACKAGING PROCEDURES FOR SUBMARINE REPAIR PARTS |
MIL-I-81400 Base Document:1966
|
INSTRUMENT, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-A-22424 Revision A:1967
|
ADAPTERS, COMPENSATING, MS281O7, MA-1 COMPASS SYSTEM |
SAE AIR 4728 : 2013
|
REFERENCES, SPACECRAFT AND SPACECRAFT SERVICING, FLUID SYSTEM COMPONENTS (ABBREVIATIONS, ACRONYMS, DEFINITIONS, APPLICABLE DOCUMENTS AND ENVIRONMENTAL CONDITIONS) |
SAE AMS 5373 : 2017
|
ALLOY CASTINGS, SAND, CORROSION AND HEAT RESISTANT, 16CO - 29CR - 4.5W, AS CAST, UNS R30006 |
SAE AMS 4176 : 2001
|
HONEYCOMB CORE - FOR SANDWICH CONSTRUCTION 5056, 350-DEG F (175-DEG C) |
SAE AMS 7878 : 1987
|
TUNGSTEN CARBIDE POWDER, COBALT COATED |
SAE AMS 7464 : 2017
|
BOLTS AND SCREWS, STEEL, LOW-ALLOY HEAT RESISTANT, 222,000 PSI (1517 MPA) TENSILE STRENGTH, HARDENED AND TEMPERED, ROLL THREADED |
SAE AMS 3815 : 2016
|
BRAID, FLAT, NYLON, ELECTRICAL TYING SYNTHETIC RUBBER COATED |
SAE AMS 2690 : 2017
|
PARALLEL GAP, WELDING, MICROELECTRONIC INTERCONNECTIONS TO THIN FILM SUBSTRATES |
SAE AMS5341:2012(S2017)
|
STEEL CASTINGS, INVESTMENT, CORROSION RESISTANT, 19.5CR - 10.5NI - 0.25S (TYPE 303), SOLUTION HEAT TREATED |
SAE AMS 7466 : 1993
|
BOLTS AND SCREWS - NICKEL ALLOY, CORROSION AND HEAT RESISTANT, UPSET HEADED, ROLL THREADED, FATIGUE RESISTANT |
SAE AMS 3688 : 2014
|
ADHESIVE, FOAMING, HONEYCOMB CORE SPLICE, STRUCTURAL, -55 DEGREES C TO +82 DEGREES C (-65 DEGREES F TO +180 DEGREES F) |
SAE AMS 2399 : 2011
|
ELECTROLESS NICKEL-BORON PLATING |
SAE AMS 3813 : 2016
|
ROPE, ARAMID FIBER, JACKETED FOR ANTENNA-SUPPORT SYSTEMS |
MIL-R-81498 Revision C:1979
|
RECEIVING-DECODING GROUP AN/ARA-63 |
MIL-T-81187 Base Document:1966
|
TRANSMITTER, RATE OF FUEL FLOW, SYNCHRO TYPE MS90361 |
MIL-G-23083 Revision C:1972
|
GYROSCOPE, RATE SWITCHING MS 17399 |
MIL-STD-1367 Revision A:1989
|
PACKAGING, HANDLING, STORAGE, AND TRANSPORTABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS) |
MIL-A-25933 Revision B:1985
|
ALTIMETER, PRESSURIZED COMPARTMENT, INTEGRALLY LIGHTED 0-50,000 FEET, 1-7/8 INCH DIAL |
MIL-F-8615 Revision D:1976
|
FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
MIL-I-85112 Base Document:1978
|
INDICATOR SET, VERTICAL SCALE |
MIL-T-27-233 Base Document:1978
|
TRANSFORMERS AND INDUCTORS (AUDIO POWER AND HIGH POWER PULSE) INDUCTOR CHARGING TF5S37ZZ |
MIL-I-25130 Revision B:1974
|
INDICATOR, PRESSURE, OIL, 0-300PSI, TYPE MO-1 |
MIL T 21038 : D
|
TRANSFORMERS, PULSE, LOW POWER, GENERAL SPECIFICATION FOR |
MIL C 55330 : B
|
CONNECTORS, PREPARATION FOR DELIVERY OF |
MIL-A-26360 Revision B:1982
|
AMPLIFIER, ELECTRONIC CONTROL ASU-3/A |
MIL-A-27330 Revision B:1987
|
ACCELEROMETER, ELECTRICAL, LINEAR TRU-3/A |
MIL-B-23459 Revision D:1988
|
BUOY, HOSE SUPPORT, INFLATABLE |
MIL V 9439 : D
|
VALVE, OXYGEN, CYLINDER, HIGH PRESSURE |
SAE AMS 4805 : 2012(S2018)
|
BEARINGS, SINTERED METAL POWDER, 89CU - 10SN, OIL IMPREGNATED |
MIL-W-6940 Revision D:1985
|
WIRE STRAND, STEEL, NONFLEXIBLE (PREFORMED) |
MIL F 38642 : A
|
FIN ASSEMBLY, BOMB, MXU-469/B AND MXU-467/B |
MIL-F-85720 Base Document:1985
|
FITTING, TUBE, FLUID SYSTEMS, SEPARABLE, HIGH PRESSURE, DYNAMIC BEAM, SEAL, GENERAL SPECIFICATION FOR |
MIL T 83174 : B (3)
|
TRANSMITTER, ACCELEROMETER, AXIAL |
MIL-S-7470 Revision A:1975
|
SHAFT, POWER TRANSMISSION, AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR |
MIL-T-81838 Base Document:1971
|
TANK, FUEL, AIRCRAFT, AUXILIARY EXTERNAL 300 GALLON, TYPE AERO 1D |
SAE AMS 2689 : 2016
|
FUSION WELDING TITANIUM AND TITANIUM ALLOYS |
SAE AMS 3732 : 2015
|
POTTING COMPOUND, EPOXY ONE PART, FILLED, HEAT CURE, LOW CTE |
SAE AMS 3912 : 2014
|
RADOMES, FOAM SANDWICH, POLYIMIDE/QUARTZ CLOTH CONSTRUCTION |
MIL-I-25482 Revision D:1993
|
INDICATOR, ENGINE TESTING |
MIL-A-85505 Base Document:1983
|
ALTIMETER, STANDBY, TYPES 1 AND 2 |
MIL-H-58108 Base Document:1986
|
HEADSET-MICROPHONE KIT MK-2193/AIC |
MIL-I-7112 Revision B:1985
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, CYLINDER HEAD 0 DEGREES C TO 300 DEGREES C |
MIL-M-29417 Base Document:1984
|
MODULE, FUEL PUMP [SIXCON] |
MIL-N-25161 Revision C:1969
|
NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
MIL-G-26988 Revision C:1971
|
GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
MIL-A-81605 Revision D:1984
|
ALTIMETER SET, ELECTRONIC AN/APN-194(V) |
MIL-I-83245 Revision A:1994
|
INDICATOR SET, OIL PRESSURE A/A24J-17 |
SAE AMS 3579 : 2017
|
PLASTIC TUBING, ELECTRICAL INSULATION, NON-CROSSLINKED POLYVINYL CHLORIDE, FLEXIBLE, HEAT SHRINKABLE, 1.6 TO 1 SHRINK RATIO |
MIL-I-27680 Revision C:1973
|
INDICATOR, ATTITUDE, ARU-12/A, REMOTE |
SAE AS 85075 : 2000
|
TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR |
SAE AMS 5115 : 2017
|
Wire, Carbon Steel 0.60 - 0.75C Hardened and Tempered |
SAE AMS 3684 : 2016
|
RESIN, POLYIMIDE, SEALING HIGH-TEMPERATURE RESISTANT, 315 DEGREES C (600 DEGREES F) UNFILLED |
MIL-P-116 Revision J:1988
|
PRESERVATION, METHODS OF |
MIL-A-29505 Base Document:1966
|
ANTENNA GROUP, TACAN, OE-273(V)/URN |
MIL-P-85585 Base Document:1982
|
PROBES, EDDY CURRENT, UNSHIELDED, SINGLE COIL, ABSOLUTE |
MIL T 25502 : C
|
TRUE HEADING COMPUTER GROUP AN/AJA-I |
MIL W 3970 : C
|
WAVEGUIDE ASSEMBLIES, RIGID, GENERAL SPECIFICATION FOR |
MIL-W-45562 Revision C:1992
|
WELDING AND SOLDERING EQUIPMENT, SUPPLIES AND ACCESSORIES, PACKAGING OF |
MIL-I-81453 Revision A:1977
|
INTERROGATOR SET AN APX 76B(V) |
MIL-I-27623 Revision C:1972
|
INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
MIL-T-85678 Base Document:1974
|
TRANSPONDER, RADAR TRACKING |
MIL-I-25950 Revision B:1967
|
INDICATOR, PRESSURE, OIL, 0-100 PSI |
MIL-I-7087 Revision A:1968
|
INDICATOR, PRESSURE OIL, 0-200 PSI |
MIL-A-81296 Revision D:1985
|
ALTIMETER SET, ELECTRONIC AN/APN-171(V) |
MIL-I-83117 Revision B:1975
|
INDICATOR, ANGLE OF ATTACK |
MIL-H-21594 Revision C:1986
|
HOOKPOINT, AIRCRAFT ARRESTING |
MIL-T-25485 Revision C:1974
|
TRANSMITTER, THRUST, SINGLE SYNCHRO STYLE, PRESSURE RATIO, TYPE MK-2 |
GG-E-916 Revision F:1987
|
EXPLORERS, DENTAL; EXPLORER-PROBE, DENTAL |
MIL-C-26237 Revision C:1983
|
CRADLE, AIRCRAFT-MISSILE COMPONENTS MMU-1/E |
MIL L 12606 : D
|
LOUDSPEAKER, PERMANENT MAGNET (UNENCASED, 3 INCH AND 4 INCH DIAMETER CONE, 2 WATT, FUNGUS, GUNBLAST, AND IMMERSION RESISTANT), TYPE LL-445/U, M12606-01, AND M12606-02 |
MIL-B-42027 Base Document:1986
|
BROACH, PULP CANAL, BARBED, STERILE |
MIL-C-87970 Base Document:1982
|
CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
MIL L 10911 : D
|
LOUDSPEAKER, PERMANENT MAGNET (UNENCASED, 2.5-, 3-, 4-, 5-, 6-, 8-, 10-, AND 12-, INCH DIAMETER CONE) |
MIL-S-81977 Base Document:1974
|
SIMULATOR, RADAR SIGNAL SM-697/UPQ-5 |
MIL-I-7084 Revision A:1988
|
INDICATOR, PRESSURE, HYDRAULIC 0-4,000 PSI |
MIL-G-25591 Revision E:1981
|
GYROSCOPE, RATE, SWITCHING, TYPE MC-1 |
MIL-B-4330 Revision C:1984
|
BOOT, EXTREME COLD WEATHER |
GG-B-101 Revision G:1986
|
BANDAGE, CAST, PLASTER OF PARIS IMPREGNATED (HARD COATED) |
MIL-T-7258 Revision B:1985
|
TRANSMITTER, TEMPERATURE ELECTRICAL RESISTANCE TYPE B-4 |
MIL T 25435 : B
|
TRANSMITTER, PRESSURE, AIRCRAFT, VARIABLE RELUCTANCE TYPE, GENERAL SPECIFICATION FOR |
MIL-C-87975 Base Document:1985
|
CLOCK, AIRCRAFT, MECHANICAL ABU-32/A |
GG-F-599 Revision B:1988
|
FORCEPS, DRESSING, DENTAL |
MIL-E-22437 Revision E:1981
|
EQUIPMENT, DEGAUSSING FOR MCM SHIPS |
MIL-A-25175 Revision C:1976
|
AIR TRANSPORT, NONTACTICAL, PACKING FOR |
MIL-I-27619 Revision G:1974
|
INDICATORS, ATTITUDE DIRECTOR |
MIL H 87961 : NOTICE 2
|
HOSE AND HOSE ASSEMBLIES, AIR DUCT, AIR BREATHING, OXYGEN SYSTEM GENERAL SPECIFICATION FOR |
MIL-B-4792 Revision E:1994
|
BUMPER, RUBBER, DUPLEX ROUND |
MIL I 27851 : B
|
INDICATOR, INDICATED AIRSPEED AVU-17/A |
MIL-C-38418 Revision E:1981
|
CONTROL ASSEMBLY, GYROSCOPE, ATTITUDE A/A24G-39 |
MIL-T-8249 Revision B:1979
|
TRANSMITTER, RATE OF FLOW, FUEL, TYPE MB-2 |
MIL-I-8974 Revision A:1981
|
INDICATOR, EVENT COUNTING, GENERAL SPECIFICATION FOR |
MIL-A-28624 Revision B:1984
|
AUGER, EARTH, PORTABLE; HAND-HELD, TWO-MAN, GASOLINE-ENGINE DRIVEN |
GG-R-1472 Revision B:1987
|
RETAINER, MATRIX, DENTAL (TOFFLEMIRE) |
MIL T 26898 : B
|
TEST SET, AIRFIELD LIGHTING SYSTEMS, TYPE MM-1 |
AA-S-130 Revision B:1991
|
SCREENS, BEDSIDE, ALUMINUM |
MIL-B-27044 Revision C:1968
|
BOMB, PRACTICE BDU-12/B |
MIL-C-22585 Revision A:1984
|
COMPUTER, PRESSURE REDUCTION, METEOROLOGICAL CP-402/UM() |
MIL-P-85511 Revision A:1987
|
PANEL ASSEMBLY, TARGET, BANNER, AERIAL TDU-32 SERIES |
MIL B 38634 : LATEST
|
BOMB, FIRE, BLU 32A B |
SAE AMS 3823 : 2015
|
CLOTH, GLASS, STYLE 7781, CHROME-SILANE FINISH |
MIL-V-85830 Base Document:1989
|
VENTILATOR, TACTICAL, HELICOPTER AIRCREWMEN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE |
MIL C 25666 : E (1)
|
CONVERTER, LIQUID OXYGEN, CAPACITANCE TYPE GAGING, GENERAL SPECIFICATION FOR |
DOD-C-85050 Base Document:1982
|
CHARGERS, BATTERY, NICKEL-CADMIUM, AIRCRAFT, GENERAL SPECIFICATION FOR |
SAE MA 1568 : 2018
|
NUT, SELF LOCKING - UNS S66286, 425 DEGREE C AND 650 DEGREE C, 1100 MPA, MJ THREAD, PROCUREMENT SPECIFICATION FOR, METRIC |
MIL-C-81883 Base Document:1976
|
CONTROL GROUP, ELECTRIC POWER OK-XXX (V) A GENERAL SPECIFICATION FOR |
MIL-I-7802 Revision A:1967
|
INDICATOR, MS 28088, TURN AND SLIP [THREE PHASE] |
MIL-I-23832 Revision A:1980
|
INDICATOR, TACHOMETER, TRIPLE POINTER, HELICOPTER |
MIL-D-38134 Revision A:1971
|
DETECTOR, MAGNETIC AZIMUTH DSU-4/A, HIGH TEMPERATURE |
MIL-I-81049 Revision A:1972
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
GG-C-1320 Revision B:1985
|
CUP, POLISHING, DENTAL HANDPIECE (SCREW STEM) |
MIL-T-5420 Revision B:1970
|
TUBE, PITOT STATIC, ELECTRICALLY HEATED, AIRCRAFT |
MIL-R-17772 Revision C:1982
|
RADIATOR, HEATING, BASEBOARD PANEL, STEAM AND HOT WATER |
GG-B-140 Revision D:1986
|
BATH, WATER, DENTAL IMPRESSION COMPOUND |
GG-C-1282 Revision C:1985
|
CURETTES, ALVEOLAR (MOLT AND MILLER) |
MIL-P-87133 Base Document:1978
|
PLOTTER, COMBAT MISSION PLU-6/C (AIR NAVIGATION) |
MIL-I-42044 Revision A:1991
|
SEXUAL ASSAULT DETERMINATION KIT |
MIL-T-4638 Revision B:1985
|
TESTERS, MATERIAL HARDNESS (ROCKWELL TYPE) |
MIL I 83361 : (4)
|
INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
MIL-P-38136 Revision A:1969
|
PITOT STATIC TUBE COMPENSATED TRU 62/A |
MIL M 5388 : B
|
MACHMETER; PITOT STATIC OPERATED, RANGE 0.5 TO 1.5, TYPE A-2B |
MIL R 85725 : 0
|
RACK, INTEGRATED AVIONICS, FORCED AIR COOLED, GENERAL SPECIFICATION FOR |
MIL-L-5567 Revision F:1983
|
LIFE RAFTS, INFLATABLE 4 AND 7 MAN FOR AIRCRAFT USE |
GGG-M-125-10 Revision A:1982
|
RESPIRATOR ASSEMBLY: HELMET WITH POWERED AIR-PURIFYING UNIT |
GGG-M-125-8 Revision B:1985
|
RESPIRATOR ASSEMBLY: HALF MASK, AIR-PURIFYING PARTICULATE-FILTER (FOR DUSTS AND MISTS) |
MIL-G-8170 Revision D:1987
|
GAGE, OIL PRESSURE, DIRECT INDICATING, SINGLE CLAMP MOUNTED 0 -200 PSI 320 DEGREE SCALE 2 INCH SIZE, TYPE AGU 12/A AND AGU 13/A |
MIL-STD-834 Revision C:1974
|
PACKAGING DATA FORMS, INSTRUCTIONS FOR PREPARATION AND USE OF |
MIL-A-85434 Revision A:1983
|
AMPLIFIER, TRAVELING WAVE TUBE AM-6937/DLQ-3B |
MIL T 25627 : C
|
TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |
MIL-E-82578 Base Document:1973
|
ENCODER, SHAFT ANGLE POSITION, CYCLIC DECIMAL CODED (FOR TORPEDO TEST SET MARK 281 MOD 1) |
MIL H 83776 : A
|
HELMET, FLYER'S, WINTER |
SAE AMS 7311 : 2017
|
PISTON RINGS, CENTRIFUGALLY-CASE ALLOYED IRON, 0.50MO - 0.50CU |
SAE AMS 3081 : 1978
|
ANTI SCUFFING TREATMENT, GRAPHITE VARNISH |
SAE AMS 1451 : 1998
|
DISINFECTANT, AIRCRAFT FOR USE IN CARGO COMPARTMENTS |
SAE AS 23899 : 2012
|
AURAL PROTECTOR, SOUND |
SAE AMS5328E:1987(S2017)
|
STEEL CASTINGS, INVESTMENT, 0.80CR - 1.8NI - 0.35MO (0.28 - 0.36C) (SAE 4330 MODIFIED), ANNEALED |