|
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 |
|
MIL-T-5842 Revision B:1985
|
TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR |
|
MIL-T-38034 Revision E:1970
|
TIMER, FIRE CONTROL, BOMBING, DUAL |
|
MIL-A-38307 Revision A:1981
|
ACCELEROMETER, AIRCRAFT, MX-6663/AJB-7 |
|
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 AS 8181 : 1997
|
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 |
|
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 |
|
MIL-E-23001 Revision B:1976
|
ELECTRIC GENERATING SYSTEM, VARIABLE SPEED CONSTANT FREQUENCY, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
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 |
|
MIL-T-83460 Base Document:1975
|
TRANSDUCER, MOTIONAL PICKUP TRU-164/A |
|
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
|
CONNECTOR, ELECTRIC, CIRCULAR, MINIATURE, RACK AND PANEL OR PUSH-PULL COUPLING, ENVIRONMENT RESISTING |
|
MIL-A-5885 Revision D:1987
|
ACCELEROMETER, AIRCRAFT |
|
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 |
|
MIL-T-5483 Revision D:1964
|
TRANSMITTER, PRESSURE, SYNCHRO AIRCRAFT 165 DEGREE MOVEMENT |
|
MIL-I-85071 Revision A:1992
|
INVERTERS, AIRCRAFT, DC TO AC, GENERAL SPECIFICATION FOR |
|
MIL-STD-7080 Base Document:1994
|
SELECTION & 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 |
|
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 AND 9-A |
|
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 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 |
|
MIL-I-27709 Revision A:1962
|
INDICATOR, ATTITUDE ARU-14/A, REMOTE |
|
MIL-G-7818 Base Document:1951
|
GAGE, FUEL QUANTITY, CAPACITOR TYPE, COMPENSATED, GENERAL SPECIFICATION FOR |
|
MIL-E-5627 Revision B:1965
|
EXTINGUISHERS, FIRE, CARBON DIOXIDE, PORTABLE |
|
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 |
|
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) |
|
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 |
|
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, SEL-LOCKING, CLINCH GENERAL SPECIFICATION FOR |
|
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 |
|
MIL-S-45909 Revision C:1989
|
STUD, LOCKED IN - RING LOCKED SERRATED |
|
MIL-C-19179 Revision B:1963
|
COUPLING ASSEMBLY, QUICK-DISCONNECT, FUEL |
|
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 |
|
MS122116THRUMS122155 Revision D:1976
|
INSERT CRES HELICAL COIL COARSE THREAD 1 1/2 DIA NOMINAL LENGTH |
|
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 DEG F, 450 DEG F, AND 850 DEG F |
|
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 |
|
MIL V 5523 : D
|
VALVE, RELIEF, HYDRAULIC PRESSURE |
|
MS124731THRUMS124770 Revision D:1976
|
INSERT, CRES HELICAL COIL FINE THREAD, 2 DIA NOMINAL LENGTH |
|
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 |
|
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 AS 5590 : 2013
|
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
|
CONNECTOR, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT ENVIRONMENT RESISTING, AND ACCESSORIES GENERAL SPECIFICATION FOR |
|
MIL R 23016 : A
|
RADIO SET AN/ARC-94 |
|
MIL-A-6752 Revision A:1953
|
AMMETER, VOLTMETERS, AND LOADMETERS; DIRECT CURRENT |
|
SAE AS 81511 : 2016
|
CONNECTORS, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT, ENVIRONMENT RESISTING AND ACCESSORIES, GENERAL SPECIFICATION FOR |
|
MIL-C-85049 Revision A:1990
|
CONNECTOR ACCESSORIES, ELECTRICAL GENERAL 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 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
|
GAGE - PRESSURE, DIAL INDICATING |
|
MIL-A-6589 Revision A:1968
|
AMPLIFIER, ELECTRONIC CONTROL, SINGLE CHANNEL, TYPE A-2 |
|
MIL-C-6100 Revision A:1973
|
CONNECTOR, RECEPTACLE, ELECTRICAL, AIRCRAFT |
|
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) |
|
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 AND 1 |
|
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 |
|
MIL-B-81365 Base Document:1966
|
BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
|
MIL-B-83769 Revision D:1983
|
BATTERY, STORAGE, LEAD ACID, GENERAL SPECIFICATION FOR |
|
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, PILOTS STANDBY |
|
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 |
|
MIL-C-9082 Revision H:1986
|
CONVERTER, OXYGEN, AIRCRAFT, LIQUID TO GASEOUS, GENERAL SPECIFICATION FOR |
|
MIL-C-24360 Revision A:1969
|
CABLE ASSEMBLY, AIRCRAFT AUTONAVIGATOR ALIGNMENT, UMBILICAL |
|
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-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 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG] |
|
MIL-P-8564 Revision D:1970
|
PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
|
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 AS 7481 : 2015
|
STUDS, STEEL, UNS S66286 AGED AFTER ROLL THREADED PROCUREMENT SPECIFICATION FOR |
|
SAE AS 81703 : 2012
|
CONNECTORS, ELECTRIC, CIRCULAR, MINIATURE, RACK AND PANEL OR PUSH-PULL COUPLING, ENVIRONMENT RESISTING |
|
I.S. EN 6105:2016
|
AEROSPACE SERIES - STUD WITH SHOULDER |
|
SAE AS 39901 : 2012
|
BEARINGS, ROLLER, NEEDLE, AIRFRAME, ANTIFRICTION, INCH |
|
NASM 7838 : 2004
|
BOLT, INTERNAL WRENCHING, 160 KSI FTU |
|
SAE AS 50151 : 2015
|
CONNECTORS, ELECTRICAL, CIRCULAR THREADED, AN TYPE, GENERAL SPECIFICATION FOR |
|
NASM24694:2012
|
SCREW, MACHINE, FLAT COUNTERSUNK HEAD, 100 DEGREES, STRUCTURAL, CROSS RECESSED, UNC-3A AND UNF-3A |
|
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 |
|
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 AS 29600 : 2017
|
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 |
|
MS27075 Revision D:2013
|
NIPPLE, FLARED, TUBE TO HOSE - SWIVEL NUT |
|
MS27071 Revision D:2013
|
UNION, NIPPLE |
|
SAE AS 18802 : 2013
|
FUEL AND OIL LINES, AIRCRAFT, INSTALLATION OF |
|
MIL-I-8505 Base Document:1948
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE -50 TO PLUS 300 C |
|
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 |
|
MIL C 22992 : E
|
CONNECTOR, PLUGS AND RECEPTACLES, ELECTRICAL, WATERPROOF, QUICK DISCONNECT, HEAVY DUTY TYPE GENERAL SPECIFICATION FOR |
|
MIL-DTL-7899 Revision D:2014
|
VALVES, CHECK, AIRCRAFT FUEL SYSTEM |
|
MIL-A-6425 Revision B:1959
|
ADAPTOR, PRESSURE FUEL SERVICING, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL-A-38331 Base Document:1964
|
AMPLIFIER-POWER SUPPLY AM-4080/ASN-55, LEVELLING |
|
MS172236THRUMS172270 Revision B:1974
|
NUT, SPANNER, BEARING RETAINING, AERONAUTICAL (ASG) |
|
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 |
|
SAE AS 4073 : 2013(R2018)
|
AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES |
|
MIL-G-22169 Base Document:1959
|
GYRO, VERTICAL AND MOUNT |
|
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 |
|
MIL-C-18053 Revision A:1958
|
CONTROL AMPLIFIER, ALTITUDE (P-1 AUTOMATIC PILOT RADAR SET, AN/APN-22) |
|
MIL T 5350 : E
|
TRANSMITTER, SYNCHRO OPERATED, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL-S-9487 Revision C:1985
|
SWITCH, TRIGGER, SINGLE POLE, TWO STAGE, MOMENTARY |
|
MIL-R-19750 Revision A:1958
|
REGULATOR; VOLTAGE, 28 V, 120 DEGREE C, FOR 30 V DIRECT-CURRENT GENERATOR, GENERAL SPECIFICATION FOR |
|
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 |
|
MIL A 38726 : 0
|
ADAPTER ASSEMBLY, REUSABLE, FLEXIBLE HOSE, LOW PRESSURE |
|
MIL-T-7771 Revision B:1980
|
TUBE, EXTENSION, GYRO STABILIZED DRIFT METER |
|
MS21236 Base Document:1967
|
RING, CARGO TIEDOWN (10,000 LB), TYPE 3 |
|
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 PRESSURE |
|
MIL-R-47321 Base Document:1987
|
REGULATOR, PRESSURE |
|
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 |
|
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 |
|
MIL I 7304 : B
|
INDICATOR, PRESSURE TORQUE SENSITIVE TYPE A 9 |
|
MS25050 Revision B:2005
|
ADAPTOR, ANTENNA |
|
MIL-I-5488 Revision A:1957
|
INDICATOR TURN AND SLIP 28V DC 2 3/4 SIX, TYPE MD 10 |
|
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 |
|
MIL-C-81790 Revision A:1990
|
CONNECTORS, RECEPTACLE, EXTERNAL ELECTRIC POWER, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
SAE AS 7252 : 2015
|
NUTS, SELF-LOCKING, STEEL HIGH STRENGTH, ALL METAL 450 DEGREES F USE, UN AND UNJ THREAD FORM |
|
SAE AS 7250D : 2013(R2018)
|
NUTS, SELF-LOCKING, STEEL, CORROSION AND HEAT RESISTANT HIGH STRENGTH, ALL METAL 1200 DEGREES F USE, UN THREAD FORM |
|
SAE ARP 1616 : 2017
|
SELF-SEALING BREAKAWAY VALVES FOR CRASH-RESISTANT AIRCRAFT FUEL AND OIL SYSTEMS |
|
SAE AS 1046 : 2016
|
MINIMUM STANDARD FOR PORTABLE GASEOUS, OXYGEN EQUIPMENT |
|
SAE AS 58091 : 2012
|
CIRCUIT BREAKERS, TRIP-FREE, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
NASM 3 THRU NASM 20:2014
|
BOLT, MACHINE, AIRCRAFT |
|
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 H1 |
|
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
|
JOINT SERVICE SPECIFICATION GUIDE - 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 |
|
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 RODS; ROUND AND SQUARE, AIRCRAFT |
|
MIL R 7790 : 0
|
RESISTOR, THERMOCOUPLE LEAD SPOOL |
|
MIL-L-21652 Revision A:1964
|
LIGHT, BEACON, ANTI COLLISION 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 |
|
MIL-I-58067 Revision A:1977
|
INDICATOR, VERTICAL VELOCITY, RAPID RESPONSE ACCELERATION SENSITIVE, GENERAL SPECIFICATION FOR |
|
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, 4OO HZ, TYPE MA-1 |
|
MIL-I-25931 Revision B:1964
|
INDICATOR, POSITION, LANDING GEAR, SYMBOL-INDICATING, INTEGRALLY LIGHTED |
|
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, OR HERMETICALLY SEALED WITH NON-REMOVABLE CONTACTS, GENERAL SPECIFICATION FOR |
|
MIL S 5807 : C NOTICE 1
|
SEXTANT, AIRCRAFT PERISCOPIC |
|
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 |
|
MIL-R-8573 Revision A:1957
|
RESERVOIRS, 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 |
|
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-1O13(*)/A |
|
MIL A 25088 : C
|
|
|
MIL-I-25861 Revision D:1967
|
INDICATOR, PRESSURE, HYDRAULIC, 0-4000 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 |
|
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 AND 1 |
|
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 |
|
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 |
|
MIL-R-9221 Base Document:1953
|
RELAY, FIELD CONTROL, GENERATOR 24 VOLT DC TYPE M AND 2 |
|
MIL-C-7488 Revision A:1974
|
COOLERS, OIL, PLATE, AIRCRAFT |
|
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-DTL-7830 Revision E:2007
|
LIGHT ASSEMBLY, MARKER, AIRCRAFT OBSTRUCTION |
|
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 AND 1 |
|
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 |
|
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 |
|
MIL-R-8373 Revision A:1954
|
RELAY, CURRENT TYPE D 1 [115 VOLTS 400 CYCLE SINGLE POLE] |
|
MIL-T-38306 Base Document:1964
|
TRANSMITTER, RATE GYROSCOPE T 970/AJB - 7 |
|
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 |
|
MIL-DTL-81014 Revision B:2001
|
HOOK, HELICOPTER EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C |
|
MIL-T-18232 Revision B:1968
|
TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
|
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 |
|
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-9075 Revision A:1968
|
COMPUTER AND TRANSMITTER, TRUE AIRSPEED, PITOT STATIC, 150-900 KNOTS, TYPE MA 1 |
|
MIL-I-38391 Base Document:1965
|
INDICATOR, ELECTRICAL TACHOMETER, ERU-12/A 0-350 RPM (ROTOR), 0-7000 RPM (ENGINE) |
|
MIL A 83419 : C
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
|
MIL-D-7106 Revision C:1987
|
DRIFTMETER, ELECTRICALLY DRIVEN GYRO STABILIZED |
|
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, 4OOO 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 |
|
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 |
|
SAE AS 81582 : 2017
|
CONNECTORS, ELECTRICAL, BAYONET COUPLING, ENVIRONMENT RESISTING, UMBILICAL, GENERAL SPECIFICATION FOR |
|
SAE ARP 260 : 2012 (S2018)
|
CONTROL LEVER CONNECTIONS (60 DEGREES V SERRATIONS) |
|
SAE AS 85049 : 2016
|
CONNECTOR ACCESSORIES, ELECTRICAL GENERAL SPECIFICATION FOR |
|
SAE ARP 493 : 2017
|
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 |
|
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 |
|
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 |
|
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-T-27-233 Base Document:1978
|
TRANSFORMERS AND INDUCTORS (AUDIO POWER AND HIGH POWER PULSE) INDUCTOR CHARGING TF5S37ZZ |
|
MIL-I-25479 Revision A:1987
|
INDICATOR, MACH NUMBER, SENSITIVE, SERVOED, RANGE .5 TO 1.O, TYPE ME-5 |
|
MIL-A-26360 Revision B:1982
|
AMPLIFIER, ELECTRONIC CONTROL ASU-3/A |
|
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 2 |
|
MIL-I-21718 Base Document:1958
|
INDICATOR, AIRSPEED, PITOT STATIC, MAXIMUM ALLOWABLE SPEED, 4O-4OO 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
|
SWITCH, LIQUID LEVEL, GENERAL SPECIFICATION FOR |
|
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 |
|
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 |
|
NASM 21209 : 2003
|
INSERT, SCREW THREAD, COARSE AND FINE, SCREW LOCKING, HELICAL COIL, CRES |
|
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 |
|
MIL-A-83212 Revision A:1976
|
ALTIMETER, PRESSURE AAU-27/A |
|
MIL-G-26988 Revision C:1971
|
GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
|
MS123131 Revision D:2010
|
PLUG - STRAIGHT THREAD, O-RING SEAL, 1 1/8 INCH, ALUMINUM |
|
SAE AS 5604 : 2012
|
COMPASS: MAGNETIC, PILOT'S STANDBY |
|
MIL-I-83262 Revision B:1977
|
INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
|
MIL-I-83245 Revision A:1994
|
INDICATOR SET, OIL PRESSURE A/A24J-17 |
|
MIL-V-23219 Base Document:1962
|
VALVE MANIFOLDS, HIGH PRESSURE AIR REDUCING |
|
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 8712 : 2013
|
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 |
|
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-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 |
|
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 |
|
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 |
|
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 |
|
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
|
FILTER 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 |
|
MIL-C-87975 Base Document:1985
|
CLOCK, AIRCRAFT, MECHANICAL ABU-32/A |
|
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 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 |
|
MIL-S-6904 Revision B:1965
|
SIGNAL, EMERGENCY WARNING, GENERAL SPECIFICATION FOR |
|
MIL-P-5315 Revision B:1964
|
PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT |
|
MIL-T-58082 Revision A:1974
|
TESTER, PYROMETER & THERMOCOUPLE, FIELD, TYPE N-3A |
|
MIL-T-5583 Revision C:1987
|
TRANSMITTER, POSITION, 28 VOLTS DC |
|
MIL-M-7969 Revision C:1965
|
MOTOR, ALTERNATING CURRENT, 400 CYCLE, 115/200 VOLT SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL-L-19844 Revision A:1963
|
LEAD; SHIELDED, DETACHABLE IGNITION |
|
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
|
INDICATORS, AIRCRAFT, PRESSURE, VOLTAGE RATIO TYPE, GENERAL SPECIFICATION FOR |
|
MIL-B-3990 Revision D:1980
|
BEARINGS, ROLLER, NEEDLE, AIRFRAME, ANTIFRICTION, INCH |
|
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
|
CHARGERS, BATTERY, NICKEL-CADMIUM, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
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
|
INDICATORS, RATE OF FLOW, 0-5,000 PPH, INTEGRALLY LIGHTED |
|
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 |
|
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
|
TUBE, 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 |
|
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 |
|
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 |
|
MIL-DTL-25666 Revision F:1995
|
CONVERTER, LIQUID OXYGEN, CAPACITANCE TYPE GAGING, 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 |
|
MIL-W-48757 Base Document:1975
|
WARHEAD SECTION, GM, HE: M251 AND M251A1 SPARE PARTS FOR |
|
AND10050 Revision 21:2005
|
BOSSES, STRAIGHT DIMENSIONS FOR GASKET SEAL STRAIGHT THREAD |
|
MIL-C-7079 Revision A:1965
|
CIRCUIT BREAKERS, NON TRIP-FREE GENERAL SPECIFICATION FOR |
|
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-2A |
|
SAE ARP 5794 : 2014
|
CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD |
|
SAE AS 1371 : 2015
|
NUTS, SELF-LOCKING, CORROSION RESISTANT STEEL, HIGH STRENGTH, PREVAILING TORQUE, ALL METAL, 800 DEGREES F (427 DEGREES C) USE, UNJ THREAD FORM |
|
SAE AS 838 : 2013
|
AIRCRAFT HYDRAULIC STARTER/PUMPS |
|
NAS1599:1980
|
CONNECTORS, GENERAL PURPOSE, ELECTRICAL, MINIATURE CIRCULAR, ENVIRONMENT RESISTING, 200 DEG. C. MAXIMUM TEMPERATURE |
|
SAE MA 2250 : 2015
|
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 2, AND MIL-DTL-27599, SERIES 2 |