MIL I 23659 : C
|
INITIATOR, ELECTRIC, GENERAL DESIGN SPECIFICATION |
MIL-R-38370 Revision B:1972
|
RECORDING SET, FLIGHT DATA A/A24U-10 |
MIL-T-38034 Revision E:1970
|
TIMER, FIRE CONTROL, BOMBING, DUAL |
SAE MA 4098 : 2015
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, HEAVY DUTY, METALLIC REINFORCED, 204 DEGREE C, 35000 KPA, HYDRAULIC AND PNEUMATIC, METRIC |
MIL-STD-885 Revision B:1971
|
PROCUREMENT DATA PACKAGES |
MIL-I-7062 Revision C:1975
|
INDICATOR, POSITION, CONTROL SURFACES, 28 VOLT DC, GENERAL SPECIFICATION FOR |
MIL V 81940 : B
|
VALVE, SAMPLING AND BLEED, HYDRAULIC, TYPE LI SYSTEMS |
MIL H 38534 : B (1)
|
HYBRID MICROCIRCUITS, GENERAL SPECIFICATION FOR |
MIL-G-83872 Revision A:1977
|
GYROSCOPE, DISPLACEMENT, TYPE SBU-23/A |
JSGS-87231 Revision A:1995
|
ENGINES, AIRCRAFT, TURBINE |
MIL-I-83152 Revision B:1974
|
INDICATOR, INDICATED-AIRSPEED AVU-22/A (INDICATOR-TRANSDUCER) |
MIL-T-83460 Base Document:1975
|
TRANSDUCER, MOTIONAL PICKUP TRU-164/A |
MIL-STD-1375 Base Document:1970
|
PROVISIONING, INITIAL SUPPORT, GENERAL REQUIREMENTS FOR (INT NOTICE 1 (EC) |
MIL-I-7721 Revision D:1992
|
INDICATOR, VERTICAL SPEED, 3-INCH |
MIL-STD-188-125 Revision A:1994
|
HIGH-ALTITUDE ELECTROMAGNETIC PULSE (HEMP) PROTECTION FOR GROUND-BASED C41 FACILITIES PERFORMING CRITICAL, TIME-URGENT MISSIONS - VOLUME 1 - FIXED FACILITIES (METRIC) |
MIL-A-85055 Base Document:1979
|
AVIONICS SYSTEM PERFORMANCE SPECIFICATION FOR A-4M/AV-8 BOMBING SET, ANGLE RATE AN/ASB-19(V) |
MIL H 26626 : D
|
HOSE ASSEMBLY, TETRAFLUOROETHYLENE, OXYGEN |
MIL D 83320 : 0
|
DETECTOR, MAGNETIC AZIMUTH DSU-14/A |
MIL C 38214 : B
|
COMPASS, MAGNETIC,MOUNTED |
MIL-T-38473 Revision A:1972
|
TIMER, PRECISION, BOMBING, 0 - 30 MINUTES |
MIL-A-38140 Revision B:1977
|
ALTIMETER, PRESSURE AAU-16/A |
MIL-G-25597 Revision D:1973
|
GYROSCOPE, DISPLACEMENT, ROLL AND PITCH, TYPE MD-1 |
MIL-STD-482 Revision A:1974
|
CONFIGURATION STATUS ACCOUNTING DATA ELEMENTS AND RELATED FEATURES |
NMA MS2 : 1978
|
|
MIL B 8954 : B
|
BASE AND ACCESSORIES, AIRPORT MARKER LIGHTS, GENERAL SPECIFICATION FOR |
MIL-T-27305 Revision C:1987
|
TRANSFORMER AND INDUCTORS [AUDIO, POWER AND HIGH POWER PULSE] INDUCTOR, POWER TF5S04ZZ |
MIL M 87268 : 1992
|
MANUALS, INTERACTIVE ELECTRONIC TECHNICAL - GENERAL CONTENT, STYLE, FORMAT & USER-INTERACTION REQUIREMENTS |
MIL P 83207 : B
|
PITOT STATIC TUBE, NOSE BOOM, COMPENSATED, GENERAL SPECIFICATION FOR |
SAE AS 6451 : 2013
|
SHIELDS, PROTECTIVE, AIRCRAFT AND MISSILES |
MIL-D-8684 Revision B:1959
|
DATA AND TESTS, ENGINEERING, CONTACT REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE SYSTEMS |
MIL-P-6457 Revision E:1974
|
POWER SUPPLY, METALLIC RECTIFIER TYPE, GENERAL SPECIFICATION FOR |
MIL B 83424 : 0
|
BATTERY SYSTEMS, SEALED CELL, NICKEL CADMIUM, INTEGRAL CHARGE CONTROL, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-D-81303 Revision A:1966
|
DESIGN AND EVALUATION OF CARTRIDGES FOR STORES SUSPENSION EQUIPMENT |
MIL-STD-188-125-1 Base Document:1998
|
HIGH-ALTITUDE ELECTROMAGNETIC PULSE (HEMP) PROTECTION FOR GROUND-BASED C[4]1 FACILITIES PERFORMING CRITICAL, TIME-URGENT MISSIONS PART 1 FIXED FACILITIES |
MIL-DTL-25949 Revision F:1995
|
ACCELEROMETER, AIRCRAFT RANGE -5 TO 10G UNITS, INTEGRALLY LIGHTED |
SAE ARP 1987 : 2013
|
TITLES, SAE G-3 COMMITTEE DOCUMENT, SELECTION OF |
SAE AS 1501 : 1994
|
HOSE, AIR DUCT, FLEXIBLE, NONMETALLIC, AIRCRAFT |
MIL-C-4751 Revision D:1983
|
CASTERS, RIGID AND SWIVEL, PRECISION HEAVY DUTY, AND SHOCK ABSORBING |
MIL-HDBK-2193 Base Document:1994
|
HYDRAULIC SYSTEM COMPONENTS, SHIP |
MIL BULL 343 : A
|
DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
MIL I 38535 : B (1)
|
INTEGRATED CIRCUITS (MICROCIRCUITS) MANUFACTURING, GENERAL SPECIFICATION FOR |
MIL-S-6451 Revision E:1977
|
SHIELD, PROTECTIVE, AIRCRAFT AND MISSILES |
MIL C 38159 : B
|
CONNECTOR, ELECTRIC, RAMP POWER, 480/277 VOLTS, GENERAL SPECIFICATION FOR |
MIL-H-8775 Revision D:1976
|
HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
MIL-W-44167 Revision B:1992
|
WASHING MACHINE, LAUNDRY: OPEN END TYPE, TRAILER MOUNTED |
MIL-D-23615 Revision C:1993
|
DESIGN AND EVALUATION OF CARTRIDGE ACTUATED DEVICES |
MIL-DTL-6162 Revision C:2000
|
GENERATORS AND STARTER-GENERATORS, ELECTRICAL DIRECT CURRENT, NOMINAL 30 VOLTS, AIRCRAFT GENERAL SPECIFICATION FOR |
MIL-H-25475 Revision B:1971
|
HYDRAULIC SYSTEM, MISSILE, DESIGN, INSTALLATION TESTS AND DATE REQUIREMENTS, GENERAL REQUIREMENTS FOR |
MIL-I-6447 Revision C:1974
|
INDICATOR, TRUE AIRSPEED TYPE M 1A |
MIL-C-48481 Revision C:1995
|
CIRCUIT CARD ASSEMBLY - FTS INPUT SIMULATER AND DL TEST |
MIL-M-87113 Revision A:1993
|
MASK, OXYGEN, MBU-10/P |
EIA CMB 6-1 : 2014 STABILIZED
|
CONFIGURATION AND DATA MANAGEMENT REFERENCES |
MIL-STD-875 Revision A:1974
|
TYPE DESIGNATION SYSTEM FOR AERONAUTICAL AND SUPPORT EQUIPMENT |
MIL-P-24423 Base Document:1970
|
PROPULSION AND AUXILIARY CONTROL CONSOLES AND ASSOCIATED CONTROL AND INSTRUMENTATION EQUIPMENT, NAVAL SHIPBOARD USE, BASIC DESIGN REQUIREMENTS |
FF-L-2740 Revision A:1997
|
LOCKS, COMBINATION |
MIL-R-38435 Revision B:1968
|
RECORDING SET, SIGNAL DATA A/A 24U-6 |
MIL-C-38392 Revision A:1969
|
COMPRESSOR, HERMETIC, AIR CONDITIONING, GENERAL SPECIFICATION FOR |
MIL-STD-973 Base Document:1992
|
CONFIGURATION MANAGEMENT |
MIL-R-8931 Revision A:1994
|
RESERVOIRS, AIRCRAFT AND MISSILE, HYDRAULIC SEPARATED TYPE |
MIL-C-5778 Revision D:1992
|
COVER, AIRCRAFT COMPONENTS, GENERAL REQUIREMENTS FOR |
MIL G 26611 : D
|
GENERATOR, TACHOMETER GEU-7/A, MINIATURE |
MIL-A-83469 Base Document:1976
|
ADJUSTER, LAP BELT, 1-3/4 INCH WEBBING |
MIL M 63010 : 0
|
MANUAL, TECHNICAL, DOD STANDARD GENERATOR SETS |
MIL-B-26220 Revision D:1974
|
BATTERIES, STORAGE, AIRCRAFT, NICKEL-CADMIUM GENERAL SPECIFICATION FOR |
MIL-S-63280 Base Document:1978
|
SOLENOID FOR MACHINE GUN, CALIBER .50, FIXED M85 |
MIL S 25057 : B
|
SCREEN SYSTEM, AIR INLET, AIRCRAFT TURBINE ENGINE, GENERAL SPECIFICATION FOR |
MIL-S-8512 Revision D:1974
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
MIL-T-26017 Revision C:1972
|
TEST STAND, HYDRAULIC SYSTEM COMPONENTS, TYPE MK-3A (STAND, TEST, AIRCRAFT HYDRAULIC SYSTEM, ELECTRIC MOTOR DRIVEN, TYPE MK-3A) |
MIL-A-27471 Revision C:1993
|
ADAPTER, PRESSURE-REDUCER, IN-LINE CRU-43A/A |
MIL W 50275 : A NOTICE 2
|
WARHEAD, HE, M18A1 PARTS FOR |
MIL-S-83427 Base Document:1974
|
SURVIVAL KIT CONTAINERS, CNU-129(V)/P AND CNU-130/P |
MIL L 58085 : A
|
LIGHT, BEACON, ANTI COLLISION AIRCRAFT |
MIL B 8075 : D
|
BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
MIL-S-83129 Revision A:1972
|
SPECTROMETER, FLUID ANALYSIS A/E35U-3 |
MIL-D-8685 Revision B:1967
|
DATA AND TESTS, ENGINEERING, CONTRACT REQUIREMENTS FOR GUIDED MISSILE TARGET SYSTEMS |
MIL-DTL-85110 Revision B:1997
|
BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR |
SAE MA 2151 : 2015
|
CLAMP ASSEMBLIES, SADDLE OR OMEGA STYLE, TWO POINT MOUNT, MULTIPLE SHAPES, METRIC |
SAE MA 1975 : 2015
|
HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID REINFORCED, 135 DEGREE C, STANDARD DUTY, 28000/21000 KPA, HYDRAULIC, AIRCRAFT SYSTEMS |
SAE AS 8700 : 1999
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL C 83867 : B
|
CONNECTOR, OXYGEN MASK HOSE NON-EJECTION TYPE |
MIL-H-38360 Revision B:1966
|
HOSE, ASSEMBLIES, TETRAFLUOROETHYLENE, HIGH-TEMPERATURE, HIGH PRESSURE, 3000 PSI HYDRAULIC AND PNEUMATIC |
MIL-S-8812 Revision D:1975
|
STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
MIL-M-27274 Revision E:1993
|
MASK, OXYGEN MBU-5/P |
MIL F 83296 : 0
|
FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, HIGH PRESSURE (3,000 PSI HYDRAULIC AND PNEUMATIC) |
MIL T 5350 : E
|
TRANSMITTER, SYNCHRO OPERATED, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-A-83216 Revision B:1976
|
AIR CONDITIONER A/E32C-39 |
MIL-I-27304 Revision E:1977
|
INDICATOR, RATE OF FLOW |
MIL-T-7771 Revision B:1980
|
TUBE, EXTENSION, GYRO STABILIZED DRIFT METER |
MIL-D-8804 Revision B:1993
|
DE-ICING SYSTEM, PNEUMATIC BOOT, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-C-7474 Revision E:1978
|
CASTER, INDUSTRIAL |
MIL-STD-965 Revision B:1993
|
PARTS CONTROL PROGRAM |
MIL-R-7705 Revision B:1975
|
RADOME, GENERAL SPECIFICATION FOR |
AWS B5.4 : 2005
|
SPECIFICATION FOR THE QUALIFICATION OF WELDER TEST FACILITIES |
MIL-R-38162 Revision B:1971
|
RADIOSONDE SET AN/AMT 13 |
MIL-A-38202 Revision C:1972
|
AIRCRAFT ARRESTING SYSTEM BAK-12A/E32A; PORTABLE, ROTARY FRICTION |
MIL-STD-1806 Base Document:1990
|
MARKING TECHNICAL DATA PREPARED BY OR FOR THE DEPARTMENT OF DEFENSE |
MIL C 71167 : 0
|
CARTRIDGE, 7.62mm, M973 BALL SHORT RANGE TRAINING AMMUNITION, PERFORMANCE SPECIFICATION FOR |
MIL-C-5136 Revision C:1968
|
CABLE, POWER, ELECTRICAL POLYCHLOROPRENE SHEATHED, BUNA COMPOUND INSULATED |
MIL-T-27200 Revision C:1975
|
TRANSMITTER, RATE GYROSCOPE TRU-2A/A |
MIL-M-38761-1 Revision B:1994
|
MICROFILM IMAGE CARDS AND TABULATING CARDS USED FOR RECORDING ENGINEERING DRAWINGS AND ASSOCIATED DATA |
MIL-I-8700 Revision A:1970
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
SAE MA 1339 : 2015
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 21,000 KPA, 204 DEGREE C, LIGHTWEIGHT, HYDRAULIC AND PNEUMATIC, METRIC |
SAE AS 838 : 2013
|
AIRCRAFT HYDRAULIC STARTER/PUMPS |
SAE AS 4098 : 2013
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, HEAVY DUTY, METALLIC REINFORCED, 400 DEGREE F, 5000 PSI HYDRAULIC AND PNEUMATIC |
MIL C 71168 : 0
|
CARTRIDGE, 7.62mm, M974 TRACER SHORT RANGE TRAINING AMMUNITION PERFORMANCE SPECIFICATION FOR |
MIL L 27639 : C (2)
|
LIFE PRESERVER INFLATING ASSEMBLY FLU-1A/P |
MIL-D-55176 Revision C:1966
|
DATA, ELECTRONICS COMMAND ENGINEERING DOCUMENT CONTROL |
MIL I 38135 : B (3)
|
INDICATOR, INDICATED AIRSPEED AVU 19/A STANDBY |
SAE ARP 1281 : 2002
|
ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
MIL G 8360 : A
|
GAGE, PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE, 10-75 IN MERCURY TYPE MB 1 |
MIL S 9479 : C
|
|
MIL S 29580 : B
|
SPECTACLES, AVIATOR'S, MULTIPLE WAVE LENGTH LASER PROTECTIVE, EDU 5 P (WITH CASE) |
MIL-F-60342 Revision A:1972
|
FUZE, POINT DETONATING, M525 LOADING, ASSEMBLING AND PACKING |
MIL-A-5034 Revision B:1979
|
ADAPTER, BOMB RACK, 30-INCH, AERO 1A |
MIL-C-48480 Revision C:1995
|
CIRCUIT CARD ASSEMBLY - LOGIC AND REFERENCE |
MIL-M-63023 Revision A:1991
|
MANUAL, TECHNICAL, TRANSPORTABILITY GUIDANCE FOR MILITARY MATERIAL PREPARATION OF |
MIL-S-62300 Base Document:1983
|
SWITCH, PRESSURE |
MIL C 27889 : D
|
COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING, CPU-46/A, GENERAL SPECIFICATION FOR AND MTU-38/A MOUNTING TRAY |
MIL-V-27296 Revision C:1993
|
VALVE, OXYGEN MASK, COMBINATION INHALATION AND EXHALATION |
MIL-STD-1947 Base Document:1985
|
ULTRASONIC WELDING OF ALUMINUM AND ALUMINUM ALLOY MATERIALS |
MIL-C-26485 Revision D:1968
|
CONTROL ASSEMBLY, ATTITUDE, GYROSCOPIC AF/A24G-1A |
MIL-I-22126 Revision B:1972
|
INDICATOR, TORQUEMETER, ENGINE, TURBOPROP |
MIL I 83452 : LATEST
|
INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
MIL-M-82376 Revision B:1990
|
MANUAL, TECHNICAL, OPERATION AND MAINTENANCE INSTRUCTIONS FOR TRAINING DEVICES |
MIL-I-25861 Revision D:1967
|
INDICATOR, PRESSURE, HYDRAULIC, 0-4000 PSI INTEGRALLY LIGHTED |
MIL D 5480 : F
|
DATA, ENGINEERING AND TECHNICAL REPRODUCTION REQUIREMENTS FOR |
MIL-H-27269 Revision A:1977
|
HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
MIL-DTL-32018 Base Document:2001
|
CORD ASSEMBLY, MILD DETONATION, CANOPY PERIPHERY, P/N 837AS118 |
MIL-HDBK-814 Base Document:1994
|
IONIZING DOSE AND NEUTRON HARDNESS ASSURANCE GUIDELINES FOR MICROCIRCUITS AND SEMICONDUCTOR DEVICES |
MIL C 7989 : B
|
COVER, LIGHT TRANSMITTING, FOR AERONAUTICAL LIGHTS, GENERAL SPECIFICATION FOR |
DOD-D-1000 Revision B:1977
|
DRAWINGS, ENGINEERING AND ASSOCIATED LISTS |
MIL-D-24241 Base Document:1966
|
DRAWING, SONAR SYSTEMS, PRELIMINARY INSTALLATION PLANNING |
MIL-I-25645 Revision D:1970
|
INDICATOR, LIQUID OXYGEN QUANTITY, CAPACITANCE TYPE, GENERAL SPECIFICATION FOR |
MIL S 38039 : B
|
SYSTEM, ILLUMINATED, WARNING, CAUTION, AND ADVISORY, GENERAL SPECIFICATION FOR |
MIL R 83055 : 0
|
RAIN REPELLENT DISPENSING SYSTEMS, AIRCRAFT WINDSHIELD, GENERAL SPECIFICATION FOR |
MIL-DTL-25561 Revision B:1995
|
GRIP ASSEMBLY, CONTROLLER, AIRCRAFT, TYPE MC-2 |
MIL-C-7488 Revision A:1974
|
COOLERS, OIL, PLATE, AIRCRAFT |
MIL-G-83380 Base Document:1979
|
GENERATOR SET, GAS TURBINE ENGINE DRIVEN, 30 AND 60 KW, 400 HZ |
MIL-E-25499 Revision C:1970
|
ELECTRICAL SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION OF, GENERAL REQUIREMENTS FOR |
MIL-HDBK-3001 Base Document:2001
|
GUIDE TO THE GENERAL STYLE AND FORMAT OF U.S. NAVY WORK PACKAGE TECHNICAL MANUALS |
MIL-DTL-81014 Revision B:2001
|
HOOK, HELICOPTER EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C |
MIL M 63005 : C
|
MANUAL, TECHNICAL FOR PREPARATION FOR SHIPMENT OF ARMY AIRCRAFT |
MIL-S-38399 Revision A:1975
|
STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR |
MIL-A-0083216 Revision C:1976
|
AIR CONDITIONER, HORIZONTAL, 54,000 BTUH, 208/230 V |
MIL-F-50990 Base Document:1973
|
FUZE, BOMB: MECHANICAL NOSE, THERMALLY PROTECTED, M904E4, ASSEMBLY |
MIL A 83419 : C
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
MIL A 85046 : 0
|
ACTUATOR, LINEAR ELECTROMECHANICAL |
MIL P 83206 : B
|
PITOT STATIC TUBE, L SHAPED, COMPENSATED, GENERAL SPECIFICATION FOR |
MIL M 63000 : C (1)
|
MANUALS, TECHNICAL - GENERAL REQUIREMENTS FOR MANUSCRIPTS |
MIL-A-48078 Revision A:1988
|
AMMUNITION, STANDARD QUALITY ASSURANCE PROVISIONS, GENERAL SPECIFICATION FOR |
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 F 38363 : B (3)
|
FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-A-27261 Revision A:1966
|
ACCELEROMETER, AIRCRAFT |
SAE MA 620 : 2015
|
HOSE ASSEMBLIES, CONVOLUTED POLYTETRAFLUOROETHYLENE METALLIC REINFORCED, HIGH TEMPERATURE, MEDIUM PRESSURE, AIRCRAFT METRIC |
MIL-A-81403 Base Document:1967
|
ALTIMETER-ENCODER, AAU-21/A |
SAE AS 4604 : 2003
|
HOSE ASSEMBLY, 3000 PSI, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 400 DEGREES F, HEAVY DUTY, AIRCRAFT HYDRAULIC SYSTEMS |
SAE AS 1227 : 2013
|
HOSE ASSEMBLY, CONVOLUTED POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, LOW PRESSURE, UP TO 400 DEGREES F, AIRCRAFT |
SAE MA 614 : 2015
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE (PTFE), METALLIC REINFORCED, 28,000 KPA, 204 DEGREES C, HYDRAULIC, METRIC |
MIL C 38240 : C
|
COMPUTER, ALTITUDE, ALTITUDE ENCODING CPU 66, GENERAL SPECIFICATION FOR AND MTU 39/A MOUNTING TRAY |
MIL-H-11689 Revision C:1974
|
HAMMER, PNEUMATIC, PORTABLE, NAIL-DRIVING |
MIL-F-8615 Revision D:1976
|
FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
MIL-B-4173 Revision B:1969
|
BENCH, WORK, GENERAL PURPOSE |
MIL D 26392 : C
|
DUMMY CONVERTERS, LIQUID OXYGEN INDICATOR SYSTEM 10 LITER CRU-23/A AND 25 LITER CRU-24/A |
MIL-G-58103 Base Document:1979
|
GRIP ASSEMBLY, CYCLIC CONTROLLER, HELICOPTER |
MIL T 83174 : B (3)
|
TRANSMITTER, ACCELEROMETER, AXIAL |
MIL-S-7470 Revision A:1975
|
SHAFT, POWER TRANSMISSION, AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR |
MIL-H-21660 Revision A:1992
|
HOOK, THRUST, JATO - 1000 POUNDS NOMINAL THRUST |
MIL-E-83304 Revision B:1975
|
EXTINGUISHER UNIT, FIRE BROMOCHLORODIFLUOROMETHANE, FEU-2/S32P, 40 GALLON CAPACITY, TRUCK MOUNTING |
SAE AS 1472 : 2013
|
HOSE ASSEMBLY, LOW PRESSURE, POTABLE WATER |
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 |
MIL-I-83245 Revision A:1994
|
INDICATOR SET, OIL PRESSURE A/A24J-17 |
MIL-I-83262 Revision B:1977
|
INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
MIL-D-18300 Revision H:1993
|
DESIGN EXAMINATIONS, ENGINEERING AVIONIC SYSTEMS/EQUIPMENT GENERAL REQUIREMENTS FOR |
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-I-83117 Revision B:1975
|
INDICATOR, ANGLE OF ATTACK |
DOD-STD-2101 Base Document:1979
|
CLASSIFICATION OF CHARACTERISTICS |
MIL-T-60530 Revision A:1971
|
TECHNICAL DATA PACKAGE FOR AMC MATERIAL |
MIL M 4803 : D
|
MOTOR-GENERATOR, 400 HZ PRECISE OUTPUT, GENERAL REQUIREMENTS FOR |
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-I-7084 Revision A:1988
|
INDICATOR, PRESSURE, HYDRAULIC 0-4,000 PSI |
MIL-PRF-63003 Revision B:1998
|
MANUALS, TECHNICAL: BATTLEFIELD DAMAGE ASSESSMENT AND REPAIR, PREPARATION OF |
MIL-STD-188-125-2 Base Document:1999
|
HIGH-ALTITUDE ELECTROMAGNETIC PULSE (HEMP) PROTECTION FOR GROUND-BASED C[4]I FACILITIES PERFORMING CRITICAL, TIME-URGENT MISSIONS - PART 2 - TRANSPORTABLE SYSTEMS |
MIL-C-27505 Revision B:1967
|
Cartridge, Engine Starter MXU-4A/A |
MIL-I-27619 Revision G:1974
|
INDICATORS, ATTITUDE DIRECTOR |
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 T 26898 : B
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TEST SET, AIRFIELD LIGHTING SYSTEMS, TYPE MM-1 |
MIL-B-3990 Revision D:1980
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BEARINGS, ROLLER, NEEDLE, AIRFRAME, ANTIFRICTION, INCH |
MIL-DTL-29469 Revision A:1998
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CHAPLAIN'S KIT - COMBAT |
MIL R 5149 : B
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ROCKET ENGINE, LIQUID PROPELLANT GENERAL SPECIFICATION FOR |
MIL-I-81049 Revision A:1972
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INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
MIL I 27190 : B
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INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI |
MIL-D-38134 Revision A:1971
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DETECTOR, MAGNETIC AZIMUTH DSU-4/A, HIGH TEMPERATURE |
MIL-T-5955 Revision C:1970
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TRANSMISSION SYSTEM, VTOL-STOL GENERAL REQUIREMENTS FOR |
MIL-DTL-85855 Revision A:1999
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VALVE, QUICK DISCONNECT, FOR THE PROTECTIVE ASSEMBLY, CHEMICAL, BIOLOGICAL, RADIOLOGICAL (CBR), A/P22P-9 (V) |
MIL-P-48494 Revision A:1995
|
|
MIL I 83361 : (4)
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INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
MIL-P-38136 Revision A:1969
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PITOT STATIC TUBE COMPENSATED TRU 62/A |
MIL-DTL-25666 Revision F:1995
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CONVERTER, LIQUID OXYGEN, CAPACITANCE TYPE GAGING, GENERAL SPECIFICATION FOR |
MIL-P-8945 Revision A:1967
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PANEL, RELAY, PILOT, ENCLOSED, AIRPORT LIGHTING |
MIL-STD-834 Revision C:1974
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PACKAGING DATA FORMS, INSTRUCTIONS FOR PREPARATION AND USE OF |
SAE AS 5778 : 1997
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COVERS, AIRCRAFT COMPONENTS, GENERAL REQUIREMENTS FOR |
MIL-PRF-63045 Revision B:1997
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MANUALS, TECHNICAL: PREPARATION OF DEPOT MANUALS FOR DEPOT TEST, MEASUREMENT AND DIAGNOSTIC EQUIPMENT |
MIL T 25627 : C
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TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |
SAE MA 2150 : 2015
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CLAMPS, LOOP OR P STYLE, SINGLE POINT MOUNT, MULTIPLE SHAPES, METRIC |
MIL-A-83039 Revision B:1971
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AIR CONDITIONER A/M32C-10A AIR CYCLE FOR AIRCRAFT GROUND SUPPORT |
SAE AS 38404 : 2013
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COUPLINGS, HOSE, REATTACHABLE SCREW-ON |
SAE MA 4623 : 2015
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Hose Assembly, Polytetrafluoroethylene, Para Aramid Reinforced Heavy-Duty, 21 000 kPa, 135 °C, Aircraft Hydraulic Systems, Metric |