|
MIL C 83867 : B
|
CONNECTOR, OXYGEN MASK HOSE NON-EJECTION TYPE |
|
MIL DTL 6162 : C
|
GENERATORS AND STARTER-GENERATORS, ELECTRICAL DIRECT CURRENT, NOMINAL 30 VOLTS, AIRCRAFT GENERAL SPECIFICATION FOR |
|
MIL C 71168 : 0
|
CARTRIDGE, 7.62mm, M974 TRACER SHORT RANGE TRAINING AMMUNITION PERFORMANCE SPECIFICATION FOR |
|
MIL H 38360 : B
|
HOSE, ASSEMBLIES, TETRAFLUOROETHYLENE, HIGH-TEMPERATURE, HIGH PRESSURE, 3000 PSI HYDRAULIC AND PNEUMATIC |
|
MIL H 25475 : B
|
HYDRAULIC SYSTEM, MISSILE, DESIGN, INSTALLATION TESTS AND DATE REQUIREMENTS, GENERAL REQUIREMENTS FOR |
|
MIL C 38240 : C
|
COMPUTER, ALTITUDE, ALTITUDE ENCODING CPU 66, GENERAL SPECIFICATION FOR AND MTU 39/A MOUNTING TRAY |
|
MIL I 6447 : C
|
INDICATOR, TRUE AIRSPEED TYPE M 1A |
|
MIL C 48481 : C
|
CIRCUIT CARD ASSEMBLY - FTS INPUT SIMULATER AND DL TEST |
|
MIL I 23659 : C
|
INITIATOR, ELECTRIC, GENERAL DESIGN SPECIFICATION |
|
MIL L 27639 : C (2)
|
LIFE PRESERVER INFLATING ASSEMBLY FLU-1A/P |
|
MIL D 55176 : C
|
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 S 8812 : D
|
STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
|
MIL M 87113 : A
|
MASK, OXYGEN, MBU-10/P |
|
MIL R 38370 : B
|
RECORDING SET, FLIGHT DATA A/A24U-10 |
|
MIL T 38034 : E
|
TIMER, FIRE CONTROL, BOMBING, DUAL |
|
MIL H 11689 : C
|
HAMMER, PNEUMATIC, PORTABLE, NAIL-DRIVING |
|
MIL F 8615 : D
|
FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
|
MIL B 4173 : B
|
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 : 0
|
GRIP ASSEMBLY, CYCLIC CONTROLLER, HELICOPTER |
|
MIL G 8360 : A
|
GAGE, PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE, 10-75 IN MERCURY TYPE MB 1 |
|
MIL S 9479 : C
|
|
|
EIA CMB 6-1 : 2014 STABILIZED
|
CONFIGURATION AND DATA MANAGEMENT REFERENCES |
|
MIL STD 875 : A
|
TYPE DESIGNATION SYSTEM FOR AERONAUTICAL AND SUPPORT EQUIPMENT |
|
MIL T 83174 : B (3)
|
TRANSMITTER, ACCELEROMETER, AXIAL |
|
MIL S 7470 : A
|
SHAFT, POWER TRANSMISSION, AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR |
|
MIL H 21660 : A
|
HOOK, THRUST, JATO - 1000 POUNDS NOMINAL THRUST |
|
MIL S 29580 : B
|
SPECTACLES, AVIATOR'S, MULTIPLE WAVE LENGTH LASER PROTECTIVE, EDU 5 P (WITH CASE) |
|
MIL F 60342 : A
|
FUZE, POINT DETONATING, M525 LOADING, ASSEMBLING AND PACKING |
|
MIL A 5034 : B
|
ADAPTER, BOMB RACK, 30-INCH, AERO 1A |
|
MIL C 48480 : C
|
CIRCUIT CARD ASSEMBLY - LOGIC AND REFERENCE |
|
MIL M 63023 : A
|
MANUAL, TECHNICAL, TRANSPORTABILITY GUIDANCE FOR MILITARY MATERIAL PREPARATION OF |
|
MIL STD 885 : B
|
PROCUREMENT DATA PACKAGES |
|
MIL E 83304 : B
|
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 : D
|
AMPLIFIER-INDICATOR GROUP, INDICATED AIRSPEED A/A24G-10 |
|
MIL A 83212 : A
|
ALTIMETER, PRESSURE AAU-27/A |
|
MIL G 26988 : C
|
GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
|
MIL I 83245 : A
|
INDICATOR SET, OIL PRESSURE A/A24J-17 |
|
MIL I 83262 : B
|
INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
|
MIL S 62300 : 0
|
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 : C
|
VALVE, OXYGEN MASK, COMBINATION INHALATION AND EXHALATION |
|
MIL P 24423 : 0
|
PROPULSION AND AUXILIARY CONTROL CONSOLES AND ASSOCIATED CONTROL AND INSTRUMENTATION EQUIPMENT, NAVAL SHIPBOARD USE, BASIC DESIGN REQUIREMENTS |
|
MIL I 7062 : C
|
INDICATOR, POSITION, CONTROL SURFACES, 28 VOLT DC, GENERAL SPECIFICATION FOR |
|
MIL STD 1947 : 0
|
ULTRASONIC WELDING OF ALUMINUM AND ALUMINUM ALLOY MATERIALS |
|
MIL C 26485 : D
|
CONTROL ASSEMBLY, ATTITUDE, GYROSCOPIC AF/A24G-1A |
|
MIL I 22126 : B
|
INDICATOR, TORQUEMETER, ENGINE, TURBOPROP |
|
MIL I 83452 : LATEST
|
INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
|
MIL M 82376 : B
|
MANUAL, TECHNICAL, OPERATION AND MAINTENANCE INSTRUCTIONS FOR TRAINING DEVICES |
|
MIL I 25861 : D
|
INDICATOR, PRESSURE, HYDRAULIC, 0-4000 PSI INTEGRALLY LIGHTED |
|
MIL D 5480 : F
|
DATA, ENGINEERING AND TECHNICAL REPRODUCTION REQUIREMENTS FOR |
|
MIL M 27274 : E
|
MASK, OXYGEN MBU-5/P |
|
FF L 2740 : A
|
LOCKS, COMBINATION |
|
MIL R 38435 : B
|
RECORDING SET, SIGNAL DATA A/A 24U-6 |
|
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 : A
|
GYROSCOPE, DISPLACEMENT, TYPE SBU-23/A |
|
JSGS 87231 : A
|
ENGINES, AIRCRAFT, TURBINE |
|
MIL D 18300 : H
|
DESIGN EXAMINATIONS, ENGINEERING AVIONIC SYSTEMS/EQUIPMENT GENERAL REQUIREMENTS FOR |
|
MIL I 27623 : C
|
INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
|
MIL I 25950 : B
|
INDICATOR, PRESSURE, OIL, 0-100 PSI |
|
MIL I 7087 : A
|
INDICATOR, PRESSURE OIL, 0-200 PSI |
|
MIL H 27269 : A
|
HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
|
MIL DTL 32018 : 2001
|
CORD ASSEMBLY, MILD DETONATION, CANOPY PERIPHERY, P/N 837AS118 |
|
MIL HDBK 814 : 0
|
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 : B
|
DRAWINGS, ENGINEERING AND ASSOCIATED LISTS |
|
MIL D 24241 : 0
|
DRAWING, SONAR SYSTEMS, PRELIMINARY INSTALLATION PLANNING |
|
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 C 38392 : A
|
COMPRESSOR, HERMETIC, AIR CONDITIONING, GENERAL SPECIFICATION FOR |
|
MIL I 83152 : B
|
INDICATOR, INDICATED-AIRSPEED AVU-22/A (INDICATOR-TRANSDUCER) |
|
MIL T 83460 : 0
|
TRANSDUCER, MOTIONAL PICKUP TRU-164/A |
|
MIL STD 1375 : 0
|
PROVISIONING, INITIAL SUPPORT, GENERAL REQUIREMENTS FOR (INT NOTICE 1 (EC) |
|
MIL I 7721 : D
|
INDICATOR, VERTICAL SPEED, 3-INCH |
|
MIL I 7071 : B
|
INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
|
MIL I 83117 : B
|
INDICATOR, ANGLE OF ATTACK |
|
DOD STD 2101 : 0
|
CLASSIFICATION OF CHARACTERISTICS |
|
MIL T 60530 : A
|
TECHNICAL DATA PACKAGE FOR AMC MATERIAL |
|
MIL M 4803 : D
|
MOTOR-GENERATOR, 400 HZ PRECISE OUTPUT, GENERAL REQUIREMENTS FOR |
|
MIL I 25645 : D
|
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 : B
|
GRIP ASSEMBLY, CONTROLLER, AIRCRAFT, TYPE MC-2 |
|
MIL C 7488 : A
|
COOLERS, OIL, PLATE, AIRCRAFT |
|
MIL A 83216 : B
|
AIR CONDITIONER A/E32C-39 |
|
MIL STD 973 : 0
|
CONFIGURATION MANAGEMENT |
|
MIL R 8931 : A
|
RESERVOIRS, AIRCRAFT AND MISSILE, HYDRAULIC SEPARATED TYPE |
|
MIL C 5778 : D
|
COVER, AIRCRAFT COMPONENTS, GENERAL REQUIREMENTS FOR |
|
MIL STD 188/125 : A
|
HIGH-ALTITUDE ELECTROMAGNETIC PULSE (HEMP) PROTECTION FOR GROUND-BASED C41 FACILITIES PERFORMING CRITICAL, TIME-URGENT MISSIONS - VOLUME 1 - FIXED FACILITIES (METRIC) |
|
MIL A 85055 : 0
|
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 I 27848 : B
|
INDICATOR, HORIZONTAL SITUATION AQU-4/A |
|
MIL L 85314 : A
|
LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
|
MIL I 7084 : A
|
INDICATOR, PRESSURE, HYDRAULIC 0-4,000 PSI |
|
MIL PRF 63003 : B
|
MANUALS, TECHNICAL: BATTLEFIELD DAMAGE ASSESSMENT AND REPAIR, PREPARATION OF |
|
MIL STD 188 125 2 : 0
|
HIGH-ALTITUDE ELECTROMAGNETIC PULSE (HEMP) PROTECTION FOR GROUND-BASED C[4]I FACILITIES PERFORMING CRITICAL, TIME-URGENT MISSIONS - PART 2 - TRANSPORTABLE SYSTEMS |
|
MIL G 83380 : 0
|
GENERATOR SET, GAS TURBINE ENGINE DRIVEN, 30 AND 60 KW, 400 HZ |
|
MIL E 25499 : C
|
ELECTRICAL SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION OF, GENERAL REQUIREMENTS FOR |
|
MIL I 27304 : E
|
INDICATOR, RATE OF FLOW |
|
MIL T 7771 : B
|
TUBE, EXTENSION, GYRO STABILIZED DRIFT METER |
|
MIL G 26611 : D
|
GENERATOR, TACHOMETER GEU-7/A, MINIATURE |
|
MIL A 83469 : 0
|
ADJUSTER, LAP BELT, 1-3/4 INCH WEBBING |
|
MIL M 63010 : 0
|
MANUAL, TECHNICAL, DOD STANDARD GENERATOR SETS |
|
MIL T 38473 : A
|
TIMER, PRECISION, BOMBING, 0 - 30 MINUTES |
|
MIL A 38140 : B
|
ALTIMETER, PRESSURE AAU-16/A |
|
MIL C 27505 : B
|
CARTRIDGE, ENGINE STARTER MXU-4A/A |
|
MIL I 27619 : G
|
INDICATORS, ATTITUDE DIRECTOR |
|
MIL I 27851 : B
|
INDICATOR, INDICATED AIRSPEED AVU-17/A |
|
MIL T 25307 : D
|
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
|
TEST SET, AIRFIELD LIGHTING SYSTEMS, TYPE MM-1 |
|
MIL B 3990 : D
|
BEARINGS, ROLLER, NEEDLE, AIRFRAME, ANTIFRICTION, INCH |
|
MIL DTL 29469 : A
|
CHAPLAIN'S KIT - COMBAT |
|
MIL HDBK 3001 : 0
|
GUIDE TO THE GENERAL STYLE AND FORMAT OF U.S. NAVY WORK PACKAGE TECHNICAL MANUALS |
|
MIL DTL 81014 : B
|
HOOK, HELICOPTER EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C |
|
MIL M 63005 : C
|
MANUAL, TECHNICAL FOR PREPARATION FOR SHIPMENT OF ARMY AIRCRAFT |
|
MIL D 8804 : B
|
DE-ICING SYSTEM, PNEUMATIC BOOT, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL C 7474 : E
|
CASTER, INDUSTRIAL |
|
MIL STD 965 : B
|
PARTS CONTROL PROGRAM |
|
MIL R 7705 : B
|
RADOME, GENERAL SPECIFICATION FOR |
|
AWS B5.4 : 2005
|
SPECIFICATION FOR THE QUALIFICATION OF WELDER TEST FACILITIES |
|
MIL B 26220 : D
|
BATTERIES, STORAGE, AIRCRAFT, NICKEL-CADMIUM GENERAL SPECIFICATION FOR |
|
MIL S 63280 : 0
|
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 : D
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
|
MIL T 26017 : C
|
TEST STAND, HYDRAULIC SYSTEM COMPONENTS, TYPE MK-3A (STAND, TEST, AIRCRAFT HYDRAULIC SYSTEM, ELECTRIC MOTOR DRIVEN, TYPE MK-3A) |
|
MIL A 27471 : C
|
ADAPTER, PRESSURE-REDUCER, IN-LINE CRU-43A/A |
|
MIL G 25597 : D
|
GYROSCOPE, DISPLACEMENT, ROLL AND PITCH, TYPE MD-1 |
|
MIL STD 482 : A
|
CONFIGURATION STATUS ACCOUNTING DATA ELEMENTS AND RELATED FEATURES |
|
NMA MS2 : 1978
|
|
|
MIL R 5149 : B
|
ROCKET ENGINE, LIQUID PROPELLANT GENERAL SPECIFICATION FOR |
|
MIL I 81049 : A
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
|
MIL I 27190 : B
|
INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI |
|
MIL D 38134 : A
|
DETECTOR, MAGNETIC AZIMUTH DSU-4/A, HIGH TEMPERATURE |
|
MIL T 5955 : C
|
TRANSMISSION SYSTEM, VTOL-STOL GENERAL REQUIREMENTS FOR |
|
MIL DTL 85855 : A
|
VALVE, QUICK DISCONNECT, FOR THE PROTECTIVE ASSEMBLY, CHEMICAL, BIOLOGICAL, RADIOLOGICAL (CBR), A/P22P-9 (V) |
|
MIL P 48494 : A
|
|
|
MIL I 83361 : (4)
|
INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
|
MIL P 38136 : A
|
PITOT STATIC TUBE COMPENSATED TRU 62/A |
|
MIL S 38399 : A
|
STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR |
|
MIL A 0083216 : C
|
AIR CONDITIONER, HORIZONTAL, 54,000 BTUH, 208/230 V |
|
MIL F 50990 : 0
|
FUZE, BOMB: MECHANICAL NOSE, THERMALLY PROTECTED, M904E4, ASSEMBLY |
|
MIL A 83419 : C
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
|
MIL R 38162 : B
|
RADIOSONDE SET AN/AMT 13 |
|
MIL A 38202 : C
|
AIRCRAFT ARRESTING SYSTEM BAK-12A/E32A; PORTABLE, ROTARY FRICTION |
|
MIL STD 1806 : 0
|
MARKING TECHNICAL DATA PREPARED BY OR FOR THE DEPARTMENT OF DEFENSE |
|
MIL W 50275 : A NOTICE 2
|
WARHEAD, HE, M18A1 PARTS FOR |
|
MIL S 83427 : 0
|
SURVIVAL KIT CONTAINERS, CNU-129(V)/P AND CNU-130/P |
|
MIL L 58085 : A
|
LIGHT, BEACON, ANTI COLLISION AIRCRAFT |
|
MIL B 8954 : B
|
BASE AND ACCESSORIES, AIRPORT MARKER LIGHTS, GENERAL SPECIFICATION FOR |
|
MIL T 27305 : C
|
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 |
|
MIL DTL 25666 : F
|
CONVERTER, LIQUID OXYGEN, CAPACITANCE TYPE GAGING, GENERAL SPECIFICATION FOR |
|
MIL P 8945 : A
|
PANEL, RELAY, PILOT, ENCLOSED, AIRPORT LIGHTING |
|
MIL STD 834 : C
|
PACKAGING DATA FORMS, INSTRUCTIONS FOR PREPARATION AND USE OF |
|
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 : A
|
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 : A
|
ACCELEROMETER, AIRCRAFT |
|
SAE MA 620 : 2015
|
HOSE ASSEMBLIES, CONVOLUTED POLYTETRAFLUOROETHYLENE METALLIC REINFORCED, HIGH TEMPERATURE, MEDIUM PRESSURE, AIRCRAFT METRIC |
|
MIL A 81403 : 0
|
ALTIMETER-ENCODER, AAU-21/A |
|
MIL C 71167 : 0
|
CARTRIDGE, 7.62mm, M973 BALL SHORT RANGE TRAINING AMMUNITION, PERFORMANCE SPECIFICATION FOR |
|
MIL C 5136 : C
|
CABLE, POWER, ELECTRICAL POLYCHLOROPRENE SHEATHED, BUNA COMPOUND INSULATED |
|
MIL T 27200 : C
|
TRANSMITTER, RATE GYROSCOPE TRU-2A/A |
|
MIL M 38761/1 : B
|
MICROFILM IMAGE CARDS AND TABULATING CARDS USED FOR RECORDING ENGINEERING DRAWINGS AND ASSOCIATED DATA |
|
MIL I 8700 : A
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL B 8075 : D
|
BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
|
MIL S 83129 : A
|
SPECTROMETER, FLUID ANALYSIS A/E35U-3 |
|
MIL D 8685 : B
|
DATA AND TESTS, ENGINEERING, CONTRACT REQUIREMENTS FOR GUIDED MISSILE TARGET SYSTEMS |
|
MIL DTL 85110 : B
|
BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR |
|
SAE AS 6451 : 2013
|
SHIELDS, PROTECTIVE, AIRCRAFT AND MISSILES |
|
MIL D 8684 : B
|
DATA AND TESTS, ENGINEERING, CONTACT REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE SYSTEMS |
|
MIL P 6457 : E
|
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 : A
|
DESIGN AND EVALUATION OF CARTRIDGES FOR STORES SUSPENSION EQUIPMENT |
|
MIL STD 188 125 1 : 0
|
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 : F
|
ACCELEROMETER, AIRCRAFT RANGE -5 TO 10G UNITS, INTEGRALLY LIGHTED |
|
SAE AS 5778 : 1997
|
COVERS, AIRCRAFT COMPONENTS, GENERAL REQUIREMENTS FOR |
|
MIL PRF 63045 : B
|
MANUALS, TECHNICAL: PREPARATION OF DEPOT MANUALS FOR DEPOT TEST, MEASUREMENT AND DIAGNOSTIC EQUIPMENT |
|
MIL T 25627 : C
|
TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |
|
SAE MA 2150 : 2015
|
CLAMPS, LOOP OR P STYLE, SINGLE POINT MOUNT, MULTIPLE SHAPES, METRIC |
|
MIL A 83039 : B
|
AIR CONDITIONER A/M32C-10A AIR CYCLE FOR AIRCRAFT GROUND SUPPORT |
|
SAE MA 1339 : 2015
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 21,000 KPA, 204 DEGREE C, LIGHTWEIGHT, HYDRAULIC AND PNEUMATIC, METRIC |
|
SAE AS 38404 : 2013
|
COUPLINGS, HOSE, REATTACHABLE SCREW-ON |
|
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 |
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SAE AS 838 : 2013
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AIRCRAFT HYDRAULIC STARTER/PUMPS |
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SAE AS 4098 : 2013
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HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, HEAVY DUTY, METALLIC REINFORCED, 400 DEGREE F, 5000 PSI HYDRAULIC AND PNEUMATIC |
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SAE ARP 1987 : 2013
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TITLES, SAE G-3 COMMITTEE DOCUMENT, SELECTION OF |
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SAE MA 2151 : 2015
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CLAMP ASSEMBLIES, SADDLE OR OMEGA STYLE, TWO POINT MOUNT, MULTIPLE SHAPES, METRIC |
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SAE MA 1975 : 2015
|
HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID REINFORCED, 135 DEGREE C, STANDARD DUTY, 28000/21000 KPA, HYDRAULIC, AIRCRAFT SYSTEMS |
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SAE MA 614 : 2015
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HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE (PTFE), METALLIC REINFORCED, 28,000 KPA, 204 DEGREES C, HYDRAULIC, METRIC |
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SAE MA 4623 : 2015
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED HEAVY-DUTY, 21000 KPA, 135 DEGREE C, AIRCRAFT HYDRAULIC SYSTEMS, METRIC |
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SAE AS 1501 : 1994
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HOSE, AIR DUCT, FLEXIBLE, NONMETALLIC, AIRCRAFT |
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SAE MA 4098 : 2015
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, HEAVY DUTY, METALLIC REINFORCED, 204 DEGREE C, 35000 KPA, HYDRAULIC AND PNEUMATIC, METRIC |
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SAE AS 8700 : 1999
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INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |