MIL-A-83783 Base Document:1972
|
Adapter, Test, MX-9042/G |
MIL-A-38307 Revision A:1981
|
ACCELEROMETER, AIRCRAFT, MX-6663/AJB-7 |
MIL-STD-2156 Base Document:1983
|
LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
MIL-HDBK-59 Revision B:1994
|
COMPUTER AIDED ACQUISITION AND LOGISTIC SUPPORT (CALS) PROGRAM IMPLEMENTATION GUIDE |
MIL F 27272 : B
|
FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
DOD STD 100 : C NOTICE 6
|
ENGINEERING DRAWING PRACTICES |
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-R-81202 Revision D:1981
|
RECEIVER ASSEMBLY, NITROGEN, FOR LAU-7 SERIES LAUNCHERS |
MIL-T-26561 Revision C:1984
|
TESTER, TYPE MA-2 RECEPTION COUPLING BREAK-AWAY FORCE, PORTABLE |
MIL-S-25948 Revision J:1984
|
SUNGLASSES, HGU-4/P (WITH CASE) |
MIL-I-983 Revision E:1966
|
INTERIOR COMMUNICATION EQUIPMENT, NAVAL SHIPBOARD, BASIC DESIGN REQUIREMENTS FOR |
MIL-P-9388 Revision B:1986
|
PUMP, PRESSURE, OIL FREE AIR TYPE MA-2 |
MIL-HDBK-11991 Base Document:1996
|
DESIGN OF ELECTRICAL, ELECTRONIC, AND ELECTRO-MECHANICAL EQUIPMENT, GUIDED MISSILE AND ASSOCIATED WEAPONS SYSTEMS |
MIL C 27536 : B
|
COUPLING, CLAMP, GROOVED, V-BAND |
MIL-STD-372 Base Document:1988
|
WELDING, GAS METAL-ARC AND GAS TUNGSTEN-ARC, ALUMINUM ALLOYS, READILY WELDABLE FOR STRUCTURES, EXCLUDING ARMOR |
MIL B 5806 : F
|
BOX, SHIPPING, AND STORAGE, HELICOPTER BLADE |
MIL-A-55503 Base Document:1966
|
ATTITUDE HEADING REFERENCE SET AN/ASN-76 |
MIL-STD-1943 Base Document:1985
|
WELDING REPAIR OF STEEL CASTINGS (OTHER THAN ARMOR) METAL-ARC, MANUAL |
MIL-I-27196 Revision C:1988
|
INDICATOR, VERTICAL VELOCITY AAU-9/A, INTEGRALLY LIGHTED |
MIL V 27166 : D
|
VALVE, PRESSURE EQUALIZING, GASEOUS PRODUCTS |
MIL T 25620 : C
|
TESTER, OXYGEN MASK, HEADSET AND MICROPHONE, TYPE MQ-1A |
MIL I 27279 : B
|
INDICATOR, MACH NUMBER AVU-11/A, INTEGRAL LIGHTING |
MIL-B-82549 Revision A:1989
|
BOMB, GENERAL PURPOSE, MARK 83, 1000 POUND, EXPLOSIVE LOADING ASSEMBLING, AND PACKING |
DSCC 82027 : F
|
COIL, RADIOFREQUENCY AND CHOKE, RADIOFREQUENCY |
MIL-F-5591 Revision C:1986
|
FASTENERS, PANEL, NONSTRUCTURAL |
MIL-A-81973 Base Document:1974
|
AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR |
MIL V 24630 : 0
|
VALVES, CHECK, IN-LINE, FOR HYDRAULIC FLUID AND LUBRICATING OIL FLUID |
MIL-C-7580 Revision C:1989
|
COUPLING, FIRE HOSE, REUSABLE HIGH PRESSURE |
MIL V 5523 : D
|
VALVE, RELIEF, HYDRAULIC PRESSURE |
MIL-C-85521 Base Document:1983
|
CONCENTRATOR, OXYGEN, GGU-7/A |
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-STD-2097 Revision A:1989
|
ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
MIL-L-7806 Revision A:1956
|
LIGHT, PANEL, PLASTIC PLATE, LIGHTING |
MIL-M-19417 Revision D:1992
|
Mask Assemblies, Oxygen and Smoke, Full Face |
EIA CMB 6-1 : 2014 STABILIZED
|
CONFIGURATION AND DATA MANAGEMENT REFERENCES |
MIL-M-70466 Base Document:1993
|
MACHINE GUN, 7.62mm: M60E3 |
MIL V 7899 : C
|
VALVE, CHECK, AIRCRAFT FUEL SYSTEM |
MIL-A-27195 Revision A:1989
|
ACCELEROMETER, AIRCRAFT, MECHANICAL ABU-6/A |
MIL-A-6589 Revision A:1968
|
AMPLIFIER, ELECTRONIC CONTROL, SINGLE CHANNEL, TYPE A-2 |
MIL T 25446 : D
|
TRANSMITTER, TEMPERATURE, ELECTRICAL RESISTANCE |
MIL-S-63280 Base Document:1978
|
SOLENOID FOR MACHINE GUN, CALIBER .50, FIXED M85 |
MIL-S-6150 Revision D:1987
|
STARTER, ENGINE, ELECTRICAL, DIRECT CRANKING, AIRCRAFT 28 VOLT DC |
MIL-HDBK-2097 Revision A:1997
|
ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
MIL-C-4150 Revision J:1989
|
CASE, TRANSIT AND STORAGE, WATERPROOF AND WATER-VAPORPROOF |
MIL-DTL-85110 Revision B:1997
|
BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR |
DSCC 90029 : B
|
SHIELDING BEADS, FERRITE |
DOD-STD-1702 Base Document:1985
|
INTEGRATED LOGISTICS SUPPORT PROGRAMS FOR EQUIPMENT, SUBSYSTEMS AND SYSTEMS (METRIC) |
MIL-S-85510 Base Document:1981
|
|
MIL-S-7852 Revision B:1968
|
SEAT, AIRCREW, ADJUSTABLE SWIVEL TYPE E-1 |
MIL-V-8610 Revision B:1984
|
VALVE, FUEL SHUTOFF SOLENOID OPERATED, 28 VOLT, DC |
MIL-A-8868 Revision B:1987
|
AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS |
MIL-STD-1561 Revision B:1984
|
PROVISIONING PROCEDURES, UNIFORM DOD |
MIL-A-7237 Revision B:1975
|
AIR INDUCTION SYSTEM, RECIPROCATING ENGINE, GENERAL SPECIFICATION FOR |
MIL-M-85522 Revision A:1991
|
MONITOR, OXYGEN CRU-91/A |
MIL-S-9487 Revision C:1985
|
SWITCH, TRIGGER, SINGLE POLE, TWO STAGE, MOMENTARY |
MIL-G-5514 Revision G:1993
|
GLAND DESIGN, PACKINGS, HYDRAULIC GENERAL REQUIREMENTS FOR |
MIL-HDBK-400 Base Document:1985
|
CRITERIA FOR PREPARATION OF GEAR AND SPLINE ENGINEERING DRAWINGS |
MIL-STD-1345 Revision B:1981
|
TEST REQUIREMENT DOCUMENT PREPARATION OF |
MIL-STD-483 Revision A:1985
|
CONFIGURATION MANAGEMENT PRACTICES FOR SYSTEMS, EQUIPMENT, MUNITIONS, AND COMPUTER PROGRAMS |
MIL-STD-1456 Revision A:1989
|
CONTRACTOR CONFIGURATION MANAGEMENT PLANS |
MIL M 5755 : C
|
MIRROR, REARVIEW, NONMAGNETIC, GENERAL REQUIREMENTS FOR [FOR AERONAUTICAL USE] |
MIL-I-25863 Revision D:1990
|
INDICATOR, ELECTRICAL TACHOMETER 0-110 PERCENT RPM, 2-INCH SIZE, INTEGRALLY LIGHTED |
MIL-A-81852 Revision A:1986
|
ALTIMETER-ENCODER AAU-32/A |
MIL-M-4871 Revision C:1984
|
MAINTENANCE PLATFORM |
MIL-C-4952 Revision E:1988
|
CARTRIDGES, DESICCANT, DEHYDRATOR |
MIL-T-85530 Base Document:1982
|
TEST SET, TOW TARGET, A/E24T-143 |
MIL-H-7365 Revision D:1986
|
HOSE, AIR DUCT, FOR GROUND HEATERS |
MIL-B-82572 Revision A:1989
|
BOMB, GENERAL PURPOSE, MARK 84, 2000 POUND, EXPLOSIVE LOADING ASSEMBLING AND PACKING |
MIL-C-85248 Revision A:1984
|
CAMERA, STILL PICTURE, PANORAMIC, KA-99A |
MIL-STD-808 Revision A:1983
|
FINISH, MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN SUPPORT EQUIPMENT |
MIL S 25073 : 0
|
|
MIL-V-85033 Revision A:1981
|
VALVE CHARGING |
MIL-C-5584 Revision D:1988
|
CONTAINER, SHIPPING AND STORAGE, METAL REUSABLE |
SAE MA 2126 : 2015
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE (PTFE), UP TO 232 DEGREES C AND 10 500 KPA PROCUREMENT SPECIFICATION, METRIC |
MIL I 25689 : A NOTICE 1
|
INDICATOR, ELECTRICAL TACHOMETER |
MIL I 25725 : A
|
INDICATOR, TORQUE PRESSURE, MAGNESYN STYLE, SINGLE CLAMP MOUNTED, 2 IN SIZE, 50-400 PSI TYPE A-8 |
MIL-I-85889 Base Document:1988
|
IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
MIL-STD-490 Revision A:1985
|
SPECIFICATION PRACTICES |
MIL T 6349 : C NOTICE 1
|
TEST SET, SYNCHRO |
MIL-I-26689 Revision C:1981
|
INDICATOR, HORIZONTAL SITUATION, AQU-2/A |
MIL-S-6551 Revision A:1981
|
|
MIL M 7793 : F
|
METER, TIME TOTALIZING |
MIL-S-63523 Revision A:1985
|
SIMULATOR, LAUNCHING, ANTI-TANK, GUIDED MISSILE AND ROCKET, M22, PERFORMANCE SPECIFICATION |
MIL-STD-1947 Base Document:1985
|
ULTRASONIC WELDING OF ALUMINUM AND ALUMINUM ALLOY MATERIALS |
MIL-R-23761 Revision B:1975
|
Regulators, Voltage, and Control Panels Aircraft, Direct Current Generator, General Specification for |
MIL-T-26639 Revision C:1969
|
TESTER, TORQUE WRENCH |
MIL A 25088 : C
|
|
MIL-B-3402 Revision C:1984
|
BLOWER, GASOLINE-DRIVEN, AIRCRAFT VENTILATION, PORTABLE 2,900 CFM TYPE A-2 |
MIL G 8348 : H
|
GAGE, ASSEMBLIES, AIR PRESSURE, DIAL INDICATING CHUCK TYPE SELF CONTAINED |
MIL-C-5026 Revision F:1984
|
CUTOUT RELAY, ENGINE GENERATOR |
MIL R 83536 : SUPP 1
|
RELAYS, ELECTROMAGNETIC, ESTABLISHED RELIABILITY |
MIL-A-83136 Revision A:1990
|
ARRESTING HOOK INSTALLATION, RUNWAY ARRESTING SYSTEM, AIRCRAFT, EMERGENCY |
MIL-I-23252 Revision B:1981
|
INDICATOR, PRESSURE |
MIL-B-38977 Base Document:1968
|
Bomb, Practice BDU-38/B |
MIL-P-83126 Revision A:1980
|
PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
MIL-I-8671 Revision D:1994
|
INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
MIL-D-9898 Revision C:1986
|
DRAWING, TUBE BEND |
JSSG-2010-12 Base Document:1998
|
Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
MIL D 22706 : F
|
DUCT AND SCUFF COVER, PNEUMATIC, FLEXIBLE |
MIL-D-7106 Revision C:1987
|
DRIFTMETER, ELECTRICALLY DRIVEN GYRO STABILIZED |
MIL-A-48078 Revision A:1988
|
AMMUNITION, STANDARD QUALITY ASSURANCE PROVISIONS, GENERAL SPECIFICATION FOR |
MIL-V-23255 Revision B:1976
|
VALVE, PRESSURE RELIEF |
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 |
MIL-I-8500 Revision D:1980
|
INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES |
MIL-V-25023 Revision B:1967
|
VALVE, FUEL DRAIN, SELF-LOCKING |
MIL-T-8598 Revision B:1990
|
TRANSMITTER, TEMPERATURE, ELECTRICAL RESISTANCE, FLUSH-MOUNTED, FREE AIR |
MIL-A-25933 Revision B:1985
|
ALTIMETER, PRESSURIZED COMPARTMENT, INTEGRALLY LIGHTED 0-50,000 FEET, 1-7/8 INCH DIAL |
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-T-26609 Revision C:1994
|
TRANSMITTER, POSITION |
MIL-G-58103 Base Document:1979
|
GRIP ASSEMBLY, CYCLIC CONTROLLER, HELICOPTER |
MIL-T-81838 Base Document:1971
|
TANK, FUEL, AIRCRAFT, AUXILIARY EXTERNAL 300 GALLON, TYPE AERO 1D |
MIL-S-63348 Revision A:1981
|
SUBMACHINE GUN, 5.56MM, PORT FIRING, M231 |
MIL-I-7112 Revision B:1985
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, CYLINDER HEAD 0 DEGREES C TO 300 DEGREES C |
MIL-N-25161 Revision C:1969
|
NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
MIL A 002550 : C
|
AMMUNITION, GENERAL SPECIFICATION FOR |
MIL-S-3443 Revision G:1993
|
SHOTGUN, 12 GAGE, RIOT TYPE |
MIL P 7788 : F
|
PANEL, INFORMATION INTEGRALLY ILLUMINATED |
MIL-P-11268 Revision L:1983
|
PART, MATERIALS, AND PROCESSES USED IN ELECTRONIC EQUIPMENT |
MIL-T-26963 Revision D:1992
|
TESTER, PRESSURE GAGE, HYDRAULIC, PORTABLE TYPE MP-1 |
DOD-STD-2101 Base Document:1979
|
CLASSIFICATION OF CHARACTERISTICS |
MIL-C-26237 Revision C:1983
|
CRADLE, AIRCRAFT-MISSILE COMPONENTS MMU-1/E |
MIL-B-82548 Revision A:1989
|
BOMB, GENERAL PURPOSE, MARK 82, 500 POUND, EXPLOSIVE LOADING, ASSEMBLING AND PACKING |
MIL-T-7258 Revision B:1985
|
TRANSMITTER, TEMPERATURE ELECTRICAL RESISTANCE TYPE B-4 |
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-L-6723 Revision C:1987
|
LIGHT, AIRCRAFT, GENERAL SPECIFICATION FOR |
EIA CMB5 : 2014 STABILIZED
|
CONFIGURATION MANAGEMENT REQUIREMENTS FOR SUBCONTRACTORS/VENDORS |
MIL-T-85549 Base Document:1982
|
Test Program Set (TPS) - Operational Test Program Sets (OTPS) For F/A-18 Units Under Test (UUT), General Specification For |
MIL-C-5414 Revision G:1993
|
COMPUTER, AIR NAVIGATION DEAD RECKONING TYPE MB 4A AND TYPE CPU 26A/P |
MIL-HDBK-246 Revision A:1982
|
PROGRAM MANAGERS GUIDE FOR THE STANDARD ELECTRONIC MODULES PROGRAM |
MIL W 6496 : B NOTICE 1
|
WINCH, DRUM, ENGINE OF TURRET HOIST, TYPE A-1 |
MIL-M-23677 Revision A:1987
|
METER, AMPERE HOUR (NON MERCURY TYPE) |
EIA CMB 7-2 : 2014 STABILIZED
|
GUIDELINE FOR TRANSITIONING CONFIGURATION MANAGEMENT TO AN AUTOMATED ENVIRONMENT |
MIL C 25531 : D
|
COUPLING HALF, QUICK DISCONNECT, PNEUMATIC STARTER, EXTERNAL, LOW PRESSURE, DIRECT RELEASE |
MIL-DTL-26517 Revision B:2000
|
POWER SUPPLY, TRANSFORMER-RECTIFIER, AIRCRAFT GENERAL SPECIFICATION FOR |
SAE AIR 4728 : 2013
|
REFERENCES, SPACECRAFT AND SPACECRAFT SERVICING, FLUID SYSTEM COMPONENTS (ABBREVIATIONS, ACRONYMS, DEFINITIONS, APPLICABLE DOCUMENTS AND ENVIRONMENTAL CONDITIONS) |
GEIA CMB6-4:1991(S2014)
|
CONFIGURATION CONTROL |
MIL-P-85576 Revision B:1987
|
POWER SUPPLY PP-2581C/A |
MIL-A-27391 Revision B:1963
|
ALTIMETER, PRESSURE AAU-2A |