MIL-A-85802 Base Document:1986
|
ACTUATOR, ELECTROMECHANICAL, LINEAR |
MIL C 83166 : LATEST
|
CONVERTER MULTIPLEXER, SIGNAL DATA, GENERAL SPECIFICATION FOR |
MIL-A-52679 Revision B:1983
|
ANCHOR, SURFACING MEMBRANE: 12 INCH |
MIL M 81927 : B
|
MANUAL, TECHNICAL, GENERAL STYLE AND FORMAT OF (WORK PACKAGE CONCEPT) |
MIL-C-70723 Base Document:1993
|
CARTRIDGE, CALIBER .50, M-858 BALL AND M-860 TRACER SHORT RANGE TRAINING AMMUNITION |
MIL-J-26149 Revision E:1988
|
Jack, Hydraulic, Aircraft Maintenance, General Specification for |
BS EN 61182-2-2:2012
|
Printed board assembly products. Manufacturing description data and transfer methodology Sectional requirements for implementation of printed board fabrication data description |
MIL-HDBK-59 Revision B:1994
|
COMPUTER AIDED ACQUISITION AND LOGISTIC SUPPORT (CALS) PROGRAM IMPLEMENTATION GUIDE |
MIL-A-24741 Base Document:1990
|
ASSEMBLIES, METAL ELECTRICAL BACKPLANE, ONE AND TWO LAYER, GENERAL SPECIFICATION FOR |
MIL-A-26846 Revision B:1984
|
AIR CONDITIONER, A/M32C-4, TRAILER MOUNTED, VAPOR CYCLE, ELECTRIC, MOTOR DRIVEN |
MIL-C-5809 Revision G:1987
|
CIRCUIT BREAKERS, TRIP-FREE, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL T 6396 : E
|
TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
MIL H 26385 : E
|
HOSE, OXYGEN AND PRESSURIZATION, OZONE RESISTANT |
MIL I 27197 : C
|
INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
MIL-A-5885 Revision D:1987
|
ACCELEROMETER, AIRCRAFT |
MIL-F-8839 Revision A:1988
|
FITTING, LUBRICATION, DRIVE TYPE |
MIL-F-85421 Revision B:1986
|
FITTINGS, TUBE, FLUID SYSTEMS, SEPARABLE, BEAM SEAM, 3000/4000 PSI - GENERAL SPECIFICATION FOR |
MIL-C-8605 Revision B:1990
|
CAP, PRESSURE FUEL SERVICING |
MIL-P-85833 Base Document:1989
|
PROTECTIVE ASSEMBLY, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL |
MIL-T-27305 Revision C:1987
|
TRANSFORMER AND INDUCTORS [AUDIO, POWER AND HIGH POWER PULSE] INDUCTOR, POWER TF5S04ZZ |
MIL-STD-372 Base Document:1988
|
WELDING, GAS METAL-ARC AND GAS TUNGSTEN-ARC, ALUMINUM ALLOYS, READILY WELDABLE FOR STRUCTURES, EXCLUDING ARMOR |
MIL-C-87972 Revision A:1987
|
CASTERS, RIGID AND SWIVEL, GENERAL SPECIFICATION FOR |
MIL-A-85072 Revision A:1987
|
ACTUATOR, ELECTROMECHANICAL, LINEAR |
MIL-T-83823 Base Document:1991
|
TRUCK, FIRE FIGHTING (STRUCTURAL OR BRUSH STRUCTURAL) |
MIL STD 2080 : 0
|
MAINTENANCE ENGINEERING, PLANNING AND ANALYSIS FOR AERONAUTICAL SYSTEMS, SUBSYSTEMS, EQUIPMENT AND SUPPORT EQUIPMENT |
MIL-B-385 Revision G:1985
|
BREAKERS, PAVING, PNEUMATIC-POWERED (7/8-INCH HEXAGON BY 2-3/4-INCH CHUCK AND 7/8-INCH HEXAGON BY 3-1/4-INCH CHUCK) |
MIL-STD-1943 Base Document:1985
|
WELDING REPAIR OF STEEL CASTINGS (OTHER THAN ARMOR) METAL-ARC, MANUAL |
MIL V 85855 : 0
|
VALVE, QUICK DISCONNECT, FOR THE PROTECTIVE ASSEMBLY, CHEMICAL, RADIOLOGICAL |
MIL-I-27202 Revision A:1980
|
INDICATOR, ELECTRICAL TACHOMETER, 0-110 PERCENT RPM 2-INCH SIZE, INTEGRALLY LIGHTED |
SAE AS 5944 : 1999
|
SLINGS, AIRCRAFT, GENERAL SPECIFICATION FOR |
PD IEC/PAS 61182-12:2014
|
Generic requirements for printed board assembly products manufacturing description data and transfer methodology |
IEC 61182-2:2006
|
Printed board assembly products - Manufacturing description data and transfer methodology - Part 2: Generic requirements |
EN 61182-2-2:2012
|
Printed board assembly products - Manufacturing description data and transfer methodology - Part 2-2: Sectional requirements for implementation of printed board fabrication data description |
MIL-W-5088 Revision L:1991
|
Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
MIL-A-83477 Revision A:1976
|
AIR CONDITIONER, A/M32C-18 TRAILER MOUNTED, DIESEL ENGINE DRIVEN |
MIL-C-85521 Base Document:1983
|
CONCENTRATOR, OXYGEN, GGU-7/A |
MIL V 7891 : E
|
VALVE, OXYGEN FILLER, LOW AND PRESSURE |
MIL-C-85829 Base Document:1989
|
COUPLING ASSEMBLY, HOSE, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE |
MIL-HDBK-288 Revision B:1991
|
REVIEW AND ACCEPTANCE OF ENGINEERING DRAWING PACKAGES |
MIL-STD-2097 Revision A:1989
|
ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
MIL-C-70726 Revision A:1993
|
CARTRIDGE, CALIBER .50, BLANK, XM928, PERFORMANCE SPECIFICATION FOR |
MIL-H-4607 Revision E:1987
|
HEATER, ENGINE AND SHELTER, GROUND |
MIL-A-28870 Revision A:1990
|
ASSEMBLIES, ELECTRICAL BACKPLANE, PRINTED WIRING, GENERAL SPECIFICATION FOR |
MIL-T-47500-1 Base Document:1989
|
TECHNICAL DATA PACKAGES, DRAWINGS, DESIGN |
MIL T 38804 : B
|
TIME COMPLIANCE TECHNICAL ORDERS (TCTOS) PREPARATION OF |
MIL T 38170 : F
|
TANK, MOBILE STORAGE, LIQUID OXYGEN TMU 27/M |
MIL-A-81918 Base Document:1976
|
ADAPTER, LAUNCHER, AIRCRAFT, ADU-299A/A |
MIL-M-70466 Base Document:1993
|
MACHINE GUN, 7.62mm: M60E3 |
MIL-A-26624 Revision B:1981
|
AIR CONDITIONER, A/M32C-5, TRAILER MOUNTED, VAPOR CYCLE, ELECTRIC MOTOR DRIVEN |
MIL M 81929 : B
|
MANUAL, TECHNICAL, ILLUSTRATED PARTS BREAKDOWN, (WORK PACKAGE CONCEPT),PREPARATION OF |
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-B-85598 Base Document:1988
|
BEARINGS, ELASTOMERIC GENERAL SPECIFICATION FOR |
MIL M 87158 : A
|
MANUALS, TECHNICAL, AIRCRAFT BATTLE DAMAGE ASSESSMENT AND REPAIR |
MIL STD 1836 : NOTICE 1
|
STANDARDIZATION & CONTROL PROGRAM FOR PARTS, MATERIALS & PROCESSES USED IN INTERCONTINENTAL BALLISTIC MISSILE WEAPON SYSTEMS |
MIL-R-85895 Base Document:1988
|
RACK, BOMB EJECTOR, AIRCRAFT BRU-32/A |
MIL-S-85377 Revision A:1983
|
SWITCH, STEPPING, DIRECT CURRENT AIRCRAFT DISPENSER |
MIL-HDBK-817 Base Document:1994
|
SYSTEM DEVELOPMENT RADIATION HARDNESS ASSURANCE |
MIL-S-87233 Base Document:1985
|
SUPPORT EQUIPMENT SYSTEMS (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
MIL-C-70724 Base Document:1992
|
CARTRIDGE, 5.56MM, BLANK, M200A1 PERFORMANCE SPECIFICATION FOR |
MIL-C-9082 Revision H:1986
|
CONVERTER, OXYGEN, AIRCRAFT, LIQUID TO GASEOUS, GENERAL SPECIFICATION FOR |
MIL-STD-2198 Base Document:1990
|
DESIGN REQUIREMENTS FOR METAL ELECTRICAL BACKPLANE ASSEMBLIES |
MIL-HDBK-2097 Revision A:1997
|
ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
MIL-M-85831 Base Document:1989
|
MASK, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE, NON-OXYGEN |
MIL-C-4150 Revision J:1989
|
CASE, TRANSIT AND STORAGE, WATERPROOF AND WATER-VAPORPROOF |
IPC 2581 : B
|
GENERIC REQUIREMENTS FOR PRINTED BOARD ASSEMBLY PRODUCTS MANUFACTURING DESCRIPTION DATA AND TRANSFER METHODOLOGY |
MIL-D-81992 Revision B:1994
|
DIRECTIVE, TECHNICAL, PREPARATION OF |
MIL-R-85880 Base Document:1988
|
ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
DOD-STD-1702 Base Document:1985
|
INTEGRATED LOGISTICS SUPPORT PROGRAMS FOR EQUIPMENT, SUBSYSTEMS AND SYSTEMS (METRIC) |
MIL-M-7997 Revision C:1981
|
MOTOR, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT GENERAL SPECIFICATION FOR |
MIL-C-38404 Revision E:1992
|
COUPLING, HOSE, REATTACHABLE SCREW-ON |
MIL-STD-1561 Revision B:1984
|
PROVISIONING PROCEDURES, UNIFORM DOD |
MIL-T-81259 Revision B:1991
|
TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR |
MIL-M-85522 Revision A:1991
|
MONITOR, OXYGEN CRU-91/A |
MIL V 87223 : 0
|
VALVE, PRESSURE, ANTI-G SUIT, MXU-804/A AND MXU-805/A |
MIL-HDBK-400 Base Document:1985
|
CRITERIA FOR PREPARATION OF GEAR AND SPLINE ENGINEERING DRAWINGS |
MIL-STD-1261 Revision C:1988
|
ARC WELDING PROCEDURES FOR CONSTRUCTIONAL STEELS |
MIL-S-18471 Revision G:1983
|
|
MIL-STD-1345 Revision B:1981
|
TEST REQUIREMENT DOCUMENT PREPARATION OF |
MIL-STD-275 Revision E:1984
|
PRINTED WIRING - ELECTRONIC EQUIPMENT |
MIL-STD-361-3 Base Document:1992
|
MANUALS, TECHNICAL: REQUIREMENTS FOR GRAPHICS |
MIL I 85581 : 0
|
INTERVALOMETER, ROCKET LAUNCHER, REUSABLE |
MIL A 87221 : 0
|
AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
MIL-STD-483 Revision A:1985
|
CONFIGURATION MANAGEMENT PRACTICES FOR SYSTEMS, EQUIPMENT, MUNITIONS, AND COMPUTER PROGRAMS |
MIL-I-85832 Base Document:1989
|
INTERCOM, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE SET |
MIL-H-85042 Revision A:1983
|
HOOKS, BOMB RACK, GENERAL SPECIFICATION FOR |
MIL D 83532 : A (3) SUPP 1
|
DELAY LINES, ACTIVE |
MIL BULL 103 : AC NOTICE 1
|
LIST OF STANDARD MICROCIRCUIT DRAWINGS |
MIL-C-5584 Revision D:1988
|
CONTAINER, SHIPPING AND STORAGE, METAL REUSABLE |
MIL-C-83864 Revision A:1982
|
CONTAINER, INNER, SURVIVAL KIT |
DOD-STD-863 Revision B:1979
|
WIRING DATA AND SYSTEM SCHEMATIC DIAGRAMS PREPARATION OF |
MIL-G-85468 Base Document:1981
|
GENERATOR CONTROL INDICATOR SG-118/AST-4(V) |
MIL-E-24743 Base Document:1991
|
ENCLOSURE, COMMON ELECTRONIC EQUIPMENT, GENERAL SPECIFICATION |
MIL M 63029 : C
|
MANUAL, TECHNICAL, REQUIREMENTS FOR OPERATOR S MANUALS AND CHECKLISTS FOR AIRCRAFT |
IPC 2588 : 2007
|
SECTIONAL REQUIREMENTS FOR IMPLEMENTATION OF PART LIST PRODUCT DATA DESCRIPTION |
SAE AS 7997:1999
|
MOTORS, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT - GENERAL SPECIFICATION FOR |
IEC PAS 61182-12:2014
|
Generic requirements for printed board assembly products manufacturing description data and transfer methodology |
MIL-C-70725 Revision A:1993
|
CARTRIDGE, 5.56MM, M862 SHORT RANGE TRAINING AMMUNITION PERFORMANCE SPECIFICATION FOR |
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-D-38386 Revision E:1989
|
DUCT ASSEMBLY, GROUND, CONDITIONED AIR, INSULATED, FLEXIBLE |
MIL-HDBK-339 Base Document:1984
|
CUSTOM LARGE SCALE INTEGRATED CIRCUIT DEVELOPMENT & ACQUISITION FOR SPACE VEHICLES |
IPC 2583 : 2007
|
SECTIONAL REQUIREMENTS FOR IMPLEMENTATION OF DESIGN CHARACTERISTICS FOR MANUFACTURING DATA DESCRIPTION |
MIL-STD-361-9 Base Document:1992
|
MANUALS, TECHNICAL: TROUBLESHOOTING PROCEDURES |
MIL-A-25915 Revision A:1980
|
ACCELEROMETER, AIRCRAFT, PILOTS WARNING, TYPE MA-2 |
MIL-S-5944 Revision C:1990
|
SLING, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-B-87167 Base Document:1985
|
BELT, AIRCRAFT SAFETY, HBU-12/A |
MIL-F-13926 Revision B:1984
|
FIRE CONTROL MATERIAL MANUFACTURE AND INSPECTION, GENERAL SPECIFICATION FOR |
MIL M 63045 : A
|
MANUAL, TECHNICAL, PREPARATION OF DEPOT MANUALS FOR DEPOT TEST, MEASUREMENT AND DIAGNOSTIC EQUIPMENT |
MIL-F-27656 Revision C:1987
|
FILTER UNIT, FLUID, PRESSURE MXU-4O8/M, ABSOLUTE 5 MICRON, HYDRAULIC |
MIL-C-27718 Revision D:1984
|
CRANE, HYDRAULIC, TRUCK MOUNTED, A/S32A-16 16,5OO POUND CRANE CAPACITY, 6X4, DED |
MIL-A-83136 Revision A:1990
|
ARRESTING HOOK INSTALLATION, RUNWAY ARRESTING SYSTEM, AIRCRAFT, EMERGENCY |
SAE AS 85352 : 2011
|
INFLATOR ASSEMBLY AND GAGE ELEMENTS, PNEUMATIC PRESSURE, REMOTE CONTROL, DIRECT READING |
MIL-S-85508 Base Document:1981
|
Spectacles, Aviator\'s, Neodymium Laser Protective, EDU-1/P (with case) |
MIL-T-47500 Base Document:1989
|
TECHNICAL DATA PACKAGE, GENERAL SPECIFICATION FOR |
MIL-STD-2118 Base Document:1984
|
FLEXIBLE AND RIGID FLEX PRINTED WIRING FOR ELECTRONIC EQUIPMENT DESIGN REQUIREMENTS FOR |
MIL M 63002 : F
|
MANUAL, TECHNICAL, REQUIREMENTS FOR PREPARATION OF MODIFICATION WORK ORDERS |
MIL-STD-805 Revision B:1987
|
TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR |
MIL I 26359 : B
|
INDICATOR, ATTITUDE, REMOTE ARU-4/A |
MIL-P-83126 Revision A:1980
|
PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
MIL-D-9898 Revision C:1986
|
DRAWING, TUBE BEND |
MIL-STD-1174 Revision B:1979
|
ASSOCIATED LISTS FOR ARRADCOM ENGINEERING DRAWINGS |
MIL E 21981B:1986
|
ELECTRONICS EQUIPMENT, NOMENCLATURE, SERIAL NUMBERS AND IDENTIFICATION PLATES: REQUIREMENTS FOR |
MIL V 9050 : E (1)
|
VALVE, OXYGEN, PRESSURE RELIEF, AIRCRAFT |
MIL-HDBK-263 Revision B:1994
|
ELECTROSTATIC DISCHARGE CONTROL HANDBOOK FOR PROTECTION OF ELECTRICAL & ELECTRONIC PARTS, ASSEMBLIES & EQUIPMENT |
MIL C 85052 : A
|
CLAMP LOOP, CUSHION, GENERAL SPECIFICATION FOR |
MIL-C-11218 Revision E:1988
|
CONVEYORS, ROLLER AND WHEEL, GRAVITY AND CONVEYER SUPPORTS |
MIL-STD-2078 Base Document:1981
|
REQUIREMENT FOR PREPARATION OF SUPPORT EQUIPMENT DEPOT LEVEL REWORK STANDARDS |
MIL V 87255 : 0
|
VALVE, PRESSURE, ANTI-G SUIT, HIGH FLOW |
MIL-P-85573 Base Document:1983
|
POWER UNIT AIRCRAFT AUXILIARY, GAS TURBINE, GENERAL SPECIFICATION FOR |
SAE MA 2100 : 2015
|
HOSE ASSEMBLIES, METAL MEDIUM PRESSURE, HIGH TEMPERATURE, METRIC |
IEC 61182-2-2:2012
|
Printed board assembly products - Manufacturing description data and transfer methodology - Part 2-2: Sectional requirements for implementation of printed board fabrication data description |
BS IEC 61182-2:2006
|
Printed board assembly products. Manufacturing description data and transfer methodology Generic requirements |
MIL-D-19326 Revision H:1990
|
DESIGN AND INSTALLATION OF LIQUID OXYGEN SYSTEMS IN AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL A 5503 : E
|
ACTUATOR, AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
MIL-B-81934 Revision B:1991
|
BEARING, SLEEVE, PLAIN AND FLANGED, SELF LUBRICATING |
MIL M 63003 : A
|
MANUALS, TECHNICAL: BATTLEFIELD DAMAGE ASSESSMENT AND REPAIR, PREPARATION OF |
MIL-S-29594 Base Document:1992
|
SPECTACLES, AVIATOR'S, SEVEN WAVELENGTH LASER EYE PROTECTIVE |
MIL-A-26360 Revision B:1982
|
AMPLIFIER, ELECTRONIC CONTROL ASU-3/A |
MIL-A-27330 Revision B:1987
|
ACCELEROMETER, ELECTRICAL, LINEAR TRU-3/A |
MIL-F-85720 Base Document:1985
|
FITTING, TUBE, FLUID SYSTEMS, SEPARABLE, HIGH PRESSURE, DYNAMIC BEAM, SEAL, GENERAL SPECIFICATION FOR |
MIL-STD-2119 Revision A:1990
|
DESIGN REQUIREMENTS FOR PRINTED WIRING ELECTRICAL BACKPLANE ASSEMBLIES |
MIL-S-3443 Revision G:1993
|
SHOTGUN, 12 GAGE, RIOT TYPE |
MIL-P-11268 Revision L:1983
|
PART, MATERIALS, AND PROCESSES USED IN ELECTRONIC EQUIPMENT |
SAE AS 1960 : 2013
|
COUPLING ASSEMBLY, V-BAND, SHEET METAL FLANGE, PNEUMATIC TUBE |
SAE MA 2007A : 2015
|
HOSE ASSEMBLY, TETRAFLUOROETHYLENE, LIGHTWEIGHT, 204 DEGREE C, 21000 KPA HYDRAULIC, METRIC |
MIL-I-25941 Revision D:1986
|
INDICATOR, TURN AND SLIP, 2-INCH SIZE, INTEGRALLY LIGHTED |
MIL-C-87970 Base Document:1982
|
CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
MIL-G-25591 Revision E:1981
|
GYROSCOPE, RATE, SWITCHING, TYPE MC-1 |
MIL T 25435 : B
|
TRANSMITTER, PRESSURE, AIRCRAFT, VARIABLE RELUCTANCE TYPE, GENERAL SPECIFICATION FOR |
MIL-L-6273 Revision D:1983
|
LIGHT, NAVIGATIONAL, BEACON, OBSTACLE OR CODE, TYPE G 1 |
MIL D 28000 : A
|
DIGITAL REPRESENTATION FOR COMMUNICATION OF PRODUCT DATA: IGES APPLICATION SUBSETS |
EIA CMB5 : 2014 STABILIZED
|
CONFIGURATION MANAGEMENT REQUIREMENTS FOR SUBCONTRACTORS/VENDORS |
MIL-T-81490 Revision A:1991
|
TRANSMISSION LINES, TRANSVERSE ELECTROMAGNETIC MODE |
MIL-I-25437 Revision B:1984
|
INDICATORS, AIRCRAFT, PRESSURE, VOLTAGE RATIO TYPE, GENERAL SPECIFICATION FOR |
MIL-B-83183 Revision B:1987
|
BARRIER, AIRCRAFT ARRESTING |
MIL C 25666 : E (1)
|
CONVERTER, LIQUID OXYGEN, CAPACITANCE TYPE GAGING, GENERAL SPECIFICATION FOR |
MIL-V-85830 Base Document:1989
|
VENTILATOR, TACTICAL, HELICOPTER AIRCREWMEN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE |
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 |
EIA CMB 7-2 : 2014 STABILIZED
|
GUIDELINE FOR TRANSITIONING CONFIGURATION MANAGEMENT TO AN AUTOMATED ENVIRONMENT |
MIL L 7830 : D
|
LIGHT ASSEMBLY, MARKER, AIRCRAFT OBSTRUCTION |
I.S. EN 61182-2-2:2012
|
PRINTED BOARD ASSEMBLY PRODUCTS - MANUFACTURING DESCRIPTION DATA AND TRANSFER METHODOLOGY - PART 2-2: SECTIONAL REQUIREMENTS FOR IMPLEMENTATION OF PRINTED BOARD FABRICATION DATA DESCRIPTION (IEC 61182-2-2:2012 (EQV)) |
MIL-D-23140 Revision D:1992
|
DRAWINGS, INSTALLATION CONTROL, FOR SHIPBOARD ELECTRONIC EQUIPMENT |
MIL-V-29591 Base Document:1992
|
VISOR ASSEMBLY, AVIATOR'S SEVEN WAVELENGTH LASER PROTECTIVE, GENERAL SPECIFICATION FOR |
GEIA CMB6-4:1991(S2014)
|
CONFIGURATION CONTROL |
IPC 2582 : 2007
|
SECTIONAL REQUIREMENTS FOR IMPLEMENTATION OF ADMINISTRATIVE METHODS FOR MANUFACTURING DATA DESCRIPTION |
MIL-P-85576 Revision B:1987
|
POWER SUPPLY PP-2581C/A |
SAE AS 4388 : 2013
|
HOSE ASSEMBLY PTFE HEAVY DUTY, -65 TO 400 DEGREES F (-55 TO 204 DEGREES C) 8000 PSI (56000 KPA) HYDRAULIC AND PNEUMATIC |
SAE MA 2079 : 2015
|
HOSE ASSEMBLY, CONVOLUTED POLYTETRAFLUOROETHYLENE, HIGH TEMPERATURE, MEDIUM PRESSURE, AIRCRAFT, METRIC |