DOD-D-1000 Revision B:1977
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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DRAWINGS, ENGINEERING AND ASSOCIATED LISTS
Available format(s)
PDF
Superseded date
20-04-2005
Superseded by
Publisher
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. NOTES
Describes the requirements for engineering drawings and associated lists acquired in support of Department of Defense Materiel.
| Committee |
FSC DRPR
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| DevelopmentNote |
B NOTICE 1 - Notice of Inactivation for New Design - For New Design use MIL T 31000. (06/2000) B NOTICE 2 - Notice of Cancellation/Superseded by MIL DTL 31000. (04/2005)
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| DocumentType |
Standard
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| Pages |
44
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| 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 | Seats, Helicopter Cabin, Crashworthy, General Specification for |
| 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, 4,000 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 |
| MIL D 5480 : F | DATA, ENGINEERING AND TECHNICAL REPRODUCTION REQUIREMENTS FOR |
| MIL-STD-100 Revision G:1997 | ENGINEERING DRAWINGS |
| DOD STD 1476 : A | METRIC SYSTEM, APPLICATION IN NEW DESIGN |
| DOD 5220.22M : 95 SUP1 CHANGE 1 | INDUSTRIAL SECURITY MANUAL FOR SAFEGUARDING CLASSIFIED INFORMATION |
| MIL-M-9868 Revision E:1993 | MICROFILMING OF ENGINEERING DATA 35 MM REQUIREMENTS FOR |
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