MIL-STD-100 Revision G:1997
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
ENGINEERING DRAWINGS
Available format(s)
PDF
Superseded date
14-12-2001
Publisher
1 Scope
2 Applicable documents
3 Definitions
4 General requirements
5 Detailed requirements
6 Notes
Chapter 100 - Preparation of engineering drawings
Chapter 200 - Types of engineering drawings
Chapter 300 - Drawing titles
Chapter 400 - Numbering, coding and identification
Chapter 500 - Markings on engineering drawings
Appendix A - Security classification markings and notations
Appendix B - Qualification provisions for source control drawings
Establishes essential requirements and reference documents applicable to the preparation and revision of engineering drawings and associated lists for or by Departments and Agencies of the Department of Defense. Coverage includes applicable documents, definitions, preparation of engineering drawings, drawing titles, markings on engineering drawings, and revision of engineering drawings.
| Committee |
AREA DRPR
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| DevelopmentNote |
G Notice 1 - Notice of Cancellation/Superseded by ASME Y 14.100, ASME Y 14.24, ASME Y 14.35M & ASME Y 14.34M. (01/2002) Supersedes MIL D 1000/2 & MIL STD 1174 (07/2004)
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| DocumentType |
Standard
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| Pages |
86
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| 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 | TEST SET, AIRFIELD LIGHTING SYSTEMS, TYPE MM-1 |
| MIL-B-3990 Revision D:1980 | BEARINGS, ROLLER, NEEDLE, AIRFRAME, ANTIFRICTION, INCH |
| MIL-DTL-29469 Revision A:1998 | CHAPLAIN'S KIT - COMBAT |
| MIL R 5149 : B | ROCKET ENGINE, LIQUID PROPELLANT GENERAL SPECIFICATION FOR |
| MIL-I-81049 Revision A:1972 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
| MIL I 27190 : B | INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI |
| MIL-D-38134 Revision A:1971 | DETECTOR, MAGNETIC AZIMUTH DSU-4/A, HIGH TEMPERATURE |
| MIL-T-5955 Revision C:1970 | TRANSMISSION SYSTEM, VTOL-STOL GENERAL REQUIREMENTS FOR |
| MIL-DTL-85855 Revision A:1999 | 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) | INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
| MIL-P-38136 Revision A:1969 | PITOT STATIC TUBE COMPENSATED TRU 62/A |
| MIL-DTL-25666 Revision F:1995 | CONVERTER, LIQUID OXYGEN, CAPACITANCE TYPE GAGING, GENERAL SPECIFICATION FOR |
| MIL-P-8945 Revision A:1967 | PANEL, RELAY, PILOT, ENCLOSED, AIRPORT LIGHTING |
| MIL-STD-834 Revision C:1974 | PACKAGING DATA FORMS, INSTRUCTIONS FOR PREPARATION AND USE OF |
| SAE AS 5778 : 1997 | COVERS, AIRCRAFT COMPONENTS, GENERAL REQUIREMENTS FOR |
| MIL-PRF-63045 Revision B:1997 | 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 Revision B:1971 | AIR CONDITIONER A/M32C-10A AIR CYCLE FOR AIRCRAFT GROUND SUPPORT |
| SAE AS 38404 : 2013 | COUPLINGS, HOSE, REATTACHABLE SCREW-ON |
| SAE MA 4623 : 2015 | Hose Assembly, Polytetrafluoroethylene, Para Aramid Reinforced Heavy-Duty, 21 000 kPa, 135 °C, Aircraft Hydraulic Systems, Metric |
| MIL-STD-2118 Base Document:1984 | FLEXIBLE AND RIGID FLEX PRINTED WIRING FOR ELECTRONIC EQUIPMENT DESIGN REQUIREMENTS FOR |
| IPC D 275 : 91 AMD 1 96 | DESIGN STANDARD FOR RIGID PRINTED BOARDS AND RIGID PRINTED BOARD ASSEMBLIES |
| IPC T 50 : M | TERMS AND DEFINITIONS FOR INTERCONNECTING AND PACKAGING ELECTRONIC CIRCUITS |
| MIL-STD-280 Revision A:1969 | DEFINITIONS OF ITEM LEVELS, ITEM EXCHANGEABILITY, MODELS, AND RELATED TERMS |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| L-P-519 Revision C:1977 | PLASTIC SHEET: TRACING, GLAZED AND MATTE FINISH |
| MIL D 5480 : F | DATA, ENGINEERING AND TECHNICAL REPRODUCTION REQUIREMENTS FOR |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| A-A-2946 Base Document:1995 | PAPER, TRACING |
| MIL-STD-883 Revision K:2016 | TEST METHOD STANDARD - MICROCIRCUITS |
| MIL-STD-1306 Revision A:1972 | FLUERICS TERMINOLOGY AND SYMBOLS |
| MIL-STD-1686 Revision C:1995 | ELECTROSTATIC DISCHARGE CONTROL PROGRAM FOR PROTECTION OF ELECTRICAL AND ELECTRONIC PARTS, ASSEMBLIES AND EQUIPMENT (EXCLUDING ELECTRICALLY INITIATED EXPLOSIVE DEVICES) |
| MIL-STD-196 Revision F:2013 | JOINT ELECTRONICS TYPE DESIGNATION AUTOMATED SYSTEM |
| MIL-PRF-28001 Revision C:1997 | MARKUP REQUIREMENTS AND GENERIC STYLE SPECIFICATION EXCHANGE OF TEXT AND ITS PRESENTATION |
| MIL-HDBK-2164 Revision A:1996 | ENVIRONMENTAL STRESS SCREENING PROCESS FOR ELECTRONIC EQUIPMENT |
| MIL-STD-1661 Base Document:1978 | MARK AND MOD NOMENCLATURE SYSTEM |
| MIL-STD-1840 Revision C:1997 | AUTOMATED INTERCHANGE OF TECHNICAL INFORMATION |
| MIL-STD-1464 Revision A:1987 | Army Nomenclature System |
| MIL-PRF-28002 Revision C:1997 | RASTER GRAPHICS REPRESENTATION IN BINARY FORMAT, REQUIREMENTS FOR |
| MIL-STD-1388-1 Revision A:1983 | LOGISTIC SUPPORT ANALYSIS |
| MIL-STD-973 Base Document:1992 | CONFIGURATION MANAGEMENT |
| IPC FC 250 : A1986 | SPECIFICATION FOR SINGLE AND DOUBLE-SIDED FLEXIBLE PRINTED WIRING |
| MIL-STD-1812 Base Document:1997 | TYPE DESIGNATION, ASSIGNMENT AND METHOD FOR OBTAINING |
| MIL-HDBK-263 Revision B:1994 | ELECTROSTATIC DISCHARGE CONTROL HANDBOOK FOR PROTECTION OF ELECTRICAL & ELECTRONIC PARTS, ASSEMBLIES & EQUIPMENT |
| MIL-STD-882 Revision E:2012 | System Safety |
| MIL-DTL-31000 Revision C:2004 | TECHNICAL DATA PACKAGES |
| MIL-HDBK-780 Revision D:2004 | STANDARD MICROCIRCUIT DRAWINGS |
| MIL-STD-962 Revision D:2003 | DEFENSE STANDARDS FORMAT AND CONTENT |
| MIL-STD-1285 Revision D:2004 | MARKING OF ELECTRICAL AND ELECTRONIC PARTS |
| DODISS : 1999 | DEPARTMENT OF DEFENSE INDEX OF STANDARDS AND SPECIFICATIONS |
| MIL-PRF-28000 Revision B:1999 | DIGITAL REPRESENTATION FOR COMMUNICATION OF PRODUCT DATA: IGES APPLICATION SUBSETS AND IGES APPLICATION PROTOCOLS |
| MIL-STD-25 Revision B:1984 | SHIP STRUCTURAL SYMBOLS FOR USE ON SHIP DRAWINGS |
| MIL-STD-961 Revision E:2003 | DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT |
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