MIL-STD-970 Base Document:1987
Withdrawn
Withdrawn
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STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF
Available format(s)
PDF
Withdrawn date
10-18-1994
Publisher
Gives preferred order for selection of standards and specifications used in design, acquisition, construction and support of material for DOD in compliance with OMB Circular A-119. Coverage includes referenced documents, definitions, technical suitability, and economic considerations. Also gives detailed notes.
| Committee |
AREA GDRQ
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| DocumentType |
Standard
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| Pages |
14
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Withdrawn
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| Supersedes |
| MIL-M-87113 Revision A:1993 | MASK, OXYGEN, MBU-10/P |
| MIL-B-44421 Base Document:1991 | Body Armor, Small Arms Protective, Aircrew, Survival (No S/S Document) |
| MIL-J-26149 Revision E:1988 | Jack, Hydraulic, Aircraft Maintenance, General Specification for |
| MIL STD 680 : B NOTICE 1 | CONTRACTOR STANDARDIZATION PROGRAM REQUIREMENTS |
| MIL F 27272 : B | FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL-I-7721 Revision D:1992 | INDICATOR, VERTICAL SPEED, 3-INCH |
| MIL-I-38121 Revision C:1989 | INDICATOR, PRESSURE, EGU-9/A |
| MIL-R-8236 Revision F:1995 | REEL, SHOULDER HARNESS, INERTIA LOCK |
| MIL I 27197 : C | INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
| MIL S 5765 : F | STRAND, WIRE ROPE, ARMORED STEEL |
| MIL H 26626 : D | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, OXYGEN |
| MIL-A-5885 Revision D:1987 | ACCELEROMETER, AIRCRAFT |
| MIL-I-85071 Revision A:1992 | INVERTERS, AIRCRAFT, DC TO AC, GENERAL SPECIFICATION FOR |
| MIL-STD-7080 Base Document:1994 | SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
| MIL F 5373 : D | FUSEHOLDER, BLOCK TYPE, AIRCRAFT |
| MIL-I-82787 Base Document:1990 | IGNITER ASSEMBLY, ROCKET MOTOR MK 104 |
| MIL-C-44417 Base Document:1991 | CARRIER, BODY ARMOUR, SMALL ARMS PROTECTIVE, AIRCREW, SURVIVAL |
| MIL-T-27305 Revision C:1987 | Transmitter, Rate of Flow |
| MIL BULL 147 : E | SPECIFICATIONS AND STANDARDS OF NON-GOVERNMENT ORGANIZATIONS RELEASED FOR FLIGHT VEHICLE DESIGN AND CONSTRUCTION |
| MIL-T-83823 Base Document:1991 | TRUCK, FIRE FIGHTING (STRUCTURAL OR BRUSH STRUCTURAL) |
| MIL-STD-1662 Revision C:1992 | ORDNANCE ALTERATION (ORDALT) INSTRUCTIONS, PREPARATION OF |
| SAE AS5944 | Slings, Aircraft, General Specification For |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-C-4751 Revision D:1983 | CASTERS, RIGID AND SWIVEL, PRECISION HEAVY DUTY, AND SHOCK ABSORBING |
| MIL-HDBK-1587 Base Document:1996 | MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM |
| MIL-T-83303 Revision C:1988 | TRUCK, FIREFIGHTING, AIRFIELD RAMP, 4X4, A/S32P-20, TWIN AGENT, SKID MOUNTED |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL F 83798 : B | FITTING, RUBBER HOSE, LIGHTWEIGHT MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| MIL C 38159 : B | CONNECTOR, ELECTRIC, RAMP POWER, 480/277 VOLTS, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-C-7580 Revision C:1989 | COUPLING, FIRE HOSE, REUSABLE HIGH PRESSURE |
| MIL T 28800 : E | TEST EQUIPMENT FOR USE WITH ELECTRICAL AND ELECTRONIC EQUIPMENT GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-T-83965 Revision B:1990 | TRUCK, FIRE FIGHTING, A/S32P-10, FORCIBLE ENTRY |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL V 5523 : D | VALVE, RELIEF, HYDRAULIC PRESSURE |
| MIL-D-23615 Revision C:1993 | DESIGN AND EVALUATION OF CARTRIDGE ACTUATED DEVICES |
| MIL P 23928 : D | PANEL, ELECTRICAL, POWER DISTRIBUTION AND MANUAL TRANSFER, CIRCUIT BREAKER TYPE |
| SAE AS53731A | Fuse Holder, Block Type, Aircraft |
| MIL-STD-973 Base Document:1992 | CONFIGURATION MANAGEMENT |
| MIL-A-47312 Revision A:1992 | ACTUATOR, HYDRAULIC |
| MIL-A-27195 Revision A:1989 | ACCELEROMETER, AIRCRAFT, MECHANICAL ABU-6/A |
| MIL-T-85230 Revision A:1992 | TARGET, TOW, AERIAL, TDU-34/A |
| MIL V 6164 : E | VALVE, AIRCRAFT, AIR HIGH PRESSURE |
| MIL-R-81553 Revision B:1992 | REGULATOR, CHEST MOUNTED, OXYGEN, POSITIVE PRESSURE, CRU-79/P |
| DOD 4120.3M : 1993 | DEFENSE STANDARDIZATION PROGRAM (DSP) POLICIES AND PROCEDURES OFFICE OF THE ASSISTANT SECRETARY OF DEFENSE PRODUCTION AND LOGISTICS |
| MIL-A-27471 Revision C:1993 | ADAPTER, PRESSURE-REDUCER, IN-LINE CRU-43A/A |
| MIL-C-83821 Base Document:1990 | CRANE, WHEEL MOUNTED, CRASH, ROUGH TERRAIN, HYDRAULIC FULL REVOLVING, 4X4, DED, FIGHTER TYPE AIRCRAFT |
| MIL-I-82826 Base Document:1985 | IGNITER ASSEMBLY |
| MIL-C-21049 Revision F:1990 | Coupling Assemblies, Quick Disconnect, Aircraft Liquid Oxygen Systems |
| MIL-HDBK-2097 Revision A:1997 | ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
| MIL C 38271 : B | CONNECTOR, OXYGEN MASK TO REGULATOR CRU-60/P |
| MIL-STD-2131 Revision A:1991 | LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| MIL-C-4150 Revision J:1989 | CASE, TRANSIT AND STORAGE, WATERPROOF AND WATER-VAPORPROOF |
| MIL-F-7179 Revision G:1993 | FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM |
| SAE AS55151A | Pump, Hydraulic, Ram, Hand Driven |
| SAE ARP1616B | Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel and Oil Systems |
| SAE AS8700 | Installation and Test of Electronic Equipment in Aircraft, General Specification for |
| MIL-F-3541 Revision C:1989 | FITTING, LUBRICATION, GENERAL SPECIFICATION FOR |
| MIL E 917 : E | ELECTRIC POWER EQUIPMENT, BASIC REQUIREMENTS (NAVAL SHIPBOARD USE) |
| MIL-C-38404 Revision E:1992 | COUPLING, HOSE, REATTACHABLE SCREW-ON |
| MIL-M-27274 Revision E:1993 | MASK, OXYGEN MBU-5/P |
| MIL T 5350 : E | TRANSMITTER, SYNCHRO OPERATED, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-M-85522 Revision A:1991 | MONITOR, OXYGEN CRU-91/A |
| MIL-I-27304 Revision E:1977 | Indicator, Rate of Flow |
| MIL-B-9972 Revision B:1994 | BRAZING, NICKEL, ALLOY, GENERAL SPECIFICATION FOR |
| MIL C 9401 : B | CANOPY, PARACHUTE, RING SLOT, GENERAL SPECIFICATION FOR CONSTRUCTION OF 0ASG] |
| MIL-STD-965 Revision B:1993 | PARTS CONTROL PROGRAM |
| MIL-I-25863 Revision D:1990 | INDICATOR, ELECTRICAL TACHOMETER 0-110 PERCENT RPM, 2-INCH SIZE, INTEGRALLY LIGHTED |
| MIL-A-47309 Revision A:1991 | AMPLIFIER, PNEUMATIC |
| MIL-A-24780 Base Document:1992 | ACTUATING ASSEMBLY, SINGLE LINEAR MOTION, FOR THE REMOTE ACTUATION OF QUICK ACTING VALVES, GENERAL SPECIFICATION FOR |
| MIL B 8111 : F | BOX SET, WOOD, NESTED, ORGANIZATIONAL EQUIPMENT TYPE MG AND 1A |
| MIL I 6839 : C | INDICATOR, POSITION, LANDING GEAR |
| MIL-C-83864 Revision A:1982 | CONTAINER, INNER, SURVIVAL KIT |
| MIL-I-8700 Revision A:1970 | INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL I 25689 : A NOTICE 1 | INDICATOR, ELECTRICAL TACHOMETER |
| MIL-I-85889 Base Document:1988 | IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL C 83867 : B | CONNECTOR, OXYGEN MASK HOSE NON-EJECTION TYPE |
| MIL S 9479 : C | |
| MIL-H-21722 Revision B:1992 | HOOK, THRUST STABILIZING, JATO-45OO POUNDS NOMINAL THRUST |
| MIL-H-21660 Revision A:1992 | HOOK, THRUST, JATO - 1000 POUNDS NOMINAL THRUST |
| MIL-V-27296 Revision C:1993 | VALVE, OXYGEN MASK, COMBINATION INHALATION AND EXHALATION |
| MIL-A-18717 Revision C:1993 | ARRESTING HOOK INSTALLATIONS, AIRCRAFT |
| MIL-S-5944 Revision C:1990 | SLING, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL H 26499 : C | HOSE ASSEMBLY, METAL, FLEXIBLE, BREATHING OXYGEN |
| MIL-STD-1399-502 Revision A:1995 | INTERFACE STANDARD FOR SHIPBOARD SYSTEMS, ELECTRONIC SYSTEMS PARAMETERS, SECTION 502 ELECTRONIC SYSTEMS PARAMETERS |
| MIL-STD-1476 Revision C:1993 | METRIC SYSTEM APPLICATION IN NEW DESIGN |
| MIL H 83797 : 0 | HOSE, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
| MIL-W-5013 Revision L:1991 | WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL S 12285 : D | SWITCH, THERMOSTATIC |
| MIL L 7961 : C | LIGHT, INDICATOR, PRESS TO TEST |
| MIL-I-38391 Base Document:1965 | INDICATOR, ELECTRICAL TACHOMETER, ERU-12/A 0-350 RPM (ROTOR), 0-7000 RPM (ENGINE) |
| MIL A 83419 : C | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
| MIL V 47306 : B | VALVE, STOP LIFT CHECK |
| MIL V 87255 : 0 | VALVE, PRESSURE, ANTI-G SUIT, HIGH FLOW |
| MIL-A-81403 Base Document:1967 | ALTIMETER-ENCODER, AAU-21/A |
| 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-T-8598 Revision B:1990 | Transmitter, Temperature, Electrical Resistance, Flush-Mounted, Free Air |
| MIL D 26392 : C | DUMMY CONVERTERS, LIQUID OXYGEN INDICATOR SYSTEM 10 LITER CRU-23/A AND 25 LITER CRU-24/A |
| 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-I-83245 Revision A:1994 | INDICATOR SET, OIL PRESSURE A/A24J-17 |
| MIL-R-25410 Revision G:1991 | REGULATORS, OXYGEN, DILUTER-DEMAND AUTOMATIC-PRESSURE BREATHING |
| MIL-D-18300 Revision H:1993 | DESIGN EXAMINATIONS, ENGINEERING AVIONIC SYSTEMS/EQUIPMENT GENERAL REQUIREMENTS FOR |
| MIL-T-26963 Revision D:1992 | TESTER, PRESSURE GAGE, HYDRAULIC, PORTABLE TYPE MP-1 |
| MIL L 25370 : E | LIFE PRESERVER INFLATING ASSEMBLY, MA-1 |
| MIL-B-55252 Revision B:1992 | BATTERIES, NON-RECHARGEABLE, MAGNESIUM |
| MIL-I-27848 Revision B:1994 | INDICATOR, HORIZONTAL SITUATION AQU-4/A |
| MIL D 83753 : NOTICE 2 | DISPENSER, BOMB, TYPE SUU-21/A |
| MIL-C-5414 Revision G:1993 | COMPUTER, AIR NAVIGATION DEAD RECKONING TYPE MB 4A AND TYPE CPU 26A/P |
| MIL-R-5049 Revision D:1989 | RING, WIPER, PISTON ROD |
| MIL C 7115 : F | CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-I-26299 Revision G:1990 | INDICATORS, RATE OF FLOW, 0-5,000 PPH, INTEGRALLY LIGHTED |
| MIL-P-38268 Revision C:1988 | AURAL PROTECTORS, SOUND |
| MIL-V-47311 Base Document:1989 | VALVE, PNEUMATIC EXHAUST |
| MIL-STD-490 Revision A:1985 | SPECIFICATION PRACTICES |
| MIL-STD-962 Revision D:2003 | DEFENSE STANDARDS FORMAT AND CONTENT |
| MIL-STD-961 Revision E:2003 | DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT |
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