MIL-STD-970 Base Document:1987
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STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF (NO S/S DOCUMENT)
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Published date
10-01-1987
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Withdrawn date
10-18-1994
US$20.00
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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.
| DocumentType |
Standard
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| Pages |
14
|
| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Withdrawn
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| Supersedes |
This standard sets forth the order of preference for the selection of standards and specifications used in the design, acquisition, construction and support of material for the Department of Defense in compliance with the Office of Management and Budget (OME) Circular A-119 on using commercial practices and non-Government standards.
| 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-9A (No S/S Document) |
| 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 (No S/S Document) |
| MIL-I-85071 Revision A:1992 | Inverters, Aircraft, DC to AC, General Specification for (S/S by MIL-PRF-7032) |
| MIL-STD-7080 Base Document:1994 | Selection and 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 (No S/S Document) |
| MIL-C-44417 Base Document:1991 | Carrier, Body Armor, Small Arms Protective, Aircrew, Survival (No S/S Document) |
| 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, 1,250 GPM, 4 X 2 OR 4 X 4 CHASSIS) (NO S/S DOCUMENT) |
| 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 (S/S by NASM4751) |
| MIL-HDBK-1587 Base Document:1996 | Materials and Process Requirements for Air Force Weapons Systems (S/S by MIL-STD-1587) |
| MIL-T-83303 Revision C:1988 | TRUCK, FIREFIGHTING, AIRFIELD RAMP, 4X4, A/S32P-20, TWIN AGENT, SKID MOUNTED (NO S/S DOCUMENT) |
| 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 (No S/S Document) |
| 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-RESCUE, A/S32P-10 FORCIBLE ENTRY (NO S/S DOCUMENT) |
| 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 (S/S by EIA649) |
| MIL-A-47312 Revision A:1992 | Actuator, Hydraulic (No S/S Document) |
| MIL-A-27195 Revision A:1989 | Accelerometer, Aircraft, Mechanical ABU-6/A |
| MIL-T-85230 Revision A:1992 | Target, Tow, Aerial, Tdu-34A/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 DAPTER, CRU-43/A (No S/S Document) |
| 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 (No S/S Document) |
| 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 | Cases, Transit and Storage, Waterproof and Water-Vaporproof (No S/S Document) |
| MIL-F-7179 Revision G:1993 | Finishes, Coatings, and Sealants for the Protection of Aerospace Weapons Systems (S/S by MIL-STD-7179) |
| 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 | Fittings, Lubrication, General Specification for (S/S by SAE-AS35411) |
| MIL E 917 : E | ELECTRIC POWER EQUIPMENT, BASIC REQUIREMENTS (NAVAL SHIPBOARD USE) |
| MIL-C-38404 Revision E:1992 | Couplings, Hose, Reattachable Screw-on (S/S by SAE-AS38404) |
| MIL-M-27274 Revision E:1993 | Mask, Oxygen MBU-5/P (No S/S Document) |
| 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 (S/S by AWS-C3.6) |
| MIL C 9401 : B | CANOPY, PARACHUTE, RING SLOT, GENERAL SPECIFICATION FOR CONSTRUCTION OF 0ASG] |
| MIL-STD-965 Revision B:1993 | PARTS CONTROL PROGRAM (S/S BY MIL-HDBK-965) |
| 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 (S/S by SAE-ARP763) |
| 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 (No S/S Document) |
| MIL-I-8700 Revision A:1970 | Installation and Test of Electronic Equipment in Aircraft, General Specification for (S/S by SAE-AS8700) |
| 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 | Hooks, Thrust and Stabilizing, JATO 4500 Pounds Nominal Thrust |
| MIL-H-21660 Revision A:1992 | Hook, Thrust, JATO 1000 Pounds Nominal Thrust (No S/S Document) |
| MIL-V-27296 Revision C:1993 | Valve, Oxygen Mask, Combination Inhalation and Exhalation |
| MIL-A-18717 Revision C:1993 | Arresting Hook Installation, Aircraft (S/S by MIL STD-18717) |
| MIL-S-5944 Revision C:1990 | SLINGS, AIRCRAFT, GENERAL SPECIFICATION FOR (S/S BY SAE-AS5944) |
| MIL H 26499 : C | HOSE ASSEMBLY, METAL, FLEXIBLE, BREATHING OXYGEN |
| MIL-STD-1399-502 Revision A:1995 | Interface Standard for Shipboard Systems Section 502 Electronic Systems Parameters |
| MIL-STD-1476 Revision C:1993 | METRIC SYSTEM APPLICATION IN NEW DESIGN (NO S/S DOCUMENT) |
| 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) (No S/S Document) |
| 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 (No S/S Document) |
| 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 (No S/S Document) |
| MIL-A-83212 Revision A:1976 | Altimeter, Pressure AAU-27/A (No S/S Document) |
| MIL-I-83245 Revision A:1994 | Indicator Set, Oil Pressure A/A24J-17 (No S/S Document) |
| 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 (No S/S Document) |
| MIL L 25370 : E | LIFE PRESERVER INFLATING ASSEMBLY, MA-1 |
| MIL-B-55252 Revision B:1992 | Batteries, Non-Rechargeable, Magnesium (No S/S Document) |
| 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 | Indicator, Rate of Flow, 0-5,000 PPH, Integrally Lighted (No S/S Document) |
| MIL-P-38268 Revision C:1988 | AURAL PROTECTORS, SOUND (S/S BY A-A-58084) |
| MIL-V-47311 Base Document:1989 | VALVE, PNEUMATIC EXHAUST (NO S/S DOCUMENT) |
| MIL-STD-490 Revision A:1985 | SpecificationPractices (S/S by MIL-STD-961) |
| 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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