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MIL-STD-970 Base Document:1987

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF (NO S/S DOCUMENT)

Available format(s)

PDF

Published date

10-01-1987

Withdrawn date

10-18-1994

US$20.00
Excluding Tax where applicable

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
Pages
14
PublisherName
US Military Specs/Standards/Handbooks
Status
Withdrawn
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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