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  • MIL-STD-970 Base Document:1987

    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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

    Available format(s):  PDF

    Withdrawn date:  18-10-1994

    Language(s): 

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    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.

    General Product Information - (Show below) - (Hide below)

    Committee AREA GDRQ
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Withdrawn
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    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 TRANSFORMER AND INDUCTORS [AUDIO, POWER AND HIGH POWER PULSE] INDUCTOR, POWER TF5S04ZZ
    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 AS 5944 : 1999 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 AS 53731 : 2014 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 AS 55151 : 2001 PUMP, HYDRAULIC, RAM, HAND DRIVEN
    SAE ARP 1616 : 2017 SELF-SEALING BREAKAWAY VALVES FOR CRASH-RESISTANT AIRCRAFT FUEL AND OIL SYSTEMS
    SAE AS 8700 : 1999 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

    Standards Referencing This Book - (Show below) - (Hide below)

    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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