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  • MIL C 6021 : H NOTICE 1

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    CASTINGS, CLASSIFICATION AND INSPECTION OF

    Available format(s): 

    Superseded date:  26-03-1985

    Language(s): 

    Published date:  12-01-2013

    Publisher:  US Military Specs/Standards/Handbooks

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    Development Note Supersedes NAS 507. (04/2005)
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Superseded
    Superseded By
    Supersedes

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

    MIL-S-26547 Revision C:1985 STARTER-GENERATOR ENGINE STU-6A
    MIL-F-63428 Base Document:1981 FEED ASSEMBLY, AMMO FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2
    MIL-E-23001 Revision B:1976 ELECTRIC GENERATING SYSTEM, VARIABLE SPEED CONSTANT FREQUENCY, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL T 6396 : E TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING
    MIL-W-63328 Base Document:1979 WARHEAD GM, HE, M248 INERT PARTS FOR
    MIL-Q-45970 Revision A:1975 QUALITY ASSURANCE FOR WEAPONS AND SUPPORT MATERIAL
    MIL-S-22141 Revision B:1976 STEEL, INVESTMENT CASTINGS ALLOY AND CARBON
    MIL-A-23121 Revision C:1970 AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR
    MIL-A-81973 Base Document:1974 AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR
    MIL F 9490 : D FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-W-63150 Base Document:1977 WEAPONS AND SUPPORT MATERIAL STANDARD QUALITY ASSURANCE PROVISIONS FOR
    MIL-STD-2156 Base Document:1983 LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR
    MIL F 16377 : G FIXTURE, LIGHTING, INCANDESCENT, GENERAL LIGHTING 100 WATTS, 120 VOLTS, DRIPPROOF 15 DEGREES, SYMBOLS 89 & 90.2
    MIL-A-19736 Revision A:1960 AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR
    QQ-A-596 Revision E:1981 ALUMINUM ALLOY PERMANENT AND SEMI-PERMANENT MOLD CASTINGS
    MIL S 867 : A STEEL CASTING, CORROSION RESISTING AUSTENITIC
    MIL V 7899 : C VALVE, CHECK, AIRCRAFT FUEL SYSTEM
    MIL S 25057 : B SCREEN SYSTEM, AIR INLET, AIRCRAFT TURBINE ENGINE, GENERAL SPECIFICATION FOR
    MIL-B-81365 Base Document:1966 BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR
    MIL-S-8512 Revision D:1974 SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF
    MIL L 38671 : A LUG, SUSPENSION, BOMB MAU-129/A, "T" TYPE
    MIL-S-83427 Base Document:1974 SURVIVAL KIT CONTAINERS, CNU-129(V)/P AND CNU-130/P
    MIL-STD-789 Revision C:1983 CONTRACTOR TECHNICAL INFORMATION CODING OF REPLENISHMENT PARTS
    MIL-S-48303 Base Document:1973 SWITCH ASSEMBLY. M167
    MIL-S-85510 Base Document:1981
    MIL L 24560 : 0 LIGHTS AND GLASSWARE FOR NAVIGATION, SIGNAL AND WARNING, NAVAL SHIPBOARD USE, GENERAL SPECIFICATION FOR
    MIL E 24021 : J NOTICE 1 ELECTRIC POWER MONITORS, EXTERNAL, AIRCRAFT
    MIL-P-45971 Base Document:1975 PRODUCT ENGINEERING QUALITY ENGINEERING SYSTEM (PEQES) FOR WEAPONS AND SUPPORT MATERIAL
    SAE AMS 5348 : 2017 STEEL CASTINGS, TUBULAR, CENTRIFUGAL, CORROSION RESISTANT, 15CR - 4.6NI - 0.22 (CB+TA) - 2.8CU, SOLUTION HEAT TREATED
    MIL-P-5238 Revision C:1974 PUMP, CENTRIFUGAL, FUEL BOOSTER, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL G 6162 : B GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION
    JSSG-2006 Base Document:1998 JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
    MIL H 24653 : 0 HASP, HIGH SECURITY, SHROUDED FOR SHIPBOARD DOORS AND HATCHES USING HIGH AND MEDIUM SECURITY PADLOCK
    MIL-S-58095 Revision A:1986 SEAT SYSTEM: CRASH RESISTANCE, NON-EJECTION, AIRCREW, GENERAL SPECIFICATION FOR
    MIL-B-87167 Base Document:1985 BELT, AIRCRAFT SAFETY, HBU-12/A
    MIL-I-83751 Base Document:1967 INDICATOR, SAFETY LEVEL, RF
    MIL-A-25896 Revision E:1983 ADAPTER, PRESSURE FUEL SERVICING, NOMINAL 2.5 INCH DIAMETER
    MIL-E-85583 Revision A:1987 ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-P-83126 Revision A:1980 PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR
    MIL-S-38399 Revision A:1975 STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR
    MIL-D-63516 Base Document:1981 DRIVE ASSEMBLY, GUN FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2
    MIL-F-8615 Revision D:1976 FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG]
    MIL-S-7470 Revision A:1975 SHAFT, POWER TRANSMISSION, AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR
    MIL-S-63429 Base Document:1981 SLIDER ASSEMBLY FOR ARMAMENT SUBSYSTEM, HELICOPTER 20MM, M97E1 AND M97E2
    MIL-W-18326 Revision A:1956 WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR
    MIL-R-46509 Revision A:1982 ROCKET MOTOR, XM30, METAL PARTS FOR
    MIL-P-85315 Base Document:1979 Pump, Ejector, Air Vehicle Fuel, General Specification For
    NASA MSFC STD 506 : 1988 MATERIALS AND PROCESSES CONTROL
    DOD-C-85050 Base Document:1982 CHARGERS, BATTERY, NICKEL-CADMIUM, AIRCRAFT, GENERAL SPECIFICATION FOR
    QQ-A-601 Revision F:1981 ALUMINUM ALLOY SAND CASTINGS
    MIL-A-81724 Base Document:1969 ADAPTER, LAUNCHER, AIRCRAFT, ADU-299/E
    SAE AMS S 22141 : 1998 STEEL, INVESTMENT CASTINGS - ALLOY AND CARBON
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