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MIL C 6021 : H NOTICE 1

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

CASTINGS, CLASSIFICATION AND INSPECTION OF

Published date

12-01-2013

Superseded date

26-03-1985

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DevelopmentNote
Supersedes NAS 507. (04/2005)
DocumentType
Standard
PublisherName
US Military Specs/Standards/Handbooks
Status
Superseded
SupersededBy

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 (S/S by MIL-E-85583)
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 (S/S BY MIL-W-63150)
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 (No S/S Document)
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 (No S/S Document)
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 Materiel 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 Refueling Systems, General Specification for
QQ-A-596 Revision E:1981 Aluminum Alloy Permanent and Semipermanent Mold Castings (S/S by ASTM-B108)
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 Specification 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 (NO S/S DOCUMENT)
MIL-S-85510 Base Document:1981 Seats, Helicopter Cabin, Crashworthy, General Specification for
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 Weaponsand Support Materiel (No S/S Document)
SAE AMS5348C 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 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 RESISTANT, NON-EJECTION, AIRCREW, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT)
MIL-B-87167 Base Document:1985 BELT, AIRCRAFT SAFETY, HBU-12/A
MIL-I-83751 Base Document:1967 Indicator, Safety Level, RF (No S/S Document)
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 (No S/S Document)
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 (S/S by SAE-ARP8615)
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 (S/S BY MIL-STD-2219)
MIL-R-46509 Revision A:1982 ROCKET MOTOR, M30, METAL PARTS FOR (NO S/S DOCUMENT)
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 Charger, Battery, Nickel-Cadmium, Aircraft General Specification for (No S/S Document)
QQ-A-601 Revision F:1981 Aluminum Alloy Sand Castings (S/S by ASTM-B26/B26M)
MIL-A-81724 Base Document:1969 Adapter, Launcher, Aircraft, ADU-299/E
SAE AMSS22141A Steel, Investment Castings Alloy and Carbon

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