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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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CASTINGS, CLASSIFICATION AND INSPECTION OF
Published date
12-01-2013
Publisher
Superseded date
26-03-1985
Superseded by
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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Superseded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 (No S/S Document) |
| SAE AMSS22141A | Steel, Investment Castings Alloy and Carbon |
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