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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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
Superseded date
26-03-1985
Superseded by
Published date
12-01-2013
Publisher
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| DevelopmentNote |
Supersedes NAS 507. (04/2005)
|
| DocumentType |
Standard
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| 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 | 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 WEAPONS AND SUPPORT MATERIAL |
| 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 | 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 AMSS22141A | Steel, Investment Castings Alloy and Carbon |
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