MIL-STD-1523 Revision A:1984
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIAL
Available format(s)
PDF
Superseded date
30-01-1995
Superseded by
Publisher
Outlines the maximum ages of age sensitive elastomeric items used in military missiles and aircraft and for space vehicles.
DocumentType |
Standard
|
Pages |
12
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
Superseded
|
SupersededBy |
DOD-STD-35-24 Revision A:1978 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, BEARINGS |
MIL-A-17161 Revision D:1985 | ABSORBER, RADIO FREQUENCY RADIATION (MICROWAVE ABSORBING MATERIAL), GENERAL SPECIFICATION FOR |
MIL-C-8605 Revision B:1990 | CAP, PRESSURE FUEL SERVICING |
MIL H 8790 : D | HOSE ASSEMBLY, RUBBER HYDRAULIC HIGH PRESSURE [3,000 PSI] |
MIL H 27516 : D | HOSE AND HOSE ASSEMBLY, NON-METALLIC, SUCTION AND DISCHARGE |
MIL-I-38338 Revision D:1991 | INDICATOR, OIL QUANTITY, CONTINUOUS TRANSMISSION, NUCLEONIC |
MIL-V-81356 Revision B:1992 | VALVE, FUEL SYSTEM PRESSURIZATION AND VENT |
DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-HDBK-1587 Base Document:1996 | MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM |
DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-C-85521 Base Document:1983 | Concentrator, Oxygen, GGU-7/A |
DOD-STD-35-20 Revision C:1986 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, FITTINGS AND COUPLINGS |
MIL H 83796 : 0 | HOSE ASSEMBLY, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
MIL-R-8931 Revision A:1994 | RESERVOIRS, AIRCRAFT AND MISSILE, HYDRAULIC SEPARATED TYPE |
MIL-H-4495 Revision D:1985 | HOSE ASSEMBLY, RUBBER, AERIAL REFUELING |
MIL S 25057 : B | SCREEN SYSTEM, AIR INLET, AIRCRAFT TURBINE ENGINE, GENERAL SPECIFICATION FOR |
DOD-STD-35-36 Revision B:1979 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM SEALS, GASKETS AND PACKING |
MIL H 5593 : C | HOSE, AIRCRAFT, LOW-PRESSURE, FLEXIBLE |
MIL-C-38373 Revision B:1975 | CAP, FLUID TANK FILLER |
MIL-S-8812 Revision D:1975 | STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
DOD-STD-35-46 Revision B:1986 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, VALVES (POWERED) |
MIL-V-8610 Revision B:1984 | VALVE, FUEL SHUTOFF SOLENOID OPERATED, 28 VOLT, DC |
MIL H 6000 : B | HOSE, RUBBER [FUEL, OIL, COOLANT, WATER AND ALCOHOL] |
MIL-M-85522 Revision A:1991 | MONITOR, OXYGEN CRU-91/A |
MIL-F-85596 Base Document:1983 | FIN, RETARDER, AIR INFLATABLE BSU-85/B |
MIL-STD-1547 Revision B:1992 | ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE VEHICLES |
SAE AS 5316 : 2017 | STORAGE OF ELASTOMER SEALS AND SEAL ASSEMBLIES WHICH INCLUDE AN ELASTOMER ELEMENT PRIOR TO HARDWARE ASSEMBLY |
MIL H 8795 : D | HOSE ASSEMBLY, RUBBER HYDRAULIC, FUEL AND OIL RESISTANT |
MIL-HDBK-692 Revision B:1983 | A Guide to the Selection of Rubber O-Rings |
SAE AS708B | TOP VISUAL QUALITY (TVQ) O-RING PACKINGS AND GASKETS - SURFACE INSPECTION GUIDE AND ACCEPTANCE STANDARD |
IPC HDBK 630 : 0 | GUIDELINES FOR DESIGN, MANUFACTURE, INSPECTION AND TESTING OF ELECTRONIC ENCLOSURES ASSEMBLY |
MIL C 25478 : B | COOLER, LUBRICATING OIL, AIRCRAFT ENGINE, SYNTHETIC OIL, GENERAL SPECIFICATION FOR |
MIL-A-25896 Revision E:1983 | ADAPTER, PRESSURE FUEL SERVICING, NOMINAL 2.5 INCH DIAMETER |
MIL H 7061 : B | HOSE, RUBBER, AIRCRAFT, SELF SEALING, AROMATIC FUEL |
MIL-P-85573 Base Document:1983 | POWER UNIT AIRCRAFT AUXILIARY, GAS TURBINE, GENERAL SPECIFICATION FOR |
SAE AIR797E | HOSE CHARACTERISTICS AND SELECTION CHART |
MIL-S-38399 Revision A:1975 | STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR |
MIL-F-8615 Revision D:1976 | FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
MIL-R-3065 Revision E:1984 | RUBBER, FABRICATED PRODUCT |
MIL-P-87210 Base Document:1984 | PNEUMATIC POWER SYSTEMS, HIGH PRESSURE |
MIL H 13444 : E | HOSE & HOSE ASSEMBLIES, RUBBER: FUEL AND OIL |
MIL A 5498 : D | ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
MIL F 81836 : A SUPP 1 | FILTER AND DISPOSABLE ELEMENT, FLUID PRESSURE, HYDRAULIC, 3 MICRON ABSOLUTE |
DOD-STD-35-121 Base Document:1978 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, EYELETS, FERRULES, AND GROMMETS |
SAE AIR1364A | AGE CONTROL OF AGE SENSITIVE ELASTOMERIC MATERIALS |
MIL-P-85315 Base Document:1979 | Pump, Ejector, Air Vehicle Fuel, General Specification For |
MIL-V-62381 Revision A:1985 | VALVE, SOLENOID OPERATED |
MIL M 62361 : C | MOTOR, DRIVE, DIRECT CURRENT 2 RPM/8RPM |
MIL D 83753 : NOTICE 2 | DISPENSER, BOMB, TYPE SUU-21/A |
MIL M 62368 : A | MOTOR, GEARHEAD, 18-30 VOLTS, DIRECT CURRENT |
MIL H 83797 : 0 | HOSE, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
MIL H 7061 : B | HOSE, RUBBER, AIRCRAFT, SELF SEALING, AROMATIC FUEL |
MIL H 6000 : B | HOSE, RUBBER [FUEL, OIL, COOLANT, WATER AND ALCOHOL] |
MIL-P-5315 Revision B:1964 | PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT |
MIL H 27516 : D | HOSE AND HOSE ASSEMBLY, NON-METALLIC, SUCTION AND DISCHARGE |
MIL H 8794 : D | HOSE, RUBBER, HYDRAULIC, FUEL AND OIL RESISTANT |
MIL R 6855 : E | RUBBER, SYNTHETIC, SHEETS, STRIPS, MOLDED OR EXTRUDED SHAPES |
MIL-H-7938 Revision A:1983 | HOSE, RUBBER, FLAME-RESISTANT |
MIL H 5593 : C | HOSE, AIRCRAFT, LOW-PRESSURE, FLEXIBLE |
MIL H 8790 : D | HOSE ASSEMBLY, RUBBER HYDRAULIC HIGH PRESSURE [3,000 PSI] |
MIL H 26521 : J | HOSE ASSEMBLY, NONMETALLIC, FUEL, COLLAPSIBLE, LOW TEMPERATURE WITH NON-REUSABLE COUPLINGS |
MIL H 8795 : D | HOSE ASSEMBLY, RUBBER HYDRAULIC, FUEL AND OIL RESISTANT |
MIL-P-83461 Revision B:1980 | PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, IMPROVED PERFORMANCE AT 275 DEGREES F (135 DEGREES C) |
MIL H 83796 : 0 | HOSE ASSEMBLY, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
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