MS20995 Revision E:1974
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
WIRE, SAFETY OR LOCK
Available format(s)
PDF
Superseded date
12-06-1998
Superseded by
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.| Committee |
FSC 9505
|
| DocumentType |
Standard
|
| Pages |
6
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| SAE AS8181A | Detector, Ice, Air Intake Duct, Aircraft Engines and Airframe Systems, General Specification For |
| MIL T 6396 : E | TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
| MIL-C-8605 Revision B:1990 | CAP, PRESSURE FUEL SERVICING |
| NASA KSC STD Z 0005 : 1988 | DESIGN OF PNEUMATIC GROUND-SUPPORT EQUIPMENT, STANDARD FOR |
| MIL M 62338 : A | MULTIPLE LAUNCH ROCKET SYSTEM (MLRS) XM993, PROCESSING FOR STORAGE AND SHIPMENT OF |
| MIL-V-81356 Revision B:1992 | VALVE, FUEL SYSTEM PRESSURIZATION AND VENT |
| MIL-C-19179 Revision B:1963 | COUPLING ASSEMBLY, QUICK-DISCONNECT, FUEL |
| MIL-STD-35-72 Base Document:1974 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, ACTUATORS, ELECTROMECHANICAL, ROTARY |
| MIL-HDBK-2193 Base Document:1994 | HYDRAULIC SYSTEM COMPONENTS, SHIP |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL-STD-35-73 Base Document:1974 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, ACTUATORS, ELECTROMECHANICAL, LINEAR |
| MIL-H-8775 Revision D:1976 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
| MIL V 5523 : D | VALVE, RELIEF, HYDRAULIC PRESSURE |
| MIL-C-24217 Revision A:1984 | CONNECTOR, ELECTRICAL, DEEP SUBMERGENCE, SUBMARINE |
| MIL-C-85049 Revision A:1990 | CONNECTOR ACCESSORIES, ELECTRICAL GENERAL SPECIFICATION FOR |
| MIL-A-19736 Revision A:1960 | AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-I-23870 Base Document:1963 | INDICATOR, FUEL RATE OF FLOW, 0 TO 15 GPM |
| MIL-H-8890 Base Document:1961 | HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG] |
| MIL-P-8564 Revision D:1970 | PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
| MIL-A-62019 Revision B:1969 | ARMORED RECONNAISSANCE/AIRBORNE ASSAULT VEHICLE: FULL-TRACKED, 152 MM, M551; PROCESSING FOR STORAGE AND SHIPMENT OF |
| MIL-C-38373 Revision B:1975 | CAP, FLUID TANK FILLER |
| SAE ARP1616B | Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel and Oil Systems |
| MIL-P-82436 Base Document:1966 | PUMP, FUEL |
| MIL-R-29565 Revision A:1990 | ROCKET MOTOR, MK 125 MOD 1 |
| MIL-A-23622 Base Document:1963 | ACTUATOR, AIRCRAFT, ELECTRO-MECHANICAL, LINEAR, DIRECT CURRENT |
| MIL C 24356 : A | COUPLING, SEGMENTED AND SPLIT CLAMPS REATTACHABLE, 2-1/2-, 4-, 6- AND 7- INCH, FOR REFUELING-AT-SEA HOSE |
| MIL-S-8710 Revision B:1969 | STRAINER, AIRFRAME FUEL SYSTEM, GENERAL SPECIFICATION FOR |
| MIL-A-6425 Revision B:1959 | ADAPTOR, PRESSURE FUEL SERVICING, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-V-8610 Revision B:1984 | VALVE, FUEL SHUTOFF SOLENOID OPERATED, 28 VOLT, DC |
| MIL C 22263 : B | COUPLING FUEL LINE, FLEXIBLE, 125 PSI, GENERAL SPECIFICATION FOR |
| MIL-P-24627 Base Document:1984 | PENETRATORS, BULKHEAD, CONNECTORIZED, FIBER OPTIC (FOR INBOARD USE ON NAVY SHIPS AND SUBMARINES) |
| 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-D-8181 Revision B:1965 | DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR |
| MIL-S-48405 Base Document:1973 | Shielded and Confined Mild Detonating Cord Assemblies |
| MIL-S-38399 Revision A:1975 | STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR |
| MIL-V-25023 Revision B:1967 | VALVE, FUEL DRAIN, SELF-LOCKING |
| MIL-S-21277 Revision A:1958 | SWITCH, LIQUID LEVEL, GENERAL SPECIFICATION FOR |
| MIL-S-7470 Revision A:1975 | SHAFT, POWER TRANSMISSION, AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR |
| MIL-N-25161 Revision C:1969 | NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
| MIL C 31031 : 0 | CONNECTORS, ELECTRICAL, PLUGS AND RECEPTACLES, COAXIAL, RADIO FREQUENCY, HIGH RELIABILITY, FOR FLEXIBLE AND SEMIRIGID CABLES GENERAL SPECIFICATION FOR |
| MIL-P-85315 Base Document:1979 | Pump, Ejector, Air Vehicle Fuel, General Specification For |
| MIL-F-5504 Revision B:1958 | Filters and Filter Elements, Fluid Pressure, Hydraulic Micronic Type |
| MIL-P-5315 Revision B:1964 | PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT |
| MIL C 25531 : D | COUPLING HALF, QUICK DISCONNECT, PNEUMATIC STARTER, EXTERNAL, LOW PRESSURE, DIRECT RELEASE |
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