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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
WIRE, SAFETY OR LOCK (S/S BY NASM20995)
Available format(s)
PDF
Published date
17-09-1974
Publisher
Superseded date
12-06-1998
$31.16
Including GST where applicable
| DocumentType |
Standard
|
| Pages |
6
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| 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 (S/S by MIL-C-24788) |
| MIL-STD-35-72 Base Document:1974 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, ACTUATORS, ELECTRO-MECHANICAL, ROTARY (NO S/S DOCUMENT) |
| MIL-HDBK-2193 Base Document:1994 | Hydraulic System Components, Ship (S/S by MIL-STD-2193) |
| 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 (NO S/S DOCUMENT) |
| MIL-H-8775 Revision D:1976 | Hydraulic System Components, Aircraft and Missiles General Specification for (S/S by SAE-AS8775) |
| MIL V 5523 : D | VALVE, RELIEF, HYDRAULIC PRESSURE |
| MIL-C-24217 Revision A:1984 | Connectors, Electrical, Deep Submergence, Submarine |
| MIL-C-85049 Revision A:1990 | Connector Accessories, Electrical General Specification for (S/S by SAE-AS85049) |
| MIL-A-19736 Revision A:1960 | Air Refueling Systems, General Specification for |
| MIL-I-23870 Base Document:1963 | Indicator, Fuel Rate of Flow, 0 to 15 GPM (No S/S Document) |
| MIL-H-8890 Base Document:1961 | Hydraulic Components, Type III (-65 Degrees to Plus 450 Degrees F) General Specification for (ASG) |
| MIL-P-8564 Revision D:1970 | Pneumatic System Components, Aeronautical, General Specification for |
| MIL-A-62019 Revision B:1969 | Armored Reconnaissance/Airborne Assault Vehicle Full Tracked, 152MM, M551; Processing for Storage and Shipment of (See Notice 1 for Replacement Information) |
| MIL-C-38373 Revision B:1975 | Cap, Fluid Tank Filler (No S/S Document) |
| 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 | Adapter, Pressure Fuel Servicing, Aircraft, General Specification for (S/S by MIL-A-25896) |
| 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), GENERAL SPECIFICATION FOR (NO S/S DOCUMENT) |
| 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 (S/S by SAE-AS8181) |
| 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 (No S/S Document) |
| MIL-V-25023 Revision B:1967 | Valve, Fuel Drain, Self-Locking |
| MIL-S-21277 Revision A:1958 | SWITCHES, LIQUID LEVEL, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT) |
| 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 (S/S BY SAE-AMS-P-5315) |
| MIL C 25531 : D | COUPLING HALF, QUICK DISCONNECT, PNEUMATIC STARTER, EXTERNAL, LOW PRESSURE, DIRECT RELEASE |
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