MS33540 Revision J:1986
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR (S/S BY NASM33540)
Available format(s)
PDF
Published date
23-07-1986
Publisher
Superseded date
30-06-1998
€16.67
Excluding VAT
| DevelopmentNote |
J NOTICE 1 - Notice of Validation. J NOTICE 2 - Notice of Cancellation/Superseded by NASM 33540. (03/2010)
|
| DocumentType |
Standard
|
| Pages |
6
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SAE AS8181A | Detector, Ice, Air Intake Duct, Aircraft Engines and Airframe Systems, General Specification For |
| MIL-A-83577 Revision B:1988 | Assemblies, Moving Mechanical, for Space and Launch Vehicles, General Specification for (No S/S Document) |
| JSGS-87231 Revision A:1995 | Engines, Aircraft, Turbine (S/S by JSSG-2007) |
| MIL T 6396 : E | TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
| MIL-S-38399 Revision A:1975 | Starter, Pneumatic, Aircraft Engine General Specification For (No S/S Document) |
| MIL-STD-7080 Base Document:1994 | Selection and Installation of Aircraft Electric Equipment |
| DOD-E-83578 Revision A:1987 | EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) (NO S/S DOCUMENT) |
| 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 BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL-HDBK-2193 Base Document:1994 | Hydraulic System Components, Ship (S/S by MIL-STD-2193) |
| MIL-STD-35-73 Base Document:1974 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM ACTUATORS, ELECTROMECHANICAL, LINEAR (NO S/S DOCUMENT) |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| MIL-H-8775 Revision D:1976 | Hydraulic System Components, Aircraft and Missiles General Specification for (S/S by SAE-AS8775) |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL V 5523 : D | VALVE, RELIEF, HYDRAULIC PRESSURE |
| MIL-V-25023 Revision B:1967 | Valve, Fuel Drain, Self-Locking |
| MIL-A-19736 Revision A:1960 | Air Refueling Systems, General Specification for |
| MIL-P-5994 Revision D:1972 | Pump Units, Hydraulic, Electric Motor Driven, Variable Delivery, General Specification for (No S/S Document) |
| MIL G 26611 : D | GENERATOR, TACHOMETER GEU-7/A, MINIATURE |
| MIL-S-8512 Revision D:1974 | Support Equipment, Aeronautical, Special, General Specification for the Design of |
| MIL-E-7080 Revision B:1962 | Electric Equipment, Aircraft, Selection and Installation of (S/S by MIL-STD-7080) |
| MIL-S-87233 Base Document:1985 | SUPPORT EQUIPMENT SYSTEMS (S/S BY AFGS-87233) |
| 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-S-8710 Revision B:1969 | Strainer, Airframe Fuel System, General Specification for |
| DOD-STD-35-46 Revision B:1986 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM VALVES (POWERED) (NO S/S DOCUMENT) |
| MIL-A-6425 Revision B:1959 | Adapter, Pressure Fuel Servicing, Aircraft, General Specification for (S/S by MIL-A-25896) |
| MIL-R-19750 Revision A:1958 | REGULATOR; VOLTAGE, 28V, 120 DEG. C, FOR 30V DIRECT-CURRENT GENERATOR, GENERAL SPECIFICATION FOR (S/S BY MIL-R-23761) |
| MIL-I-8673 Base Document:1955 | Installation and Test of Aircraft Flexible Weapons Systems (No S/S Document) |
| MIL C 22263 : B | COUPLING FUEL LINE, FLEXIBLE, 125 PSI, GENERAL SPECIFICATION FOR |
| SAE ARP1616B | Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel and Oil Systems |
| NASA MSFC STD 486 : 1992 | STANDARD, THREADED FASTENERS, TORQUE LIMITS FOR |
| MIL G 6162 : B | GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION |
| MIL-A-23622 Base Document:1963 | Actuator, Aircraft, Electro-Mechanical, Linear, Direct Current |
| MIL D 62559 : LATEST | DISTRIBUTION BOX, VEHICLE |
| MIL-R-21530 Revision D:1962 | RESOLVER, ELECTRICAL, AC, FOR USE IN POLARIS FLEET BALLISTIC MISSILE WEAPON SYSTEM GENERAL SPECIFICATION FOR (NO S/S DOCUMENT) |
| MIL-A-25896 Revision E:1983 | Adapter, Pressure Fuel Servicing, Nominal 2.5-Inch Diameter |
| DOD-STD-35-117 Base Document:1978 | Automated Engineering Document Preparation System Switches, Pressure (No S/S Document) |
| DOD-E-8983 Revision C:1977 | ELECTRONIC EQUIPMENT, AEROSPACE, EXTENDED SPACE ENVIRONMENT, GENERAL SPECIFICATION FOR |
| 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-P-85034 Base Document:1976 | POWER PACKAGE, EMERGENCY AC/DC GENERATOR, RAM AIR TURBINE DRIVEN (NO S/S DOCUMENT) |
| MIL-S-48405 Base Document:1973 | Shielded and Confined Mild Detonating Cord Assemblies |
| MIL-P-85573 Base Document:1983 | POWER UNIT AIRCRAFT AUXILIARY, GAS TURBINE, GENERAL SPECIFICATION FOR |
| MIL-T-26609 Revision C:1994 | Transmitter, Position |
| 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-B-18558 Revision B:1988 | Bearing, Propulsion Line Shaft, Oil Disc Lubricated |
| MIL G 5413 : D NOTICE 1 | GENERATOR, TACHOMETER, FOUR POLE |
| MIL-T-5583 Revision C:1987 | Transmitter, Position, 28 Volts DC |
| MIL-M-7969 Revision C:1965 | Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for |
| MIL-I-8672 Revision B:1969 | Installation and Test of Aircraft Pyrotechnic Equipment in Aircraft, General Specification for (No S/S Document) |
| MIL G 21480 : A | GENERATOR SYSTEM, 400 HERTZ ALTERNATING CURRENT, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL G 9398 : C | GENERATOR, TACHOMETER, TWO POLE HIGH TEMPERATURE AIRCRAFT |
| MIL C 25531 : D | COUPLING HALF, QUICK DISCONNECT, PNEUMATIC STARTER, EXTERNAL, LOW PRESSURE, DIRECT RELEASE |
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