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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR
Available format(s)
PDF
Superseded date
30-06-1998
Superseded by
Publisher
| Committee |
FSC MISC
|
| 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 J NOTICE 2 - Notice of Cancellation/Superseded by NASM 33540.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Superseded
|
| SupersededBy |
| 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 |
| JSGS-87231 Revision A:1995 | ENGINES, AIRCRAFT, TURBINE |
| 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 |
| MIL-STD-7080 Base Document:1994 | SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
| DOD-E-83578 Revision A:1987 | EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) |
| 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 BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL-HDBK-2193 Base Document:1994 | HYDRAULIC SYSTEM COMPONENTS, SHIP |
| MIL-STD-35-73 Base Document:1974 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, ACTUATORS, ELECTROMECHANICAL, LINEAR |
| 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 |
| 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 REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-P-5994 Revision D:1972 | PUMP, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY, GENERAL SPECIFICATION FOR |
| 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 |
| MIL-S-87233 Base Document:1985 | SUPPORT EQUIPMENT SYSTEMS (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
| 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-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) |
| MIL-A-6425 Revision B:1959 | ADAPTOR, PRESSURE FUEL SERVICING, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-R-19750 Revision A:1958 | REGULATOR; VOLTAGE, 28 V, 120 DEGREE C, FOR 30 V DIRECT-CURRENT GENERATOR, GENERAL SPECIFICATION FOR |
| MIL-I-8673 Base Document:1955 | INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
| 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 |
| IPC HDBK 630 : 0 | GUIDELINES FOR DESIGN, MANUFACTURE, INSPECTION AND TESTING OF ELECTRONIC ENCLOSURES ASSEMBLY |
| 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 | RESOLVERS, ELECTRICAL, AC FOR USE IN POLARIS FLEET BALLISTIC MISSILE WEAPON SYSTEM GENERAL SPECIFICATION FOR |
| 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 |
| 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 |
| MIL-P-85034 Base Document:1976 | POWER PACKAGE, EMERGENCY AC/DC GENERATOR, RAM AIR TURBINE DRIVEN |
| 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 |
| NASM20995:2012 | WIRE, SAFETY OR LOCK |
| 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 [ASG] |
| 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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