MS33540 Revision J:1986

Superseded

View Superseded by

SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR

Available format(s)

PDF

Superseded date

30-06-1998

Publisher

US Military Specs/Standards/Handbooks

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 J NOTICE 2 - Notice of Cancellation/Superseded by NASM 33540.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Status	Superseded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	NASM33540:2003

SAE AS 8181 : 1997	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 ARP 1616 : 2017	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