MS33678 Revision A:2004
Current
Current
The latest, up-to-date edition.
Connector, Receptacle, Electric, Integral Mounting
Available format(s)
PDF
Published date
07-09-2004
Publisher
US$20.00
Excluding Tax where applicable
| DevelopmentNote |
A NOTICE 1 - Notice of Validation. (05/2009)
|
| DocumentType |
Standard
|
| Pages |
7
|
| ProductNote |
NEW CHILD NOT 2 2019 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| MIL-I-27674 Revision C:1994 | Indicator, Temperature, Electrical Resistance (No S/S Document) |
| MIL-I-8580 Revision B:1965 | Indicator, Tachometer, Helicopter, 0-4000 RPM, Type MA-1 (No S/S Document) |
| MIL-I-7065 Revision A:1976 | Indicator, Position, Aileron Trim Tab |
| MIL-I-38121 Revision C:1989 | Indicator, Pressure, EGU-9A (No S/S Document) |
| MIL I 25688 : A | INDICATOR, ELECTRICAL TACHOMETER ERU-3/A. CRANKSHAFT SPEED 500-4,000 RPM, 3 1/4 INCH SIZE |
| MIL-DTL-27188 Revision C:2006 | Indicator, Pressure EGU-2/A, Oil, 0-100 PSI |
| MIL-G-25597 Revision D:1973 | Gyroscope, Displacement, Roll and Pitch, Type MD-1 |
| MIL-I-83262-1 Revision A:1987 | Indicator, Temperature, Thermocouple EHU-31A/A (No S/S Document) |
| MIL I 7231 : B | INDICATOR, TRUE AIRSPEED, SYNCHRO REPEATER TYPE N 1 |
| SAE ARP843A | Chip Detector, Electrical Connection, Remote Indicating |
| MIL-I-27202 Revision A:1980 | Indicator, Electrical Tachometer, 0-110 Percent RPM 2-Inch Size, Integrally Lighted |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL-STD-1353 Revision C:2014 | Electrical Connectors, Plug-in Sockets and Associated Hardware, Selection and Use of |
| MIL-DTL-27723 Revision F:2013 | Probe, Total Temperature, Deiceable |
| MIL-DTL-28827-1 Revision C:2011 | Switch, Thermostatic (Volatile Liquid), Hermetic Sealed, Single Pole Double Throw (SPDT), Medium Response Time |
| MIL-G-83872 Revision A:1977 | Gyroscope, Displacement, Type SBU-23/A |
| MIL-T-38049 Revision A:1972 | TRANSMITTER, PRESSURE TRU-60-A (NO S/S DOCUMENT) |
| MIL I 38120 : A (3) | INDICATOR, RATE OF FLOW AND TRANSFER EFU 20/A |
| MIL G 26611 : D | GENERATOR, TACHOMETER GEU-7/A, MINIATURE |
| MIL-I-5133 Revision C:1953 | Indicator, Attitude, Type J-8 (No S/S Document) |
| MIL I 7077 : B | INDICATOR, TEMPERATURE ELECTRICAL RESISTANCE, MULTIFUNCTION -70 DEG TO PLUS 150 DEG. C 2 INCH SIZE |
| MIL I 25689 : A NOTICE 1 | INDICATOR, ELECTRICAL TACHOMETER |
| MIL-I-25325 Revision A:1961 | Indicator, Rate of Flow, Fuel, Totalizing, 0-100,000 PPH, Type MA-8 |
| MIL T 5350 : E | TRANSMITTER, SYNCHRO OPERATED, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-I-25863 Revision D:1990 | Indicator, Electrical Tachometer 0-110 Percent RPM, 2 Inch Size, Integrally Lighted |
| MIL-I-6533 Revision B:1970 | Indicator, Temperature, Electrical Resistance Multi-Function, Type G-10 |
| MIL I 6839 : C | INDICATOR, POSITION, LANDING GEAR |
| MIL-I-5482 Revision C:1960 | Indicator, Pressure, Synchro, Aircraft, 165 Degree Scale (No S/S Document) |
| MIL-DTL-83361 Revision B:2007 | Indicator, Pressure, Oil, Dual, 0-100 PSI, EGU-18/A |
| MIL I 25725 : A | INDICATOR, TORQUE PRESSURE, MAGNESYN STYLE, SINGLE CLAMP MOUNTED, 2 IN SIZE, 50-400 PSI TYPE A-8 |
| MIL-DTL-38394 Revision E:2009 | Transmitter, Pressure TRU-81/A, Oil, 0-500 PSI |
| MIL-DTL-5790 Revision H:2008 | Transmitter, Pressure, Oil, Synchro, 0-200 PSI 320-Degree Movement, 26V, Single Phase, 400 Cycles |
| MIL-P-38027 Revision A:1973 | PRESSURE INDICATING SYSTEM, HYDRAULIC A/A27J-1 (S/S BY MIL-I-27190 AND MS28005) |
| MIL I 8136 : A | INDICATOR, FUEL FLOW RATE, SYNCHRO STYLE, SINGLE CLAMP MOUNTED 2 INCH SIZE 300 TO 3,000 PPH TYPE A 12 |
| MIL-PRF-25435 Revision D:2008 | Transmitters, Pressure, Aircraft 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-I-27665 Revision B:1984 | Indicator, Temperature, Electrical Resistance, Minus 50 Degrees to Plus 50 Degrees C |
| SAE AS8181A | Detector, Ice, Air Intake Duct, Aircraft Engines and Airframe Systems, General Specification For |
| MIL-I-27247 Revision C:1985 | Indicator, Temperature, Synchro |
| MIL-I-38391 Base Document:1965 | Indicator, Electrical Tachometer, ERU-12/A 0-350 RPM (Rotor), 0-7000 RPM (Engine) (No S/S Document) |
| MIL I 7491 : B | INDICATOR RATE OF FLOW, FUEL TOTALIZING, SERVO STYLE, TYPE F 1 |
| SAE AS50151C | Connectors, Electrical, Circular Threaded, AN Type, General Specification For |
| MIL-I-25130 Revision B:1974 | Indicator, Pressure, Oil, 0-300 PSI, Type MO-1 (No S/S Document) |
| MIL-I-25479 Revision A:1987 | Indicator, Mach Number, Sensitive, Servoed, Range .5 to 1.0, Type ME-5 (No S/S Document) |
| MIL-I-27552 Revision C:1995 | Indicator, Temperature, Thermocouple EHU-15A/A, Potentiometer Type, White Lighted |
| MIL-I-25482 Revision D:1993 | Indicator, Engine Testing |
| MIL-W-18326 Revision A:1956 | WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR (S/S BY MIL-STD-2219) |
| MIL-I-25859 Revision C:1995 | Indicator, Thrust AEU-2/A, Synchro Style, Pressure Ratio, 1.2-3.4 Units, Integrally Lighted (No S/S Document) |
| MIL-I-83245 Revision A:1994 | Indicator Set, Oil Pressure A/A24J-17 (No S/S Document) |
| MIL-I-27673 Revision C:1993 | Indicator, True Airspeed AVU-15/A |
| MIL-I-5914 Revision E:1993 | Indicator, Rate of Flow, Fuel, Type EFU-24/A and Type EFU-25/A (No S/S Document) |
| MIL-I-7087 Revision A:1968 | Indicator, Pressure, Oil, 0-200 PSI |
| MIL-T-25485 Revision C:1974 | Transmitter, Thrust, Single Synchro Style, Pressure Ratio, Type MK-2 (No S/S Document) |
| MIL-I-25941 Revision D:1986 | Indicator, Turn and Slip, 2- Inch Size, Integrally Lighted |
| MIL-I-7084 Revision A:1988 | Indicator, Pressure, Hydraulic, 0-4,000 PSI |
| MIL-T-7258 Revision B:1985 | Transmitter, Temperature, Electrical Resistance, Type B-4 |
| MIL T 25435 : B | TRANSMITTER, PRESSURE, AIRCRAFT, VARIABLE RELUCTANCE TYPE, GENERAL SPECIFICATION FOR |
| MIL-DTL-7077 Revision D:2011 | Indicator, Temperature, Electrical Resistance, Multifunction, -70 Degrees C to 150 Degrees C, 2-Inch Size |
| MIL-T-5583 Revision C:1987 | Transmitter, Position, 28 Volts DC |
| MIL-T-25307 Revision D:1985 | Transmitter, Pressure, Hydraulic, Type MJ-1 |
| MIL-I-25437 Revision B:1984 | Indicator, Aircraft, Pressure, Voltage Ratio Type, General Specification for |
| MIL-I-7075 Revision A:1965 | Indicator, Temperature, Electrical Resistance, Multifunction, -50 Degrees to +50 Degrees C, 2-Inch Size |
| MIL-T-8249 Revision B:1979 | Transmitter, Rate of Flow, Fuel, Type MB-2 |
| MIL-I-27667 Revision C:1990 | Indicator, Temperature, Electrical Resistance |
| MIL I 83361 : (4) | INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
| MIL-DTL-5015 Revision H:2000 | Connectors, Electrical, Circular Threaded, AN Type, General Specification for (S/S by SAE-AS50151) |
| MIL-STD-1651 Revision B:2015 | Insert Arrangements for SAE-AS50151, MIL-DTL-22992 (Classes C, J, and R), MIL-DTL-83723 (Series II), and SAE-AS95234 Circular Electrical Connectors |
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