| Part Number: VCT23-36-6A | Manufacturer: General Dynamics Global Imaging |
| NSN : 5990-00-847-3806 (5990008473806) | Item Name : synchro control transformer |
| CAGE Code: 10112 | FSC : 5990 Synchros and Resolvers |
| Alternate P/N : VCT23366A | INC Code: 15289 |
| NIIN : 00-847-3806 (008473806) | FSG : 59 Electrical and Electronic Equipment Components |
| Country: USA | NCB Code: 00 |
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5990-00-847-3806 Item Description: SYNCHRO,CONTROL TRANSFORMER | 5990 | 008473806 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | U | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| VCT23/36-6A | 1 | 1 | C | A |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAFZ | BODY MATERIAL | STEEL, STAINLESS |
| AAQL | BODY STYLE | STANDARD ROUND D |
| AAVH | SHOULDER DIAMETER | 1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM |
| AAVL | PILOT DIAMETER | 0.5900 INCHES MINIMUM AND 0.6000 INCHES MAXIMUM |
| AAZW | SECOND SHOULDER DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
| AAZX | SECOND SHOULDER LENGTH | 0.1680 INCHES MINIMUM AND 0.1700 INCHES MAXIMUM |
| ABKK | FLANGE DIAMETER | 2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM |
| ABKU | FLANGE THICKNESS | 0.2480 INCHES MINIMUM AND 0.2500 INCHES MAXIMUM |
| ABPM | BODY DIAMETER | 1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM |
| ABXF | SHAFT LENGTH | 0.7190 INCHES MAXIMUM SINGLE SHAFT |
| AFJN | FRAGILITY FACTOR | MODERATELY RUGGED |
| AHCG | MAXIMUM TEMP RISE | 45.0 DEG CELSIUS |
| AJSN | STATOR INPUT VOLTAGE RATING IN VOLTS | 90.0 NOMINAL |
| AJSP | STATOR INPUT CURRENT RATING | 20.0 MILLIAMPERES NOMINAL |
| AJSS | FREQUENCY IN HERTZ | 60.0 NOMINAL |
| AJSY | ZSO RESISTANCE IN OHMS | 492.00 NOMINAL |
| AJVG | MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 60.00 OUTPUT |
| AJVH | MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 75.00 |
| AJVL | ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -6.0/+6.0 |
| AJVS | ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 0.50 INCH-OUNCES MAXIMUM |
| AJVW | ALIGNMENT HOLE QUANTITY | 3 |
| AJWQ | PILOT LENGTH | 0.0360 INCHES MINIMUM AND 0.0460 INCHES MAXIMUM |
| AJWV | AFT OF FIRST FLANGE DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
| AJXA | SPLINE TOOTH DIAMETRAL PITCH | 96 SINGLE SHAFT |
| AKAF | SHAFT THREAD DIRECTION | RIGHT-HAND SINGLE SHAFT |
| AKAN | SHAFT THREAD CLASS | 2A |
| CQTM | TERMINAL LOCATION | REAR |
| CQWQ | SHAFT THREAD LENGTH | 0.2660 INCHES NOMINAL SINGLE SHAFT |
| CQXQ | PLUS J ZRO REACTANCE IN OHMS | 2746.00 NOMINAL |
| CRKL | PLUS J ZRS REACTANCE IN OHMS | 81.00 NOMINAL |
| CRSJ | SHAFT TYPE | SPLINE W/THREADS SINGLE SHAFT |
| CRSY | ALIGNMENT HOLE DEPTH | 0.1250 INCHES NOMINAL |
| CTCW | ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 1.6420 INCHES NOMINAL |
| CWBH | SHAFT NOMINAL THREAD SIZE | 0.250 INCHES SINGLE SHAFT |
| TEST | TEST DATA DOCUMENT | 81349-MIL-20708 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING |
| TTQY | TERMINAL TYPE AND QUANTITY | 5 SCREW |
| ZZZK | SPECIFICATION/STANDARD DATA | 81349-MIL-S-20708/94 GOVERNMENT SPECIFICATION |
| ABHP | OVERALL LENGTH | 4.2940 INCHES NOMINAL |
| ABWV | SHAFT DIAMETER | 0.2402 INCHES MINIMUM SINGLE SHAFT AND 0.2405 INCHES MAXIMUM SINGLE SHAFT |
| AJSL | BODY SIZE | 23 |
| AJSQ | STATOR INPUT ELECTRICAL POWER RATING | 500.0 MILLIWATTS NOMINAL |
| AJSW | ZRO RESISTANCE IN OHMS | 1015.00 NOMINAL |
| AJTA | ZRS RESISTANCE IN OHMS | 239.00 NOMINAL |
| AJVM | SPLINE TOOTH QUANTITY | 22 SINGLE SHAFT |
| AJVT | ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.20 INCH-OUNCES MAXIMUM |
| AJWR | SHOULDER LENGTH | 0.2500 INCHES NOMINAL |
| AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 3.4450 INCHES MAXIMUM |
| AJYY | SHAFT THREAD SERIES DESIGNATOR | UNF SINGLE SHAFT |
| CRGZ | PLUS J ZSO REACTANCE IN OHMS | 4027.00 NOMINAL |
| CSJY | TRANSFORMATION RATIO | 0.735 ROTOR TO STATOR NOMINAL |
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