Welcome to the NSN RFQ page on Cosmos Purchasing; from here, you may request a competitive sourcing solution for any parts of interest. As a dependable NSN part in our inventory of Synchro Control Transformer items, this component with part number HTC-11-F-8 B887 and NSN 5990000619041 is available for purchase at any time. This product is manufactured by Moog Inc, a trusted entity on our Approved Vendor List (AVL) who upholds a strict level of quality assurance in their practices. They are also a part of a larger supply network that reaches across the globe to enable expedited shipping for our customers wherever they are located.
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Having been given the CAGE Code 99932, Moog Inc follows the strict guidelines for part standardization established by the US Department of Defense. If you would like to explore similar products, we invite you to return to our page of 5990 Synchros and Resolvers products or look at the list of related items below. Start the purchasing process on part number HTC-11-F-8 B887 and any other items of interest today to learn all that Cosmos Purchasing can do as your sourcing partner!
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5990-00-061-9041 Item PartTypeName: SYNCHRO,CONTROL TRANSFORMER | 5990 | 000619041 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | U | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 101A2T5 | 3 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAFZ | BODY MATERIAL | STEEL,STAINLESS |
| AAQL | BODY STYLE | STANDARD ROUND B |
| AAVH | SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| AAVL | PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6252 INCHES MAXIMUM |
| ABHP | OVERALL LENGTH | 2.3420 INCHES MINIMUM AND 2.3740 INCHES MAXIMUM |
| ABKK | FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| ABKU | FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| ABPC | UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| ABWV | SHAFT DIAMETER | 0.1195 INCHES MINIMUM SINGLE SHAFT AND 0.1200 INCHES MAXIMUM SINGLE SHAFT |
| ABXF | SHAFT LENGTH | 0.5630 INCHES NOMINAL SINGLE SHAFT |
| AFJN | FRAGILITY FACTOR | MODERATELY RUGGED |
| AJSL | BODY SIZE | 11 |
| AJSN | STATOR INPUT VOLTAGE RATING IN VOLTS | 78.0 NOMINAL |
| AJSP | STATOR INPUT CURRENT RATING | 17.0 MILLIAMPERES NOMINAL |
| AJSQ | STATOR INPUT ELECTRICAL POWER RATING | 250.0 MILLIWATTS NOMINAL |
| AJSS | FREQUENCY IN HERTZ | 400.0 NOMINAL |
| AJSW | ZRO RESISTANCE IN OHMS | 707.00 NOMINAL |
| AJTA | ZRS RESISTANCE IN OHMS | 637.00 NOMINAL |
| AJTC | ZSS RESISTANCE IN OHMS | 876.00 NOMINAL |
| AJTS | ROTOR DC RESISTANCE IN OHMS | 370.00 NOMINAL |
| AJTT | STATOR DC RESISTANCE IN OHMS | 602.00 NOMINAL |
| AJVF | PHASE SHIFT ANGLE IN DEG | 3.400 INPUT TO OUTPUT NOMINAL |
| AJVG | MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 59.00 OUTPUT |
| AJVH | MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 94.00 |
| AJVL | ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -10.0/10.0 |
| AJVS | ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS NOMINAL |
| AJVT | ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
| AJVW | ALIGNMENT HOLE QUANTITY | 4 |
| AJWQ | PILOT LENGTH | 0.0620 INCHES NOMINAL |
| AJWR | SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7330 INCHES MINIMUM AND 1.7950 INCHES MAXIMUM |
| CQTM | TERMINAL LOCATION | REAR |
| CQXQ | PLUS J ZRO REACTANCE IN OHMS | 3194.00 NOMINAL |
| CQZS | SHAFT SLOT DEPTH | 0.0310 INCHES NOMINAL SINGLE SHAFT |
| CRHN | SHAFT SLOT WIDTH | 0.0310 INCHES NOMINAL SINGLE SHAFT |
| CRKL | PLUS J ZRS REACTANCE IN OHMS | 324.00 NOMINAL |
| CRSJ | SHAFT TYPE | ROUND,SLOTTED SINGLE SHAFT |
| CRSY | ALIGNMENT HOLE DEPTH | 0.0310 INCHES NOMINAL |
| CSFG | PLUS J ZSS REACTANCE IN OHMS | 4580.00 NOMINAL |
| CSJY | TRANSFORMATION RATIO | 0.735 ROTOR TO STATOR NOMINAL |
| CTCW | ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8120 INCHES NOMINAL |
| TTQY | TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
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